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HIGHLIGHTS
Pages which have been revised are outlined below, together with the Highlights of the
Revision
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CH/SE/SU C REASON FOR CHANGE EFFECTIVITY
PAGES
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CHAPTER 53
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53-HIGHLIGHTS Page 1 of 1
REVISION NO. 57 May 01/08
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CHAPTER 53
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FUSELAGE
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TABLE OF CONTENTS
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SUBJECT ________
CH/SE/SU C
_ PAGE ___________
____ EFFECTIVITY
FUSELAGE - GENERAL
__________________ 53-00-00
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Component Location 2 ALL
Description 2 ALL
Nose Forward Fuselage (Ref. AMM 2 ALL
531100)
Forward Fuselage (Ref. AMM 6 ALL
532100)
Center Fuselage (Ref. AMM 6 ALL
533100)
Rear Fuselage (Ref. AMM 534100) 6 ALL
Cone/Rear Fuselage (Ref. AMM 7 ALL
535100)
___________________
FUSELAGE - GENERAL 53-00-00
INSPECTION/CHECK 601 ALL
Removal and Detailed Inspection of 601 ALL
the Piston-Type Drain Valves in
the Lower Fuselage Shell
_____________________
NOSE FORWARD FUSELAGE 53-10-00
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Location 1 ALL
Description 1 ALL
Main Structure 1 ALL
Skin 5 ALL
Frames 6 001-012,
Frames 10 014-099, 101-199
901-999,
Floors 21 ALL
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Forward Lower Corner underneath
the Scuff Plate , LH and RH
Detailed Inspection of Forward 614 ALL
Face of Pressure Bulkhead,
Vertical Angle (Y=675) at Crossing
Areas with Horizontal Stiffeners
(Z=1 and Z=1329), LH/RH
General Visual Inspection of 618 001-012, 014-019
Entrance Stairs Door Surround,
Upper and Lower Corners, External
Surface, LH
General Visual Inspection of 622 ALL
Avionics Compartment Doors,
Surround Corners, External Surface
(4 Doors)
General Visual Inspection of 627 ALL
Fuselage Side Panel, below Cockpit
Side Windows, between FR 1 and FR
12, External Surface, LH/RH
General Visual Inspection of Area 631 ALL
Forward of Windshield, above Side
Panel, from FR 0 to FR 4, External
Surface, LH/RH
Detailed Inspection of Fuselage 635 ALL
Lower Panel at NLG Bay Aft
Corners, External Surface, LH/RH
Detailed Inspection of Fuselage 639 ALL
Skin above Windshield, between FR
4 and FR 12, External Surface,
LH/RH
Detailed Inspection of Upper Skin 643 ALL
of Lower Longitudinal Lap Joint,
between FR 9 and FR 20, External
Surface, LH/RH
Detailed Inspection of Upper Skin 647 ALL
of Upper Longitudinal Lap Joint,
between FR 15 and FR 16 and FR 20
and FR 24, External Surface, LH/RH
Detailed Inspection of Outer Skin 651 ALL
of Lateral Longitudinal Lap Joint,
between FR 11 and FR 14 and FR 20
and FR 24, LH/RH
Detailed Inspection of Outer Skin 655 ALL
of Lateral Longitudinal Lap Joint,
between FR 1 and FR 24, LH/RH
Detailed Inspection of FR 20 659 ALL
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Splice, between Stringer 30 and
Stringer 32, LH/RH
Detailed Inspection of Windshield 664 001-012, 014-019
Center Post, Lower Attachment
Area, internal Side
Special Detailed Inspection of 669 001-012, 014-019
Windshield Center Post, Lower
Attachment Area, Internal Side
Detailed Inspection of Windshield 674 ALL
Center Post, Upper Attachment
Area, Internal Side
Detailed Inspection of Windshield 680 001-012, 014-099
Side Post at FR 4, Lower
Attachment, Internal Side, LH/RH
Special Detailed Inspection of 685 001-012, 014-099
Windshield Side Post at FR 4,
Lower Attachment, Internal Side,
LH/RH
Special Detailed Inspection of 690 ALL
Windshield Side Post at Frame 4,
Upper Attachment, Internal Side,
LH/RH
Detailed Inspection of Side Window A602 ALL
Structure, Upper Junction, between
Forward and Rear FR, External
Surface, LH/RH
Detailed Inspection of Door Stop A606 ALL
Fittings on FR 16 and FR 20, LH/RH
Special Detailed Inspection of A610 ALL
Door Frame 16, at Double Joggle
Area in Outer Flange of Frame at
Door Stops Number 1 and 7
Location, LH/RH
Special Detailed Inspection of A617 ALL
Door FR 20, at Double Joggle Area
in Outer Flange of FR, at Door
Stops Number 1 and 7 Location,
LH/RH
Detailed Inspection of Continuity A624 ALL
Fitting between FR 20 and FR 21,
and Angle Fitting, Both Sides of
FR 21, at Stringer 41 Location,
LH/RH
General Visual Inspection of NLG A630 ALL
Bay, all Panels, LH/RH
Detailed Inspection of NLG Bay, A634 ALL
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SUBJECT CH/SE/SU
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Rear Panel Aft Face, Lower
Corners, LH/RH
Detailed Inspection of Internal A639 ALL
Structure around Forward
Passenger/Crew Door above Cabin
Floor Level, between FR 15 and FR
21 and between Stringer 8 and...
Detailed Inspection of Fuselage A646 ALL
Internal Structure, below Forward
Passenger/ Crew Doors and Cabin
Floor Level, from FR 15 to FR 21
and between Stringer ...
Detailed Inspection of Fuselage A652 ALL
Internal Structure, below
Batteries, between FR 10 and FR
16, RH
General Visual Inspection of A658 ALL
Fuselage Internal Structure below
Galley and Toilet, between FR12
and FR15 and between STRG 23 LH
and STRG 23 RH
Detailed Inspection of Cockpit A663 ALL
Windshield, Lower Front Fitting at
FR 4, Lower Attachment, External
Surface, LH/RH
Special Detailed Inspection of A667 ALL
Cockpit Windshield, Lower Front
Fitting at FR 4, Lower Attachment,
External Surface, LH/RH
Detailed Inspection of NLG, A672 ALL
Secondary Door Hinge Supports on
Fuselage, LH/RH
Detailed Inspection of Fuselage A676 ALL
Skin, between FR 21 and FR 23 LH
and FR 17 and FR 18 RH, from
Stringer 31 to Stringer 36
Detailed Inspection of Forward A684 ALL
Face of Front Pressure Bulkhead
Attached to FR 1
Detailed Inspection of Cockpit A688 ALL
Side Windows, External Visible
Portion of Framework, between FR 4
and FR 12, LH/RH
Detailed Inspection of Cockpit A692 ALL
Windshield, External Portion of
Framework Covered by Retainers
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Detailed Inspection of Cockpit A696 ALL
Windshield, External Visible
Portion of Retainers
Detailed Inspection of Forward B600 ALL
Passenger/Crew Door Cutout,
Underneath the Scuff-Plate, LH/RH
Detailed Inspection of Fuselage B604 ALL
Internal Structure and Lower
Surface of Cabin Floor Structure,
from FR 15 to FR 21, between STRG
23 and STRG 28 LH/RH
Detailed Inspection of Central and B610 001-012, 014-019
Adjacent Vertical Posts of Forward
Pressure Bulkhead and Web
Assembly, Upper Portion
Detailed Inspection of Aft Face of B614 ALL
Forward Pressure Bulkhead, Above
Cockpit Floor Level, Including FR
1, as far as Visible
Detailed Inspection of Cockpit B618 ALL
Window Frames and Closing Panels,
Internal Structure (FR 12 and
Forward)
Detailed Inspection of Cockpit B624 ALL
Floor Structure, between FR 1 and
FR 12
Detailed Inspection of Cabin Floor B629 ALL
Structure between FR 12 and FR 21
Detailed Inspection of Aft Face of B634 ALL
Forward Pressure Bulkhead, below
Cockpit Floor Level, Including FR1
and Stringer Connections
Detailed Inspection of Cabin Floor B639 ALL
Structure, below and 0.5 M around
Galleys and Toilets, between FR 21
and FR 24
Clean Door Girt Bar Fitting Stop B644 ALL
Levers
General Visual Inspection of Cabin B648 ALL
Floor Structure Excluding Areas
below Galleys and Toilets, between
FR 21 and FR 24
General Visual Inspection of B653 ALL
Fuselage Internal Structure and
Floor Structure, Including NLG Bay
Panels, Between FR 1 and FR 12,
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below Cockpit Floor Panels
General Visual Inspection of B658 ALL
Fuselage Internal Structure and
Floor Structure, Including NLG Bay
Aft Face, between FR 21 and FR 24,
below Cabin Floor Panels
Detailed Visual Inspection and B663 001-012, 014-019
Torque Check of the NLG Doors
Uplock Fitting Bolts
General Visual Inspection of B669 ALL
Fuselage Internal Structure, from
FR 1 to FR 24, above Cabin Floor
Level, as far as Visible
Detailed Inspection of Forward B674 ALL
Passenger/Crew Door Cutout Lower
Corners Internal Structure above
Cabin Floor Level, at FR 16 and FR
20 from ...
PROTECTIVE SHIELDS - FR1 53-11-41
REMOVAL/INSTALLATION 401 ALL
Removal of the Protective Shields 401 ALL
- FR1
Installation of the Protective 408 ALL
Shields - FR1
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Removal of the avionics 401 ALL
compartment floor panels
Installation of the avionics 407 ALL
compartment floor panels
RADOME 53-15-11
MAINTENANCE PRACTICES 201 ALL
Opening of the Radome 110AL 201 ALL
Closing of the Radome 110AL 205 ALL
RADOME 53-15-11
REMOVAL/INSTALLATION 401 ALL
Removal of the Radome 401 ALL
Installation of the Radome 407 ALL
Removal of a Radome Telescopic Rod 423 ALL
Installation of a Radome 427 ALL
Telescopic Rod
Removal of the Locking Handle 432 ALL
Installation of the Locking Handle 436 ALL
Removal of the Arrestor Pick-Up 444 ALL
Fitting
Installation of the Arrestor 448 ALL
Pick-Up Fitting
Removal of the Radome Seal 452 ALL
Installation of the Radome Seal 457 ALL
Removal of the Seal at Frame 1 462 ALL
Installation of the Seal at Frame 465 ALL
1
RADOME 53-15-11
ADJUSTMENT/TEST 501 ALL
Tap Test of the Radome 501 ALL
Radio Electrical Test of the 504 001-012, 014-099
Radome
Radio Electrical Test of the 506 001-012, 014-099
Radome
RADOME 53-15-11
INSPECTION/CHECK 601 ALL
Detailed Inspection of the Radome 601 ALL
RADOME 53-15-11
REPAIRS 801 ALL
Repair of the Radome 801 ALL
SCUFF PLATES - DOOR ENTRANCE 53-15-15
REMOVAL/INSTALLATION 401 ALL
Removal of the FWD Passenger/Crew 401 ALL
Door Scuff Plates
Installation of the FWD 404 ALL
Passenger/Crew Door Scuff Plates
MOUNT FITTING - CABIN 53-16-11
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REMOVAL/INSTALLATION 401 ALL
Removal of the Mount Fitting at FR 401 ALL
14
Installation of the Mount Fitting 405 ALL
at FR 14
________________
FORWARD FUSELAGE 53-20-00
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Location 1 001-012, 014-099
901-999,
Location 1 101-199,
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PAGE ___________
Description 6 ALL
Frames 6 ALL
Stringers 11 001-012, 014-019
901-901,
Stringers 11 020-099, 101-199
902-999,
Skin 12 001-012, 014-099
901-999,
Skin 12 101-199,
Cabin Floor Structure 13 ALL
Structure of Cargo Compartment 19 ALL
Floor
Cabin Windows 20 ALL
Cargo Door Frame 20 ALL
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PAGE EFFECTIVITY
Detailed Inspection of Forward 645 ALL
Cargo Door Eccentric Bolts of
Locking Mechanism at Lock
Fittings, between FR 25 and FR 27A
Detailed Inspection of 649 ALL
Circumferential Joint at FR 24,
between Stringer 6 LH and Stringer
6 RH, Internal Side
Special Detailed Inspection of 653 ALL
Circumferential Joint at FR 35,
between Stringer 10 LH and
Stringer 10 RH, External Side
General Visual Inspection of 658 ALL
Fuselage External Surface around
Water Drain Panel Cutout, between
FR 25 and FR 29 at Stringer 43 LH
General Visual Inspection of 662 ALL
Forward Cargo Door Actuator Attach
Brackets, between Cabin Floor
Beams, from FR 25A to FR 27A
Detailed Inspection of Fuselage 667 ALL
Skin and Visible Part of Window
Forging Doublers around Cabin
Windows, between FR 28 and FR 35
and between Stringer ...
Detailed Inspection of Fuselage 671 ALL
Skin at FR 35 and 10cm Forward, at
Level of Stringer 30, Internal
Side, LH/RH
Detailed Inspection of Attachment 676 ALL
Area of FR 29 to FR 34, to Cabin
Floor Beams and to Cargo Floor
Beams, LH/RH
Detailed Inspection of Forward 683 101-199,
Emergency Exit Skin Cutout, Upper
Corners, External Surface, LH
Detailed Inspection of Internal 687 ALL
Structure around Forward Cargo
Door Cutout, from FR 24 to FR 29
and between Stringer 23 and
Stringer 38, RH
Detailed Inspection of Frame 693 ALL
Splices at Stringer 35 LH, from FR
24 to FR 34
Detailed Inspection of Fuselage 698 001-012, 014-099
Internal Structure between FR 24 901-999,
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and FR 35, Including Forward Face
of Pressure Bulkhead, from
Stringer 38 LH/RH to botto...
Detailed Inspection of Fuselage A604 101-199,
Internal Structure between FR 24
and FR 35.8, Including Forward
Face of Pressure Bulkhead, from
Stringer 38 LH/RH to botto...
Detailed Inspection of Inside A610 ALL
Radius of Cross Beam at FR 25, FR
26 and FR 27 Lower Fittings,
Located above Forward Cargo Door,
RH
Special Detailed Inspection of A615 ALL
Inside Radius of Cross Beam at FR
25, FR 26 and FR 27 Lower
Fittings, Located above Forward
Cargo Door, RH
General Visual Inspection of Cabin A621 001-012, 014-099
Floor Structure, Excluding Areas 901-999,
below Galleys and Toilets (if
Installed), between FR 24 and FR
35
General Visual Inspection of Cabin A626 101-199,
Floor Structure, Excluding Areas
below Galleys and Toilets (if
Installed) and Emergency Exit
Entrance Area, between...
General Visual Inspection of A631 ALL
Forward Cargo Door Cutout, Visible
Part of Lateral FR 24A and FR 28
General Visual Inspection of A636 ALL
Forward Cargo Door Lock Fittings
and Surrounding Structure, between
FR 25 and FR 27A, External Portion
(6 places)
Detailed Inspection of Cabin Floor A641 001-012, 014-099
Structure, below and 0.5 M around 901-999,
Galleys and Toilets (if
Installed), between FR 24 and FR
35
Detailed Inspection of Cabin Floor A646 101-199,
Structure, below and 0.5 M around
Galleys and Toilets (if Installed)
and Emergency Exit Entrance Area,
between FR 24 ...
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Special Detailed Inspection of A651 101-199,
Circumferential Joint at FR35.8,
between Stringer 10LH and Stringer
10RH, External Side
Detailed Inspection of Fuselage A656 101-199,
External Surface, between FR 35
and FR 35.8 from Stringer 8 to
crown centerline, LH/RH
General Visual Inspection of A660 101-199,
Fuselage External Surface, between
FR 35.4 and FR 35.8 from Stringer
8 to Stringer 14 and Stringer 18
to Stringer 23, LH/RH
General Visual Inspection of A664 001-012, 014-099
Fuselage External Surface, between 901-999,
FR 24 and FR 35, from Stringer 23
LH/RH to bottom Centerline, except
Areas Covered...
General Visual Inspection of A668 101-199,
Fuselage External Surface, between
FR 24 and FR 35.8, from Stringer
23 LH/RH to bottom Centerline,
except Areas Covered...
Detailed Inspection of Fuselage A672 101-199,
Surface Covered by Belly Fairing,
between FR 35.5 and FR 35.7 from
Stringer 26 to Stringer 32, LH/RH
Detailed Inspection of Forward A676 101-199,
Emergency Exit Skin Cutout, Upper
Corners, External Surface, RH
Detailed Inspection of Fuselage A680 101-199,
Skin and Visible Part of Window
Forging Doublers around Cabin
Windows, between FR 35.3 and FR
35.8 and between ...
Detailed Inspection of FR 35.1 and A684 101-199,
FR 35.2A Web and Door Stop
Intercostals, at Junction Area,
between Door Stop No1 and No8
(LH)/No6 (RH), LH/RH
Detailed Inspection of Attachment A690 101-199,
Area of FR35.1 and FR35.2A to
Cabin Floor Beams, LH/RH
Detailed Inspection of Skin of A694 901-999,
Circumferential Joint at FR 35,
between Stringer 10 LH and
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Stringer 10 RH, External Side
General Visual Inspection of A698 101-199,
Fuselage Skin Around Forward
Emergency Exit Skin Cutout between
FR 35 and FR 35.3 and from
Stringer 8 to Stringer 23
External...
Detailed Inspection of Frame Webs B602 901-999,
at Stringer 18 LH/RH for: FR25,
26, 27, 28 29, 30, 34
PANELS - CABIN FLOOR 53-22-12
REMOVAL/INSTALLATION 401 ALL
Removal of the Cabin Floor Panels 401 ALL
Installation of the Cabin Floor 409 ALL
Panels
PANELS - FWD CARGO COMPARTMENT FLOOR 53-22-14
REMOVAL/INSTALLATION 401 ALL
Removal of the FWD 401 ALL
Cargo-Compartment Floor-Panels
Installation of the FWD 408 ALL
Cargo-Compartment Floor-Panels
Removal of the Maintenance Panels 413 101-199,
at Frame 35.5
Installation of the Maintenance 416 101-199,
Panels at Frame 35.5
FAIRINGS - WING TO FUSELAGE 53-25-11
REMOVAL/INSTALLATION 401 ALL
Removal of the Wing-to-Fuselage 401 ALL
Fairings (191AT, 191AB, 192AT,
192AB)
Installation of the 412 ALL
Wing-to-Fuselage Fairings (191AT,
191AB, 192AT, 192AB)
SCUFF PLATES - EMERGENCY EXIT DOOR 53-25-41
REMOVAL/INSTALLATION 401 101-199,
Removal of the FWD Emergency-Exit 401 101-199,
Scuff-Plate
Installation of the FWD 404 101-199,
Emergency-Exit Scuff-Plate
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Removal of the Drain Valves 401 ALL
Installation of the Drain Valves 405 ALL
_______________
CENTER FUSELAGE 53-30-00
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Component Location 1 ALL
Description 1 ALL
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Face, Including Vertical Beams,
Above Cargo Floor Level
Detailed Visual Inspection of 638 001-012, 014-099
Internal Structure around the 901-999,
Emergency Exit Cutouts, Both
Sides, from STGR10 to STGR23,
LH/RH
Detailed Visual Inspection of Skin 646 ALL
around Anti-Collision Light
Cutout, between FR40 and FR41 and
between Stringer 1, LH/RH,
External Surface
Detailed Visual Inspection of Skin 650 ALL
around ADF-1 Antenna Cutout,
between FR44 and FR45 and between
Stringer 1, LH/RH, External
Surface
Detailed Visual Inspection of 654 ALL
Pressure Bulkhead FWD Face and the
Pressure Deck Upper Surface,
including connections to Center
Wing Box
Detailed Visual Inspection of 663 ALL
Pressure Bulkhead AFT Face and the
Lower Skin of Pressure Deck Lower
Surface
Detailed Visual Inspection of 667 ALL
Hinge and Actuator Fittings for
MLG Doors at Keelbeam
Detailed Visual Inspection of 682 ALL
Lower Skin of Longitudinal Lap
Joints in Crack Stopper Areas, at
Stringer 6, LH/RH between FR35 and
FR47/54 External Surface
Detailed Visual Inspection of the 686 001-012, 014-099
Emergency Exit Skin Cutouts, Upper 901-999,
and Lower Corners, LH/RH
Detailed Visual Inspection of Skin 691 ALL
in Circumferential Splice and
Stringer Coupling Area at FR35,
from STGR10, LH/RH to Crown
Centerline, External Surface
Detailed Visual Inspection of Skin 697 ALL
in Circumferential Splice and
Stringer Coupling Area at FR47,
from STGR10, LH/RH to Crown
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Centerline, External Surface
Detailed Visual Inspection of A600 ALL
Visible Part of Window Forgings
and Fuselage Skin in Window
Forging Area, between FR35 and
FR47/54 LH/RH, External Surface
General Visual Inspection of Main A605 ALL
Landing Gear Bay including Main
Landing Gear Door Hinges
Detailed Visual Inspection of A609 ALL
Fuselage Skin, between FR35 and
FR36 and between Stringer 25 and
Stringer 30, LH/RH, External
Surface
Detailed Visual Inspection of A614 ALL
Lower Skin of Longitudinal Lap
Joint at Stringer 18 LH and
Stringer 18 RH, in Runout Area at
FR42, Internal
Detailed Visual Inspection of A618 001-012, 014-099
Flanges at FR38, 39, 40 and 41, 901-999,
between STGR12 to STGR21, and
Longl Beam FLange at STGR20A,
between FR38 to 39, FR40 to 41,
LH/RH
Detailed Visual Inspection of Side A626 ALL
Box Beam in Area of Attachment to
FR46, LH/RH
Detailed Visual Inspection of A631 ALL
Frame Attachments to Pressure
Floor from FR42 to FR46, LH/RH
Special Detailed Inspection of A635 ALL
Hinge and Actuator Fittings for
MLG Doors at Keelbeam
Special Detailed Inspection of A644 ALL
Lower Skin of Longitudinal Lap
Joints in Crack Stopper Areas at
Stringer 6 LH/RH, between FR35.8
and FR47, External Surface
Special Detailed Inspection of A649 ALL
Upper Flange of Longitudinal Floor
Beams at FR42 and FR46, as far as
Visible
Special Detailed Inspection of A657 ALL
Lower Skin of Longitudinal Lap
Joint at Stringer 18LH and
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________ C
_ PAGE ___________
____ EFFECTIVITY
Stringer 18RH, in Runout Area at
FR42, Internal
Special Detailed Inspection of A662 ALL
Splice Plate at Circumferential
Skin Splice at FR47, from Stringer
10, LH/RH, to Crown Centerline
Special Detailed inspection of A667 ALL
Keel Beam Box Elliptical Cutout at
FR46, LH/RH
General Visual Inspection of A673 ALL
Fuselage Structure below Cabin
Floor Panels, including Cabin
Floor Structure between FR36 and
FR46
General Visual Inspection of A678 001-012, 014-099
Pressure Bulkhead Aft Face at FR35 901-999,
and Lower Skin of Pressure Deck
Lower Surface between FR35 and
FR36
General Visual Inspection of A683 101-199,
Pressure Bulkhead Aft Face at
FR35.8 and Lower Skin of Pressure
Deck Lower Surface between FR35.8
and FR36
Special Detailed Inspection of the A687 001-012, 014-099
Frames and the Frame Feet, from
FR37 to FR41, adjacent to STGR23
Special Detailed Inspection of A695 001-012, 014-019
Fastener Holes of the Pick-up
Angles between FR35 and FR36 at
STGR 30, LH/RH
General Visual Inspection of B601 001-012, 014-099
Emergency Exit Skin Cutouts, Upper 901-999,
and Lower Corners, LH/RH
General Visual Inspection of Upper B607 ALL
Skin of Longitudinal Lap Joints
and Crack Stopper Areas at STGR6
LH/RH, between FR35 and FR47/54,
External Surface
General Visual Inspection of Upper B616 ALL
Skin of Longitudinal Lap Joints in
Crack Stopper Areas at STGR18
LH/RH, between FR35 and FR47/54,
External Surface
General Visual Inspection of Lower B625 ALL
Skin of Longitudinal Lap Joints in
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TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ PAGE ___________
____ EFFECTIVITY
Crack Stopper Areas at STGR18
LH/RH, between FR35 and FR47/54,
External Surface
General Visual Inspection of B634 ALL
Fuselage External Surface between
FR35(FR35.8) and FR47, from STGR23
LH/RH to Crown Centerline, except
areas below Belly Fairing
General Visual Inspection of B644 ALL
Fuselage Internal Structure
between FR35(FR35.8) and FR47,
above Cabin Floor Level
Detailed Visual Inspection of the B653 001-012, 014-019
Transition Angle between FR35 and
FR36 just below STGR30, LH/RH
Detailed Inspection of the B659 001-012, 014-019
Outboard Flanges around the
Fastner Holes of Frames 38 thru
41, between STGR 12 and STGR 21,
LH/RH
Detailed Visual Inspection of B665 001-012, 014-099
Riveted Area of Keel Beam Side
Panel at Attachment to Center Wing
Box, LH/RH, Area A
Detailed Visual Inspection of B673 001-012, 014-099
Riveted Area of Keel Beam Side
Panel at Attachment to Center Wing
Box, LH/RH, Area B
53-CONTENTS Page 18
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TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ ____ EFFECTIVITY
PAGE ___________
General 1 ALL
Cabin Floor Panels 1 001-012, 014-099
901-999,
Cabin Floor Panels 1 101-199,
Door Threshold Heater Panels 1 101-199,
Description and Operation 1 ALL
Cabin Floor Panels 1 001-012, 014-099
901-999,
Cabin Floor Panels 2 101-199,
Door Threshold Heater Panels 2 101-199,
PANELS - CABIN FLOOR 53-32-12
REMOVAL/INSTALLATION 401 ALL
Removal of the Cabin Floor Panels 401 ALL
Installation of the Cabin Floor 407 ALL
Panels
FAIRINGS 53-35-00
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Component Location 1 ALL
Description 1 ALL
FAIRINGS 53-35-00
INSPECTION/CHECK 601 ALL
Inspection of the Wing to Fuselage 601 ALL
Fairings and Belly Fairing Access
Panels for Missing Fasteners
Inspection of the Vanes of the 618 ALL
Belly-Fairing Louver-Panels
Refer to the CDL TASK: 53-1 618 ALL
FAIRINGS - WING TO FUSELAGE 53-35-11
REMOVAL/INSTALLATION 401 ALL
Removal of the Wing-to-Fuselage 401 ALL
Fairings
Installation of the 429 ALL
Wing-to-Fuselage Fairings
FAIRINGS - COOLING AIR INLET 53-35-12
REMOVAL/INSTALLATION 401 ALL
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TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ ____ ___________
PAGE EFFECTIVITY
Removal of the Belly Fairing 401 ALL
Blowout Panel
Installation of the Belly Fairing 406 ALL
Blowout Panel
ACCESS PANELS 53-35-13
REMOVAL/INSTALLATION 401 ALL
Removal of the Belly Fairing 401 ALL
Access Panels
Installation of the Belly Fairing 414 ALL
Access Panels
Removal of the Quick-Release 428 ALL
Access Panels from the Belly
Fairing Structure
Installation of the Quick-Release 440 ALL
Access Panels on the Belly Fairing
Structure
Removal of the Louver Panel - 450 ALL
Panel 147FB (148FB)
Installation of the Louver Panel - 454 ALL
Panel 147FB (148FB)
FITTINGS 53-36-00
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Description 1 ALL
53-CONTENTS Page 20
May 01/08
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CHAPTER 53
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TABLE OF CONTENTS
_________________
_______
SUBJECT ________
CH/SE/SU C
_ PAGE ___________
____ EFFECTIVITY
REAR FUSELAGE
_____________ 53-40-00
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Component Location 2 ALL
Description 5 ALL
Rear Fuselage Main Structure 5 ALL
Cargo Compartments 5 001-012, 014-099
901-999,
Cargo Compartments 5 101-199,
Dorsal Fin 5 ALL
Drains 5 ALL
53-CONTENTS Page 21
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CHAPTER 53
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FUSELAGE
TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ PAGE ___________
____ EFFECTIVITY
Hinge Fittings between STGR22 and
STGR23
Detailed Visual Inspection of 628 ALL
Fuselage AFT Cargo Door Hinge
Fittings and External Attachment
Area
Detailed Visual Inspection of 633 101-199,
Fuselage Skin under Bulk Cargo
Door Scuff Plate
Special Detailed Inspection of 636 101-199,
Fuselage Skin of Bulk Cargo Door
Cutout and Sealing Profile at
Upper Corners
Detailed Visual Inspection of 641 001-012, 014-099
Lower Skin of Longitudinal Lap
Joints in Crack Stopper Areas at
Stringer 32 LH, between FR47 and
FR53, External Surface
Detailed Visual Inspection of 646 101-199,
Lower Skin of Longitudinal Lap
Joints in Crack Stopper Area at
STGR 32 LH between FR47 and FR48
STGR 32 RH FR47 and FR47.5 Ext
Detailed Visual Inspection of 649 901-999,
Lower Skin of Longitudinal Lap
Joints in Crack Stopper Areas at
Stringer 32 LH, between FR47/51
and FR57, External Surface
Detailed Visual Inspection of AFT 653 ALL
Passengers/Crew Door Cutout Upper
Corners including Skin and
Internally the Visible Portion of
the Internal Doubler
Detailed Visual Inspection of 658 ALL
Frame Splices and Adjacent Area
from FR53 to FR60, located above
Stringer 18 RH
Detailed Visual Inspection of AFT 661 ALL
Cargo Door Lock Fittings and
Surrounding Structure between
Stringer 41 RH to Door Sill (6
places)
Detailed Visual Inspection of 669 ALL
Fuselage Internal Structure
between FR46 and FR65 including
AFT Face of Pressure Bulkhead from
53-CONTENTS Page 22
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CHAPTER 53
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FUSELAGE
TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ PAGE ___________
____ EFFECTIVITY
STGR 38 LH/RH to Bottom CenterLine
Detailed Visual Inspection of 674 001-012, 014-099
Visible Part of Windows Forgings
between FR47 and FR65 LH/RH,
External Surface
Detailed Visual Inspection of 681 101-199,
Visible Part of Windows Forgings
between FR47 and FR64 LH/RH,
External Surface
Detailed Visual Inspection of 684 901-999,
Visible Part of Windows Forgings
between FR47/51 and FR65 LH/RH,
External Surface
Detailed Visual Inspection of Skin 687 ALL
in Circumferential Splice at FR70
between STGR10 LH/RH and Crown
Center Line, including Cutout
Corners for Fin
Detailed Visual Inspection of Skin 691 ALL
around VHF-3 Antenna Cutout
between Stringer 1 LH/RH, External
Surface
Detailed Visual Inspection of Skin 696 ALL
in Circumferential Splice and
Stringer Coupling Areas at FR64,
from STGR10, LH/RH, to Crown
Center Line
Detailed Visual Inspection of AFT A600 ALL
Passenger/Crew Door Cutout Lower
Corners including Skin and Doubler
underneath the Scuff Plate, LH/RH
Detailed Visual Inspection of AFT A603 ALL
Cargo Door Eccentric Bolts of
Locking Mechanism at Lock Fittings
(6 places)
Detailed Visual Inspection of Bulk A607 101-199,
Cargo Door Stop Fittings and
Back-up Structure at FR60 and FR62
(10 places)
Detailed Visual Inspection of A612 ALL
Lower Skin of Longitudinal Lap
Joints in Crack Stopper Areas at
Stringer 6 LH/RH between FR47 and
FR70, External Surface
Detailed Visual Inspection of A615 101-199,
Fuselage Internal Structure around
53-CONTENTS Page 23
May 01/08
R
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CHAPTER 53
__________
FUSELAGE
TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ PAGE ___________
____ EFFECTIVITY
Bulk Cargo Door Cutout from FR59
to FR63 and between STGR23 and
STGR38
Detailed Visual Inspection of Door A619 ALL
Stop Fittings on FR66 and FR68,
LH/RH
Detailed Visual Inspection of A623 ALL
Fuselage Internal Structure, Below
Cabin Floor Panels Including Floor
Structure from FR65 to FR70
Detailed Visual Inspection of AFT A628 ALL
Cargo Door Cutout Upper and Lower
Corners, External Surface
Detailed Visual Inspection of A632 ALL
Upper Segment of FR70, Fin to
Fuselage FWD Attach Fittings and
Area between FR69 and FR70 from
STGR6 LH/RH to Crown Center Line
Detailed Visual Inspection of A636 ALL
Cabin Floor Structure, below and
0.5m around Galleys and Toilets,
from FR47/54 (318), FR47/51 (319),
FR47 (320/321) to FR70
General Visual Inspection of AFT A643 ALL
Cargo Door Lock Fittings and
Surrounding Structure, External
Portion (6 places)
Detailed Visual Inspection of Aft A647 ALL
Passenger/Crew Door Cutout,
underneath the scuff-Plate, LH/RH
Detailed Visual Inspection of Skin A651 101-199,
in Circumferential Splice and
Stringer Coupling areas at FR47.5
from Stringer 16 LH/RH to Crown
Centerline, External
Detailed Visual Inspection of the A655 101-199,
Aft Emergency Skin Cutouts Upper
and Lower Corners, External
Surface LH/RH
Detailed Visual Inspection of the A658 101-199,
Emergency-Exit Escape Chute
Compartment Skin Cutouts, Upper
and Lower Corners External Surface
LH/RH
Detailed Visual Inspection of the A661 101-199,
Skin at the Window Cutout between
53-CONTENTS Page 24
May 01/08
R
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CHAPTER 53
__________
FUSELAGE
TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ PAGE ___________
____ EFFECTIVITY
FR47 and FR47.2 from Stringer 14
to Stringer 18, External Surface
LH/RH
Detailed Visual Inspection of the A664 101-199,
Door Stop Fittings on FR47.2A and
FR47.4, LH and RH
Detailed Visual Inspection of A668 101-199,
Internal Structure around
Emergency Exit Cutouts above Cabin
Floor Level between FR47.2 and
FR47.5 and STGR 10 to 23
Detailed Visual Inspection of the A671 101-199,
Escape Chute Slide Compartment
Internal Structure Between FR47.2A
and FR47.4 from Stringer 24 to
Stringer 28 LH/RH
General Visual Inspection of Cabin A674 ALL
Floor Structure, excluding Areas
below Galleys and Toilets and Door
Entrance Area, from FR47 to FR70
General Visual Inspection of A678 ALL
Fuselage External Surface and
Belly Fairing Support Structure
under the Belly Fairing
General Visual Inspection of AFT A684 ALL
Cargo Door Cutout, Visible Part of
Lateral Frames
General Visual Inspection of A689 101-199,
Sealing Profile of Bulk Cargo Door
Cutout at Upper Corners
General Visual Inspection of Bulk A693 101-199,
Cargo Door Stop Fittings and
Back-Up Structure, at FR60 and
FR62 (10 Places)
Detailed Visual Inspection of the A696 ALL
Fuselage Skin External Surface
between FR64 and FR70 from
Stringer 6 to Crown Center Line LH
and RH
General Visual Inspection of Upper B600 ALL
Skin of Longitudinal Lap Joints,
including Crack Stopper Areas at
Stringer 6, LH/RH between FR47 and
FR70
General Visual Inspection of Upper B604 ALL
Skin of Longitudinal Lap Joints,
53-CONTENTS Page 25
May 01/08
R
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CHAPTER 53
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FUSELAGE
TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ PAGE ___________
____ EFFECTIVITY
including Crack Stopper Areas at
Stringer 32 LH and Stringer 41 RH,
External Surface
General Visual Inspection of Upper B614 ALL
Skin of Longitudinal Lap Joints,
including Crack Stopper Areas at
Stringer 32 LH/RH and Stringer 41
RH, External Surface
General Visual Inspection of B622 ALL
Fuselage External Surface from
Stringer 23 LH/RH to Bottom
Centerline, except Area covered by
Belly Fairing
General Visual Inspection of Upper B629 ALL
Skin of Longitudinal Lap Joints,
including Crack Stopper Areas at
Stringer 18 LH/RH between FR47 and
FR64 External Surface
General Visual Inspection of Lower B636 ALL
Skin of Longitudinal Lap Joints in
Crack Stopper Areas at Stringer 18
LH/RH, between FR47 and FR64
External Surface
General Visual Inspection of Lower B643 ALL
Skin of Longitudinal Lap Joints in
Crack Stopper Areas at Stringer 32
LH/RH, between FR59 and FR70
External Surface
General Visual Inspection of B650 ALL
Fuselage Skin around AFT
Passenger/Crew Door Cutouts,
External Surface (except Area
under Scuff Plates), LH/RH
General Visual Inspection of B654 ALL
Fuselage Skin around Outflow Valve
Cutout, between FR 65 and FR 66
and from Stringer 26 to Stringer
31, RH, External Surface
General Visual Inspection of B658 ALL
Fuselage Skin around Water Service
Panel Cutout between FR 65 and FR
66 and from STGR 37 to STGR 43,
LH, External Surface
General Visual Inspection of B662 ALL
Fuselage Skin around Waste Service
Panel Cutout between FR 65 and FR
53-CONTENTS Page 26
May 01/08
R
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CHAPTER 53
__________
FUSELAGE
TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ PAGE ___________
____ EFFECTIVITY
66 and from STGR 33 to STGR 40,
RH, External Surface
General Visual Inspection of Upper B666 ALL
Skin of Longitudinal Lap Joints,
including Crack Stopper Areas at
STGR 41 RH, between FR 51 and FR
58, External Surface
General Visual Inspection of AFT B672 ALL
Cargo Door Actuator Attach
Bracket, between Floor Beams
General Visual Inspection of B680 101-199,
Circumferential Joint above AFT
Emergency Exit Door at FR 47.3
from Stringer 6 to Stringer 12,
External Surface, LH/RH
General Visual Inspection of B685 ALL
Fuselage External Surface, between
FR 47 and FR 70 From STGR 23 LH/RH
to Crown Centerline
General Visual Inspection of the B693 ALL
Fuselage Internal Structure, From
FR 47 to FR 70, above the Cabin
Floor Level
General Visual Inspection of C601 ALL
Fuselage Internal Structure,
between Cabin Floor Panels and
Cargo Compartment Floor, inc.
Cabin Floor Stucture, FR46 to FR
65
General Visual Inspection of AFT C611 101-199,
Emergency Exit Skin Cutouts, Upper
and Lower Corners, External
Surface, LH/RH
Special Detailed Inspection of C616 ALL
Lower Skin of Longitudinal Lap
Joints in Crack Stopper Areas at
Stringer 6 LH/RH between FR47 and
FR70, External Surface
Special Detailed Inspection of C622 ALL
Frame Splices and Adjacent Area
from FR53 to FR60, located above
Stringer 18 RH
Special Detailed Inspection of C626 ALL
Lower Skin of Longitudinal Lap
Joints in Crack Stopper Areas at
Stringer 32 LH, between FR47 and
53-CONTENTS Page 27
May 01/08
R
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CHAPTER 53
__________
FUSELAGE
TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ PAGE ___________
____ EFFECTIVITY
FR59, External Surface
Special Detailed Internal C634 ALL
Inspection of the Lock Fittings
and Adjacent Structure at the AFT
Cargo-Compartment Door.
Special Detailed Inspection of C637 ALL
Internal Doubler Forward and AFT
Water Service Panel Cutout between
STGR38 and STGR42 LH
Special Detailed Inspection of AFT C642 ALL
Passenger/Crew Door Cutout Lower
Corners including Skin and Doubler
underneath the Scuff Plate, LH/RH
Special Detailed Inspection of C647 ALL
Internal Doubler Forward and AFT
of Waste Service Panel Cutout
between STGR35 and STGR39 RH
Special Detailed Inspection of C652 ALL
Splice Plate at Circumferential
Skin Splice at FR64, from Stringer
10, LH/RH, to Crown Centerline
Special Detailed Inspection of Aft C657 ALL
Cargo Door Lock Fitting and
Surrounding Structure between FR53
and FR55A, from STGR41 RH to Door
Sill (6 Places)
Special Detailed Inspection of C665 101-199,
Splice Plate at Circumferential
Skin Splice at FR47.5 from
Stringer 16 LH and RH to Crown
Center Line, External
Special Detailed Inspection of C669 001-010,
Gusset Plate Attachment Holes on
FR66 at Stringer Positions 18, 20
and 22
Special Detailed Inspection of C674 001-012, 014-019
Former Junction Fastener Holes and
Tooling Hole on FR68, LH/RH
Detailed Visual Inspection of AFT C679 ALL
Passenger/Crew Door-Cutout above
Cabin Floor Level, at FR66 and
FR68 from STGR22 to STGR23 and
around Girt Bar Fittings
Detailed Visual Inspection of C684 ALL
Cabin Floor Structure and
Structure below AFT Entrance Area,
53-CONTENTS Page 28
May 01/08
R
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CHAPTER 53
__________
FUSELAGE
TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ PAGE ___________
____ EFFECTIVITY
between FR66 and FR68 and Lateral
Shear Plates FR68 and FR70
General Visual Inspection of C692 101-199, 901-999
Longitudinal Butt Joint at
STGR30(RH) from FR47 to FR64
External Surface (Area covered by
Belly-Fairing)
53-CONTENTS Page 29
May 01/08
R
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CHAPTER 53
__________
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TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ PAGE ___________
____ EFFECTIVITY
ZONE 150
REMOVAL/INSTALLATION 401 ALL
Removal of the AFT 401 ALL
Cargo-Compartment Floor-Panels
Zone 150
Installation of the AFT 409 ALL
Cargo-Compartment Floor-Panels
Zone 150
FLOOR PANELS - AFT CARGO COMPARTMENT 53-42-17
ZONE 160
REMOVAL/INSTALLATION 401 ALL
Removal of the BULK 401 ALL
Cargo-Compartment Floor-Panels
Installation of the BULK 409 ALL
Cargo-Compartment Floor-Panels
FAIRINGS 53-45-00
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Component Location 1 ALL
DORSAL FIN 53-45-11
REMOVAL/INSTALLATION 401 ALL
Removal of the Dorsal Fin 321AL 401 ALL
Installation of the Dorsal Fin 406 ALL
321AL
SCUFF PLATES - DOOR ENTRANCE 53-45-15
REMOVAL/INSTALLATION 401 ALL
Removal of the Scuff Plates at the 401 ALL
AFT Passenger/Crew Doors
Installation of the Scuff Plates 404 ALL
at the AFT Passenger/Crew Doors
Removal of the Scuff Plates at the 411 101-199,
BULK Cargo-Compartment Door
Installation of the Scuff Plates 414 101-199,
at the BULK Cargo-Compartment Door
53-CONTENTS Page 30
May 01/08
R
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CHAPTER 53
__________
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TABLE OF CONTENTS
_________________
SUBJECT
_______ CH/SE/SU
________ C
_ PAGE ___________
____ EFFECTIVITY
FITTINGS 53-46-00
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Component Location 1 ALL
Description 1 ALL
__________________
CONE/REAR FUSELAGE 53-50-00
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Component Location 1 ALL
Description 1 ALL
Cone/Rear Fuselage Shell 1 ALL
Structure
Cone/Rear Fuselage Access 1 001-012, 014-019
Cone/Rear Fuselage Access 1 020-099, 101-199
901-999,
Jacking Point 3 ALL
Stabilizer Attach Points 3 ALL
Systems and Components 3 ALL
53-CONTENTS Page 31
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CHAPTER 53
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TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ PAGE ___________
____ EFFECTIVITY
Pressure Bulkhead AFT Face and
Fuselage Internal Structure, FR70
and FR71, from STGR 26 LH/RH to
Bottom Center Line
Detailed Visual Inspection of Rear 606 ALL
Pressure Bulkhead Forward Face
below Cabin Floor Level
Detailed Visual Inspection of the 611 ALL
Ring Frame at the Circumferential
Joint of the Rear Pressure
Bulkhead Skin at FR70 AFT Face
Detailed Visual Inspection of 615 ALL
Fuselage Skin at Horizontal
Stabilizer Cutout at Forward Upper
and Lower Corners LH/RH
Detailed Visual Inspection of 618 ALL
FR74, Splices at STGR12 and STGR19
LH/RH, Internal Structure
Detailed Visual Inspection of 622 ALL
Horizontal Stabilizer Attachment
and Back-up Structure at FR77,
from Stringer 8 to Stringer 21
LH/RH
Detailed Visual Inspection of Rear 626 ALL
Pressure Bulkhead Forward Face
above Cabin Floor Level
Detailed Visual Inspection of Tail 631 ALL
Cone Attachment Fittings at FR77
and FR78
Detailed Visual Inspection of Fin 635 ALL
to Fuselage MID and AFT Attach
Fittings inside Fuselage, in Areas
of Attachment to Fuselage Skin and
to FR72 and FR74
Detailed Visual Inspection of 639 ALL
Attach Fittings for Horizontal
Stabilizer Trim Actuator at FR73
Detailed Visual Inspection of Fin 643 ALL
to Fuselage FWD, MID and AFT
Attach Fittings, Outside Fuselage,
LH/RH
Detailed Visual Inspection of Rear 647 ALL
Pressure Bulkhead AFT Face,
Reinforcement Splice at Forward
Fin Attachment Area
Detailed Visual Inspection of Rear 651 ALL
53-CONTENTS Page 32
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CHAPTER 53
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TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ PAGE ___________
____ EFFECTIVITY
Pressure Bulkhead, Skin Splices
AFT Face
Detailed Visual Inspection of Rear 655 ALL
Pressure Bulkhead, Areas around
Outlet Cutouts, AFT Face
Detailed Visual Tnspection of 659 ALL
Shear Ties and Frame Clips at FR72
and FR74, between Stringer 3 and
Stringer 9, LH/RH, Internal
Structure
General Visual Inspection of 663 ALL
Fuselage Skin around Cutout for
Tail Compartment Access Door,
between FR 70 and FR 73, STGR 25
RH and Bottom Center Line
General Visual Inspection of the 667 ALL
Fuselage External Surface and the
Vertical Stabilizer Attachment
Fitting, below the Vertical
Stabilizer/Fuselage Fairings
General Visual Inspection of the 672 ALL
Rear Fuselage Internal Structure,
between FR70 and FR77
General Visual Inspection of the 677 ALL
Rear Fuselage External Surface,
between FR70 and FR87
MAINTENANCE PLATFORM 53-51-17
REMOVAL/INSTALLATION 401 ALL
Removal of the Maintenance 401 ALL
Platform Panels (AFT Equipment
Compartment)
Installation of the Maintenance 404 ALL
Platform Panels (AFT Equipment
Compartment)
53-CONTENTS Page 33
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CHAPTER 53
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TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ PAGE ___________
____ EFFECTIVITY
FR77
Removal of the Diagonal Support 410 ALL
Struts at FR77
Installation of the Diagonal 414 ALL
Support Struts at FR77
FAIRINGS 53-55-00
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Component Location 1 ALL
FAIRINGS - VERTICAL STABILIZER 53-55-11
REMOVAL/INSTALLATION 401 ALL
Removal of the Fairings 401 ALL
323AL/323AR
Installation of the Fairings 405 ALL
323AL/323AR
FAIRINGS - RUDDER 53-55-12
REMOVAL/INSTALLATION 401 ALL
Removal of the Rudder Fairings 401 ALL
325AL and 325AR
Installation of the Rudder 406 ALL
Fairings 325AL and 325AR
FAIRINGS - TRIMMABLE HORIZONTAL 53-55-13
STABILIZER
REMOVAL/INSTALLATION 401 ALL
Removal of the Fairings at the THS 401 ALL
Fittings.
Installation of the Fairings at 405 ALL
the THS Fittings.
FITTINGS 53-56-00
DESCRIPTION AND OPERATION 1 ALL
General 1 ALL
Component Location 1 ALL
Description 1 ALL
The Cone/Rear Fuselage Fittings 1 ALL
The Vertical Stabilizer Fittings 1 ALL
The Horizontal Stabilizer 1 ALL
Fittings
The Tailcone Atachment Fittings 1 ALL
FITTINGS - TRIMMABLE HORIZONTAL 53-56-11
STABILIZER
REMOVAL/INSTALLATION 401 ALL
Removal of the Support Fittings of 401 ALL
the Trimmable Horizontal
Stabilizer (THS)
53-CONTENTS Page 34
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TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ ____ ___________
PAGE EFFECTIVITY
Installation of the Support 413 ALL
Fittings of the Trimmable
Horizontal Stabilizer (THS)
53-CONTENTS Page 35
May 01/08
R
IAC
FUSELAGE - GENERAL - DESCRIPTION AND OPERATION
______________________________________________
1. _______
General
R The fuselage is a semi-monocoque structure. Light alloy circular frames and
R longitudinal stringers support and strengthen the main fuselage skin. There
R are no longitudinal stringers in the nose assembly.
R
R The fuselage is made of separate assemblies which are put together to make
R the complete fuselage shell. The assemblies are as follows:
R - nose forward fuselage,
R - forward fuselage,
R - center fuselage,
R - rear fuselage,
R - cone/rear fuselage.
R Frames 24, 35, 47 and 70 make the joints for the assemblies.
R
R Pressure bulkheads are installed at FR1 and FR70. The pressure bulkheads and
R the fuselage skin make the basic pressurized zone. The cockpit, cabin,
R avionics compartment and the FWD and AFT cargo compartments are included in
R the pressurized zone.
R
R The structure is made of frames, stringers and skin panels. They are riveted
R together to make the fuselage shell. Crossbeams make the shell stronger in
R the forward and aft fuselage. Support struts are attached to each end of the
R crossbeams (Ref. AMM 533300/534300). Longerons and seat tracks that are
R attached to the crossbeams make the cabin floor structure. The belly fairing
R primary structure (Ref. AMM 533500) is installed on the exterior of the
R lower fuselage between FR31/35 and FR48/FR53. It is an extension to the
R lower fuselage and contains the air-conditioning and hydraulic services
R equipment.
R
R The cabin floor structure divides the fuselage into two areas, the upper
R fuselage and the lower fuselage. The upper fuselage includes the cockpit and
R the cabin. The lower fuselage includes the avionics compartments, nose and
R main gear bays and the FWD and AFT cargo compartments. Crossbeams and
R support struts support the cabin floor structure at STGR23.
R
R The floor panels are made of a honeycomb core which is bonded between Glass-
R fiber Reinforced Plastic (GFRP) sheets (Ref. AMM 533200/534200).
R
R The radome, wing center box, nose and main gear bays, belly fairing and
R cone/rear fuselage are not in the pressurized zone.
R
R Skin stiffeners make the fuselage skin stronger. They are riveted to the
R skin in areas of high stress (door openings, emergency exits, cabin windows,
R etc.).
R
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The cabin windows are installed between STGR14 and STGR18 (Ref. AMM 562100).
2. __________________
Component Location
3. Description
___________
(1) The nose forward fuselage extends from FR1 to FR24. The upper part of
the assembly includes the cockpit and the entrance area for the two
FWD passenger/crew doors (Ref. AMM 521100). The nose gear bay and the
avionics compartment are installed in the lower part of the assembly.
(2) Longitudinal stringers are not included in the nose forward fuselage.
More frames are installed at approximately half the distance of those
installed in the other sections of the fuselage shell.
(3) Crossbeams make the shell stronger; they are attached to the frames.
Support struts are attached to each end of the crossbeams. Longerons
are attached to the crossbeams to make the cockpit and the
entrance-area floor structure.
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Fuselage - Component Location
Figure 001
R
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001-012, 014-099, 53-00-00
Page 3
May 01/06
IAC
R Fuselage - Component Location
R Figure 001A
EFF :
101-199, 53-00-00
Page 4
Feb 01/07
IAC
Fuselage - Component Location
R Figure 001B
R
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901-999, 53-00-00
Page 5
Feb 01/07
IAC
B. Forward Fuselage (Ref. AMM 532100)
(1) The forward fuselage extends from FR24 to FR35. The upper part of the
assembly contains the forward cabin area. The FWD cargo compartment
is included in the lower part of the assembly. The upper and the
lower parts of the assembly are in the pressurized zone.
(1) The center fuselage extends from FR35 to FR47. The upper part of the
assembly contains the center cabin area and the left and right
overwing emergency exits between FR38 and FR41 (Ref. AMM 522100). The
wing center box and the main gear bay are installed in the lower
assembly, below the cabin floor. Only the cabin area of the assembly
is in the pressurized zone.
(2) The wing center box is installed between FR36 and FR42. The structure
extends across the width of the lower fuselage and is a continuation
of the wing cantilever box. The main gear bay is installed between
FR42 and FR46.
(3) A keel beam is installed in the bottom of the lower fuselage and
extends from FR35 to FR46. The keel beam keeps the longitudinal
structural strength of the lower fuselage and transmits the fuselage
bending loads.
(1) The rear fuselage extends from FR47 to FR70. It is made of two
separate subassemblies which are then put together. The joint for the
two subassemblies is made at FR64.
(2) The upper part of the complete assembly contains the rear cabin and
the entrance area for the AFT passenger/crew doors (Ref. AMM 521300).
The AFT cargo compartment is installed in the lower part of the
assembly, between FR46/47 and FR65. The upper and the lower parts of
the assembly are in the pressurized zone.
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R
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E. Cone/Rear Fuselage (Ref. AMM 535100)
(1) The cone/rear fuselage extends from FR70 to FR86. The assembly is
made of two separate subassemblies. The joint for the two
subassemblies is made at FR77.
NOTE : The specification given for the two subassemblies, and used in
____
this topic, is cone/rear fuselage (FR70 to FR77) and tailcone
(FR77 to FR86).
(2) The basic structure of both subassemblies is similar. They are made
of frames, stringers and skin panels riveted together to make the
cone/rear fuselage and tailcone shells.
(4) The Auxiliary Power Unit (APU) is installed in the tailcone (Ref. AMM
535800). The APU compartment is a specified fire zone and firewalls
close the compartment on all sides. The firewalls are made of
titanium sheets. You can remove the tailcone from the aircraft as one
complete unit.
(5) Maintenance access doors are included in the lower right side of the
two subassemblies (Ref. AMM 524100). The cone/rear fuselage access
door 314AR is installed between FR78 and FR80; the APU access doors
315AL and 316AR are installed between FR80 and FR84.
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Feb 01/07
IAC
FUSELAGE - GENERAL - INSPECTION/CHECK
_____________________________________
TASK 53-00-00-210-001
Removal and Detailed Inspection of the Piston-Type Drain Valves in the Lower
Fuselage Shell
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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May 01/06
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-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-00-00-010-050
A. Get Access
(2) Open the access doors 811, 824 (Ref. TASK 52-41-00-010-002).
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(3) Open the FWD and the AFT cargo-compartment doors (Ref. TASK 52-30-00-
860-001)
(4) Put an access platform in position position below the cargo doors.
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(5) Remove the floor panels 131AF, 131HF from the FWD cargo compartment
(Ref. TASK 53-22-14-000-001).
(6) Remove the floor panels 151DF, 151GF, 161AF from the AFT cargo
compartment (Ref. TASK 53-42-14-000-001) (Ref. TASK 53-42-17-000-
001).
(7) From the inside of the aircraft, clean the areas around the drain
valves with a clean cloth.
R Subtask 53-00-00-010-050-B
R A. Get Access
R (2) Open the access doors 811, 824 (Ref. TASK 52-41-00-010-002).
R WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
R BEFORE YOU START A TASK ON OR NEAR:
R - THE FLIGHT CONTROLS
R - THE FLIGHT CONTROL SURFACES
R - THE LANDING GEAR AND THE RELATED DOORS
R - COMPONENTS THAT MOVE.
R (3) Open the FWD and the AFT cargo-compartment doors (Ref. TASK 52-30-00-
R 860-001)
R (4) Put an access platform in position position below the cargo doors.
R (5) Remove the floor panels 131AF, 131HF from the FWD cargo compartment
R (Ref. TASK 53-22-14-000-001).
R (6) Remove the floor panels 151CG, 151TF, 152TF, 151GF from the AFT cargo
R compartment (Ref. TASK 53-42-14-000-001). Remove the floor panel
R 161AF from the BULK cargo compartment (Ref. TASK 53-42-17-000-001).
R (7) From the inside of the aircraft, clean the areas around the drain
R valves with a clean cloth.
R
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R **ON A/C 901-999,
Subtask 53-00-00-010-050-A
A. Get Access
(2) Open the access doors 811, 824 (Ref. TASK 52-41-00-010-002).
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(3) Open the FWD and the AFT cargo-compartment doors (Ref. TASK 52-30-00-
860-001)
(4) Put an access platform in position position below the cargo doors.
(5) Remove the floor panels 131AF, 131CG from the FWD cargo compartment
(Ref. TASK 53-22-14-000-001).
(6) Remove the floor panels 151VG, 151ZG, 151CE from the AFT cargo
compartment (Ref. TASK 53-42-14-000-001).
(7) From the inside of the aircraft, clean the areas around the drain
valves with a clean cloth.
4. Procedure
_________
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Piston-Type Drain Valves
Figure 601/TASK 53-00-00-991-001
R
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001-012, 014-099, 53-00-00
Page 605
May 01/06
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R Piston-Type Drain Valves
R Figure 601A/TASK 53-00-00-991-001-B
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Page 606
Feb 01/07
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R **ON A/C 901-999,
Subtask 53-00-00-210-050
A. Inspection Procedure
(1) Do the removal and the detailed inspection of the piston-type drain
valves in the lower fuselage shell:
(a) Remove the basic valves from the drain valve assemblies.
(b) Make sure that the basic valves are not blocked. Remove any
blockage.
(c) Carefully push a PROBE - NON METALLIC, FLEXIBLE into the center
of each basic valve and make sure that the valves are open.
5. Close-up
________
Subtask 53-00-00-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the floor panels 151DF, 151GF, 161AF in the AFT cargo
compartment (Ref. TASK 53-42-14-400-001) (Ref. TASK 53-42-17-400-
001).
(3) Install the floor panels 131AF, 131HF in the FWD cargo compartment
(Ref. TASK 53-22-14-400-001).
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Piston-Type Drain Valves
R Figure 601B/TASK 53-00-00-991-001-A
R
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901-999, 53-00-00
Page 608
Feb 01/07
IAC
(5) Close the FWD and the AFT cargo-compartment doors (Ref. TASK 52-30-
00-860-002).
(6) Close the access doors 811, 824 (Ref. TASK 52-41-00-410-002).
(8) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R Subtask 53-00-00-410-050-B
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Install the floor panels 131AF, 131HF in the FWD cargo compartment
R and (Ref. TASK 53-22-14-400-001).
R (3) Install the floor panels 151CG, 151TF, 152TF, 151GF in the AFT cargo
R compartment (Ref. TASK 53-42-14-400-001). Install the floor panel
R 161AF in the BULK cargo compartment (Ref. TASK 53-42-17-400-001).
R (5) Close the FWD and the AFT cargo-compartment doors (Ref. TASK 52-30-
R 00-860-002).
R (6) Close the access doors 811, 824 (Ref. TASK 52-41-00-410-002).
R (8) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
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Page 609
Feb 01/07
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R **ON A/C 901-999,
Subtask 53-00-00-410-050-A
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the floor panels 151VG, 151ZG, 151CE in the AFT cargo
compartment (Ref. TASK 53-42-14-400-001) (Ref. TASK 53-42-17-400-
001).
(3) Install the floor panels 131AF, 131CG in the FWD cargo compartment
(Ref. TASK 53-22-14-400-001).
(5) Close the FWD and the AFT cargo-compartment doors (Ref. TASK 52-30-
00-860-002).
(6) Close the access doors 811, 824 (Ref. TASK 52-41-00-410-002).
(8) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
901-999, 53-00-00
Page 610
Feb 01/07
IAC
NOSE FORWARD FUSELAGE - DESCRIPTION AND OPERATION
_________________________________________________
1. General
_______
R A. Location
The nose forward fuselage extends from STA254 to FR24. It is divided into
two zones : non-pressurized zone and pressurized zone.
(1) The non-pressurized zone forward of FR1 includes the radome which
houses the radar and the ILS antennas.
(2) The pressurized zone extends between FR1 and FR24 and comprises:
- the cockpit at the upper part between FR1 and FR13 forward of
STA621 and the forward section of the cabin aft of STA621,
- the avionics compartment and the nose landing gear well at the
lower part.
2. Description
___________
A. Main Structure
The structure of the nose forward fuselage comprises three parts:
- the forward upper structure between FR1 and FR11,
(Ref. Fig. 001)
- the aft upper structure between FR12 and FR23,
(Ref. Fig. 002)
- the lower structure between FR1 and FR23.
(Ref. Fig. 003)
(1) The forward upper structure between FR1 and FR11 comprises:
- four closed frames and bulkheads FR1, FR2, FR8 and FR11,
- four open frames comprising the openings for the windshield and the
side windows ; FR3, FR4, FR5, FR6, FR7, FR9, FR10,
- a windshield and side window frame to which the structural frames
are attached,
- two lateral boxes at floor level,
- a forward pressure bulkhead,
- a floor support structure,
(2) The aft upper structure between FR12 and FR23 comprises:
- an assembly of closed frames,
- the passenger/crew door frames between FR16 and FR20,
- three open frames FR17A, FR18 and FR19A in the zone of the
passenger/crew door,
- stringers,
- a floor support structure.
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Forward Upper Structure - FR1 to FR11
Figure 001
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Feb 01/96
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Aft Upper Structure - FR12 to FR24
Figure 002
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Nose Forward Fuselage
Figure 003
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**ON A/C 001-012, 014-019,
B. Skin
(Ref. Fig. 003)
The skin panels are formed from aluminium alloy sheets and include
cut-outs and reinforcement obtained through chemical milling.
NOTE : The skin panels above and below the windshield are made of
____
titanium to provide improved protection against bird impact.
The lower section of the fuselage comprises three skin panels extending
from FR1 to FR24.
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The central panel has an opening for access between frames 3 and 5 and
the opening for the nose landing gear between frames 9 and 20. The lower
right panel has two access openings between FR12 and FR14 and FR21 and
FR23.
The lower left panel has an access opening between FR13 and FR15.
The forward upper part of the fuselage (FR1 to FR12) comprises the
lateral skin panels and five upper skin panels. These panels are secured
to the windshield and side window frames.
The aft upper part of the fuselage section (FR12 to FR24) consists of
lateral skin panels and an upper skin panel. The lateral panels contain
the frames of the passenger/crew doors between FR16 and FR20. A channel
is installed above the doors.
All the skin panels are riveted together with an application of sealant.
C. Frames
(Ref. Fig. 004)
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R
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Frame Location
Figure 004
R
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001-012, 014-019, 53-10-00
Page 7
May 01/01
IAC
Frame Location
Figure 004A
R
EFF :
020-099, 101-199, 901-999, 53-10-00
Page 8
Feb 01/07
IAC
Frame 1 and Pressure Bulkhead
Figure 005
R
EFF :
001-012, 53-10-00
Page 9
May 01/01
IAC
R **ON A/C 014-099, 101-199, 901-999,
C. Frames
R
EFF :
014-099, 101-199, 901-999, 53-10-00
Page 10
Feb 01/07
IAC
Frame 1 and Pressure Bulkhead
Figure 005A
R
EFF :
014-099, 101-199, 901-999, 53-10-00
Page 11
Feb 01/07
IAC
**ON A/C ALL
(2) Frame 2
(Ref. Fig. 006)
The top of the frame is closed by a machined curved member the upper
section of which is straight. This provides a forward attachment
point for the instrument panel and the frame for the windshield. The
lateral and lower curved members are formed from folded Z-section
sheet.
(3) Frame 3
Consists of machined lateral and lower curved members. Its upper
section is open.
(4) Frame 4
Consists of folded sheet lateral and lower curved members. Its upper
and lower sections are open.
(5) Frame 5
The lower curved member is machined and the lateral curved members
are formed from folded sheet.
(7) Frame 8
(Ref. Fig. 007)
This frame is closed and consists of machined upper, lateral and
lower curved members. The upper curved members form the posts between
the side windows. The frame supports a cross beam of the cockpit
floor. This cross beam is also supported by two rods which are
themselves supported by the lower section of the frame.
(8) Frame 9
(Ref. Fig. 008)
The frame which is open at the level of the side windows consists ;
of an upper curved member formed from folded sheet, and machined
lateral and upper curved members. The lower section provides the
forward bulkhead of the nose landing gear box. Two reinforcement rods
are attached to the top corners of the landing gear box and to the
lateral curved members of the frame.
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R
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Frames 2 and 4
Figure 006
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May 01/01
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Frame 8
Figure 007
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May 01/01
R
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Frame 9
Figure 008
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May 01/01
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(9) Frame 10
Consists of an upper curved member and lateral curved members formed
from folded sheet and two machined lower curved members attached to
the landing gear well.
(10) Frame 11
(Ref. Fig. 009)
The upper lateral and lower curved members are machined. The upper
curved members provide the aft posts of the side windows. A floor
cross beam is secured to the frame. This cross beam is supported by
two rods which are supported by the landing gear well.
(11) Frame 12
The upper and lateral curved members are formed from folded sheet.
They comprise an extruded T-section and a splice which provide the
skin joint. The lower curved members are machined. This frame
supports a cross beam of the floor reinforced by two rods attached to
the landing gear well.
(15) Frame 18
The upper curved member is formed from folded sheet and the lower
curved members are machined.
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Frame 11
Figure 009
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May 01/01
R
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Frame 16
Figure 010
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May 01/01
R
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Frame 17
Figure 011
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May 01/01
R
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Frame 20
Figure 012
R
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(17) Frame 23
This frame is closed. The upper and lateral curved members are formed
from folded sheet and the lower curved member is machined. This frame
supports a cross beam of the floor reinforced by two struts.
D. Floors
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Typical Floor Assemblies
Figure 013
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Page 22
May 01/01
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Typical Floor Assemblies
Figure 013A
R
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Page 23
Feb 01/07
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MAIN STRUCTURE - INSPECTION/CHECK
_________________________________
TASK 53-11-00-210-001
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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3. __________
Job Set-up
Subtask 53-11-00-010-050
A. Get Access
Subtask 53-11-00-110-051
R (1) Clean the inspection areas with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
4. Procedure
_________
Subtask 53-11-00-220-066
A. Inspection
(Ref. Fig. 601/TASK 53-11-00-991-001)
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Page 602
May 01/03
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R Upper Corners of the Door Frame of the Forward Passenger/Crew Door
Figure 601/TASK 53-11-00-991-001
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Page 603
May 01/03
IAC
(b) other damage (cracks, scratches, stress, marks, dents,
bumps,...):
R - If you find other damage, refer to the Structural Repair Manual
R (Ref. SRM 511100 P.Block 001) for damage classification and
R corrective action.
5. Close-up
________
Subtask 53-11-00-410-050
A. Close Access
R
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
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Page 604
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TASK 53-11-00-210-002
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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3. __________
Job Set-up
Subtask 53-11-00-010-051
A. Get Access
R (2) Open the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
010-001).
Subtask 53-11-00-020-057
R (1) Remove the forward corner of the scuff plate of the forward
R passenger/crew door (Ref. TASK 53-15-15-000-001).
Subtask 53-11-00-110-052
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
4. Procedure
_________
Subtask 53-11-00-220-067
A. Inspection
(Ref. Fig. 602/TASK 53-11-00-991-002)
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Page 606
May 01/03
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R Door Frame below the Forward Lower Corner of the Scuff Plate
Figure 602/TASK 53-11-00-991-002
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May 01/03
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(2) Make sure that there is no:
5. Close-up
________
Subtask 53-11-00-420-055
R (1) Install the forward corner of the scuff plate of the forward
R passenger/crew door(Ref. TASK 53-15-15-400-001).
Subtask 53-11-00-410-051
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R (2) Close the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
410-001).
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TASK 53-11-00-210-028
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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Page 609
May 01/03
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3. __________
Job Set-up
Subtask 53-11-00-010-068
A. Get Access
R (2) Open the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
010-001).
Subtask 53-11-00-020-064
R (1) Remove the forward corner of the scuff plate from the sill of the
R forward passenger/crew door (Ref. TASK 53-15-15-000-001).
Subtask 53-11-00-110-053
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
(2) Make sure that the surface of the inspection area is clean and
smooth.
EFF :
ALL 53-11-00
Page 610
May 01/03
IAC
R Door Frame - Forward Lower Corner below Scuff Plate - Inspection Area
R Figure 603/TASK 53-11-00-991-072
EFF :
ALL 53-11-00
Page 611
Nov 01/99
IAC
(4) Make sure that there is no:
4. Procedure
_________
Subtask 53-11-00-270-050
A. Inspection
(Ref. Fig. 603/TASK 53-11-00-991-072)
5. Close-up
________
Subtask 53-11-00-420-062
R (1) Install the forward corner of the scuff plate on the sill of the
R forward passenger/crew door (Ref. TASK 53-15-15-400-001)
EFF :
ALL 53-11-00
Page 612
May 01/03
IAC
Subtask 53-11-00-410-068
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R (2) Close the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
410-001).
EFF :
ALL 53-11-00
Page 613
May 01/03
IAC
TASK 53-11-00-210-003
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page 614
May 01/03
IAC
3. __________
Job Set-up
Subtask 53-11-00-010-052
A. Get Access
Subtask 53-11-00-110-054
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
4. Procedure
_________
Subtask 53-11-00-220-068-A
A. Inspection
(Ref. Fig. 604/TASK 53-11-00-991-003)
EFF :
ALL 53-11-00
Page 615
May 01/03
IAC
R Forward Face of the Forward Pressure Bulkhead
Figure 604/TASK 53-11-00-991-003
EFF :
ALL 53-11-00
Page 616
May 01/03
IAC
(2) Make sure that there is no:
5. Close-up
________
Subtask 53-11-00-410-052
A. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-11-00
Page 617
May 01/03
IAC
R **ON A/C 001-012, 014-019,
R TASK 53-11-00-210-808
R General Visual Inspection of Entrance Stairs Door Surround, Upper and Lower
R Corners, External Surface, LH
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R
EFF :
001-012, 014-019, 53-11-00
Page 618
May 01/03
IAC
R 3. __________
Job Set-up
R Subtask 53-11-00-010-099
R A. Get Access
R Subtask 53-11-00-110-114
R (1) Clean the inspection areas with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
R 4. Procedure
_________
R Subtask 53-11-00-210-088
R A. Inspection
R (Ref. Fig. 605/TASK 53-11-00-991-082)
R
EFF :
001-012, 014-019, 53-11-00
Page 619
May 01/03
IAC
R Entrance-Stairs Door Surround - Upper and Lower Corners - External Surface
R Figure 605/TASK 53-11-00-991-082
R
EFF :
001-012, 014-019, 53-11-00
Page 620
May 01/03
IAC
R (b) other damage (cracks, scratches, stress, marks, dents,
R bumps,...):
R - If you find other damage, refer to the Structural Repair Manual
R (Ref. SRM 511100 P.Block 001) for damage classification and
R corrective action.
R 5. Close-up
________
R Subtask 53-11-00-410-099
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R
EFF :
001-012, 014-019, 53-11-00
Page 621
May 01/03
IAC
R **ON A/C ALL
R TASK 53-11-00-210-809
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page 622
May 01/03
IAC
R 3. __________
Job Set-up
R Subtask 53-11-00-941-088
R A. Get Access
R (1) Put an access platform in position at the zones 811, 812, 822 and
R 824.
R Subtask 53-11-00-110-115
R (1) Clean the inspection areas with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
R 4. Procedure
_________
R Subtask 53-11-00-210-089
R A. Inspection
R (Ref. Fig. 606/TASK 53-11-00-991-083)
EFF :
ALL 53-11-00
Page 623
May 01/03
IAC
R Avionics Compartment Doors - External Surface
R Figure 606/TASK 53-11-00-991-083- 12 (SHEET 1)
EFF :
ALL 53-11-00
Page 624
May 01/03
IAC
R Avionics Compartment Doors - External Surface
R Figure 606/TASK 53-11-00-991-083- 22 (SHEET 2)
EFF :
ALL 53-11-00
Page 625
May 01/03
IAC
R (2) Make sure that there is no:
R 5. Close-up
________
R Subtask 53-11-00-942-096
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
EFF :
ALL 53-11-00
Page 626
May 01/03
IAC
R TASK 53-11-00-210-810
R General Visual Inspection of Fuselage Side Panel, below Cockpit Side Windows,
R between FR 1 and FR 12, External Surface, LH/RH
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page 627
May 01/03
IAC
R 3. __________
Job Set-up
R Subtask 53-11-00-941-085
R A. Get Access
R (1) Put an access platform in position at the zones 211 and 212.
R Subtask 53-11-00-110-116
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
R 4. Procedure
_________
R Subtask 53-11-00-210-090
R A. Inspection
R (Ref. Fig. 607/TASK 53-11-00-991-079)
EFF :
ALL 53-11-00
Page 628
May 01/03
IAC
R Fuselage Side Panel below Cockpit Side Windows - External Surface
R Figure 607/TASK 53-11-00-991-079
EFF :
ALL 53-11-00
Page 629
May 01/03
IAC
R (b) Other damage (cracks, scratches, stress, marks, dents,
R bumps,...):
R - If you find other damage, refer to the Structural Repair Manual
R (Ref. SRM 511100 P.Block 001) for damage classification and
R corrective action.
R 5. Close-up
________
R Subtask 53-11-00-942-093
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
EFF :
ALL 53-11-00
Page 630
May 01/03
IAC
R TASK 53-11-00-210-811
R General Visual Inspection of Area Forward of Windshield, above Side Panel, from
R FR 0 to FR 4, External Surface, LH/RH
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page 631
May 01/03
IAC
R 3. __________
Job Set-up
R Subtask 53-11-00-941-087
R A. Get Access
R (1) Put an access platform in position at the zones 211 and 212.
R Subtask 53-11-00-110-117
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
R 4. Procedure
_________
R Subtask 53-11-00-210-091
R A. Inspection
R (Ref. Fig. 608/TASK 53-11-00-991-080)
EFF :
ALL 53-11-00
Page 632
May 01/03
IAC
R External Fuselage Structure - Area forward of the Windshield - External Surface
R Figure 608/TASK 53-11-00-991-080
EFF :
ALL 53-11-00
Page 633
May 01/03
IAC
R (b) Other damage (cracks, scratches, stress, marks, dents,
R bumps,...):
R - If you find other damage, refer to the Structural Repair Manual
R (Ref. SRM 511100 P.Block 001) for damage classification and
R corrective action.
R 5. Close-up
________
R Subtask 53-11-00-942-095
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
EFF :
ALL 53-11-00
Page 634
May 01/03
IAC
TASK 53-11-00-210-005
R Detailed Inspection of Fuselage Lower Panel at NLG Bay Aft Corners, External
R Surface, LH/RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page 635
May 01/03
IAC
3. __________
Job Set-up
R Subtask 53-11-00-941-089
R A. Get Access
Subtask 53-11-00-110-057
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
4. Procedure
_________
Subtask 53-11-00-220-070
A. Inspection
R (Ref. Fig. 609/TASK 53-11-00-991-005)
EFF :
ALL 53-11-00
Page 636
May 01/03
IAC
Edges of the Corners of the Nose-Gear Door Frame
R Figure 609/TASK 53-11-00-991-005
EFF :
ALL 53-11-00
Page 637
May 01/03
IAC
(b) other damage (cracks, scratches, stress, marks, dents,
bumps,...):
R - If you find other damage, refer to the Structural Repair Manual
R (Ref. SRM 511100 P.Block 001) for damage classification and
R corrective action.
R 5. Close-up
________
R Subtask 53-11-00-942-097
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
EFF :
ALL 53-11-00
Page 638
May 01/03
IAC
TASK 53-11-00-210-006
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page 639
May 01/03
IAC
3. __________
Job Set-up
Subtask 53-11-00-941-054
A. Get Access
Subtask 53-11-00-110-058
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
4. Procedure
_________
Subtask 53-11-00-220-071
A. Inspection
R (Ref. Fig. 610/TASK 53-11-00-991-006)
EFF :
ALL 53-11-00
Page 640
May 01/03
IAC
R Upper Skin Panels above the Windshield
R Figure 610/TASK 53-11-00-991-006
EFF :
ALL 53-11-00
Page 641
May 01/03
IAC
(b) other damage (cracks, scratches, stress, marks, dents,
bumps,...):
R - If you find other damage, refer to the Structural Repair Manual
R (Ref. SRM 511100 P.Block 001) for damage classification and
R corrective action.
5. Close-up
________
Subtask 53-11-00-942-054
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-11-00
Page 642
May 01/03
IAC
TASK 53-11-00-210-007
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page 643
May 01/03
IAC
3. __________
Job Set-up
Subtask 53-11-00-941-055
A. Get Access
Subtask 53-11-00-110-059
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
4. Procedure
_________
Subtask 53-11-00-220-072
A. Inspection
R (Ref. Fig. 611/TASK 53-11-00-991-007)
R (1) Do a detailed inspection of the structure of the lap joint from FR9
R to FR20, L and R sides.
EFF :
ALL 53-11-00
Page 644
May 01/03
IAC
Lap Joint from FR9 to FR20
R Figure 611/TASK 53-11-00-991-007
EFF :
ALL 53-11-00
Page 645
May 01/03
IAC
(b) other damage (cracks, scratches, stress, marks, dents,
bumps,...):
R - If you find other damage, refer to the Structural Repair Manual
R (Ref. SRM 511100 P.Block 001) for damage classification and
R corrective action.
5. Close-up
________
Subtask 53-11-00-942-055
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-11-00
Page 646
May 01/03
IAC
TASK 53-11-00-210-008
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-11-00
Page 647
May 01/03
IAC
3. __________
Job Set-up
Subtask 53-11-00-941-056
A. Get Access
Subtask 53-11-00-110-060
R (1) Clean the inspection areas with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
4. Procedure
_________
Subtask 53-11-00-220-073
A. Inspection
R (Ref. Fig. 612/TASK 53-11-00-991-008)
R
EFF :
ALL 53-11-00
Page 648
May 01/03
IAC
R Upper-Longitudinal Lap Joints - Upper Skin - External Surface from FR15 to FR16
R and FR20 to FR24
R Figure 612/TASK 53-11-00-991-008
R EFF :
ALL
53-11-00 Page 649
May 01/03
IAC
(b) other damage (cracks, scratches, stress, marks, dents,
bumps,...):
R - If you find other damage, refer to the Structural Repair Manual
R (Ref. SRM 511100 P.Block 001) for damage classification and
R corrective action.
5. Close-up
________
Subtask 53-11-00-942-056
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
ALL 53-11-00
Page 650
May 01/03
IAC
TASK 53-11-00-210-009
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-11-00
Page 651
May 01/03
IAC
3. __________
Job Set-up
Subtask 53-11-00-941-057
A. Get Access
Subtask 53-11-00-110-061
R (1) Clean the inspection areas with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
4. Procedure
_________
Subtask 53-11-00-220-074
A. Inspection
R (Ref. Fig. 613/TASK 53-11-00-991-009)
R
EFF :
ALL 53-11-00
Page 652
May 01/03
IAC
R Lateral-Longitudinal Lap Joints - Outer Skin from FR11 to FR14 and FR20 to FR24
R Figure 613/TASK 53-11-00-991-009
R
EFF :
ALL 53-11-00
Page 653
May 01/03
IAC
(b) other damage (cracks, scratches, stress, marks, dents,
bumps,...):
R - If you find other damage, refer to the Structural Repair Manual
R (Ref. SRM 511100 P.Block 001) for damage classification and
R corrective action.
5. Close-up
________
Subtask 53-11-00-942-057
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
ALL 53-11-00
Page 654
May 01/03
IAC
TASK 53-11-00-210-010
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-11-00
Page 655
May 01/03
IAC
3. __________
Job Set-up
Subtask 53-11-00-941-058
A. Get Access
Subtask 53-11-00-110-064
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
4. Procedure
_________
Subtask 53-11-00-220-075
A. Inspection
R (Ref. Fig. 614/TASK 53-11-00-991-010)
R
EFF :
ALL 53-11-00
Page 656
May 01/03
IAC
R Lateral-Longitudinal Lap Joints - Outer Skin from FR1 to FR24
R Figure 614/TASK 53-11-00-991-010
EFF :
ALL 53-11-00
Page 657
May 01/03
IAC
(b) other damage (cracks, scratches, stress, marks, dents,
bumps,...):
R - If you find other damage, refer to the Structural Repair Manual
R (Ref. SRM 511100 P.Block 001) for damage classification and
R corrective action.
5. Close-up
________
Subtask 53-11-00-942-058
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-11-00
Page 658
May 01/03
IAC
TASK 53-11-00-210-011
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page 659
May 01/03
IAC
3. __________
Job Set-up
Subtask 53-11-00-010-054
A. Get Access
R (2) Open the lateral avionics-compartment door 824 (Ref. TASK 52-41-00-
R 010-002).
Subtask 53-11-00-020-058
R (1) Remove the insulation at the FR20 in the area of the left and right
R STGR31 (Ref. TASK 25-80-00-000-001).
R (2) Remove part of the gasket (left and right sides), if installed.
Subtask 53-11-00-110-065
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
EFF :
ALL 53-11-00
Page 660
May 01/03
IAC
4. Procedure
_________
Subtask 53-11-00-220-076
A. Inspection
R (Ref. Fig. 615/TASK 53-11-00-991-025)
5. Close-up
________
Subtask 53-11-00-420-056
R (2) Install the insulation blankets at FR20 in the area of the left and
R right STGR31 (Ref. TASK 25-80-00-400-001).
EFF :
ALL 53-11-00
Page 661
May 01/03
IAC
R Splices of the FR20 at the STGR30 and STGR32
R Figure 615/TASK 53-11-00-991-025
EFF :
ALL 53-11-00
Page 662
May 01/03
IAC
**ON A/C ALL
Subtask 53-11-00-410-054
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Close the lateral avionics-compartment door 824 (Ref. TASK 52-41-00-
410-002).
R
EFF :
ALL 53-11-00
Page 663
May 01/03
IAC
**ON A/C 001-012, 014-019,
TASK 53-11-00-210-012
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
001-012, 014-019, 53-11-00
Page 664
May 01/03
IAC
3. __________
Job Set-up
Subtask 53-11-00-010-055
A. Get Access
R (2) Open the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
010-001).
R (3) Remove the vertical lining panel 211MW and the lining panel 211LW
R from the windshield center post.
R
R (Ref. Fig. 616/TASK 53-11-00-991-038)
R
Subtask 53-11-00-110-066
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a clint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
4. Procedure
_________
Subtask 53-11-00-220-077
A. Inspection
R (Ref. Fig. 617/TASK 53-11-00-991-012)
R
EFF :
001-012, 014-019, 53-11-00
Page 665
May 01/03
IAC
Lining Panels near the Windshield Center Post
R Figure 616/TASK 53-11-00-991-038
R
EFF :
001-012, 014-019, 53-11-00
Page 666
May 01/03
IAC
R Windshield Center Post - Lower Attachment
R Figure 617/TASK 53-11-00-991-012
R
EFF :
001-012, 014-019, 53-11-00
Page 667
May 01/03
IAC
(2) Make sure that there is no:
5. Close-up
________
Subtask 53-11-00-410-055
A. Close Access
(Ref. Fig. 616/TASK 53-11-00-991-038)
(1) Install the lining panel 211MW and the vertical lining panel 211LW on
the windshield center post.
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Close the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
410-001).
EFF :
001-012, 014-019, 53-11-00
Page 668
Nov 01/03
R
IAC
TASK 53-11-00-220-001
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
001-012, 014-019, 53-11-00
Page 669
May 01/03
IAC
3. __________
Job Set-up
Subtask 53-11-00-010-071
A. Get Access
R (2) Open the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
010-001).
R (3) Remove the vertical lining panel 211MW and the lining panel 211LW
R from the windshield center post.
R
R (Ref. Fig. 616/TASK 53-11-00-991-038)
R
Subtask 53-11-00-110-067
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
(2) Make sure that the surface of the inspection area is clean and
smooth.
R
EFF :
001-012, 014-019, 53-11-00
Page 670
May 01/03
IAC
R Windshield Center Post - Lower Attachment - Internal Side
R Figure 618/TASK 53-11-00-991-073
R
EFF :
001-012, 014-019, 53-11-00
Page 671
May 01/03
IAC
(4) Make sure that there is no:
4. Procedure
_________
Subtask 53-11-00-250-050
A. Inspection
R (Ref. Fig. 618/TASK 53-11-00-991-073)
5. Close-up
________
Subtask 53-11-00-410-071
A. Close Access
R (Ref. Fig. 617/TASK 53-11-00-991-012)
R (1) Install the lining panel 211LW and the vertical lining panel 211MW on
R the windshield center post.
R
R
EFF :
001-012, 014-019, 53-11-00
Page 672
May 01/03
IAC
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Close the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
410-001).
EFF :
001-012, 014-019, 53-11-00
Page 673
Nov 01/05
IAC
**ON A/C ALL
TASK 53-11-00-210-013
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-11-00
Page 674
Nov 01/05
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-056
A. Get Access
(2) Open the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
010-001).
(3) Remove the vertical lining panels 211MC, 211MW from the windshield
center post.
R
(Ref. Fig. 619/TASK 53-11-00-991-039)
R
(4) Remove the ceiling panels 211LC, 212LC.
R
(Ref. Fig. 619/TASK 53-11-00-991-039)
EFF :
ALL 53-11-00
Page 675
May 01/06
IAC
Linings of the Upper Attachment of the Windshield Center Post
Figure 619/TASK 53-11-00-991-039
R
EFF :
ALL 53-11-00
Page 676
May 01/06
IAC
R
Subtask 53-11-00-110-068
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-078
A. Inspection
(Ref. Fig. 620/TASK 53-11-00-991-014)
EFF :
ALL 53-11-00
Page 677
May 01/06
IAC
Upper Attachment of the Windshield Center Post - Internal Side
R Figure 620/TASK 53-11-00-991-014
EFF :
ALL 53-11-00
Page 678
Nov 01/05
IAC
5. Close-up
________
Subtask 53-11-00-410-056
A. Close Access
(2) Install the lining panels 211MC, 211MW on the windshield center post.
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Close the forward passenger/crew door 831 841 (Ref. TASK 52-10-00-
410-001).
EFF :
ALL 53-11-00
Page 679
May 01/06
R
IAC
R **ON A/C 001-012, 014-099,
TASK 53-11-00-210-014
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
001-012, 014-099, 53-11-00
Page 680
May 01/06
IAC
3. __________
Job Set-up
Subtask 53-11-00-010-057
A. Get Access
(2) Open the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
010-001).
(5) Remove the lining panel 211NW (212NW) from the side post at FR4.
(Ref. Fig. 621/TASK 53-11-00-991-040)
Subtask 53-11-00-110-069
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-079
A. Inspection
(Ref. Fig. 622/TASK 53-11-00-991-015)
R
EFF :
001-012, 014-099, 53-11-00
Page 681
May 01/06
IAC
Linings of the Lower Area of the Side Post at FR4
Figure 621/TASK 53-11-00-991-040
R
EFF :
001-012, 014-099, 53-11-00
Page 682
May 01/06
IAC
Lower Attachment Area of the Windshield Side Post at FR4 - Internal Side
Figure 622/TASK 53-11-00-991-015
R
EFF :
001-012, 014-099, 53-11-00
Page 683
May 01/06
IAC
(2) Make sure that there is no:
5. Close-up
________
Subtask 53-11-00-410-057
A. Close Access
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
410-001).
R
EFF :
001-012, 014-099, 53-11-00
Page 684
May 01/06
IAC
TASK 53-11-00-210-029
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
001-012, 014-099, 53-11-00
Page 685
May 01/06
IAC
3. __________
Job Set-up
Subtask 53-11-00-010-069
A. Get Access
(2) Open the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
010-001).
(5) Remove the lining panel 211NW (212NW) from the side post at FR4.
(Ref. Fig. 621/TASK 53-11-00-991-040)
Subtask 53-11-00-110-070
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
(2) Make sure that the surface of the inspection area is clean and
smooth.
R
EFF :
001-012, 014-099, 53-11-00
Page 686
May 01/06
IAC
Lower Attachment Area of the Windshield Side Post at FR4 - Internal Side
Figure 623/TASK 53-11-00-991-075
R
EFF :
001-012, 014-099, 53-11-00
Page 687
May 01/06
IAC
(4) Make sure that there is no:
4. Procedure
_________
Subtask 53-11-00-250-057
A. Inspection
(Ref. Fig. 623/TASK 53-11-00-991-075)
5. Close-up
________
Subtask 53-11-00-410-069
A. Close Access
(1) Install the lining panel 211NW (212NW) on the side post at FR4.
R
EFF :
001-012, 014-099, 53-11-00
Page 688
May 01/06
IAC
(3) Close the sliding window.
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
410-001).
R
EFF :
001-012, 014-099, 53-11-00
Page 689
May 01/06
IAC
**ON A/C ALL
TASK 53-11-00-210-026
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page 690
May 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-066
A. Get Access
(2) Open the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
010-001).
EFF :
ALL 53-11-00
Page 691
Nov 01/05
IAC
Lining Panels of the Windshield Side Post at FR4
R Figure 624/TASK 53-11-00-991-041
EFF :
ALL 53-11-00
Page 692
Nov 01/05
IAC
(5) Remove the lining panels 211BC, 211KC, 211LC (212BC, 212KC, 212LC).
R (Ref. Fig. 624/TASK 53-11-00-991-041)
Subtask 53-11-00-020-062
Subtask 53-11-00-020-062-A
Subtask 53-11-00-110-071
EFF :
ALL 53-11-00
Page 693
Nov 01/05
IAC
Bolts at the Upper Attachment of the Windshield Side Post, at FR4
R Figure 625/TASK 53-11-00-991-042
R
EFF :
001-012, 014-019, 53-11-00
Page 694
Nov 01/05
IAC
Bolts at the Upper Attachment of the Windshield Side Post, at FR4
R Figure 625A/TASK 53-11-00-991-042-B
EFF :
ALL 53-11-00
Page 695
Nov 01/05
IAC
Windshield Side Post at FR4 - Upper Attachment
R Figure 626/TASK 53-11-00-991-069
R
EFF :
001-012, 014-019, 53-11-00
Page 696
Nov 01/05
IAC
Windshield Side Post at FR4 - Upper Attachment
R Figure 626A/TASK 53-11-00-991-069-A
EFF :
ALL 53-11-00
Page 697
Nov 01/05
IAC
**ON A/C ALL
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
(2) Make sure that the surface of the inspection area is clean and
smooth.
R
EFF :
ALL 53-11-00
Page 698
Nov 01/05
IAC
4. Procedure
_________
Subtask 53-11-00-250-055
A. Inspection
R (Ref. Fig. 626/TASK 53-11-00-991-069)
Subtask 53-11-00-250-055-A
A. Inspection
R (Ref. Fig. 626A/TASK 53-11-00-991-069-A)
EFF :
ALL 53-11-00
Page 699
Nov 01/05
IAC
(b) Other damage (cracks, scratches, stress, marks, dents, bumps...):
- If you find this type of damage, refer to the Structural Repair
Manual (Ref. SRM 511100,P.Block 001) for damage classification
and corrective action.
5. Close-up
________
Subtask 53-11-00-914-050
(1) Make sure that the parts retained from the removed component are
clean and in the correct condition.
(2) Apply a bead of SEALANTS (Material No. 09-005) around the bolts (1)
and the nuts (2).
Subtask 53-11-00-420-060
R (1) Install the 14 bolts (1) and the new nuts (2). Refer to the
R Structural Repair Manual (Ref. SRM 514211,P.Block 001).
Subtask 53-11-00-420-060-A
R (1) Install the 3 bolts (1) and the new nuts (2). Refer to the Structural
R Repair Manual (Ref. SRM 514211,P.Block 001).
EFF :
ALL 53-11-00
Page A600
May 01/07
IAC
**ON A/C ALL
Subtask 53-11-00-410-066
C. Close Access
(1) Install the lining panels 211BC, 211KC, 211LC (212BC, 212KC, 212LC).
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
410-001).
EFF :
ALL 53-11-00
Page A601
Nov 01/05
R
IAC
TASK 53-11-00-210-015
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A602
Nov 01/05
IAC
3. __________
Job Set-up
Subtask 53-11-00-941-063
A. Get Access
Subtask 53-11-00-110-072
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-080
A. Inspection
R (Ref. Fig. 627/TASK 53-11-00-991-016)
EFF :
ALL 53-11-00
Page A603
Nov 01/05
IAC
External Surface of the Upper Junction of the Side Window Stucture - Forward
and Aft of the Frame
R Figure 627/TASK 53-11-00-991-016
EFF :
ALL
53-11-00 Page A604
Nov 01/05
IAC
(b) other damage (cracks, scratches, stress, marks, dents,
bumps,...):
- If you find other damage, refer to the Structural Repair Manual
(Ref. SRM 511100 P.Block 001) for damage classification and
corrective action.
5. Close-up
________
Subtask 53-11-00-942-063
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-11-00
Page A605
Nov 01/05
R
IAC
TASK 53-11-00-210-017
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A606
Nov 01/05
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-059
A. Get Access
(2) Open the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
010-001).
Subtask 53-11-00-110-073
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
EFF :
ALL 53-11-00
Page A607
Nov 01/05
IAC
4. Procedure
_________
Subtask 53-11-00-220-081
A. Inspection
R (Ref. Fig. 628/TASK 53-11-00-991-018)
5. Close-up
________
Subtask 53-11-00-410-059
A. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Close the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
410-001).
EFF :
ALL 53-11-00
Page A608
Nov 01/05
IAC
Stop Fittings on the Frame of the Forward Passenger/Crew Door - Left and Right
Sides
R Figure 628/TASK 53-11-00-991-018
EFF :
ALL
53-11-00 Page A609
Nov 01/05
IAC
TASK 53-11-00-210-025
Special Detailed Inspection of Door Frame 16, at Double Joggle Area in Outer
Flange of Frame at Door Stops Number 1 and 7 Location, LH/RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A610
Nov 01/06
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-065
A. Get Access
(2) Open the forward passenger/crew door 831 (841), and lock it in the
open position (Ref. TASK 52-10-00-010-001).
EFF :
ALL 53-11-00
Page A611
May 01/07
IAC
Subtask 53-11-00-020-061
(2) Remove the threaded pins (HI-LITE) (1) and the nuts (2). Refer to the
R Structural Repair Manual (Ref. SRM 514211, P.Block 001).
(Ref. Fig. 629/TASK 53-11-00-991-043)
(3) Remove the FWD galleys (Ref. TASK 25-31-41-000-001), (Ref. TASK 25-
31-41-000-002), (Ref. TASK 25-31-41-000-008), (Ref. TASK 25-31-41-
000-013), if installed.
Subtask 53-11-00-110-074
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
(2) Make sure that the surface of the inspection area is clean and
smooth.
EFF :
ALL 53-11-00
Page A612
May 01/07
IAC
Bolts at the Outer Flange of the Frame at the Double Joggle Area (FR16)
R Figure 629/TASK 53-11-00-991-043
EFF :
ALL 53-11-00
Page A613
Nov 01/05
IAC
Door Frame FR16 - Inspection Areas
R Figure 630/TASK 53-11-00-991-070
EFF :
ALL 53-11-00
Page A614
Nov 01/05
IAC
(4) Make sure that there is no:
4. Procedure
_________
Subtask 53-11-00-250-054
A. Inspection
(Ref. Fig. 630/TASK 53-11-00-991-070)
(1) Do a special detailed inspection of the door frame 16, left and right
sides. This inspection is applicable at the double joggle area in the
outer flange of the frame (at the door stops Number 1 and 7).
R Refer to the Non-destructive Testing Manual (Ref. NTM 531153, P.Block
R 601).
5. Close-up
________
Subtask 53-11-00-914-051
(1) Make sure that the parts retained from the removed component are
clean and in the correct condition.
(2) Apply a bead of SEALANTS (Material No. 09-005) around the screws (1)
and the nuts (2).
EFF :
ALL 53-11-00
Page A615
May 01/07
IAC
Subtask 53-11-00-420-059
(2) Install the FWD galleys (Ref. TASK 25-31-41-400-001), (Ref. TASK 25-
31-41-400-002), (Ref. TASK 25-31-41-400-008), (Ref. TASK 25-31-41-
400-013), if removed.
R (3) Install the threaded pins (HI-LITE) (1) with SEALANTS (Material No.
R 09-016) and the new nuts (2). Refer to the Structural Repair Manual
R (Ref. SRM 514211, P.Block 001).
(Ref. Fig. 629/TASK 53-11-00-991-043)
Subtask 53-11-00-410-065
C. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
410-001).
EFF :
ALL 53-11-00
Page A616
May 01/07
IAC
TASK 53-11-00-210-027
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A617
Nov 01/05
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-067
A. Get Access
(2) Open the forward passenger/crew door 831 (841), and lock it in the
open position (Ref. TASK 52-10-00-010-001).
Subtask 53-11-00-020-063
(2) Remove the threaded pins (HI-LITE) (1) and the nuts (2).
Refer to the Structural Repair Manual (Ref. SRM 514211,P.Block 001).
R (Ref. Fig. 631/TASK 53-11-00-991-044)
EFF :
ALL 53-11-00
Page A618
Nov 01/05
IAC
Bolts at the Outer Flange of FR20 at the Double Joggle Area
R Figure 631/TASK 53-11-00-991-044
EFF :
ALL 53-11-00
Page A619
Nov 01/05
IAC
Subtask 53-11-00-110-075
(1) Clean the inspection surface with CLEANING AGENTS (Material No. 11-
004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-
003), if necessary.
(2) Make sure that the surface of the inspection area is clean and
smooth.
EFF :
ALL 53-11-00
Page A620
Nov 01/05
IAC
Door Stops at FR20 - Inspection Area
R Figure 632/TASK 53-11-00-991-071
EFF :
ALL 53-11-00
Page A621
Nov 01/05
IAC
4. Procedure
_________
Subtask 53-11-00-250-056
A. Inspection
R (Ref. Fig. 632/TASK 53-11-00-991-071)
(1) Do a special detailed inspection of the door FR20, left and right
sides. This inspection is applicable at the double joggle area in the
outer flange of the frame (at the door stops 1 and 7).
Refer to the Non-destructive Testing Manual (Ref. NTM 531155,P.Block-
601).
5. Close-up
________
Subtask 53-11-00-914-052
(1) Make sure that the parts retained from the removed component are
clean and in the correct condition.
(2) Apply a bead of SEALANTS (Material No. 09-005) around the screws (1)
and the nuts (2).
Subtask 53-11-00-420-061
(1) Install the threaded pins (HI-LITE) (1) and the nuts (2).
Refer to the Structural Repair Manual (Ref. SRM 514211,P.Block 001).
R (Ref. Fig. 631/TASK 53-11-00-991-044)
EFF :
ALL 53-11-00
Page A622
Nov 01/05
IAC
Subtask 53-11-00-410-067
C. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
410-001).
EFF :
ALL 53-11-00
Page A623
Nov 01/05
R
IAC
TASK 53-11-00-210-021
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A624
Nov 01/05
IAC
3. __________
Job Set-up
Subtask 53-11-00-010-062
A. Get Access
(2) Open the lateral avionics-compartment door 824 (Ref. TASK 52-41-00-
010-002).
Subtask 53-11-00-020-060-A
(1) Remove the two quick-release pins (1) and lift and remove the ladder
(2), if necessary.
(2) Remove the floor panel 127CG (4) of the avionics compartment
(Ref. TASK 53-12-13-000-001).
Subtask 53-11-00-020-060-B
(1) Remove the two quick-release pins (1) and lift and remove the ladder
(2), if necessary.
(2) Remove the floor panel 127BG (4) of the avionics compartment
(Ref. TASK 53-12-13-000-001).
EFF :
ALL 53-11-00
Page A625
Feb 01/07
IAC
Ladder
R Figure 633/TASK 53-11-00-991-093
EFF :
ALL 53-11-00
Page A626
Nov 01/05
IAC
R **ON A/C ALL
Subtask 53-11-00-110-076
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-085
A. Inspection
(Ref. Fig. 634/TASK 53-11-00-991-022)
EFF :
ALL 53-11-00
Page A627
May 01/06
IAC
Continuity Fitting between FR20 and FR21 and Angle Fittings at FR21
R Figure 634/TASK 53-11-00-991-022
EFF :
ALL 53-11-00
Page A628
Nov 01/05
IAC
5. Close-up
________
Subtask 53-11-00-420-058-A
(1) Install the floor panel 127CG (4) in the avionics compartment
(Ref. TASK 53-12-13-400-001).
(2) Install the ladder (2) on the floor fittings (3), if necessary, and
install the two quick-release pins (1).
Subtask 53-11-00-420-058-B
(1) Install the floor panel 127BG (4) in the avionics compartment
(Ref. TASK 53-12-13-400-001).
(2) Install the ladder (2) on the floor fittings (3), if necessary, and
install the two quick-release pins (1).
Subtask 53-11-00-410-062
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Close the lateral avionics-compartment door 824 (Ref. TASK 52-41-00-
410-002).
EFF :
ALL 53-11-00
Page A629
Feb 01/07
IAC
TASK 53-11-00-210-803
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
A. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A630
Nov 01/05
IAC
3. __________
Job Set-up
Subtask 53-11-00-010-094
A. Get Access
(1) Open the nose landing-gear doors 713 (714) (Ref. TASK 32-22-00-010-
001).
Subtask 53-11-00-110-109
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-210-083
A. Inspection
R (Ref. Fig. 635/TASK 53-11-00-991-064)
EFF :
ALL 53-11-00
Page A631
Nov 01/05
IAC
Nose-Landing-Gear Well Panels
R Figure 635/TASK 53-11-00-991-064
EFF :
ALL 53-11-00
Page A632
Nov 01/05
IAC
(b) other damage (cracks, scratches, stress, marks, dents,
bumps,...):
- If you find other damage, refer to the Structural Repair Manual
(Ref. SRM 511100 P.Block 001) for damage classification and
corrective action.
Subtask 53-11-00-916-066
(1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fittings adjacent to the
area.
5. Close-up
________
Subtask 53-11-00-410-094
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Close the nose landing-gear doors 713 (714) (Ref. TASK 32-22-00-410-
001).
EFF :
ALL 53-11-00
Page A633
Nov 01/05
R
IAC
TASK 53-11-00-210-018
Detailed Inspection of NLG Bay, Rear Panel Aft Face, Lower Corners, LH/RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A634
Nov 01/05
IAC
3. __________
Job Set-up
Subtask 53-11-00-010-060
A. Get Access
(2) Open the lateral avionics-compartment door 824 (Ref. TASK 52-41-00-
010-002).
Subtask 53-11-00-020-059-A
(1) Remove the two quick-release pins (1) and lift and remove the ladder
(2), if necessary.
(2) Remove the floor panel 127AG (4) of the avionics compartment
(Ref. TASK 53-12-13-000-001).
Subtask 53-11-00-020-059-B
(1) Remove the two quick-release pins (1) and lift and remove the ladder
(2), if necessary.
(2) Remove the floor panel 127BG (4) of the avionics compartment
(Ref. TASK 53-12-13-000-001).
EFF :
ALL 53-11-00
Page A635
Feb 01/07
IAC
NLG Well - Rear Panel Aft Face - Lower Corners
R Figure 636/TASK 53-11-00-991-019
EFF :
ALL 53-11-00
Page A636
Nov 01/05
IAC
R **ON A/C ALL
Subtask 53-11-00-110-077
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-082
A. Inspection
(Ref. Fig. 636/TASK 53-11-00-991-019)
EFF :
ALL 53-11-00
Page A637
May 01/06
IAC
5. Close-up
________
Subtask 53-11-00-420-057-A
(1) Install the floor panel 127AG (4) in the avionics compartment
(Ref. TASK 53-12-13-400-001).
(2) Install the ladder (2) on the floor fittings (3), if necessary, and
install the two quick-release pins (1).
Subtask 53-11-00-420-057-B
(1) Install the floor panel 127BG (4) in the avionics compartment
(Ref. TASK 53-12-13-400-001).
(2) Install the ladder (2) on the floor fittings (3), if necessary, and
install the two quick-release pins (1).
Subtask 53-11-00-410-060
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Close the lateral avionics-compartment door 824 (Ref. TASK 52-41-00-
410-002).
EFF :
ALL 53-11-00
Page A638
Feb 01/07
IAC
TASK 53-11-00-210-019
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A639
Nov 01/05
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-061
A. Get Access
(2) Open the forward passenger/crew door 831 (841), and lock it in the
open position (Ref. TASK 52-10-00-010-001).
(3) Remove the lining panels around the frame of the passenger/crew door
at FR16 and FR20:
- For the frame of the left door:
221AW, 221BW, 221CW, 221DW, 221EW, 221FW, 221GW, 221HW, 221JW,
221KW, 221LW, 221MW, 221NW, 221PW, 221QW. (Ref. TASK 25-23-45-000-
005)
- For the frame of the right door:
EFF :
ALL 53-11-00
Page A640
Nov 01/05
IAC
222AW, 222BW, 222CW, 222DW, 222EW, 222FW, 222GW, 222HW, 222JW,
222KW, 222LW, 222MW, 222NW, 222PW, 222QW. (Ref. TASK 25-23-45-000-
002)
(5) Remove the insulation blankets around the frame of the passenger/crew
door. (Ref. TASK 25-80-00-000-001)
Subtask 53-11-00-010-061-A
A. Get Access
(2) Open the forward passenger/crew door 831 (841), and lock it in the
open position (Ref. TASK 52-10-00-010-001).
(3) Remove the lining panels around the frame of the passenger/crew door
at FR16 and FR20:
- For the frame of the left door:
221AW, 221BW, 221CW, 221EW, 221FW, 221RW, 221SW, 221VW, (Ref. TASK
25-23-45-000-005).
- For the frame of the right door:
222RW, 222SW, 222TW, 222UW, 222VW, (Ref. TASK 25-23-45-000-002).
(5) Remove the insulation blankets around the frame of the passenger/crew
door. (Ref. TASK 25-80-00-000-001)
EFF :
ALL 53-11-00
Page A641
Feb 01/07
IAC
**ON A/C ALL
Subtask 53-11-00-110-078
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-083
A. Inspection
R (Ref. Fig. 637/TASK 53-11-00-991-020)
EFF :
ALL 53-11-00
Page A642
Nov 01/05
IAC
Internal Structure around the Passenger/Crew Doors
R Figure 637/TASK 53-11-00-991-020
EFF :
ALL 53-11-00
Page A643
Nov 01/05
IAC
Subtask 53-11-00-916-050
(1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fittings adjacent to the
area.
5. Close-up
________
Subtask 53-11-00-410-061
A. Close Access
(3) Install the lining panels around the frame of the passenger/crew door
at FR16 and FR20:
- For the left passenger/crew door:
221AW, 221BW, 221CW, 221DW, 221EW, 221FW, 221GW, 221HW, 221JW,
221KW, 221LW, 221MW, 221NW, 221PW, 221QW. (Ref. TASK 25-23-45-400-
006)
- For the right passenger/crew door:
EFF :
ALL 53-11-00
Page A644
Nov 01/05
R
IAC
222AW, 222BW, 222CW, 222DW, 222EW, 222FW, 222GW, 222HW, 222JW,
222KW, 222LW, 222MW, 222NW, 222PW, 222QW. (Ref. TASK 25-23-45-400-
007)
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Close the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
410-001).
Subtask 53-11-00-410-061-A
A. Close Access
(3) Install the lining panels around the frame of the passenger/crew door
at FR16 and FR20:
- For the left passenger/crew door:
221AW, 221BW, 221CW, 221EW, 221FW, 221RW, 221SW, 221VW, (Ref. TASK
25-23-45-400-006).
- For the right passenger/crew door:
222RW, 222SW, 222TW, 222UW, 222VW, (Ref. TASK 25-23-45-400-007).
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Close the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
410-001).
EFF :
ALL 53-11-00
Page A645
Feb 01/07
IAC
**ON A/C ALL
TASK 53-11-00-210-801
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-11-00
Page A646
Nov 01/05
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-093-A
A. Get Access
(2) Open the lateral avionics-compartment doors 812 (824) (Ref. TASK 52-
41-00-010-002).
Subtask 53-11-00-010-093
A. Get Access
(2) Open the lateral avionics-compartment doors 812 (824) (Ref. TASK 52-
41-00-010-002).
EFF :
ALL 53-11-00
Page A647
Feb 01/07
IAC
**ON A/C ALL
Subtask 53-11-00-110-107
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-090
A. Inspection
R (Ref. Fig. 638/TASK 53-11-00-991-045)
EFF :
ALL 53-11-00
Page A648
Nov 01/05
IAC
Internal Structure below the Forward Passenger/Crew Doors and the Cabin Floor
Level
R Figure 638/TASK 53-11-00-991-045
EFF :
ALL
53-11-00 Page A649
Nov 01/05
IAC
Subtask 53-11-00-916-065
(1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fittings adjacent to the
area.
5. Close-up
________
Subtask 53-11-00-410-093-A
A. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Close the lateral avionics-compartment doors 812 (824) (Ref. TASK 52-
41-00-410-002).
EFF :
ALL 53-11-00
Page A650
Nov 01/05
R
IAC
R **ON A/C 020-099, 101-199, 901-999,
Subtask 53-11-00-410-093
A. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Close the lateral avionics-compartment doors 812 (824) (Ref. TASK 52-
41-00-410-002).
R
EFF :
020-099, 101-199, 901-999, 53-11-00
Page A651
Feb 01/07
IAC
**ON A/C ALL
TASK 53-11-00-210-036
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A652
Nov 01/05
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-076
A. Get Access
(2) Open the avionics compartment door 822 (Ref. TASK 52-41-00-010-002).
Subtask 53-11-00-110-084
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
EFF :
ALL 53-11-00
Page A653
Nov 01/05
IAC
4. Procedure
_________
Subtask 53-11-00-220-052
A. Inspection
R (Ref. Fig. 639/TASK 53-11-00-991-048)
Subtask 53-11-00-916-055
(1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fittings adjacent to the
area.
EFF :
ALL 53-11-00
Page A654
Nov 01/05
IAC
5. Close-up
________
Subtask 53-11-00-410-076
A. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Close the avionics compartment door 822 (Ref. TASK 52-41-00-410-002)
.
EFF :
ALL 53-11-00
Page A655
Nov 01/05
R
IAC
Fuselage Internal Structure - Below Batteries, between FR10 and FR16
R Figure 639/TASK 53-11-00-991-048- 12 (SHEET 1)
EFF :
ALL 53-11-00
Page A656
Nov 01/05
IAC
Fuselage Internal Structure - Below Batteries, between FR10 and FR16
R Figure 639/TASK 53-11-00-991-048- 22 (SHEET 2)
EFF :
ALL 53-11-00
Page A657
Nov 01/05
IAC
TASK 53-11-00-210-804
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A658
Nov 01/05
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-095
A. Get Access
Subtask 53-11-00-110-110
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a MISCELLANEOUS (Material No. 19-003), if necessary.
EFF :
ALL 53-11-00
Page A659
Nov 01/05
IAC
4. Procedure
_________
Subtask 53-11-00-210-084
A. Inspection
R (Ref. Fig. 640/TASK 53-11-00-991-049)
(2) Make sure that there are no signs of corrosion, cracks or damage.
(3) Make sure that all the installations are attached correctly.
Subtask 53-11-00-916-067
(1) Cover the equipment and fittings adjacent to the area with masking
tape or masking paper, if necessary.
5. Close-up
________
Subtask 53-11-00-410-095
A. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-11-00
Page A660
Nov 01/05
IAC
Temporary Protection Location Zone 125 (126)
R Figure 640/TASK 53-11-00-991-049
EFF :
ALL 53-11-00
Page A661
Nov 01/05
IAC
(4) Remove the access platform(s).
EFF :
ALL 53-11-00
Page A662
Nov 01/05
R
IAC
TASK 53-11-00-210-038
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A663
Nov 01/05
IAC
3. __________
Job Set-up
Subtask 53-11-00-020-053
A. Get Access
(1) Put an access platform in position at the zone 210 in front of the
windshield.
Subtask 53-11-00-110-086
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-053
A. Inspection
R (Ref. Fig. 641/TASK 53-11-00-991-050)
EFF :
ALL 53-11-00
Page A664
Nov 01/05
IAC
Cockpit Windshield - Lower Front Fitting at FR4
R Figure 641/TASK 53-11-00-991-050
EFF :
ALL 53-11-00
Page A665
Nov 01/05
IAC
(b) Other damage (cracks, scratches, stress, marks, dents,
bumps,...):
- If you find other damage, refer to the Structural Repair Manual
(Ref. SRM 511100 P.Block 001) for damage classification and
corrective action.
5. Close-up
________
Subtask 53-11-00-420-051
A. Close Access
(2) Make sure that the inspection area is clean and clear of tools and
other items.
EFF :
ALL 53-11-00
Page A666
Nov 01/05
R
IAC
TASK 53-11-00-210-039
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A667
Nov 01/05
IAC
3. __________
Job Set-up
Subtask 53-11-00-020-054
A. Get Access
(1) Put an access platform in position at the zone 210 in front of the
windshield.
Subtask 53-11-00-110-087
(1) Remove the sealant from the inspection area with a non metallic
scraper.
(2) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
(3) Make sure that the surface of the inspection area is clean and
smooth.
EFF :
ALL 53-11-00
Page A668
Nov 01/05
IAC
Cockpit Windshield - Lower Front Fitting at FR4
R Figure 642/TASK 53-11-00-991-076
EFF :
ALL 53-11-00
Page A669
Nov 01/05
IAC
(5) Make sure that there is no:
4. Procedure
_________
Subtask 53-11-00-250-051
A. Inspection
R (Ref. Fig. 642/TASK 53-11-00-991-076)
5. Close-up
________
Subtask 53-11-00-420-052
A. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-11-00
Page A670
Nov 01/05
IAC
(3) Remove the access platform(s).
EFF :
ALL 53-11-00
Page A671
Nov 01/05
R
IAC
TASK 53-11-00-210-020
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A672
Nov 01/05
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-072
A. Get Access
(2) Open the aft nose gear doors 715 and 716.
Subtask 53-11-00-110-079
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-084
A. Inspection
R (Ref. Fig. 643/TASK 53-11-00-991-021)
EFF :
ALL 53-11-00
Page A673
Nov 01/05
IAC
Hinge Supports of the Aft Nose-Gear Doors
R Figure 643/TASK 53-11-00-991-021
EFF :
ALL 53-11-00
Page A674
Nov 01/05
IAC
(2) Make sure that there is no:
Subtask 53-11-00-916-051
(1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fittings adjacent to the
area.
5. Close-up
________
Subtask 53-11-00-410-072
A. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-11-00
Page A675
Nov 01/05
R
IAC
TASK 53-11-00-210-032
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A676
May 01/06
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-941-080
Subtask 53-11-00-110-080
EFF :
ALL 53-11-00
Page A677
Feb 01/07
IAC
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-088
A. Inspection
EFF :
ALL 53-11-00
Page A678
Feb 01/07
IAC
Fuselage Skin Between FR21 and FR23, Left Side, from STGR31 to STGR36
Figure 644/TASK 53-11-00-991-035
R
EFF :
001-012, 014-099, 53-11-00
Page A679
May 01/06
IAC
Fuselage Skin Between FR21 and FR23, Left Side, from STGR31 to STGR36
Figure 644A/TASK 53-11-00-991-035-A
R
EFF :
101-199, 901-999, 53-11-00
Page A680
Feb 01/07
IAC
Fuselage Skin between FR17 and FR18, Right Side, from STGR31 to STGR36
Figure 645/TASK 53-11-00-991-034
R
EFF :
001-012, 014-099, 53-11-00
Page A681
May 01/06
IAC
Fuselage Skin between FR17 and FR18, Right Side, from STGR31 to STGR36
Figure 645A/TASK 53-11-00-991-034-A
R
EFF :
101-199, 901-999, 53-11-00
Page A682
Feb 01/07
IAC
R **ON A/C ALL
5. Close-up
________
Subtask 53-11-00-942-088
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-11-00
Page A683
May 01/06
IAC
TASK 53-11-00-210-040
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A684
May 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-11-00-010-078
A. Get Access
Subtask 53-11-00-110-088
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-054
A. Inspection
(Ref. Fig. 646/TASK 53-11-00-991-051)
EFF :
ALL 53-11-00
Page A685
May 01/06
R
IAC
Forward Face of the Forward Pressure Bulkhead Attached to FR1
Figure 646/TASK 53-11-00-991-051
EFF :
ALL 53-11-00
Page A686
May 01/06
R
IAC
(2) Make sure that there is no:
5. Close-up
________
Subtask 53-11-00-410-078
A. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-11-00
Page A687
May 01/06
R
IAC
TASK 53-11-00-210-041
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A688
May 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-11-00-941-082
A. Get Access
Subtask 53-11-00-110-089
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-055
A. Inspection
(Ref. Fig. 647/TASK 53-11-00-991-052)
(1) Do a detailed inspection of the external portion that you can see of
the frame of the cockpit side windows. This inspection is applicable
between FR4 and FR12 (left and right sides).
EFF :
ALL 53-11-00
Page A689
May 01/06
R
IAC
Frame of the Cockpit Side Windows - FR4 to FR12
Figure 647/TASK 53-11-00-991-052
EFF :
ALL 53-11-00
Page A690
May 01/06
R
IAC
(b) Other damage (cracks, scratches, stress, marks, dents,
bumps,...):
- If you find other damage, refer to the Structural Repair Manual
(Ref. SRM 511100 P.Block 001) for damage classification and
corrective action.
5. Close-up
________
Subtask 53-11-00-942-090
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-11-00
Page A691
May 01/06
R
IAC
TASK 53-11-00-210-042
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A692
May 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-11-00-020-055
A. Get Access
1
_ Remove the retainer (Ref. TASK 56-11-11-000-001).
2
_ Clean the inspection area (Ref. para. 3.B.).
3
_ Do an inspection of the structure (Ref. para. 4.A.).
4
_ Install the retainer (Ref. TASK 56-11-11-400-001).
5
_ Do the same operation for the other retainers.
Subtask 53-11-00-110-090
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
EFF :
ALL 53-11-00
Page A693
May 01/06
R
IAC
4. Procedure
_________
Subtask 53-11-00-220-056
A. Inspection
(Ref. Fig. 648/TASK 53-11-00-991-053)
5. Close-up
________
Subtask 53-11-00-420-053
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-11-00
Page A694
May 01/06
R
IAC
Cockpit Windshield Frame
Figure 648/TASK 53-11-00-991-053
EFF :
ALL 53-11-00
Page A695
May 01/06
R
IAC
TASK 53-11-00-210-043
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page A696
May 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-11-00-941-083
A. Get Access
Subtask 53-11-00-110-091
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-057
A. Inspection
(Ref. Fig. 649/TASK 53-11-00-991-054)
(1) Do a detailed visual inspection of the external portion that you can
see of the cockpit windshield retainers.
EFF :
ALL 53-11-00
Page A697
May 01/06
R
IAC
Cockpit Windshield Retainers
Figure 649/TASK 53-11-00-991-054
EFF :
ALL 53-11-00
Page A698
May 01/06
R
IAC
(b) Other damage (cracks, scratches, stress, marks, dents,
bumps,...):
- If you find other damage, refer to the Structural Repair Manual
(Ref. SRM 511100 P.Block 001) for damage classification and
corrective action.
5. Close-up
________
Subtask 53-11-00-942-091
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-11-00
Page A699
May 01/06
R
IAC
TASK 53-11-00-210-044
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page B600
May 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-11-00-020-056
A. Get Access
(2) Open the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
010-001).
(3) Remove the scuff plates (Ref. TASK 53-15-15-000-001) of the forward
passenger/crew doors.
Subtask 53-11-00-110-093
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-058
A. Inspection
(Ref. Fig. 650/TASK 53-11-00-991-055)
EFF :
ALL 53-11-00
Page B601
May 01/06
R
IAC
Forward Passenger/Crew Door Cutout below Scuff Plate
Figure 650/TASK 53-11-00-991-055
EFF :
ALL 53-11-00
Page B602
May 01/06
R
IAC
(2) Make sure that there is no:
5. Close-up
________
Subtask 53-11-00-420-054
A. Close Access
(1) Install the scuff plates (Ref. TASK 53-15-15-400-001) of the forward
passenger/crew doors.
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
410-001).
EFF :
ALL 53-11-00
Page B603
May 01/06
R
IAC
TASK 53-11-00-210-035
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page B604
May 01/06
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-075
A. Get Access
(1) Put an adjustable access platform in position at the zone 121 (122).
(2) Open the lateral avionics compartment doors 812 and 824 (Ref. TASK
52-41-00-010-002) .
(3) Remove the floor panels from FR15 to FR21 (Ref. TASK 53-12-12-000-
001).
Subtask 53-11-00-865-056
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
122VU DOORS/STAIRS/PWR SPLY/STBY 1MW T15
122VU DOORS/STAIRS/PWR SPLY/NORM 2MW T14
122VU DOORS/STAIRS CTL/STBY 3MW T11
122VU DOORS/STAIRS CTL/NORM 4MW T10
EFF :
ALL 53-11-00
Page B605
May 01/06
R
IAC
Subtask 53-11-00-860-055
Subtask 53-11-00-110-083
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-051
A. Inspection
(Ref. Fig. 651/TASK 53-11-00-991-047)
EFF :
ALL 53-11-00
Page B606
May 01/06
R
IAC
Fuselage Internal Structure from FR15 to FR21, between STGR23 and STGR28
Figure 651/TASK 53-11-00-991-047
R
EFF :
ALL 53-11-00
Page B607
May 01/06
IAC
(2) Make sure that there is no:
Subtask 53-11-00-916-054
(1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fittings adjacent to the
area.
R
EFF :
ALL 53-11-00
Page B608
May 01/06
IAC
5. Close-up
________
Subtask 53-11-00-860-056
Subtask 53-11-00-865-057
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
1MW, 2MW, 3MW, 4MW.
Subtask 53-11-00-410-075
C. Close Access
(1) Install the floor panels from FR15 to FR21 (Ref. TASK 53-12-12-400-
001).
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Close the lateral avionics compartment doors 812 and 824 (Ref. TASK
52-41-00-410-002).
R
EFF :
ALL 53-11-00
Page B609
May 01/06
IAC
**ON A/C 001-012, 014-019,
TASK 53-11-00-210-045
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
001-012, 014-019, 53-11-00
Page B610
May 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-11-00-010-079
A. Get Access
Subtask 53-11-00-110-092
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-059
A. Inspection
(Ref. Fig. 652/TASK 53-11-00-991-056)
R
EFF :
001-012, 014-019, 53-11-00
Page B611
May 01/06
IAC
Forward Pressure Bulkhead Vertical Posts
Figure 652/TASK 53-11-00-991-056
R
EFF :
001-012, 014-019, 53-11-00
Page B612
May 01/06
IAC
(b) Other damage (cracks, scratches, stress, marks, dents,
bumps,...):
- If you find other damage, refer to the Structural Repair Manual
(Ref. SRM 511100 P.Block 001) for damage classification and
corrective action.
5. Close-up
________
Subtask 53-11-00-410-079
A. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
001-012, 014-019, 53-11-00
Page B613
May 01/06
IAC
**ON A/C ALL
TASK 53-11-00-210-046
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page B614
May 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-11-00-010-080
A. Get Access
Subtask 53-11-00-110-094
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-060
A. Inspection
(Ref. Fig. 653/TASK 53-11-00-991-057)
EFF :
ALL 53-11-00
Page B615
May 01/06
R
IAC
Aft Face of the Forward Pressure Bulkhead
Figure 653/TASK 53-11-00-991-057
EFF :
ALL 53-11-00
Page B616
May 01/06
R
IAC
(2) Make sure that there is no:
5. Close-up
________
Subtask 53-11-00-410-080
A. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-11-00
Page B617
May 01/06
R
IAC
TASK 53-11-00-210-047
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page B618
May 01/06
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-081
A. Get Access
(Ref. Fig. 654/TASK 53-11-00-991-058)
(3) Open the forward passenger/crew Door 831 (841) (Ref. TASK 52-10-00-
010-001).
(4) Remove the linings around the cockpit windows: 211GW, 211DW, 211PW,
211NW, 211LW, 211MW, 211KC, 211AC, 211LC, 211MC, 212LC, 212AC, 212KC,
212NW, 212PW, 212DW, 212KW, 212GW, (Ref. TASK 25-13-41-000-001),
(Ref. TASK 25-13-41-000-002).
Subtask 53-11-00-110-095
EFF :
ALL 53-11-00
Page B619
May 01/06
R
IAC
Cockpit Lining Panels
Figure 654/TASK 53-11-00-991-058
EFF :
ALL 53-11-00
Page B620
May 01/06
R
IAC
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-061
A. Inspection
(Ref. Fig. 655/TASK 53-11-00-991-059)
5. Close-up
________
Subtask 53-11-00-410-081
A. Close Access
(3) Install the lining panels around the cockpit windows 211GW, 211DW,
211PW, 211NW, 211LW, 211MW, 211KC, 211AC, 211LC, 211MC, 212LC, 212AC,
212KC, 212NW, 212PW, 212DW, 212KW, 212GW, (Ref. TASK 25-13-41-400-
001), (Ref. TASK 25-13-41-400-002).
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Close the forward passenger/crew Door 831 (841) (Ref. TASK 52-10-00-
410-001).
EFF :
ALL 53-11-00
Page B621
May 01/06
R
IAC
Cockpit Window Frames
Figure 655/TASK 53-11-00-991-059
EFF :
ALL 53-11-00
Page B622
May 01/06
R
IAC
(6) Close the avionics-compartment door 811 (Ref. TASK 52-41-00-410-002).
EFF :
ALL 53-11-00
Page B623
May 01/06
R
IAC
TASK 53-11-00-210-048
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page B624
May 01/06
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-082
A. Get Access
(2) Open the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
010-001).
(3) Remove the floor panels of the cockpit (Ref. TASK 53-12-11-000-001).
Subtask 53-11-00-110-096
EFF :
ALL 53-11-00
Page B625
May 01/06
R
IAC
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-062
A. Inspection
(Ref. Fig. 656/TASK 53-11-00-991-060)
Subtask 53-11-00-916-071
(1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fittings adjacent to the
area.
EFF :
ALL 53-11-00
Page B626
May 01/06
R
IAC
Cockpit Floor Structure
Figure 656/TASK 53-11-00-991-060
EFF :
ALL 53-11-00
Page B627
May 01/06
R
IAC
5. Close-up
________
Subtask 53-11-00-410-082
A. Close Access
(2) Install the floor panels of the cockpit (Ref. TASK 53-12-11-400-001).
(3) Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
410-001).
EFF :
ALL 53-11-00
Page B628
May 01/06
R
IAC
TASK 53-11-00-210-049
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page B629
May 01/06
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-083
A. Get Access
(2) Open the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
010-001).
(5) Remove the floor panels from FR12 to FR21 (Ref. TASK 53-12-12-000-
001).
EFF :
ALL 53-11-00
Page B630
May 01/06
R
IAC
Subtask 53-11-00-110-097
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-063
A. Inspection
(Ref. Fig. 657/TASK 53-11-00-991-061)
EFF :
ALL 53-11-00
Page B631
May 01/06
R
IAC
Floor Structure FR12 to FR21
Figure 657/TASK 53-11-00-991-061
EFF :
ALL 53-11-00
Page B632
May 01/06
R
IAC
Subtask 53-11-00-916-060
(1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fitting adjacent to the
area.
5. Close-up
________
Subtask 53-11-00-410-083
A. Close Access
(1) Install the floor panels from FR12 to FR21 (Ref. TASK 53-12-12-400-
001).
(4) Close the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
410-001).
EFF :
ALL 53-11-00
Page B633
May 01/06
R
IAC
TASK 53-11-00-220-002
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page B634
May 01/06
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-084
A. Get Access
Subtask 53-11-00-110-098
EFF :
ALL 53-11-00
Page B635
May 01/06
R
IAC
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-064
A. Inspection
(Ref. Fig. 658/TASK 53-11-00-991-062)
Subtask 53-11-00-916-058
(1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fitting adjacent to the
area.
EFF :
ALL 53-11-00
Page B636
May 01/06
R
IAC
Aft Face of the Forward Pressure Bulkhead
Figure 658/TASK 53-11-00-991-062
EFF :
ALL 53-11-00
Page B637
May 01/06
R
IAC
(2) Apply a layer of STORAGE PRESERVATION (Material No. 15-005) or
STORAGE PRESERVATION (Material No. 15-006) to the inspection area.
5. Close-up
________
Subtask 53-11-00-410-084
A. Close Access
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-11-00
Page B638
May 01/06
R
IAC
TASK 53-11-00-220-003
Detailed Inspection of Cabin Floor Structure, below and 0.5 M around Galleys
and Toilets, between FR 21 and FR 24
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page B639
Aug 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-085
A. Get Access
(2) Open the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
010-001).
(5) Remove the cabin floor panels from FR21 to FR24 (Ref. TASK 53-12-12-
000-001).
EFF :
ALL 53-11-00
Page B640
Aug 01/07
IAC
Subtask 53-11-00-110-099
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-220-065
A. Inspection
(Ref. Fig. 659/TASK 53-11-00-991-063)
(1) Do a detailed inspection of the cabin floor structure below and 0.5 M
(19.685 in.) around the galleys and the lavatories. The inspection is
applicable between FR21 and FR24.
EFF :
ALL 53-11-00
Page B641
May 01/06
R
IAC
Floor Structure, FR21 to FR24
Figure 659/TASK 53-11-00-991-063
EFF :
ALL 53-11-00
Page B642
May 01/06
R
IAC
Subtask 53-11-00-916-059
(1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fitting adjacent to the
area.
5. Close-up
________
Subtask 53-11-00-410-085
A. Close Access
(1) Install the cabin floor panels from FR21 to FR24 (Ref. TASK 53-12-12-
400-001).
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
410-001).
EFF :
ALL 53-11-00
Page B643
May 01/06
R
IAC
TASK 53-11-00-210-034
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page B644
Feb 01/07
IAC
3. __________
Job Set-up
Subtask 53-11-00-010-070
A. Get Access
R (1) Put the access platform in position at the left and right, aft and
R forward passenger/crew door.
(2) Open the door 831, 832, 841 842, (Ref. TASK 52-10-00-010-001).
4. Procedure
_________
Subtask 53-11-00-110-050
A. Cleaning
R (1) Clean the girt-bar fitting stop-levers and its adjacent area with a
R vacuum cleaner to remove the dirt and dust in these areas.
Subtask 53-11-00-720-050
B. Test
(Ref. Fig. 660/TASK 53-11-00-991-037)
R (1) Press the lever (1) down and release it to do an operational test.
R (a) Clean the lever (1) with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
R (b) Press the lever (1) down again and release it to do the
R operational test again.
EFF :
ALL 53-11-00
Page B645
Feb 01/07
IAC
Girt Bar Fitting
Figure 660/TASK 53-11-00-991-037
EFF :
ALL 53-11-00
Page B646
May 01/06
R
IAC
(c) Install the girt bar fitting (Ref. TASK 52-11-31-400-003) or
(Ref. TASK 52-13-31-400-003)
5. Close-up
________
Subtask 53-11-00-410-070
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Close the door 831, 832, 841 842, (Ref. TASK 52-10-00-410-001).
EFF :
ALL 53-11-00
Page B647
Feb 01/07
R
IAC
TASK 53-11-00-210-805
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page B648
Feb 01/07
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-096
A. Get Access
(2) Open the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
010-001).
(3) Remove the floor panels between FR21 and FR24 (Ref. TASK 53-12-12-
000-001).
Subtask 53-11-00-110-111
EFF :
ALL 53-11-00
Page B649
Feb 01/07
R
IAC
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-210-085
A. Inspection
(Ref. Fig. 661/TASK 53-11-00-991-065)
(3) Make sure that all the installations are attached correctly.
Subtask 53-11-00-916-068
(1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fittings adjacent to the
area.
EFF :
ALL 53-11-00
Page B650
Feb 01/07
R
IAC
Cabin Floor Structure between FR21 and FR24
Figure 661/TASK 53-11-00-991-065
EFF :
ALL 53-11-00
Page B651
Feb 01/07
R
IAC
(2) Apply a layer of STORAGE PRESERVATION (Material No. 15-005) or
STORAGE PRESERVATION (Material No. 15-006) to the inspection area.
5. Close-up
________
Subtask 53-11-00-410-096
A. Close Access
(2) Install the floor panels between FR21 and FR24 (Ref. TASK 53-12-12-
400-001).
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Close the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
410-001).
EFF :
ALL 53-11-00
Page B652
Feb 01/07
R
IAC
TASK 53-11-00-210-806
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page B653
Feb 01/07
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-097
A. Get Access
(2) Open the avionics-compartment doors 811 812 822 (Ref. TASK 52-41-00-
010-002).
Subtask 53-11-00-110-112
EFF :
ALL 53-11-00
Page B654
Feb 01/07
R
IAC
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-11-00-210-086
A. Inspection
(Ref. Fig. 662/TASK 53-11-00-991-066)
(3) Make sure that all the installations are attached correctly.
Subtask 53-11-00-916-069
(1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fittings adjacent to the
area.
EFF :
ALL 53-11-00
Page B655
Feb 01/07
R
IAC
Fuselage Internal Structure between FR1 and FR12
Figure 662/TASK 53-11-00-991-066
EFF :
ALL 53-11-00
Page B656
Feb 01/07
R
IAC
(3) Remove the masking tape or the masking paper.
5. Close-up
________
Subtask 53-11-00-410-097
A. Close Access
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Close the avionics-compartment door 811 812 822 (Ref. TASK 52-41-00-
410-002) .
EFF :
ALL 53-11-00
Page B657
Feb 01/07
R
IAC
TASK 53-11-00-210-807
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page B658
Feb 01/07
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-098
A. Get Access
(2) Open the lateral avionics-compartment door 824 (Ref. TASK 52-41-00-
010-002).
(3) Remove the floor panels 127BF, 127CF, 127DF, 128CF (Ref. TASK 53-12-
13-000-001).
Subtask 53-11-00-110-113
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
EFF :
ALL 53-11-00
Page B659
Feb 01/07
R
IAC
4. Procedure
_________
Subtask 53-11-00-210-087
A. Inspection
(Ref. Fig. 663/TASK 53-11-00-991-067)
(3) Make sure that all the installations are attached correctly.
Subtask 53-11-00-916-070
(1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fittings adjacent to the
area.
EFF :
ALL 53-11-00
Page B660
Feb 01/07
R
IAC
Fuselage internal Stucture between FR21 and FR24
Figure 663/TASK 53-11-00-991-067
EFF :
ALL 53-11-00
Page B661
Feb 01/07
R
IAC
5. Close-up
________
Subtask 53-11-00-410-098
A. Close Access
(1) Install the floor panels 127BF, 127CF, 127DF, 128CF (Ref. TASK 53-12-
13-400-001).
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Close the lateral avionics-compartment door 824 (Ref. TASK 52-41-00-
410-002).
R
EFF :
ALL 53-11-00
Page B662
Feb 01/07
IAC
**ON A/C 001-012, 014-019,
TASK 53-11-00-220-005
Detailed Visual Inspection and Torque Check of the NLG Doors Uplock Fitting
Bolts
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
001-012, 014-019, 53-11-00
Page B663
Feb 01/07
R
IAC
3. __________
Job Set-up
Subtask 53-11-00-010-092
A. Get Access
(3) Open the nose gear doors 713, 714 (Ref. TASK 32-22-00-010-001).
Subtask 53-11-00-110-106
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a MISCELLANEOUS (Material No. 19-003), if necessary.
4. Procedure
_________
Subtask 53-11-00-220-089
A. Inspection
(Ref. Fig. 664/TASK 53-11-00-991-068)
(1) Do a detailed visual inspection of the inside and outside of the gear
well, four fasteners of the door uplock fitting.
EFF :
001-012, 014-019, 53-11-00
Page B664
Feb 01/07
R
IAC
INTENTIONALLY BLANK
R
53-11-00
Page B665
Feb 01/07
IAC
NLG Doors Uplock Fittings Bolts
Figure 664/TASK 53-11-00-991-068- 12 (SHEET 1)
EFF :
001-012, 014-019, 53-11-00
Page B666
Feb 01/07
R
IAC
NLG Doors Uplock Fittings Bolts
Figure 664/TASK 53-11-00-991-068- 22 (SHEET 2)
R
EFF :
001-012, 014-019, 53-11-00
Page B667
Feb 01/07
IAC
(3) If one or several fasteners is(are) broken replace, by new
fastener(s). TORQUE to the same torque value and apply a STORAGE
PRESERVATION (Material No. 15-007) on the head of the fasteners
NOTE : Do not remove all the fasteners at the same time but replace
____
them one after the other.
5. Close-up
________
Subtask 53-11-00-410-092
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Close the nose gear doors 713, 714 (Ref. TASK 32-22-00-410-001).
R
EFF :
001-012, 014-019, 53-11-00
Page B668
Feb 01/07
IAC
R **ON A/C ALL
R TASK 53-11-00-210-814
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R A. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R B. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page B669
Aug 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R 3. __________
Job Set-up
R Subtask 53-11-00-010-101
R A. Get Access
R (3) Remove the door frame linings (Ref. TASK 25-23-45-000-005) (Ref. TASK
R 25-23-45-000-002).
R (5) Remove the ceiling panels (Ref. TASK 25-23-41-000-001) (Ref. TASK 25-
R 23-42-000-001).
EFF :
ALL 53-11-00
Page B670
Aug 01/07
IAC
R Subtask 53-11-00-110-120
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
R 4. Procedure
_________
R Subtask 53-11-00-210-094
R A. Inspection
R (Ref. Fig. 665/TASK 53-11-00-991-085)
EFF :
ALL 53-11-00
Page B671
Aug 01/07
IAC
R Fuselage Internal Structure from FR1 to FR24, above Cabin Floor Level
R Figure 665/TASK 53-11-00-991-085
EFF :
ALL 53-11-00
Page B672
Aug 01/07
IAC
R 5. Close-up
________
R Subtask 53-11-00-410-101
R A. Close Access
R (2) Install the ceiling panels (Ref. TASK 25-23-41-400-001) (Ref. TASK
R 25-23-42-400-001).
EFF :
ALL 53-11-00
Page B673
Aug 01/07
IAC
R
TASK 53-11-00-220-006
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-00
Page B674
Aug 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-00-010-104
A. Get Access
R (2) Open the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
010-001).
Subtask 53-11-00-020-070
R (1) Remove the girt bar fittings at the forward passenger/crew doors
R (Ref. TASK 52-11-31-000-003).
EFF :
ALL 53-11-00
Page B675
Feb 01/08
IAC
Subtask 53-11-00-110-123
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
(2) Make sure that the surface of the inspection area is clean and
smooth.
EFF :
ALL 53-11-00
Page B676
Feb 01/08
IAC
FWD Door-Cutout Lower-Corners
Figure 666/TASK 53-11-00-991-094
EFF :
ALL 53-11-00
Page B677
Feb 01/08
R
IAC
4. Procedure
_________
Subtask 53-11-00-220-091
A. Inspection
(Ref. Fig. 666/TASK 53-11-00-991-094)
Subtask 53-11-00-916-073
R (1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
R (Material No. 08-074) on the equipment and fittings adjacent to the
area.
EFF :
ALL 53-11-00
Page B678
Feb 01/08
IAC
5. Close-up
________
Subtask 53-11-00-420-067
R (2) Install the girt bar fittings at the forward passenger/crew doors
R (Ref. TASK 52-11-31-400-003).
Subtask 53-11-00-410-104
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R (2) Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
410-001).
EFF :
ALL 53-11-00
Page B679
Feb 01/08
IAC
PROTECTIVE SHIELDS - FR1 - REMOVAL/INSTALLATION
_______________________________________________
TASK 53-11-41-000-001
CAUTION : DO NOT USE THE LOCALIZER ANTENNA AT THE BOTTOM OF THE RADOME AS A
_______
SUPPORT.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-41
Page 401
Feb 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-41-861-050
Subtask 53-11-41-865-050
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
EFF :
ALL 53-11-41
Page 402
Feb 01/07
IAC
Subtask 53-11-41-010-050
C. Get Access
(1) Put an access platform in position below the radome in the zone 110.
WARNING : DO NOT OPEN THE RADOME IF THE WIND SPEED IS MORE THAN 35
_______
KNOTS.
4. Procedure
_________
Subtask 53-11-41-020-050
(1) Remove the bolts (1), the washers (2) and the clamps (3) and (5).
(3) Remove the nuts (7), the washers (8) and the plates (9).
Subtask 53-11-41-020-050-A
EFF :
ALL 53-11-41
Page 403
Feb 01/07
IAC
Upper Protective Shield
Figure 401/TASK 53-11-41-991-001
EFF :
001-012, 53-11-41
Page 404
Nov 01/99
IAC
Upper Protective Shield
Figure 401A/TASK 53-11-41-991-001-A
R
EFF :
014-099, 101-199, 901-999, 53-11-41
Page 405
Feb 01/07
IAC
Lower Protective Shields
Figure 402/TASK 53-11-41-991-002
EFF :
001-012, 53-11-41
Page 406
Nov 01/99
IAC
Lower Protective Shields
Figure 402A/TASK 53-11-41-991-002-A
R
EFF :
014-099, 101-199, 901-999, 53-11-41
Page 407
Feb 01/07
IAC
**ON A/C ALL
TASK 53-11-41-400-001
CAUTION : DO NOT USE THE LOCALIZER ANTENNA AT THE BOTTOM OF THE RADOME AS A
_______
SUPPORT.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
EFF :
ALL 53-11-41
Page 408
Nov 01/99
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-11-41-860-050
(2) Make sure that access platform is in position below the radome in the
zone 110.
EFF :
ALL 53-11-41
Page 409
Feb 01/07
IAC
(3) Make sure that the radome 110AL is open (Ref. TASK 53-15-11-010-001).
WARNING : DO NOT OPEN THE RADOME IF THE WIND SPEED IS MORE THAN 35
_______
KNOTS.
Subtask 53-11-41-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
4. Procedure
_________
Subtask 53-11-41-420-050
(2) Install the nuts (7), the washers (8) and the plates (9).
(3) Install the bolts (1), the washers (2) and the clamps (3) and (5).
(5) Safety the nuts (7) with the new cotter pins (6).
EFF :
ALL 53-11-41
Page 410
Feb 01/07
R
IAC
R **ON A/C 014-099, 101-199, 901-999,
Subtask 53-11-41-420-050-A
5. Close-up
________
Subtask 53-11-41-865-052
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
5SQ1, 5SQ2.
Subtask 53-11-41-410-050
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 53-11-41-862-050
EFF :
ALL 53-11-41
Page 411
Feb 01/07
IAC
FLOOR PANELS - REPAIRS
______________________
TASK 53-12-00-300-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-12-00
Page 801
Nov 01/04
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-12-00-941-050
A. Get Access
Subtask 53-12-00-020-050
(1) Remove the damaged panel (Ref. TASK 53-12-11-000-001) or (Ref. TASK
53-12-12-000-001) or (Ref. TASK 53-12-13-000-001).
EFF :
ALL 53-12-00
Page 802
May 01/00
IAC
4. Procedure
_________
Subtask 53-12-00-350-050
A. Repair Procedure
(Ref. Fig. 801/TASK 53-12-00-991-001)
(1) Cut out the damaged area of the corrosion-protection adhesive tape of
the floor panel edge.
(2) Clean and degrease the damaged area with CLEANING AGENTS (Material
No. 11-003) or CLEANING AGENTS (Material No. 11-004).
(3) Prepare BONDING AND ADHESIVE COMPOUNDS (Material No. 08-032) (1) for
the cutout limits.
(4) Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-032) (1) to the
damaged area.
5. Close-up
________
Subtask 53-12-00-420-050
(1) Install the repaired panel (Ref. TASK 53-12-11-400-001) or (Ref. TASK
53-12-12-400-001) or (Ref. TASK 53-12-13-400-001).
Subtask 53-12-00-942-050
B. Close Access
(1) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-12-00
Page 803
Nov 01/04
IAC
Repair of the Damaged Area of the Adhesive Tape
Figure 801/TASK 53-12-00-991-001
EFF :
ALL 53-12-00
Page 804
May 01/00
IAC
R TASK 53-12-00-300-002
R 1. __________________
Reason for the Job
R Self Explanatory
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
ALL 53-12-00
Page 805
Nov 01/07
IAC
R 3. __________
Job Set-up
R Subtask 53-12-00-941-051
R A. Get Access
R 4. Procedure
_________
R Subtask 53-12-00-350-051
R A. Repair Procedure
R (1) Apply masking tape to the adjacent area which you will not rub with
R the abrasive cloth (grade 320).
R (2) Lightly rub the contact surface of the floor panel 221FF(222FF) with
R abrasive cloth (grade 320) or finer to remove the external anti-slip
R top layer. Do not cause damage to the basic primer.
R (5) Do an inspection for damaged paint in the areas that had masking tape
R on them.
R (7) Apply the BONDING AND ADHESIVE COMPOUNDS (Material No. 08-117).
R 5. Close-up
________
R Subtask 53-12-00-942-051
R A. Close Access
R (1) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
EFF :
ALL 53-12-00
Page 806
Nov 01/07
IAC
R (3) Remove the access platform(s).
EFF :
ALL 53-12-00
Page 807
Nov 01/07
IAC
PANELS - COCKPIT FLOOR - REMOVAL/INSTALLATION
_____________________________________________
TASK 53-12-11-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-12-11-941-050
A. Get Access
EFF :
ALL 53-12-11
Page 401
Nov 01/05
IAC
**ON A/C 001-012, 014-099,
Subtask 53-12-11-020-052
Subtask 53-12-11-020-052-A
4. Procedure
_________
Subtask 53-12-11-020-050
EFF :
ALL 53-12-11
Page 402
Feb 01/07
IAC
R Cockpit Floor Panels
Figure 401/TASK 53-12-11-991-001
EFF :
ALL 53-12-11
Page 403
Nov 01/97
IAC
Floor Panels from FR1 thru FR6
Figure 402/TASK 53-12-11-991-002
EFF :
ALL 53-12-11
Page 404
Feb 01/96
IAC
(4) Remove the screws (1).
Subtask 53-12-11-020-051
EFF :
ALL 53-12-11
Page 405
May 01/06
R
IAC
Floor Panels from FR6 thru FR12
Figure 403/TASK 53-12-11-991-003-A
EFF :
ALL 53-12-11
Page 406
May 01/06
R
IAC
TASK 53-12-11-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-12-11
Page 407
Feb 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-12-11-869-050
(2) Make sure that the passenger/crew door is open (Ref. TASK 52-10-00-
010-001).
Subtask 53-12-11-160-050
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
EFF :
ALL 53-12-11
Page 408
May 01/06
R
IAC
(1) Remove the adhesive of the old strips with CLEANING AGENTS (Material
No. 11-021).
Subtask 53-12-11-210-050
(1) Make sure that the parts retained from the removed component are
clean and in the correct condition.
Subtask 53-12-11-210-052
(1) Make sure that the adhesive tapes are clean and in the correct
condition.
If necessary, repair the related adhesive tape (Ref. TASK 53-12-00-
300-001).
Subtask 53-12-11-210-054
(1) Examine the shims between FR1 and FR12. If the shims are damaged, do
the steps that follow:
(b) Clean the area between the shims and the structure with CLEANING
AGENTS (Material No. 11-003) and a MISCELLANEOUS (Material No.
19-003).
(c) Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-004) on the
surface between the shims and the structure.
EFF :
ALL 53-12-11
Page 409
May 01/06
R
IAC
Shims from FR1 thru FR12
Figure 404/TASK 53-12-11-991-004
EFF :
ALL 53-12-11
Page 410
May 01/06
R
IAC
4. Procedure
_________
Subtask 53-12-11-420-050
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Apply SPECIAL MATERIALS (Material No. 05-002) to the screws (1).
(4) Install the screws (1) and TORQUE to between 0.15 and 0.20 m.daN
(13.27 and 17.69 lbf.in).
(6) Apply SPECIAL MATERIALS (Material No. 05-002) to the screws (3).
(7) Install the screws (3) and TORQUE to between 0.15 and 0.20 m.daN
(13.27 and 17.69 lbf.in).
Subtask 53-12-11-420-051-A
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 53-12-11-420-053
(1) Apply SPECIAL MATERIALS (Material No. 05-002) to the screws (11).
(2) Install the screws (11) and TORQUE to between 0.15 and 0.20 m.daN
(13.27 and 17.69 lbf.in).
EFF :
ALL 53-12-11
Page 411
May 01/06
R
IAC
5. Close-up
________
Subtask 53-12-11-420-052
Subtask 53-12-11-420-052-A
Subtask 53-12-11-942-050
B. Close Access
(1) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-12-11
Page 412
Feb 01/07
IAC
PANELS - CABIN FLOOR - REMOVAL/INSTALLATION
___________________________________________
TASK 53-12-12-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-12-12
Page 401
Feb 01/08
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-12-12
Page 402
Feb 01/08
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-12-12-941-050
A. Get Access
(2) Open the FWD passenger/crew door 831 (841) (Ref. TASK 52-10-00-010-
001).
Subtask 53-12-12-020-052
(1) Remove the toilets (Ref. TASK 25-41-41-000-001), (Ref. TASK 25-41-42-
000-001), (Ref. TASK 25-41-44-000-001) and (Ref. TASK 25-42-41-000-
001), if installed.
(2) Remove the galleys (Ref. TASK 25-31-41-000-001), (Ref. TASK 25-31-41-
000-002) and (Ref. TASK 25-32-41-000-001), if installed.
4. Procedure
_________
Subtask 53-12-12-020-053
(1) Remove the screws (3) and (5) and the washers (2) and (4).
EFF :
ALL 53-12-12
Page 403
Feb 01/08
R
IAC
Angles at FR16 and FR20
Figure 401/TASK 53-12-12-991-004
EFF :
ALL 53-12-12
Page 404
Nov 01/02
R
IAC
**ON A/C 001-012, 014-027,
Subtask 53-12-12-020-050
(1) Pull the cords (4) up to remove the sealant from the floor panel
joints.
NOTE : Identify the position of the screws when you remove the panels
____
to prevent the incorrect position of the screws during the
installation.
R
EFF :
001-012, 014-027, 53-12-12
Page 405
Feb 01/08
IAC
Floor Panels at FR12 thru FR24
Figure 402/TASK 53-12-12-991-001
R
EFF :
001-012, 014-019, 53-12-12
Page 406
Feb 01/08
IAC
Floor Panels at FR12 thru FR24
Figure 402A/TASK 53-12-12-991-001-B
R
EFF :
020-099, 53-12-12
Page 407
Feb 01/08
IAC
R Floor Panels at FR12 thru FR24
R Figure 402B/TASK 53-12-12-991-001-D
R
EFF :
101-199, 901-999, 53-12-12
Page 408
Feb 01/08
IAC
Floor Panels at FR12 thru FR24
R Figure 402C/TASK 53-12-12-991-001-C
R
EFF :
001-012, 014-099, 53-12-12
Page 409
Feb 01/08
IAC
**ON A/C 028-099, 101-199, 901-999,
Subtask 53-12-12-020-050-A
(1) Pull the cords (4) up to remove the sealant from the floor panel
joints.
NOTE : Identify the position of the screws when you remove the panels
____
R to prevent the incorrect position of the screws during
R installation.
EFF :
028-099, 101-199, 901-999, 53-12-12
Page 410
May 01/08
IAC
R Floor Panels at FR12 thru FR24
R Figure 403/TASK 53-12-12-991-003
R
EFF :
001-012, 014-099, 53-12-12
Page 411
Feb 01/08
IAC
R Floor Panels at FR12 thru FR24
R Figure 403A/TASK 53-12-12-991-003-C
R
EFF :
101-199, 901-999, 53-12-12
Page 412
Feb 01/08
IAC
**ON A/C 028-099,
(4) Remove the screws (21) and the washers (22) from the panel (23).
R (6) Make sure that the clipnuts (24) are installed on the structure (25).
EFF :
028-099, 101-199, 901-999, 53-12-12
Page 413
May 01/08
IAC
R Floor Panels at FR12 thru FR24
R Figure 403B/TASK 53-12-12-991-003-B
EFF :
001-012, 014-099, 53-12-12
Page 414
Feb 01/08
IAC
**ON A/C ALL
TASK 53-12-12-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-12-12
Page 415
Feb 01/08
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-12-12
Page 416
Feb 01/08
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-12-12
Page 417
Feb 01/08
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-12-12-869-050
(2) Make sure that the FWD passenger/crew door 831 (841) is in the open
position (Ref. TASK 52-10-00-010-001).
Subtask 53-12-12-160-050
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1) Remove the remaining sealant from the floor panels and the component
interface with a non metallic scraper. If the sealant is not easy to
remove, use CLEANING AGENTS (Material No. 11-003) and a lint-free
cloth.
(2) Use CLEANING AGENTS (Material No. 11-021) to remove the remaining
adhesive from the used strips of adhesive tape.
EFF :
ALL 53-12-12
Page 418
Feb 01/08
R
IAC
Subtask 53-12-12-210-050
(1) Make sure that the parts retained from the removed component are
clean and in the correct condition.
Subtask 53-12-12-210-052
(1) Make sure that the adhesive tapes are clean and in the correct
condition.
If necessary, repair the damaged adhesive tapes (Ref. TASK 53-12-00-
300-001).
Subtask 53-12-12-210-054
(1) Examine the shims between FR12 and FR24. If the shims are damaged, do
the steps that follow:
(b) Clean the area between the shims and the structure with CLEANING
AGENTS (Material No. 11-003) and a MISCELLANEOUS (Material No.
19-003).
EFF :
ALL 53-12-12
Page 419
Feb 01/08
R
IAC
Shims from FR12 thru FR24
Figure 404/TASK 53-12-12-991-006
R
EFF :
001-012, 014-099, 53-12-12
Page 420
Feb 01/08
IAC
Shims from FR12 thru FR24
Figure 404A/TASK 53-12-12-991-006-A
EFF :
ALL 53-12-12
Page 421
Feb 01/08
R
IAC
(c) Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-004) on the
surface between the shims and the structure.
4. Procedure
_________
Subtask 53-12-12-420-050-A
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Make sure that the adhesive tapes (5) are in position.
Subtask 53-12-12-420-053
CAUTION : BEFORE YOU INSTALL THE SCREWS ON THE PANEL, MAKE SURE THAT THE
_______
POSITION OF THE SCREWS IS CORRECT. AN INCORRECT POSITION OF THE
SCREWS CAN CAUSE DAMAGE TO THE EQUIPMENT BELOW THE PANEL.
EFF :
ALL 53-12-12
Page 422
May 01/08
R
IAC
**ON A/C 020-027,
(1) Apply SPECIAL MATERIALS (Material No. 05-002) to the screws (1).
(2) Install the screws (1) and TORQUE to between 0.30 and 0.40 m.daN
(26.54 and 35.39 lbf.in).
(3) Install the cords (4) MISCELLANEOUS (Material No. 19-027) in the
joints between the floor panels (2). Make a loop at the end of the
cord for the subsequent removal procedure.
Subtask 53-12-12-420-050-B
EFF :
ALL 53-12-12
Page 423
Feb 01/08
IAC
R **ON A/C 028-099, 101-199, 901-999,
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 53-12-12-420-053-B
CAUTION : BEFORE YOU INSTALL THE SCREWS ON THE PANEL, MAKE SURE THAT THE
_______
POSITION OF THE SCREWS IS CORRECT. AN INCORRECT POSITION OF THE
SCREWS CAN CAUSE DAMAGE TO THE EQUIPMENT BELOW THE PANEL.
EFF :
028-099, 101-199, 901-999, 53-12-12
Page 424
Feb 01/08
IAC
**ON A/C 028-099,
(1) Apply SPECIAL MATERIALS (Material No. 05-002) to the screws (21).
(3) Install the screws (21) and TORQUE to between 0.30 and 0.40 m.daN
(26.54 and 35.39 lbf.in).
(4) Install the cords (4) MISCELLANEOUS (Material No. 19-027) in the
joints between the floor panels (2). Make a loop at the end of the
cord for the subsequent removal procedure.
R (5) Make sure that the clipnuts (24) are installed on the structure (25).
Subtask 53-12-12-914-050
EFF :
ALL 53-12-12
Page 425
May 01/08
IAC
R **ON A/C 001-012, 014-099,
(1) Apply SEALANTS (Material No. 09-016) in the joints between the floor
panels (2).
Subtask 53-12-12-420-054
(1) Apply SEALANTS (Material No. 09-018) on the surface of the angles (1)
and (6) that touches the metal surface of the cabin floor.
(3) Install the washers (2) and (4) and the screws (3) and (5) and
tighten them.
(4) Remove the unwanted sealant with MISCELLANEOUS (Material No. 19-003).
5. Close-up
________
Subtask 53-12-12-420-052
(4) Install the galleys (Ref. TASK 25-31-41-400-001), (Ref. TASK 25-31-
41-400-002) and (Ref. TASK 25-32-41-400-001), if removed.
(5) Install the toilets (Ref. TASK 25-41-41-400-001), (Ref. TASK 25-41-
42-400-001), (Ref. TASK 25-41-44-400-001) and (Ref. TASK 25-32-41-
400-001), if removed.
EFF :
ALL 53-12-12
Page 426
Feb 01/08
IAC
Subtask 53-12-12-210-056
(1) Make sure that the anti-slip surface of the passenger/crew floor
R panel 221FF (222FF) is in correct condition.
If necessary, repair the damaged anti-slip surface (Ref. TASK 53-12-
00-300-002).
Subtask 53-12-12-210-055
R (1) Examine the anti-slip strips on the passenger door sills. If the
R anti-slip strips are damaged, do the steps that follow:
(b) Clean the area between the anti-slip strips and the panels with
CLEANING AGENTS (Material No. 11-016) and a MISCELLANEOUS
(Material No. 19-003).
Subtask 53-12-12-942-050
D. Close Access
(1) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
(2) Close the FWD passenger/crew door 831 (841) (Ref. TASK 52-10-00-410-
001).
EFF :
ALL 53-12-12
Page 427
May 01/08
IAC
PANELS - AVIONICS COMPARTMENT FLOOR - REMOVAL/INSTALLATION
__________________________________________________________
TASK 53-12-13-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-12-13
Page 401
Feb 01/07
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-12-13-010-050
A. Get Access
(1) Put the access platforms in position in the zones 121/122 and 128.
4. Procedure
_________
Subtask 53-12-13-020-050
(1) Find one of the ends of the synthetic fiber cord (5) at one of the
floor panel joints.
(2) Pull the cord (5) up to remove the sealant from between the floor
panels (4).
Subtask 53-12-13-020-051
EFF :
ALL 53-12-13
Page 402
Feb 01/07
IAC
FWD Avionics-Compartment Floor-Panels
Figure 401/TASK 53-12-13-991-001
EFF :
ALL 53-12-13
Page 403
Feb 01/96
IAC
AFT Avionics-Compartment Floor-Panels
Figure 402/TASK 53-12-13-991-002
R
EFF :
001-012, 014-099, 53-12-13
Page 404
May 01/06
IAC
AFT Avionics-Compartment Floor-Panels
Figure 402A/TASK 53-12-13-991-002-A
R
EFF :
101-199, 901-999, 53-12-13
Page 405
Feb 01/07
IAC
R **ON A/C ALL
(7) Find one of the ends of the synthetic fiber cord at one of the floor
panel joints.
(8) Pull the cord up to remove the sealant from between the floor panels.
EFF :
ALL 53-12-13
Page 406
May 01/06
IAC
TASK 53-12-13-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-12-13
Page 407
Feb 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-12-13-869-050
(1) Make sure that the access platform is in position in zone 121/122 and
128.
(2) Make sure that the doors 811 and 824 are open.
Subtask 53-12-13-160-050
EFF :
ALL 53-12-13
Page 408
Feb 01/07
IAC
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1) Remove the old sealant from the floor panels and the component
interface with a non metallic scraper if the sealant is not easy to
remove use CLEANING AGENTS (Material No. 11-003) and a lint-free
cloth.
(2) Remove the adhesive of the old strips with CLEANING AGENTS (Material
No. 11-021).
Subtask 53-12-13-210-050
(1) Make sure that the parts retained from the removed component are
clean and in the correct condition.
Subtask 53-12-13-210-051
(1) Make sure that adhesive tapes are clean and in correct condition.
If necessary, repair the related adhesive tape (Ref. TASK 53-12-00-
300-001).
4. Procedure
_________
Subtask 53-12-13-420-050
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Apply SPECIAL MATERIALS (Material No. 05-002) to the screws (3).
EFF :
ALL 53-12-13
Page 409
May 01/06
R
IAC
(5) Put the stiffener (2) in position.
(6) Apply SPECIAL MATERIALS (Material No. 05-002) to the screws (1).
(7) Install the screws (1) and TORQUE them to between 0.15 and 0.40 m.daN
(13.27 and 35.39 lbf.in)
Subtask 53-12-13-420-051
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Put the floor panels (14), (15), (16) and (17) in position.
(3) Apply SPECIAL MATERIALS (Material No. 05-002) to the screws (13).
(4) Install the screws (13) and TORQUE them to between 0.15 and 0.40
m.daN (13.27 and 35.39 lbf.in)
(6) Apply SPECIAL MATERIALS (Material No. 05-002) to the screws (19).
(8) TORQUE the screws (19) to between 0.15 and 0.40 m.daN (13.27 and
35.39 lbf.in)
(10) Apply SPECIAL MATERIALS (Material No. 05-002) to the screws (11).
EFF :
ALL 53-12-13
Page 410
Feb 01/07
IAC
(11) Install the screws (11) and TORQUE them to between 0.15 and 0.40
m.daN (13.27 and 35.39 lbf.in)
Subtask 53-12-13-914-050
(1) Install the cord MISCELLANEOUS (Material No. 19-002) in the gap
between the floor panels. Make a loop at the end of the cord, this
helps for the next removal procedure.
(2) Apply SEALANTS (Material No. 09-018) in the joints between the floor
panels.
Subtask 53-12-13-420-052
(1) Put the fitting (24), the track (27) and the sheet metal assembly
(30) in position.
(2) Install the screws (22), (25), (28) and the washers (23), (26), (29).
(3) TORQUE the screws (22), (25) and (28), to between 0.15 and 0.40 m.daN
(13.27 and 35.39 lbf.in)
EFF :
ALL 53-12-13
Page 411
Feb 01/07
IAC
5. Close-up
________
Subtask 53-12-13-410-050
A. Close Access
(1) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-12-13
Page 412
May 01/06
IAC
RADOME (1560WM) - MAINTENANCE PRACTICES
_______________________________________
TASK 53-15-11-010-001
WARNING : MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THE WEATHER RADAR ARE
_______
OPENED, SAFETIED AND TAGGED.
WARNING : DO NOT OPEN THE RADOME IF THE WIND SPEED IS MORE THAN 35 KNOTS.
_______
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-15-11
Page 201
May 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-15-11-865-058
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
Subtask 53-15-11-941-055
B. Get Access
4. Procedure
_________
Subtask 53-15-11-010-053
WARNING : DO NOT OPEN THE RADOME IF THE WIND SPEED IS MORE THAN 35 KNOTS.
_______
NOTE : You must fully close the radome to lock it correctly in open
____
position.
NOTE : Two persons are necessary for this task, one on each side of the
____
radome. Each person must release the latches (1) on his side and
lift the radome (3) to its maximum open and locked position.
EFF :
ALL 53-15-11
Page 202
Aug 01/06
IAC
R Opening/Closing of the Radome
Figure 201/TASK 53-15-11-991-004
EFF :
ALL 53-15-11
Page 203
Nov 01/98
IAC
(2) Lift the radome (3) until the two rods (4) are locked and you hear
the locking click of each rod (4).
EFF :
ALL 53-15-11
Page 204
May 01/06
R
IAC
TASK 53-15-11-410-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-15-11-869-052
(1) Make sure that the access platform is in position in the zone 110.
EFF :
ALL 53-15-11
Page 205
May 01/06
R
IAC
Subtask 53-15-11-865-059
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
4. Procedure
_________
Subtask 53-15-11-410-053
(1) Support the radome (3) but do not lift it (person A in front of the
radome).
(a) Push the bush (2) of the two rods (4) (person B) to the end of
travel until you hear the unlocking click of the rods (4).
NOTE : The painted red mark on the lower tube comes into view.
____
(a) Lift the radome (3) (person A) until you hear the unlocking click
of the rods (4).
EFF :
ALL 53-15-11
Page 206
Aug 01/06
IAC
(6) Make sure that the radome (3) is closed.
5. Close-up
________
Subtask 53-15-11-865-060
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
5SQ1, 5SQ2
Subtask 53-15-11-942-056
B. Close Access
EFF :
ALL 53-15-11
Page 207
May 01/06
IAC
RADOME (1560WM) - REMOVAL/INSTALLATION
______________________________________
TASK 53-15-11-000-001
WARNING : MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THE WEATHER RADAR ARE
_______
OPENED, SAFETIED AND TAGGED.
NOTE : You must first fully close the radome to lock it correctly in the open
____
position.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-15-11
Page 401
May 01/01
IAC
3. __________
Job Set-up
Subtask 53-15-11-865-050
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
Subtask 53-15-11-941-050
B. Get Access
WARNING : DO NOT OPEN THE RADOME IF THE WIND SPEED IS MORE THAN 35 KNOTS.
_______
(1) Put the access platform in position in the zone 110 in front of the
radome.
Subtask 53-15-11-620-050
CAUTION : DO NOT USE THE LOCALIZER ANTENNA AT THE BOTTOM OF THE RADOME AS
_______
A SUPPORT.
EFF :
ALL 53-15-11
Page 402
Aug 01/06
IAC
Subtask 53-15-11-420-052
(2) Attach the ends of the sling to the housings of the handles (41) and
to the hinge fittings.
Subtask 53-15-11-420-053
4. Procedure
_________
Subtask 53-15-11-020-052
(a) Remove the nuts (6), the bolts (10) and the washers(9).
(2) Disconnect the rods (13) from the hinge fittings (7) of the radome.
EFF :
ALL 53-15-11
Page 403
Aug 01/06
R
IAC
Radome Sling
Figure 401/TASK 53-15-11-991-001
EFF :
ALL 53-15-11
Page 404
Aug 01/06
R
IAC
R Radome
Figure 402/TASK 53-15-11-991-002
EFF :
ALL 53-15-11
Page 405
May 01/97
IAC
Subtask 53-15-11-210-050
Subtask 53-15-11-020-050
Subtask 53-15-11-020-054
EFF :
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Page 406
Aug 01/06
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IAC
TASK 53-15-11-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 407
May 01/06
IAC
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-15-11
Page 408
Feb 01/07
IAC
3. __________
Job Set-up
Subtask 53-15-11-869-050
Subtask 53-15-11-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
Subtask 53-15-11-420-056
Subtask 53-15-11-820-051
(2) Extend the rods and lock them with the bushes (22).
EFF :
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Page 409
Feb 01/07
R
IAC
(3) Loosen the nut (21) and turn the eye end (20) to set the rod (13) to
a nominal center-to-center distance of L=544 +1 -1 mm (21.4173
+0.0393 -0.0393 in.).
R (5) Lubricate the bolts and the eye ends of the rods (13) with COMMON
GREASE (Material No. 04-004).
4. Procedure
_________
Subtask 53-15-11-420-050
CAUTION : DO NOT USE THE LOCALIZER ANTENNA AT THE BOTTOM OF THE RADOME AS
_______
A SUPPORT.
(1) Carefully put the radome in position with the lifting equipment.
(a) Put the hinge fittings (7) of the radome in position opposite the
support fittings of the radome.
Subtask 53-15-11-420-055
(1) Install the rods (13) on the hinge fittings of the radome.
EFF :
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Feb 01/07
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(d) Install the cotter pins (18).
(a) Install the bolts (10), the washers (9) and the nuts (6).
Subtask 53-15-11-020-055
Subtask 53-15-11-820-050
R (1) Close then open the radome two times (Ref. TASK 53-15-11-410-001)
R (Ref. TASK 53-15-11-010-001).
R (4) Make sure that the tension of the lock is between 8 daN (17.9847 lbf)
R and 12 daN (26.9770 lbf).
R (b) Adjust the tension of the lock to between 8 daN (17.9847 lbf) and
R 12 daN (26.9770 lbf) with the nut (31) of the spring rod (32).
R
EFF :
ALL 53-15-11
Page 411
Feb 01/07
IAC
Adjustment of the Locking Handle of the Radome
Figure 403/TASK 53-15-11-991-003
EFF :
ALL 53-15-11
Page 412
May 01/04
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IAC
**ON A/C 001-012, 014-099,
Subtask 53-15-11-820-056
R (1) Make sure that the out-of-flush dimension between the hinge arm (92)
R and the radome (91) is J1= 0.5 -1.5 +1.5 mm (0.0196 -0.0590 +0.0590
in.).
Subtask 53-15-11-820-056-A
R (1) Make sure that the out-of-flush dimension between the hinge arm (93)
R and the radome (92) is J1= 0.5 -1.5 +1.5 mm (0.0196 -0.0590 +0.0590
R in.).
R (b) Adjust the position of the fitting (94) with the serrated plate
R (95).
(c) TORQUE the four screws (91) to between 0.26 and 0.30 m.daN (23.00
and 26.54 lbf.in).
EFF :
ALL 53-15-11
Page 413
Feb 01/07
IAC
R Check of Hook Out-of-Flush Dimension
Figure 404/TASK 53-15-11-991-012
EFF :
001-012, 014-099, 53-15-11
Page 414
Feb 01/07
IAC
R Check of Hook Out-of-Flush Dimension and Adjustment
Figure 404A/TASK 53-15-11-991-012-A
R
EFF :
101-199, 901-999, 53-15-11
Page 415
Feb 01/07
IAC
**ON A/C ALL
Subtask 53-15-11-220-053
(1) Open then close the radome two times (Ref. TASK 53-15-11-010-001)
(Ref. TASK 53-15-11-410-001).
(c) In the FR1 intermediate area (points 8 and 11), make sure that A1
is between -1.5 mm (-0.0590 in.) and +3.5 mm (+0.1377 in.) on the
radome periphery.
(d) In the FR1 lower area (points 9 and 10), make sure that A1 is
between -1.5 mm (-0.0590 in.) and +4.5 mm (+0.1771 in.) on the
radome periphery.
(3) Measure the peripheral clearance J1 between the radome and the
aircraft structure. You must do this at:
- 15 equidistant points: 1 to 3, 5 to 14, 16 and 17.
- 2 specified points at the top left and right corners of the radome:
4 and 15.
R (a) Make sure that J1 is 2 -1.8 +1.5 mm (0.0787 -0.0708 +0.0590 in.).
EFF :
ALL 53-15-11
Page 416
Aug 01/07
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R Clearances between the Radome and the Aircraft Structure
R Figure 405/TASK 53-15-11-991-006
R
EFF :
ALL 53-15-11
Page 417
Feb 01/07
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Subtask 53-15-11-220-055
(1) Close the radome (102) until the seals (104) touch the aircraft
structure (101).
R (4) Make sure that the arrestor pick-up fittings are connected correctly
R to the bonding-clips.
R (6) Make sure that the two radome seals (104) are correctly compressed
along their full length and make sure that the seal compression D1 -
D2 is 3 +2 -2 mm (0.1181 +0.0787 -0.0787 in.).
Subtask 53-15-11-720-050
(2) Measure the ohmic resistance between each lightning arrestor strip of
the radome and the adjacent primary structure of the aircraft
(Ref. TASK 20-28-00-869-002).
Subtask 53-15-11-640-052
J. Application of Grease
(Ref. Fig. 407/TASK 53-15-11-991-014)
(2) Clean the contact surface of the stop fittings (41) with CLEANING
AGENTS (Material No. 11-003) and MISCELLANEOUS (Material No. 19-003).
R (3) Apply SPECIAL MATERIALS (Material No. 05-001) on the surface of the
R stop fittings (41) that touch the structure.
R
EFF :
ALL 53-15-11
Page 418
Feb 01/07
IAC
Radome - Seal Compression
Figure 406/TASK 53-15-11-991-015
EFF :
ALL 53-15-11
Page 419
Feb 01/07
R
IAC
Stop Fittings - Application of Grease
Figure 407/TASK 53-15-11-991-014
EFF :
ALL 53-15-11
Page 420
Feb 01/07
R
IAC
5. Close-up
________
Subtask 53-15-11-865-052
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
5SQ1, 5SQ2
Subtask 53-15-11-160-051
Subtask 53-15-11-942-051
C. Close Access
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-15-11
Page 421
Feb 01/07
IAC
INTENTIONALLY BLANK
R
53-15-11
Page 422
Feb 01/07
IAC
TASK 53-15-11-000-002
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-15-11
Page 423
May 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-15-11-865-055
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
Subtask 53-15-11-941-053
B. Get Access
(1) Put the access platform in position in the zone 110 in front of the
radome.
(2) In the cockpit put a warning notice in position to tell persons not
to operate the radar system.
Subtask 53-15-11-620-051
Subtask 53-15-11-420-054
(2) Attach the ends of the sling to the housings of the handles (41) and
to the hinge fittings.
EFF :
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Page 424
Aug 01/06
IAC
(3) Put the lifting equipment with a capacity of 50 kg (110.2311 lb) in
position.
4. Procedure
_________
Subtask 53-15-11-020-051
EFF :
ALL 53-15-11
Page 425
May 01/06
R
IAC
Radome
Figure 408/TASK 53-15-11-991-005
EFF :
ALL 53-15-11
Page 426
May 01/06
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IAC
TASK 53-15-11-400-002
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
EFF :
ALL 53-15-11
Page 427
May 01/06
IAC
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-15-11-869-051
(2) Make sure that the warning notice is in position in the cockpit to
tell persons not to operate the radar system.
Subtask 53-15-11-865-056
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
EFF :
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Page 428
Aug 01/06
IAC
R
Subtask 53-15-11-820-053
(3) Pull up the bush (13) and extend the rod (4).
(4) Push down the bush (13) to lock the rod in the extended position.
Subtask 53-15-11-640-051
D. Lubrication.
(1) Lubricate the bolts and the ends of the rod (4) with the COMMON
GREASE (Material No. 04-004).
4. Procedure
_________
Subtask 53-15-11-420-051
(2) Install the bolt (2) with the head on the outer side of the aircraft.
EFF :
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Page 429
Aug 01/06
IAC
(7) Install the bolt (3) with the head on the outer side of the aircraft.
If it is necessary, pull the heads of the rods to install the bolt
(3) easily.
Subtask 53-15-11-020-056
(1) Loosen SLING-RADOME (42) and remove it from the radome (10).
Subtask 53-15-11-720-051
C. Functionnal Test.
5. Close-up
________
Subtask 53-15-11-010-054
Subtask 53-15-11-865-057
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
5SQ1, 5SQ2
EFF :
ALL 53-15-11
Page 430
May 01/06
R
IAC
Subtask 53-15-11-942-055
C. Close Access
(2) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-15-11
Page 431
May 01/06
R
IAC
TASK 53-15-11-000-003
WARNING : MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THE WEATHER RADAR ARE
_______
OPENED, SAFETIED AND TAGGED.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-15-11
Page 432
Aug 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-15-11-865-061
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
Subtask 53-15-11-941-056
B. Get Access
WARNING : DO NOT OPEN THE RADOME IF THE WIND SPEED IS MORE THAN 35 KNOTS.
_______
(1) Put the access platform in position in the zone 110 in front of the
radome.
4. Procedure
_________
Subtask 53-15-11-020-057
EFF :
ALL 53-15-11
Page 433
Aug 01/06
IAC
Locking Handle
Figure 409/TASK 53-15-11-991-007
EFF :
ALL 53-15-11
Page 434
May 01/06
R
IAC
(3) Remove the bolt (56), the washer (55) and remove the locking handle
(54).
EFF :
ALL 53-15-11
Page 435
Aug 01/06
R
IAC
TASK 53-15-11-400-003
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-15-11
Page 436
Aug 01/06
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-15-11-869-054
(1) Make sure that the radome is open (Ref. TASK 53-15-11-010-001).
(2) Make sure that the access platform is in position in the zone 110.
(3) Make sure that the warning notice which tells persons not to operate
the radar system is in position on the center pedestal.
Subtask 53-15-11-865-065
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
EFF :
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Page 437
Feb 01/07
IAC
4. Procedure
_________
Subtask 53-15-11-420-058
Subtask 53-15-11-820-055
(4) Make sure that the tension of the lock is to between 8 daN (17.9847
lbf) and 12 daN (26.9770 lbf).
(b) Adjust the tension of the lock to between 8 daN (17.9847 lbf) and
12 daN (26.9770 lbf) with the nut (57) of the spring rod (58).
EFF :
ALL 53-15-11
Page 438
Feb 01/07
R
IAC
Locking Handle Adjustment
Figure 410/TASK 53-15-11-991-008
EFF :
ALL 53-15-11
Page 439
Aug 01/06
R
IAC
**ON A/C 001-012, 014-099,
Subtask 53-15-11-820-057
(1) Check that the out-of-flushness between hinge arm (102) and radome
(101) is J1= 0.5 -1.5 +1.5 mm (0.0196 -0.0590 +0.0590 in.).
Subtask 53-15-11-820-057-A
(1) Check that the out-of-flushness between hinge arm (103) and radome
(102) is J1= 0.5 -1.5 +1.5 mm (0.0196 -0.0590 +0.0590 in.).
5. Close-up
________
Subtask 53-15-11-865-066
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
5SQ1, 5SQ2
EFF :
ALL 53-15-11
Page 440
Feb 01/07
IAC
Check of Hook Out-of-Flushness
Figure 411/TASK 53-15-11-991-013
R
EFF :
001-012, 014-099, 53-15-11
Page 441
Aug 01/06
IAC
Check of Hook Out-of-Flushness and Adjustment
Figure 411A/TASK 53-15-11-991-013-A
R
EFF :
101-199, 901-999, 53-15-11
Page 442
Feb 01/07
IAC
Subtask 53-15-11-942-058
B. Close Access
(2) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-15-11
Page 443
Aug 01/06
R
IAC
TASK 53-15-11-000-004
WARNING : MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THE WEATHER RADAR ARE
_______
OPENED, SAFETIED AND TAGGED.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-15-11
Page 444
Aug 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-15-11-865-064
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
Subtask 53-15-11-941-058
B. Get Access
WARNING : DO NOT OPEN THE RADOME IF THE WIND SPEED IS MORE THAN 35 KNOTS.
_______
(1) Put the access platform in position in the zone 110 in front of the
radome.
4. Procedure
_________
Subtask 53-15-11-020-058
EFF :
ALL 53-15-11
Page 445
Aug 01/06
IAC
Arrestor Pick-Up Fitting
Figure 412/TASK 53-15-11-991-009
EFF :
ALL 53-15-11
Page 446
Aug 01/06
R
IAC
(2) Remove the arrestor pick-up fitting (62).
EFF :
ALL 53-15-11
Page 447
Aug 01/06
R
IAC
TASK 53-15-11-400-004
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-15-11
Page 448
Aug 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-15-11-869-055
(1) Make sure that the radome is open (Ref. TASK 53-15-11-010-001).
(2) Make sure that the access platform is in position in the zone 110.
(3) Make sure that the warning notice which tells persons not to operate
the radar system is in position on the center pedestal.
Subtask 53-15-11-865-067
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
EFF :
ALL 53-15-11
Page 449
Aug 01/06
IAC
R
4. Procedure
_________
Subtask 53-15-11-110-050
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1) Clean the mating surfaces of the arrestor pick-up fitting and the
frame edge of the radome with CLEANING AGENTS (Material No. 11-003)
and MISCELLANEOUS (Material No. 19-003).
(2) Make sure that the parts retained from the removed component are
clean and in the correct condition.
Subtask 53-15-11-420-059
(1) Apply SEALANTS (Material No. 09-016) on the mating surfaces of the
arrestor pick-up fitting and the frame edge of the radome.
EFF :
ALL 53-15-11
Page 450
Aug 01/06
IAC
(5) Close the radome (Ref. TASK 53-15-11-410-001).
Subtask 53-15-11-720-053
(1) Make sure that the radome is closed (Ref. TASK 53-15-11-410-001).
(2) Measure the ohmic resistance between each lightning arrestor strip of
the radome and the adjacent primary structure of the aircraft
(Ref. TASK 20-28-00-869-002).
5. Close-up
________
Subtask 53-15-11-865-068
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
5SQ1, 5SQ2
Subtask 53-15-11-942-059
B. Close Access
(2) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-15-11
Page 451
Aug 01/06
R
IAC
TASK 53-15-11-000-005
WARNING : MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THE WEATHER RADAR ARE
_______
OPENED, SAFETIED AND TAGGED.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-15-11
Page 452
Feb 01/07
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-15-11-865-069
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
Subtask 53-15-11-941-057
B. Get Access
WARNING : DO NOT OPEN THE RADOME IF THE WIND SPEED IS MORE THAN 35 KNOTS.
_______
(1) Put the access platform in position in the zone 110 in front of the
radome.
4. Procedure
_________
Subtask 53-15-11-020-059
EFF :
ALL 53-15-11
Page 453
Feb 01/07
R
IAC
Radome Seal
Figure 413/TASK 53-15-11-991-010
R
EFF :
001-012, 014-099, 53-15-11
Page 454
Feb 01/07
IAC
R **ON A/C 101-199, 901-999,
(1) Remove the nuts (72), the supports (73) and the bolts (71).
(2) Remove the two seals (74) from the frame edge (76).
R
EFF :
ALL 53-15-11
Page 455
Feb 01/07
IAC
Radome Seal
Figure 413A/TASK 53-15-11-991-010-A
R
EFF :
101-199, 901-999, 53-15-11
Page 456
Feb 01/07
IAC
TASK 53-15-11-400-005
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-15-11
Page 457
May 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-15-11-869-056
(1) Make sure that the radome is open (Ref. TASK 53-15-11-010-001).
(2) Make sure that the access platform is in position in the zone 110.
(3) Make sure that the warning notice which tells persons not to operate
the radar system is in position on the center pedestal.
Subtask 53-15-11-865-070
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
EFF :
ALL 53-15-11
Page 458
Feb 01/07
IAC
4. Procedure
_________
Subtask 53-15-11-420-060
(2) Install the seal (74) 6 mm (0.2362 in.) from the guide (75) between
the frame edge (76) and the related support (73) with the bolts (71)
and the nuts (72). Do not tighten.
Continue this operation until the three supports (73) are fully on
the right or left seal (74), with each support at its related
location.
Subtask 53-15-11-420-060-A
(2) Install the seal (74) 6 mm (0.2362 in.) from the guide (75) between
the frame edge (76) and the related support (73) with the bolts (71)
and the nuts (72). Do not tighten.
Continue this operation until the four supports (73) are fully on the
right or left seal (74), with each support at its related location.
EFF :
ALL 53-15-11
Page 459
Feb 01/07
IAC
**ON A/C ALL
Subtask 53-15-11-220-054
(1) Close the radome (82) until the seals (84) touch the aircraft
structure (91).
(5) Make sure that the two radome seals (84) are correctly compressed
along all their length and make sure that the seal compression C1 -
C2 is 3 +2 -2 mm (0.1181 +0.0787 -0.0787 in.).
5. Close-up
________
Subtask 53-15-11-865-071
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
5SQ1, 5SQ2
Subtask 53-15-11-942-060
B. Close Access
EFF :
ALL 53-15-11
Page 460
Aug 01/06
R
IAC
Radome Seal - Clearances
Figure 414/TASK 53-15-11-991-011
EFF :
ALL 53-15-11
Page 461
Aug 01/06
R
IAC
TASK 53-15-11-000-006
WARNING : MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THE WEATHER RADAR ARE
_______
OPENED, SAFETIED AND TAGGED.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-15-11
Page 462
Aug 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-15-11-865-072
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
Subtask 53-15-11-941-059
B. Get Access
WARNING : DO NOT OPEN THE RADOME IF THE WIND SPEED IS MORE THAN 35 KNOTS.
_______
(1) Put the access platform in position in the zone 110 in front of the
radome.
4. Procedure
_________
Subtask 53-15-11-020-060
EFF :
ALL 53-15-11
Page 463
Aug 01/06
IAC
Seal at Frame 1
Figure 415/TASK 53-15-11-991-016
EFF :
ALL 53-15-11
Page 464
Aug 01/06
R
IAC
TASK 53-15-11-400-006
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-15-11-869-057
(1) Make sure that the radome is open (Ref. TASK 53-15-11-010-001).
(2) Make sure that the access platform is in position in the zone 110.
(3) Make sure that the warning notice which tells persons not to operate
the radar system is in position on the center pedestal.
EFF :
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Subtask 53-15-11-865-073
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
4. Procedure
_________
Subtask 53-15-11-420-061
(1) Install the applicable new seal (112) on its support (113).
(2) Install the retainer (111) and tighten the screws (110).
5. Close-up
________
Subtask 53-15-11-865-074
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
5SQ1, 5SQ2
EFF :
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Subtask 53-15-11-942-061
B. Close Access
EFF :
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RADOME (1560WM) - ADJUSTMENT/TEST
_________________________________
TASK 53-15-11-700-002
1. __________________
Reason for the Job
Self explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific chalk
No specific access platform 3.5 m (11 ft. 6 in.)
98A57103013000 1 TAP TEST TOOL
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-15-11-941-060
A. Get Access
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Nov 01/03
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4. Procedure
_________
Subtask 53-15-11-750-050
A. Tap Test
CAUTION : TAP THE SURFACE OF THE COMPONENT LIGHTLY. IF YOU APPLY TOO MUCH
_______
FORCE, YOU CAN CAUSE DAMAGE TO THE RADOME.
(1) Tap the full surface of the inspection area with a TAP TEST TOOL
(98A57103013000) in a grid pattern with a distance of approximately
10 mm (0.3937 in.) between the grids
(Ref. Fig. 501/TASK 53-15-11-991-017)
5. Close-up
________
Subtask 53-15-11-860-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
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Radome - Tap Test Tool and Grid Pattern
Figure 501/TASK 53-15-11-991-017
EFF :
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R **ON A/C 001-012, 014-099,
TASK 53-15-11-760-002
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-15-11-941-064
A. Get Access
Subtask 53-15-11-010-057
R
EFF :
001-012, 014-099, 53-15-11
Page 504
May 01/06
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4. Procedure
_________
Subtask 53-15-11-760-052
(1) Send the radome to a repair station for a radio electrical test.
5. Close-up
________
Subtask 53-15-11-410-056
Subtask 53-15-11-942-064
B. Close Access
R
EFF :
001-012, 014-099, 53-15-11
Page 505
May 01/06
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TASK 53-15-11-760-002- 01
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-15-11-941-065
A. Get Access
Subtask 53-15-11-010-058
R
EFF :
001-012, 014-099, 53-15-11
Page 506
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4. Procedure
_________
Subtask 53-15-11-760-053
(2) Refer to the user manual of the TEST TOOL - RADOME (LCRAD0300HM0100)
to do a radio electrical test.
5. Close-up
________
Subtask 53-15-11-410-057
Subtask 53-15-11-942-065
B. Close Access
R
EFF :
001-012, 014-099, 53-15-11
Page 507
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RADOME (1560WM) - INSPECTION/CHECK
__________________________________
TASK 53-15-11-200-001
WARNING : MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THE WEATHER RADAR ARE
_______
OPENED, SAFETIED AND TAGGED.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
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Nov 01/03
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C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-15-11-860-052
Subtask 53-15-11-941-052
B. Get Access
(1) Put an access platform in position at zone 110 and an access platform
in position at zone 811.
(2) Open the forward avionics-compartment door 811 (Ref. TASK 52-41-00-
010-002).
(3) Install warning notices in the cockpit to tell persons not to operate
the radar system.
EFF :
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Subtask 53-15-11-865-053
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
Subtask 53-15-11-100-050
(1) Remove all the particles and contamination with a vacuum cleaner.
(2) Clean the radome with CLEANING AGENTS (Material No. 11-001A) or
CLEANING AGENTS (Material No. 11-001Q) and a soft brush or a
lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
(3) Dry the radome with a lint-free cotton cloth MISCELLANEOUS (Material
No. 19-003) before the CLEANING AGENTS (Material No. 11-001A) or
CLEANING AGENTS (Material No. 11-001Q) becomes dry.
Subtask 53-15-11-210-055
(1) Do a check of the inspection area for damage in Zone A around the
fittings. If there is damage:
EFF :
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R Damage Areas
Figure 601/TASK 53-15-11-991-019
EFF :
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May 01/06
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(2) Do a check of the inspection area for damage in Zone B. If there is
damage:
(Ref. Fig. 602/TASK 53-15-11-991-020)
1
_ The distance between two adjacent areas, X, must be more than
X min. X min must be less than or equal to 300 mm (11.8110
in.) and more than or equal to max. (dia.i, dia.j).
2
_ If X is less than X min, there is one damage area.
3
_ If X is less than or equal to 300 mm (11.8110 in.) and more
than or equal to X min, there are two different damage areas.
4
_ If X is more than 300 mm (11.8110 in.), there are two
different damage areas.
1
_ The minimum distance between the repairs is 150 mm (5.9055
in.).
(c) Measure the distance between the Zone B damage and Zone A.
1
_ The distance between the damage and Zone A, C, must be more
than C min = 0 mm (0.0000 in.).
2
_ If C is more than or equal to C min, repair is permitted.
R Refer to the subsequent paragraph for permitted types of
R damage.
3
_ If C is less than C min:
- Immediately remove (Ref. TASK 53-15-11-000-001) and send the
radome to a repair station.
- Install a new radome (Ref. TASK 53-15-11-400-001).
4. Procedure
_________
Subtask 53-15-11-220-050
A. Inspection of the Outer Face for all Types of Radome (KEVLAR radome: P/N
D5311047700001, P/N D5311047700002, P/N D5311047700003, P/N
D5311047700004, P/N D5311047700005; QUARTZ radome: P/N D5311047700006,
P/N D5311047700007, P/N D53132010000)
(Ref. Fig. 603/TASK 53-15-11-991-021)
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Distance between the Damage Areas and the Repair Areas
Figure 602/TASK 53-15-11-991-020
EFF :
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May 01/06
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R Possible Types of Damage - Outer Face of the Radome
Figure 603/TASK 53-15-11-991-021
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(1) Do an inspection for scratches, gouges, nicks and peeling.
1
_ If the area has peeling, gouges or nicks of the paint:
a
_ Remove the flakes and immediately do a temporary repair
with adhesive tape (Ref. TASK 53-15-11-300-001). Do a
permanent repair at the subsequent 600FH check.
2
_ If the area has one or two plies of composite that have
scratches:
- Immediately do a temporary repair with adhesive tape
(Ref. TASK 53-15-11-300-001). Do a permanent repair at the
subsequent 600FH check.
3
_ If the area has more than two plies that have scratches:
- Immediately remove (Ref. TASK 53-15-11-000-001) and send the
radome to a repair station.
- Install a new radome (Ref. TASK 53-15-11-400-001).
(c) If the distance between the damage and the monolithic area is
less than 200 mm (7.8740 in.):
- Immediately remove (Ref. TASK 53-15-11-000-001) and send the
radome to a repair station.
- Install a new radome (Ref. TASK 53-15-11-400-001).
EFF :
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R Damage Areas and Distances between Damage Areas on the Lightning Arrester
R Strips
Figure 604/TASK 53-15-11-991-023
EFF :
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53-15-11 Page 609
May 01/07
IAC
(b) If there are burn spots on the last screw-head (structure side)
of the lightning arrester strips, do a permanent repair (one
flight only is permitted before the repair).
1
_ If there is one damage area, measure the diameter Y.
a
_ If Y is less than or equal to 7 mm (0.2755 in.), no
procedure is immediately necessary. Do a permanent repair
at the subsequent 600FH check or 6000FH check, whichever
occurs first.
b
_ If Y is more than 7 mm (0.2755 in.):
- Immediately remove (Ref. TASK 53-15-11-000-001) and send
the radome to a repair station.
- Install a new radome (Ref. TASK 53-15-11-400-001).
R 2
_ If there is more than one damage area, measure the distance Z
R between the damage areas.
R a
_ If the distance Z is less than or equal to 5 mm (0.1968
R in.) from one or more damage area, you must measure the
R diameters (Y1, Y2, Y3, ...) and calculate the sum Y of the
R diameters of the damage areas.
R - If the sum Y is less than or equal to 7 mm (0.2755 in.):
R At the subsequent 600FH check or 6000FH check, whichever
R occurs first:
R Remove the radome (Ref. TASK 53-15-11-000-001), repair it
R (Ref. CMM 531511) and install it (Ref. TASK 53-15-11-400-
001),
R Or replace the radome (Ref. TASK 53-15-11-000-001) and
R (Ref. TASK 53-15-11-400-001).
R - If the sum Y is more than 7 mm (0.2755 in.):
R Immediately remove (Ref. TASK 53-15-11-000-001) and send
R the radome to a repair station.
R Install a new radome (Ref. TASK 53-15-11-400-001).
R b
_ If the distance Z is more than 5 mm (0.1968 in.) from all
R the damage areas, refer to the one damage area paragraph.
R
EFF :
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(3) Do an inspection for delamination, debonding and core crushing in
Zone B.
(Ref. Fig. 603/TASK 53-15-11-991-021)
(a) Do a tap test to get the delamination diameter (Ref. TASK 53-15-
11-700-002).
(d) If the distance between the damage and the monolithic area is
less than 200 mm (7.8740 in.):
- Immediately remove (Ref. TASK 53-15-11-000-001) and send the
radome to a repair station.
- Install a new radome (Ref. TASK 53-15-11-400-001).
EFF :
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(5) Do an inspection for black marks on the radome.
(a) If there are black marks on the radome, clean the surface area
with CLEANING AGENTS (Material No. 11-001A).
(b) If the distance between the damage and the monolithic area is
less than 200 mm (7.8740 in.):
- Immediately remove (Ref. TASK 53-15-11-000-001) and send the
radome to a repair station.
- Install a new radome (Ref. TASK 53-15-11-400-001).
Subtask 53-15-11-220-052
B. Inspection of the Inner Face for all Types of Radome (KEVLAR radome: P/N
D5311047700001, P/N D5311047700002, P/N D5311047700003, P/N
D5311047700004, P/N D5311047700005; QUARTZ radome: P/N D5311047700006,
P/N D5311047700007, P/N D53132010000)
EFF :
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Page 612
Aug 01/07
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Possible Types of Damage - Inner Face of the Radome
Figure 605/TASK 53-15-11-991-022
EFF :
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Nov 01/06
R
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(b) If there are burn spots on the radome contact element
(radome-to-structure junction), no procedure is immediately
R necessary. Do a permanent repair at the subsequent 600FH check or
R 6000FH check.
1
_ If the area has one ply that has scratches, no procedure is
necessary.
2
_ If the area has two plies that have scratches:
a
_ Immediately do a temporary repair with adhesive tape
(Ref. TASK 53-15-11-300-001). Do a permanent repair at the
subsequent 600FH check.
3
_ If the area has X plies that have scratches:
- Immediately remove (Ref. TASK 53-15-11-000-001) and send the
radome to a repair station.
- Install a new radome (Ref. TASK 53-15-11-400-001).
(c) If the distance between the damage and the monolithic area is
less than 200 mm (7.8740 in.):
- Immediately remove (Ref. TASK 53-15-11-000-001) and send the
radome to a repair station.
- Install a new radome (Ref. TASK 53-15-11-400-001).
(a) Do a tap test to get the delamination diameter (Ref. TASK 53-15-
11-700-002).
EFF :
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(c) If the diameter is more than 250 mm (9.8425 in.):
- Immediately remove (Ref. TASK 53-15-11-000-001) and send the
radome to a repair station.
- Install a new radome (Ref. TASK 53-15-11-400-001).
(d) If the distance between the damage and the monolithic area is
less than 200 mm (7.8740 in.):
- Immediately remove (Ref. TASK 53-15-11-000-001) and send the
radome to a repair station.
- Install a new radome (Ref. TASK 53-15-11-400-001).
(b) If the distance between the damage and the monolithic area is
less than 200 mm (7.8740 in.):
- Immediately remove (Ref. TASK 53-15-11-000-001) and send the
radome to a repair station.
- Install a new radome (Ref. TASK 53-15-11-400-001).
5. Close-up
________
Subtask 53-15-11-865-054
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
5SQ1, 5SQ2.
Subtask 53-15-11-942-052
B. Close Access
(2) Close the forward avionics-compartment door 811 (Ref. TASK 52-41-00-
410-002).
EFF :
ALL 53-15-11
Page 615
Aug 01/07
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(3) Remove the access platform(s).
EFF :
ALL 53-15-11
Page 616
Aug 01/07
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RADOME (1560WM) - REPAIRS
_________________________
TASK 53-15-11-300-001
1. __________________
Reason for the Job
Self explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
No specific ADVAC03200
No specific RP13
Material No. 05-065 C Z-24.380
EROSION PROTECTIVE TAPE (Ref. 20-31-00)
Material No. 08-001 USA DOD-A-82720
GENERAL PURPOSE ADHESIVE HONEYCOMB FILLER
(Ref. 20-31-00)
Material No. 11-026D F ASN 42202
GENERAL CLEANING AGENT - MULTI PURPOSE
(Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF :
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Page 801
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C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-15-11-941-061
A. Get Access
4. Procedure
_________
Subtask 53-15-11-350-050
A. Temporary repair
R (1) For all types of radome (KEVLAR radome: PN. D5311047700001, PN.
R D5311047700002, PN. D5311047700003, PN. D5311047700004, PN.
R D5311047700005; QUARTZ radome: PN. D5311047700006, PN.
R D5311047700007, PN. D53132010000), with SPECIAL MATERIALS (Material
R No. 05-065) or Polyurethane Adhesive Tape (Supplier/Ref. 8672):
(Ref. Fig. 801/TASK 53-15-11-991-018)
(a) Clean the damage area and remove the grease with a clean
lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) soaked
with CLEANING AGENTS (Material No. 11-026D).
EFF :
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Nov 01/07
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Temporary Repair of the Radome
Figure 801/TASK 53-15-11-991-018
EFF :
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Page 803
Nov 01/03
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(b) Apply SPECIAL MATERIALS (Material No. 05-065) or Polyurethane
Adhesive Tape (Supplier 3M/Ref. 8672) to the repair area.
R (2) For QUARTZ radomes only (PN. D5311047700006, PN. D5311047700007, PN.
D53132010000), with White or Gray Self-Adhesive Patch Dia. 50 mm
(1.9685 in.) (Supplier ADHETEC/Ref. 5015BC or 5015GS):
(a) Clean the damage area and remove the grease with a clean
lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) soaked
with CLEANING AGENTS (Material No. 11-026D).
Subtask 53-15-11-350-052
B. Permanent Repair
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R (1) For QUARTZ radomes only (PN. D5311047700006, PN. D5311047700007 and
R PN. D53132010000) with resin injection.
(Ref. Fig. 802/TASK 53-15-11-991-024)
CAUTION : MAKE SURE THAT THE DISTANCE (X) BETWEEN TWO RESIN
_______
INJECTIONS IS MORE THAN THE WIDTH OF THE LARGER RESIN
INJECTION: X > MAX. DIA.
IF THE DISTANCE IS LESS, DO NOT DO A SECOND RESIN INJECTION
BUT A PRE-PREG REPAIR THAT INCLUDES THE FIRST INJECTION.
IF THE NUMBER OF EXISTING INJECTIONS IS THE MAXIMUM
PERMITTED, THE NEW INJECTION (DIA. < 50 MM) MUST INCLUDE
THE PREVIOUS INJECTION IF POSSIBLE. IF IT CANNOT, YOU MUST
TO A PRE-PREG REPAIR.
(c) Clean the damage area and remove the grease with a lint-free
cotton cloth MISCELLANEOUS (Material No. 19-003) soaked with
CLEANING AGENTS (Material No. 11-026D).
(e) Remove swarf and clean with CLEANING AGENTS (Material No. 11-
026D). Carefully clean drilled holes.
(f) Fill the syringe with BONDING AND ADHESIVE COMPOUNDS (Material
No. 08-001), RP13 or ADVAC03200 and put it through the holes into
the honeycomb until the resin overflows.
EFF :
ALL 53-15-11
Page 805
Nov 01/07
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R Definitive repair of the Radome
R Figure 802/TASK 53-15-11-991-024
EFF :
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Page 806
Aug 01/06
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5. Close-up
________
Subtask 53-15-11-860-051
A. Close Access
(1) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-15-11
Page 807
Aug 01/06
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SCUFF PLATES - DOOR ENTRANCE - REMOVAL/INSTALLATION
___________________________________________________
TASK 53-15-15-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-15-15-941-050
A. Get Access
(2) Open the applicable FWD passenger/crew door 831 or 841 (Ref. TASK 52-
10-00-010-001).
EFF :
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R
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4. Procedure
_________
Subtask 53-15-15-020-050
CAUTION : MAKE SURE THAT YOU DO NOT DAMAGE THE FUSELAGE WHEN YOU REMOVE
_______
THE SCUFF PLATES.
R NOTE : The scuff plates can become damaged during the subsequent removal
____
R procedure.
(1) Remove the screws (1) and the cover strip (2).
(2) Remove the sealant between the scuff plates (3) (5) and (9) with a
non metallic scraper.
(3) Remove the screws (6) and (8), the nuts (4), and the washers (7) from
the scuff plates (3), (5) and (9).
(4) Blow air on the scuff plates (3), (5) and (9) with a hot air blower.
(5) Carefully put a non metallic wedge between the fuselage and the scuff
plates (3), (5) and (9).
NOTE : If the scuff plates (3), (5) and (9) are damaged, discard
____
them.
EFF :
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Page 402
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R FWD Passenger/Crew Door Scuff Plate
Figure 401/TASK 53-15-15-991-001
EFF :
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Page 403
Nov 01/00
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TASK 53-15-15-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 404
Nov 01/04
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C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-15-15-869-050
(2) Make sure that the applicable FWD passenger/crew door is open.
EFF :
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Subtask 53-15-15-110-051
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1) Clean the contact surfaces of the scuff plates and the fuselage skin
with CLEANING AGENTS (Material No. 11-003) and MISCELLANEOUS
(Material No. 19-003).
R
R (2) Make sure that the scuff plates are in the correct position and are
R not damaged. If necessary, replace the damaged scuff plates.
(4) Put the vacuum equipment adjacent to the required FWD passenger/crew
door.
NOTE : We recommend that you use a strong vacuum pump for attachment
____
of the scuff plates.
4. Procedure
_________
Subtask 53-15-15-420-050
NOTE : This procedure is applicable only when you install new scuff
____
plates.
EFF :
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Page 406
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(a) Take the new scuff plates:
- for the left passenger/crew door scuff plate (3), scuff plate
(5) and scuff plate (9).
- for the right passenger/crew door scuff plate (3), scuff plate
(5) and scuff plate (9).
(b) Put the scuff plates (3), (5) and (9) in position on the door
sill.
R (c) Drill the attachment hole of the scuff plates to the final
R diameter of 4.8 mm (0.1889 in.).
(d) Remove and deburr the scuff plates (3), (5) and (9).
(2) Make the top coat of the scuff plates (3), (5) and (9) rough with
scotch brite on an area of:
- 15 mm (0.5905 in.) width on the scuff plate periphery,
- 20 mm (0.7874 in.) radius around each fastener hole.
(3) Clean the rough area with CLEANING AGENTS (Material No. 11-003) and
MISCELLANEOUS (Material No. 19-003).
NOTE : The correct application of the release agent makes sure that
____
the scuff plates are not damaged during the subsequent removal
procedure.
(4) Apply adhesive tape on the rough area of the scuff plates.
(5) Apply a thin layer of SPECIAL MATERIALS (Material No. 05-013A) to the
remaining inner areas of the scuff plates (3), (5) and (9).
(6) Remove the adhesive tape from the scuff plates (3), (5) and (9).
(8) Put the scuff plates (3), (5) and (9) in position on the fuselage
skin.
(9) Install the cover strip (2), the screws (6), (8) and (1) with
SEALANTS (Material No. 09-016), the washers (7) and the nuts (4).
(10) Tighten the nuts (4) and the screws (1) , (6) and (8).
(11) Remove unwanted sealant around the scuff plates (3), (5) and (9).
EFF :
ALL 53-15-15
Page 407
Aug 01/07
IAC
R Scuff Plates - Installation Procedure
Figure 402/TASK 53-15-15-991-002- 12 (SHEET 1)
EFF :
ALL 53-15-15
Page 408
Nov 01/00
IAC
R Scuff Plates - Installation Procedure
Figure 402/TASK 53-15-15-991-002- 22 (SHEET 2)
EFF :
ALL 53-15-15
Page 409
Nov 01/00
IAC
(12) Apply SEALANTS (Material No. 09-030) around and approximately 30 mm
(1.1811 in.) from the edges of the scuff plates (3), (5) and (9).
(13) Cover the scuff plates (3), (5) and (9) with a sheet of porous
material.
(14) Attach the porous material with BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-065) to the scuff plates (3), (5) and (9).
(15) Connect the vacuum valve to the SPECIAL MATERIALS (Material No. 05-
068).
(16) Cover the scuff plates (3), (5) and (9) and SEALANTS (Material No.
09-030) with SPECIAL MATERIALS (Material No. 05-068). You must make
an overlap of 30 mm (1.2 in.) from the edge of SEALANTS (Material No.
09-030).
R (18) Operate the vacuum pump and increase the vacuum around the scuff
R plates (3), (5) and (9) to 0 bar (0.0000 psi).
Refer to the temperature given in the table:
-------------------------------------------------------------------------------
TEMPERATURE TIME
-------------------------------------------------------------------------------
(21) Remove the vacuum valve from the SPECIAL MATERIALS (Material No. 05-
068), the porous material, and SEALANTS (Material No. 09-030).
(22) Apply SEALANTS (Material No. 09-016) on the external joints of the
scuff plates (3), (5) and (9) and around the scuff plates.
(23) Remove unwanted sealant with CLEANING AGENTS (Material No. 11-003)
AND MISCELLANEOUS (Material No. 19-003).
EFF :
ALL 53-15-15
Page 410
Aug 01/07
IAC
5. Close-up
________
Subtask 53-15-15-942-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Close the applicable FWD passenger/crew door (Ref. TASK 52-10-00-410-
001).
EFF :
ALL 53-15-15
Page 411
Nov 01/00
R
IAC
MOUNT FITTING - CABIN - REMOVAL/INSTALLATION
____________________________________________
TASK 53-16-11-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-16-11-860-050
EFF :
ALL 53-16-11
Page 401
Nov 01/05
IAC
Subtask 53-16-11-010-050
B. Get Access
(2) Open the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
010-001).
4. Procedure
_________
Subtask 53-16-11-020-050
EFF :
ALL 53-16-11
Page 402
Nov 01/05
IAC
R Mount Fitting at FR 14
Figure 401/TASK 53-16-11-991-001
EFF :
ALL 53-16-11
Page 403
May 01/06
IAC
(3) For the plate (4)
(d) Remove the washers (16), the bolts (11) and the plate (4)
EFF :
ALL 53-16-11
Page 404
May 01/06
R
IAC
TASK 53-16-11-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-16-11
Page 405
May 01/06
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-16-11-860-051
(1) Make sure that the ground service network is energized (Ref. TASK 24-
42-00-861-001).
Subtask 53-16-11-010-051
B. Get Access
(1) Make sure that the access platform is in position at zone 831 (841).
(2) Make sure that the forward passenger/crew door 831 (841) is open
(Ref. TASK 52-10-00-010-001).
(3) Make sure that the Anti-Hijack-System Camera is removed (Ref. TASK
23-72-51-000-001), if installed.
(4) Make sure that the ceiling panel 221AC is removed (Ref. TASK 25-23-
42-000-001).
(5) Make sure that the lining panel 211HC is removed (Ref. TASK 25-13-41-
000-001).
(6) Make sure that the cockpit door is removed (Ref. TASK 52-51-11-000-
001).
EFF :
ALL 53-16-11
Page 406
Nov 01/05
IAC
4. Procedure
_________
Subtask 53-16-11-420-050
(a) Install the bolts (22), the washers (20) and the new nut (21)
(b) Install the bolts (24), the washers (18) and the new nut (19)
(a) Install the bolts (11), the washers (16) and the new nut (17)
(a) Install the bolts (12) and the new nut (15)
(b) Install the bolts (23), the washers (10) and the new nut (9)
(a) Install the bolts (3), the washers (5) and the new nut (6)
(b) Install the bolts (14) and the new nut (8).
5. Close-up
________
Subtask 53-16-11-410-050
A. Close Access
EFF :
ALL 53-16-11
Page 407
Nov 01/05
IAC
(3) Install the ceiling panel 221AC (Ref. TASK 25-23-42-400-001).
(5) Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
410-001).
Subtask 53-16-11-862-050
EFF :
ALL 53-16-11
Page 408
Nov 01/05
IAC
MISCELLANEOUS (EG : DRAINS) - DESCRIPTION AND OPERATION
_______________________________________________________
1. _______
General
Drains are installed in the nose forward fuselage structure of the aircraft
at or near to the lowest points in an area. The drains let water and
condensation drain out so that they do not cause corrosion.
2. ___________
Description
(Ref. Fig. 001)
Drain valves are installed in the nose forward fuselage shell. When the
cabin pressurizes, the valves, preset to operate when cabin pressurization
reaches 2 psi (0.1378 bar) , close to prevent loss of cabin pressure. As the
cabin pressure decreases below the preset value (normally after the aircraft
has landed), the valves open (under spring tension) to allow any water that
has collected to drain away. You can remove the drain valves, for inspection
or replacement, with an allen key from outside the aircraft.
In other structural components (doors, door frames, stringers, brackets and
fittings) holes are drilled at the lowest points to make sure that water and
condensation drain to the drain valves.
EFF :
ALL 53-19-00
Page 1
May 01/99
IAC
Nose Forward Fuselage - Drains
Figure 001
EFF :
ALL 53-19-00
Page 2
May 01/99
IAC
MISCELLANEOUS (EG : DRAINS) - INSPECTION/CHECK
______________________________________________
TASK 53-19-00-210-001
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific flashlight
No specific sponge
No specific access platform 3.50 m (11 ft. 6 in.)
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-19-00
Page 601
May 01/06
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-19-00-010-050
A. Get Access
(1) Put the access platform in position at the zone 831 (841).
(2) Open the FWD passenger/crew door 831 (841) (Ref. TASK 52-10-00-010-
001).
Subtask 53-19-00-110-050
(1) Clean the inspection area with a sponge and a solution of water and
soap and dry with a MISCELLANEOUS (Material No. 19-003).
4. Procedure
_________
Subtask 53-19-00-210-050
A. Inspection
(Ref. Fig. 601/TASK 53-19-00-991-001)
(2) Make sure that there is no unwanted material (dirt, water, debris):
- If there is unwanted material (dirt, water, debris), clean the area
following the procedure given above para. 3.B.
EFF :
ALL 53-19-00
Page 602
May 01/06
IAC
Cockpit Grid Collector Assy
Figure 601/TASK 53-19-00-991-001
EFF :
ALL 53-19-00
Page 603
May 01/06
R
IAC
**ON A/C ALL
5. Close-up
________
Subtask 53-19-00-410-050
A. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Close the FWD passenger/crew door 831 (841) (Ref. TASK 52-10-00-410-
001).
EFF :
ALL 53-19-00
Page 604
May 01/06
IAC
**ON A/C ALL
TASK 53-19-00-710-001
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific flashlight
No specific adjustable access platform 2 m (6 ft. 7 in.)
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-19-00
Page 605
May 01/06
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-19-00-010-054
A. Get Access
(2) Open the FWD passenger/crew door 831 (841) (Ref. TASK 52-10-00-010-
001).
(5) Open the avionics compartment door 824 (Ref. TASK 52-41-00-010-002).
4. Procedure
_________
Subtask 53-19-00-710-050
A. Inspection
(Ref. Fig. 602/TASK 53-19-00-991-002)
(a) Use a flashlight to make sure that the drainage pipe connectors
on the outputs of the fluid collector are in the correct
condition.
EFF :
ALL 53-19-00
Page 606
May 01/06
IAC
Cockpit Drainage Pipe
Figure 602/TASK 53-19-00-991-002
EFF :
ALL 53-19-00
Page 607
May 01/05
R
IAC
(b) Do a detailed visual inspection of the cockpit drainage pipe:
- fill the fluid collector with water and do a check of the
drainage pipe for leaks.
(c) If the drainage pipe is blocked, flush the drainage pipe with
water.
5. Close-up
________
Subtask 53-19-00-410-054
A. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Close the avionics compartment door 824 (Ref. TASK 52-41-00-410-002).
(5) Close the FWD passenger/crew door 831 (841) (Ref. TASK 52-10-00-410-
001).
EFF :
ALL 53-19-00
Page 608
May 01/06
IAC
**ON A/C ALL
TASK 53-19-00-710-003
Operational Check of Piston Type Drain Valves in Lower Fuselage Shell from
Outside
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-19-00
Page 609
May 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-19-00-010-056
A. Get Access
4. Procedure
_________
Subtask 53-19-00-710-052
A. Inspection Procedure
EFF :
ALL 53-19-00
Page 610
Feb 01/07
IAC
Piston-Type Drain Valves
Figure 603/TASK 53-19-00-991-003
R
EFF :
001-012, 014-099, 53-19-00
Page 611
May 01/06
IAC
R Piston-Type Drain Valves
R Figure 603A/TASK 53-19-00-991-003-B
EFF :
101-199, 53-19-00
Page 612
Feb 01/07
IAC
Piston-Type Drain Valves
R Figure 603B/TASK 53-19-00-991-003-A
R
EFF :
901-999, 53-19-00
Page 613
Feb 01/07
IAC
**ON A/C ALL
(a) Make sure that the basic valves are not blocked. Remove any
blockage.
(b) Carefully push a PROBE - NON METALLIC, FLEXIBLE into the center
of each basic valve and make sure that the valves are open.
5. Close-up
________
Subtask 53-19-00-860-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-19-00
Page 614
Feb 01/07
IAC
DRAINS - NOSE FORWARD FUSELAGE - REMOVAL/INSTALLATION
_____________________________________________________
TASK 53-19-41-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-19-41
Page 401
May 01/06
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-19-41-861-050
Subtask 53-19-41-010-050
B. Get Access
(2) Open the FWD passenger/crew door 831 (Ref. TASK 52-10-00-010-001).
4. Procedure
_________
Subtask 53-19-41-020-050
EFF :
ALL 53-19-41
Page 402
May 01/06
IAC
Collector Grid and Container
Figure 401/TASK 53-19-41-991-001
EFF :
ALL 53-19-41
Page 403
Nov 01/99
IAC
(5) Remove the screws (6) and the washers (5).
EFF :
ALL 53-19-41
Page 404
Nov 01/99
IAC
**ON A/C ALL
TASK 53-19-41-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-19-41
Page 405
May 01/05
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-19-41-860-050
(1) Make sure that the access platform is in position at zone 812.
(2) Make sure that the access platform is in position at zone 831.
(3) Make sure that the FWD passenger/crew door 831 is open (Ref. TASK 52-
10-00-010-001).
(4) Make sure that the avionics-compartment access door 812 is open.
EFF :
ALL 53-19-41
Page 406
May 01/06
IAC
**ON A/C ALL
4. Procedure
_________
Subtask 53-19-41-840-050
(1) Flush the collector grid (2) and the container (9).
(3) Dry the collector grid (2), the container (9) and the strainers (10).
Subtask 53-19-41-420-050
(7) Install the clamps (7) and TORQUE the clamps to 0.28 m.daN (24.77
lbf.in).
EFF :
ALL 53-19-41
Page 407
May 01/06
IAC
(10) Apply a layer of SEALANTS (Material No. 09-016) between the structure
and the grid rack assembly, on the heads of the screws (1) and on the
ends of the screws (4) and (6).
5. Close-up
________
Subtask 53-19-41-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Close the FWD passenger/crew door 831 (Ref. TASK 52-10-00-410-001).
Subtask 53-19-41-862-050
EFF :
ALL 53-19-41
Page 408
May 01/06
IAC
R **ON A/C ALL
R TASK 53-19-41-000-003
R 1. __________________
Reason for the Job
R Self Explanatory
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
ALL 53-19-41
Page 409
Nov 01/00
IAC
R 3. __________
Job Set-up
R Subtask 53-19-41-861-052
R Subtask 53-19-41-010-053
R Subtask 53-19-41-010-054
R C. Removal of Components
R 4. Procedure
_________
R Subtask 53-19-41-020-052
R (1) Remove the remaining sealant with CLEANING AGENTS (Material No. 11-
R 004), MISCELLANEOUS (Material No. 19-003) and a non metallic scraper
R around the valve (4).
EFF :
ALL 53-19-41
Page 410
Nov 01/00
IAC
R Drain Valve
R Figure 402/TASK 53-19-41-991-003
EFF :
ALL 53-19-41
Page 411
Nov 01/00
IAC
R (4) Remove the remaining sealant with CLEANING AGENTS (Material No. 11-
R 004), MISCELLANEOUS (Material No. 19-003) and a non metallic scraper
R around the retaining valve (2).
EFF :
ALL 53-19-41
Page 412
Nov 01/00
IAC
TASK 53-19-41-400-003
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-19-41
Page 413
May 01/05
IAC
R 3. __________
Job Set-up
R Subtask 53-19-41-860-052
R (1) Make sure that the aircraft electrical circuits are energized
R (Ref. TASK 24-41-00-861-002).
R Subtask 53-19-41-010-055
R B. Get Access
R (1) Make sure that the access platform is in position at zone 811.
R (2) Make sure that the avionics-compartment access door 811 is open.
R (3) Make sure that the access platform is in position at zone 824.
R (4) Make sure that the avionics-compartment access door 824 is open.
R (6) In the avionics compartment, make sure that the applicable floor
R panel is removed (Ref. TASK 53-12-13-000-001).
R 4. Procedure
_________
R Subtask 53-19-41-840-052
R (1) Make sure that the parts retained from the removed component are
R clean and in the correct condition.
EFF :
ALL 53-19-41
Page 414
Nov 01/00
IAC
R Subtask 53-19-41-420-052
R (3) Apply SEALANTS (Material No. 09-025) around the retaining valve (2).
R (5) Install the two bolts (3). Tighten the two nuts (1).
R (6) Apply SEALANTS (Material No. 09-018) or SEALANTS (Material No. 09-
R 019) between the valve (4) and the structure.
R 5. Close-up
________
R Subtask 53-19-41-410-052
R A. Installation of Components
R (2) Make sure that the work area is clean and clear of tool(s) and other
R items.
R Subtask 53-19-41-941-051
R B. Close Access
EFF :
ALL 53-19-41
Page 415
Nov 01/00
IAC
R Subtask 53-19-41-862-052
EFF :
ALL 53-19-41
Page 416
Nov 01/00
IAC
R **ON A/C 001-012, 014-019,
R TASK 53-19-41-000-004
R 1. __________________
Reason for the Job
R Self Explanatory
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R 3. __________
Job Set-up
R Subtask 53-19-41-860-054
EFF :
001-012, 014-019, 53-19-41
Page 417
May 01/06
IAC
R Subtask 53-19-41-010-056
R B. Get Access
R (2) Open the FWD Passenger/crew door 831 (Ref. TASK 52-10-00-010-001).
R 4. Procedure
_________
R Subtask 53-19-41-020-053
R (b) Remove the washer (16) and the bolt (14) from the pan (4).
EFF :
001-012, 014-019, 53-19-41
Page 418
May 01/06
IAC
R Airstairs Drain Panel
R Figure 403/TASK 53-19-41-991-004
EFF :
001-012, 014-019, 53-19-41
Page 419
May 01/06
IAC
R (j) Remove the washer (12) and the screw (13)
EFF :
001-012, 014-019, 53-19-41
Page 420
May 01/06
IAC
R TASK 53-19-41-400-004
R 1. __________________
Reason for the Job
R Self Explanatory
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Expendable Parts
R -------------------------------------------------------------------------------
R FIG.ITEM |DESIGNATION |IPC-CSN
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
001-012, 014-019, 53-19-41
Page 421
May 01/06
IAC
R 3. __________
Job Set-up
R Subtask 53-19-41-860-055
R (1) Make sure that the access platform is in position at zone 812.
R (2) Make sure that the access platform is in position at zone 831.
R (3) Make sure that the FWD Passenger/Crew door 831 is open (Ref. TASK 52-
R 10-00-010-001).
R (4) Make sure that the avionics-compartment access door 812 is open.
R 4. Procedure
_________
R Subtask 53-19-41-420-053
R (a) Install the screws (23), the washers (22) and the new nuts (21)
R (b) Install the screws (5), the washers (6) and the new nuts (10)
R (c) Install the screw (1), the washer (2) and the new nut (3)
R (d) Install the screw (7), the washer (8) and the new nut (9)
R (e) Install the screw (13), the washer (12) and the new nut (11)
R (f) Install the screw (26), the washer (25) and the new nut (24).
R (a) Install the bolt (14), the washer (16) and the new nut (17).
EFF :
001-012, 014-019, 53-19-41
Page 422
May 01/06
IAC
R 5. Close-up
________
R Subtask 53-19-41-410-053
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Close the FWD passenger/crew door 831 (Ref. TASK 52-10-00-410-001).
R Subtask 53-19-41-862-053
EFF :
001-012, 014-019, 53-19-41
Page 423
May 01/06
IAC
BLANKING PLATE - STATIC PORT - REMOVAL/INSTALLATION
___________________________________________________
TASK 53-19-42-000-001
WARNING : MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THE WEATHER RADAR ARE
_______
OPENED, SAFETIED AND TAGGED.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
101-199, 901-999, 53-19-42
Page 401
Feb 01/07
IAC
3. __________
Job Set-up
Subtask 53-19-42-865-050
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
122VU ANTI ICE/PROBES/PHC/3 2DA3 Y16
122VU ANTI ICE/PROBES/3/PITOT 3DA3 Z16
122VU ANTI ICE/PROBES/3/AOA 4DA3 Z15
122VU ANTI ICE/PROBES/3/STATIC 5DA3 Z14
Subtask 53-19-42-941-050
B. Get Access
4. Procedure
_________
Subtask 53-19-42-020-050
(1) Remove the sealant from the area between the static port
blanking-plate (3) and the fuselage structure with a nonmetallic
scraper.
R
EFF :
101-199, 901-999, 53-19-42
Page 402
Feb 01/07
IAC
Static Port Blanking-Plate
Figure 401/TASK 53-19-42-991-001
R
EFF :
101-199, 901-999, 53-19-42
Page 403
Feb 01/07
IAC
TASK 53-19-42-400-001
WARNING : MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THE WEATHER RADAR ARE
_______
OPENED, SAFETIED AND TAGGED.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
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101-199, 901-999, 53-19-42
Page 404
Feb 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-19-42-865-051
A. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
122VU ANTI ICE/PROBES/PHC/3 2DA3 Y16
122VU ANTI ICE/PROBES/3/PITOT 3DA3 Z16
122VU ANTI ICE/PROBES/3/AOA 4DA3 Z15
122VU ANTI ICE/PROBES/3/STATIC 5DA3 Z14
Subtask 53-19-42-860-050
(1) Make sure that the access platform is in position at the zone 122.
Subtask 53-19-42-020-051
R
EFF :
101-199, 901-999, 53-19-42
Page 405
Feb 01/07
IAC
Subtask 53-19-42-110-050
D. Cleaning
(Ref. Fig. 401/TASK 53-19-42-991-001)
WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO:
_______
- FLUSH IT AWAY WITH CLEAN WATER
- GET MEDICAL AID.
(1) Remove the remaining sealant from the mating surface of the fuselage
with a nonmetallic scraper.
(2) Clean the mating surface of the fuselage with CLEANING AGENTS
(Material No. 11-003) and MISCELLANEOUS (Material No. 19-003).
(3) Remove the remaining sealant from the screws (1) and (2) with a
nonmetallic scraper.
(4) Clean the screws (1) and (2) with CLEANING AGENTS (Material No. 11-
003) and MISCELLANEOUS (Material No. 19-003).
(5) Remove the remaining sealant from the component interface with a
nonmetallic scraper.
(6) Clean the component interface with CLEANING AGENTS (Material No. 11-
003) and MISCELLANEOUS (Material No. 19-003).
Subtask 53-19-42-220-051
(1) Put the static port blanking-plate (3) in position on the fuselage
structure.
R
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Page 406
Feb 01/07
IAC
(2) In zone D, make sure that the out-of-flush dimension A1 is 0.55 -0.25
+0.25 mm (0.0216 -0.0098 +0.0098 in.) between the fuselage structure
and the static port blanking-plate (3).
(3) In zone E, make sure that the out-of-flush dimension A1 is 0.55 -0.35
+0.35 mm (0.0216 -0.0137 +0.0137 in.) between the fuselage structure
and the static port blanking-plate (3).
(4) If necessary, remove the unwanted layers of the laminated shim (4) to
adjust the thickness of the static port blanking-plate (3).
(5) Remove the static port blanking-plate (3) from the fuselage
structure.
Subtask 53-19-42-390-051
F. Application of Sealants
(Ref. Fig. 402/TASK 53-19-42-991-003)
WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO:
_______
- FLUSH IT AWAY WITH CLEAN WATER
- GET MEDICAL AID.
CAUTION : MAKE SURE THAT NO SEALANT GOES INTO THE MIDDLE HOLES OF THE
_______
BLANKING PLATE. SEALANT IN THE HOLES CAN CAUSE DAMAGE TO THE
STATIC PROBE AND CAN CAUSE THE PROBE TO GIVE INCORRECT DATA.
(1) On the component interface, put masking tape on the middle holes.
R
EFF :
101-199, 901-999, 53-19-42
Page 407
Feb 01/07
IAC
Installation of the Static Port Blanking-Plate
Figure 402/TASK 53-19-42-991-003- 12 (SHEET 1)
R
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101-199, 901-999, 53-19-42
Page 408
Feb 01/07
IAC
Installation of the Static Port Blanking-Plate
Figure 402/TASK 53-19-42-991-003- 22 (SHEET 2)
R
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101-199, 901-999, 53-19-42
Page 409
Feb 01/07
IAC
(2) Apply SEALANTS (Material No. 09-019B) to the mating surface of the
static port blanking-plate (3).
(4) Apply SPECIAL MATERIALS (Material No. 05-013A) to the mating surface
of the static port blanking-plate (3).
(a) Fill the space between the laminated shim (4) and the bottom hole
of the static port blanking-plate (3) with SEALANTS (Material No.
09-016).
(b) Apply a bead of SEALANTS (Material No. 09-016) on the inner side
of the middle hole of the laminated shim (4).
(6) Apply SEALANTS (Material No. 09-016) below the heads of the screws
(1) and (2).
(8) Apply SPECIAL MATERIALS (Material No. 05-013A) below the heads of the
screws (1) and (2).
4. Procedure
_________
Subtask 53-19-42-420-050
(1) Put the static port blanking-plate (3) in position on the fuselage
structure.
(2) Install the screws (1) and (2) and tighten them.
EFF :
101-199, 901-999, 53-19-42
Page 410
May 01/08
IAC
Subtask 53-19-42-220-050
(1) In zone D, make sure that the out-of-flush dimension A1 is 0.55 -0.25
+0.25 mm (0.0216 -0.0098 +0.0098 in.) between the fuselage structure
and the static port blanking-plate (3).
(2) In zone E, make sure that the out-of-flush dimension A1 is 0.55 -0.35
+0.35 mm (0.0216 -0.0137 +0.0137 in.) between the fuselage structure
and the static port blanking-plate (3).
(3) Make sure that the peripheral clearance J1 between the fuselage
structure and the static port blanking-plate (3) is 3.1 -1 +1 mm
(0.1220 -0.0393 +0.0393 in.).
(4) The permitted mismatch for the head of the 8 pins of the
blanking-plate is -0.05 mm (-0.0019 in.) to -0.35 mm (-0.0137 in.).
R Subtask 53-19-42-390-050
R (1) Fill the remaining space between the static port blanking-plate (3)
R and the fuselage structure with SEALANTS (Material No. 09-016).
R (2) Make the contour of the sealant around the static port blanking-plate
R (3) smooth.
5. Close-up
________
Subtask 53-19-42-420-051
CAUTION : MAKE SURE THAT NO SEALANT GOES INTO THE MIDDLE HOLES OF THE
_______
BLANKING PLATE. SEALANT IN THE HOLES CAN CAUSE DAMAGE TO THE
STATIC PROBE AND CAN CAUSE THE PROBE TO GIVE INCORRECT DATA.
(1) With a non metallic pin 2.5 mm (0.0984 in.) dia., remove the masking
tape through the middle holes of the static port blanking-plate (3).
EFF :
101-199, 901-999, 53-19-42
Page 411
May 01/08
IAC
Subtask 53-19-42-865-052
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
2DA3, 3DA3, 4DA3, 5DA3.
Subtask 53-19-42-942-050
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
101-199, 901-999, 53-19-42
Page 412
May 01/08
R
IAC
FORWARD FUSELAGE - DESCRIPTION AND OPERATION
____________________________________________
1. General
_______
A. Location
The section 13/14 is the intermediate part of the forward fuselage. It
lies between the FR24 and FR35. The upper part contains the front section
of the cabin. The lower part contains the forward cargo compartment. The
opening for the cargo door is on the right side of the aircraft between
FR24A and FR28.
R A. Location
R The section 13/14 is the intermediate part of the forward fuselage. It
R lies between the FR24 and FR35. The upper part contains the front section
R of the cabin. The lower part contains the forward cargo compartment. The
R opening for the cargo door is on the right side of the aircraft between
R FR24A and FR28.
R The section 14A is the intermediate part of the forward fuselage. It lies
R between the FR35 and FR35.8. The top part contains the front section of
R the cabin. The bottom part contains the forward cargo compartment. The
R opening for the emergency exit door is on each side of the aircraft
R between FR35.1 and FR35.2A.
EFF :
ALL 53-20-00
Page 1
Feb 01/07
IAC
Forward Fuselage - Section 13/14
Figure 001
R
EFF :
001-012, 014-099, 53-20-00
Page 2
May 01/06
IAC
R Forward Fuselage - Section 13/14
R Figure 001A
EFF :
101-199, 53-20-00
Page 3
Feb 01/07
IAC
Forward Fuselage - Section 13/14
R Figure 001B
R
EFF :
901-999, 53-20-00
Page 4
Feb 01/07
IAC
R Forward fuselage - Section 14A
R Figure 002
R
EFF :
101-199, 53-20-00
Page 5
Feb 01/07
IAC
**ON A/C ALL
2. Description
___________
A. Frames
(1) Frame 24
Frame 24 provides the splice between sections 13/14 and 11/12 (Ref.
53-10-00). The core of the frame consists of curved members formed
from L-section sheet metal joined by splices. The skin of the two
sections is secured by a T-section edging by lockbolts to the frame
core and a splice.
(4) Frames 29 to 34
These closed frames consist of curved members formed from Z-section
sheet metal connected by splices.
EFF :
ALL 53-20-00
Page 6
May 01/07
IAC
Fuselage Section
Figure 003
R
EFF :
001-012, 014-019, 901-901, 53-20-00
Page 7/8
May 01/07
IAC
Fuselage Section
Figure 003A
R
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020-099, 101-199, 902-999, 53-20-00
Page 9/10
May 01/07
IAC
**ON A/C 101-199,
(5) Frame 35
Frame 35 provides the splice between sections 13/14 and 14A. The core
of the frame consists of curved members formed from L-section sheet
metal joined by splices. The skin of the two sections is secured by a
T-section edging by lockbolts to the frame core and a splice.
B. Stringers
(Ref. Fig. 003)
The fuselage stringers consist of folded aluminium alloy Z-section sheet.
They are arranged longitudinally and, together with the frames, they
stiffen the fuselage ; the skin is attached to them.
Between the frame 31 and 35, the left stringer 41 side to the right
stringer 41 side are reinforced.
At the frame 24, the rivets are replace by lockbolts in titanium.
B. Stringers
(Ref. Fig. 003A)
The fuselage stringers consist of folded aluminium alloy Z-section sheet
metal. They are arranged longitudinally and, together with the frames,
they stiffen the fuselage ; the skin is attached to them. At the stringer
18,added lockbolts in place of rivets
EFF :
ALL 53-20-00
Page 11
May 01/07
IAC
**ON A/C 001-012, 014-099, 901-999,
C. Skin
The outer skin comprises three upper panels extending from FR24 to FR35
and fire lower panels. The two upper lateral panels include the openings
for the cabin windows. The forward right lower panel includes the opening
for the cargo door. The forward wing to fuselage fairings are attached to
the lower section of the skin (Ref. 53-25-11).
The skin panels are aluminium alloy sheets lightened by cut-outs formed
by chemical milling. Skin joints are formed by overlapping the edges of
the upper panel on the lower panels on stringers 6, 18, 32 and 41. They
are reinforced by crack-stop plates on frame intersections. The skin is
secured to the frame via frame doublers and to the stringers.
C. Skin
(Ref. Fig. 001A, 002, 003A)
The outer skin comprises three upper panels extending from FR24 to FR35.8
and fire lower panels. The two upper lateral panels include the openings
for the cabin windows. The forward right lower panel includes the opening
R
EFF :
ALL 53-20-00
Page 12
May 01/07
IAC
for the cargo door. The forward wing to fuselage fairings are attached to
the lower section of the skin (Ref. 53-25-11).
The skin panels are aluminium alloy sheets lightened by cut-outs formed
by chemical milling. Skin joints are formed by overlapping the edges of
the upper panel on the lower panels on stringers 6, 18, 32 and 41. They
are reinforced by crack-stop plates on frame intersections. The skin is
secured to the frame via frame doublers and to the stringers.
EFF :
ALL 53-20-00
Page 13
May 01/07
IAC
Cabin Floor Structure - Section 13/14
R Figure 004
R
EFF :
001-012, 014-099, 53-20-00
Page 14
Feb 01/07
IAC
INTENTIONALLY BLANK
R
53-20-00
Page 15
Feb 01/07
IAC
R Cabin Floor Structure - Section 13/14 and Section 14A
R Figure 004A (SHEET 1)
EFF :
101-199, 53-20-00
Page 16
Feb 01/07
IAC
R Cabin Floor Structure - Section 13/14 and Section 14A
R Figure 004A (SHEET 2)
EFF :
101-199, 53-20-00
Page 17
Feb 01/07
IAC
Cabin Floor Structure - Section 13/14
R Figure 004B
EFF :
901-999, 53-20-00
Page 18
Feb 01/07
IAC
(1) Cross Beams
The cross beams consist of aluminium alloy extruded sections riveted
to the frames in the zones of stringers 23 and 24. They reinforce the
frames and increase fuselage stability. The cross beams are supported
by two struts on either side of the fuselage. These struts are
riveted to the lower part of the frame level with stringers 32.
EFF :
ALL 53-20-00
Page 19
May 01/07
IAC
**ON A/C ALL
F. Cabin Windows
The drop-forged frames in which the cabin windows are installed, are
riveted on both sides of the fuselage between stringers 14 and 18.
There are no stringers at window level.
EFF :
ALL 53-20-00
Page 20
May 01/07
R
IAC
**ON A/C 101-199,
The sides of the cargo door opening are formed by frames 24A and 28.
Frame 24A is riveted to frame 24 on attach-fittings.
The top and bottom zones of the door are formed by stringers 23 and 29.
The top of the door opening is reinforced by the lower sections of frames
25, 26 and 27 which are attached to the cross beams of the cabin floor by
the door edging plates.
The bottom of the door opening is reinforced by a door threshold box, on
to which the door latch fittings are secured.
EFF :
ALL 53-20-00
Page 21
Feb 01/07
IAC
MAIN STRUCTURE - INSPECTION/CHECK
_________________________________
R TASK 53-21-00-200-018
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
ALL 53-21-00
Page 601
Feb 01/07
IAC
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R 3. __________
Job Set-up
R Subtask 53-21-00-010-059
R A. Get Access
R (2) Open the forward emergency exit door 833 (843) (Ref. TASK 52-22-00-
R 010-001).
R (3) Remove the door frame linings (Ref. TASK 25-23-47-000-004) (Ref. TASK
R 25-23-47-000-009).
R (4) Remove the sidewall panels: 231AX, 232AX, 231PX, 232PX, 231BX, 232BX,
R 231QX, 232QX (Ref. TASK 25-23-43-000-001).
R
EFF :
101-199, 53-21-00
Page 602
Feb 01/07
IAC
R (5) Remove the cove light panels: 231CX, 231FX, 231RX, 232CX, 232FX,
R 232RX (Ref. TASK 25-23-48-000-001).
R (7) Remove the overhead stowage compartments, if installed (Ref. TASK 25-
R 24-41-000-001).
R Subtask 53-21-00-110-050
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
R 4. Procedure
_________
R Subtask 53-21-00-220-050
R A. Inspection
R (Ref. Fig. 601/TASK 53-21-00-991-020)
R
EFF :
101-199, 53-21-00
Page 603
Feb 01/07
IAC
R Forward Emergency Exit Cutouts - Internal Structure
R Figure 601/TASK 53-21-00-991-020- 12 (SHEET 1)
R
EFF :
101-199, 53-21-00
Page 604
Feb 01/07
IAC
R Forward Emergency Exit Cutouts - Internal Structure
R Figure 601/TASK 53-21-00-991-020- 22 (SHEET 2)
R
EFF :
101-199, 53-21-00
Page 605
Feb 01/07
IAC
R (2) Make sure that there is no:
R Subtask 53-21-00-916-050
R (1) Put masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
R (Material No. 08-074) on the equipment and fittings adjacent to the
R area.
R 5. Close-up
________
R Subtask 53-21-00-410-058
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R
EFF :
101-199, 53-21-00
Page 606
Feb 01/07
IAC
R (4) Install the ceiling panels (Ref. TASK 25-23-41-400-001).
R (5) Install the cove light panels 231CX, 231FX, 231RX, 232CX, 232FX,
R 232RX (Ref. TASK 25-23-48-400-001).
R (6) Install the sidewall panels 231AX, 232AX, 231PX, 232PX, 231BX, 232BX,
R 231QX, 232QX (Ref. TASK 25-23-43-400-001).
R (8) Close the forward emergency exit door 833 (843) (Ref. TASK 52-22-00-
R 410-001).
R
EFF :
101-199, 53-21-00
Page 607
Feb 01/07
IAC
R TASK 53-21-00-200-019
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R
EFF :
101-199, 53-21-00
Page 608
Feb 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R 3. __________
Job Set-up
R Subtask 53-21-00-010-060
R A. Get Access
R (2) Open the forward emergency exit door 833 (843), (Ref. TASK 52-22-00-
R 010-001).
R (3) Remove the door frame linings (Ref. TASK 25-23-47-000-004) (Ref. TASK
R 25-23-47-000-009).
R Subtask 53-21-00-110-051
R (1) Clean the inspection area with a CLEANING AGENTS (Material No. 11-
R 004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-
R 003), if necessary.
EFF :
101-199, 53-21-00
Page 609
Feb 01/07
IAC
R 4. Procedure
_________
R Subtask 53-21-00-220-051
R A. Inspection
R (Ref. Fig. 602/TASK 53-21-00-991-021)
R 5. Close-up
________
R Subtask 53-21-00-410-059
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (3) Close the forward emergency exit 833 (843), (Ref. TASK 52-22-00-410-
R 001).
R
EFF :
101-199, 53-21-00
Page 610
Feb 01/07
IAC
R Door Stop Fitting, FR35.1 and FR35.2A, Left and Right Sides
R Figure 602/TASK 53-21-00-991-021
R
EFF :
101-199, 53-21-00
Page 611
Feb 01/07
IAC
R TASK 53-21-00-200-020
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R
EFF :
101-199, 53-21-00
Page 612
Feb 01/07
IAC
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R 3. __________
Job Set-up
R Subtask 53-21-00-010-061
R A. Get Access
R (2) Open the forward cargo compartment door 825 (Ref. TASK 52-30-00-860-
R 003).
R Subtask 53-21-00-110-052
R
EFF :
101-199, 53-21-00
Page 613
Feb 01/07
IAC
R (1) Clean the inspection area with a CLEANING AGENTS (Material No. 11-
R 004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-
R 003), if necessary.
R 4. Procedure
_________
R Subtask 53-21-00-220-052
R A. Inspection
R (Ref. Fig. 603/TASK 53-21-00-991-022)
R Subtask 53-21-00-916-059
R (1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
R (Material No. 08-074) on the equipment and fittings adjacent to the
R area.
R
EFF :
101-199, 53-21-00
Page 614
Feb 01/07
IAC
R Escape-Slide Stowage Compartment
R Figure 603/TASK 53-21-00-991-022
R
EFF :
101-199, 53-21-00
Page 615
Feb 01/07
IAC
R (3) Remove the masking paper or masking tape.
R 5. Close-up
________
R Subtask 53-21-00-410-060
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (3) Close the forward cargo compartment door 825 (Ref. TASK 52-30-00-860-
R 004).
R
EFF :
101-199, 53-21-00
Page 616
Feb 01/07
IAC
R TASK 53-21-00-200-021
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R
EFF :
101-199, 53-21-00
Page 617
Feb 01/07
IAC
R 3. __________
Job Set-up
R Subtask 53-21-00-010-062
R A. Get Access
R (2) Open the forward emergency exit door 833 (843) (Ref. TASK 52-22-00-
R 010-002).
R (3) Remove the scuff-plate below the forward emergency exit (Ref. TASK
R 53-25-41-000-001) (left and right sides).
R Subtask 53-21-00-110-053
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
R 4. Procedure
_________
R Subtask 53-21-00-220-053
R A. Inspection
R (Ref. Fig. 604/TASK 53-21-00-991-023)
R
EFF :
101-199, 53-21-00
Page 618
Feb 01/07
IAC
R Scuff plates of the FWD Emergency Exit
R Figure 604/TASK 53-21-00-991-023
R
EFF :
101-199, 53-21-00
Page 619
Feb 01/07
IAC
R (2) Make sure that there is no:
R 5. Close-up
________
R Subtask 53-21-00-410-061
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Install the scuff-plates under the forward emergency exit (Ref. TASK
R 53-25-41-400-001) (left and right sides).
R (3) Close the forward emergency exit 833 (843) (Ref. TASK 52-22-00-410-
R 002).
R
EFF :
101-199, 53-21-00
Page 620
Feb 01/07
IAC
R **ON A/C 001-012, 014-099, 101-199,
TASK 53-21-00-200-001
Detailed Inspection of Frame Webs at Stringer 18 LH/RH for: FR25, 26, 27, 28,
32, 33, 34
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
001-012, 014-099, 101-199, 53-21-00
Page 621
Feb 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-21-00-010-050
A. Get Access
(2) Open the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
010-001).
R
EFF :
001-012, 014-099, 101-199, 53-21-00
Page 622
Feb 01/07
IAC
(3) Remove the linings and the insulation panels between FR21 and FR36 in
the zone 231 (232) at the STGR18: 231DW, 231EW, 231FW, 231GW, 231HW,
231JW, 231KW, 231LW, 231MW, 231NW, 231PW, 231QW, 231RW, 231SW, 231TW,
231UW, 231VW, 231WW, 231XW, 231YW, 232DW, 232EW, 232FW, 232GW, 232HW,
232JW, 232KW, 232LW, 232MW, 232NW, 232PW, 232QW, 232RW, 232SW, 232TW,
232UW, 232VW, 232WW, 232XW, 232YW, (Ref. TASK 25-23-43-000-001),
(Ref. TASK 25-23-44-000-001), (Ref. TASK 25-23-48-000-001).
R Subtask 53-21-00-010-050-A
R A. Get Access
R (2) Open the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
R 010-001).
R (3) Remove the linings and the insulation panels between FR21 and FR35.1
R in the zone 231 (232) at the STGR18: 231DW, 231EW, 231FW, 231GW,
R 231HW, 231JW, 231KW, 231LW, 231MW, 231NW, 231PW, 231QW, 231RW, 231SW,
R 231TW, 231UW, 231VW, 231WW, 231AX, 231BX, 232DW, 232EW, 232FW, 232GW,
R 232HW, 232JW, 232KW, 232LW, 232MW, 232NW, 232PW, 232QW, 232RW, 232SW,
R 232TW, 232UW, 232VW, 232WW, 232AX, 232BX, (Ref. TASK 25-23-43-000-
R 001), (Ref. TASK 25-23-44-000-001), (Ref. TASK 25-23-48-000-001).
Subtask 53-21-00-110-054
R
EFF :
001-012, 014-099, 101-199, 53-21-00
Page 623
Feb 01/07
IAC
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE
_______
MATERIAL/S.
USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-21-00-220-056
A. Inspection
(1) Do a detailed inspection of the frame webs at the STGR18 for: FR25,
FR26, FR27, FR28, FR32, FR33, FR34, left and right sides.
R
EFF :
001-012, 014-099, 101-199, 53-21-00
Page 624
Feb 01/07
IAC
Frame Webs at FR25, FR26, FR27, FR28, FR32, FR33, FR34 at STGR18, Left and
Right Sides
R Figure 605/TASK 53-21-00-991-001
R EFF :
001-012, 014-099,
53-21-00 Page 625
Feb 01/07
IAC
R Frame Webs at FR25, FR26, FR27, FR28, FR32, FR33, FR34 at STGR18, Left and
R Right sides
R Figure 605A/TASK 53-21-00-991-001-B
R EFF :
101-199,
53-21-00 Page 626
Feb 01/07
IAC
5. Close-up
________
Subtask 53-21-00-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the linings and the insulation panels between FR21 and FR36
in the zone 231 (232) at the STGR18: 231DW, 231EW, 231FW, 231GW,
231HW, 231JW, 231KW, 231LW, 231MW, 231NW, 231PW, 231QW, 231RW, 231SW,
231TW, 231UW, 231VW, 231WW, 231XW, 231YW, 232DW, 232EW, 232FW, 232GW,
232HW, 232JW, 232KW, 232LW, 232MW, 232NW, 232PW, 232QW, 232RW, 232SW,
232TW, 232UW, 232VW, 232WW, 232XW, 232YW, (Ref. TASK 25-23-43-400-
001), (Ref. TASK 25-23-44-400-001), (Ref. TASK 25-23-48-400-001).
(3) Close the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
410-001).
R Subtask 53-21-00-410-050-A
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Install the linings and the insulation panels between FR21 and FR35.1
R in the zone 231 (232) at the STGR18: 231DW, 231EW, 231FW, 231GW,
R 231HW, 231JW, 231KW, 231LW, 231MW, 231NW, 231PW, 231QW, 231RW, 231SW,
R 231TW, 231UW, 231VW, 231WW, 231AX, 231BX, 232DW, 232EW, 232FW, 232GW,
R 232HW, 232JW, 232KW, 232LW, 232MW, 232NW, 232PW, 232QW, 232RW, 232SW,
R 232TW, 232UW, 232VW, 232WW, 232AX, 232BX, (Ref. TASK 25-23-43-400-
R 001), (Ref. TASK 25-23-44-400-001), (Ref. TASK 25-23-48-400-001).
R (3) Close the forward passenger/crew door 831 (841), (Ref. TASK 52-10-00-
R 410-001).
R
EFF :
001-012, 014-099, 101-199, 53-21-00
Page 627
Feb 01/07
IAC
**ON A/C ALL
TASK 53-21-00-200-002
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-21-00
Page 628
Feb 01/07
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-21-00-010-051
A. Get Access
(2) Open the forward cargo compartment door 825 (Ref. TASK 52-30-00-860-
003).
(3) Remove the partition panels 132BW, 132EW (Ref. TASK 25-54-11-000-
001).
EFF :
ALL 53-21-00
Page 629
Feb 01/07
IAC
Subtask 53-21-00-110-055
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-21-00-220-057
A. Inspection
R (Ref. Fig. 606/TASK 53-21-00-991-002)
EFF :
ALL 53-21-00
Page 630
Feb 01/07
IAC
Junction with the Cabin Floor Beam at STGR23, Right Internal Side
Figure 606/TASK 53-21-00-991-002
R
EFF :
ALL 53-21-00
Page 631
Nov 01/07
IAC
INTENTIONALLY BLANK
R
53-21-00
Page 632
Nov 01/07
IAC
5. Close-up
________
Subtask 53-21-00-410-051
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Install the partition panels 132BW, 132EW (Ref. TASK 25-54-11-400-
001).
(5) Close the forward cargo compartment door 825 (Ref. TASK 52-30-00-860-
004).
EFF :
ALL 53-21-00
Page 633
Feb 01/07
R
IAC
TASK 53-21-00-200-027
Detailed Inspection of Fuselage Forward Cargo Door Hinge Fitting and External
Attachment Area
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-21-00
Page 634
Feb 01/07
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-21-00-941-086
Subtask 53-21-00-110-101
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
EFF :
ALL 53-21-00
Page 635
Feb 01/07
IAC
4. Procedure
_________
Subtask 53-21-00-220-082
A. Inspection
R (Ref. Fig. 607/TASK 53-21-00-991-003)
Subtask 53-21-00-010-094
B. Get Access
(1) Open the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
001)
Subtask 53-21-00-110-102
EFF :
ALL 53-21-00
Page 636
Feb 01/07
IAC
Hinge-Fitting of the Forward Cargo-Compartment Door, Fuselage and External
Attachment Area
R Figure 607/TASK 53-21-00-991-003
EFF :
ALL
53-21-00 Page 637
Feb 01/07
IAC
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE
_______
MATERIAL/S.
USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
Subtask 53-21-00-220-083
D. Inspection
R (Ref. Fig. 607/TASK 53-21-00-991-003)
Subtask 53-21-00-916-068
(1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fittings adjacent to the
area.
EFF :
ALL 53-21-00
Page 638
Feb 01/07
IAC
(2) Apply a layer of STORAGE PRESERVATION (Material No. 15-005) or
STORAGE PRESERVATION (Material No. 15-006) to the inspection area.
5. Close-up
________
Subtask 53-21-00-410-088
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
004)
EFF :
ALL 53-21-00
Page 639
Feb 01/07
R
IAC
TASK 53-21-00-200-004
Detailed Inspection of Forward Cargo Door Cutout Panels, Upper and Lower
Corners, External Surface
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-21-00
Page 640
Feb 01/07
IAC
3. __________
Job Set-up
Subtask 53-21-00-010-067
Subtask 53-21-00-110-057
(1) Clean the inspection surface with CLEANING AGENTS (Material No. 11-
004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-
003), if necessary.
NOTE : You must remove and replace the sealant if it has cracks or
____
damage, or if its edges are not attached to the structure.
4. Procedure
_________
Subtask 53-21-00-220-060
A. Inspection
R (Ref. Fig. 608/TASK 53-21-00-991-004)
EFF :
ALL 53-21-00
Page 641
Feb 01/07
IAC
Forward Cargo-Compartment Door - Cutout Panels - Upper and Lower Corners
R Figure 608/TASK 53-21-00-991-004
EFF :
ALL 53-21-00
Page 642
Feb 01/07
IAC
(2) Make sure that there is no :
Subtask 53-21-00-010-064
B. Get Access
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
DURING CARGO COMPARTMENT DOOR OPERATION.
(1) Open the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
001).
Subtask 53-21-00-110-058
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
EFF :
ALL 53-21-00
Page 643
Feb 01/07
R
IAC
Subtask 53-21-00-220-061
D. Inspection
R (Ref. Fig. 608/TASK 53-21-00-991-004)
5. Close-up
________
Subtask 53-21-00-410-063
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
002).
EFF :
ALL 53-21-00
Page 644
Feb 01/07
IAC
TASK 53-21-00-200-005
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-21-00
Page 645
Feb 01/07
IAC
3. __________
Job Set-up
Subtask 53-21-00-941-054
A. Get Access
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
DURING CARGO COMPARTMENT DOOR OPERATION.
(2) Open the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
001).
Subtask 53-21-00-020-050
Subtask 53-21-00-110-071
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-21-00-220-062
A. Inspection
R (Ref. Fig. 609/TASK 53-21-00-991-005)
EFF :
ALL 53-21-00
Page 646
Feb 01/07
IAC
Eccentric Bolts on the Locking Mechanism Fittings of the Forward Cargo
Compartment Door
R Figure 609/TASK 53-21-00-991-005
EFF :
ALL
53-21-00 Page 647
Feb 01/07
IAC
(2) Make sure that there is no :
5. Close-up
________
Subtask 53-21-00-420-050
Subtask 53-21-00-942-056
B. Close Access
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
DURING CARGO COMPARTMENT DOOR OPERATION.
(1) Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
002).
EFF :
ALL 53-21-00
Page 648
Feb 01/07
R
IAC
TASK 53-21-00-200-006
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-21-00
Page 649
Feb 01/07
IAC
3. __________
Job Set-up
Subtask 53-21-00-941-055
A. Get Access
Subtask 53-21-00-010-052
(1) Remove the ceiling panels 231BC, 231CC (Ref. TASK 25-23-41-000-001).
Subtask 53-21-00-110-069
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) if
necessary.
4. Procedure
_________
Subtask 53-21-00-220-063
A. Inspection
R (Ref. Fig. 610/TASK 53-21-00-991-006)
EFF :
ALL 53-21-00
Page 650
Feb 01/07
IAC
Circumferential Joint at FR24
R Figure 610/TASK 53-21-00-991-006
EFF :
ALL 53-21-00
Page 651
Feb 01/07
IAC
(2) Make sure that there is no :
5. Close-up
________
Subtask 53-21-00-410-052
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the ceiling panels 231BC, 231CC (Ref. TASK 25-23-41-400-001).
Subtask 53-21-00-942-058
B. Close Access
EFF :
ALL 53-21-00
Page 652
Feb 01/07
R
IAC
TASK 53-21-00-200-024
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-21-00
Page 653
Feb 01/07
IAC
3. __________
Job Set-up
Subtask 53-21-00-941-070
A. Get Access
Subtask 53-21-00-110-070
(1) Remove the top layer paint from the inspection area (Ref. TASK 51-75-
12-300-001), (Ref. SRM 517500,P.Block-001), (Ref. SRM 512300,P.Block-
001).
(2) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
(3) Make sure that the surface of the inspection area is clean and
smooth.
EFF :
ALL 53-21-00
Page 654
Feb 01/07
IAC
Circumferential Joint at FR35
R Figure 611/TASK 53-21-00-991-042
EFF :
ALL 53-21-00
Page 655
Feb 01/07
IAC
(5) Make sure that there is no:
4. Procedure
_________
Subtask 53-21-00-250-050
A. Inspection
R (Ref. Fig. 611/TASK 53-21-00-991-042)
5. Close-up
________
Subtask 53-21-00-370-050
A. Application of Paint
(1) Apply the top layer paint on the inspection area (Ref. TASK 51-75-12-
300-001), (Ref. SRM 517500,P.Block-001), (Ref. SRM 512300,P.Block-
001).
EFF :
ALL 53-21-00
Page 656
Feb 01/07
IAC
Subtask 53-21-00-942-075
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-21-00
Page 657
Feb 01/07
R
IAC
TASK 53-21-00-210-007
General Visual Inspection of Fuselage External Surface around Water Drain Panel
Cutout, between FR 25 and FR 29 at Stringer 43 LH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-21-00
Page 658
Feb 01/07
IAC
3. __________
Job Set-up
Subtask 53-21-00-941-082
A. Get Access
Subtask 53-21-00-110-097
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-21-00-210-081
A. Inspection
R (Ref. Fig. 612/TASK 53-21-00-991-053)
EFF :
ALL 53-21-00
Page 659
Feb 01/07
IAC
Fuselage External Surface around the Water-Drain Panel Cutout between FR25 and
FR29 at STGR43, Left Side
R Figure 612/TASK 53-21-00-991-053
EFF :
ALL
53-21-00 Page 660
Feb 01/07
IAC
(b) Other damage (cracks, scratches, stress, marks, dents,
bumps,...):
If you find other damage, refer to the Structural Repair Manual
(Ref. SRM 511100 P.Block 001) for damage classification and
corrective action.
5. Close-up
________
Subtask 53-21-00-942-088
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-21-00
Page 661
Feb 01/07
R
IAC
TASK 53-21-00-210-008
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-21-00
Page 662
Feb 01/07
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-21-00-941-083
A. Get Access
(2) Open the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
001).
Subtask 53-21-00-010-089
Subtask 53-21-00-010-089-A
EFF :
ALL 53-21-00
Page 663
Feb 01/07
IAC
**ON A/C ALL
Subtask 53-21-00-110-098
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-21-00-210-082
A. Inspection
R (Ref. Fig. 613/TASK 53-21-00-991-052)
EFF :
ALL 53-21-00
Page 664
Feb 01/07
IAC
Forward Cargo Door Actuator - Attach Brackets
R Figure 613/TASK 53-21-00-991-052
EFF :
ALL 53-21-00
Page 665
Feb 01/07
IAC
5. Close-up
________
Subtask 53-21-00-410-085
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 53-21-00-410-085-A
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 53-21-00-942-089
B. Close Access
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
DURING CARGO COMPARTMENT DOOR OPERATION.
(1) Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
002).
EFF :
ALL 53-21-00
Page 666
Feb 01/07
IAC
TASK 53-21-00-200-008
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-21-00
Page 667
Feb 01/07
IAC
3. __________
Job Set-up
Subtask 53-21-00-941-057
A. Get Access
(1) Put an access platform in position at the zone 231 (232) in front of
the cabin windows.
Subtask 53-21-00-110-065
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-21-00-220-064
A. Inspection
R (Ref. Fig. 614/TASK 53-21-00-991-008)
EFF :
ALL 53-21-00
Page 668
Feb 01/07
IAC
Cabin Window Frame, External Surface
R Figure 614/TASK 53-21-00-991-008
EFF :
ALL 53-21-00
Page 669
Feb 01/07
IAC
(b) Other damage (cracks, scratches, stress, marks, dents,
bumps,...):
- If you find this type of damage, refer to the Structural Repair
Manual (Ref. SRM 511100 P.Block 001) for damage classification
and corrective action.
5. Close-up
________
Subtask 53-21-00-942-061
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-21-00
Page 670
Feb 01/07
R
IAC
TASK 53-21-00-200-023
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-21-00
Page 671
Feb 01/07
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-21-00-010-066
A. Get Access
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
DURING CARGO COMPARTMENT DOOR OPERATION.
(2) Open the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
001).
(3) Remove the lining at the zone 137 (138): 131PW, 132PW (Ref. TASK 25-
54-12-000-001).
Subtask 53-21-00-110-066
EFF :
ALL 53-21-00
Page 672
Feb 01/07
IAC
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-21-00-220-055
A. Inspection
R (Ref. Fig. 615/TASK 53-21-00-991-025)
5. Close-up
________
Subtask 53-21-00-410-065
A. Close Access
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
DURING CARGO COMPARTMENT DOOR OPERATION.
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the lining panels 131PW, 132PW (Ref. TASK 25-54-12-400-001).
(4) Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
002).
EFF :
ALL 53-21-00
Page 673
Feb 01/07
IAC
Fuselage Skin at FR35, and at the STGR30 Level, Left and Right Sides
R Figure 615/TASK 53-21-00-991-025
EFF :
ALL 53-21-00
Page 674
Feb 01/07
IAC
(5) Remove the access platform(s).
EFF :
ALL 53-21-00
Page 675
Feb 01/07
R
IAC
TASK 53-21-00-200-009
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-21-00
Page 676
Feb 01/07
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-21-00-941-058
A. Get Access
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
DURING CARGO COMPARTMENT DOOR OPERATION.
(2) Open the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
001).
Subtask 53-21-00-010-053
(1) Remove the lower sidewall panels 132KW, 132MW, 132LW, 131HW, 131MW.
(2) Remove the cargo-compartment floor panels 131EF, 131HF (Ref. TASK 53-
22-14-000-001).
EFF :
ALL 53-21-00
Page 677
Feb 01/07
IAC
R **ON A/C 101-199,
R Subtask 53-21-00-010-053-B
R (1) Remove the lower sidewall panels 132KW, 132MW, 132QW, 132LW, 131HW,
R 131MW, 131QW
R (2) Remove the cargo-compartment floor panels 131EF, 131HF (Ref. TASK 53-
R 22-14-000-001).
Subtask 53-21-00-010-053-A
(1) Remove the lower sidewall panels 132KW, 132SW, 132LW, 131HW, 131SW.
(2) Remove the cargo-compartment floor panels 131CG, 131DG, 131EG, 132DG,
132EG (Ref. TASK 53-22-14-000-001).
Subtask 53-21-00-110-063
EFF :
ALL 53-21-00
Page 678
Feb 01/07
IAC
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-21-00-220-065
A. Inspection
R (Ref. Fig. 616/TASK 53-21-00-991-009)
5. Close-up
________
Subtask 53-21-00-410-053
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the cargo-compartment floor panels 131EF, 131HF (Ref. TASK
53-22-14-400-001).
(4) Install the insulation blankets and the sidewall panels 132KW, 132MW,
132LW, 131HW, 131MW.
EFF :
ALL 53-21-00
Page 679
Feb 01/07
IAC
Cabin-Floor Cross Beams
R Figure 616/TASK 53-21-00-991-009
EFF :
ALL 53-21-00
Page 680
Feb 01/07
IAC
R **ON A/C 101-199,
R Subtask 53-21-00-410-053-B
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (3) Install the cargo-compartment floor panels 131EF, 131HF (Ref. TASK
R 53-22-14-400-001).
R (4) Install the insulation blankets and the sidewall panels 132KW, 132MW,
R 132QW, 132LW, 131HW, 131MW, 131QW.
Subtask 53-21-00-410-053-A
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the cargo floor panels 131CG, 131DG, 131EG, 132DG, 132EG
(Ref. TASK 53-22-14-400-001).
(4) Install the insulation blankets and the sidewall panels 132KW, 132SW,
132LW, 131HW, 131SW.
R
EFF :
101-199, 901-999, 53-21-00
Page 681
Feb 01/07
IAC
**ON A/C ALL
Subtask 53-21-00-942-063
B. Close Access
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
DURING CARGO COMPARTMENT DOOR OPERATION.
(1) Close the forward cargo compartment door 825 (Ref. TASK 52-30-00-860-
002)
EFF :
ALL 53-21-00
Page 682
Feb 01/07
R
IAC
R **ON A/C 101-199,
R TASK 53-21-00-200-022
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R
EFF :
101-199, 53-21-00
Page 683
Feb 01/07
IAC
R 3. __________
Job Set-up
R Subtask 53-21-00-010-065
R A. Get Access
R (2) Open the forward emergency exit 833 (Ref. TASK 52-22-00-010-002).
R Subtask 53-21-00-110-062
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
R 4. Procedure
_________
R Subtask 53-21-00-220-054
R A. Inspection
R (Ref. Fig. 617/TASK 53-21-00-991-024)
R
EFF :
101-199, 53-21-00
Page 684
Feb 01/07
IAC
R Forward Emergency Exit, Upper Corners - External Surface, Left Side
R Figure 617/TASK 53-21-00-991-024
R
EFF :
101-199, 53-21-00
Page 685
Feb 01/07
IAC
R (2) Make sure that there is no:
R 5. Close-up
________
R Subtask 53-21-00-410-064
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Close the forward emergency exit 833 (Ref. TASK 52-22-00-410-002).
R
EFF :
101-199, 53-21-00
Page 686
Feb 01/07
IAC
R **ON A/C ALL
TASK 53-21-00-200-011
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-21-00
Page 687
Feb 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-21-00-010-070
A. Get Access
(2) Open the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
001).
Subtask 53-21-00-010-054
(2) Remove the floor panels 132GF, 132FF (Ref. TASK 53-22-14-000-001).
EFF :
ALL 53-21-00
Page 688
Feb 01/07
IAC
(3) Remove the sidewall panel 132KW (Ref. TASK 25-54-12-000-003).
(5) Remove the insulation blankets at the location of the removed panels
(Ref. TASK 25-80-00-000-001).
Subtask 53-21-00-010-054-A
(1) Remove the ceiling panels 131MC, 131PC (Ref. TASK 25-54-12-000-002).
(2) Remove the floor panels 132GF, 132FF (Ref. TASK 53-22-14-000-001).
(5) Remove the insulation blankets at the location of the removed panels
(Ref. TASK 25-80-00-000-001).
Subtask 53-21-00-110-067
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
EFF :
ALL 53-21-00
Page 689
Feb 01/07
IAC
4. Procedure
_________
Subtask 53-21-00-220-066
A. Inspection
Subtask 53-21-00-916-051
(1) Apply masking tape or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fittings adjacent to the
area.
EFF :
ALL 53-21-00
Page 690
Feb 01/07
R
IAC
5. Close-up
________
Subtask 53-21-00-410-054
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Install the floor panels 132GF, 132FF (Ref. TASK 53-22-14-400-001).
Subtask 53-21-00-410-054-A
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Install the floor panels 132GF, 132FF (Ref. TASK 53-22-14-400-001).
(6) Install the ceiling panels 131MC, 131PC (Ref. TASK 25-54-12-400-002).
EFF :
ALL 53-21-00
Page 691
Feb 01/07
IAC
**ON A/C ALL
Subtask 53-21-00-410-068
B. Close Access
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
DURING CARGO COMPARTMENT DOOR OPERATION.
(1) Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
002).
EFF :
ALL 53-21-00
Page 692
Feb 01/07
R
IAC
TASK 53-21-00-200-012
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-21-00
Page 693
Feb 01/07
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-21-00-941-061
A. Get Access
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
DURING CARGO COMPARTMENT DOOR OPERATION.
(2) Open the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
001).
Subtask 53-21-00-010-068
(1) Remove the cargo floor panels 131BF, 131FF, 131JF (Ref. TASK 53-22-
14-000-001).
Subtask 53-21-00-010-068-A
(1) Remove the cargo floor panels 131BF and 131DG (Ref. TASK 53-22-14-
000-001).
EFF :
ALL 53-21-00
Page 694
Feb 01/07
IAC
**ON A/C ALL
Subtask 53-21-00-110-064
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-21-00-220-067
A. Inspection
R (Ref. Fig. 618/TASK 53-21-00-991-012)
EFF :
ALL 53-21-00
Page 695
Feb 01/07
IAC
Inspection of the Splices at STGR35 in the Forward Cargo Compartment
R Figure 618/TASK 53-21-00-991-012
EFF :
ALL 53-21-00
Page 696
Feb 01/07
IAC
5. Close-up
________
Subtask 53-21-00-410-066
(1) Install the insulation blankets of the floor panels 131BF, 131FF,
131JF (Ref. TASK 25-80-00-400-001).
(2) Install the cargo floor panels 131BF, 131FF, 131JF (Ref. TASK 53-22-
14-400-001).
Subtask 53-21-00-410-066-A
(1) Install the insulation blankets of the floor panels 131BF and 131DG
(Ref. TASK 25-80-00-400-001).
(2) Install the cargo floor panels 131BF and 131DG (Ref. TASK 53-22-14-
400-001).
Subtask 53-21-00-942-082
B. Close access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
002).
EFF :
ALL 53-21-00
Page 697
Feb 01/07
IAC
R **ON A/C 001-012, 014-099, 901-999,
TASK 53-21-00-200-013
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
001-012, 014-099, 901-999, 53-21-00
Page 698
Feb 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-21-00-010-093
A. Get Access
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
DURING CARGO COMPARTMENT DOOR OPERATION.
(2) Open the forward cargo compartment door 825 (Ref. TASK 52-30-00-860-
001).
(3) Remove the floor panels of the forward cargo compartment (Ref. TASK
53-22-14-000-001).
R
EFF :
001-012, 014-099, 901-999, 53-21-00
Page 699
Feb 01/07
IAC
Subtask 53-21-00-110-068
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-21-00-220-068
A. Inspection
R (Ref. Fig. 619/TASK 53-21-00-991-013)
R
EFF :
001-012, 014-099, 901-999, 53-21-00
Page A600
Feb 01/07
IAC
Fuselage Internal Structure between FR24 and FR35 from STGR38 to bottom
Centerline, Left and Right Sides
R Figure 619/TASK 53-21-00-991-013
R EFF :
001-012, 014-099, 901-999,
53-21-00 Page A601
Feb 01/07
IAC
Subtask 53-21-00-916-052
(1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fittings adjacent to the
area.
5. Close-up
________
Subtask 53-21-00-410-067
(1) Install the floor panels of the forward cargo compartment (Ref. TASK
53-22-14-400-001).
Subtask 53-21-00-942-067
B. Close Access
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
DURING CARGO COMPARTMENT DOOR OPERATION.
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
002).
R
EFF :
001-012, 014-099, 901-999, 53-21-00
Page A602
Feb 01/07
IAC
(3) Remove the access platform(s).
R
EFF :
001-012, 014-099, 901-999, 53-21-00
Page A603
Feb 01/07
IAC
R **ON A/C 101-199,
R TASK 53-21-00-200-013-A
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R
EFF :
101-199, 53-21-00
Page A604
Feb 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R 3. __________
Job Set-up
R Subtask 53-21-00-010-092
R A. Get Access
R WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
R DURING CARGO COMPARTMENT DOOR OPERATION.
R (2) Open the forward cargo compartment door 825 (Ref. TASK 52-30-00-860-
R 001).
R (3) Remove the floor panels of the forward cargo compartment (Ref. TASK
R 53-22-14-000-001), (Ref. TASK 53-22-14-000-002)
R
EFF :
101-199, 53-21-00
Page A605
Feb 01/07
IAC
R Subtask 53-21-00-110-079
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
R 4. Procedure
_________
R Subtask 53-21-00-220-072
R A. Inspection
R (Ref. Fig. 620/TASK 53-21-00-991-032)
R
EFF :
101-199, 53-21-00
Page A606
Feb 01/07
IAC
R Fuselage Internal Structure between FR24 and FR35.8 from STGR38 to bottom
R Centerline, Left and Right Sides
R Figure 620/TASK 53-21-00-991-032
R EFF :
101-199,
53-21-00 Page A607
Feb 01/07
IAC
R Subtask 53-21-00-916-060
R (1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
R (Material No. 08-074) on the equipment and fittings adjacent to the
R area.
R 5. Close-up
________
R Subtask 53-21-00-410-075
R (1) Install the floor panels of the forward cargo compartment (Ref. TASK
R 53-22-14-400-001) (Ref. TASK 53-22-14-400-002) .
R Subtask 53-21-00-942-077
R B. Close Access
R WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
R DURING CARGO COMPARTMENT DOOR OPERATION.
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
R 002).
R
EFF :
101-199, 53-21-00
Page A608
Feb 01/07
IAC
R (3) Remove the access platform(s).
EFF :
101-199, 53-21-00
Page A609
Feb 01/07
IAC
R **ON A/C ALL
TASK 53-21-00-200-016
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-21-00
Page A610
Feb 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-21-00-941-066
A. Get Access
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
DURING CARGO COMPARTMENT DOOR OPERATION.
Subtask 53-21-00-010-055
(1) Disconnect the actuator from the cargo door structure (Ref. TASK 52-
36-18-000-001).
R
EFF :
ALL 53-21-00
Page A611
Feb 01/07
IAC
Subtask 53-21-00-110-060
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-21-00-220-069
A. Inspection
R (Ref. Fig. 621/TASK 53-21-00-991-017)
R
EFF :
ALL 53-21-00
Page A612
Feb 01/07
IAC
Fittings at FR25, FR26 and FR27.
R Figure 621/TASK 53-21-00-991-017
R
EFF :
ALL 53-21-00
Page A613
Feb 01/07
IAC
5. Close-up
________
Subtask 53-21-00-410-055
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Connect the actuator to the door structure (Ref. TASK 52-36-18-400-
001).
Subtask 53-21-00-942-073
B. Close Access
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
DURING CARGO COMPARTMENT DOOR OPERATION.
(1) Close the forward compartment door 825 (Ref. TASK 52-30-00-860-002).
R
EFF :
ALL 53-21-00
Page A614
Feb 01/07
IAC
TASK 53-21-00-200-017
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-21-00
Page A615
Feb 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-21-00-941-068
A. Get Access
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
DURING CARGO COMPARTMENT DOOR OPERATION.
(2) Open the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
001).
Subtask 53-21-00-010-057
(1) Disconnect the actuator from the door structure (Ref. TASK 52-36-18-
000-001).
EFF :
ALL 53-21-00
Page A616
Feb 01/07
IAC
Subtask 53-21-00-110-061
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
(2) Make sure that the surface of the inspection area is clean and
smooth.
EFF :
ALL 53-21-00
Page A617
Feb 01/07
IAC
Cross Beams at FR25, FR26 and FR27
R Figure 622/TASK 53-21-00-991-040
EFF :
ALL 53-21-00
Page A618
Feb 01/07
IAC
4. Procedure
_________
Subtask 53-21-00-250-051
A. Inspection
R (Ref. Fig. 622/TASK 53-21-00-991-040)
5. Close-up
________
Subtask 53-21-00-410-057
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Connect the actuator to the door structure (Ref. TASK 52-36-18-400-
001).
Subtask 53-21-00-942-074
B. Close Access
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE ELEVATORS ARE CLEAR
_______
DURING CARGO COMPARTMENT DOOR OPERATION.
(1) Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
002).
EFF :
ALL 53-21-00
Page A619
Feb 01/07
IAC
(2) Remove the access platform(s).
EFF :
ALL 53-21-00
Page A620
Feb 01/07
IAC
R **ON A/C 001-012, 014-099, 901-999,
TASK 53-21-00-210-001
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
001-012, 014-099, 901-999, 53-21-00
Page A621
Feb 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-21-00-010-082
A. Get Access
(2) Open the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
010-001).
Subtask 53-21-00-110-086
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
EFF :
001-012, 014-099, 901-999, 53-21-00
Page A622
Feb 01/07
IAC
4. Procedure
_________
Subtask 53-21-00-210-071
A. Inspection
R (Ref. Fig. 623/TASK 53-21-00-991-026)
(3) Make sure that all the installations are attached correctly.
Subtask 53-21-00-916-061
(1) Put masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fittings adjacent to the
area.
EFF :
001-012, 014-099, 901-999, 53-21-00
Page A623
Feb 01/07
IAC
Cabin Floor Structure between FR24 and FR35
R Figure 623/TASK 53-21-00-991-026
EFF :
001-012, 014-099, 901-999, 53-21-00
Page A624
Feb 01/07
IAC
5. Close-up
________
Subtask 53-21-00-410-080
A. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
410-001).
EFF :
001-012, 014-099, 901-999, 53-21-00
Page A625
Feb 01/07
IAC
R **ON A/C 101-199,
R TASK 53-21-00-210-001-A
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
101-199, 53-21-00
Page A626
Feb 01/07
IAC
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R 3. __________
Job Set-up
R Subtask 53-21-00-010-085
R A. Get Access
R (2) Open the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
R 010-001).
R Subtask 53-21-00-110-089
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
EFF :
101-199, 53-21-00
Page A627
Feb 01/07
IAC
R 4. Procedure
_________
R Subtask 53-21-00-210-074
R A. Inspection
R (Ref. Fig. 624/TASK 53-21-00-991-027)
R (3) Make sure that all the installations are attached correctly.
R Subtask 53-21-00-916-064
R (1) Put masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
R (Material No. 08-074) on the equipment and fittings adjacent to the
R area.
EFF :
101-199, 53-21-00
Page A628
Feb 01/07
IAC
R Cabin Floor Structure between FR24 and FR35.8
R Figure 624/TASK 53-21-00-991-027
EFF :
101-199, 53-21-00
Page A629
Feb 01/07
IAC
R 5. Close-up
________
R Subtask 53-21-00-410-083
R A. Close Access
R (2) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (3) Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
R 410-001).
EFF :
101-199, 53-21-00
Page A630
Feb 01/07
IAC
R **ON A/C ALL
TASK 53-21-00-210-002
General Visual Inspection of Forward Cargo Door Cutout, Visible Part of Lateral
FR 24A and FR 28
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-21-00
Page A631
Feb 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-21-00-010-083
A. Get Access
(2) Open the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
001).
Subtask 53-21-00-110-087
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
EFF :
ALL 53-21-00
Page A632
Feb 01/07
IAC
4. Procedure
_________
Subtask 53-21-00-210-072
A. Inspection
(Ref. Fig. 625/TASK 53-21-00-991-028)
Subtask 53-21-00-916-062
(1) Put masking paper or MASKING TAPE BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fittings adjacent to the
area.
EFF :
ALL 53-21-00
Page A633
Feb 01/08
IAC
Forward Cargo Door Cutout at FR24A and FR28
R Figure 625/TASK 53-21-00-991-028
EFF :
ALL 53-21-00
Page A634
Feb 01/07
IAC
5. Close-up
________
Subtask 53-21-00-410-081
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
002).
EFF :
ALL 53-21-00
Page A635
Feb 01/07
IAC
TASK 53-21-00-210-006
General Visual Inspection of Forward Cargo Door Lock Fittings and Surrounding
Structure, between FR 25 and FR 27A, External Portion (6 places)
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-21-00
Page A636
Feb 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-21-00-941-080
A. Get Access
(2) Open the forward cargo compartment door 825 (Ref. TASK 52-30-00-860-
001)
Subtask 53-21-00-110-095
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
EFF :
ALL 53-21-00
Page A637
Feb 01/07
IAC
4. Procedure
_________
Subtask 53-21-00-210-079
A. Inspection
(Ref. Fig. 626/TASK 53-21-00-991-029)
(1) Do a visual inspection of the lock fittings of the forward cargo door
and the adjacent structure. This inspection includes the area between
FR25 and FR27A, and the external part (6 places).
Subtask 53-21-00-916-065
(1) Put masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fittings adjacent to the
area.
EFF :
ALL 53-21-00
Page A638
Feb 01/08
IAC
Forward Cargo Door - Lock Fittings and the Adjacent Structure, FR25 and FR27A
R Figure 626/TASK 53-21-00-991-029
EFF :
ALL 53-21-00
Page A639
Feb 01/07
IAC
5. Close-up
________
Subtask 53-21-00-942-086
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Close the forward cargo compartment door 825 (Ref. TASK 52-30-00-860-
002).
EFF :
ALL 53-21-00
Page A640
Feb 01/07
IAC
R **ON A/C 001-012, 014-099, 901-999,
TASK 53-21-00-220-001
Detailed Inspection of Cabin Floor Structure, below and 0.5 M around Galleys
and Toilets (if Installed), between FR 24 and FR 35
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
001-012, 014-099, 901-999, 53-21-00
Page A641
Feb 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-21-00-010-075
A. Get Access
(2) Open the forward passenger/crew door 831 841 (Ref. TASK 52-10-00-010-
001).
EFF :
001-012, 014-099, 901-999, 53-21-00
Page A642
Nov 01/07
IAC
(4) Remove the galleys if installed (Ref. TASK 25-31-41-000-002)
(Ref. TASK 25-31-41-000-001) (Ref. TASK 25-32-41-000-001).
(5) Remove the cabin floor panels from FR24 to FR35 (Ref. TASK 53-22-12-
000-001).
Get Access
Subtask 53-21-00-110-076
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-21-00-220-070
A. Inspection
R (Ref. Fig. 623/TASK 53-21-00-991-026)
(1) Do a detailed inspection of the cabin floor structure below and 0.5 m
(1.64 ft.) around the galleys and the lavatories. This inspection is
applicable between FR24 and FR35 and includes the seat tracks and
cross beams.
EFF :
001-012, 014-099, 901-999, 53-21-00
Page A643
Feb 01/07
IAC
(b) Other damage (cracks, scratches, stress, marks, dents,
bumps,...):
- If you find other damage, refer to the Structural Repair Manual
(Ref. SRM 511100 P.Block 001) for damage classification and
corrective action.
Subtask 53-21-00-916-057
(1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-074) on the equipment and fittings adjacent to the
area.
5. Close-up
________
Subtask 53-21-00-410-073
A. Close Access
(1) Install the cabin floor panels from FR24 to FR35 (Ref. TASK 53-22-12-
400-001).
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
001-012, 014-099, 901-999, 53-21-00
Page A644
Nov 01/07
IAC
(5) Close the forward passenger/crew door 831 841 (Ref. TASK 52-10-00-
410-001).
EFF :
001-012, 014-099, 901-999, 53-21-00
Page A645
Feb 01/07
IAC
R **ON A/C 101-199,
R TASK 53-21-00-220-001-A
R Detailed Inspection of Cabin Floor Structure, below and 0.5 M around Galleys
R and Toilets (if Installed) and Emergency Exit Entrance Area, between FR 24 ...
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
101-199, 53-21-00
Page A646
Feb 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R 3. __________
Job Set-up
R Subtask 53-21-00-010-076
R A. Get Access
R (2) Open the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
R 010-001).
EFF :
101-199, 53-21-00
Page A647
Feb 01/07
IAC
R (4) Remove the galleys, if installed (Ref. TASK 25-31-41-000-001)
R (Ref. TASK 25-31-41-000-002) (Ref. TASK 25-32-41-000-001).
R (5) Remove the cabin floor panels from FR24 to FR35.8 (Ref. TASK 53-22-
R 12-000-001).
R Subtask 53-21-00-110-077
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
R 4. Procedure
_________
R Subtask 53-21-00-220-071
R A. Inspection
R (Ref. Fig. 624/TASK 53-21-00-991-027)
EFF :
101-199, 53-21-00
Page A648
Feb 01/07
IAC
R (b) Other damage (cracks, scratches, stress, marks, dents,
R bumps,...):
R - If you find other damage, refer to the Structural Repair Manual
R (Ref. SRM 511100 P.Block 001) for damage classification and
R corrective action.
R Subtask 53-21-00-916-058
R (1) Put masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS
R (Material No. 08-074) on the equipment and fittings adjacent to the
R area.
R 5. Close-up
________
R Subtask 53-21-00-410-074
R A. Close Access
R (1) Install the cabin floor panels from FR24 to FR35.8 (Ref. TASK 53-22-
R 12-400-001).
R (4) Make sure that the work area is clean and clear of tool(s) and other
R items.
EFF :
101-199, 53-21-00
Page A649
Feb 01/07
IAC
R (5) Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
R 410-001).
EFF :
101-199, 53-21-00
Page A650
Feb 01/07
IAC
R TASK 53-21-00-200-025
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
101-199, 53-21-00
Page A651
Feb 01/07
IAC
R 3. __________
Job Set-up
R Subtask 53-21-00-941-071
R A. Get Access
R Subtask 53-21-00-110-078
R (1) Remove the top layer paint from the inspection area (Ref. TASK 51-75-
R 12-300-001), (Ref. SRM 517500,P.Block-001), (Ref. SRM 512300,P.Block-
R 001).
R (2) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
R (3) Make sure that the surface of the inspection area is clean and
R smooth.
EFF :
101-199, 53-21-00
Page A652
Feb 01/07
IAC
R Circumferential Joint at FR35.8
R Figure 627/TASK 53-21-00-991-043
EFF :
101-199, 53-21-00
Page A653
Feb 01/07
IAC
R (5) Make sure that there is no:
R 4. Procedure
_________
R Subtask 53-21-00-250-052
R A. Inspection
R (Ref. Fig. 627/TASK 53-21-00-991-043)
R 5. Close-up
________
R Subtask 53-21-00-370-051
R A. Application of Paint
R (1) Apply the top layer paint on the inspection area (Ref. TASK 51-75-12-
R 300-001), (Ref. SRM 517500,P.Block-001), (Ref. SRM 512300,P.Block-
R 001).
EFF :
101-199, 53-21-00
Page A654
Feb 01/07
IAC
R Subtask 53-21-00-942-076
R B. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
EFF :
101-199, 53-21-00
Page A655
Feb 01/07
IAC
R TASK 53-21-00-220-002
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
101-199, 53-21-00
Page A656
Feb 01/07
IAC
R 3. __________
Job Set-up
R Subtask 53-21-00-941-073
R A. Get Access
R Subtask 53-21-00-110-080
R (1) Clean the inspection area with a CLEANING AGENTS (Material No. 11-
R 004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-
R 003), if necessary.
R 4. Procedure
_________
R Subtask 53-21-00-220-073
R A. Inspection
R (Ref. Fig. 628/TASK 53-21-00-991-033)
EFF :
101-199, 53-21-00
Page A657
Feb 01/07
IAC
R Fuselage External Surface between FR35 and 35.8
R Figure 628/TASK 53-21-00-991-033
EFF :
101-199, 53-21-00
Page A658
Feb 01/07
IAC
R (b) Other damage (cracks, scratches, stress, marks, dents,
R bumps,...):
R - If you find other damage, refer to the Structural Repair Manual
R (Ref. SRM 511100 P.Block 001) for damage classification and
R corrective action.
R 5. Close-up
________
R Subtask 53-21-00-942-078
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
EFF :
101-199, 53-21-00
Page A659
Feb 01/07
IAC
R TASK 53-21-00-210-004
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
101-199, 53-21-00
Page A660
Feb 01/07
IAC
R 3. __________
Job Set-up
R Subtask 53-21-00-941-077
R A. Get Access
R Subtask 53-21-00-110-092
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-
R 003), if necessary.
R 4. Procedure
_________
R Subtask 53-21-00-210-076
R A. Inspection
R (Ref. Fig. 629/TASK 53-21-00-991-048)
EFF :
101-199, 53-21-00
Page A661
Feb 01/07
IAC
R Fuselage External Surface between FR35.4 and FR35.8
R Figure 629/TASK 53-21-00-991-048
EFF :
101-199, 53-21-00
Page A662
Feb 01/07
IAC
R (b) Other damage (cracks, scratches, stress, marks, dents,
R bumps,...):
R If you find other damage, refer to the Structural Repair Manual
R (Ref. SRM 511100 P.Block 001) for damage classification and
R corrective action.
R 5. Close-up
________
R Subtask 53-21-00-942-083
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
EFF :
101-199, 53-21-00
Page A663
Feb 01/07
IAC
R **ON A/C 001-012, 014-099, 901-999,
TASK 53-21-00-210-005
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
001-012, 014-099, 901-999, 53-21-00
Page A664
Feb 01/07
IAC
3. __________
Job Set-up
Subtask 53-21-00-941-078
A. Get Access
Subtask 53-21-00-110-093
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-
003), if necessary.
4. Procedure
_________
Subtask 53-21-00-210-077
A. Inspection
R (Ref. Fig. 630/TASK 53-21-00-991-049)
EFF :
001-012, 014-099, 901-999, 53-21-00
Page A665
Feb 01/07
IAC
Fuselage External Surface between FR24 and FR35
R Figure 630/TASK 53-21-00-991-049
EFF :
001-012, 014-099, 901-999, 53-21-00
Page A666
Feb 01/07
IAC
(2) Make sure that there is no:
5. Close-up
________
Subtask 53-21-00-942-084
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
001-012, 014-099, 901-999, 53-21-00
Page A667
Feb 01/07
IAC
R **ON A/C 101-199,
R TASK 53-21-00-210-005-A
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
101-199, 53-21-00
Page A668
Feb 01/07
IAC
R 3. __________
Job Set-up
R Subtask 53-21-00-941-079
R A. Get Access
R Subtask 53-21-00-110-094
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-
R 003), if necessary.
R 4. Procedure
_________
R Subtask 53-21-00-210-078
R A. Inspection
R (Ref. Fig. 631/TASK 53-21-00-991-050)
EFF :
101-199, 53-21-00
Page A669
Feb 01/07
IAC
R Fuselage External Surface between FR24 and FR35.8 from STGR23 to the bottom
R Centerline, Left and Right Sides
R Figure 631/TASK 53-21-00-991-050
EFF :
101-199,
53-21-00 Page A670
Feb 01/07
IAC
R (2) Make sure that there is no:
R 5. Close-up
________
R Subtask 53-21-00-942-085
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
EFF :
101-199, 53-21-00
Page A671
Feb 01/07
IAC
R TASK 53-21-00-220-003
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
101-199, 53-21-00
Page A672
Feb 01/07
IAC
R 3. __________
Job Set-up
R Subtask 53-21-00-010-078
R A. Get Access
R (2) Remove the access panels 191AT (192AT) (Ref. TASK 53-25-11-000-001).
R Subtask 53-21-00-110-081
R (1) Clean the inspection area with a CLEANING AGENTS (Material No. 11-
R 004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-
R 003), if necessary.
R 4. Procedure
_________
R Subtask 53-21-00-220-074
R A. Inspection
R (Ref. Fig. 632/TASK 53-21-00-991-034)
EFF :
101-199, 53-21-00
Page A673
Feb 01/07
IAC
R Fuselage Surface Below the Belly Fairing, from FR35.5 to FR35.7
R Figure 632/TASK 53-21-00-991-034
EFF :
101-199, 53-21-00
Page A674
Feb 01/07
IAC
R (2) Make sure that there is no:
R 5. Close-up
________
R Subtask 53-21-00-410-076
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Install the access panels 191AT (192AT) (Ref. TASK 53-25-11-400-001).
EFF :
101-199, 53-21-00
Page A675
Feb 01/07
IAC
R TASK 53-21-00-220-004
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
101-199, 53-21-00
Page A676
Feb 01/07
IAC
R 3. __________
Job Set-up
R Subtask 53-21-00-010-079
R A. Get Access
R (2) Open the forward emergency exit door 843 (Ref. TASK 52-22-00-010-
R 002).
R Subtask 53-21-00-110-082
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
R 4. Procedure
_________
R Subtask 53-21-00-220-075
R A. Inspection
R (Ref. Fig. 633/TASK 53-21-00-991-035)
EFF :
101-199, 53-21-00
Page A677
Feb 01/07
IAC
R Forward Emergency Exit, Upper corners - External Surface, Right Side
R Figure 633/TASK 53-21-00-991-035
EFF :
101-199, 53-21-00
Page A678
Feb 01/07
IAC
R (2) Make sure that there is no:
R 5. Close-up
________
R Subtask 53-21-00-410-077
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Close the forward emergency exit door 843 (Ref. TASK 52-22-00-410-
R 002).
EFF :
101-199, 53-21-00
Page A679
Feb 01/07
IAC
R TASK 53-21-00-220-005
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
101-199, 53-21-00
Page A680
Feb 01/07
IAC
R 3. __________
Job Set-up
R Subtask 53-21-00-941-074
R A. Get Access
R Subtask 53-21-00-110-083
R (1) Clean the inspection area with a CLEANING AGENTS (Material No. 11-
R 004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-
R 003), if necessary.
R 4. Procedure
_________
R Subtask 53-21-00-220-076
R A. Inspection
R (Ref. Fig. 634/TASK 53-21-00-991-036)
EFF :
101-199, 53-21-00
Page A681
Feb 01/07
IAC
R Fuselage Skin and the Window Forging Doublers around the Cabin Windows, Left
R and Right Sides
R Figure 634/TASK 53-21-00-991-036
EFF :
101-199,
53-21-00 Page A682
Feb 01/07
IAC
R (2) Make sure that there is no:
R 5. Close-up
________
R Subtask 53-21-00-942-079
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
EFF :
101-199, 53-21-00
Page A683
Feb 01/07
IAC
R TASK 53-21-00-220-006
R Detailed Inspection of FR 35.1 and FR 35.2A Web and Door Stop Intercostals, at
R Junction Area, between Door Stop No1 and No8 (LH)/No6 (RH), LH/RH
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
101-199, 53-21-00
Page A684
Feb 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R 3. __________
Job Set-up
R Subtask 53-21-00-010-080
R A. Get Access
R (2) Open the forward emergency exit door 833 (843), (Ref. TASK 52-22-00-
R 010-002).
R (3) Remove the door frame linings (Ref. TASK 25-23-47-000-004) (Ref. TASK
R 25-23-47-000-009).
R Subtask 53-21-00-110-084
R (1) Clean the inspection area with a CLEANING AGENTS (Material No. 11-
R 004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-
R 003), if necessary.
EFF :
101-199, 53-21-00
Page A685
Feb 01/07
IAC
R 4. Procedure
_________
R Subtask 53-21-00-220-077
R A. Inspection
R (Ref. Fig. 635/TASK 53-21-00-991-037)
R (1) Do a detailed inspection of the FR35.1 and FR35.2A web and the door
R stop intercostals. This inspection is applicable at the junction area
R :
R - For the left side, between door stop No. 1 and No. 8
R - For the right side, between door stop No. 1 and No. 6.
R 5. Close-up
________
R Subtask 53-21-00-410-078
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (4) Close the forward emergency exit door 833 (843), (Ref. TASK 52-22-00-
R 410-002).
EFF :
101-199, 53-21-00
Page A686
Feb 01/07
IAC
INTENTIONALLY BLANK
53-21-00
Page A687
Feb 01/07
IAC
R FR35.1 and FR35.2A Web and Door Stop Intercostals
R Figure 635/TASK 53-21-00-991-037- 12 (SHEET 1)
EFF :
101-199, 53-21-00
Page A688
Feb 01/07
IAC
R FR35.1 and FR35.2A Web and Door Stop Intercostals
R Figure 635/TASK 53-21-00-991-037- 22 (SHEET 2)
EFF :
101-199, 53-21-00
Page A689
Feb 01/07
IAC
R TASK 53-21-00-220-007
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
101-199, 53-21-00
Page A690
Feb 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R 3. __________
Job Set-up
R Subtask 53-21-00-010-081
R A. Get Access
R (2) Open the forward cargo compartment door 825 (Ref. TASK 52-30-00-860-
R 001).
R (3) Remove the sidewall panels 131QW, 131RW, 132QW, 132RW (Ref. TASK 25-
R 54-12-000-003).
R Subtask 53-21-00-110-085
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
EFF :
101-199, 53-21-00
Page A691
Feb 01/07
IAC
R 4. Procedure
_________
R Subtask 53-21-00-220-078
R A. Inspection
R (Ref. Fig. 636/TASK 53-21-00-991-038)
R 5. Close-up
________
R Subtask 53-21-00-410-079
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (3) Install the sidewall panels 131QW, 131RW, 132QW, 132RW (Ref. TASK 25-
R 54-12-400-003).
R (4) Close the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-
R 002).
EFF :
101-199, 53-21-00
Page A692
Feb 01/07
IAC
R Attachment Area of FR35.1 and FR35.2A to the Cabin Floor Beams
R Figure 636/TASK 53-21-00-991-038
EFF :
101-199, 53-21-00
Page A693
Feb 01/07
IAC
R **ON A/C 901-999,
TASK 53-21-00-200-026
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
901-999, 53-21-00
Page A694
Feb 01/07
IAC
3. __________
Job Set-up
Subtask 53-21-00-941-075
A. Get Access
Subtask 53-21-00-110-091
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-21-00-220-081
A. Inspection
R (Ref. Fig. 637/TASK 53-21-00-991-044)
EFF :
901-999, 53-21-00
Page A695
Feb 01/07
IAC
Circumferential Joint at FR35
R Figure 637/TASK 53-21-00-991-044
EFF :
901-999, 53-21-00
Page A696
Feb 01/07
IAC
(b) Other damage (cracks, scratches, stress, marks, dents,
bumps,...).
- If you find this type of damage, refer to the Structural Repair
Manual (Ref. SRM 511100 P.Block 001) for damage classification
and corrective action.
5. Close-up
________
Subtask 53-21-00-942-081
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
901-999, 53-21-00
Page A697
Feb 01/07
IAC
R **ON A/C 101-199,
R TASK 53-21-00-210-015
R General Visual Inspection of Fuselage Skin Around Forward Emergency Exit Skin
R Cutout between FR 35 and FR 35.3 and from Stringer 8 to Stringer 23 External...
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
101-199, 53-21-00
Page A698
Feb 01/07
IAC
R 3. __________
Job Set-up
R Subtask 53-21-00-010-103
R A. Get Access
R Subtask 53-21-00-110-112
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
R and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
R necessary.
R 4. Procedure
_________
R Subtask 53-21-00-210-091
R A. Inspection
R (Ref. Fig. 638/TASK 53-21-00-991-062)
EFF :
101-199, 53-21-00
Page A699
Feb 01/07
IAC
R Skin Around the Forward Emergency Exit - from FR35 to 35.3 and from STGR8 to
R STGR23, External Surface
R Figure 638/TASK 53-21-00-991-062
EFF :
101-199,
53-21-00 Page B600
Feb 01/07
IAC
R (b) Other damage (cracks, scratches, stress, marks, dents,
R bumps,...):
R - If you find other damage, refer to the Structural Repair Manual
R (Ref. SRM 511100 P.Block 001) for damage classification and
R corrective action.
R 5. Close-up
________
R Subtask 53-21-00-410-097
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
EFF :
101-199, 53-21-00
Page B601
Feb 01/07
IAC
R **ON A/C 901-999,
TASK 53-21-00-200-030
Detailed Inspection of Frame Webs at Stringer 18 LH/RH for: FR25, 26, 27, 28
29, 30, 34
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
901-999, 53-21-00
Page B602
Feb 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-21-00-010-104
A. Get Access
(2) Open the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
010-001).
(3) Remove the linings and the insulation panels between FR24 and FR35 in
zone 231 (232) at STGR18:
231GW, 231KW, 231NW, 231RW, 232GW, 232KW, 232NW, 232RW (Ref. TASK 25-
23-44-000-001),
231HW, 231LW, 231PW, 231SW, 232HW, 232LW, 232PW, 232SW (Ref. TASK 25-
23-43-000-001).
EFF :
901-999, 53-21-00
Page B603
Nov 01/07
IAC
Subtask 53-21-00-110-121
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
4. Procedure
_________
Subtask 53-21-00-220-089
A. Inspection
R
(1) Do a detailed inspection of the frame webs at STGR18 for: FR25, FR26,
FR27, FR28, FR29, FR30, FR34, left and right sides.
EFF :
901-999, 53-21-00
Page B604
Nov 01/07
IAC
5. Close-up
________
Subtask 53-21-00-410-098
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the linings and the insulation panels between FR24 and FR35
in zone 231 (232) at STGR18:
231GW, 231KW, 231NW, 231RW, 232GW, 232KW, 232NW, 232RW (Ref. TASK 25-
23-44-400-001),
231HW, 231LW, 231PW, 231SW, 232HW, 232LW, 232PW, 232SW (Ref. TASK 25-
23-43-400-001).
(3) Close the forward passenger/crew door 831 (841) (Ref. TASK 52-10-00-
410-001).
EFF :
901-999, 53-21-00
Page B605
Feb 01/07
IAC
PANELS - CABIN FLOOR - REMOVAL/INSTALLATION
___________________________________________
TASK 53-22-12-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-22-12
Page 401
Nov 01/07
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-22-12-861-050
Subtask 53-22-12-010-050
B. Get Access.
(1) Remove the necessary equipment and furnishings to get access to the
cabin floor panels.
4. Procedure
_________
EFF :
ALL 53-22-12
Page 402
Nov 01/07
IAC
Cabin Floor Panel Installation - FR24 thru FR35
Figure 401/TASK 53-22-12-991-001
R
EFF :
001-012, 014-099, 53-22-12
Page 403
May 01/06
IAC
R Cabin Floor Panel Installation - FR24 thru FR35.8
R Figure 401A/TASK 53-22-12-991-001-C
EFF :
101-199, 53-22-12
Page 404
Nov 01/07
IAC
Cabin Floor Panel Installation - FR24 thru FR35
Figure 401B/TASK 53-22-12-991-001-A
R
EFF :
901-901, 53-22-12
Page 405
Nov 01/07
IAC
R Cabin Floor Panel Installation - FR24 thru FR35
R Figure 401C/TASK 53-22-12-991-001-D
R
EFF :
902-999, 53-22-12
Page 406
Nov 01/07
IAC
R **ON A/C 001-012, 014-099, 901-901,
Subtask 53-22-12-020-050
(1) Pull the cord (1) up to remove the sealant from the floor panel
joints.
NOTE : Identify the floor panels. This will help the installation
____
procedure.
R Subtask 53-22-12-020-050-C
R (1) Pull the cord (4) up to remove the sealant from between the floor
R panel joints.
R NOTE : Identify the floor panels (1). This will help with the
____
R installation procedure.
R (4) If necessary, remove the heated floor panels 5DS (6DS) at the forward
R emergency exits (Ref. TASK 25-27-51-000-001).
R
EFF :
001-012, 014-099, 101-199, 901-901, 53-22-12
Page 407
Nov 01/07
IAC
R **ON A/C 902-999,
R Subtask 53-22-12-020-050-B
R (1) Pull the cord (4) up, to remove the sealant from the floor panel
R joints.
R NOTE : Identify the floor panels (1). This will help with the
____
R installation procedure.
R
EFF :
902-999, 53-22-12
Page 408
Nov 01/07
IAC
**ON A/C ALL
TASK 53-22-12-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-22-12
Page 409
Nov 01/07
R
IAC
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-22-12
Page 410
Feb 01/08
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-22-12-860-050
(1) Make sure the ground service network is energized (Ref. TASK 24-42-
00-861-001).
(2) Make sure the necessary equipment is removed to get access to the
cabin floor panels.
4. Procedure
_________
Subtask 53-22-12-160-050
R
EFF :
ALL 53-22-12
Page 411
Nov 01/07
IAC
(2) Remove the old sealant from the floor panels with a SCRAPER - NON
METALLIC.
(3) Make sure that the self-adhesive foam tape (2) is in the correct
condition. If necessary:
(b) Clean the contact surfaces with the CLEANING AGENTS (Material No.
11-026) and a clean lint-free cloth MISCELLANEOUS (Material No.
19-003).
(4) Make sure that the parts retained from the removed component are
clean and in the correct condition.
R Subtask 53-22-12-160-050-B
R (2) Remove the used sealant from the floor panels (1) with a SCRAPER -
R NON METALLIC.
R (3) Make sure that the clipnuts (5) are clean and in the correct
R condition. If necessary, replace the defective clipnuts.
R
EFF :
001-012, 014-099, 101-199, 902-999, 53-22-12
Page 412
Nov 01/07
IAC
R (4) Make sure that the self-adhesive foam tape (3) is in the correct
R condition. If necessary:
R (b) Clean the surfaces with the CLEANING AGENTS (Material No. 11-026)
R and a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
R (5) Make sure that the parts retained from the removed component are
R clean and in the correct condition.
Subtask 53-22-12-160-050-A
(1) Remove the used sealant from the floor panels with a SCRAPER - NON
METALLIC.
(a) Clean the component interface and the adjacent area with the
CLEANING AGENTS (Material No. 11-026) and a lint-free cotton
cloth, MISCELLANEOUS (Material No. 19-003).
(3) Make sure that the parts retained from the removed component are
clean and in the correct condition.
(5) Make sure that the clipnuts (5) are clean and in the correct
condition. If necessary, replace the defective clipnuts (5).
(6) Make sure that the self-adhesive foam tape (2), the self-adhesive
foam tape (7) and the self-adhesive foam tape (8) are in the correct
condition. If necessary:
(a) Remove the defective self-adhesive foam tapes (2), (7) and/or
(8).
R
EFF :
101-199, 901-999, 53-22-12
Page 413
Nov 01/07
IAC
(b) Clean the contact surfaces
1
_ Clean the contact surfaces of the self-adhesive foam tapes
(2), (7) and/or (8) with the CLEANING AGENTS (Material No. 11-
026) and a lint-free cotton cloth, MISCELLANEOUS (Material No.
19-003).
(c) Install the new self-adhesive foam tapes (2), (7) and/or (8) with
the correct width and thickness.
NOTE : The self-adhesive foam tapes (2), (7) and (8) have
____
different widths and thicknesses:
- The self-adhesive foam tape (2) is 25 mm (0.9842 in.)
wide and 2 mm (0.0787 in.) thick
- The self-adhesive foam tape (7) is 38 mm (1.4960 in.)
wide and 2 mm (0.0787 in.) thick
- The self-adhesive foam tape (8) is 38 mm (1.4960 in.)
wide and 4 mm (0.1574 in.) thick.
Subtask 53-22-12-420-050
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
001-012, 014-099, 901-901, 53-22-12
Page 414
Nov 01/07
IAC
(3) Apply the SPECIAL MATERIALS (Material No. 05-002) to the screws (3).
(4) Install the screws (3) and TORQUE to 0.42 m.daN (37.16 lbf.in).
(5) Install the cord (1) MISCELLANEOUS (Material No. 19-027) in the
clearance between the floor panels.
NOTE : Make a loop at the end of the cord, this will help the
____
subsequent removal procedure.
(6) Apply the SEALANTS (Material No. 09-016) in the clearance between the
floor panels.
R Subtask 53-22-12-420-050-C
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) If removed, install the heated floor panels 5DS (6DS), at the forward
R emergency exits (Ref. TASK 25-27-51-400-001).
R (4) Apply the zinc chromate putty SPECIAL MATERIALS (Material No. 05-002)
R to the screws (2).
R (5) Install the screws (2) and TORQUE to 0.42 m.daN (37.16 lbf.in).
R (6) Install the cord (4) MISCELLANEOUS (Material No. 19-027) in the
R clearance between the floor panels (1). Make a loop at the end of the
R cord. This will help with the subsequent removal procedure.
R (7) Apply the SEALANTS (Material No. 09-016) in the space between the
R floor panels (1).
EFF :
001-012, 014-099, 101-199, 901-901, 53-22-12
Page 415
Nov 01/07
IAC
R **ON A/C 902-999,
R Subtask 53-22-12-420-050-B
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (3) Apply the zinc chromate putty SPECIAL MATERIALS (Material No. 05-002)
R to the screws (2).
R (4) Install the screws (2) and TORQUE to 0.42 m.daN (37.16 lbf.in).
R (5) Install the cord (4) MISCELLANEOUS (Material No. 19-027) in the space
R between the floor panels (1). Make a loop at the end of the cord.
R This will help with the subsequent removal procedure.
R (6) Apply the SEALANTS (Material No. 09-016) in the space between the
R floor panels (1).
5. Close-up
________
Subtask 53-22-12-410-051
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the equipment removed to get access to the cabin floor
panels.
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-22-12
Page 416
Nov 01/07
IAC
Subtask 53-22-12-862-050
EFF :
ALL 53-22-12
Page 417
Nov 01/07
IAC
PANELS - FWD CARGO COMPARTMENT FLOOR - REMOVAL/INSTALLATION
___________________________________________________________
TASK 53-22-14-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-22-14
Page 401
Feb 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-22-14-010-050
A. Get Access
(2) Put the access platform in position below the FWD cargo-compartment
door.
4. Procedure
_________
EFF :
ALL 53-22-14
Page 402
Feb 01/07
IAC
FWD Cargo-Compartment Floor-Panels
Figure 401/TASK 53-22-14-991-001
R
EFF :
001-012, 014-019, 53-22-14
Page 403
May 01/01
IAC
R FWD Cargo-Compartment Floor-Panels
R Figure 401A/TASK 53-22-14-991-001-A
R
EFF :
020-099, 53-22-14
Page 404
May 01/01
IAC
R FWD Cargo-Compartment Floor-Panels
R Figure 401B/TASK 53-22-14-991-001-C
EFF :
101-199, 53-22-14
Page 405
Feb 01/07
IAC
FWD Cargo-Compartment Floor-Panels
R Figure 401C/TASK 53-22-14-991-001-B
R
EFF :
901-999, 53-22-14
Page 406
Feb 01/07
IAC
**ON A/C 001-012, 014-019,
Subtask 53-22-14-020-050
(2) Pull the cord (7) up to remove the sealant from between the floor
panels (1).
(3) Remove the sealant from between the cutouts and the tiedown positions
with a nonmetallic scraper.
(5) Remove the floor panels (1) and the seals (3), (4), (5) and (6).
Subtask 53-22-14-020-050-A
(2) Pull the cord (7) up to remove the sealant from between the floor
panels (1).
(3) Remove the sealant from between the cutouts and the tiedown positions
with a nonmetallic scraper.
(5) Remove the floor panels (1) and the seals (3) and (6).
EFF :
ALL 53-22-14
Page 407
Feb 01/07
IAC
**ON A/C ALL
TASK 53-22-14-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-22-14
Page 408
Feb 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-22-14-860-050
(1) Make sure that the aircraft is in the same configuration as for the
removal task.
4. Procedure
_________
EFF :
ALL 53-22-14
Page 409
Nov 01/07
IAC
**ON A/C 020-099,
Subtask 53-22-14-916-050
R (1) Remove the used sealant from the floor panels with a SCRAPER - NON
R METALLIC.
R (2) Clean the component interface and the adjacent area with the CLEANING
R AGENTS (Material No. 11-026) and a clean lint-free cloth
R MISCELLANEOUS (Material No. 19-003).
(3) Make sure that the parts retained from the removed component are
clean and in the correct condition.
Subtask 53-22-14-420-050
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Put the floor panels (1) and the seals (3) thru (6) in position.
EFF :
ALL 53-22-14
Page 410
Nov 01/07
IAC
R (3) Apply the SEALANTS (Material No. 09-005) in the holes at the end of
R each seal.
R (4) Make sure that all the seal intersections are flush with each other.
R (5) Apply the zinc chromate putty SPECIAL MATERIALS (Material No. 05-002)
R to the screws (2).
R (6) Install the screws (2) and TORQUE to 0.42 m.daN (37.16 lbf.in).
R (7) Install the cord (7) FIBER GLASS CORD 1.1MM DIA. (DAN107-1) in the
R spaces between the floor panels (1).
R
R (8) Make a loop at the end of the cord. This will help with the subsequet
R removal procedure.
R (9) Apply the SEALANTS (Material No. 09-005) in the spaces between the
R floor panels (1) and the cutouts of the tiedown positions.
Subtask 53-22-14-420-050-A
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Put the floor panels (1) and the seals (3) and (6) in position.
R (3) Apply the SEALANTS (Material No. 09-005) in the holes at the end of
R each seal.
R (4) Make sure that all the seal intersections are flush with each other.
R (5) Apply the zinc chromate putty SPECIAL MATERIALS (Material No. 05-002)
R to the screws (2).
R (6) Install the screws (2) and TORQUE to 0.42 m.daN (37.16 lbf.in).
R (7) Install the cord (7) FIBER GLASS CORD 1.1MM DIA. (DAN107-1) in the
R spaces between the floor panels (1).
R
EFF :
ALL 53-22-14
Page 411
May 01/07
IAC
R (8) Make a loop at the end of the cord. This will help with the susequent
R removal procedure.
R (9) Apply the SEALANTS (Material No. 09-005) in the spaces between the
R floor panels (1) and the cutouts of the tiedown positions.
5. Close-up
________
Subtask 53-22-14-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-22-14
Page 412
May 01/07
IAC
R **ON A/C 101-199,
R TASK 53-22-14-000-002
R 1. __________________
Reason for the Job
R Self Explanatory
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R 3. __________
Job Set-up
R Subtask 53-22-14-010-051
R A. Get Access
EFF :
101-199, 53-22-14
Page 413
Feb 01/07
IAC
R 4. Procedure
_________
R Subtask 53-22-14-020-051
R (1) Remove the screws (2) and the countersunk washers (3).
EFF :
101-199, 53-22-14
Page 414
Feb 01/07
IAC
R Maintenance Panels at Frame 35.5
R Figure 402/TASK 53-22-14-991-003
EFF :
101-199, 53-22-14
Page 415
Feb 01/07
IAC
R TASK 53-22-14-400-002
R 1. __________________
Reason for the Job
R Self Explanatory
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
101-199, 53-22-14
Page 416
Feb 01/07
IAC
R 3. __________
Job Set-up
R Subtask 53-22-14-860-051
R (1) Make sure that the aircraft is in the same configuration as for the
R removal task.
R 4. Procedure
_________
R Subtask 53-22-14-916-051
R WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
R MATERIAL.
R THIS MATERIAL IS DANGEROUS.
R (1) Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-064) to the
R maintenance panels (1), if necessary.
R (2) Clean the component interface and the adjacent area with CLEANING
R AGENTS (Material No. 11-004) and a clean cloth MISCELLANEOUS
R (Material No. 19-003).
R (3) Make sure that the parts retained from the removed component are
R clean and in the correct condition.
EFF :
101-199, 53-22-14
Page 417
Feb 01/07
IAC
R Subtask 53-22-14-420-051
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (3) Install the screws (2) with the countersunk washers (3).
R 5. Close-up
________
R Subtask 53-22-14-410-051
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (5) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
EFF :
101-199, 53-22-14
Page 418
Feb 01/07
IAC
FAIRINGS - WING TO FUSELAGE - REMOVAL/INSTALLATION
__________________________________________________
TASK 53-25-11-000-001
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-25-11
Page 401
Feb 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-25-11-865-050
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU AIR COND/RAM/AIR/INLET 1HZ D10
106VU CSM/G /EV/MAN/SPLY 6XE B04
EFF :
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Page 402
Feb 01/07
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-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
122VU AIR COND/PACK TEMP/CTL SYS1/1/28VDC 3HH X21
122VU AIR COND/PACK TEMP CTL SYS2/2/28VDC 24HH Y21
122VU AIR COND/PACK TEMP CTL SYS2/2/115VAC 22HH Y20
122VU AIR COND/PACK TEMP CTL SYS2/1/28VDC 4HH Y19
122VU AIR COND/PACK TEMP CTL SYS2/1/115VAC 2HH Y18
Subtask 53-25-11-869-052
(1) Make sure that the slats are extended (Ref. TASK 27-80-00-866-004).
Subtask 53-25-11-010-050
C. Get Access
(1) Put the access platform in position in the zones 191 and 192.
4. Procedure
_________
Subtask 53-25-11-020-051
EFF :
ALL 53-25-11
Page 403
Feb 01/07
IAC
R Fairing - Left Access Panels
Figure 401/TASK 53-25-11-991-001
EFF :
001-012, 014-019, 53-25-11
Page 404
May 01/00
IAC
Fairing - Left Access Panels
Figure 401A/TASK 53-25-11-991-001-A
R
EFF :
020-099, 901-999, 53-25-11
Page 405
Feb 01/07
IAC
R Fairing - Left Access Panels
R Figure 401B/TASK 53-25-11-991-001-B
R
EFF :
101-199, 53-25-11
Page 406
Feb 01/07
IAC
R **ON A/C 001-012, 014-019,
(1) Hold the fairing you want to remove. Remove the screws (1) and the
washers (2) and keep them.
R
EFF :
ALL 53-25-11
Page 407
Feb 01/07
IAC
Fairing - Right Access Panels
Figure 402/TASK 53-25-11-991-002
R
EFF :
001-012, 014-019, 53-25-11
Page 408
Feb 01/07
IAC
Fairing - Right Access Panels
Figure 402A/TASK 53-25-11-991-002-A
R
EFF :
020-099, 901-999, 53-25-11
Page 409
Feb 01/07
IAC
R Fairing - Right Access Panels
R Figure 402B/TASK 53-25-11-991-002-B
R
EFF :
101-199, 53-25-11
Page 410
Feb 01/07
IAC
Fairing-Wing to Fuselage - Typical Installation
Figure 403/TASK 53-25-11-991-003
EFF :
ALL 53-25-11
Page 411
Feb 01/07
R
IAC
TASK 53-25-11-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-25-11
Page 412
Feb 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-25-11-869-050
(1) Make sure that the slats are extended (Ref. TASK 27-80-00-866-004).
EFF :
ALL 53-25-11
Page 413
Feb 01/07
IAC
Subtask 53-25-11-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU AIR COND/RAM/AIR/INLET 1HZ D10
106VU CSM/G /EV/MAN/SPLY 6XE B04
Subtask 53-25-11-210-050
(1) Examine the seals on the panels you removed. If necessary, replace
them.
Subtask 53-25-11-110-050
D. Cleaning of Component.
(1) Clean and degrease the washers (2) (to the bare metal) with CLEANING
AGENTS (Material No. 11-003).
EFF :
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Page 414
Feb 01/07
IAC
4. Procedure
_________
Subtask 53-25-11-420-050
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
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Page 415
Feb 01/07
IAC
(3) Temporarily attach the fairings (3) with four screws (1) and washers
(2) at the locating holes (4).
(4) TORQUE the four screws to between 0.20 and 0.25 m.daN (17.69 and
22.12 lbf.in).
(5) Install the remaining screws (1) and washers (2) in position.
(6) Do a visual check to make sure that the seals touch the fuselage
and/or the edges of the wings.
(7) TORQUE all the screws (1) to between 0.35 and 0.45 m.daN (30.97 and
39.82 lbf.in).
5. Close-up
________
Subtask 53-25-11-865-052
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
1HZ, 1HH, 2HH, 3HH, 4HH, 21HH, 22HH, 23HH, 24HH, 6XE
Subtask 53-25-11-942-050
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-25-11
Page 416
Feb 01/07
IAC
SCUFF PLATES - EMERGENCY EXIT DOOR - REMOVAL/INSTALLATION
_________________________________________________________
TASK 53-25-41-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-25-41-941-050
A. Get Access
(2) Open the applicable emergency exit 833 or 843 (Ref. TASK 52-22-00-
010-002).
EFF :
101-199, 53-25-41
Page 401
Feb 01/07
IAC
4. Procedure
_________
Subtask 53-25-41-020-050
CAUTION : MAKE SURE THAT YOU DO NOT DAMAGE THE FUSELAGE WHEN YOU REMOVE
_______
THE SCUFF PLATES.
(1) Remove the screws (1) and (2), and the washers (6).
(2) Remove the sealant between the scuff plates (3), (5) and (9) with a
non metallic scraper.
(3) Remove the screws (8), the nuts (4), and the washers (7) from the
scuff plates (3), (5) and (9).
(4) Blow air on the scuff plates (3), (5) and (9) with a hot air blower.
(5) Carefully put a non metallic wedge between the fuselage and the scuff
plates (3), (5) and (9).
NOTE : If the scuff plates (3), (5) and (9) are damaged, discard
____
them.
EFF :
101-199, 53-25-41
Page 402
Feb 01/07
IAC
FWD Emergency-Exit Scuff-Plate
Figure 401/TASK 53-25-41-991-001
EFF :
101-199, 53-25-41
Page 403
Feb 01/07
IAC
TASK 53-25-41-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
101-199, 53-25-41
Page 404
Feb 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-25-41-869-050
(2) Make sure that the applicable emergency exit door is open.
Subtask 53-25-41-110-050
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1) Clean the contact surfaces of the scuff plates and the fuselage skin
with CLEANING AGENTS (Material No. 11-003) and MISCELLANEOUS
(Material No. 19-003).
(2) Make sure that the parts retained from the removed component are
clean and in the correct condition.
EFF :
101-199, 53-25-41
Page 405
Feb 01/07
IAC
(4) Put the vacuum equipment adjacent to the required emergency exit.
NOTE : We recommend that you use a strong vacuum pump for attachment
____
of the scuff plates.
4. Procedure
_________
Subtask 53-25-41-420-050
NOTE : This procedure is applicable only when you install new scuff
____
plates.
(a) Put the scuff plates (3), (5) and (9) in position on the door
sill.
(b) Drill the attachment hole of the scuff plates to the final
diameter of 4.8 mm (0.1889 in.).
(c) Remove and deburr the scuff plates (3), (5) and (9).
(2) Make the top coat of the scuff plates (3), (5) and (9) rough with
scotch brite on an area of:
- 15 mm (0.5905 in.) width on the scuff plate periphery,
- 20 mm (0.7874 in.) radius around each fastener hole.
(3) Clean the rough area with CLEANING AGENTS (Material No. 11-003) and
MISCELLANEOUS (Material No. 19-003).
(4) Apply adhesive tape on the rough area of the scuff plates.
(5) Apply a thin layer of SPECIAL MATERIALS (Material No. 05-013A) to the
remaining inner areas of the scuff plates (3), (5) and (9).
(6) Remove the adhesive tape from the scuff plates (3), (5) and (9).
(8) Put the scuff plates (3), (5) and (9) in position on the fuselage
skin.
EFF :
101-199, 53-25-41
Page 406
Feb 01/07
IAC
(9) Install the screws (2), (8) and (1) with SEALANTS (Material No. 09-
016), the washers (7) and (6) and the nuts (4).
(10) Tighten the nuts (4) and the screws (1), (2) and (8).
(11) Remove unwanted sealant around the scuff plates (3), (5) and (9).
(13) Cover the scuff plates (3), (5) and (9) with a sheet of porous
material.
(14) Attach the porous material with BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-065) to the scuff plates (3), (5) and (9).
(15) Connect the vacuum valve to the SPECIAL MATERIALS (Material No. 05-
068).
(16) Cover the scuff plates (3), (5) and (9) and SEALANTS (Material No.
09-030) with SPECIAL MATERIALS (Material No. 05-068). You must make
an overlap of 30 mm (1.2 in.) from the edge of SEALANTS (Material No.
09-030).
(18) Operate the vacuum pump to extract the air from the scuff plates (3),
(5) and (9).
Refer to the temperature given in the table:
-------------------------------------------------------------------------------
TEMPERATURE TIME
-------------------------------------------------------------------------------
EFF :
101-199, 53-25-41
Page 407
Feb 01/07
IAC
Scuff Plates - Installation Procedure
Figure 402/TASK 53-25-41-991-002- 12 (SHEET 1)
EFF :
101-199, 53-25-41
Page 408
Feb 01/07
IAC
Scuff Plates - Installation Procedure
Figure 402/TASK 53-25-41-991-002- 22 (SHEET 2)
EFF :
101-199, 53-25-41
Page 409
Feb 01/07
IAC
(21) Remove the vacuum valve from the SPECIAL MATERIALS (Material No. 05-
068), the porous material, and SEALANTS (Material No. 09-030).
(22) Apply SEALANTS (Material No. 09-016) on the external joints of the
scuff plates (3), (5) and (9) and around the scuff plates.
(23) Remove unwanted sealant with CLEANING AGENTS (Material No. 11-003)
AND MISCELLANEOUS (Material No. 19-003).
5. Close-up
________
Subtask 53-25-41-942-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
101-199, 53-25-41
Page 410
Feb 01/07
IAC
MISCELLANEOUS (EG : DRAINS) - DESCRIPTION AND OPERATION
_______________________________________________________
1. _______
General
Drains are installed in the forward fuselage structure of the aircraft at or
near to the lowest points in an area. The drains let water and condensation
drain out so that they do not cause corrosion.
2. Description
___________
Drain valves are installed in the forward fuselage shell. When the cabin
pressurizes, the valves, preset to operate when cabin pressurization reaches
2 psi (0.1378 bar) , close to prevent loss of cabin pressure. As the cabin
pressure decreases below the preset value (normally after the aircraft has
landed), the valves open (under spring tension) to allow any water that has
collected to drain away. You can remove the drain valves, for inspection or
replacement, with an allen key from outside the aircraft.
In other structural components (doors, door frames, stringers, brackets and
fittings) holes are drilled at the lowest points to make sure that water and
condensation drain to the drain valves.
EFF :
ALL 53-29-00
Page 1
Feb 01/07
IAC
Forward Fuselage - Drains
Figure 001
R
EFF :
001-012, 014-099, 101-199, 53-29-00
Page 2
Feb 01/07
IAC
Forward Fuselage - Drains
Figure 001A
R
EFF :
901-999, 53-29-00
Page 3
Feb 01/07
IAC
DRAINS - FORWARD FUSELAGE - REMOVAL/INSTALLATION
________________________________________________
TASK 53-29-41-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-29-41
Page 401
Feb 01/07
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-29-41-861-050
Subtask 53-29-41-010-050
B. Get Access
(2) Open the FWD cargo-compartment door 825 (Ref. TASK 52-30-00-860-001).
(4) In the FWD cargo compartment, remove the applicable floor panel
(Ref. TASK 53-22-14-000-001)
4. Procedure
_________
Subtask 53-29-41-020-050
(2) Remove the nut (1), the screws (3) and the retainers (4).
EFF :
ALL 53-29-41
Page 402
Feb 01/07
IAC
Drain Valve
Figure 401/TASK 53-29-41-991-001
R
EFF :
001-012, 014-099, 101-199, 53-29-41
Page 403
Feb 01/07
IAC
Drain Valve
Figure 401A/TASK 53-29-41-991-001-A
R
EFF :
901-999, 53-29-41
Page 404
Feb 01/07
IAC
TASK 53-29-41-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-29-41
Page 405
May 01/06
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-29-41-860-050
(1) Make sure that the aircraft electrical circuits are energized.
(Ref. TASK 24-41-00-861-002).
EFF :
ALL 53-29-41
Page 406
Feb 01/07
IAC
Subtask 53-29-41-010-052
B. Get Access
(1) Make sure that the access platform is in position at the FWD
cargo-compartment door 825.
(2) Make sure that the FWD cargo-compartment door 825 is open (Ref. TASK
52-30-00-860-001).
(3) Make sure that the CARGO COMPT LIGHT switch 6LU is at ON.
(4) In the FWD cargo compartment, make sure that the applicable floor
panel is removed (Ref. TASK 53-22-14-000-001).
Subtask 53-29-41-110-050
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1) With a SCRAPER - NON METALLIC, remove the old sealant from the
contact surfaces of the retainer and of the structure.
(2) Clean the contact surfaces of the retaining valve and the structure
with CLEANING AGENTS (Material No. 11-003) and a lint-free cloth
MISCELLANEOUS (Material No. 19-003).
(3) Make sure that the parts retained from the removed component are
clean and in the correct condition.
EFF :
ALL 53-29-41
Page 407
May 01/06
R
IAC
4. Procedure
_________
Subtask 53-29-41-420-050
(1) Apply SEALANTS (Material No. 09-016) on the contact surfaces of the
retainer (2) and of the structure.
(3) Apply SEALANTS (Material No. 09-013) on the shank of the screws (3).
(6) Remove the unwanted sealant with CLEANING AGENTS (Material No. 11-
003) and a lint-free cloth MISCELLANEOUS (Material No. 19-003), if
necessary.
(7) Apply a bead of SEALANTS (Material No. 09-016) at the edge of the
structure and of the retainer (2).
(10) Apply SEALANTS (Material No. 09-019) on the contact surface of the
valve (4) and the strucure
EFF :
ALL 53-29-41
Page 408
Feb 01/07
IAC
5. Close-up
________
Subtask 53-29-41-410-050
A. Installation of Components
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 53-29-41-410-051
B. Close Access
(2) Close the FWD cargo-compartemnt door 825 (Ref. TASK 52-30-00-860-
002).
Subtask 53-29-41-862-050
EFF :
ALL 53-29-41
Page 409
May 01/06
IAC
CENTER FUSELAGE - DESCRIPTION AND OPERATION
___________________________________________
1. _______
General
The aircraft center fuselage contains the wing-to-fuselage interface section
and part of the passenger compartment. The area below the passenger
compartment is unpressurized.
2. __________________
Component Location
3. Description
___________
The aircraft center fuselage extends from FR35 to FR47 and includes:
- the wing center box. This structure extends across the width of the
fuselage and is a continuation of the wing cantilever box. The two primary
frames for the fuselage, FR36 and FR42, are also part of the wing
center-box structure,
- the main landing-gear bay, installed between FR42 and FR46,
- the belly fairing primary-structure, installed on the exterior of the
center-fuselage lower section. This structure is an extension to the
fuselage and gives easy access to the air conditioning and hydraulic
services equipment,
- a keel beam to keep the longitudinal structural continuity of the lower
fuselage and to transmit the fuselage bending loads. The beam is installed
between FR35 and FR46. It is attached to the bottom of both frames and the
wing center-box structure. The main landing-gear inner-door fittings are
attached to the keel beam,
EFF :
ALL 53-30-00
Page 1
Feb 01/07
IAC
Center Fuselage - Component Location
Figure 001
R
EFF :
001-012, 014-099, 53-30-00
Page 2
May 01/06
IAC
R Center Fuselage - Component Location
R Figure 001A
EFF :
101-199, 53-30-00
Page 3
Feb 01/07
IAC
Center Fuselage - Component Location
R Figure 001B
R
EFF :
901-999, 53-30-00
Page 4
Feb 01/07
IAC
- a zone pressure limit-structure. The limit includes the top skin panel of
the wing center-box section and two adjacent diaphragms. The forward
diaphragm extends from FR35 to the wing box. The rear diaphragm extends
from the wing box to FR46. Pressure limit bulkheads are installed in the
wing-box front spar and in the lower part of FR35 and FR46,
- the center fuselage shell, which is made of skin-panels, frames, stringers
and skin stiffeners,
- the passenger-compartment floor structure, made of longitudinal beams,
seat and support tracks, support struts and floor panels.
R The aircraft center fuselage extends from FR35.8 to FR47 and includes:
R - the wing center box. This structure extends across the width of the
R fuselage and is a continuation of the wing cantilever box. The two primary
R frames for the fuselage, FR36 and FR42, are also part of the wing
R center-box structure,
R - the main landing-gear bay, installed between FR42 and FR46,
R - the belly fairing primary-structure, installed on the exterior of the
R center-fuselage lower section. This structure is an extension to the
R fuselage and gives easy access to the air conditioning and hydraulic
R services equipment,
R - a keel beam to keep the longitudinal structural continuity of the lower
R fuselage and to transmit the fuselage bending loads. The beam is installed
R between FR35.8 and FR46. It is attached to the bottom of both frames and
R the wing center-box structure. The main landing-gear inner-door fittings
R are attached to the keel beam,
R - a zone pressure limit-structure. The limit includes the top skin panel of
R the wing center-box section and two adjacent diaphragms. The forward
R diaphragm extends from FR35.8 to the wing box. The rear diaphragm extends
R from the wing box to FR46. Pressure limit bulkheads are installed in the
R wing-box front spar and in the lower part of FR35.8 and FR46,
R - the center fuselage shell, which is made of skin-panels, frames, stringers
R and skin stiffeners,
R - the passenger-compartment floor structure, made of longitudinal beams,
R seat and support tracks, support struts and floor panels.
The aircraft center fuselage extends from FR35 to FR47/51 and includes:
- the wing center box. This structure extends across the width of the
fuselage and is a continuation of the wing cantilever box. The two primary
frames for the fuselage, FR36 and FR42, are also part of the wing
center-box structure,
- the main landing-gear bay, installed between FR42 and FR46,
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Page 5
Feb 01/07
IAC
- the belly fairing primary-structure, installed on the exterior of the
center-fuselage lower section. This structure is an extension to the
fuselage and gives easy access to the air conditioning and hydraulic
services equipment,
- a keel beam to keep the longitudinal structural continuity of the lower
fuselage and to transmit the fuselage bending loads. The beam is installed
between FR35 and FR46. It is attached to the bottom of both frames and the
wing center-box structure. The main landing-gear inner-door fittings are
attached to the keel beam,
- a zone pressure limit-structure. The limit includes the top skin panel of
the wing center-box section and two adjacent diaphragms. The forward
diaphragm extends from FR35 to the wing box. The rear diaphragm extends
from the wing box to FR46. Pressure limit bulkheads are installed in the
wing-box front spar and in the lower part of FR35 and FR46,
- the center fuselage shell, which is made of skin-panels, frames, stringers
and skin stiffeners,
- the passenger-compartment floor structure, made of longitudinal beams,
seat and support tracks, support struts and floor panels.
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901-999, 53-30-00
Page 6
Feb 01/07
IAC
MAIN STRUCTURE - DESCRIPTION AND OPERATION
__________________________________________
1. _______
General
The center fuselage main-structure includes:
- the wing center box which makes the wing-to-fuselage joint and is
installed in the lower center-fuselage shell,
- the belly fairing structure installed on the lower exterior of the
fuselage shell,
- skin panels which make the outer skin of the fuselage shell,
- frames which are the stiffeners around the fuselage shell,
- stringers and skin stiffeners to make the skin stronger,
- floor and pressure-limit structures. The floor structure makes the
passenger compartment floor above the wing center box and the main-landing
gear bay pressure limit-zone. The pressure limit structure makes a
diaphragm between the upper (pressurized) and lower (unpressurized) areas
of the center fuselage,
- seat tracks for the installation of the passenger compartment seats.
2. Description
___________
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Wing Center Box - Component Location
Figure 001
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Feb 01/96
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B. Belly Fairing
The belly fairing is installed on the exterior of the lower center
fuselage. The structure is an extension to the fuselage and gives easy
access to the air conditioning and hydraulic services equipment Ref. Task
53-35-00.
C. Center Fuselage
The center fuselage is constructed of:
- frames which give the shape and rigidity to the semi-monocoque
structure,
- skin panels preformed to the contour of the fuselage and riveted to the
frames to make the fuselage shell,
- stringers and skin stiffeners to make the fuselage skin stronger,
- floor structures to hold the passenger compartment floor above the
pressure limit zone.
(1) Frames
(Ref. Fig. 002)
Frames are the circular stiffeners around the fuselage shell. All but
the two primary wing box frames are made of aluminum-alloy sections.
The top part of each frame is formed from sheet and the lower part is
machined from plate. The two wing box frames, FR36 and FR42, are
machined from forgings. Clips, with cutouts for stringers, are
riveted between the frames and the skin panels. The center fuselage
is constructed of the following frames:
- FR35. A full ring frame which makes the joint between the forward
and center fuselage. The forward pressure limit bulkhead is
installed in the lower part of this frame. The keel beam also
connects to the bottom of the frame,
- FR36. This is the forward primary frame of the wing-to-fuselage
joint and is part of the wing box assembly. The frame is made of
two forged sections which are machined and installed back-to-back.
The longer of the two sections extends to STGR1; the shorter
section extends to STGR18. The frame is connected to the wing-box
front spar,
- FR37 thru FR41. Five frames which are connected to the left and
right external attach points of the wing box root-ribs. FR38 and
FR39, FR40 and FR41 are installed at irregular distances to the
other center section frames. These frames give the structural
strength to the two emergency exit openings found above the wing on
each side,
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Center Fuselage - Frame and Skin Panel Location
Figure 002
R
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001-012, 014-099, 53-31-00
Page 4
May 01/06
IAC
- FR42. This is the rear primary frame of the wing-to-fuselage joint
and is part of the wing box assembly. The frame, almost the same as
FR36, is two forged sections which are machined and installed
back-to-back. The longer of the two sections extends to STGR1; the
shorter section extends to STGR11. The frame is connected to the
wing box rear spar,
- FR43 thru FR45. These frames go around the shell and connect with
the side box assemblies (left and right) and extend into the main
landing-gear bay. Two slanting frames connect with the frame ends
on each side to shape and strengthen the landing-gear wheel
openings,
- FR46. The rear pressure-limit bulkhead is installed in the lower
part of this frame. The bulkhead completes the pressure limit zone
of the center fuselage and makes the rear wall of the main
landing-gear bay. The bulkhead slopes to the rear at the bottom to
give the necessary wheel retraction area in the main landing-gear
bay. The keel beam connects to the bottom of the frame,
- FR47. A full ring frame which makes the joint between the center
and rear fuselage sections.
R
EFF :
001-012, 014-099, 53-31-00
Page 5
May 01/06
IAC
the wing leading edge. You can get access to both forward lower
side panels from behind the belly fairing structure,
- a rear lower side-panel, left and right. The panels surround the
wheel openings of the main landing-gear bay aft of the wing
centerbox structure. They are installed between FR42 and FR47 and
span between the middle side panel and keel beam structure. Two
slanting frames (connected together at one end to make an inverted
V-shape) support and strengthen each panel at the edges of the
wheel opening. The panels are chemically milled and stringers are
riveted on their outer face. You can get access to both rear lower
side panels from behind the belly fairing structure.
(b) The skin stiffeners make the skin stronger. They are riveted to
the skin in areas of high stress (fuselage section and skin panel
joints, cabin windows, emergency exits and door openings). Skin
stiffeners are chemically milled or machined from forgings.
R (1) Frames
R (Ref. Fig. 002A)
R Frames are the circular stiffeners around the fuselage shell. All but
R the two primary wing box frames are made of aluminum-alloy sections.
R The top part of each frame is formed from sheet and the lower part is
R machined from plate. The two wing box frames, FR36 and FR42, are
R machined from forgings. Clips, with cutouts for stringers, are
R riveted between the frames and the skin panels. The center fuselage
R is constructed of the following frames:
R - FR35.8. A full ring frame which makes the joint between the forward
R and center fuselage. The forward pressure limit bulkhead is
R installed in the lower part of this frame. The keel beam also
R connects to the bottom of the frame,
R - FR36. This is the forward primary frame of the wing-to-fuselage
R joint and is part of the wing box assembly. The frame is made of
R two forged sections which are machined and installed back-to-back.
R The longer of the two sections extends to STGR1; the shorter
R section extends to STGR18. The frame is connected to the wing-box
R front spar,
R
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R Center Fuselage - Frame and Skin Panel Location
R Figure 002A
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101-199, 53-31-00
Page 7
Feb 01/07
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R - FR37 thru FR41. Five frames which are connected to the left and
R right external attach points of the wing box root-ribs. These
R frames add to the structural strength of the center fuselage above
R the wing on each side,
R - FR42. This is the rear primary frame of the wing-to-fuselage joint
R and is part of the wing box assembly. The frame, almost the same as
R FR36, is two forged sections which are machined and installed
R back-to-back. The longer of the two sections extends to STGR1; the
R shorter section extends to STGR11. The frame is connected to the
R wing box rear spar,
R - FR43 thru FR45. These frames go around the shell and connect with
R the side box assemblies (left and right) and extend into the main
R landing-gear bay. Two slanting frames connect with the frame ends
R on each side to shape and strengthen the landing-gear wheel
R openings,
R - FR46. The rear pressure-limit bulkhead is installed in the lower
R part of this frame. The bulkhead completes the pressure limit zone
R of the center fuselage and makes the rear wall of the main
R landing-gear bay. The bulkhead slopes to the rear at the bottom to
R give the necessary wheel retraction area in the main landing-gear
R bay. The keel beam connects to the bottom of the frame,
R - FR47. A full ring frame which makes the joint between the center
R and rear fuselage sections.
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Page 8
Feb 01/07
IAC
R contains openings for systems interface between the fuselage and
R the wing leading edge. You can get access to both forward lower
R side panels from behind the belly fairing structure,
R - a rear lower side-panel, left and right. The panels surround the
R wheel openings of the main landing-gear bay aft of the wing
R centerbox structure. They are installed between FR42 and FR47 and
R span between the middle side panel and keel beam structure. Two
R slanting frames (connected together at one end to make an inverted
R V-shape) support and strengthen each panel at the edges of the
R wheel opening. The panels are chemically milled and stringers are
R riveted on their outer face. You can get access to both rear lower
R side panels from behind the belly fairing structure.
R (b) The skin stiffeners make the skin stronger. They are riveted to
R the skin in areas of high stress (fuselage section and skin panel
R joints, cabin windows, emergency exits and door openings). Skin
R stiffeners are chemically milled or machined from forgings.
(1) Frames
R (Ref. Fig. 002B)
Frames are the circular stiffeners around the fuselage shell. All but
the two primary wing box frames are made of aluminum-alloy sections.
The top part of each frame is formed from sheet and the lower part is
machined from plate. The two wing box frames, FR36 and FR42, are
machined from forgings. Clips, with cutouts for stringers, are
riveted between the frames and the skin panels. The center fuselage
is constructed of the following frames:
- FR35. A full ring frame which makes the joint between the forward
and center fuselage. The forward pressure limit bulkhead is
installed in the lower part of this frame. The keel beam also
connects to the bottom of the frame,
- FR36. This is the forward primary frame of the wing-to-fuselage
joint and is part of the wing box assembly. The frame is made of
two forged sections which are machined and installed back-to-back.
The longer of the two sections extends to STGR1; the shorter
section extends to STGR18. The frame is connected to the wing-box
front spar,
R
EFF :
101-199, 901-999, 53-31-00
Page 9
Feb 01/07
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Center Fuselage - Frame and Skin Panel Location
R Figure 002B
R
EFF :
901-999, 53-31-00
Page 10
Feb 01/07
IAC
- FR37 thru FR41. Five frames which are connected to the left and
right external attach points of the wing box root-ribs. These
frames add to the structural strength of the center fuselage and
emergency exit opening installed above the wing on each side,
- FR42. This is the rear primary frame of the wing-to-fuselage joint
and is part of the wing box assembly. The frame, almost the same as
FR36, is two forged sections which are machined and installed
back-to-back. The longer of the two sections extends to STGR1; the
shorter section extends to STGR11. The frame is connected to the
wing box rear spar,
- FR43 thru FR45. These frames go around the shell and connect with
the side box assemblies (left and right) and extend into the main
landing-gear bay. Two slanting frames connect with the frame ends
on each side to shape and strengthen the landing-gear wheel
openings,
- FR46. The rear pressure-limit bulkhead is installed in the lower
part of this frame. The bulkhead completes the pressure limit zone
of the center fuselage and makes the rear wall of the main
landing-gear bay. The bulkhead slopes to the rear at the bottom to
give the necessary wheel retraction area in the main landing-gear
bay. The keel beam connects to the bottom of the frame,
- FR47/51. A full ring frame which makes the joint between the center
and rear fuselage sections.
R
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901-999, 53-31-00
Page 11
Feb 01/07
IAC
- a forward lower side panel, left and right, installed in front of
the wing center box between FR35 and FR36. Each panel, complete
with stringers on the outer face, is chemically milled. The panel
contains openings for systems interface between the fuselage and
the wing leading edge. You can get access to both forward lower
side panels from behind the belly fairing structure,
- a rear lower side-panel, left and right. The panels surround the
wheel openings of the main landing-gear bay aft of the wing
centerbox structure. They are installed between FR42 and FR47/51
and span between the middle side panel and keel beam structure. Two
slanting frames (connected together at one end to make an inverted
V-shape) support and strengthen each panel at the edges of the
wheel opening. The panels are chemically milled and stringers are
riveted on their outer face. You can get access to both rear lower
side panels from behind the belly fairing structure.
(b) The skin stiffeners make the skin stronger. They are riveted to
the skin in areas of high stress (fuselage section and skin panel
joints, cabin windows, emergency exits and door openings). Skin
stiffeners are chemically milled or machined from forgings.
R
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901-999, 53-31-00
Page 12
Feb 01/07
IAC
**ON A/C 001-012, 014-099,
R
EFF :
001-012, 014-099, 53-31-00
Page 13
Feb 01/07
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Center Fuselage - Floor Structure
Figure 003
EFF :
001-012, 014-099, 53-31-00
Page 14
Feb 01/07
IAC
R **ON A/C 101-199,
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101-199, 53-31-00
Page 15
Feb 01/07
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R Center Fuselage - Floor Structure
R Figure 003A
EFF :
101-199, 53-31-00
Page 16
Feb 01/07
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R **ON A/C 901-999,
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901-999, 53-31-00
Page 17
Feb 01/07
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Center Fuselage - Floor Structure
R Figure 003B
EFF :
901-999, 53-31-00
Page 18
Feb 01/07
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MAIN STRUCTURE - INSPECTION/CHECK
_________________________________
TASK 53-31-00-210-002
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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Page 601
Nov 01/01
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3. __________
Job Set-up
Subtask 53-31-00-010-051
A. Get Access
(2) Depressurize the Green, Blue and Yellow hydraulic systems (Ref. TASK
29-10-00-864-001), (Ref. TASK 29-10-00-864-002), (Ref. TASK 29-10-00-
864-003).
(3) Put the warning notice in position to tell persons not to operate the
landing gear.
(5) Carefully clean the forward face of the pressure bulkhead at FR46
with CLEANING AGENTS (Material No. 11-002) and a lint-free cloth.
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R
IAC
Subtask 53-31-00-865-050
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R
49VU L/G/LGCIU/SYS1/NORM 1GA C09
121VU HYDRAULIC/LGCIU/SYS2 2GA Q35
121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34
4. Procedure
_________
Subtask 53-31-00-210-051
A. Inspection
(1) Examine the forward face of the pressure bulkhead at FR46 for cracks.
5. Close-up
________
Subtask 53-31-00-865-051
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
1GA, 2GA, 52GA.
Subtask 53-31-00-410-051
B. Close Access
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Page 603
Aug 01/06
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Pressure Bulkhead FR46
Figure 601/TASK 53-31-00-991-003
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Page 604
Feb 01/96
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(3) Remove the access platform(s).
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
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Page 605
May 01/06
R
IAC
TASK 53-31-00-210-003
Detailed Visual Inspection of MLG Bay Fuselage Side Panels inside MLG Bay,
between FR42 and FR46, including Slanted Frames and Side Box, LH/RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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3. __________
Job Set-up
Subtask 53-31-00-010-052
A. Get Access
(2) Depressurize the Green, Blue and Yellow hydraulic systems (Ref. TASK
29-10-00-864-001), (Ref. TASK 29-10-00-864-002), (Ref. TASK 29-10-00-
864-003).
(3) Put the warning notice in position to tell persons not to operate the
landing gear.
(5) Carefully clean the inboard face of the MLG bay side-panels with
CLEANING AGENTS (Material No. 11-002) and a lint-free cloth .
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IAC
Subtask 53-31-00-865-052
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R
49VU L/G/LGCIU/SYS1/NORM 1GA C09
121VU HYDRAULIC/LGCIU/SYS2 2GA Q35
121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34
4. Procedure
_________
Subtask 53-31-00-210-052
A. Inspection:
(1) Examine the inboard face of the MLG bay side-panels, slanted frames
and side boxes between FR42 and FR46 for:
- cracks,
- corrosion,
5. Close-up
________
Subtask 53-31-00-865-053
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
1GA, 2GA, 52GA.
Subtask 53-31-00-410-052
B. Close Access
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Inboard Face of the MLG Bay Side-Panels
Figure 602/TASK 53-31-00-991-004
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(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
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Page 610
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R
IAC
TASK 53-31-00-210-004
Detailed Visual Inspection of MLG Bay Fuselage Side Panels, Outboard Face,
between FR42 and FR47, from STGR26 to STGR36, LH/RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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IAC
3. __________
Job Set-up
Subtask 53-31-00-010-053
A. Get Access
(2) Depressurize the Green, Blue and Yellow hydraulic systems (Ref. TASK
29-10-00-864-001), (Ref. TASK 29-10-00-864-002), (Ref. TASK 29-10-00-
864-003).
(3) Put the warning notice in position to tell persons not to operate the
flight controls.
(5) Remove the access panels 191ET, 193AT, 192ET, 194AT (Ref. TASK 53-35-
11-000-001).
(6) Clean the outboard face of the MLG bay side-panels with CLEANING
AGENTS (Material No. 11-002) and a lint-free cloth .
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Subtask 53-31-00-865-054
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R
49VU L/G/LGCIU/SYS1/NORM 1GA C09
121VU HYDRAULIC/LGCIU/SYS2 2GA Q35
121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34
4. Procedure
_________
Subtask 53-31-00-210-053
A. Inspection
(1) Examine the outboard face of the MLG bay side-panels between FR42
thru FR47 and from STGR26 thru STGR36 for cracks.
5. Close-up
________
Subtask 53-31-00-865-055
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
1GA, 2GA, 52GA.
Subtask 53-31-00-410-053
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the access panels 191ET, 193AT, 192ET, 194AT (Ref. TASK 53-
35-11-400-001).
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Outboard Face of the MLG Bay Side-Panels
Figure 603/TASK 53-31-00-991-005
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May 01/06
R
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(4) Close the MLG doors (Ref. TASK 32-12-00-410-001).
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
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IAC
TASK 53-31-00-210-005
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 616
May 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-31-00-010-054
A. Get Access
(1) Remove the following floor panels 241JF, 241KF, 241LF, 241MF, 242KF,
242LF, 242MF (Ref. TASK 53-32-12-000-002).
(3) Remove the necessary cabin air supply ducts installed above the floor
structure between FR42 and FR46 (Ref. TASK 21-20-00-010-001).
(4) Clean the inspection area with CLEANING AGENTS (Material No. 11-002)
and a lint-free cloth .
4. Procedure
_________
Subtask 53-31-00-210-054
(1) Examine the pressure deck membranes (upper surfaces) and the side
boxes with the connections to the longitudinal beams and support ribs
from FR42 thru FR46 for cracks.
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Upper Surface of the Pressure Deck Membranes and the Side Boxes
Figure 604/TASK 53-31-00-991-006
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5. Close-up
________
Subtask 53-31-00-410-054
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the cabin air supply ducts removed to gain access to the
floor structure between FR42 and FR46 (Ref. TASK 21-20-00-410-001).
(4) Install the following floor panels 241JF, 241KF, 241LF, 241MF, 242KF,
242LF, 242MF (Ref. TASK 53-32-12-400-002).
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page 619
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IAC
TASK 53-31-00-210-006
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page 620
May 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-31-00-010-055
A. Get Access
(2) Depressurize the Green, Blue and Yellow hydraulic systems (Ref. TASK
29-10-00-864-001), (Ref. TASK 29-10-00-864-002), (Ref. TASK 29-10-00-
864-003).
(3) Put the warning notice in position to tell persons not to operate the
landing gear.
(5) Carefully clean the lower surface of the pressure deck with CLEANING
AGENTS (Material No. 11-002) and a lint-free cloth .
EFF :
ALL 53-31-00
Page 621
May 01/06
R
IAC
Subtask 53-31-00-865-056
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R
49VU L/G/LGCIU/SYS1/NORM 1GA C09
121VU HYDRAULIC/LGCIU/SYS2 2GA Q35
121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34
4. Procedure
_________
Subtask 53-31-00-210-055
A. Inspection
(1) Examine the lower surface of the pressure deck membranes between FR42
thru FR46 with the connections to the longitudinal beams, side boxes,
support ribs, rear spar of the wing box and the pressure bulkhead,
LH/RH for:
- cracks,
- corrosion,
5. Close-up
________
Subtask 53-31-00-865-057
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
1GA, 2GA, 52GA.
Subtask 53-31-00-410-055
B. Close Access
EFF :
ALL 53-31-00
Page 622
Aug 01/06
IAC
Lower Surface of the Pressure Deck Membranes
Figure 605/TASK 53-31-00-991-007
EFF :
ALL 53-31-00
Page 623
May 01/06
R
IAC
(3) Remove the access platform(s).
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page 624
Aug 01/06
R
IAC
TASK 53-31-00-210-007
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page 625
May 01/06
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-865-058
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R
49VU L/G/LGCIU/SYS1/NORM 1GA C09
121VU HYDRAULIC/LGCIU/SYS2 2GA Q35
121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34
EFF :
ALL 53-31-00
Page 626
Aug 01/06
IAC
R **ON A/C 001-012, 014-099,
Subtask 53-31-00-010-056
B. Get Access
(2) Depressurize the Green, Blue and Yellow hydraulic systems (Ref. TASK
29-10-00-864-001), (Ref. TASK 29-10-00-864-002), (Ref. TASK 29-10-00-
864-003).
(3) Put the warning notice in position to tell persons not to operate the
landing gear.
(5) Remove the access panels 147AB, 147BB, 147EB, 147FB, 148DB, 148FB,
191GB, 191HB, 191JB, 191KB, 192KB, 195AB and 196AB (Ref. TASK 53-35-
11-000-001), (Ref. TASK 53-35-13-000-001), (Ref. TASK 53-35-13-000-
002).
(6) Clean the keelbeam box with CLEANING AGENTS (Material No. 11-002) and
a lint-free cloth.
EFF :
001-012, 014-099, 53-31-00
Page 627
Aug 01/06
IAC
R **ON A/C 101-199, 901-999,
Subtask 53-31-00-010-056-A
B. Get Access
(2) Depressurize the Green, Blue and Yellow hydraulic systems (Ref. TASK
29-10-00-864-001), (Ref. TASK 29-10-00-864-002), (Ref. TASK 29-10-00-
864-003).
(3) Put the warning notice in position to tell persons not to operate the
landing gear.
(5) Remove the access panels 147AB, 147BB, 147EB, 147FB, 148DB, 148FB,
191BB, 191GB, 191HB, 191JB, 191KB, 192KB, 195AB and 196AB (Ref. TASK
53-35-11-000-001), (Ref. TASK 53-35-13-000-001), (Ref. TASK 53-35-13-
000-002).
(6) Clean the keelbeam box with CLEANING AGENTS (Material No. 11-002) and
a lint-free cloth.
R
EFF :
101-199, 901-999, 53-31-00
Page 628
Feb 01/07
IAC
**ON A/C ALL
4. Procedure
_________
Subtask 53-31-00-210-056
A. Inspection
(1) Examine the keelbeam box between FR35 thru FR47 for corrosion.
R Subtask 53-31-00-210-056-B
R A. Inspection
R (1) Examine the keelbeam box between FR35.8 thru FR47 for corrosion.
Subtask 53-31-00-210-056-A
A. Inspection
(1) Examine the keelbeam box between FR35 thru FR47/51 for corrosion.
EFF :
ALL 53-31-00
Page 629
Feb 01/07
IAC
Keelbeam Box
Figure 606/TASK 53-31-00-991-008
EFF :
ALL 53-31-00
Page 630
May 01/06
R
IAC
**ON A/C ALL
5. Close-up
________
Subtask 53-31-00-916-055
Subtask 53-31-00-865-059
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
1GA, 2GA, 52GA.
Subtask 53-31-00-410-056
C. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the access panels 147AB, 147BB, 147EB, 147FB, 148DB, 148FB,
191GB, 191HB, 191JB, 191KB, 192KB, 195AB and 196AB (Ref. TASK 53-35-
11-400-001), (Ref. TASK 53-35-13-400-001), (Ref. TASK 53-35-13-400-
002).
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page 631
Feb 01/07
R
IAC
R **ON A/C 101-199, 901-999,
Subtask 53-31-00-410-056-A
C. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the access panels 147AB, 147BB, 147EB, 147FB, 148DB, 148FB,
191BB, 191GB, 191HB, 191JB, 191KB, 192KB, 195AB and 196AB (Ref. TASK
53-35-11-400-001), (Ref. TASK 53-35-13-400-001), (Ref. TASK 53-35-13-
400-002).
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
101-199, 901-999, 53-31-00
Page 632
Feb 01/07
IAC
**ON A/C ALL
TASK 53-31-00-210-008
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page 633
Feb 01/07
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-010-058
A. Get Access
(4) Remove the AFT cargo-compartment partitions 151AW, 151BW and 152BW
(Ref. TASK 25-55-11-000-001).
(5) Remove the insulation blankets from the aft face of the pressure
bulkhead (Ref. TASK 25-80-00-000-001).
(6) Cleaning.
EFF :
ALL 53-31-00
Page 634
Feb 01/07
IAC
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______
MATERIALS ONLY WITH A GOOD SUPPLY OF AIR.
OBEY THE MANUFACTURERS INSTRUCTIONS.
PUT ON PROTECTIVE CLOTHING.
DO NOT GET THEM IN YOUR MOUTH.
DO NOT SMOKE.
DO NOT BREATHE THE GAS.
THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT.
GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
(a) Clean the aft face of the pressure bulkhead and the vertical
beams with CLEANING AGENTS (Material No. 11-002) and a lint-free
cloth.
4. Procedure
_________
Subtask 53-31-00-210-057
A. Inspection
(1) Examine the AFT face of the pressure bulkhead at FR46 and the
vertical beams above the AFT cargo-compartment floor level for:
- cracks,
- corrosion.
5. Close-up
________
Subtask 53-31-00-916-056
Subtask 53-31-00-410-058
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-31-00
Page 635
Feb 01/07
R
IAC
Aft Face of the Pressure Bulkhead and Vertical Beams at FR46
Figure 607/TASK 53-31-00-991-009
EFF :
ALL 53-31-00
Page 636
Feb 01/07
R
IAC
(3) Install the partitions 151AW, 151BW and 152BW (Ref. TASK 25-55-11-
400-001).
(4) If removed, install the additional center tank(s) (Ref. AMM 28-11-27,
Page Block 401).
(7) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page 637
Feb 01/07
R
IAC
**ON A/C 001-012, 014-099, 901-999,
TASK 53-31-00-210-009
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
R A. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
001-012, 014-099, 901-999, 53-31-00
Page 638
Feb 01/08
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-010-059
A. Get Access
R (2) Remove the sidewall panels 241CW, 241LW, 242CW, 242LW (Ref. TASK 25-
R 23-47-000-002).
(3) Remove the cove light panels above the emergency exits (Ref. TASK 25-
23-48-000-001).
(4) Remove the riser duct and the cabin air outlet assembly from both
sides of the cabin, between FR37 and FR41 (Ref. TASK 21-20-00-010-
001).
EFF :
001-012, 014-099, 901-999, 53-31-00
Page 639
Feb 01/08
IAC
(5) Remove the necessary insulation blankets from the inspection area
(Ref. TASK 25-80-00-000-001).
R
R (6) Clean the inspection area with the CLEANING AGENTS (Material No. 11-
R 026) and a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
Subtask 53-31-00-010-059-A
A. Get Access
R (2) Remove the sidewall panels 241FW, 242FW (Ref. TASK 25-23-47-000-002).
(3) Remove the cove light panels above the emergency exits (Ref. TASK 25-
23-48-000-001).
(4) Remove the riser duct and the cabin air outlet assembly from both
sides of the cabin, between FR39 and FR41 (Ref. TASK 21-20-00-010-
001).
(5) Remove the necessary insulation blankets from the inspection area
(Ref. TASK 25-80-00-000-001).
R
R (6) Clean the inspection area with the CLEANING AGENTS (Material No. 11-
R 026) and a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
4. Procedure
_________
EFF :
001-012, 014-099, 901-999, 53-31-00
Page 640
Feb 01/08
IAC
Emergency-Exit Hatch Cutouts and Adjacent Structure
Figure 608/TASK 53-31-00-991-010
R
EFF :
001-012, 014-099, 53-31-00
Page 641
Feb 01/08
IAC
INTENTIONALLY BLANK
R
53-31-00
Page 642
Feb 01/08
IAC
Emergency-Exit Hatch Cutouts and Adjacent Structure
Figure 608A/TASK 53-31-00-991-010-A
R
EFF :
901-999, 53-31-00
Page 643
Feb 01/07
IAC
**ON A/C 001-012, 014-099,
Subtask 53-31-00-210-058
Subtask 53-31-00-210-058-A
5. Close-up
________
Subtask 53-31-00-916-057
R
EFF :
001-012, 014-099, 901-999, 53-31-00
Page 644
Feb 01/07
IAC
**ON A/C 001-012, 014-099,
Subtask 53-31-00-410-059
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the riser duct and cabin air outlet assembly (Ref. TASK 21-
20-00-410-001).
R (5) Install the sidewall panels 241CW, 241LW, 242CW, 242LW (Ref. TASK 25-
R 23-47-400-002).
(7) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 53-31-00-410-059-A
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the riser duct and cabin air outlet assembly (Ref. TASK 21-
20-00-410-001).
R (5) Install the sidewall panels 241FW, 242FW (Ref. TASK 25-23-47-400-
R 002).
(7) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
001-012, 014-099, 901-999, 53-31-00
Page 645
Feb 01/08
IAC
R **ON A/C ALL
TASK 53-31-00-210-010
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page 646
May 01/06
IAC
3. __________
Job Set-up
Subtask 53-31-00-010-060
A. Get Access
(2) Clean the area around the anticollision light cutout with CLEANING
AGENTS (Material No. 11-003) and a lint-free cloth.
4. Procedure
_________
Subtask 53-31-00-210-059
A. Inspection:
(1) Examine the area around the anti-collision light cutout between FR40
and FR41 and STGR1 LH to STGR1 RH for:
- corrosion,
- cracks.
EFF :
ALL 53-31-00
Page 647
May 01/06
R
IAC
Anti Collision Light Cutout
Figure 609/TASK 53-31-00-991-011
R
EFF :
ALL 53-31-00
Page 648
May 01/06
IAC
5. Close-up
________
Subtask 53-31-00-410-060
A. Close Access
(2) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page 649
May 01/06
R
IAC
TASK 53-31-00-210-011
Detailed Visual Inspection of Skin around ADF-1 Antenna Cutout, between FR44
and FR45 and between Stringer 1, LH/RH, External Surface
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page 650
May 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-31-00-010-061
A. Get Access
(2) Clean the area around the ADF1 antenna 3RP1 cutout with CLEANING
AGENTS (Material No. 11-003) and a lint-free cloth.
4. Procedure
_________
Subtask 53-31-00-210-060
A. Inspection:
(1) Examine the area between the fuselage external skin around the ADF1
antenna cutout between FR44 and FR45 and STRG1 LH/RH for:
- corrosion,
- cracks,
EFF :
ALL 53-31-00
Page 651
May 01/06
R
IAC
Skin Cutout of the ADF1 Antenna 3RP1
Figure 610/TASK 53-31-00-991-012
EFF :
ALL 53-31-00
Page 652
May 01/06
R
IAC
5. Close-up
________
Subtask 53-31-00-410-061
A. Close Access
(2) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page 653
May 01/06
R
IAC
TASK 53-31-00-210-012
Detailed Visual Inspection of Pressure Bulkhead FWD Face and the Pressure Deck
Upper Surface, including connections to Center Wing Box
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page 654
Feb 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page 655
Feb 01/07
IAC
R **ON A/C ALL
3. __________
Job Set-up
Subtask 53-31-00-010-062
A. Get Access
R (2) Put the ACCESS PLATFORM 2M (6 FT) in position below the cargo door.
(4) Remove the insulation blankets from the inspection area (Ref. TASK
25-80-00-000-001).
R (6) Remove the lower part of the mixer unit (Ref. TASK 21-21-43-000-002).
Subtask 53-31-00-010-062-A
A. Get Access
R (2) Put the ACCESS PLATFORM 2M (6 FT) in position below the cargo door.
(3) Remove the potable water tank 3000 MM (Ref. TASK 38-11-41-000-001).
R (4) Remove the forward cargo-compartment partition 131PW (Ref. TASK 25-
54-12-000-001).
(5) Remove the insulation blankets from the inspection area (Ref. TASK
25-80-00-000-001).
EFF :
ALL 53-31-00
Page 656
Feb 01/07
IAC
R (7) Remove the lower part of the mixer unit (Ref. TASK 21-21-43-000-002).
Subtask 53-31-00-110-059
B. Cleaning
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-002)
and a lint-free cloth.
4. Procedure
_________
EFF :
ALL 53-31-00
Page 657
Feb 01/07
IAC
Forward Face of the Pressure Bulkhead FR35
Figure 611/TASK 53-31-00-991-013
R
EFF :
001-012, 014-099, 901-999, 53-31-00
Page 658
Feb 01/07
IAC
R Inspection Areas of the Pressure Bulkhead and the Pressure Deck
R Figure 611A/TASK 53-31-00-991-013-A
R
EFF :
101-199, 53-31-00
Page 659
Feb 01/07
IAC
R **ON A/C 001-012, 014-099, 901-999,
Subtask 53-31-00-210-061
A. Inspection:
(1) Examine the forward face of the pressure bulkhead at FR35 and the
upper surface of the pressure deck between FR35 and FR36, and the
connections to the center wing box, for:
R - Cracks
R - Corrosion.
R Subtask 53-31-00-210-061-A
R A. Inspection:
R (1) Examine the forward face of the pressure bulkhead at FR35.8 and the
R upper surface of the pressure deck between FR35.8 and FR36, and the
R connections to the center wing box, for:
R - Cracks
R - Corrosion.
5. Close-up
________
Subtask 53-31-00-916-059
EFF :
ALL 53-31-00
Page 660
Feb 01/07
IAC
R **ON A/C 001-012, 014-019, 101-199,
Subtask 53-31-00-410-067
B. Close Access
R (3) Install the lower part of the mixer unit (Ref. TASK 21-21-43-400-
R 003).
(4) Install the partitions 131NW, 131PW, 132PW (Ref. TASK 25-54-12-400-
001).
(7) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 53-31-00-410-067-A
B. Close Access
R (3) Install the lower part of the mixer unit (Ref. TASK 21-21-43-400-
R 003).
(5) Install the potable water tank 3000 MM (Ref. TASK 38-11-41-400-002).
EFF :
ALL 53-31-00
Page 661
Feb 01/07
IAC
(8) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
020-099, 901-999, 53-31-00
Page 662
Feb 01/07
IAC
**ON A/C ALL
TASK 53-31-00-210-013
Detailed Visual Inspection of Pressure Bulkhead AFT Face and the Lower Skin of
Pressure Deck Lower Surface
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page 663
Feb 01/07
R
IAC
3. __________
Job Set-up
Subtask 53-31-00-010-066
A. Get Access
(1) Remove the wing-to-fuselage panels 191BB, 191EB, 192EB and 192FB
(Ref. TASK 53-25-11-000-001).
(2) Clean the inspection area with CLEANING AGENTS (Material No. 11-002)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-31-00-210-062
A. Inspection:
(1) Examine the AFT face of the pressure bulkhead at FR35 and the skin of
the pressure deck lower surface, between FR35 and FR36, for:
- cracks,
- corrosion,
EFF :
ALL 53-31-00
Page 664
Feb 01/07
IAC
Pressure Bulkhead Aft-Face FR35 and Pressure Deck Lower-Face FR35 to FR36
Figure 612/TASK 53-31-00-991-014
EFF :
ALL 53-31-00
Page 665
Feb 01/07
R
IAC
R **ON A/C 101-199,
R Subtask 53-31-00-210-062-A
R A. Inspection:
R (1) Examine the AFT face of the pressure bulkhead at FR35.8 and the skin
R of the pressure deck lower surface, between FR35.8 and FR36, for:
R - cracks,
R - corrosion,
5. Close-up
________
Subtask 53-31-00-410-062
A. Close Access
(1) Install the wing-to-fuselage panels 191BB, 191EB, 192EB and 192FB
(Ref. TASK 53-25-11-400-001).
(2) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page 666
Feb 01/07
IAC
TASK 53-31-00-210-014
Detailed Visual Inspection of Hinge and Actuator Fittings for MLG Doors at
Keelbeam
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
Material No. 15-005 AIB TN 10138 TYPE I GRADE 2
CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND
(Ref. 20-31-00)
Material No. 15-006 AIB TN 10138 TYPE I GRADE 3
CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND
(Ref. 20-31-00)
R
EFF :
ALL 53-31-00
Page 667
Aug 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page 668
Aug 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-010-067
A. Get Access
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE
_______
LANDING GEAR.
R (2) Make sure that the ground lock-sleeve is installed on the applicable
R MLG door actuator-cylinder (Ref. TASK 32-00-00-481-002).
R (3) Depressurize the Green, Blue and Yellow hydraulic systems (Ref. TASK
R 29-10-00-864-001), (Ref. TASK 29-10-00-864-002) and (Ref. TASK 29-10-
00-864-003).
R (4) Put the WARNING NOTICE in position to tell persons not to operate the
landing gear.
EFF :
ALL 53-31-00
Page 669
Aug 01/07
IAC
4. Procedure
_________
R
EFF :
ALL 53-31-00
Page 670
Aug 01/07
IAC
R Inspection areas of the Hinge Fittings and the Actuator Fitting of the MLG Door
R Figure 613/TASK 53-31-00-991-074
R
EFF :
001-012, 014-099, 53-31-00
Page 671
Aug 01/07
IAC
R Inspection areas of the Hinge Fittings and the Actuator Fitting of the MLG Door
R Figure 613A/TASK 53-31-00-991-074-A
R
EFF :
101-199, 53-31-00
Page 672
Aug 01/07
IAC
R Inspection areas of the Hinge Fittings and the Actuator Fitting of the MLG Door
R Figure 613B/TASK 53-31-00-991-074-B
R
EFF :
901-999, 53-31-00
Page 673
Aug 01/07
IAC
Inspection of the Keel Beam Hinge Fittings
Figure 614/TASK 53-31-00-991-072-A
R
EFF :
001-012, 014-099, 53-31-00
Page 674
Aug 01/07
IAC
Inspection of the Keel Beam Hinge Fittings
Figure 614A/TASK 53-31-00-991-072
R
EFF :
101-199, 901-999, 53-31-00
Page 675
Aug 01/07
IAC
Inspection of the Keel Beam Actuator-Hinge Fittings
Figure 615/TASK 53-31-00-991-073-A
R
EFF :
001-012, 014-099, 53-31-00
Page 676
Aug 01/07
IAC
Inspection of the Keel Beam Actuator-Hinge Fittings
Figure 615A/TASK 53-31-00-991-073
R
EFF :
101-199, 901-999, 53-31-00
Page 677
Aug 01/07
IAC
**ON A/C 001-012, 014-099,
Subtask 53-31-00-210-063-A
R A. Inspection
R
R (a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
R damage.
R (3) Make sure the MLG door forward and aft hinges are installed and
R adjusted correctly. Make sure that the spacer and a maximum of two
R shim washers are installed (Ref. TASK 32-12-11-400-001).
R (4) Measure and record the dimension A between the washer and the
R keelbeam hinge-fitting.
R
EFF :
001-012, 014-099, 53-31-00
Page 678
Aug 01/07
IAC
R (6) If damage has been found:
R (a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
R damage.
R (7) Make sure the MLG door actuator and the spacer are installed and
R adjusted correctly (Ref. TASK 32-31-35-400-001).
R (8) Measure and record the dimension B between the washer and the
R actuator-fitting.
R
Subtask 53-31-00-210-063
R A. Inspection
R (1) Do a detailed inspection of the keelbeam MLG door forward and aft
R hinge-fittings, LH/RH. Do a check for corrosion, fretting and wear on
R the items that follow:
R - The hinge-fitting
R - The bearing
R - The spacers
R - Around the head of the bolt.
R
R (a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
R damage.
EFF :
ALL 53-31-00
Page 679
Aug 01/07
IAC
R (b) If you find corrosion damage:
R - Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
R corrosion data
R - Refer to the AMM (Ref. AMM 51-74-11-300-001) for the repair of
R the corroded areas.
R (3) Make sure the MLG door forward and aft hinges are installed and
R adjusted correctly. Make sure that the spacer and a maximum of two
R shim washers are installed (Ref. TASK 32-12-11-400-001).
R
R (4) Measure and record the dimension A between the washer and the
R keelbeam hinge-fitting.
R
R (a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
R damage.
R
EFF :
101-199, 901-999, 53-31-00
Page 680
Aug 01/07
IAC
R (7) Make sure the MLG door actuator and the spacer are installed and
R adjusted correctly (Ref. TASK 32-31-35-400-001).
R
R (8) Measure and record the dimension B between the washer and the
R actuator-fitting.
R
5. Close-up
________
Subtask 53-31-00-916-061
Subtask 53-31-00-410-063
B. Close Access
(2) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page 681
Aug 01/07
IAC
TASK 53-31-00-210-015
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page 682
Aug 01/07
R
IAC
3. __________
Job Set-up
Subtask 53-31-00-010-071
A. Get Access
(2) Clean the inspection area with the CLEANING AGENTS (Material No. 11-
026) and a clean lint free cloth MISCELLANEOUS (Material No. 19-003).
4. Procedure
_________
Subtask 53-31-00-210-064
A. Inspection
(1) Examine the lower skin of the longitudinal lap joints in the crack
stopper area between FR35 thru FR47, LH/RH external surface, for
cracks.
Subtask 53-31-00-210-064-A
A. Inspection
(1) Examine the lower skin of the longitudinal lap joints in the crack
stopper area between FR35.8 thru FR47, LH/RH external surface, for
cracks.
EFF :
ALL 53-31-00
Page 683
Aug 01/07
R
IAC
Lap Joint FR35 thru FR47
Figure 616/TASK 53-31-00-991-016
R
EFF :
ALL 53-31-00
Page 684
Aug 01/07
IAC
**ON A/C ALL
5. Close-up
________
Subtask 53-31-00-410-069
A. Close Access
(2) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
ALL 53-31-00
Page 685
Aug 01/07
IAC
**ON A/C 001-012, 014-099, 901-999,
TASK 53-31-00-210-016
Detailed Visual Inspection of the Emergency Exit Skin Cutouts, Upper and Lower
Corners, LH/RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
001-012, 014-099, 901-999, 53-31-00
Page 686
Aug 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-010-068
A. Get Access
(2) Clean the inspection area with CLEANING AGENTS (Material No. 11-002)
and a lint-free cloth where necessary.
4. Procedure
_________
EFF :
001-012, 014-099, 901-999, 53-31-00
Page 687
Aug 01/07
R
IAC
Upper and Lower Corners of the Emergency Exit Hatch-Cutouts
Figure 617/TASK 53-31-00-991-017
R
EFF :
001-012, 014-099, 53-31-00
Page 688
Aug 01/07
IAC
**ON A/C 901-999,
Subtask 53-31-00-210-066
A. Inspection
(1) Examine the skin cutouts at the upper and lower corners of the
emergency exit hatches for:
- cracks,
- corrosion,
5. Close-up
________
Subtask 53-31-00-410-064
A. Close Access
(2) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
001-012, 014-099, 901-999, 53-31-00
Page 689
Aug 01/07
IAC
Upper and Lower Corners of the Emergency Exit Hatch-Cutouts
Figure 617A/TASK 53-31-00-991-017-A
R
EFF :
901-999, 53-31-00
Page 690
Aug 01/07
IAC
**ON A/C ALL
TASK 53-31-00-210-018
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page 691
Aug 01/07
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-010-072
A. Get Access
(1) Put the warning notice in position to tell persons not to operate the
flight controls.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(3) Clean the inspection area with CLEANING AGENTS (Material No. 11-002)
and a lint-free cloth.
R
EFF :
ALL 53-31-00
Page 692
Aug 01/07
IAC
4. Procedure
_________
Subtask 53-31-00-210-067
A. Inspection
(1) Examine the external surface of the skin in the areas of the
circumferential splice and stringer coupling at FR35, from STGR10 to
the crown centerline, for cracks.
Subtask 53-31-00-210-067-A
A. Inspection
(1) Examine the external surface of the skin in the areas of the
circumferential splices and the stringer couplings at FR35 and
FR35.8. Do this from STGR10 LH/RH to the crown centerline.
R
EFF :
ALL 53-31-00
Page 693
Aug 01/07
IAC
Circumferential Skin Splice at FR35
Figure 618/TASK 53-31-00-991-018
R
EFF :
001-012, 014-099, 901-999, 53-31-00
Page 694
Aug 01/07
IAC
Circumferential Skin Splices at FR35 and FR35.8
Figure 618A/TASK 53-31-00-991-018-A
R
EFF :
101-199, 53-31-00
Page 695
Aug 01/07
IAC
**ON A/C ALL
5. Close-up
________
Subtask 53-31-00-410-070
A. Close Access
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page 696
Aug 01/07
R
IAC
TASK 53-31-00-210-019
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page 697
Aug 01/07
R
IAC
3. __________
Job Set-up
Subtask 53-31-00-010-073
A. Get Access
(1) Put the WARNING NOTICE in position to tell persons not to operate the
flight controls.
(3) Clean the inspection area with the CLEANING AGENTS (Material No. 11-
026) and a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
4. Procedure
_________
Subtask 53-31-00-210-068
A. Inspection
5. Close-up
________
Subtask 53-31-00-410-071
A. Close Access
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page 698
Aug 01/07
R
IAC
Circumferential Skin Splice at FR47
Figure 619/TASK 53-31-00-991-019
EFF :
ALL 53-31-00
Page 699
Aug 01/07
R
IAC
TASK 53-31-00-210-020
Detailed Visual Inspection of Visible Part of Window Forgings and Fuselage Skin
in Window Forging Area, between FR35 and FR47/54 LH/RH, External Surface
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page A600
Aug 01/07
R
IAC
3. __________
Job Set-up
Subtask 53-31-00-010-074
A. Get Access
(1) Put the warning notice in position to tell persons not to operate the
flight controls.
(3) Carefully clean the window forgings with CLEANING AGENTS (Material
No. 11-002) and a lint-free cloth.
4. Procedure
_________
Subtask 53-31-00-210-069
A. Inspection
(1) Examine the external surface of the window forgings and the fuselage
skin in the window forging area between FR35 thru FR47, for cracks.
Subtask 53-31-00-210-069-B
A. Inspection
(1) Examine the external surface of the window forgings and the fuselage
skin in the window forging area between FR35.8 thru FR47, for cracks.
EFF :
ALL 53-31-00
Page A601
Aug 01/07
R
IAC
Window Forgings FR35 thru FR47
Figure 620/TASK 53-31-00-991-020
EFF :
ALL 53-31-00
Page A602
Aug 01/07
R
IAC
Window Forgings - Permitted Damage
Figure 621/TASK 53-31-00-991-023
EFF :
ALL 53-31-00
Page A603
Aug 01/07
R
IAC
**ON A/C 901-999,
Subtask 53-31-00-210-069-A
A. Inspection
(1) Examine the external surface of the window forgings and the fuselage
skin in the window forging area between FR35 thru FR47/51, for
cracks.
5. Close-up
________
Subtask 53-31-00-410-072
A. Close Access
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page A604
Aug 01/07
R
IAC
TASK 53-31-00-210-023
General Visual Inspection of Main Landing Gear Bay including Main Landing Gear
Door Hinges
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page A605
Aug 01/07
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-010-070
A. Get Access:
(3) Put the warning notice in position to tell persons not to operate the
landing gear.
(4) Put the access platform in position below the main landing-gear bay.
4. Procedure
_________
Subtask 53-31-00-210-071
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
EFF :
ALL 53-31-00
Page A606
Aug 01/07
R
IAC
Area of Inspection in the MLG Bay
Figure 622/TASK 53-31-00-991-024
EFF :
ALL 53-31-00
Page A607
Aug 01/07
R
IAC
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______
MATERIALS ONLY WITH A GOOD SUPPLY OF AIR.
OBEY THE MANUFACTURERS INSTRUCTIONS.
PUT ON PROTECTIVE CLOTHING.
DO NOT GET THEM IN YOUR MOUTH.
DO NOT SMOKE.
DO NOT BREATHE THE GAS.
THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT.
GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
(1) Carefully clean the MLG bay and the MLG door hinges with CLEANING
AGENTS (Material No. 11-002) and a MISCELLANEOUS (Material No. 19-
003).
(2) Do a general visual inspection of the MLG bay including the MLG door
hinges for corrosion and other damage.
5. Close-up
________
Subtask 53-31-00-410-068
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page A608
Aug 01/07
R
IAC
TASK 53-31-00-210-025
Detailed Visual Inspection of Fuselage Skin, between FR35 and FR36 and between
Stringer 25 and Stringer 30, LH/RH, External Surface
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page A609
Aug 01/07
IAC
3. __________
Job Set-up
Subtask 53-31-00-010-082
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(2) Put the warning notice on the slat/flap control lever to tell persons
not to operate the slats.
Subtask 53-31-00-110-076
B. Cleaning Procedure
EFF :
ALL 53-31-00
Page A610
Aug 01/07
IAC
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint free cloth , if necessary. Make sure the area is dry
before you continue.
4. Procedure
_________
Subtask 53-31-00-210-073
EFF :
ALL 53-31-00
Page A611
Aug 01/07
R
IAC
External Surface of Fuselage Skin between FR35 and FR36, and between Stringer
25 and Stringer 30, LH/RH
Figure 623/TASK 53-31-00-991-030
EFF :
ALL
53-31-00 Page A612
Aug 01/07
R
IAC
**ON A/C 101-199,
Subtask 53-31-00-210-073-A
5. Close-up
________
Subtask 53-31-00-410-080
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(7) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page A613
Aug 01/07
IAC
TASK 53-31-00-210-027
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page A614
Aug 01/07
R
IAC
3. __________
Job Set-up
Subtask 53-31-00-861-055
Subtask 53-31-00-010-083
B. Get Access
(1) Remove the necessary upper sidewall panels (Ref. TASK 25-23-43-000-
001).
Subtask 53-31-00-110-072
C. Cleaning Procedure
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint free cloth, if necessary. Make sure the area is dry before
you continue.
EFF :
ALL 53-31-00
Page A615
Aug 01/07
R
IAC
4. Procedure
_________
Subtask 53-31-00-210-074
5. Close-up
________
Subtask 53-31-00-410-081
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 53-31-00-862-055
R
EFF :
ALL 53-31-00
Page A616
Aug 01/07
IAC
Internal Lower Skin of Longitudinal Lap Joint at Stringer 18 LH and RH, in
Runout at FR42
Figure 624/TASK 53-31-00-991-029
R EFF :
ALL
53-31-00 Page A617
Aug 01/07
IAC
**ON A/C 001-012, 014-099, 901-999,
TASK 53-31-00-210-028
Detailed Visual Inspection of Flanges at FR38, 39, 40 and 41, between STGR12 to
STGR21, and Longl Beam FLange at STGR20A, between FR38 to 39, FR40 to 41, LH/RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
001-012, 014-099, 901-999, 53-31-00
Page A618
Aug 01/07
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-861-057
Subtask 53-31-00-010-086
B. Get Access
(1) Remove the sidewall linings 241CW, 241LW, 242CW, 242LW (Ref. TASK 25-
23-47-000-001).
(2) Remove the cove light panels above the emergency exits (Ref. TASK 25-
23-48-000-001).
EFF :
001-012, 014-099, 901-999, 53-31-00
Page A619
Aug 01/07
R
IAC
(3) Remove the riser duct and the cabin air outlet assembly from both
sides of the cabin, between FR37 and FR41 (Ref. TASK 21-20-00-010-
001).
(4) Remove the necessary insulation blankets from the inspection area
(Ref. TASK 25-80-00-000-001).
Subtask 53-31-00-010-086-A
B. Get Access
(1) Remove the sidewall linings 241FW, 242FW (Ref. TASK 25-23-47-000-
001).
(2) Remove the cove light panels above the emergency exits (Ref. TASK 25-
23-48-000-001).
(3) Remove the riser duct and the cabin air outlet assembly from both
sides of the cabin, between FR40 and FR41 (Ref. TASK 21-20-00-010-
001).
(4) Remove the necessary insulation blankets from the inspection area
(Ref. TASK 25-80-00-000-001).
Subtask 53-31-00-110-078
C. Cleaning Procedure
R
EFF :
001-012, 014-099, 901-999, 53-31-00
Page A620
Aug 01/07
IAC
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint free cloth, if necessary. Make sure the area is dry before
you continue.
4. Procedure
_________
Subtask 53-31-00-210-076
EFF :
001-012, 014-099, 901-999, 53-31-00
Page A621
Aug 01/07
R
IAC
Frame Flanges at FR38 thru FR41, between STGR12 and STGR21, and Longitudinal
Beam Flange at STGR20A, between FR38 and FR39, and between FR40 and FR41, LH/RH
Figure 625/TASK 53-31-00-991-033
R EFF :
001-012, 014-099,
53-31-00 Page A622
Aug 01/07
IAC
**ON A/C 901-999,
Subtask 53-31-00-210-076-A
5. Close-up
________
Subtask 53-31-00-410-084
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the riser duct and cabin air outlet assembly (Ref. TASK 21-
20-00-410-001).
(5) Install the sidewall linings 241CW, 241LW, 242CW, 242LW (Ref. TASK
25-23-47-400-001).
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
001-012, 014-099, 901-999, 53-31-00
Page A623
Aug 01/07
R
IAC
Frame Flanges at FR40 and FR41, between STGR12 and STGR21, and Longitudinal
Beam Flange at STGR20A, between FR40 and FR41, LH/RH
Figure 625A/TASK 53-31-00-991-033-A
R EFF :
901-999,
53-31-00 Page A624
Aug 01/07
IAC
**ON A/C 901-999,
Subtask 53-31-00-410-084-A
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the riser duct and cabin air outlet assembly (Ref. TASK 21-
20-00-410-001).
(5) Install the sidewall linings 241FW, 242FW (Ref. TASK 25-23-47-400-
001).
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 53-31-00-862-057
R
EFF :
001-012, 014-099, 901-999, 53-31-00
Page A625
Aug 01/07
IAC
**ON A/C ALL
TASK 53-31-00-210-029
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific flashlight
No specific lint free cloth
No specific warning notice
No specific access platform 1.5 m (4 ft. 11 in.)
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page A626
Aug 01/07
R
IAC
3. __________
Job Set-up
Subtask 53-31-00-010-087
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE
_______
LANDING GEAR.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE LANDING GEAR ARE CLEAR.
_______
(2) Put the warning notice in position to tell persons not to operate the
landing gear.
(3) Put the access platform in position below the MLG compartment.
Subtask 53-31-00-110-079
B. Cleaning Procedure
EFF :
ALL 53-31-00
Page A627
Aug 01/07
R
IAC
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint free cloth , if necessary. Make sure the area is dry
before you continue.
4. Procedure
_________
Subtask 53-31-00-210-077
(1) Do a detailed visual inspection of the side box beam in the area
where it attaches to FR46, LH and RH, for cracks.
5. Close-up
________
Subtask 53-31-00-410-085
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-31-00
Page A628
Aug 01/07
R
IAC
Side Box Beam Attachment Area to FR46, LH/RH
Figure 626/TASK 53-31-00-991-032
EFF :
ALL 53-31-00
Page A629
Aug 01/07
R
IAC
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page A630
Aug 01/07
R
IAC
TASK 53-31-00-210-030
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific flashlight
No specific lint free cloth
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page A631
Aug 01/07
R
IAC
3. __________
Job Set-up
Subtask 53-31-00-861-059-A
Subtask 53-31-00-010-089-A
B. Get Access
(1) Remove the necessary lower sidewall panels between FR42 and FR46
(Ref. TASK 25-23-44-000-001).
(2) Release and carefully pull back the necessary insulation blankets
from the sides of the fuselage, below the floor level, between FR42
and FR46.
(3) Attach them temporarily to the fuselage structure above the floor
level.
Subtask 53-31-00-110-081-A
C. Cleaning Procedure
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
EFF :
ALL 53-31-00
Page A632
Aug 01/07
R
IAC
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint free cloth , if necessary. Make sure the area is dry
before you continue.
4. Procedure
_________
Subtask 53-31-00-210-078-A
5. Close-up
________
Subtask 53-31-00-410-087-A
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Release and fold down the insulation blankets, and attach them in
their initial positions.
(3) Install the lower sidewall panels between FR42 and FR46 (Ref. TASK
25-23-44-400-001).
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 53-31-00-862-059-A
EFF :
ALL 53-31-00
Page A633
Aug 01/07
R
IAC
Frame Attachments to Pressure Floor from FR42 to FR46, LH/RH
Figure 627/TASK 53-31-00-991-034-A
EFF :
ALL 53-31-00
Page A634
Aug 01/07
R
IAC
TASK 53-31-00-220-001
Special Detailed Inspection of Hinge and Actuator Fittings for MLG Doors at
Keelbeam
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-31-00
Page A635
Aug 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-010-069
A. Get Access
Subtask 53-31-00-860-062
R
EFF :
ALL 53-31-00
Page A636
Aug 01/07
IAC
R Inspection Areas of the Hinge Fittings and the Actuator Fitting of the MLG Door
Figure 628/TASK 53-31-00-991-063
R
EFF :
001-012, 014-099, 53-31-00
Page A637
Aug 01/07
IAC
R **ON A/C 101-199,
(1) Make sure that the inspection areas of the hinge and actuator
fittings of the MLG door are:
- Clean and smooth
- Free from paint runs and used sealant.
(2) If necessary, clean the inspection areas with the CLEANING AGENTS
(Material No. 11-026) and a clean lint-free MISCELLANEOUS (Material
No. 19-003). Make sure the inspection areas are dry before you
continue.
(3) If necessary, make the surface of the inspection areas smooth with
the abrasive cloth, grade 280.
(4) Do a visual inspection of the inspection areas. Look for damage and
defects in the condition of the surface.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
damage.
EFF :
ALL 53-31-00
Page A638
Aug 01/07
IAC
R Inspection Areas of the Hinge Fittings and the Actuator Fitting of the MLG Door
R Figure 628A/TASK 53-31-00-991-063-B
R
EFF :
101-199, 53-31-00
Page A639
Aug 01/07
IAC
R Inspection Areas of the Hinge Fittings and the Actuator Fitting of the MLG Door
R Figure 628B/TASK 53-31-00-991-063-C
R
EFF :
901-999, 53-31-00
Page A640
Aug 01/07
IAC
4. Procedure
_________
R Subtask 53-31-00-220-052-A
R (1) If the hinge fittings are painted, before you do the inspection you
R must:
R (a) Refer to the procedure steps in the NTM (Ref. NTM 533154 Part 6),
R Preparation for Inspection.
R (c) Make sure that the paint thickness is less than the given limit.
R (2) Do the special detailed inspection of the keelbeam MLG door center
R hinge-fitting, LH/RH (Ref. NTM 533154 Part 6) and (Ref. NTM 533160
R Part 6).
R (b) If cracks are found, contact AIRBUS for the correct repair
R procedure.
EFF :
ALL 53-31-00
Page A641
Aug 01/07
IAC
R (3) Do the special detailed inspection of the keelbeam MLG door
R actuator-fitting, LH/RH (Ref. NTM 533154 Part 4) and (Ref. NTM 533154
R Part 6) and (Ref. NTM 533160 Part 6).
R (b) If cracks are found, contact AIRBUS for the correct repair
R procedure.
Subtask 53-31-00-220-052
(1) If the hinge fittings are painted, before you do the inspection you
must:
(a) Refer to the procedure steps in the NTM (Ref. NTM 533154 Part 6),
Preparation for Inspection.
(c) Make sure that the paint thickness is less than the given limit.
R (2) Do the special detailed inspection of the keelbeam MLG door forward
R hinge-fitting, LH/RH (Ref. NTM 533154 Part 6) and (Ref. NTM 533160
Part 6).
(b) If cracks are found, contact AIRBUS for the correct repair
procedure.
(b) If cracks are found, contact AIRBUS for the correct repair
procedure.
EFF :
ALL 53-31-00
Page A642
Aug 01/07
IAC
R **ON A/C ALL
5. Close-up
________
Subtask 53-31-00-370-054
(1) If necessary, refer to the ASRM (Ref. ASRM 51-75-12-001) and repair
the paint coating in the inspection areas.
Subtask 53-31-00-410-065
B. Close Access
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
ALL 53-31-00
Page A643
Aug 01/07
IAC
TASK 53-31-00-220-002
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page A644
Aug 01/07
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-010-075
A. Get Access
(1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position below the
inspection area.
Subtask 53-31-00-860-053
(1) Make sure that the surfaces of the inspection areas are clean and
smooth.
(2) If necessary, clean the inspection areas with the CLEANING AGENTS
(Material No. 11-026) and a clean lint free cloth MISCELLANEOUS
(Material No. 19-003). Make sure the inspection areas are dry before
you continue.
(3) If necessary, make the surface of the inspection areas smooth with
the abrasive cloth, grade 280.
(4) Do a visual inspection of the inspection areas. Look for damage and
defects in the shape of the external surface.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
EFF :
ALL 53-31-00
Page A645
Aug 01/07
R
IAC
(c) If you find other types of damage:
- Refer to the ASRM (Ref. ASRM 51-73-00-001) for the repair of
the minor damage.
4. Procedure
_________
Subtask 53-31-00-220-053
(2) Write a report if you find damage during the inspection procedure.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
EFF :
ALL 53-31-00
Page A646
Aug 01/07
R
IAC
**ON A/C 101-199,
Subtask 53-31-00-220-053-B
(2) Write a report if you find damage during the inspection procedure.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
Subtask 53-31-00-220-053-A
(2) Write a report if you find damage during the inspection procedure.
R
EFF :
101-199, 901-999, 53-31-00
Page A647
Aug 01/07
IAC
(3) If you find damage:
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
5. Close-up
________
Subtask 53-31-00-370-051
Subtask 53-31-00-410-073
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page A648
Aug 01/07
R
IAC
TASK 53-31-00-220-003
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page A649
Aug 01/07
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
ASRM 53-31-14-001
NTM 533110-Part.6
ASRM 51-73-00-001 (for corrective action)
ASRM 51-74-00-001 (for corrective action)
ASRM 51-75-12-001 (for corrective action)
53-31-00-991-044 Fig. 629
3. __________
Job Set-up
Subtask 53-31-00-860-054
Subtask 53-31-00-010-080
B. Get Access
(1) Remove the necessary equipment and furnishing to get access to the
cabin floor panels.
(2) Remove the floor panels 241MF, 241LF, 241KF, 241JF, 242KF, 242LF,
242MF (Ref. TASK 53-32-12-000-002).
(3) Disconnect the electrical wire bundles from the floor beams at FR42
and FR43, as necessary, to get access to the inspection area.
Subtask 53-31-00-860-052
(1) Make sure that the surfaces of the inspection areas are clean and
smooth.
EFF :
ALL 53-31-00
Page A650
Aug 01/07
R
IAC
INTENTIONALLY BLANK
R
53-31-00
Page A651
Aug 01/07
IAC
Inspection Areas of Upper Flanges of Floor Beams at FR42 and FR46
Figure 629/TASK 53-31-00-991-044- 12 (SHEET 1)
EFF :
ALL 53-31-00
Page A652
Aug 01/07
R
IAC
Inspection Areas of Upper Flanges of Floor Beams at FR42 and FR46
Figure 629/TASK 53-31-00-991-044- 22 (SHEET 2)
EFF :
ALL 53-31-00
Page A653
Aug 01/07
R
IAC
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR
MOUTH OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10
AND 15 MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS,
FLAMMABLE AND SKIN IRRITANTS.
(2) If necessary, clean the inspection areas with the CLEANING AGENTS
(Material No. 11-004) and a MISCELLANEOUS (Material No. 19-003). Make
sure the areas are dry before you continue.
(3) If necessary, make the surface of the inspection areas smooth with
the abrasive cloth, grade 280.
(4) Make sure that the inspection areas are clean and dry before you
continue.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
EFF :
ALL 53-31-00
Page A654
Aug 01/07
R
IAC
4. Procedure
_________
Subtask 53-31-00-220-055
(b) Do the inspection on the upper and lower surfaces and along the
edges on both sides of the upper flange.
(c) Do the inspection only in the areas of the upper flange that you
can see.
(d) Do not inspect the areas of the upper flange which are below the
seat-track support fittings.
(2) Write a report about the damage you find during the inspection
procedure.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
EFF :
ALL 53-31-00
Page A655
Aug 01/07
R
IAC
(c) If you find other types of damage:
- refer to the ASRM (Ref. ASRM 51-73-00-001) for the repair of
the minor damage
5. Close-up
________
Subtask 53-31-00-370-050
(1) If necessary, refer to the ASRM (Ref. ASRM 51-75-12-001) and repair
the paint coating in the inspection areas.
Subtask 53-31-00-410-078
B. Close Access
(1) Connect the electrical wire bundles to the floor beams at FR42 and
FR43.
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the floor panels 241MF, 241LF, 241KF, 241JF, 242KF, 242LF,
242MF (Ref. TASK 53-32-12-400-002).
(4) Install the equipment and furnishing, removed to get access to the
cabin floor panels.
Subtask 53-31-00-860-055
EFF :
ALL 53-31-00
Page A656
Aug 01/07
R
IAC
TASK 53-31-00-220-004
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page A657
Aug 01/07
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
NTM 533138-Part.6
ASRM 51-73-00-001 (for corrective action)
ASRM 51-74-00-001 (for corrective action)
ASRM 51-75-12-001 (for corrective action)
ASRM 53-31-11-101 (for corrective action)
ASRM 53-31-11-201 (for corrective action)
53-31-00-991-029 Fig. 624
3. __________
Job Set-up
Subtask 53-31-00-860-056
Subtask 53-31-00-010-081
B. Get Access
(1) Remove the necessary upper sidewall panels LH/RH in the area of FR42
and FR43 (Ref. TASK 25-23-43-000-001).
(2) Remove the necessary insulation blankets in the area of STGR18 LH/RH
at FR42 (Ref. TASK 25-80-00-000-001).
Subtask 53-31-00-860-058
(1) Make sure that the surfaces of the inspection areas are clean and
smooth.
EFF :
ALL 53-31-00
Page A658
Aug 01/07
R
IAC
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR
MOUTH OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10
AND 15 MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS,
FLAMMABLE AND SKIN IRRITANTS.
(2) If necessary, clean the inspection areas with the CLEANING AGENTS
(Material No. 11-004) and a MISCELLANEOUS (Material No. 19-003). Make
sure the inspection areas are dry before you continue.
(3) If necessary, make the surface of the inspection areas smooth with
the abrasive cloth, grade 280.
(4) Make sure that the inspection areas are clean and dry before you
continue.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
EFF :
ALL 53-31-00
Page A659
Aug 01/07
R
IAC
4. Procedure
_________
Subtask 53-31-00-220-056
(2) Write a report if you find damage during the inspection procedure.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
EFF :
ALL 53-31-00
Page A660
Aug 01/07
R
IAC
5. Close-up
________
Subtask 53-31-00-370-052
(1) If necessary, refer to the ASRM (Ref. ASRM 51-75-12-001) and repair
the paint coatings in the inspection areas.
Subtask 53-31-00-410-079
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the insulation blankets in the area of STGR18 LH/RH at FR42
(Ref. TASK 25-80-00-400-001).
(3) Install the upper sidewall panels LH/RH in the area of FR42 and FR43
(Ref. TASK 25-23-43-400-001).
Subtask 53-31-00-860-057
EFF :
ALL 53-31-00
Page A661
Aug 01/07
R
IAC
TASK 53-31-00-220-006
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page A662
Aug 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-860-060
(2) Put the warning notice on the slat/flap control lever to tell persons
not to operate the slats.
Subtask 53-31-00-010-084
B. Get Access
Subtask 53-31-00-860-059
(1) Make sure that the outer surface of the inspection area is clean and
smooth.
EFF :
ALL 53-31-00
Page A663
Aug 01/07
IAC
Circumferential Skin Splice at FR47, from STGR10 LH/RH to Crown Centerline
Figure 630/TASK 53-31-00-991-045
EFF :
ALL 53-31-00
Page A664
Aug 01/07
R
IAC
(2) If necessary, clean the outer surface of the inspection area with the
CLEANING AGENTS (Material No. 11-026) and a clean lint-free cloth
MISCELLANEOUS (Material No. 19-003). Make sure the inspection area is
dry before you continue.
(3) If necessary, make the outer surface of the inspection area smooth
with the abrasive cloth, grade 280.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
damage.
4. Procedure
_________
Subtask 53-31-00-220-057
(2) Write a report about the damage you find during the inspection
procedure.
EFF :
ALL 53-31-00
Page A665
Aug 01/07
R
IAC
5. Close-up
________
Subtask 53-31-00-370-053
Subtask 53-31-00-410-082
B. Close Access
Subtask 53-31-00-860-061
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page A666
Aug 01/07
IAC
TASK 53-31-00-220-007
Special Detailed inspection of Keel Beam Box Elliptical Cutout at FR46, LH/RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page A667
Aug 01/07
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
ASRM 53-36-11-001
NTM 511008-Part.6
NTM 533155-Part.6
ASRM 51-73-00-001 (for corrective action)
ASRM 51-74-00-001 (for corrective action)
53-31-00-991-035 Fig. 631
3. __________
Job Set-up
Subtask 53-31-00-010-090
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE
_______
LANDING GEAR.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE LANDING GEAR ARE CLEAR.
_______
(2) Put the warning notice in position to tell persons not to operate the
landing gear.
(3) Put the access platform in position below the MLG compartment.
Subtask 53-31-00-860-063
(1) Make sure that the surfaces of the inspection areas are clean and
smooth.
EFF :
ALL 53-31-00
Page A668
Aug 01/07
R
IAC
Keel Beam Box Elliptical Cutout at FR46, LH/RH
Figure 631/TASK 53-31-00-991-035
EFF :
ALL 53-31-00
Page A669
Aug 01/07
R
IAC
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR
MOUTH OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10
AND 15 MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS,
FLAMMABLE AND SKIN IRRITANTS.
(2) If necessary, clean the inspection areas with the CLEANING AGENTS
(Material No. 11-004) and a MISCELLANEOUS (Material No. 19-003). Make
sure the areas are dry before you continue.
(3) If necessary, make the surface of the inspection areas smooth with
the abrasive cloth, grade 280.
(4) Make sure that the inspection areas are clean and dry before you
continue.
EFF :
ALL 53-31-00
Page A670
Aug 01/07
R
IAC
4. Procedure
_________
Subtask 53-31-00-220-059
(2) Write a report about the damage you find during the inspection
procedure.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
EFF :
ALL 53-31-00
Page A671
Aug 01/07
R
IAC
5. Close-up
________
Subtask 53-31-00-370-055
Subtask 53-31-00-410-088
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page A672
Aug 01/07
R
IAC
TASK 53-31-00-210-031
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-31-00
Page A673
Aug 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-010-092
A. Get Access
(1) Remove the necessary equipment and furnishing to get access to the
cabin floor panels.
(2) Remove the following floor panels 241HF, 241GF, 241FF, 241EF, 242FF,
242GF, 242HF, 241MF, 241LF, 241KF, 241JF, 242KF, 242LF, 242MF
(Ref. TASK 53-32-12-000-002).
(3) Remove the necessary lower sidewall panels between FR36 and FR46
(Ref. TASK 25-23-44-000-001).
(4) Remove the necessary cabin air supply ducts installed above the floor
structure between FR36 and FR46 (Ref. TASK 21-20-00-010-001).
(5) Release and carefully pull back the necessary insulation blankets
from the sides of the fuselage, below the floor level, between FR36
and FR46.
(6) Attach them temporarily to the fuselage structure above the floor
level.
R
EFF :
ALL 53-31-00
Page A674
Aug 01/07
IAC
4. Procedure
_________
Subtask 53-31-00-210-080
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint free cloth. Make sure that the area is dry before you
continue.
(3) If necessary, refer to the ASRM (Ref. ASRM 53-31-14-001) for the
correct repair procedure.
R
EFF :
ALL 53-31-00
Page A675
Aug 01/07
IAC
Fuselage Internal Structure below Cabin Floor Panels, including Cabin Floor
Structure between FR36 and FR46
Figure 632/TASK 53-31-00-991-042
EFF :
ALL
53-31-00 Page A676
Aug 01/07
R
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(4) Apply STORAGE PRESERVATION (Material No. 15-005) or STORAGE
PRESERVATION (Material No. 15-005A) or STORAGE PRESERVATION (Material
No. 15-006) or equivalent to the fuselage internal structure below
the cabin floor panels, including the cabin floor structure between
FR36 and FR46.
5. Close-up
________
Subtask 53-31-00-410-090
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Release and fold down the insulation blankets and attach them in
their initial positions.
(3) Install the cabin air supply ducts, removed to gain access to the
cabin floor structure between FR36 and FR46 (Ref. TASK 21-20-00-410-
001).
(4) Install the lower sidewall panels between FR42 and FR46 (Ref. TASK
25-23-44-400-001).
(5) Install the floor panels 241HF, 241GF, 241FF, 241EF, 242FF, 242GF,
242HF, 241MF, 241LF, 241KF, 241JF, 242KF, 242LF, 242MF (Ref. TASK 53-
32-12-400-002).
(6) Install the equipment and furnishing, removed to get access to the
cabin floor panels.
(7) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
ALL 53-31-00
Page A677
Aug 01/07
IAC
**ON A/C 001-012, 014-099, 901-999,
TASK 53-31-00-210-032
General Visual Inspection of Pressure Bulkhead Aft Face at FR35 and Lower Skin
of Pressure Deck Lower Surface between FR35 and FR36
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
001-012, 014-099, 901-999, 53-31-00
Page A678
Aug 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-010-093
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(2) Put the warning notice on the slat/flap control lever to tell persons
not to operate the slats.
R
EFF :
001-012, 014-099, 901-999, 53-31-00
Page A679
Aug 01/07
IAC
4. Procedure
_________
Subtask 53-31-00-210-081
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint free cloth. Make sure that the area is dry before you
continue.
(3) If necessary, refer to the ASRM (Ref. ASRM 53-31-16-001) and (Ref.
ASRM 53-31-14-001) for the correct repair procedures.
R
EFF :
001-012, 014-099, 901-999, 53-31-00
Page A680
Aug 01/07
IAC
Inspection Areas of the Aft Face of the Pressure Bulkhead and the Bottom
Surface of the Pressure Deck
Figure 633/TASK 53-31-00-991-043
R EFF :
ALL
53-31-00 Page A681
Aug 01/07
IAC
(4) Apply STORAGE PRESERVATION (Material No. 15-005) or STORAGE
PRESERVATION (Material No. 15-005A) or STORAGE PRESERVATION (Material
No. 15-006) or equivalent to the pressure bulkhead AFT face at FR35
and the lower skin of the pressure deck lower surface between FR35
and FR36.
5. Close-up
________
Subtask 53-31-00-410-091
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
001-012, 014-099, 901-999, 53-31-00
Page A682
Aug 01/07
IAC
**ON A/C 101-199,
TASK 53-31-00-210-032-A
General Visual Inspection of Pressure Bulkhead Aft Face at FR35.8 and Lower
Skin of Pressure Deck Lower Surface between FR35.8 and FR36
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
101-199, 53-31-00
Page A683
Aug 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-010-114
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(2) Put the WARNING NOTICE in position on the slat/flap control lever to
tell persons not to operate the flaps/slats.
R
EFF :
101-199, 53-31-00
Page A684
Aug 01/07
IAC
4. Procedure
_________
Subtask 53-31-00-210-098
A. Inspection
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the inspection area with the CLEANING AGENTS (Material No. 11-
026) and a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
Make sure that the area is dry before you continue.
(2) Do a general visual inspection of the items that follow for corrosion
and other damage:
- The pressure bulkhead aft face at FR35.8
- The lower skin of the pressure deck lower surface between FR35.8
and FR36.
R
EFF :
101-199, 53-31-00
Page A685
Aug 01/07
IAC
(3) If you find corrosion damage:
- Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data
- Refer to the AMM (Ref. AMM 51-74-11-300-001) for the repair of the
corroded areas.
(5) Apply the STORAGE PRESERVATION (Material No. 15-005) or the STORAGE
PRESERVATION (Material No. 15-005A) or the STORAGE PRESERVATION
(Material No. 15-006) or equivalent, to:
- The pressure bulkhead aft face at FR35.8
- The lower skin of the pressure deck lower surface between FR35.8
and FR36.
5. Close-up
________
Subtask 53-31-00-410-111
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
101-199, 53-31-00
Page A686
Aug 01/07
IAC
**ON A/C 001-012, 014-099,
TASK 53-31-00-220-009
Special Detailed Inspection of the Frames and the Frame Feet, from FR37 to
FR41, adjacent to STGR23
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
001-012, 014-099, 53-31-00
Page A687
Aug 01/07
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-010-094
A. Get Access
(1) Remove the passenger seats between the FR36 and the FR42 LH and RH
(Ref. TASK 25-21-41-000-001).
(2) Remove the textile floor covering between the FR36 and the FR42 LH
and RH (Ref. TASK 25-28-41-000-001).
EFF :
001-012, 014-099, 53-31-00
Page A688
Aug 01/07
R
IAC
(3) Remove the lower sidewall panels 241AW, 241BW, 241EW, 241KW, 241JW,
241NW, 242AW, 242EW, 242KW, 242JW, 242NW between the FR36 and the
FR42 LH and RH (Ref. TASK 25-23-44-000-001).
(4) Remove the cabin floor panels 241HF, 242HF between the FR36 and the
FR42 LH and RH (Ref. TASK 53-32-12-000-002).
(6) Remove the insulation blankets as necessary between the FR37 and the
FR41 LH and RH (Ref. TASK 25-80-00-000-001).
(7) Remove the emergency power-supply units as necessary between the FR37
and the FR41 LH and RH (Ref. TASK 33-51-38-000-001).
Subtask 53-31-00-860-065
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Make sure that the inspection areas of the frames and frame feets
are:
- clean and smooth
- free from paint runs and used sealant.
(2) If necessary, clean the inspection areas with the CLEANING AGENTS
(Material No. 11-004) and a MISCELLANEOUS (Material No. 19-003). Make
sure the inspection areas are dry before you continue.
EFF :
001-012, 014-099, 53-31-00
Page A689
Aug 01/07
R
IAC
Location and Inspection Area of the Frames and Frame Feet from FR37 to FR41
Figure 634/TASK 53-31-00-991-046- 12 (SHEET 1)
R
EFF :
001-012, 014-099, 53-31-00
Page A690
Aug 01/07
IAC
Location and Inspection Area of the Frames and Frame Feet from FR37 to FR41
Figure 634/TASK 53-31-00-991-046- 22 (SHEET 2)
R
EFF :
001-012, 014-099, 53-31-00
Page A691
Aug 01/07
IAC
(3) If necessary, make the surface of the inspection areas smooth with
the abrasive cloth, grade 280.
(4) Do a visual inspection of the inspection areas. Look for damage and
defects in the condition of the surface.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
4. Procedure
_________
Subtask 53-31-00-220-061
(2) Write a report about the damage you find during the inspection
procedure.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
R
EFF :
001-012, 014-099, 53-31-00
Page A692
Aug 01/07
IAC
(b) If you find corrosion damage:
- refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data
- refer to the ASRM (Ref. ASRM 51-74-00-001) for the repair of
the corroded areas.
(d) If you find damage which is more than the limits for minor
damage:
- refer to the Airbus Industrie (Ref. SB No. 53-1141) for the
necessary corrective action procedure.
5. Close-up
________
Subtask 53-31-00-370-056
Subtask 53-31-00-410-092
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the removed the emergency power-supply units between the FR37
and the FR41 LH and RH (Ref. TASK 33-51-38-400-001).
(3) Install the removed the insulation blankets between the FR37 and the
FR41 LH and RH (Ref. TASK 25-80-00-400-001).
(5) Install the cabin floor panels between the FR36 and the FR42 LH and
RH (Ref. TASK 53-32-12-400-002).
(6) Install the lower sidewall panels 241AW, 241BW, 241EW, 241KW, 241JW,
241NW, 242AW, 242EW, 242KW, 242JW, 242NW between the FR36 and the
FR42 LH and RH (Ref. TASK 25-23-44-400-001).
R
EFF :
001-012, 014-099, 53-31-00
Page A693
Aug 01/07
IAC
(7) Install the textile floor covering between the FR36 and the FR42 LH
and RH (Ref. TASK 25-28-41-400-001).
(8) Install the passenger seats between the FR36 and the FR42 LH and RH
(Ref. TASK 25-21-41-400-001).
R
EFF :
001-012, 014-099, 53-31-00
Page A694
Aug 01/07
IAC
**ON A/C 001-012, 014-019,
TASK 53-31-00-220-011
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
001-012, 014-019, 53-31-00
Page A695
Aug 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-860-072
Subtask 53-31-00-010-104
B. Get Access
(2) Put the WARNING NOTICE on the slat/flap control lever to tell persons
not to operate the slats.
R
EFF :
001-012, 014-019, 53-31-00
Page A696
Aug 01/07
IAC
(3) Put the ACCESS PLATFORM 2M (6 FT) in position at the FWD
cargo-compartment door.
(8) Remove the heat and sound insulation from the area between FR35 and
FR36 above STGR30 LH and RH.
(9) Remove the bleed air duct between FR35 and FR36, STGR30, LH and RH
(Ref. TASK 36-11-48-000-003).
Subtask 53-31-00-110-095
(1) Make sure that the surfaces of the inspection areas are clean.
R
EFF :
001-012, 014-019, 53-31-00
Page A697
Aug 01/07
IAC
4. Procedure
_________
Subtask 53-31-00-220-064
(1) Do the special detailed inspection (Ref. NTM 511001) of the fastener
holes of the pick-up angles between FR35 and FR36 at STGR 30, LH/RH.
(2) Write a report about the damage you find during the inspection
procedure.
NOTE : No repair data is given in the ASRM for the fastener holes of
____
the pick-up angles between FR35 and FR36 at STGR 30, LH/RH.
(3) If the fastener holes are damaged you must contact AIRBUS INDUSTRIE
for the necessary corrective action procedure.
5. Close-up
________
Subtask 53-31-00-410-101
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the bleed air duct between FR35 and FR36, STGR30, LH and RH
(Ref. TASK 36-11-48-400-003).
(3) Install the heat and sound insulation from the area between FR35 and
FR36 above STGR30 LH and RH.
(5) Install the quick release access panels (Ref. TASK 53-35-13-400-002):
- 191BB and 191EB on the left side,
- 192FB and 192EB on the right side.
R
EFF :
001-012, 014-019, 53-31-00
Page A698
Aug 01/07
IAC
Inspection Areas of the LH and RH Pick-up Angle Fasteners
Figure 635/TASK 53-31-00-991-065
R
EFF :
001-012, 014-019, 53-31-00
Page A699
Aug 01/07
IAC
R (7) Remove the LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION
R (98D27803000000) on the slat/flap control lever when working near the
slats/flaps.
(10) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 53-31-00-862-062
R
EFF :
001-012, 014-019, 53-31-00
Page B600
Aug 01/07
IAC
**ON A/C 001-012, 014-099, 901-999,
TASK 53-31-00-210-033
General Visual Inspection of Emergency Exit Skin Cutouts, Upper and Lower
Corners, LH/RH
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
A. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
001-012, 014-099, 901-999, 53-31-00
Page B601
Aug 01/07
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
ASRM 51-23-11-001
ASRM 53-31-11-101
ASRM 53-31-11-201 (for corrective action)
3. __________
Job Set-up
Subtask 53-31-00-010-099
A. Get Access
(1) Remove the LH and the RH emergency-exit hatches (Ref. TASK 52-21-11-
000-001).
Subtask 53-31-00-110-087
(1) Make sure that the surfaces of the inspection areas are clean.
R
EFF :
001-012, 014-099, 901-999, 53-31-00
Page B602
Aug 01/07
IAC
(2) If necessary, clean the inspection areas with a lint-free cotton
cloth, MISCELLANEOUS (Material No. 19-003) and the CLEANING AGENTS
(Material No. 11-002).
4. Procedure
_________
Subtask 53-31-00-210-082
A. Inspection Procedure
(a) Look for scratches, dents, cracks, corrosion and damage to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
(b) Refer to the ASRM (Ref. ASRM 53-31-11-101) for the allowable
damage limits for this structure.
(c) Repair the scratches which are in the limits (Ref. TASK 51-73-11-
300-001) or (Ref. TASK 51-73-11-300-004), as necessary.
(d) Repair the dents which are in the limits (Ref. TASK 51-73-11-300-
003).
(e) For damage that is more than the limits for minor damage, refer
to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data.
R
EFF :
001-012, 014-099, 901-999, 53-31-00
Page B603
Aug 01/07
IAC
Inspection Areas of the Fuselage Cutouts of the Emergency Exits
Figure 636/TASK 53-31-00-991-057
R
EFF :
001-012, 014-099, 53-31-00
Page B604
Aug 01/07
IAC
Inspection Areas of the Fuselage Cutouts of the Emergency Exits
Figure 636A/TASK 53-31-00-991-057-A
R
EFF :
901-999, 53-31-00
Page B605
Aug 01/07
IAC
(3) If you find corrosion:
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint coating of the aircraft.
(b) Repair the damage to the paint system (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
5. Close-up
________
Subtask 53-31-00-410-096
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the LH and the RH emergency-exit hatches (Ref. TASK 52-21-11-
400-001).
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
001-012, 014-099, 901-999, 53-31-00
Page B606
Aug 01/07
IAC
**ON A/C ALL
TASK 53-31-00-210-035
General Visual Inspection of Upper Skin of Longitudinal Lap Joints and Crack
Stopper Areas at STGR6 LH/RH, between FR35 and FR47/54, External Surface
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
R
R Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page B607
May 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-941-063
(1) Put the ACCESS PLATFORM 8M (26 FT) - ADJUSTABLE in position at the
inspection area.
R
EFF :
ALL 53-31-00
Page B608
Aug 01/07
IAC
Subtask 53-31-00-110-089
(1) Make sure that the surfaces of the inspection areas are clean.
4. Procedure
_________
Subtask 53-31-00-210-084
A. Inspection Procedure
(a) Look for scratches, dents, cracks, corrosion and damage to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
damage.
R
EFF :
ALL 53-31-00
Page B609
Aug 01/07
IAC
Inspection Areas of the Center Fuselage Lap-Joint at STGR6, LH/RH
Figure 637/TASK 53-31-00-991-058
R
EFF :
001-012, 014-099, 53-31-00
Page B610
Aug 01/07
IAC
Inspection Areas of the Center Fuselage Lap-Joint at STGR6, LH/RH
Figure 637A/TASK 53-31-00-991-058-B
R
EFF :
101-199, 53-31-00
Page B611
Aug 01/07
IAC
Inspection Areas of the Center Fuselage Lap-Joint at STGR6, LH/RH
Figure 637B/TASK 53-31-00-991-058-A
R
EFF :
901-999, 53-31-00
Page B612
Aug 01/07
IAC
(b) Refer to the ASRM (Ref. ASRM 53-31-11-101) for the permitted
damage limits for this structure.
(c) Repair the scratches which are in the limits (Ref. TASK 51-73-11-
300-001) or (Ref. TASK 51-73-11-300-004), as necessary.
(d) Repair the dents which are in the limits (Ref. TASK 51-73-11-300-
003).
(e) For damage that is more than the limits for minor damage, refer
to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint layers of the aircraft.
(b) Repair the damage to the paint layer(s) (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
Subtask 53-31-00-210-084-B
A. Inspection Procedure
(a) Look for scratches, dents, cracks, corrosion and damage to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
damage.
R
EFF :
001-012, 014-099, 101-199, 53-31-00
Page B613
Aug 01/07
IAC
(b) Refer to the ASRM (Ref. ASRM 53-31-11-101) for the permitted
damage limits for this structure.
(c) Repair the scratches which are in the limits (Ref. TASK 51-73-11-
300-001) or (Ref. TASK 51-73-11-300-004), as necessary.
(d) Repair the dents which are in the limits (Ref. TASK 51-73-11-300-
003).
(e) For damage that is more than the limits for minor damage, refer
to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint layers of the aircraft.
(b) Repair the damage to the paint layer(s) (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
Subtask 53-31-00-210-084-A
A. Inspection Procedure
(a) Look for scratches, dents, cracks, corrosion and damage to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
damage.
R
EFF :
101-199, 901-999, 53-31-00
Page B614
Aug 01/07
IAC
(b) Refer to the ASRM (Ref. ASRM 53-31-11-101) for the permitted
damage limits for this structure.
(c) Repair the scratches which are in the limits (Ref. TASK 51-73-11-
300-001) or (Ref. TASK 51-73-11-300-004), as necessary.
(d) Repair the dents which are in the limits (Ref. TASK 51-73-11-300-
003).
(e) For damage that is more than the limits for minor damage, refer
to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint layers of the aircraft.
(b) Repair the damage to the paint layer(s) (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
5. Close-up
________
Subtask 53-31-00-942-076
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
ALL 53-31-00
Page B615
Aug 01/07
IAC
TASK 53-31-00-210-036
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
R
R Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page B616
May 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-941-064
(1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the
inspection area.
R
EFF :
ALL 53-31-00
Page B617
Aug 01/07
IAC
Subtask 53-31-00-110-090
(1) Make sure that the surfaces of the inspection areas are clean.
4. Procedure
_________
Subtask 53-31-00-210-085
A. Inspection Procedure
(a) Look for scratches, dents, cracks, corrosion and damage to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
damage.
R
EFF :
ALL 53-31-00
Page B618
Aug 01/07
IAC
Inspection Areas of the Center Fuselage Lap-Joint at STGR18, LH/RH
Figure 638/TASK 53-31-00-991-059
R
EFF :
001-012, 014-099, 53-31-00
Page B619
Aug 01/07
IAC
Inspection Areas of the Center Fuselage Lap-Joint at STGR18, LH/RH
Figure 638A/TASK 53-31-00-991-059-B
R
EFF :
101-199, 53-31-00
Page B620
Aug 01/07
IAC
Inspection Areas of the Center Fuselage Lap-Joint at STGR18, LH/RH
Figure 638B/TASK 53-31-00-991-059-A
R
EFF :
901-999, 53-31-00
Page B621
Aug 01/07
IAC
(b) Refer to the ASRM (Ref. ASRM 53-31-11-101) for the permitted
damage limits for this structure.
(c) Repair the scratches which are in the limits (Ref. TASK 51-73-11-
300-001) or (Ref. TASK 51-73-11-300-004), as necessary.
(d) Repair the dents which are in the limits (Ref. TASK 51-73-11-300-
003).
(e) For damage that is more than the limits for minor damage, refer
to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint layers of the aircraft.
(b) Repair the damage to the paint layer(s) (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
Subtask 53-31-00-210-085-B
A. Inspection Procedure
(a) Look for scratches, dents, cracks, corrosion and damage to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
damage.
R
EFF :
001-012, 014-099, 101-199, 53-31-00
Page B622
Aug 01/07
IAC
(b) Refer to the ASRM (Ref. ASRM 53-31-11-101) for the permitted
damage limits for this structure.
(c) Repair the scratches which are in the limits (Ref. TASK 51-73-11-
300-001) or (Ref. TASK 51-73-11-300-004), as necessary.
(d) Repair the dents which are in the limits (Ref. TASK 51-73-11-300-
003).
(e) For damage that is more than the limits for minor damage, refer
to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint layers of the aircraft.
(b) Repair the damage to the paint layer(s) (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
Subtask 53-31-00-210-085-A
A. Inspection Procedure
(a) Look for scratches, dents, cracks, corrosion and damage to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
damage.
R
EFF :
101-199, 901-999, 53-31-00
Page B623
Aug 01/07
IAC
(b) Refer to the ASRM (Ref. ASRM 53-31-11-101) for the permitted
damage limits for this structure.
(c) Repair the scratches which are in the limits (Ref. TASK 51-73-11-
300-001) or (Ref. TASK 51-73-11-300-004), as necessary.
(d) Repair the dents which are in the limits (Ref. TASK 51-73-11-300-
003).
(e) For damage that is more than the limits for minor damage, refer
to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint layers of the aircraft.
(b) Repair the damage to the paint layer(s) (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
5. Close-up
________
Subtask 53-31-00-942-077
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
ALL 53-31-00
Page B624
Aug 01/07
IAC
TASK 53-31-00-210-037
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
R
R Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page B625
May 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-941-065
(1) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position at the
inspection area.
R
EFF :
ALL 53-31-00
Page B626
Aug 01/07
IAC
Subtask 53-31-00-110-091
(1) Make sure that the surfaces of the inspection areas are clean.
4. Procedure
_________
Subtask 53-31-00-210-086
A. Inspection Procedure
(a) Look for scratches, dents, cracks, corrosion and damage to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
damage.
R
EFF :
ALL 53-31-00
Page B627
Aug 01/07
IAC
Inspection Areas of the Center Fuselage Lap-Joint at STGR18, LH/RH
Figure 639/TASK 53-31-00-991-060
R
EFF :
001-012, 014-099, 53-31-00
Page B628
Aug 01/07
IAC
Inspection Areas of the Center Fuselage Lap-Joint at STGR18, LH/RH
Figure 639A/TASK 53-31-00-991-060-B
R
EFF :
101-199, 53-31-00
Page B629
Aug 01/07
IAC
Inspection Areas of the Center Fuselage Lap-Joint at STGR18, LH/RH
Figure 639B/TASK 53-31-00-991-060-A
R
EFF :
901-999, 53-31-00
Page B630
Aug 01/07
IAC
(b) Refer to the ASRM (Ref. ASRM 53-31-11-101) for the permitted
damage limits for this structure.
(c) Repair the scratches which are in the limits (Ref. TASK 51-73-11-
300-001) or (Ref. TASK 51-73-11-300-004), as necessary.
(d) Repair the dents which are in the limits (Ref. TASK 51-73-11-300-
003).
(e) For damage that is more than the limits for minor damage, refer
to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint layers of the aircraft.
(b) Repair the damage to the paint layer(s) (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
Subtask 53-31-00-210-086-B
A. Inspection Procedure
(a) Look for scratches, dents, cracks, corrosion and damage to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
damage.
R
EFF :
001-012, 014-099, 101-199, 53-31-00
Page B631
Aug 01/07
IAC
(b) Refer to the ASRM (Ref. ASRM 53-31-11-101) for the permitted
damage limits for this structure.
(c) Repair the scratches which are in the limits (Ref. TASK 51-73-11-
300-001) or (Ref. TASK 51-73-11-300-004), as necessary.
(d) Repair the dents which are in the limits (Ref. TASK 51-73-11-300-
003).
(e) For damage that is more than the limits for minor damage, refer
to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint layers of the aircraft.
(b) Repair the damage to the paint layer(s) (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
Subtask 53-31-00-210-086-A
A. Inspection Procedure
(a) Look for scratches, dents, cracks, corrosion and damage to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
damage.
R
EFF :
101-199, 901-999, 53-31-00
Page B632
Aug 01/07
IAC
(b) Refer to the ASRM (Ref. ASRM 53-31-11-101) for the permitted
damage limits for this structure.
(c) Repair the scratches which are in the limits (Ref. TASK 51-73-11-
300-001) or (Ref. TASK 51-73-11-300-004), as necessary.
(d) Repair the dents which are in the limits (Ref. TASK 51-73-11-300-
003).
(e) For damage that is more than the limits for minor damage, refer
to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint layers of the aircraft.
(b) Repair the damage to the paint layer(s) (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
5. Close-up
________
Subtask 53-31-00-942-078
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
ALL 53-31-00
Page B633
Aug 01/07
IAC
TASK 53-31-00-210-038
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-31-00
Page B634
Aug 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-941-066
(1) Put the ACCESS PLATFORM 8M (26 FT) - ADJUSTABLE in position at the
inspection area.
R
EFF :
ALL 53-31-00
Page B635
Aug 01/07
IAC
Subtask 53-31-00-110-092
(1) Make sure that the surfaces of the inspection areas are clean.
4. Procedure
_________
R
EFF :
ALL 53-31-00
Page B636
Aug 01/07
IAC
Inspection Areas of the Center Fuselage, from STGR23 LH/RH to Crown Centerline
Figure 640/TASK 53-31-00-991-061
R
EFF :
001-012, 014-099, 53-31-00
Page B637
Aug 01/07
IAC
Inspection Areas of the Center Fuselage, from STGR23 LH/RH to Crown Centerline
Figure 640A/TASK 53-31-00-991-061-B
R
EFF :
101-199, 53-31-00
Page B638
Aug 01/07
IAC
Inspection Areas of the Center Fuselage, from STGR23 LH/RH to Crown Centerline
Figure 640B/TASK 53-31-00-991-061-A
R
EFF :
901-999, 53-31-00
Page B639
Aug 01/07
IAC
**ON A/C 001-012, 014-099,
Subtask 53-31-00-210-087
A. Inspection Procedure
(a) Look for scratches, dents, cracks, corrosion and damage to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
(b) Refer to the ASRM (Ref. ASRM 53-31-11-101) for the allowable
damage limits for this structure.
(c) Repair the scratches which are in the limits (Ref. TASK 51-73-11-
300-001) or (Ref. TASK 51-73-11-300-004), as necessary.
(d) Repair the dents which are in the limits (Ref. TASK 51-73-11-300-
003).
(e) For damage that is more than the limits for minor damage, refer
to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint coating of the aircraft.
R
EFF :
001-012, 014-099, 53-31-00
Page B640
Aug 01/07
IAC
(b) Repair the damage to the paint system (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
Subtask 53-31-00-210-087-B
A. Inspection Procedure
(a) Look for scratches, dents, cracks, corrosion and damage to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
(b) Refer to the ASRM (Ref. ASRM 53-31-11-101) for the allowable
damage limits for this structure.
(c) Repair the scratches which are in the limits (Ref. TASK 51-73-11-
300-001) or (Ref. TASK 51-73-11-300-004), as necessary.
(d) Repair the dents which are in the limits (Ref. TASK 51-73-11-300-
003).
(e) For damage that is more than the limits for minor damage, refer
to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
R
EFF :
001-012, 014-099, 101-199, 53-31-00
Page B641
Aug 01/07
IAC
(4) If you find damage to the surface protection:
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint coating of the aircraft.
(b) Repair the damage to the paint system (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
Subtask 53-31-00-210-087-A
A. Inspection Procedure
(a) Look for scratches, dents, cracks, corrosion and damage to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
(b) Refer to the ASRM (Ref. ASRM 53-31-11-101) for the allowable
damage limits for this structure.
(c) Repair the scratches which are in the limits (Ref. TASK 51-73-11-
300-001) or (Ref. TASK 51-73-11-300-004), as necessary.
(d) Repair the dents which are in the limits (Ref. TASK 51-73-11-300-
003).
(e) For damage that is more than the limits for minor damage, refer
to the ASRM (Ref. ASRM 53-31-11-201) for the correct repair data.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
R
EFF :
101-199, 901-999, 53-31-00
Page B642
Aug 01/07
IAC
(b) Repair the corroded areas (Ref. TASK 51-74-11-300-001) or
(Ref. TASK 51-74-11-300-002), as necessary.
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint coating of the aircraft.
(b) Repair the damage to the paint system (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
5. Close-up
________
Subtask 53-31-00-942-079
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
ALL 53-31-00
Page B643
Aug 01/07
IAC
TASK 53-31-00-210-039
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
A. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-31-00
Page B644
Aug 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
ASRM 51-22-00-001
ASRM 51-23-11-001
3. __________
Job Set-up
Subtask 53-31-00-010-102
A. Get Access
(1) Remove the lower sidewall panels from the inspection areas (Ref. TASK
25-23-44-000-001).
(2) Remove the upper sidewall panels from the inspection areas (Ref. TASK
25-23-43-000-001).
(3) Remove the cove light panels from the inspection areas (Ref. TASK 25-
23-48-000-001).
(4) Remove the ceiling panels from the inspection areas (Ref. TASK 25-23-
41-000-001).
(5) Remove the overhead stowage compartments from the inspection areas
(Ref. TASK 25-24-41-000-001).
R
EFF :
ALL 53-31-00
Page B645
Aug 01/07
IAC
(6) Move sufficient of the insulation blankets away from the structure,
to get access to the inspection areas (Ref. TASK 25-80-00-000-001).
Subtask 53-31-00-110-093
(1) Make sure that the surfaces of the inspection areas are clean.
4. Procedure
_________
R
EFF :
ALL 53-31-00
Page B646
Aug 01/07
IAC
Inspection Areas of the Center Fuselage above Cabin Floor Level
Figure 641/TASK 53-31-00-991-062
R
EFF :
001-012, 014-099, 53-31-00
Page B647
Aug 01/07
IAC
Inspection Areas of the Center Fuselage above Cabin Floor Level
Figure 641A/TASK 53-31-00-991-062-B
R
EFF :
101-199, 53-31-00
Page B648
Aug 01/07
IAC
Inspection Areas of the Center Fuselage above Cabin Floor Level
Figure 641B/TASK 53-31-00-991-062-A
R
EFF :
901-999, 53-31-00
Page B649
Aug 01/07
IAC
**ON A/C 001-012, 014-099,
Subtask 53-31-00-210-088
A. Inspection Procedure
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint coating of the aircraft.
(b) Repair the damage to the paint system (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
Subtask 53-31-00-210-088-B
A. Inspection Procedure
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
R
EFF :
001-012, 014-099, 101-199, 53-31-00
Page B650
Aug 01/07
IAC
(3) If you find damage to the surface protection:
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint coating of the aircraft.
(b) Repair the damage to the paint system (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
Subtask 53-31-00-210-088-A
A. Inspection Procedure
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint coating of the aircraft.
(b) Repair the damage to the paint system (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
R
EFF :
101-199, 901-999, 53-31-00
Page B651
Aug 01/07
IAC
**ON A/C ALL
5. Close-up
________
Subtask 53-31-00-410-099
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(8) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
ALL 53-31-00
Page B652
Aug 01/07
IAC
**ON A/C 001-012, 014-019,
TASK 53-31-00-210-040
Detailed Visual Inspection of the Transition Angle between FR35 and FR36 just
below STGR30, LH/RH
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
001-012, 014-019, 53-31-00
Page B653
Aug 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-860-068
Subtask 53-31-00-010-103
B. Get Access
(2) Put the WARNING NOTICE on the slat/flap control lever to tell persons
not to operate the slats.
(3) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the FWD
cargo-compartment door.
EFF :
001-012, 014-019, 53-31-00
Page B654
Aug 01/07
IAC
(4) Open the FWD cargo-compartment door (Ref. TASK 52-30-00-860-001).
(8) Remove the heat and sound insulation from the area between FR35 and
FR36 above STGR30 LH and RH.
(9) Remove the bleed air duct between FR35 and FR36, STGR30, LH and RH
(Ref. TASK 36-11-48-000-003).
Subtask 53-31-00-110-094
(1) Make sure that the surfaces of the inspection areas are clean.
EFF :
001-012, 014-019, 53-31-00
Page B655
Aug 01/07
R
IAC
4. Procedure
_________
Subtask 53-31-00-210-089
5. Close-up
________
Subtask 53-31-00-410-100
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the bleed air duct between FR35 and FR36, STGR30, LH and RH
(Ref. TASK 36-11-48-400-003).
(3) Install the heat and sound insulation from the area between FR35 and
FR36 above STGR30 LH and RH.
(5) Install the quick release access panels (Ref. TASK 53-35-13-400-002):
- 191BB and 191EB on the left side,
- 192FB and 192EB on the right side.
EFF :
001-012, 014-019, 53-31-00
Page B656
Aug 01/07
IAC
Inspection Areas of the LH/RH Transition Angle
Figure 642/TASK 53-31-00-991-064
EFF :
001-012, 014-019, 53-31-00
Page B657
Aug 01/07
R
IAC
(10) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 53-31-00-862-060
EFF :
001-012, 014-019, 53-31-00
Page B658
Aug 01/07
R
IAC
TASK 53-31-00-210-042
Detailed Inspection of the Outboard Flanges around the Fastner Holes of Frames
38 thru 41, between STGR 12 and STGR 21, LH/RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
A. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-860-070
EFF :
001-012, 014-019, 53-31-00
Page B659
Aug 01/07
IAC
Subtask 53-31-00-010-107
B. Get Access
(2) Remove the thermal and acoustic insulation (Ref. TASK 25-80-00-000-
001).
Subtask 53-31-00-110-098
(1) Make sure that the surfaces of the inspection areas are clean.
4. Procedure
_________
Subtask 53-31-00-210-092
NOTE : No repair data is given in the ASRM for the fastener holes at
____
FR38 thru FR41 between STGR 12 and STGR 21, LH/RH. If the
fastener holes are damaged:
(2) If the fastener holes are damaged you must contact AIRBUS INDUSTRIE
for the necessary corrective action procedure.
EFF :
001-012, 014-019, 53-31-00
Page B660
Aug 01/07
IAC
INTENTIONALLY BLANK
R
53-31-00
Page B661
Feb 01/08
IAC
Inspection Areas of the Fasteners Holes at FR38 thru FR41 between STGR12 and
STGR21, LH/RH
Figure 643/TASK 53-31-00-991-068- 12 (SHEET 1)
EFF :
001-012, 014-019,
53-31-00 Page B662
Aug 01/07
IAC
Inspection Areas of the Fasteners Holes at FR38 thru FR41 between STGR12 and
STGR21, LH/RH
Figure 643/TASK 53-31-00-991-068- 22 (SHEET 2)
EFF :
001-012, 014-019,
53-31-00 Page B663
Aug 01/07
IAC
5. Close-up
________
Subtask 53-31-00-410-104
A. Close Access
(1) Install the thermal and acoustic insulation (Ref. TASK 25-80-00-400-
001).
Subtask 53-31-00-862-063
R
EFF :
001-012, 014-019, 53-31-00
Page B664
Feb 01/08
IAC
R **ON A/C 001-012, 014-099,
R TASK 53-31-00-210-044
R 1. __________________
Reason for the Job
R Self Explanatory
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
001-012, 014-099, 53-31-00
Page B665
May 01/08
IAC
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R 3. __________
Job Set-up
R Subtask 53-31-00-010-108
R A. Get Access
R WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
R BEFORE YOU START A TASK ON OR NEAR:
R - THE FLIGHT CONTROLS
R - THE FLIGHT CONTROL SURFACES
R - THE LANDING GEAR AND THE RELATED DOORS
R - COMPONENTS THAT MOVE.
R
EFF :
001-012, 014-099, 53-31-00
Page B666
May 01/08
IAC
R WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE
_______
R LANDING GEAR.
R WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE LANDING GEAR ARE CLEAR.
_______
R (2) Put the warning notice in position to tell persons not to operate the
R landing gear.
R (3) On the overhead panel near the hydraulic section of panel 40VU, put a
R warning notice in position to tell persons not to operate the
R hydraulic system.
R (4) On the ground service panel of the Green, Blue and Yellow hydraulic
R system,put a warning notice in position to tell persons not to
R operate the hydraulic system.
R (5) Depressurize the Green, Blue and Yellow hydraulic systems per AMM
R 29-10-00-201. Depressurize the Green, Blue and Yellow hydraulic
R reservoirs per AMM 29-14-00-201. Open and tag the circuit breakers
R for the hydraulic systems.
R (6) Put the access platform in position below the MLG compartment.
R (7) Remove the access panels 191KB, 192KB (Ref. TASK 53-35-13-000-002).
R (9) Remove the Yellow Electric Hydraulic Pump (Ref. TASK 29-24-51-000-
R 001).
R (10) Remove the Yellow Hydraulic Power Accumulator (Ref. TASK 29-13-42-
R 000-001).
R Subtask 53-31-00-110-099
R B. Cleaning Procedure
R (Ref. Fig. 644/TASK 53-31-00-991-069)
EFF :
001-012, 014-099, 53-31-00
Page B667
May 01/08
IAC
R Inspection Areas of the Riveted Area of Keel Beam Side Panel at Attachment to
R Center Wing Box
R Figure 644/TASK 53-31-00-991-069- 12 (SHEET 1)
EFF :
001-012, 014-099,
53-31-00 Page B668
May 01/08
IAC
R Inspection Areas of the Riveted Area of Keel Beam Side Panel at Attachment to
R Center Wing Box
R Figure 644/TASK 53-31-00-991-069- 22 (SHEET 2)
EFF :
001-012, 014-099,
53-31-00 Page B669
May 01/08
IAC
R WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
R AREA WHEN YOU USE SPECIAL MATERIALS.
R IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
R OR IN YOUR EYES :
R -FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
R MINUTES.
R -GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
R DO NOT BREATHE THE FUMES FROM THE MATERIAL.
R DO NOT SMOKE WHEN YOU USE THE MATERIAL.
R DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
R HEAT.
R THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
R AND SKIN IRRITANTS.
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-026)
R and a lint free cloth , if necessary. Make sure the area is dry
R before you continue. Clean the areas around the rivets and elliptical
R cutouts identified in Area A and Area B as identified in Figure 1,
R Sheets 1 and 2.
R 4. Procedure
_________
R Subtask 53-31-00-210-093
R (1) Do a detailed visual inspection in the area around the rivets of the
R keel beam side panel below the center wing box, at Stringer 42, on
R both LH and RH sides, between Frames 40 and 42, Area A as shown in
R Figure 1, Sheet 2. Inspect areas around the rivets and area around
R elliptical cutout forward of Frame 41 for cracks, use a 10X
R magnifying glass. Use of additional lighting sources and mirrors is
R recommended.
EFF :
001-012, 014-099, 53-31-00
Page B670
May 01/08
IAC
R (a) In case of single crack findings:
R 1
_ If the crack length is less than 15 mm (0.5905 in.):
R a
_ Repair the Area A within 1,700 FC or 3,800 FH, which occurs
R first in accordance with the (Ref. ASRM 53-31-29-201).
R After repair in Area A, Area B must be inspected (Ref. TASK
R 53-31-00-210-045).
R 2
_ If the crack length is between 15 mm (0.5905 in.) and 20 mm
R (0.7874 in.):
R a
_ Repair the Area A within 860 FC or 1,800 FH, which occurs
R first in accordance with the (Ref. ASRM 53-31-29-201).
R After repair in Area A, Area B must be inspected (Ref. TASK
R 53-31-00-210-045).
R 3
_ If the crack length is more than 20 mm (0.7874 in.) or in case
R of multiple crack:
R a
_ Before further flight, repair the Area A in accordance with
R the (Ref. ASRM 53-31-23-201). After repair in Area A, Area
R B must still be inspected (Ref. TASK 53-31-00-210-045).
R 5. Close-up
________
R Subtask 53-31-00-410-105
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Install the Yellow Electric Power Accumulator (Ref. TASK 29-13-42-
R 400-001).
R (3) Install the Yellow Electric Hydraulic Pump (Ref. TASK 29-24-51-400-
R 001).
EFF :
001-012, 014-099, 53-31-00
Page B671
May 01/08
IAC
R (5) Install the access panels 191KB, 192KB (Ref. TASK 53-35-13-400-002).
R (8) Reset the hydraulic system circuit breakers. Pressurize the Green,
R Blue and Yellow hydraulic reservoirs per AMM 29-14-00-201. Pressurize
R the Green, Blue and Yellow hydraulic system per AMM 29-10-00-201.
R (11) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
EFF :
001-012, 014-099, 53-31-00
Page B672
May 01/08
IAC
R **ON A/C 001-012, 014-099,
R TASK 53-31-00-210-045
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
EFF :
001-012, 014-099, 53-31-00
Page B673
May 01/08
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R 3. __________
Job Set-up
R Subtask 53-31-00-010-109
R A. Get Access
R WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
R BEFORE YOU START A TASK ON OR NEAR:
R - THE FLIGHT CONTROLS
R - THE FLIGHT CONTROL SURFACES
R - THE LANDING GEAR AND THE RELATED DOORS
R - COMPONENTS THAT MOVE.
R WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE
_______
R LANDING GEAR.
R WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE LANDING GEAR ARE CLEAR.
_______
R (2) Put the warning notice in position to tell persons not to operate the
R landing gear.
R (3) On the overhead panel near the hydraulic section of panel 40VU, put a
R warning notice in position to tell persons not to operate the
R hydraulic system.
EFF :
001-012, 014-099, 53-31-00
Page B674
May 01/08
IAC
R (4) On the ground service panel of the Green, Blue and Yellow hydraulic
R system,put a warning notice in position to tell persons not to
R operate the hydraulic system.
R (5) Depressurize the Green, Blue and Yellow hydraulic systems per AMM
R 29-10-00-201. Depressurize the Green, Blue and Yellow hydraulic
R reservoirs per AMM 29-14-00-201. Open and tag the circuit breakers
R for the hydraulic systems.
R (6) Put the access platform in position below the MLG compartment.
R (7) Remove the access panels 191KB, 192KB (Ref. TASK 53-35-13-000-002).
R (9) Remove the Yellow Electric Hydraulic Pump (Ref. TASK 29-24-51-000-
R 001).
R (10) Remove the Yellow Hydraulic Power Accumulator (Ref. TASK 29-13-42-
R 000-001).
R Subtask 53-31-00-110-100
R B. Cleaning Procedure
R (Ref. Fig. 644/TASK 53-31-00-991-069)
R WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
R AREA WHEN YOU USE SPECIAL MATERIALS.
R IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
R OR IN YOUR EYES :
R -FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
R MINUTES.
R -GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
R DO NOT BREATHE THE FUMES FROM THE MATERIAL.
R DO NOT SMOKE WHEN YOU USE THE MATERIAL.
R DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
R HEAT.
R THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
R AND SKIN IRRITANTS.
EFF :
001-012, 014-099, 53-31-00
Page B675
May 01/08
IAC
R (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-026)
R and a lint free cloth , if necessary. Make sure the area is dry
R before you continue. Clean the areas around the rivets and elliptical
R cutouts identified in Area A and Area B as identified in Figure 1,
R Sheets 1 and 2.
R 4. Procedure
_________
R Subtask 53-31-00-210-094
R (1) Do a detailed visual inspection in the area around the rivets of the
R keel beam side panel below the center wing box, at Stringer 42, on
R both LH and RH sides, between Frames 40 and 42, Area B as shown in
R Figure 1, Sheet 2. Inspect areas around the rivets for cracks using a
R 10X magnifying glass. Use of additional lighting sources and mirrors
R is recommended.
R (a) If any cracks are found, contact Liaison Engineering. Airbus must
R be contacted for repair instruction specific to the findings.
R Repair prior to further flight.
EFF :
001-012, 014-099, 53-31-00
Page B676
May 01/08
IAC
R **ON A/C 001-012, 014-099,
R 5. Close-up
________
R Subtask 53-31-00-410-106
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Install the Yellow Electric Power Accumulator (Ref. TASK 29-13-42-
R 400-001).
R (3) Install the Yellow Electric Hydraulic Pump (Ref. TASK 29-24-51-400-
R 001).
R (5) Install the access panels 191KB, 192KB (Ref. TASK 53-35-13-400-002).
R (8) Reset the hydraulic system circuit breakers. Pressurize the Green,
R Blue and Yellow hydraulic reservoirs per AMM 29-14-00-201. Pressurize
R the Green, Blue and Yellow hydraulic system per AMM 29-10-00-201.
R (11) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
EFF :
001-012, 014-099, 53-31-00
Page B677
May 01/08
IAC
MLG Door Hinge Fittings and Actuator Fitting on the Keelbeam Box
R Figure 645/TASK 53-31-00-991-015
EFF :
001-012, 014-099, 53-31-00
Page B678
May 01/08
IAC
MLG Door Hinge Fittings and Actuator Fitting on the Keelbeam Box
R Figure 645A/TASK 53-31-00-991-015-A
EFF :
101-199, 901-999, 53-31-00
Page B679
May 01/08
IAC
MAIN STRUCTURE - CLEANING/PAINTING
__________________________________
TASK 53-31-00-916-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page 701
Feb 01/07
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-010-077
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(2) Put the warning notice on the slat/flap control lever to tell persons
not to operate the slats.
Subtask 53-31-00-110-070
B. Cleaning Procedure
EFF :
ALL 53-31-00
Page 702
Feb 01/07
IAC
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Remove the old temporary protection compound from the area to be
treated with a non metallic scraper, and clean with CLEANING AGENTS
(Material No. 11-004) and a lint free cloth. Make sure that the area
is dry before you continue.
4. Procedure
_________
Subtask 53-31-00-916-064
EFF :
ALL 53-31-00
Page 703
Feb 01/07
IAC
R Pressure Bulkhead AFT Face at FR35 and Bottom Surface of Pressure Deck between
FR35 and FR36
Figure 701/TASK 53-31-00-991-026
EFF :
ALL
53-31-00 Page 704
Nov 01/96
IAC
R **ON A/C 101-199,
R Subtask 53-31-00-916-064-A
5. Close-up
________
Subtask 53-31-00-410-075
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-31-00
Page 705
Feb 01/07
IAC
TASK 53-31-00-916-002
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-31-00
Page 706
Feb 01/07
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-31-00-861-051
Subtask 53-31-00-010-078
B. Get Access
(1) Remove the necessary equipment and furnishing to get access to the
cabin floor panels.
(2) Remove the following floor panels 241HF, 241GF, 241FF, 241EF, 242FF,
242GF, 242HF, 241MF, 241LF, 241KF, 241JF, 242KF, 242LF, 242MF
(Ref. TASK 53-32-12-000-002).
(3) Remove the necessary lower sidewall panels between FR36 and FR46
(Ref. TASK 25-23-44-000-001).
(4) Remove the necessary cabin air supply ducts installed above the floor
structure between FR36 and FR46 (Ref. TASK 21-20-00-010-001).
(5) Release and carefully pull back the necessary insulation blankets
from the sides of the fuselage, below the floor level, between FR36
and FR46.
EFF :
ALL 53-31-00
Page 707
Feb 01/07
IAC
(6) Attach them temporarily to the fuselage structure above the floor
level.
Subtask 53-31-00-110-071
C. Cleaning Procedure
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Remove the old temporary protection compound from the area to be
treated with a non metallic scraper, and clean with CLEANING AGENTS
(Material No. 11-004) and a lint free cloth. Make sure that the area
is dry before you continue.
4. Procedure
_________
EFF :
ALL 53-31-00
Page 708
Feb 01/07
IAC
Subtask 53-31-00-916-065
5. Close-up
________
Subtask 53-31-00-410-076
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Release and fold down the insulation blankets and attach them in
their initial positions.
(3) Install the cabin air supply ducts, removed to gain access to the
cabin floor structure between FR36 and FR46 (Ref. TASK 21-20-00-410-
001).
R (4) Install the lower sidewall panels between FR42 and FR46 (Ref. TASK
R 25-23-44-400-001).
R (5) Install the floor panels 241HF, 241GF, 241FF, 241EF, 242FF, 242GF,
242HF, 241MF, 241LF, 241KF, 241JF, 242KF, 242LF, 242MF (Ref. TASK 53-
32-12-400-002).
R (6) Install the equipment and furnishing, removed to get access to the
cabin floor panels.
R (7) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 53-31-00-862-051
EFF :
ALL 53-31-00
Page 709
May 01/97
IAC
Fuselage Internal Structure Below Cabin Floor Panels, Including Cabin Floor
Structure between FR36 and FR46.
Figure 702/TASK 53-31-00-991-027
EFF :
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53-31-00 Page 710
May 01/97
R
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FLOOR PANELS - DESCRIPTION AND OPERATION
________________________________________
1. General
_______
2. _________________________
Description and Operation
EFF :
ALL 53-32-00
Page 1
Feb 01/07
IAC
R **ON A/C 101-199,
EFF :
101-199, 53-32-00
Page 2
Feb 01/07
IAC
PANELS - CABIN FLOOR - REMOVAL/INSTALLATION
___________________________________________
TASK 53-32-12-000-002
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-32-12-861-050
EFF :
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Page 401
Nov 01/07
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Subtask 53-32-12-010-050
B. Get access.
(1) Remove the necessary equipment and furnishing to get access to the
cabin floor panels.
4. Procedure
_________
Subtask 53-32-12-020-050
(1) Pull the cord (1) up to remove the sealant from between the floor
panel joints.
NOTE : Identify the floor panels. This will help the installation
____
procedure.
EFF :
ALL 53-32-12
Page 402
Nov 01/07
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Cabin Floor Panel Installation - FR35 thru FR47
Figure 401/TASK 53-32-12-991-002
R
EFF :
001-012, 014-099, 901-901, 53-32-12
Page 403
Nov 01/07
IAC
R Cabin Floor Panel Installation - FR35.8 thru FR47.5
R Figure 401A/TASK 53-32-12-991-002-C
EFF :
101-199, 53-32-12
Page 404
Nov 01/07
IAC
R Cabin Floor Panel Installation - FR35 thru FR47
R Figure 401B/TASK 53-32-12-991-002-B
R
EFF :
902-999, 53-32-12
Page 405
Nov 01/07
IAC
R **ON A/C 101-199,
R Subtask 53-32-12-020-050-C
R (1) Pull the cord (4) up, to remove the sealant from between the floor
R panel joints.
R NOTE : Identify the floor panels (1). This will help with the
____
R installation procedure.
R (4) If necessary, remove the heated floor panels 15DS (16DS) at the aft
R emergency exits (Ref. TASK 25-27-51-000-001).
R Subtask 53-32-12-020-050-B
R (1) Pull the cord (4) up, to remove the sealant from between the floor
R panel joints.
R NOTE : Identify the floor panels (1). This will help with the
____
R installation procedure.
R
EFF :
101-199, 902-999, 53-32-12
Page 406
Nov 01/07
IAC
**ON A/C ALL
TASK 53-32-12-400-002
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-32-12
Page 407
Feb 01/08
IAC
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-32-12
Page 408
Nov 01/07
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-32-12-860-050
(1) Make sure the ground service network is energized (Ref. TASK 24-42-
00-861-001).
(2) Make sure the necessary equipment is removed to get access to the
cabin floor panels.
4. Procedure
_________
Subtask 53-32-12-160-050
(1) Remove the remaining used sealant from the floor panels with a
SCRAPER - NON METALLIC.
(2) Clean the component interface and the adjacent area with the CLEANING
AGENTS (Material No. 11-026) and a clean lint-free cloth
MISCELLANEOUS (Material No. 19-003).
(3) Make sure that the parts retained from the removed component are
clean and in the correct condition.
(5) Make sure that the self-adhesive foam tapes (2) are in the correct
condition. If necessary:
1
_ Clean the contact surfaces of the self-adhesive foam tapes (2)
with the CLEANING AGENTS (Material No. 11-026) and a lint-free
cotton cloth, MISCELLANEOUS (Material No. 19-003).
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Page 409
Feb 01/08
R
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(c) Install the new self-adhesive foam tapes (2).
Subtask 53-32-12-160-050-B
(1) Remove the used sealant from the floor panels (1) with a SCRAPER -
NON METALLIC.
(a) Clean the component interface and the adjacent area with the
CLEANING AGENTS (Material No. 11-026) and a clean lint-free
cotton cloth MISCELLANEOUS (Material No. 19-003).
(3) Make sure that the parts retained from the removed component are
clean and in the correct condition.
(5) Make sure that the clipnuts (5) are clean and in the correct
condition. If necessary, replace the defective clipnuts (5).
(6) Make sure that the self-adhesive foam tapes (3) are in the correct
condition. If necessary:
(b) Clean the surfaces of the self-adhesive foam tapes (3) with the
CLEANING AGENTS (Material No. 11-026) and a lint-free cotton
cloth MISCELLANEOUS (Material No. 19-003).
EFF :
001-012, 014-099, 101-199, 902-999, 53-32-12
Page 410
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R
IAC
(c) Install the new self-adhesive foam tapes (3).
Subtask 53-32-12-160-050-A
(1) Remove the remaining used sealant from the floor panels with a
SCRAPER - NON METALLIC.
(a) Clean the component interface and the adjacent area with the
CLEANING AGENTS (Material No. 11-026) and a lint-free cotton
cloth, MISCELLANEOUS (Material No. 19-003).
(3) Make sure that the parts retained from the removed component are
clean and in the correct condition.
(5) Make sure that the clipnuts (5) are clean and in the correct
condition. If necessary, replace the defective clipnuts (5).
(6) Make sure that the self-adhesive foam tapes (2) are in the correct
condition. If necessary:
1
_ Clean the contact surfaces of the self-adhesive foam tapes (2)
with the CLEANING AGENTS (Material No. 11-026) and a lint-free
cotton cloth, MISCELLANEOUS (Material No. 19-003).
EFF :
101-199, 901-999, 53-32-12
Page 411
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R
IAC
**ON A/C 001-012, 014-099, 901-901,
Subtask 53-32-12-420-050
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Apply the SPECIAL MATERIALS (Material No. 05-002) to the screws (3).
(4) Install the screws (3) and TORQUE to 0.42 m.daN (37.16 lbf.in).
(5) Install the cord (1) MISCELLANEOUS (Material No. 19-027) in the
clearance between the floor panels.
NOTE : Make a loop at the end of the cord, this will help the
____
subsequent removal procedure.
(6) Apply the SEALANTS (Material No. 09-016) in the clearance between the
floor panels.
Subtask 53-32-12-420-050-C
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) If removed, install the heated floor panels 15DS (16DS) at the aft
emergency exits (Ref. TASK 25-27-51-400-001).
EFF :
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R
IAC
R (3) Put the floor panels (1) in position.
R (4) Apply the zinc chromate putty SPECIAL MATERIALS (Material No. 05-002)
R to the screws (2).
R (5) Install the screws (2) and TORQUE to 0.42 m.daN (37.16 lbf.in).
R (6) Install the cord (4) MISCELLANEOUS (Material No. 19-027) in the
R clearance between the floor panels (1). Make a loop at the end of the
R cord. This will help with the subsequent removal procedure.
R (7) Apply the SEALANTS (Material No. 09-016) in the space between the
R floor panels (1).
R Subtask 53-32-12-420-050-B
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (3) Apply the zinc chromate putty SPECIAL MATERIALS (Material No. 05-002)
R to the screws (2).
R (4) Install the screws (2) and TORQUE to 0.42 m.daN (37.16 lbf.in).
R (5) Install the cord (4) MISCELLANEOUS (Material No. 19-027) in the
R clearance between the floor panels (1). Make a loop at the end of the
R cord. This will help with the subsequent removal procedure.
R (6) Apply the SEALANTS (Material No. 09-016) in the space between the
R floor panels (1).
EFF :
101-199, 902-999, 53-32-12
Page 413
Nov 01/07
IAC
**ON A/C ALL
5. Close-up
________
Subtask 53-32-12-410-051
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the equipment removed to get access to the cabin floor
panels.
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 53-32-12-862-050
EFF :
ALL 53-32-12
Page 414
Nov 01/07
IAC
SUPPORT STRUTS - DESCRIPTION AND OPERATION
__________________________________________
1. _______
General
Support struts are installed to give structural strength and rigidity
between the aircraft structures, or support between structure and component
assemblies.
2. Description
___________
A. Support Struts
The support struts are made of aluminum alloy. They are set or adjustable
in length and usually tubular in shape. They are made in different tube
dimensions and wall thickness to meet special requirements. A fork-end or
eye-end fitting is attached to each end of the tube. The ends provide the
installation points to connect the strut between the structures, or the
structure and the component.
EFF :
ALL 53-33-00
Page 1
Feb 01/96
IAC
FAIRINGS - DESCRIPTION AND OPERATION
____________________________________
1. _______
General
R The belly fairing is a permanent extension to the lower fuselage and is
R installed at STA1307 (between FR30 and FR31) thru STA2456/FR53. The
R structure extends around the air conditioning and the hydraulic services
R equipment for the aircraft. It gives easy access for maintenance procedures
R to the equipment. The belly fairing spans the width of the lower fuselage,
R between the left and right wings. The extension of the structure around both
R wing roots completes the wing-to-fuselage fillet zone.
R
R The main landing gear bay is installed between FR42 and FR46. When the
R landing gear doors are up and locked (landing gear up or fully extended),
R the doors complete the belly fairing profile.
2. Component
__________________
Location
(Ref. Fig. 001)
3. ___________
Description
R The belly fairing structure is made of frames, support struts and skin
R panels. Rivets attach the frames to the aircraft lower fuselage. Most of the
R frames become an extension to the aircraft fuselage frames. They are
R installed between FR31 thru FR42 and FR46 thru FR52.
R
R A keel beam gives longitudinal structural strength at the lower center of
R the belly fairing. Rivets attach the beam to the bottom of the aircraft keel
R beam and to FR47. The belly-fairing keel-beam is installed between FR36 thru
R FR47.
R
R The belly fairing panels are made of honeycomb core, which is bonded between
R Glassfiber-Reinforced Plastic (GRP) sheets. You can remove all the panels
R from the structure. Some of them have quick-release fittings for easy
R opening or removal to give fast access to the equipment.
R
R A blow-out panel is included in the air conditioning services panel,192KB.
R If an overpressure condition occurs in the air conditioning bay, the
R blow-out panel will open. The panel is pushed open against spring tension
R and remains open until it can be closed by hand during ground maintenance.
EFF :
ALL 53-35-00
Page 1
Nov 01/04
IAC
Belly Fairing Structure - Component Location
Figure 001
EFF :
ALL 53-35-00
Page 2
Feb 01/96
IAC
FAIRINGS - INSPECTION/CHECK
___________________________
TASK 53-35-00-200-002
Inspection of the Wing to Fuselage Fairings and Belly Fairing Access Panels for
Missing Fasteners
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-35-00
Page 601
Feb 01/07
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-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-35-00-010-052
A. Get Access
EFF :
ALL 53-35-00
Page 602
Feb 01/07
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4. Procedure
_________
Subtask 53-35-00-210-051
|-------------|----------------------------------|----------------------------|
| Panel FIN | Belly Fairing Missing Fasteners | |
| | Description | |
|-------------|----------------------------------|----------------------------|
| 7504MM | No missing fastener permitted. | |
| 7505MM | | |
| | | |
|-------------|----------------------------------|----------------------------|
| 193AB/194AB | No missing fastener permitted. | |
| 193BB/194BB | | |
| | | |
|-------------|----------------------------------|----------------------------|
| 191BB/192FB | Missing fasteners are not | Replace the missing |
| | permitted on the FWD edge of each| fasteners before 10 flight |
| | panel. | cycles |
| | Missing fasteners are permitted, | |
| | only if in accordance with the | |
| | subsequent condition: | |
| | - that a minimum of two fasteners| |
| | in the first fastener positions| |
| | are installed on all corners of| |
| | each panel (count from the | |
| | corner). | |
|-------------|----------------------------------|----------------------------|
| 191AB/191AT | Missing fasteners are not | Replace the missing |
| 191LB/192AB | permitted on the FWD edge of each| fasteners before 10 flight |
| 192AT/192LB | panel. | cycles |
| | Two missing fasteners are | |
| | permitted, only if in accordance | |
R
EFF :
ALL 53-35-00
Page 603
Feb 01/07
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Belly Fairing Access Panels and Wing to Fuselage Fairings - Right Side
Figure 601/TASK 53-35-00-991-004
R
EFF :
001-012, 014-099, 53-35-00
Page 604
Feb 01/07
IAC
R Belly Fairing Access Panels and Wing to Fuselage Fairings - Right Side
R Figure 601A/TASK 53-35-00-991-004-B
R
EFF :
101-199, 53-35-00
Page 605
Feb 01/07
IAC
Belly Fairing Access Panels and Wing to Fuselage Fairings - Right Side
R Figure 601B/TASK 53-35-00-991-004-A
R
EFF :
901-999, 53-35-00
Page 606
Feb 01/07
IAC
Belly Fairing Access Panels and Wing to Fuselage Fairings - Left Side
Figure 602/TASK 53-35-00-991-005
R
EFF :
001-012, 014-099, 901-999, 53-35-00
Page 607
Feb 01/07
IAC
R Belly Fairing Access Panels and Wing to Fuselage Fairings - Left Side
R Figure 602A/TASK 53-35-00-991-005-A
R
EFF :
101-199, 53-35-00
Page 608
Feb 01/07
IAC
Wing to Fuselage Fairings - 191BT/192BT and 191CT/192CT
Figure 603/TASK 53-35-00-991-006
EFF :
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Page 609
Feb 01/07
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|-------------|----------------------------------|----------------------------|
| Panel FIN | Belly Fairing Missing Fasteners | |
| | Description | |
|-------------|----------------------------------|----------------------------|
| | with the subsequent condition: | |
| | - that a minimum of four | |
| | fasteners of the first fastener| |
| | positions are installed on all | |
| | corners of each panel (count | |
| | from the corner). | |
|-------------|----------------------------------|----------------------------|
| 191DT/192DT | Missing fasteners are not | Replace the missing |
| | permitted on the FWD edge of each| fasteners before 10 flight |
| | panel. | cycles |
| | One fastener at every fourth | |
| | fastener position is permitted | |
| | missing, only if in accordance | |
| | with the subsequent condition: | |
| | - that a minimum of four | |
| | fasteners of the first fastener| |
| | positions are installed on all | |
| | corners of each panel (count | |
| | from the corner). | |
|-------------|----------------------------------|----------------------------|
| 191EB/192EB | Missing fasteners are not | Replace the missing |
| | permitted on the FWD edge of each| fasteners before 10 flight |
| | panel. | cycles |
| | One fastener at every fourth | |
| | fastener position is permitted | |
| | missing, only if in accordance | |
| | with the subsequent condition: | |
| | - that a minimum of two fasteners| |
| | of the first fastener positions| |
| | are installed on all corners | |
| | of each panel (count from the | |
| | corner). | |
|-------------|----------------------------------|----------------------------|
| 191ET/192ET | Missing fasteners are not | Replace the missing |
| 191KB/192KB | permitted when they are located | fasteners before 10 flight |
| 197BB/198BB | directly in the area of service | cycles |
| 147CB/147BB | panels. | |
| 148FB/148DB | Missing fasteners are only | |
| 197GB/198GB | permitted on a maximum of two | |
| 196AB/197AB | sides on each panel. | |
| 191GB/191HB | | |
| 191JB/195AB | At panels without sealing | |
| 147AB/195CB | profiles: | |
R
EFF :
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Page 610
Feb 01/07
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|-------------|----------------------------------|----------------------------|
| Panel FIN | Belly Fairing Missing Fasteners | |
| | Description | |
|-------------|----------------------------------|----------------------------|
| 147EB/147FB | One fastener at every fourth | |
| | fastener position is permitted | |
| | missing, only if in accordance | |
| | with the subsequent condition: | |
| | - that a minimum of two fasteners| |
| | of the first fastener positions| |
| | are installed on all corner | |
| | areas of each panel (count from| |
| | the corner). | |
| | | |
| | At panels with sealing profiles: | |
| | One fastener at every fourth | |
| | fastener position is permitted | |
| | missing, only if in accordance | |
| | with the subsequent condition: | |
| | - that a minimum of four | |
| | fasteners of the first fastener| |
| | positions are installed on all | |
| | corner areas of each panel | |
| | (count from the corner). | |
|-------------|----------------------------------|----------------------------|
| 191BT/192BT | (Ref. Fig. 603/TASK 53-35-00-991-| Replace the missing |
| 191CT/192CT | 006-001) | fasteners before 10 flight |
| | 1 - Missing fasteners are not | cycles |
| | permitted in the corner areas| |
| | 2 - Three missing fasteners are | |
| | permitted when two fasteners | |
| | are installed at each side of| |
| | an empty hole. | |
| | 3 - One missing fastener is | |
| | permitted. | |
| | 4 - Two missing fasteners are | |
| | permitted when they are not | |
| | adjacent to each other. | |
|-------------|----------------------------------|----------------------------|
R
EFF :
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Page 611
Feb 01/07
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R **ON A/C 101-199,
R Subtask 53-35-00-210-051-B
R |-------------|----------------------------------|----------------------------|
R | Panel FIN | Belly Fairing Missing Fasteners | |
R | | Description | |
R |-------------|----------------------------------|----------------------------|
R | 193AB/194AB | No missing fastener permitted. | |
R | 193BB/194BB | | |
R | | | |
R |-------------|----------------------------------|----------------------------|
R | 191BB/192FB | Missing fasteners are not | Replace the missing |
R | | permitted on the FWD edge of each| fasteners before 10 flight |
R | | panel. | cycles |
R | | Missing fasteners are permitted, | |
R | | only if in accordance with the | |
R | | subsequent condition: | |
R | | - that a minimum of two fasteners| |
R | | in the first fastener positions| |
R | | are installed on all corners of| |
R | | each panel (count from the | |
R | | corner). | |
R |-------------|----------------------------------|----------------------------|
R | 191AB/191AT | Missing fasteners are not | Replace the missing |
R | 191LB/192AB | permitted on the FWD edge of each| fasteners before 10 flight |
R | 192AT/192LB | panel. | cycles |
R | | Two missing fasteners are | |
R | | permitted, only if in accordance | |
R | | with the subsequent condition: | |
R | | - that a minimum of four | |
R | | fasteners of the first fastener| |
R | | positions are installed on all | |
R | | corners of each panel (count | |
R | | from the corner). | |
R
EFF :
101-199, 53-35-00
Page 612
Feb 01/07
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|-------------|----------------------------------|----------------------------|
| Panel FIN | Belly Fairing Missing Fasteners | |
| | Description | |
|-------------|----------------------------------|----------------------------|
R |-------------|----------------------------------|----------------------------|
R | 191DT/192DT | Missing fasteners are not | Replace the missing |
R | | permitted on the FWD edge of each| fasteners before 10 flight |
R | | panel. | cycles |
R | | One fastener at every fourth | |
R | | fastener position is permitted | |
R | | missing, only if in accordance | |
R | | with the subsequent condition: | |
R | | - that a minimum of four | |
R | | fasteners of the first fastener| |
R | | positions are installed on all | |
R | | corners of each panel (count | |
R | | from the corner). | |
R |-------------|----------------------------------|----------------------------|
R | 191EB/192EB | Missing fasteners are not | Replace the missing |
R | | permitted on the FWD edge of each| fasteners before 10 flight |
R | | panel. | cycles |
R | | One fastener at every fourth | |
R | | fastener position is permitted | |
R | | missing, only if in accordance | |
R | | with the subsequent condition: | |
R | | - that a minimum of two fasteners| |
R | | of the first fastener positions| |
R | | are installed on all corners | |
R | | of each panel (count from the | |
R | | corner). | |
R |-------------|----------------------------------|----------------------------|
R | 191ET/192ET | Missing fasteners are not | Replace the missing |
R | 193AT/194AT | permitted when they are located | fasteners before 10 flight |
R | 191KB/192KB | directly in the area of service | cycles |
R | 197KB/198KB | panels. | |
R | 147CB/147BB | Missing fasteners are only | |
R | 148FB/148DB | permitted on a maximum of two | |
R | 196AB/197AB | sides on each panel. | |
R | 197GB/198GB | | |
R | 191GB/191HB | At panels without sealing | |
R | 191JB/195AB | profiles: | |
R | 147AB/195CB | One fastener at every fourth | |
R | 147EB/147FB | fastener position is permitted | |
R | | missing, only if in accordance | |
R | | with the subsequent condition: | |
R | | - that a minimum of two fasteners| |
R | | of the first fastener positions| |
R
EFF :
101-199, 53-35-00
Page 613
Feb 01/07
IAC
|-------------|----------------------------------|----------------------------|
| Panel FIN | Belly Fairing Missing Fasteners | |
| | Description | |
|-------------|----------------------------------|----------------------------|
R | | are installed on all corner | |
R | | areas of each panel (count from| |
R | | the corner). | |
R | | | |
R | | At panels with sealing profiles: | |
R | | One fastener at every fourth | |
R | | fastener position is permitted | |
R | | missing, only if in accordance | |
R | | with the subsequent condition: | |
R | | - that a minimum of four | |
R | | fasteners of the first fastener| |
R | | positions are installed on all | |
R | | corner areas of each panel | |
R | | (count from the corner). | |
R |-------------|----------------------------------|----------------------------|
R | 191BT/192BT | (Ref. Fig. 603/TASK 53-35-00-991-| Replace the missing |
R | 191CT/192CT | 006-001) | fasteners before 10 flight |
R | | 1 - Missing fasteners are not | cycles |
R | | permitted in the corner areas| |
R | | 2 - Three missing fasteners are | |
R | | permitted when two fasteners | |
R | | are installed at each side of| |
R | | an empty hole. | |
R | | 3 - One missing fastener is | |
R | | permitted. | |
R | | 4 - Two missing fasteners are | |
R | | permitted when they are not | |
R | | adjacent to each other. | |
R |-------------|----------------------------------|----------------------------|
Subtask 53-35-00-210-051-A
R
EFF :
101-199, 901-999, 53-35-00
Page 614
Feb 01/07
IAC
criterias in the subsequent table when you remove a fastener from
any other panel.
|-------------|----------------------------------|----------------------------|
| Panel FIN | Belly Fairing Missing Fasteners | |
| | Description | |
|-------------|----------------------------------|----------------------------|
| 7504MM | No missing fastener permitted. | |
| 7505MM | | |
| | | |
|-------------|----------------------------------|----------------------------|
| 193AB/194AB | No missing fastener permitted. | |
| 193BB/194BB | | |
| | | |
|-------------|----------------------------------|----------------------------|
| 191BB/192FB | Missing fasteners are not | Replace the missing |
| | permitted on the FWD edge of each| fasteners before 10 flight |
| | panel. | cycles |
| | Missing fasteners are permitted, | |
| | only if in accordance with the | |
| | subsequent condition: | |
| | - that a minimum of two fasteners| |
| | in the first fastener positions| |
| | are installed on all corners of| |
| | each panel (count from the | |
| | corner). | |
|-------------|----------------------------------|----------------------------|
| 191AB/191AT | Missing fasteners are not | Replace the missing |
| 191LB/192AB | permitted on the FWD edge of each| fasteners before 10 flight |
| 192AT/192LB | panel. | cycles |
| | Two missing fasteners are | |
| | permitted, only if in accordance | |
| | with the subsequent condition: | |
| | - that a minimum of four | |
| | fasteners of the first fastener| |
| | positions are installed on all | |
| | corners of each panel (count | |
| | from the corner). | |
|-------------|----------------------------------|----------------------------|
| 191DT/192DT | Missing fasteners are not | Replace the missing |
| | permitted on the FWD edge of each| fasteners before 10 flight |
| | panel. | cycles |
| | One fastener at every fourth | |
R
EFF :
901-999, 53-35-00
Page 615
Feb 01/07
IAC
|-------------|----------------------------------|----------------------------|
| Panel FIN | Belly Fairing Missing Fasteners | |
| | Description | |
|-------------|----------------------------------|----------------------------|
| | fastener position is permitted | |
| | missing, only if in accordance | |
| | with the subsequent condition: | |
| | - that a minimum of four | |
| | fasteners of the first fastener| |
| | positions are installed on all | |
| | corners of each panel (count | |
| | from the corner). | |
|-------------|----------------------------------|----------------------------|
| 191EB/192EB | Missing fasteners are not | Replace the missing |
| | permitted on the FWD edge of each| fasteners before 10 flight |
| | panel. | cycles |
| | One fastener at every fourth | |
| | fastener position is permitted | |
| | missing, only if in accordance | |
| | with the subsequent condition: | |
| | - that a minimum of two fasteners| |
| | of the first fastener positions| |
| | are installed on all corners | |
| | of each panel (count from the | |
| | corner). | |
|-------------|----------------------------------|----------------------------|
| 191ET/192ET | Missing fasteners are not | Replace the missing |
| 191KB/192KB | permitted when they are located | fasteners before 10 flight |
| 197BB/198BB | directly in the area of service | cycles |
| 147CB/147BB | panels. | |
| 148FB/148DB | Missing fasteners are only | |
| 197GB/826DR | permitted on a maximum of two | |
| 196AB/198MB | sides on each panel. | |
| 191GB/191HB | | |
| 191JB/195AB | At panels without sealing | |
| 147AB/195CB | profiles: | |
| 147EB/147FB | One fastener at every fourth | |
| 197AB | fastener position is permitted | |
| | missing, only if in accordance | |
| | with the subsequent condition: | |
| | - that a minimum of two fasteners| |
| | of the first fastener positions| |
| | are installed on all corner | |
| | areas of each panel (count from| |
| | the corner). | |
| | | |
| | At panels with sealing profiles: | |
EFF :
901-999, 53-35-00
Page 616
Feb 01/07
IAC
|-------------|----------------------------------|----------------------------|
| Panel FIN | Belly Fairing Missing Fasteners | |
| | Description | |
|-------------|----------------------------------|----------------------------|
| | One fastener at every fourth | |
| | fastener position is permitted | |
| | missing, only if in accordance | |
| | with the subsequent condition: | |
| | - that a minimum of four | |
| | fasteners of the first fastener| |
| | positions are installed on all | |
| | corner areas of each panel | |
| | (count from the corner). | |
|-------------|----------------------------------|----------------------------|
| 191BT/192BT | (Ref. Fig. 603/TASK 53-35-00-991-| Replace the missing |
| 191CT/192CT | 006-001) | fasteners before 10 flight |
| | 1 - Missing fasteners are not | cycles |
| | permitted in the corner areas| |
| | 2 - Three missing fasteners are | |
| | permitted when two fasteners | |
| | are installed at each side of| |
| | an empty hole. | |
| | 3 - One missing fastener is | |
| | permitted. | |
| | 4 - Two missing fasteners are | |
| | permitted when they are not | |
| | adjacent to each other. | |
|-------------|----------------------------------|----------------------------|
5. Close-up
________
Subtask 53-35-00-410-051
A. Close Access
(1) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-35-00
Page 617
Feb 01/07
IAC
TASK 53-35-00-040-002
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-35-00-010-054
A. Get Access
EFF :
ALL 53-35-00
Page 618
Feb 01/07
IAC
Subtask 53-35-00-860-051
(1) Depressurize the Green, Yellow and Blue hydraulic systems (Ref. TASK
29-10-00-864-001), (Ref. TASK 29-10-00-864-002) and (Ref. TASK 29-10-
00-864-003).
4. Procedure
_________
Subtask 53-35-00-200-050
(2) If you find vanes with cracks more than half their length, replace
the louver panel (Ref. TASK 53-35-13-000-004).
(3) If you find damage, replace the louver panel (Ref. TASK 53-35-13-000-
004).
(4) If more than three vanes are missing from a louver panel, replace the
louver panel in less than 50 flight cycles (Ref. TASK 53-35-13-000-
004) (Ref. CDL 53-01).
5. Close-up
________
Subtask 53-35-00-410-053
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Pressurize the Green, Yellow and Blue hydraulic systems (Ref. TASK
29-10-00-863-001), (Ref. TASK 29-10-00-863-002) and (Ref. TASK 29-10-
00-863-003).
EFF :
ALL 53-35-00
Page 619
Feb 01/07
IAC
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-35-00
Page 620
Feb 01/07
IAC
FAIRINGS - WING TO FUSELAGE - REMOVAL/INSTALLATION
__________________________________________________
TASK 53-35-11-000-001
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-35-11
Page 401
May 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-35-11
Page 402
Feb 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-35-11-010-050
A. Get Access
(2) Put the warning notice in position to tell persons not to operate the
flight controls.
EFF :
ALL 53-35-11
Page 403
Feb 01/07
IAC
Subtask 53-35-11-864-050
(2) Depressurize the Green, the Yellow and the Blue hydraulic systems
(Ref. TASK 29-10-00-864-001), (Ref. TASK 29-10-00-864-002) and
(Ref. TASK 29-10-00-864-003).
Subtask 53-35-11-865-050
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07
49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06
105VU FLT CTL/SEC1/STBY SPLY 22CE B01
R
121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
4. Procedure
_________
EFF :
ALL 53-35-11
Page 404
Aug 01/07
IAC
Fairings - Wing-to-Fuselage (LH)
Figure 401/TASK 53-35-11-991-001
R
EFF :
001-012, 014-099, 53-35-11
Page 405
May 01/06
IAC
R Fairings - Wing-to-Fuselage (LH)
R Figure 401A/TASK 53-35-11-991-001-B
EFF :
101-199, 53-35-11
Page 406
Feb 01/07
IAC
Fairings - Wing-to-Fuselage (LH)
R Figure 401B/TASK 53-35-11-991-001-A
R
EFF :
901-999, 53-35-11
Page 407
Feb 01/07
IAC
**ON A/C 001-012, 014-099,
NOTE : The procedure that follows is for one fairing only. The procedure for
____
all fairings is almost the same.
Subtask 53-35-11-020-050
A. Removal of the Root Fillet Fairing of the Fairing Panel 191BT (192BT)
R
(Ref. Fig. 411/TASK 53-35-11-991-017)
R
EFF :
ALL 53-35-11
Page 408
May 01/07
IAC
Fairings - Wing-to-Fuselage (RH)
Figure 402/TASK 53-35-11-991-002
R
EFF :
001-012, 014-099, 53-35-11
Page 409
Feb 01/07
IAC
R Fairings - Wing-to-Fuselage (RH)
R Figure 402A/TASK 53-35-11-991-002-B
R
EFF :
101-199, 53-35-11
Page 410
Feb 01/07
IAC
Fairings - Wing-to-Fuselage (RH)
R Figure 402B/TASK 53-35-11-991-002-A
R
EFF :
901-999, 53-35-11
Page 411
Feb 01/07
IAC
Panel 191BT (192BT)
Figure 403/TASK 53-35-11-991-003
EFF :
ALL 53-35-11
Page 412
Feb 01/07
R
IAC
Panel 191CT (192CT)
Figure 404/TASK 53-35-11-991-010
EFF :
ALL 53-35-11
Page 413
Feb 01/07
R
IAC
Panel 191DT (192DT)
Figure 405/TASK 53-35-11-991-011- 12 (SHEET 1)
EFF :
ALL 53-35-11
Page 414
Feb 01/07
R
IAC
Panel 191DT (192DT)
Figure 405/TASK 53-35-11-991-011- 22 (SHEET 2)
EFF :
ALL 53-35-11
Page 415
Feb 01/07
R
IAC
Panel 191ET (192ET)
Figure 406/TASK 53-35-11-991-012
EFF :
ALL 53-35-11
Page 416
Feb 01/07
R
IAC
R Panel 193AT (194AT)
R Figure 407/TASK 53-35-11-991-013
R
EFF :
101-199, 53-35-11
Page 417
Feb 01/07
IAC
Panels 147CB and 148DB
R Figure 408/TASK 53-35-11-991-014
R
EFF :
ALL 53-35-11
Page 418
Feb 01/07
IAC
Panel 191LB (192LB)
R Figure 409/TASK 53-35-11-991-015
R
EFF :
ALL 53-35-11
Page 419
Feb 01/07
IAC
Wing-to-Fuselage Fairings - Wing Seal Profile Installation
R Figure 410/TASK 53-35-11-991-004
EFF :
ALL 53-35-11
Page 420
Feb 01/07
IAC
Root Fillet Fairing
R Figure 411/TASK 53-35-11-991-017
R
EFF :
001-012, 014-099, 53-35-11
Page 421
Feb 01/07
IAC
R (2) Hold the root fillet fairing (1) and remove the screws (3) and the
R washers (2).
Subtask 53-35-11-020-050-A
A. Removal of the Root Fillet Fairing of the Fairing Panel 191BT (192BT)
(Ref. Fig. 411A/TASK 53-35-11-991-017-A)
R (3) Remove the plugs (4) from the root fillet fairing (1).
R (4) Hold the root fillet fairing (1) and remove the screws (3) and (5)
R and the washers (2).
Subtask 53-35-11-020-051
R (1) For the fairing panels 191BT (192BT), 191CT (192CT), 191DT (192DT),
R 191ET (192ET), 193AT (194AT), 147CB, 148DB and 191LB (192LB):
R (2) The fairing panels 193AT and 194AT are part of the offwing
R escape-slides. Before you remove these fairings you must remove the
R offwing escape-slides (Ref. TASK 25-62-42-000-001).
R (a) Hold the fairing panel (3) and remove the screws (1) and the
R washers (2).
EFF :
ALL 53-35-11
Page 422
May 01/07
IAC
Root Fillet Fairing
R Figure 411A/TASK 53-35-11-991-017-A
R
EFF :
101-199, 901-999, 53-35-11
Page 423
Feb 01/07
IAC
R (3) If you must replace a wing seal profile in the fairing panels 191DT
R (192DT), or 191LB (192LB):
R (a) Remove the nuts (6), the seal retainer (7), the seal profile (5),
R the washers (8) and the screws (9). Do this from the fairing
R panel (3).
Subtask 53-35-11-020-051-A
R (1) For the fairing panels 191BT (192BT), 191CT (192CT), 191ET (192ET),
R 147CB, 148DB and 191LB (192LB):
R (a) Hold the fairing panel (3) and remove the screws (1) and the
R washers (2).
R (b) Hold the fairing panel (3) and remove the screws (1) and the
R washers (2).
R (3) If you must replace a wing seal profile in the fairing panels 191DT
R (192DT) or 191LB (192LB):
R (a) Remove the nuts (6), the seal reatiner (7), the seal profile (5),
R the washers (8) and the screws (9) from the fairing panel.
EFF :
ALL 53-35-11
Page 424
May 01/07
IAC
**ON A/C ALL
Subtask 53-35-11-020-052-A
C. Removal of the Access Panel 193BB (194BB) with the Slide Panel
R (Ref. Fig. 412/TASK 53-35-11-991-019-A)
(2) Remove the screws (1) from the sealing panel (2).
(4) Remove the screws (4) from the upper side of the access panel (3),
which you can see.
(5) Remove the screws (5) from the upper clip assy (7).
(7) Remove the screws (4) from the lower side of the access panel (3).
(8) Remove the screws (5) from the lower clip assy (6).
(9) Hold the reinforcement hook plate (11) and remove the screws (10) and
the bushes (9).
(10) Remove the access panel (3) together with the slide panel (8) from
the fuselage.
(12) Pull the slide panel (8) out of the access panel (3).
(13) Remove any loose and unwanted sealant in the related area.
Subtask 53-35-11-020-053
(2) Remove the screws (2) from the sealing panel (1).
EFF :
ALL 53-35-11
Page 425
Feb 01/07
IAC
Access Panel 193BB (194BB)
R Figure 412/TASK 53-35-11-991-019-A
EFF :
ALL 53-35-11
Page 426
Feb 01/07
IAC
Panel 193AB (194AB)
R Figure 413/TASK 53-35-11-991-020
EFF :
ALL 53-35-11
Page 427
Feb 01/07
IAC
(4) Remove the screws (3) from the upper side of the access panel (7),
which you can see.
(5) Remove the screws (5) from the upper clip assy (6).
(7) Remove the screws (5) from the lower clip assy (4).
(8) Remove the screws (3) from the lower side of the access panel (7).
(10) Remove any loose and unwanted sealant in the related area.
EFF :
ALL 53-35-11
Page 428
Feb 01/07
R
IAC
TASK 53-35-11-400-001
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-35-11
Page 429
Feb 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-35-11
Page 430
Feb 01/07
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-35-11
Page 431
Feb 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-35-11-860-050
(1) Make sure that the aircraft is in the same configuration as for the
removal task.
(2) Make sure that the slats are extended (Ref. TASK 27-80-00-866-004).
(3) Make sure the warning notice is in position to tell persons not to
operate the flight controls.
Subtask 53-35-11-864-051
B. Make sure that the Green, the Yellow and the Blue hydraulic systems are
depressurized (Ref. TASK 29-10-00-864-001), (Ref. TASK 29-10-00-864-002)
and (Ref. TASK 29-10-00-864-003).
R
EFF :
ALL 53-35-11
Page 432
Feb 01/07
IAC
Subtask 53-35-11-865-051
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07
49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06
105VU FLT CTL/SEC1/STBY SPLY 22CE B01
R
121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
4. Procedure
_________
Subtask 53-35-11-560-050
EFF :
ALL 53-35-11
Page 433
Aug 01/07
IAC
(3) Examine the fuselage seal profiles (4), the wing seal profiles (5)
and/or the seals type P (10), as applicable, for damage.
NOTE : Make sure that you replace the damaged pre-mod seals with the
____
applicable post-mod seals (Ref. SIL 51-008). If a Service
Bulletin (SB) is referred to, you must fully embody the
applicable SB, before you install the post-mod seal.
(a) Put the wing seal profile (5) and the seal retainer (7) in
position at the panel (3).
(b) Install the screws (9), the washers (8) and the nuts (6).
(5) Do an inspection of the bonded seals of the panels 191BT (192BT) and
191CT (192CT) for condition. If a seal is defective, do the
subsequent repair procedure.
Subtask 53-35-11-560-050-A
(3) Examine the fuselage seal profiles (4), the wing seal profiles (5)
and the seals type P (10), as applicable, for damage.
NOTE : Make sure that you replace the damaged pre-mod seals with the
____
applicable post-mod seals (Ref. SIL 51-008). If a Service
EFF :
ALL 53-35-11
Page 434
Feb 01/07
IAC
Bulletin (SB) is referred to, you must fully embody the
applicable SB, before you install the post-mod seal.
NOTE : The procedure step (5) is only applicable if you install a new
____
panel 191DT (192DT). The procedure is the same for the panels
191DT and 192DT.
(b) With a nonmetallic pencil, put marks on the wing surface and the
fuselage skin to identify the edges of the panel.
(d) Apply adhesive tape on the wing surface and the fuselage skin
behind the marks to prevent contamination with the sealant.
(e) Make the inner surface of the seals rough with the MISCELLANEOUS
(Material No. 19-011).
R
EFF :
101-199, 901-999, 53-35-11
Page 435
Feb 01/07
IAC
Panels 191DT and 192DT - Seal Profile
R Figure 414/TASK 53-35-11-991-005
R
EFF :
101-199, 901-999, 53-35-11
Page 436
Feb 01/07
IAC
Application of Sealants
R Figure 415/TASK 53-35-11-991-009
R
EFF :
101-199, 901-999, 53-35-11
Page 437
Feb 01/07
IAC
(j) Immediately install the panel while the sealant is still soft.
NOTE : Because of the stiffness of the double lip seals and the
____
added sealant, it is necessary to apply a pressure at the
seals to install the panels.
(k) Make sure that the seals are in the correct position adjacent to
the wing surface and the fuselage skin.
(l) Make sure the seals correctly touch the wing surface and the
fuselage skin.
(m) Remove the adhesive tape from the wing surface and the fuselage
skin.
(a) Put the wing seal profile (5) and the seal retainer (7) in
position at the panel (3).
(b) Install the screws (9), the washers (8) and the nuts (6).
(6) Do an inspection of the bonded seals of the panels 191BT (192BT) and
191CT (192CT) for condition. If a seal is defective, do the
subsequent repair procedure.
Subtask 53-35-11-350-051
B. Replacement of the Bonded Seals of the Panels 191BT (192BT) and 191CT
(192CT)
R (Ref. Fig. 416/TASK 53-35-11-991-007, 417/TASK 53-35-11-991-008)
WARNING : DO NOT GET THE PAINT ON YOUR SKIN OR IN YOUR EYES. PUT ON
_______
PROTECTIVE CLOTHING, GOGGLES AND A FACE MASK. USE THE PAINT IN
A WELL VENTILATED AREA. IF IN A CONFINED AREA, USE A SUPPLIED
AIR RESPIRATOR. DO NOT BREATHE THE GAS. GET MEDICAL AID IF YOUR
SKIN OR EYES BECOME IRRITATED.
EFF :
ALL 53-35-11
Page 438
Feb 01/07
IAC
Bonded Seal Replacement, Panel 191BT (192BT)
R Figure 416/TASK 53-35-11-991-007
R
EFF :
001-012, 014-099, 53-35-11
Page 439
Feb 01/07
IAC
Bonded Seal Replacement, Panel 191CT (192CT)
R Figure 417/TASK 53-35-11-991-008
R
EFF :
001-012, 014-099, 53-35-11
Page 440
Feb 01/07
IAC
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THIS/THESE
_______
MATERIAL/S.
USE PROTECTIVE CLOTHING, RUBBER GLOVES AND A MASK.
NOTE : The seal replacement procedure for one panel is given; the
____
procedure is almost the same for all the panels.
(1) Remove the rivets (4) (Ref. ASRM 514200) from the panel (3), and
discard the rivet burrs (2).
(2) Remove and discard the defective seal (1) from the panel (3).
(3) Clean the panel with a lint-free cloth and the CLEANING AGENTS
(Material No. 11-003) to remove the remaining adhesive.
(4) Clean the new seal (1) with soap and hot water, and let it dry.
(5) Put the seal (1) in its correct position at the edge of the panel
(3).
(7) Hold the seal (1) in position and put marks on it to align with the
rivet holes in the panel (3).
(8) Remove the seal (1) and make the holes for the rivets (4).
(9) Make the surface of the panel (3) rough with the emery cloth, grade
180.
NOTE : Be careful that you do not damage the surface of the panel
____
(3).
(10) Lightly rub the mating surface of the seal (1) with the emery cloth,
grade 120 to 240.
(11) Clean the mating surfaces of the seal (1) and the panel (3) with a
lint-free cloth and the CLEANING AGENTS (Material No. 11-003).
(12) Apply a thin layer of the primer of the BONDING AND ADHESIVE
COMPOUNDS (Material No. 08-004) or the BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-004A) to the surface of the panel (3).
R
EFF :
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Page 441
Feb 01/07
IAC
(13) Let the primer dry for not less than one hour, and not more than six
hours.
NOTE : If after six hours you have not installed the seal (1), you
____
must remove the cured primer and apply new primer.
(14) Use a spatula to apply a layer of the adhesive of the BONDING AND
ADHESIVE COMPOUNDS (Material No. 08-004) or the BONDING AND ADHESIVE
COMPOUNDS (Material No. 08-004A).
(15) Make sure that air bubbles do not show. Air bubbles are not
permitted.
(16) Put the seal (1) in position, and align the holes in the seal (1)
with the pre-drilled holes in the panel (3).
NOTE : You must install the seal (1) on the panel (3) in less than
____
ten minutes from when you applied the adhesive.
(17) Put the new rivets (4) through the panel (3) and the seal (1), and
install new rivet burrs (2) on the tails of the rivets (4).
(18) Install the rivets (4) (Ref. ASRM 514200). Make sure the rivets (4)
are flush with the surface of the panel (3).
(19) Make sure that the height of the tails of the rivets (4) plus the
thickness of the rivet burrs (2) is less than 3.0 mm (0.1181 in.), as
shown.
(20) Apply the STRUCTURE PAINTS (Material No. 16-024A) to the rivet burrs
(2), and to the head and the tail of the rivets (4).
(22) Apply the PAINTS FOR DETAIL (INTERNAL AND EXTERN AL) (Material No.
07-006) to the rivet burrs (2), and to the head and the tail of the
rivets (4).
(23) Let the PAINTS FOR DETAIL (INTERNAL AND EXTERN AL) (Material No. 07-
006) dry.
R
EFF :
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Page 442
Feb 01/07
IAC
R **ON A/C 001-012, 014-099, 901-999,
Subtask 53-35-11-960-050
NOTE : The sealing replacement procedure for the panel 193AT is given;
____
the procedure for the panel 194AT is the same.
(a) Temporarily install the new sealing (7) with the sealing plate
(2) at the panel (1).
(b) Cut the new sealing (7) to agree with the shape and the contour
of the initial sealing as shown in the detail C.
R (Ref. Fig. 418/TASK 53-35-11-991-018)
(c) Remove the sealing plate (2) and the sealing (7).
(a) Put the sealing (7) and the filler (3) in the installation
position.
(b) Install the sealing plate (2) with the studs (5) and the washers
(4).
R
EFF :
001-012, 014-099, 901-999, 53-35-11
Page 443
Feb 01/07
IAC
Seal Replacement - Panel 193AT (194AT)
R Figure 418/TASK 53-35-11-991-018- 12 (SHEET 1)
R
EFF :
001-012, 014-099, 901-999, 53-35-11
Page 444
Feb 01/07
IAC
Seal Replacement - Panel 193AT (194AT)
R Figure 418/TASK 53-35-11-991-018- 22 (SHEET 2)
R
EFF :
001-012, 014-099, 901-999, 53-35-11
Page 445
Feb 01/07
IAC
Subtask 53-35-11-420-050
CAUTION : DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF
_______
CARBONFIBER REINFORCED PLASTIC.
(1) For the fairing panels 191BT (192BT), 191CT (192CT), 191ET (192ET),
147CB, 148DB and 191LB (192LB):
NOTE : Fairings 193AT and 194AT are part of the Offwing Escape
____
Slides. Before you try to install these fairings (Ref. TASK
25-62-42-400-001).
(a) Make sure that the work area is clean and clear of tool(s) and
other items.
(d) TORQUE the screws to between 0.35 and 0.45 m.daN (30.97 and 39.82
lbf.in).
(a) Make sure that the work area is clean and clear of tool(s) and
other items.
(d) TORQUE the screws to between 0.35 and 0.45 m.daN (30.97 and 39.82
lbf.in).
(a) Make sure that the seal profiles of the fairing panels (3)
correctly touch the fuselage and/or the wing skins.
(b) Examine the fuselage seal profiles (4), the wing seal profiles
(5) and/or the seals type P (10), as applicable.
R
EFF :
001-012, 014-099, 901-999, 53-35-11
Page 446
Feb 01/07
IAC
R **ON A/C 101-199,
R Subtask 53-35-11-420-050-A
R CAUTION : DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF
_______
R CARBONFIBER REINFORCED PLASTIC.
R (1) For the fairing panels 191BT (192BT), 191CT (192CT), 191DT (192DT),
R 191ET (192ET), 193AT (194AT), 147CB, 148DB and 191LB (192LB):
R (a) Make sure that the work area is clean and clear of tool(s) and
R other items.
R (d) TORQUE the screws to between 0.35 and 0.45 m.daN (30.97 and 39.82
R lbf.in).
R (e) Make sure that the seal profiles of the fairing panels (3)
R correctly touch the fuselage and/or the wing skins.
R (f) Examine the fuselage seal profiles (4), the wing seal profiles
R (5) and/or the seals type P (10), as applicable.
Subtask 53-35-11-420-051
(3) Put the root fillet fairing (1) in the installation position.
R
EFF :
001-012, 014-099, 101-199, 53-35-11
Page 447
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IAC
(6) Retract the slats (Ref. TASK 27-80-00-866-005).
Subtask 53-35-11-420-051-A
(3) If necessary, remove the old sealants from the mating surface of the
root fillet fairing and the fairing panel 191BT (192BT).
(4) Apply the SEALANTS (Material No. 09-018) to the mating surface of the
root fillet fairing (1).
(6) Install the screws (3) and (5) and the washers (2).
(7) TORQUE the screws (3) and (5) to between 0.35 and 0.45 m.daN (30.97
and 39.82 lbf.in).
(8) Install the plugs (4) with the SEALANTS (Material No. 09-018) in the
root fillet fairing (1).
(9) Fill the plugged fastener holes and clearance between the root fillet
fairing (1) and the fairing panel 191BT (192BT) with SEALANTS
(Material No. 09-018) to make a smooth surface.
EFF :
ALL 53-35-11
Page 448
Feb 01/07
IAC
**ON A/C ALL
Subtask 53-35-11-420-052-A
F. Installation of the Access Panel 193BB (194BB) with the Slide Panel
R (Ref. Fig. 412/TASK 53-35-11-991-019-A)
(1) Make sure, that the flaps are retracted (Ref. TASK 27-50-00-866-009).
(4) Install the slide panel (8) to the access panel (3).
(5) Put the access panel (3) in its correct installation position.
(6) Attach the reinforcement hook plate (11) to the slide panel (8) as
follows:
(a) Align the anchor nuts of the reinforcement hook plate (11) with
the holes of the slide panel (8).
(b) Attach the reinforcement hook plate (11) to the slide panel (8)
with the screws (10) and the bushes (9).
(7) Install the screws (5) in the lower clip assy (6).
(8) Install the screws (4) in the lower side of the access panel (3),
which you can see.
(9) Extend the flaps sufficiently to attach the upper side of the access
panel (3) and the sealing panel (2) (Ref. TASK 27-50-00-866-008).
(10) Install the screws (5) in the upper clip assy (7).
(11) Install the screws (4) in the upper side of the access panel (3).
(12) Make sure, that all the screws of the access panel (3) are installed.
(13) TORQUE the screws (4) to between 0.35 and 0.45 m.daN (30.97 and 39.82
lbf.in).
(14) TORQUE the screws (5) to between 0.35 and 0.45 m.daN (30.97 and 39.82
lbf.in).
EFF :
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Feb 01/07
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(15) Put the sealing panel (2) in its correct installation position.
(16) Install the sealing panel (2) to the access panel (3) with the screws
(1).
(17) TORQUE the screws (1) to between 0.35 and 0.45 m.daN (30.97 and 39.82
lbf.in).
(18) Fill out the gaps with the SEALANTS (Material No. 09-016) to get a
smooth contour.
Subtask 53-35-11-420-053
(1) Make sure that the flaps are retracted (Ref. TASK 27-50-00-866-009).
(5) Install the screws (3) in the lower area of the access panel (7),
which you can see.
(7) Extend the flaps sufficiently to install the screws (3) at the upper
side of the access panel (7) (Ref. TASK 27-50-00-866-008).
(9) Install the screws (3) in the upper area of the access panel (7).
(10) Make sure that all the screws of the access panel (7) are installed.
(11) TORQUE the screws (3) to between 0.35 and 0.45 m.daN (30.97 and 39.82
lbf.in).
(12) TORQUE the screws (5) to between 0.35 and 0.45 m.daN (30.97 and 39.82
lbf.in).
(14) Install the sealing panel (1) with the screws (2).
EFF :
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Page 450
Feb 01/07
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(15) TORQUE the screws (2) to between 0.35 and 0.45 m.daN (30.97 and 39.82
lbf.in).
(16) Fill the clearance between the sealing panel (1) and the access panel
(7) with SEALANTS (Material No. 09-016) to get a smooth surface.
5. Close-up
________
Subtask 53-35-11-865-052
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
R 5CV, 6CV, 7CV, 8CV, 21CE1, 21CE2, 22CE.
Subtask 53-35-11-410-052
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-35-11
Page 451
Aug 01/07
IAC
FAIRINGS - COOLING AIR INLET - REMOVAL/INSTALLATION
___________________________________________________
TASK 53-35-12-000-002
1. __________________
Reason for the Job
Self Explanatory.
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-35-12-010-054
A. Get Access
(2) Remove the quick-release access panel 192KB (Ref. TASK 53-35-13-000-
002).
EFF :
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Page 401
Feb 01/96
IAC
4. Procedure
_________
Subtask 53-35-12-020-053
NOTE : To open the blowout panel, you must push the panel by hand
____
from the rear of the quick-release access panel 192KB.
When the blowout panel is open, the compression of the
spring is released.
(b) Disengage the retaining ring (2) and remove the pin (3).
(c) Remove the nut (4), the washer (5) and disconnect the bonding
strap (6).
(d) Install the washer (5) and tighten by hand the nut (4).
(e) Disengage the retaining rings (8) and remove the pins (9) from
the two hinge assemblies (10).
(a) Support the spring assembly (23), disengage the retaining ring
(16) and remove the pin (17).
NOTE : When you remove the pin (17), you can remove the
____
compression spring (14) and the guide fitting (15) from
the spring support (18).
(3) If you must remove the hinge assemblies (10) and/or the mounting
bracket (11):
(a) Remove the nuts (4), the washers (5) and the screws (7).
EFF :
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Feb 01/96
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(b) Remove the hinge assemblies (10) and/or the mounting bracket
(11).
(a) Remove the nuts (20), the washers (21) and the screws (22) that
attach the rods (34) to the hinge bracket assembly (19).
(b) Remove the nuts (24), the washers (25), the screws (26) and the
bonding strap (6).
(a) Remove the nuts (28), the washers (29), the screws (30) and the
rods (34).
(b) Remove the nuts (31), the washers (32) and the screws (33).
EFF :
ALL 53-35-12
Page 403
Feb 01/96
IAC
Belly Fairing Blowout Panel - Component Location
Figure 401/TASK 53-35-12-991-003- 12 (SHEET 1)
EFF :
ALL 53-35-12
Page 404
Feb 01/96
IAC
Belly Fairing Blowout Panel - Component Location
Figure 401/TASK 53-35-12-991-003- 22 (SHEET 2)
EFF :
ALL 53-35-12
Page 405
Feb 01/96
IAC
TASK 53-35-12-400-002
1. __________________
Reason for the Job
Self Explanatory.
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-35-12-860-050
(2) Make sure that the quick-release access panel 192KB is removed.
EFF :
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Page 406
Feb 01/96
IAC
4. Procedure
_________
Subtask 53-35-12-560-050
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 53-35-12-420-052
(b) Put the rods (34) in position and install and tighten the screws
(30), the washers (29) and the nuts (28).
(a) Put the hinge bracket assembly (19) and bonding strap (6) in
position and install and tighten the screws (26), washers (25)
and the nuts (24). Repair the damage to the bonding point
protective coating (Ref. TASK 20-28-00-912-004).
(b) Put the rods (34) in position and install and tighten the screws
(22), the washers (21) and the nuts (20).
(a) Make sure that the spring guide (13) and the spring adjust nut
(12) are installed on the spring support (18).
(b) Put the spring (14) and the guide fitting (15) on the spring
support (18).
EFF :
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(c) Put the spring assembly (23) in position and install the pin (17)
through the guide fitting (15), spring-support bracket assembly
(27) and spring support (18).
(4) Install the hinge assemblies (10) and the mounting bracket (11):
(a) Put the hinge assemblies (10) and the mounting bracket (11) in
position and install and tighten the screws (7), the washers (5)
and the nuts (4).
NOTE : Do not install the screw, the washer and the nut required
____
for the bonding strap (6) installation.
(a) Put the blowout panel (1) in position and install the pins (9)
through the hinge bracket assembly (19) and the two hinge
assemblies (10).
(c) Install the screw (7), the bonding strap (6), the washer (5) and
the nut (4).
(d) Tighten the nut (4) and repair the damage to the bonding point
protective coating (Ref. TASK 20-28-00-912-004).
(6) Install the spring assembly (23) on the mounting bracket (11):
(a) Put the end-fitting of the spring support (18) in position at the
mounting bracket (11).
(b) Install the pin (3) through the mounting bracket (11) and the end
fitting of the spring support (18).
EFF :
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Page 408
Feb 01/96
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(d) Adjust the spring adjust nut (12) until the full dimension of the
spring (14) is 89.0 mm (3.5039 in.).
NOTE : This dimension will set the spring (14) to the approximate
____
release force required to open the blowout panel.
(e) With a spring scale that you can measure at least 45.0 daN
(101.1640 lbf), attach the spring scale to the mounting bracket
(11) at point X.
(f) Open the blowout panel (1) and make sure that the force necessary
to open the panel is 38.0 +2.0 -2.0 daN (85.4273 +4.4961 -4.4961
lbf).
NOTE : If you must adjust the force to the required limits, you
____
must do so at the spring adjust nut (12).
(h) Close the blowout panel (1) and make sure that the clearance
between the blowout panel contour and panel 192KB is:
- longitudinal 3.0 +1.5 -1.5 mm (0.1181 +0.0590 -0.0590 in.)
- lateral 3.0 +1.0 -1.0 mm (0.1181 +0.0393 -0.0393 in.).
5. Close-up
________
Subtask 53-35-12-410-055
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the quick-release access panel 192KB (Ref. TASK 53-35-13-400-
002).
EFF :
ALL 53-35-12
Page 409
Feb 01/96
IAC
ACCESS PANELS - REMOVAL/INSTALLATION
____________________________________
TASK 53-35-13-000-001
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
NOTE : The removal procedure for one panel is given; the procedure is almost
____
the same for all panels.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-35-13
Page 401
May 01/06
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-35-13
Page 402
Feb 01/07
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-35-13-010-050
A. Get Access
Subtask 53-35-13-860-050
(1) Depressurize the Green, Yellow and Blue hydraulic systems (Ref. TASK
29-10-00-864-001), (Ref. TASK 29-10-00-864-002) and (Ref. TASK 29-10-
00-864-003).
4. Procedure
_________
EFF :
ALL 53-35-13
Page 403
Feb 01/07
IAC
Access Panels - Belly Fairing (LH)
Figure 401/TASK 53-35-13-991-001
R
EFF :
001-012, 014-099, 53-35-13
Page 404
May 01/06
IAC
R Access Panels - Belly Fairing (LH)
R Figure 401A/TASK 53-35-13-991-001-B
EFF :
101-199, 53-35-13
Page 405
Feb 01/07
IAC
Access Panels - Belly Fairing (LH)
R Figure 401B/TASK 53-35-13-991-001-A
R
EFF :
901-999, 53-35-13
Page 406
Feb 01/07
IAC
Access Panels - Belly Fairing (RH)
Figure 402/TASK 53-35-13-991-002
R
EFF :
001-012, 014-099, 53-35-13
Page 407
Feb 01/07
IAC
R Access Panels - Belly Fairing (RH)
R Figure 402A/TASK 53-35-13-991-002-B
R
EFF :
101-199, 53-35-13
Page 408
Feb 01/07
IAC
**ON A/C 901-999,
Subtask 53-35-13-020-050
A. Remove the access panels: 147AB, 147BB, 147EB, 147FB, 148FB, 191AB,
191AT, 191GB, 191JB, 192AB, 192AT, 195CB, 197AB, 197GB and 198GB.
(1) Support the panel and remove the screws (1) and the washers (2).
(a) Disconnect the electrical connector from the anti collision light
6LV.
(c) Remove the bonding strap from the anti collision light.
Subtask 53-35-13-020-050-A
R A. Removal of the access panels 147AB, 147BB, 147EB, 147FB, 148FB, 191AB,
R 191AT, 191GB, 191JB, 192AB, 192AT, 195CB, 197AB, 197GB, 198MB, 826CR and
R 826DR
R (1) Hold the panel (3) with your hand and remove the screws (1) and the
R washers (2).
EFF :
ALL 53-35-13
Page 409
Aug 01/07
IAC
R Access Panels - Belly Fairing (RH)
Figure 402B/TASK 53-35-13-991-002-A
EFF :
901-999, 53-35-13
Page 410
Aug 01/07
IAC
Belly Fairing Access Panels - Typical Installation
Figure 403/TASK 53-35-13-991-003
R
EFF :
001-012, 014-099, 53-35-13
Page 411
Feb 01/07
IAC
R Belly Fairing Access Panels - Typical Installation
R Figure 403A/TASK 53-35-13-991-003-A
R
EFF :
101-199, 53-35-13
Page 412
Feb 01/07
IAC
(2) For panel 191JB:
(a) Disconnect the electrical connector from the anti collision light
6LV.
(c) Remove the bonding strap from the anti collision light.
EFF :
901-999, 53-35-13
Page 413
Aug 01/07
R
IAC
**ON A/C ALL
TASK 53-35-13-400-001
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
NOTE : The installation procedure for one panel is given; the procedure is
____
almost the same for all panels.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-35-13
Page 414
Feb 01/07
IAC
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-35-13
Page 415
Feb 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-35-13
Page 416
Feb 01/07
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-35-13-860-051
(1) Make sure that the aircraft is in the same configuration as for the
removal task.
(2) Make sure that the Green, Blue and Yellow hydraulic systems are
depressurized (Ref. TASK 29-10-00-864-001), (Ref. TASK 29-10-00-864-
002) and (Ref. TASK 29-10-00-864-003).
4. Procedure
_________
R
EFF :
ALL 53-35-13
Page 417
Feb 01/07
IAC
R **ON A/C 001-012, 014-099,
Subtask 53-35-13-560-050
CAUTION : BE CAREFUL WHEN YOU INSTALL THE LOUVER PANEL. IF YOU INSTALL IT
_______
INCORRECTLY, THE BELLY FAIRING WILL PRESSURIZE AND CAUSE DAMAGE
TO THE STRUCTURE.
(3) Do an inspection of the bonded seals of the panels 197GB (198GB) for
condition. If a seal is defective, do the subsequent repair
procedure.
Subtask 53-35-13-560-050-A
R
EFF :
ALL 53-35-13
Page 418
Feb 01/07
IAC
WARNING : DO NOT GET THE PAINT ON YOUR SKIN OR IN YOUR EYES. PUT ON
_______
PROTECTIVE CLOTHING, GOGGLES AND A FACE MASK. USE THE PAINT IN
A WELL VENTILATED AREA. IF IN A CONFINED AREA, USE A SUPPLIED
AIR RESPIRATOR. DO NOT BREATHE THE GAS. GET MEDICAL AID IF YOUR
SKIN OR EYES BECOME IRRITATED.
CAUTION : BE CAREFUL WHEN YOU INSTALL THE LOUVER PANEL. IF YOU INSTALL IT
_______
INCORRECTLY, THE BELLY FAIRING WILL PRESSURIZE AND CAUSE DAMAGE
TO THE STRUCTURE.
(3) Do an inspection of the seals on the panels 197GB and 198MB and
replace the seals if it is necessary.
(a) Drill out the rivets and remove the defective seal (Ref. ASRM
514200).
1
_ Remove the used adhesive from the panel with the CLEANING
AGENTS (Material No. 11-003) and a lint-free cotton cloth,
MISCELLANEOUS (Material No. 19-003).
(c) Make the mating area of the panel surface rough with emery cloth
grade 400.
(d) Carefully make the mating surface of the seal rough with emery
cloth grade 120 to 240.
R
EFF :
901-999, 53-35-13
Page 419
Feb 01/07
IAC
1
_ Clean all the repair areas and the seal with the CLEANING
AGENTS (Material No. 11-003) and a lint-free cotton cloth,
MISCELLANEOUS (Material No. 19-003).
(f) You can use for the bonding of the seal the BONDING AND ADHESIVE
COMPOUNDS (Material No. 08-033), the BONDING AND ADHESIVE
COMPOUNDS (Material No. 08-004) or the BONDING AND ADHESIVE
COMPOUNDS (Material No. 08-004A).
1
_ When you use the BONDING AND ADHESIVE COMPOUNDS (Material No.
08-033):
a
_ Apply a layer of the BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-033) to the seal.
b
_ Put the seal in position and align the holes in the seal
with the pre-drilled holes in the panel.
c
_ Apply a continuous force for 60 seconds over the full
length of the bonded seal.
NOTE : You must install the seal on the panel in less than
____
ten minutes from when you applied the adhesive.
2
_ When you use the BONDING AND ADHESIVE COMPOUNDS (Material No.
08-004) or the BONDING AND ADHESIVE COMPOUNDS (Material No.
08-004A):
a
_ Apply a thin layer of the primer of the BONDING AND
ADHESIVE COMPOUNDS (Material No. 08-004) or the BONDING AND
ADHESIVE COMPOUNDS (Material No. 08-004A) to the surface of
the panel.
b
_ Let the primer dry for not less than one hour, and not more
than six hours.
NOTE : If after six hours you have not installed the seal,
____
you must remove the cured primer and apply new
primer.
c
_ Use a SPATULA - WOODEN to apply a layer of the adhesive of
the BONDING AND ADHESIVE COMPOUNDS (Material No. 08-004) or
R
EFF :
901-999, 53-35-13
Page 420
Feb 01/07
IAC
the BONDING AND ADHESIVE COMPOUNDS (Material No. 08-004A)
to the seal.
d
_ Make sure that air bubbles do not show. Air bubbles are not
permitted.
e
_ Put the seal in position and align the holes in the seal
with the pre-drilled holes in the panel.
NOTE : You must install the seal on the panel in less than
____
ten minutes from when you applied the adhesive.
(g) Install the new seal with the rivets (Ref. ASRM 514200).
(h) Make sure that the new rivets are flush with the fairing skin and
a protective coating is applied.
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 53-35-13-350-050
WARNING : DO NOT GET THE PAINT ON YOUR SKIN OR IN YOUR EYES. PUT ON
_______
PROTECTIVE CLOTHING, GOGGLES AND A FACE MASK. USE THE PAINT IN
A WELL VENTILATED AREA. IF IN A CONFINED AREA, USE A SUPPLIED
AIR RESPIRATOR. DO NOT BREATHE THE GAS. GET MEDICAL AID IF YOUR
SKIN OR EYES BECOME IRRITATED.
(1) Remove the rivets (2) and the dimpled washers (4) from the panel (3)
(Ref. ASRM 514200).
R
EFF :
001-012, 014-099, 901-999, 53-35-13
Page 421
Feb 01/07
IAC
Bonded Seal Replacement - Panel 197GB (198GB)
Figure 404/TASK 53-35-13-991-010
R
EFF :
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Page 422
Feb 01/07
IAC
(2) Remove and discard the defective seal (1) from the panel (3).
(a) Clean the panel (3) with a lint-free cotton cloth, MISCELLANEOUS
(Material No. 19-003) and the CLEANING AGENTS (Material No. 11-
003), to remove the remaining adhesive.
(4) Put the new seal (1) in its correct position at the edge of the panel
(3).
(5) Cut the seal (1) to its correct length, and if necessary, cut the
edge of the seal (1) as shown, do this until the shape agrees with
the curve of the panel (3).
(6) Hold the seal (1) in position and put marks on it to align with the
rivet holes in the panel (3).
(7) Remove the seal (1) and make the holes for the rivets (2).
(8) Make the surface of the panel (3) rough with the emery cloth, grade
400.
NOTE : Be careful that you do not damage the surface of the panel
____
(3).
(9) Lightly rub the mating surface of the seal (1) with the emery cloth,
grade 120 to 240.
(a) Clean the mating surfaces of the seal (1) and the panel (3) with
a lint-free cotton cloth, MISCELLANEOUS (Material No. 19-003) and
the CLEANING AGENTS (Material No. 11-003).
(11) You can use for the bonding of the seal (1) the BONDING AND ADHESIVE
COMPOUNDS (Material No. 08-033), the BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-004) or the BONDING AND ADHESIVE COMPOUNDS (Material
No. 08-004A).
R
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(a) When you use the BONDING AND ADHESIVE COMPOUNDS (Material No. 08-
033):
1
_ Apply a layer of the BONDING AND ADHESIVE COMPOUNDS (Material
No. 08-033) to the seal (1).
2
_ Put the seal (1) in position and align the holes in the seal
with the pre-drilled holes in the panel (3).
3
_ Apply a continuous force for 60 seconds over the full length
of the bonded seal (3).
NOTE : You must install the seal (1) on the panel (3) in less
____
than ten minutes from when you applied the BONDING AND
ADHESIVE COMPOUNDS (Material No. 08-033).
(b) When you use the BONDING AND ADHESIVE COMPOUNDS (Material No. 08-
004) or the BONDING AND ADHESIVE COMPOUNDS (Material No. 08-
004A):
1
_ Apply a thin layer of the primer of the BONDING AND ADHESIVE
COMPOUNDS (Material No. 08-004) or the BONDING AND ADHESIVE
COMPOUNDS (Material No. 08-004A) to the surface of the panel
(3).
(c) Let the primer dry for not less than one hour, and not more than
six hours.
NOTE : If after six hours you have not installed the seal (1),
____
you must remove the cured primer and apply new primer.
(12) Make sure that air bubbles do not show. Air bubbles are not
permitted.
R
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Page 424
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(13) Put the seal (1) in position and align the holes in the seal with the
pre-drilled holes in the panel (3).
NOTE : You must install the seal (1) on the panel (3) in less than
____
ten minutes from when you applied the BONDING AND ADHESIVE
COMPOUNDS (Material No. 08-004) or the BONDING AND ADHESIVE
COMPOUNDS (Material No. 08-004A).
(14) Push down along the length of the seal (1), and hold it in this
position for not less than one minute.
(a) Put the new rivets (2) through the dimpled washers (4), the seal
(1) and the panel (3).
(c) Make sure the rivets (2) are flush with the surface of the panel
(3).
(d) Apply the STRUCTURE PAINTS (Material No. 16-024A) to the dimpled
washers (4), and to the head and tail of the rivets (2).
(f) Apply the PAINTS FOR DETAIL (INTERNAL AND EXTERN AL) (Material
No. 07-006) to the dimpled washers (4), and to the head and tail
of the rivets (2).
(g) Let the PAINTS FOR DETAIL (INTERNAL AND EXTERN AL) (Material No.
07-006) dry.
Subtask 53-35-13-420-050
C. Install the access panels: 147AB, 147BB, 147EB, 147FB, 148FB, 191AB,
191AT, 191GB, 191JB, 192AB, 192AT, 195CB, 197AB, 197GB and 198GB.
CAUTION : DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF
_______
CARBONFIBER REINFORCED PLASTIC.
R
EFF :
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(1) For panel 191JB:
(b) Make sure that the electrical connectors are clean and in the
correct condition.
(c) Connect the electrical connector to the anti collision light 6LV.
(4) Make sure that the gap x between the panels 192AT/191AT and
192AB/191AB is 2.0 +1.5 -1.5 mm (0.0787 +0.0590 -0.0590 in.).
NOTE : A maximum gap of 4.0 mm (0.1574 in.) between the edges of the
____
two panels is permitted if:
- the maximum value is for not more than 20% of the total
length of the panel edges,
- the panel edges and the gap sealant are in the correct
condition.
(5) TORQUE the screws (1) to between 0.35 and 0.45 m.daN (30.97 and 39.82
lbf.in).
Subtask 53-35-13-420-050-A
CAUTION : DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF
_______
CARBONFIBER REINFORCED PLASTIC.
(b) Make sure that the electrical connectors are clean and in the
correct condition.
EFF :
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Page 426
Aug 01/07
IAC
(c) Connect the electrical connector to the anti collision light 6LV.
R (4) Make sure that the clearance x between the panels 192AT and 191AT,
R and 192AB and 191AB is 2.0 +1.5 -1.5 mm (0.0787 +0.0590 -0.0590 in.).
(5) TORQUE the screws (1) to between 0.35 and 0.45 m.daN (30.97 and 39.82
lbf.in).
5. Close-up
________
Subtask 53-35-13-410-051
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-35-13
Page 427
Aug 01/07
IAC
TASK 53-35-13-000-002
Removal of the Quick-Release Access Panels from the Belly Fairing Structure
1. __________________
Reason for the Job
Self explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-35-13
Page 428
Aug 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-35-13-010-054
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(2) Put the warning notice on the slat/flap control lever to tell persons
not to operate the slats/flaps.
EFF :
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Page 429
Aug 01/07
IAC
4. Procedure
_________
Subtask 53-35-13-020-052
NOTE : On panel 191KB and panel 192KB you must disengage the pins (5)
____
attached to the cords (6).
EFF :
ALL 53-35-13
Page 430
Feb 01/07
IAC
Quick-Release Access Panels - Belly Fairing (LH)
Figure 405/TASK 53-35-13-991-004
R
EFF :
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Page 431
Feb 01/07
IAC
R Quick-Release Access Panels - Belly Fairing (LH)
R Figure 405A/TASK 53-35-13-991-004-B
R
EFF :
101-199, 53-35-13
Page 432
Feb 01/07
IAC
Quick-Release Access Panels - Belly Fairing (LH)
R Figure 405B/TASK 53-35-13-991-004-A
R
EFF :
901-999, 53-35-13
Page 433
Feb 01/07
IAC
Quick-Release Access Panels - Belly Fairing (RH)
Figure 406/TASK 53-35-13-991-005
R
EFF :
001-012, 014-099, 53-35-13
Page 434
Feb 01/07
IAC
R Quick-Release Access Panels - Belly Fairing (RH)
R Figure 406A/TASK 53-35-13-991-005-B
R
EFF :
101-199, 53-35-13
Page 435
Feb 01/07
IAC
Quick-Release Access Panels - Belly Fairing (RH)
R Figure 406B/TASK 53-35-13-991-005-A
R
EFF :
901-999, 53-35-13
Page 436
Feb 01/07
IAC
Quick-Release Access Panels - Typical Installation
Figure 407/TASK 53-35-13-991-006
R
EFF :
001-012, 014-099, 901-999, 53-35-13
Page 437
Feb 01/07
IAC
R **ON A/C 101-199,
R Subtask 53-35-13-020-052-A
R NOTE : On panel 191KB and panel 192KB you must disengage the pins (5)
____
R attached to the cords (6).
R
EFF :
101-199, 53-35-13
Page 438
Feb 01/07
IAC
R Quick-Release Access Panels - Typical Installation
R Figure 407A/TASK 53-35-13-991-006-A
EFF :
101-199, 53-35-13
Page 439
Feb 01/07
IAC
**ON A/C ALL
TASK 53-35-13-400-002
1. __________________
Reason for the Job
Self explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-35-13
Page 440
Aug 01/07
IAC
R C. Expendable Parts
R -------------------------------------------------------------------------------
R FIG.ITEM |DESIGNATION |IPC-CSN
R -------------------------------------------------------------------------------
R D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-35-13
Page 441
May 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-35-13-860-053
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(2) Make sure the warning notice is put on the slat/flap control lever,
to tell persons not to operate the flaps/slats.
(3) Make sure the adjustable access platform is in the required position.
EFF :
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Page 442
Aug 01/07
IAC
4. Procedure
_________
Subtask 53-35-13-560-052
R
(1) Clean the component interface and/or the adjacent area.
R (3) Do a check of the adhesive tape (2) and the profile sections (1) for
R damage. If necessary, replace the tape and/or the profile sections.
R (4) If you have removed the panels 191EB/192EB, do a check of the sealant
R bead on the lower belly-fairing structure for the correct condition.
R If the sealant bead is not in the correct condition, do the steps
R that follow:
R
R (a) Remove the used sealant bead from the lower side of the belly
R fairing structure with a SCRAPER - NON METALLIC.
R
R (b) Apply the release agent SPECIAL MATERIALS (Material No. 05-013A)
R to the panel in the area of the sealant bead.
R
EFF :
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Page 443
May 01/07
IAC
R Access Panel 195AB (196AB) and 195BB (196BB) - Location and Detail
R Figure 408/TASK 53-35-13-991-015- 12 (SHEET 1)
EFF :
ALL 53-35-13
Page 444
May 01/07
IAC
R Access Panel 195AB (196AB) and 195BB (196BB) - Location and Detail
R Figure 408/TASK 53-35-13-991-015- 22 (SHEET 2)
EFF :
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Page 445
May 01/07
IAC
R (d) Apply a new bead of the SEALANTS (Material No. 09-002) (Ref. TASK
51-76-11-300-001).
R (a) Make sure the sealing strip (8) is in the correct condition on
R access panel (7).
R (b) If necessary, remove the sealing strip (8) with a SCRAPER - NON
R METALLIC.
R (c) Clean the area with the CLEANING AGENTS (Material No. 11-026) and
R a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
R (d) Install the new sealing strip (8) on the access panel (7). Cut
R the sealing strip to the necessary length.
R
R (a) Make sure the sealing strip (9) is in the correct condition on
R access panel (10).
R (b) If necessary, remove the sealing strip (9) with a SCRAPER - NON
R METALLIC.
R (c) Clean the area with the CLEANING AGENTS (Material No. 11-026) and
R a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
R (d) Install the new sealing strip (9) on the access panel (10). Cut
R the sealing strip to the necessary length.
R (7) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 53-35-13-420-051
EFF :
ALL 53-35-13
Page 446
May 01/07
IAC
**ON A/C 901-999,
(2) On panel 191KB and/or panel 192KB, install the pins (5) and let the
panel hang down on the cords (6).
NOTE : When you tighten the studs, do not TORQUE to more than 0.3
____
m.daN (26.54 lbf.in).
R
EFF :
001-012, 014-099, 901-999, 53-35-13
Page 447
May 01/07
IAC
**ON A/C 101-199,
Subtask 53-35-13-420-051-A
(2) On panel 191KB and/or panel 192KB, install the pins (5) and let the
panel hang down on the cords (6).
NOTE : When you tighten the studs, do not TORQUE to more than 0.3
____
m.daN (26.54 lbf.in).
5. Close-up
________
Subtask 53-35-13-410-053
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-35-13
Page 448
Aug 01/07
IAC
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
ALL 53-35-13
Page 449
May 01/07
IAC
TASK 53-35-13-000-004
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-35-13
Page 450
May 01/07
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-35-13-010-055
A. Get Access
Subtask 53-35-13-860-054
(1) Depressurize the Green, Yellow and Blue hydraulic systems (Ref. TASK
29-10-00-864-001), (Ref. TASK 29-10-00-864-002) and (Ref. TASK 29-10-
00-864-003).
4. Procedure
_________
Subtask 53-35-13-020-056
(1) Remove the nuts (1), the washers (2) and the screws (3) from the
louver panel (4).
EFF :
ALL 53-35-13
Page 451
May 01/07
IAC
Louver Panel - Panel 147FB (148FB) - Location and Detail
R Figure 409/TASK 53-35-13-991-011
R
EFF :
001-012, 014-099, 53-35-13
Page 452
May 01/07
IAC
Louver Panel - Panel 147FB (148FB) - Location and Detail
R Figure 409A/TASK 53-35-13-991-011-A
R
EFF :
101-199, 901-999, 53-35-13
Page 453
May 01/07
IAC
TASK 53-35-13-400-004
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-35-13
Page 454
May 01/07
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-35-13-860-055
(1) Make sure that the aircraft is in the same configuration as for the
removal task.
(2) Depressurize the Green, Yellow and Blue hydraulic systems (Ref. TASK
29-10-00-864-001), (Ref. TASK 29-10-00-864-002) and (Ref. TASK 29-10-
00-864-003).
4. Procedure
_________
Subtask 53-35-13-560-054
EFF :
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Page 455
May 01/07
IAC
**ON A/C 001-012, 014-099,
Subtask 53-35-13-420-055
CAUTION : BE CAREFUL WHEN YOU INSTALL THE LOUVER PANEL. IF YOU INSTALL IT
_______
INCORRECTLY, THE BELLY FAIRING WILL PRESSURIZE AND CAUSE DAMAGE
TO THE STRUCTURE.
(1) Put the louver panel (4) in its correct installation position. Make
sure that the openings of the vanes point to the rear of the
aircraft.
(2) Install the screws (3), the washers (2) and the nuts (1).
Subtask 53-35-13-420-055-A
CAUTION : BE CAREFUL WHEN YOU INSTALL THE LOUVER PANEL. IF YOU INSTALL IT
_______
INCORRECTLY, THE BELLY FAIRING WILL PRESSURIZE AND CAUSE DAMAGE
TO THE STRUCTURE.
(1) Put the louver panel (4) in its correct installation position. Make
sure that the openings of the vanes point to the rear of the
aircraft.
(2) Install the screws (3), the washers (2) and the nuts (1).
5. Close-up
________
Subtask 53-35-13-410-054
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
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Page 456
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IAC
(3) Close the MLG doors (Ref. TASK 32-12-00-410-001).
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-35-13
Page 457
May 01/07
IAC
FITTINGS - DESCRIPTION AND OPERATION
____________________________________
1. _______
General
Fittings make possible the connection of structural parts directly to the
fuselage, or to those components that are attached to the fuselage.
2. ___________
Description
The fittings are made of aluminum alloy. They are machined from forgings or
sheet.
EFF :
ALL 53-36-00
Page 1
Feb 01/96
IAC
MISCELLANEOUS (EG : DRAINS) - DESCRIPTION AND OPERATION
_______________________________________________________
1. General
_______
A. Drain Assemblies
B. Overpressure Valves
2. Component
__________________
Location
(Ref. Fig. 001)
3. ___________
Description
Fuselage Drains:
The center fuselage drain assemblies have a rubber seal and an upper plate.
The rubber seal is sensitive to cabin pressure and will move to close or
open a water drain hole. The upper plate limits the movement of the rubber
seal when it moves up.
As the cabin pressurizes, the pressure sensitive rubber seal will move down
to close the drain hole. When the hole is closed, loss of cabin pressure
through the drain hole is prevented. When the cabin pressure decreases the
rubber seal will move up to its usual position and open the drain hole. Any
water that has collected will drain away through the main gear bay.
Overpressure Valves:
EFF :
ALL 53-39-00
Page 1
Feb 01/96
IAC
R Center Fuselage Drains - Component Location
Figure 001
EFF :
ALL 53-39-00
Page 2
Aug 01/96
IAC
The overpressure valves are sensitive to differential air pressures. The
valves open to bleed off excessive pressure when the belly fairing FWD
sections are in an overpressure condition. This operation maintains a normal
pressure throughout the belly fairing structure at all aircraft altitudes.
Each valve has a large piston positioned to close a bleed hole cut in the
structure. The piston is held in the normally closed position under spring
tension. Any overpressure will act on the piston and force the piston to
open against spring tension. As the piston opens, the overpressure bleeds
into the belly fairing AFT sections until an equal pressure again exists.
EFF :
ALL 53-39-00
Page 3
Feb 01/96
IAC
MISCELLANEOUS (EG : DRAINS) - INSPECTION/CHECK
______________________________________________
TASK 53-39-00-210-001
R Operational Check of Rubber Flap Drain Valve Holes in Pressure Floor from MLG
R Bay
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
R
No specific access platform 0.5 m (1 ft. 8 in.)
R No specific 1 PROBE - NON METALLIC, FLEXIBLE
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-39-00-010-050
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
EFF :
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Page 601
Nov 01/03
IAC
(2) Put the access platform in position under the main landing-gear bay.
4. Procedure
_________
Subtask 53-39-00-210-050
R A. Inspection Procedure
R (1) Do the operational check of the drain holes of the rubber flap
R drain-valves in the pressure floor from the main landing-gear bay:
R
R (a) Make sure that the drain holes in the forward ceiling area of the
R landing gear bay are not blocked.
R
R (c) Carefully push a PROBE - NON METALLIC, FLEXIBLE into each drain
R hole and make sure that the rubber seal operates correctly.
5. Close-up
________
Subtask 53-39-00-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-39-00
Page 602
Nov 01/03
IAC
R FWD Drain Holes - Component Location
Figure 601/TASK 53-39-00-991-001
EFF :
ALL 53-39-00
Page 603
Nov 01/03
IAC
VALVE - OVERPRESSURE - REMOVAL/INSTALLATION
___________________________________________
TASK 53-39-41-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-39-41-010-050
A. Get Access
(1) Put the access platform in position in zone 191 and 192.
EFF :
ALL 53-39-41
Page 401
May 01/05
IAC
4. Procedure
_________
Subtask 53-39-41-020-052
(1) Compress the spring (8) to remove the nuts (1) and shutter assembly
(2) easily.
(4) Remove the nuts (3), the bolts (4) and the spacers (5).
EFF :
ALL 53-39-41
Page 402
Feb 01/96
IAC
Overpressure Valve
Figure 401/TASK 53-39-41-991-001
EFF :
ALL 53-39-41
Page 403
Feb 01/96
IAC
TASK 53-39-41-400-002
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-39-41-869-050
(1) Make sure that the access platform is in position in zone 191 and
192.
(2) Make sure that the access panels 191EB, 191LB, 192EB, 192LB are
removed : (Ref. TASK 53-25-11-000-001)
Subtask 53-39-41-210-050
B. Inspection of Seal.
(1) Make sure that the seal of the shutter assembly is in good condition.
EFF :
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Page 404
May 01/05
IAC
4. Procedure
_________
Subtask 53-39-41-420-050
A. Installation of Component.
(Ref. Fig. 401/TASK 53-39-41-991-001)
(2) Install the bolts (4), the spacers (5) and the nuts (3).
(3) TORQUE the nuts (3) to between 0.35 and 0.45 m.daN (30.97 and 39.82
lbf.in).
(4) Put the shutter assembly (2) in position on the shaft (7).
(5) Compress the spring (8) to install the Shutter assembly (2) and nut
(1) easily.
(7) TORQUE the nut (1) to between 0.70 and 0.80 m.daN (61.94 and 70.79
lbf.in).
(8) Make sure that the travel range of the shutter assembly (2) is
correct.
5. Close-up
________
Subtask 53-39-41-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-39-41
Page 405
Feb 01/96
IAC
REAR FUSELAGE - DESCRIPTION AND OPERATION
_________________________________________
1. General
_______
The rear fuselage assembly is a pressurized area, which extends from FR47 to
FR70. The passenger compartment floor divides the rear fuselage into its
upper and lower fuselage sections.
The upper section of the fuselage assembly contains:
- the aft section of the passenger cabin
- the AFT passenger/crew doors (Ref. 52-13-00), installed between FR66 and
FR68, left and right
- the aft utility area
- the galleys
- the lavatories.
The lower section of the fuselage assembly contains:
- the AFT cargo compartment
- the AFT cargo-compartment door (Ref. 52-32-00), installed on the right
side of the fuselage, between FR52A and FR56
- the BULK cargo compartment.
R The rear fuselage assembly is a pressurized area, which extends from FR47 to
R FR70. The passenger compartment floor divides the rear fuselage into its
R upper and lower fuselage sections.
R The upper section of the fuselage assembly contains:
R - the aft section of the passenger cabin
R - the AFT emergency exit doors (Ref. 52-22-00), installed between FR47.2 and
R FR47.4, left and right
R - the AFT passenger/crew doors (Ref. 52-13-00), installed between FR66 and
R FR68, left and right
R - the aft utility area
R - the galleys
R - the lavatories.
R The lower section of the fuselage assembly contains:
R - the AFT cargo compartment
R - the AFT cargo-compartment door (Ref. 52-32-00), installed on the right
R side of the fuselage, between FR52A and FR56
R - the BULK cargo compartment
R - the BULK cargo-compartment door (Ref. 52-33-00), installed on the right
R side of the fuselage, between FR60 and FR62.
EFF :
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Page 1
Feb 01/07
IAC
R **ON A/C 901-999,
The rear fuselage assembly is a pressurized area, which extends from FR47 to
FR70. The passenger compartment floor divides the rear fuselage into its
upper and lower fuselage sections.
The upper section of the fuselage assembly contains:
- the aft section of the passenger cabin
- the AFT passenger/crew doors (Ref. 52-13-00), installed between FR66 and
FR68, left and right
- the aft utility area
- the galleys
- the lavatories.
The lower section of the fuselage assembly contains:
- the AFT cargo compartment
- the AFT cargo-compartment door (Ref. 52-32-00), installed on the right
side of the fuselage, between FR55A and FR59
- the BULK cargo compartment.
2. __________________
Component Location
EFF :
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Page 2
Feb 01/07
IAC
Rear Fuselage
Figure 001
R
EFF :
001-012, 014-099, 901-999, 53-40-00
Page 3
Feb 01/07
IAC
R Rear Fuselage
R Figure 001A
EFF :
101-199, 53-40-00
Page 4
Feb 01/07
IAC
R **ON A/C ALL
3. Description
___________
B. Cargo Compartments
Access to the AFT cargo compartment is through the AFT cargo-compartment
door. The BULK cargo compartment is installed behind the AFT cargo
compartment. Nets divide the two cargo compartments. Access to the BULK
cargo compartment is through the AFT cargo compartment.
R B. Cargo Compartments
R Access to the AFT cargo compartment is through the AFT cargo-compartment
R door. The BULK cargo compartment is installed behind the AFT cargo
R compartment. Access to the BULK cargo compartment is through the BULK
R cargo-compartment door or through the AFT cargo compartment.
C. Dorsal Fin
The dorsal fin (Ref. 53-45-00) is a fairing, which is installed at the
leading edge of the vertical stabilizer-to-fuselage joint. The fairing
permits the airflow to flow smoothly around the joint, and keeps the air
turbulence to a minimum.
D. Drains
Drain valves (Ref. 53-49-00) are installed in the bottom of the fuselage,
at locations where it is possible for water and condensation to collect.
Drain holes in the internal structure let the water and condensation flow
to the drain valves.
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Page 5
Feb 01/07
IAC
MAIN STRUCTURE - DESCRIPTION AND OPERATION
__________________________________________
1. _______
General
The main structure of the rear-fuselage is primary, made of aluminum-alloy.
It has skin plates, frames, stringers and skin stiffeners, they are riveted
together to make the fuselage shell. Top beams and seat tracks, riveted to
crossbeams make the cabin floor stronger. Support struts and diagonal braces
make the fuselage structure stronger.
2. Component
__________________
Location
R (Ref. Fig. 001)
3. Description
___________
R A. Skin Plates
R The skin plates are made of aluminum-alloy sheets and stringers which are
R riveted to them make them stronger. Skin plates are preformed to the
R contour of the fuselage before they are riveted to the frames.
R B. Frames
R The frames are the stiffeners that go around the fuselage shell. They are
R made of aluminum-alloy sections which are formed or machined. Clips, with
R cut-outs for stringers, are riveted between the frames and the skin
R plates. Door frames and beams make the frame structure stronger in the
R area of the aft passenger/crew and cargo compartment(s) doors.
R D. Crossbeams
R The crossbeams are made of aluminum-alloy C-sections which are extruded.
R They are riveted to the frames. They are the primary structure of the
R cabin floor. Support struts which are riveted to the crossbeams make them
R stronger.
EFF :
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Page 1
Nov 01/04
IAC
Rear Fuselage Main-Structure
Figure 001 (SHEET 1)
EFF :
ALL 53-41-00
Page 2
Feb 01/96
IAC
Rear Fuselage Main-Structure
Figure 001 (SHEET 2)
EFF :
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Page 3
Feb 01/96
IAC
R F. Floor Panels
R The floor panels are made of honeycomb core which is bonded between
R Glassfiber Reinforced-Polyester or aluminum sheets. Screws attach the
R floor panels to the floor structure.
R (2) The rear pressure-bulkhead has a frame made of aluminum alloy which
R is machined. The segments, made of aluminum-alloy sheets, are riveted
R to the frame to make a pressure diaphragm.
R (3) The top part of the frame is made stronger to support the fwd
R attachment fittings of the vertical stabilizer.
R H. Fittings
R The fittings let structural parts be directly connected to the fuselage
R or to the components already connected to the fuselage.
EFF :
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Page 4
Nov 01/04
IAC
MAIN STRUCTURE - INSPECTION/CHECK
_________________________________
TASK 53-41-00-210-002
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page 601
May 01/06
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-074
A. Get Access
(2) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-057
(a) Make sure that you examine the frames, the stringers and the
internal surface of the fuselage skin.
R
EFF :
001-012, 014-099, 53-41-00
Page 602
May 01/06
IAC
Skin Cutout of the ADF 2 Antenna
Figure 601/TASK 53-41-00-991-003
R
EFF :
001-012, 014-099, 53-41-00
Page 603
May 01/06
IAC
(b) Look for corrosion and other damage to the metal parts and to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion-protection data.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
(b) Refer to the ASRM (Ref. ASRM 51-11-11-001) for the allowable
damage limits.
(c) Repair the minor damage (Ref. AMM 517311300001) or (Ref. AMM
517311300004).
(d) If you find other damage to the metal parts, that is more than
the limits for minor damage, you must:
1
_ Refer to the ASRM for the material details, the item
identification and the action/repair data:
- for the skin plates, refer to the ASRM (Ref. ASRM 53-41-11-
001)
- for the frames, refer to the ASRM (Ref. ASRM 53-41-12-001)
- for the stringers, refer to the ASRM (Ref. ASRM 53-41-13-
001).
5. Close-up
________
Subtask 53-41-00-410-073
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
001-012, 014-099, 53-41-00
Page 604
May 01/06
IAC
R **ON A/C ALL
TASK 53-41-00-210-003
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 605
May 01/06
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-070
A. Get Access
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Page 606
Feb 01/07
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(3) Remove the door frame linings (Ref. TASK 25-23-45-000-003) (Ref. TASK
25-23-45-000-004).
(4) Remove the insulation blankets from the inspection area (Ref. TASK
25-80-00-000-001).
Subtask 53-41-00-110-059
B. Clean the inspection area with CLEANING AGENTS (Material No. 11-003) and
a lint-free cloth.
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
4. Procedure
_________
Subtask 53-41-00-210-056
A. Inspection
R (1) Examine the internal structure around the aft passenger/crew door
R above cabin floor level. Do this between FR65 and FR69 and between
R stringer 6 and stringer 23, LH/RH and look for:
- corrosion,
R - skin distortion.
R NOTE : The door entrance area between FR66 and FR68, between stringer
____
R 22 and stringer 23, LH/RH is not examined in this procedure.
EFF :
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Page 607
Nov 01/04
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R Internal Structure around the Aft Passenger/Crew Door-Cutouts
Figure 602/TASK 53-41-00-991-004
EFF :
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Page 608
Aug 01/96
IAC
(2) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-001) for the
correct repair procedure.
5. Close-up
________
Subtask 53-41-00-916-050
Subtask 53-41-00-410-071
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page 609
Nov 01/05
IAC
TASK 53-41-00-210-004
Detailed Visual Inspection of Fuselage Internal Structure around AFT Cargo Door
Cutout between STGR23 and STGR38
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page 610
Nov 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page 611
Nov 01/07
IAC
3. __________
Job Set-up
Subtask 53-41-00-010-075
A. Get Access
R (2) Put the ACCESS PLATFORM 2M (6 FT) in position below the cargo door.
R (3) If installed, remove the rear additional center-tank (Ref. TASK 28-
R 11-27-000-001).
R
R (4) Remove the aft cargo-compartment sidewall linings 152HW and 152DW
R (Ref. TASK 25-55-12-000-001).
R (5) Remove the aft cargo-compartment floor panels 152EF, 152FF, 152MF,
R and 152NF (Ref. TASK 53-42-14-000-001).
(7) Remove the insulation blankets from the inspection area (Ref. TASK
25-80-00-000-001).
R (8) Clean the inspection area with the CLEANING AGENTS (Material No. 11-
R 026) and a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
R Subtask 53-41-00-010-075-A
R A. Get Access
R (2) Put the ACCESS PLATFORM 2M (6 FT) in position below the cargo door.
EFF :
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Page 612
Nov 01/07
IAC
R (3) If installed, remove the rear additional center-tank (Ref. TASK 28-
R 11-27-000-001).
R (4) Remove the aft cargo-compartment sidewall linings 152DW and 152HW
R (Ref. TASK 25-55-12-000-001).
R (5) Remove the aft cargo-compartment floor panels 152RG, 152QG, 152MF,
R and 152NF (Ref. TASK 53-42-14-000-001).
R (7) Remove the insulation blankets from the inspection area (Ref. TASK
R 25-80-00-000-001).
R (8) Clean the inspection area with CLEANING AGENTS (Material No. 11-026)
R and a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
R Subtask 53-41-00-010-075-B
R A. Get Access
R (2) Put an ACCESS PLATFORM 2M (6 FT) in position below the cargo door.
R (3) If installed, remove the rear additional center-tank (Ref. TASK 28-
R 11-27-000-001).
R (4) Remove the aft cargo-compartment sidewall linings 152TW and 162AW
R (Ref. TASK 25-55-12-000-001).
R (5) Remove the aft cargo-compartment floor panels 152WG, 152XG, 162BF,
R and 162CF (Ref. TASK 53-42-14-000-001).
R (7) Remove the insulation blankets from the inspection area (Ref. TASK
R 25-80-00-000-001).
R
EFF :
101-199, 901-999, 53-41-00
Page 613
Nov 01/07
IAC
R (8) Clean the inspection area with CLEANING AGENTS (Material No. 11-026)
R and a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
4. Procedure
_________
Subtask 53-41-00-210-058
(a) Make sure that you examine the frames, the stringers and the
internal surface of the fuselage skin.
(b) Look for corrosion and other damage to the metal parts and to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion-protection data.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
(b) Refer to the ASRM (Ref. ASRM 51-11-11-001) for the allowable
damage limits.
(c) Repair the minor damage (Ref. AMM 517311300001) or (Ref. AMM
517311300004).
EFF :
ALL 53-41-00
Page 614
Nov 01/07
IAC
Internal Structure around the AFT Cargo-Compartment Door-Cutout
Figure 603/TASK 53-41-00-991-005
EFF :
ALL 53-41-00
Page 615
Nov 01/07
R
IAC
(d) If you find other damage to the metal parts, that is more than
the limits for minor damage, you must:
1
_ Refer to the ASRM for the material details, the item
identification and the action/repair data:
- for the skin plates, refer to the ASRM (Ref. ASRM 53-41-11-
001)
- for the frames, refer to the ASRM (Ref. ASRM 53-41-12-001)
- for the stringers, refer to the ASRM (Ref. ASRM 53-41-13-
001).
Subtask 53-41-00-210-058-A
(a) Make sure that you examine the frames, the stringers and the
internal surface of the fuselage skin.
(b) Look for corrosion and other damage to the metal parts and to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion-protection data.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
(b) Refer to the ASRM (Ref. ASRM 51-11-11-001) for the allowable
damage limits.
(c) Repair the minor damage (Ref. AMM 517311300001) or (Ref. AMM
517311300004).
EFF :
ALL 53-41-00
Page 616
Nov 01/07
R
IAC
(d) If you find other damage to the metal parts, that is more than
the limits for minor damage, you must:
1
_ Refer to the ASRM for the material details, the item
identification and the action/repair data:
- for the skin plates, refer to the ASRM (Ref. ASRM 53-41-11-
001)
- for the frames, refer to the ASRM (Ref. ASRM 53-41-12-001)
- for the stringers, refer to the ASRM (Ref. ASRM 53-41-13-
001).
5. Close-up
________
Subtask 53-41-00-916-051
Subtask 53-41-00-410-074
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(6) If removed, install the rear additional center tank (Ref. AMM
28-11-27, Page Block 401).
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Page 617
Nov 01/07
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(8) Close the AFT cargo-compartment door (Ref. TASK 52-30-00-860-002) or
(Ref. TASK 52-30-00-860-004).
(9) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R Subtask 53-41-00-410-074-A
R B. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (4) Install the aft cargo-compartment floor panels 152RG, 152QG, 152MF,
R and 152NF (Ref. TASK 53-42-14-400-001).
R (5) Install the aft cargo-compartment sidewall linings 152DW and 152HW
R (Ref. TASK 25-55-12-400-001).
R (6) If removed, install the rear additional center-tank (Ref. TASK 28-11-
R 27-400-001).
R (9) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
R
EFF :
001-012, 014-099, 101-199, 53-41-00
Page 618
Nov 01/07
IAC
R **ON A/C 901-999,
R Subtask 53-41-00-410-074-B
R B. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (4) Install the aft cargo-compartment floor panels 152WG, 152XG, 162BF,
R and 162CF (Ref. TASK 53-42-14-400-001).
R (5) Install the aft cargo-compartment sidewall linings 152TW and 162AW
R (Ref. TASK 25-55-12-400-001).
R (6) If removed, install the rear additional center-tank (Ref. TASK 28-11-
R 27-400-001).
R (9) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
R
EFF :
901-999, 53-41-00
Page 619
Nov 01/07
IAC
R **ON A/C ALL
TASK 53-41-00-210-005
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page 620
Nov 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-076
A. Get Access
(3) If installed, remove the rear additional center tank (Ref. AMM
28-11-27, Page Block 401).
(4) Remove the lower sidewall panels 252GW, 252KW and 252NW of the
passenger compartment (Ref. TASK 25-23-44-000-001).
(6) Cleaning.
EFF :
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Page 621
Nov 01/07
R
IAC
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______
MATERIALS ONLY WITH A GOOD SUPPLY OF AIR.
OBEY THE MANUFACTURERS INSTRUCTIONS.
PUT ON PROTECTIVE CLOTHING.
DO NOT GET THEM IN YOUR MOUTH.
DO NOT SMOKE.
DO NOT BREATHE THE GAS.
THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT.
GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
(a) Clean the inspection area with CLEANING AGENTS (Material No. 11-
003) and a lint-free cloth.
Subtask 53-41-00-010-076-A
A. Get Access
(3) If installed, remove the rear additional center tank (Ref. AMM
28-11-27, Page Block 401).
(4) Remove the lower sidewall panels 252NW, 252RW and 252UW of the
passenger compartment (Ref. TASK 25-23-44-000-001).
(6) Cleaning.
EFF :
ALL 53-41-00
Page 622
Nov 01/07
R
IAC
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______
MATERIALS ONLY WITH A GOOD SUPPLY OF AIR.
OBEY THE MANUFACTURERS INSTRUCTIONS.
PUT ON PROTECTIVE CLOTHING.
DO NOT GET THEM IN YOUR MOUTH.
DO NOT SMOKE.
DO NOT BREATHE THE GAS.
THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT.
GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
(a) Clean the inspection area with CLEANING AGENTS (Material No. 11-
003) and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-059
(a) Make sure that you examine the beam and the internal surface of
the fuselage skin.
(b) Look for corrosion and other damage to the metal parts.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion-protection data.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
EFF :
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Page 623
Nov 01/07
R
IAC
Fuselage Structure at the Internal Attachment of the Hinge Fittings at the AFT
Cargo-Compartment Door
Figure 604/TASK 53-41-00-991-006
R EFF :
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53-41-00 Page 624
Nov 01/07
IAC
(b) Refer to the ASRM (Ref. ASRM 51-11-11-001) for the allowable
damage limits.
(c) Repair the minor damage (Ref. AMM 51-73-11-300-001) or (Ref. AMM
51-73-11-300-004).
(d) If you find other damage to the metal parts, that is more than
the limits for minor damage, you must:
1
_ Refer to the ASRM for the material details, the item
identification and the action/repair data:
- For the skin plates, refer to the ASRM (Ref. ASRM 53-41-11-
001).
- For the beam, refer to the ASRM (Ref. ASRM 53-41-49-001).
Subtask 53-41-00-210-059-A
(a) Make sure that you examine the beam and the internal surface of
the fuselage skin.
(b) Look for corrosion and other damage to the metal parts.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion-protection data.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
(b) Refer to the ASRM (Ref. ASRM 51-11-11-001) for the allowable
damage limits.
EFF :
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Page 625
Nov 01/07
R
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(c) Repair the minor damage (Ref. AMM 51-73-11-300-001) or (Ref. AMM
51-73-11-300-004).
(d) If you find other damage to the metal parts, that is more than
the limits for minor damage, you must:
1
_ Refer to the ASRM for the material details, the item
identification and the action/repair data:
- For the skin plates, refer to the ASRM (Ref. ASRM 53-41-11-
001).
- For the beam, refer to the ASRM (Ref. ASRM 53-41-49-001).
5. Close-up
________
Subtask 53-41-00-410-075
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the lower sidewall panels 252GW, 252KW and 252NW of the
passenger compartment (Ref. TASK 25-23-44-400-001).
(4) If removed, install the rear additional center tank (Ref. AMM
28-11-27, Page Block 401).
(6) Close the aft cargo compartment door (Ref. TASK 52-30-00-860-002).
(7) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page 626
Nov 01/07
R
IAC
**ON A/C 901-999,
Subtask 53-41-00-410-075-A
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the lower sidewall panels 252NW, 252RW and 252UW of the
passenger compartment (Ref. TASK 25-23-44-400-001).
(4) If removed, install the rear additional center tank (Ref. AMM
28-11-27, Page Block 401).
(6) Close the aft cargo compartment door (Ref. TASK 52-30-00-860-002).
(7) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
901-999, 53-41-00
Page 627
Nov 01/07
IAC
**ON A/C ALL
TASK 53-41-00-210-006
Detailed Visual Inspection of Fuselage AFT Cargo Door Hinge Fittings and
External Attachment Area
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page 628
Nov 01/07
R
IAC
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-115
A. Get Access
(1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position at the aft
cargo-compartment door.
(2) If installed, remove the aft Additional Center Tank (ACT) (Ref. AMM
28-11-27, Page Block 401).
EFF :
ALL 53-41-00
Page 629
Nov 01/07
R
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(3) Carefully clean the inspection area with the CLEANING AGENTS
(Material No. 11-026) and a clean lint-free cloth MISCELLANEOUS
(Material No. 19-003).
4. Procedure
_________
Subtask 53-41-00-210-060
A. Inspection
(1) Examine the hinge fittings and external attachment at the AFT
cargo-compartment door for:
- cracks,
- corrosion.
Subtask 53-41-00-865-050
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
121VU HYDRAULIC/HYD POWER/Y 3803GX N30
122VU DOORS/CARGO 1MJ T12
123VU Y HYD/ELEC/PUMP 3802GX AB06
Subtask 53-41-00-110-063
C. Carefully clean the inspection area with the CLEANING AGENTS (Material
No. 11-026) and a clean lint-free cloth MISCELLANEOUS (Material No. 19-
003).
R
EFF :
ALL 53-41-00
Page 630
Nov 01/07
IAC
Hinge Fittings at the AFT Cargo-Compartment Door
Figure 605/TASK 53-41-00-991-008
R
EFF :
ALL 53-41-00
Page 631
Nov 01/07
IAC
Subtask 53-41-00-210-061
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-46-11-101) for the
____
correct repair procedure.
5. Close-up
________
Subtask 53-41-00-916-090
Subtask 53-41-00-865-051
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
3803GX, 1MJ, 3802GX
Subtask 53-41-00-410-112
C. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) If removed, install the rear additional center tank (Ref. AMM
28-11-27, Page Block 401).
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
ALL 53-41-00
Page 632
Nov 01/07
IAC
**ON A/C 101-199,
TASK 53-41-00-210-007
Detailed Visual Inspection of Fuselage Skin under Bulk Cargo Door Scuff Plate
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-077
A. Get Access
EFF :
101-199, 53-41-00
Page 633
Nov 01/07
R
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(3) Remove the scuff plate at the BULK cargo-compartment door (Ref. TASK
53-45-15-000-002).
4. Procedure
_________
Subtask 53-41-00-210-063
A. Inspection
(1) Examine the fuselage skin below the scuff plate for:
- corrosion,
- cracks,
5. Close-up
________
Subtask 53-41-00-410-076
A. Close Access
(1) Install the scuff plate at the BULK cargo-compartment door (Ref. TASK
53-45-15-400-002).
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
101-199, 53-41-00
Page 634
Nov 01/07
R
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Scuff Plate and Sealing Profile at the BULK Cargo-Compartment Door
Figure 606/TASK 53-41-00-991-009
EFF :
101-199, 53-41-00
Page 635
Nov 01/07
R
IAC
TASK 53-41-00-210-008
Special Detailed Inspection of Fuselage Skin of Bulk Cargo Door Cutout and
Sealing Profile at Upper Corners
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
101-199, 53-41-00
Page 636
Nov 01/07
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-078
A. Get Access
Subtask 53-41-00-860-062
(1) Make sure that the surface of the inspection area is clean and
smooth.
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR
MOUTH OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10
AND 15 MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS,
FLAMMABLE AND SKIN IRRITANTS.
(2) If necessary, clean the surface of the inspection area with the
CLEANING AGENTS (Material No. 11-004) and a MISCELLANEOUS (Material
No. 19-003).
EFF :
101-199, 53-41-00
Page 637
Nov 01/07
R
IAC
Upper Corners of the Cutout and Sealing Profile at the BULK Cargo-Compartment
Door
Figure 607/TASK 53-41-00-991-010
R EFF :
101-199,
53-41-00 Page 638
Nov 01/07
IAC
(3) If necessary, make the surface of the inspection area smooth with the
abrasive cloth, grade 280.
(4) Make sure the inspection area is clean and dry before you continue.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
4. Procedure
_________
Subtask 53-41-00-210-064
(1) Do the special detailed inspection of the fuselage skin at the cutout
for the bulk cargo door. Do this at the forward and aft upper corners
of the cutout (Ref. NTM 534171-Part.6).
(2) Write a report about the damage you find during the inspection
procedure.
R
EFF :
101-199, 53-41-00
Page 639
Nov 01/07
IAC
(3) If you find damage:
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
5. Close-up
________
Subtask 53-41-00-370-059
Subtask 53-41-00-410-077
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
101-199, 53-41-00
Page 640
Nov 01/07
IAC
R **ON A/C 001-012, 014-099,
TASK 53-41-00-210-009
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
A. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
001-012, 014-099, 53-41-00
Page 641
Feb 01/08
IAC
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-080
A. Get Access
(1) Remove the belly-fairing access panels 197BB and 197GB (Ref. TASK 53-
35-13-000-001) (Ref. TASK 53-35-13-000-002).
(2) Clean the inspection area with the CLEANING AGENTS (Material No. 11-
026) and a clean lint free cloth MISCELLANEOUS (Material No. 19-003).
R
R
EFF :
001-012, 014-099, 53-41-00
Page 642
Feb 01/08
IAC
4. Procedure
_________
R
(Ref. Fig. 608/TASK 53-41-00-991-025)
R
Subtask 53-41-00-210-066
R A. Inspection
R
R (1) Do the detailed inspection of the lower skin of the lap joints in the
R crack stopper areas. Do this at STGR32 LH, between FR47 and FR53.
R (a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
R damage.
R
EFF :
001-012, 014-099, 53-41-00
Page 643
Feb 01/08
IAC
Long Lap Joints at STGR32
Figure 608/TASK 53-41-00-991-025
R
EFF :
001-012, 014-099, 101-199, 53-41-00
Page 644
Nov 01/07
IAC
5. Close-up
________
Subtask 53-41-00-410-079
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the belly-fairing access panels 197BB and 197GB (Ref. TASK
53-35-13-400-001) (Ref. TASK 53-35-13-400-002).
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
R
EFF :
001-012, 014-099, 53-41-00
Page 645
Feb 01/08
IAC
R **ON A/C 101-199,
R TASK 53-41-00-210-009-A
R WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
R START A TASK ON OR NEAR:
R - THE FLIGHT CONTROLS
R - THE FLIGHT CONTROL SURFACES
R - THE LANDING GEAR AND THE RELATED DOORS
R - COMPONENTS THAT MOVE.
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R
EFF :
101-199, 53-41-00
Page 646
Feb 01/08
IAC
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R 3. __________
Job Set-up
R Subtask 53-41-00-010-178
R A. Get Access
R (1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the
R belly-fairing access panels.
R (2) Remove the belly-fairing access panels 197KB, 198KB and 197GB, 198GB
R (Ref. TASK 53-35-13-000-001) (Ref. TASK 53-35-13-000-002).
R Subtask 53-41-00-100-052
R B. Cleaning
R (1) Clean the inspection area with the CLEANING AGENTS (Material No. 11-
R 026) and a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
R
EFF :
101-199, 53-41-00
Page 647
Feb 01/08
IAC
R 4. Procedure
_________
R Subtask 53-41-00-210-146
R A. Detailed Inspection
R (1) Do the detailed inspection of the lower skin of the lap joints in the
R crack stopper areas. Do this at STGR32 LH, between FR47 and FR48 and
R STGR32 RH, between FR47 and FR47.5.
R (a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
R damage.
R 5. Close-up
________
R Subtask 53-41-00-410-174
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Install the belly-fairing access panels 197KB, 198KB and 197GB, 198GB
R (Ref. TASK 53-35-13-400-001) (Ref. TASK 53-35-13-400-002).
R (4) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
R
EFF :
101-199, 53-41-00
Page 648
Feb 01/08
IAC
R **ON A/C 901-999,
R TASK 53-41-00-210-009-B
R WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
R START A TASK ON OR NEAR:
R - THE FLIGHT CONTROLS
R - THE FLIGHT CONTROL SURFACES
R - THE LANDING GEAR AND THE RELATED DOORS
R - COMPONENTS THAT MOVE.
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R
EFF :
901-999, 53-41-00
Page 649
Feb 01/08
IAC
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R 3. __________
Job Set-up
R Subtask 53-41-00-010-179
R A. Get Access
R (1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the
R belly-fairing access panels.
R (2) Remove the belly-fairing access panels 197BB and 197GB (Ref. TASK 53-
R 35-13-000-001) (Ref. TASK 53-35-13-000-002).
R Subtask 53-41-00-100-051
R B. Cleaning
R (1) Clean the inspection area with the CLEANING AGENTS (Material No. 11-
R 026) and a clean lint free cloth MISCELLANEOUS (Material No. 19-003).
R
EFF :
901-999, 53-41-00
Page 650
Feb 01/08
IAC
R 4. Procedure
_________
R Subtask 53-41-00-210-147
R A. Detailed Inspection
R (1) Do the detailed inspection of the lower skin of the lap joints in the
R crack stopper areas. Do this at STGR32 LH, between FR47/51 and FR57.
R (a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
R damage.
R 5. Close-up
________
R Subtask 53-41-00-410-175
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Install the belly-fairing access panels 197BB and 197GB (Ref. TASK
R 53-35-13-400-001) (Ref. TASK 53-35-13-400-002).
R (4) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
R
EFF :
901-999, 53-41-00
Page 651
Feb 01/08
IAC
Long Lap Joints at STGR32
Figure 608A/TASK 53-41-00-991-025-A
R
EFF :
901-999, 53-41-00
Page 652
Feb 01/08
IAC
**ON A/C ALL
TASK 53-41-00-210-010
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page 653
Feb 01/08
R
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3. __________
Job Set-up
Subtask 53-41-00-010-082
A. Get Access
(1) Remove the door linings 261HW, 261JW, 261RW, 261SW, 262HW, 262JW,
262RW, 262SW.
(2) Remove the insulation blankets from the inspection area (Ref. TASK
25-80-00-000-001).
(3) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth.
Subtask 53-41-00-010-082-A
A. Get Access
(2) Remove the insulation blankets from the inspection area (Ref. TASK
25-80-00-000-001).
EFF :
ALL 53-41-00
Page 654
Feb 01/08
R
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(3) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-067
A. Inspection
5. Close-up
________
Subtask 53-41-00-410-081
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-41-00
Page 655
Feb 01/08
R
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Top Corners of the Aft Passenger/Crew Door-Cutout, Fuselage Skin and Internal
Doubler
Figure 609/TASK 53-41-00-991-012
EFF :
ALL
53-41-00 Page 656
Feb 01/08
R
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(3) Install the door frame linings 261HW, 261JW, 261RW, 261SW and 262HW,
262JW, 262RW, 262SW.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 53-41-00-410-081-A
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the door frame linings 261UW, 261VW, 262UW, 262VW.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page 657
Feb 01/08
R
IAC
**ON A/C ALL
TASK 53-41-00-210-011
Detailed Visual Inspection of Frame Splices and Adjacent Area from FR53 to
FR60, located above Stringer 18 RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
A. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page 658
Feb 01/08
R
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3. __________
Job Set-up
Subtask 53-41-00-010-083
A. Get Access
(1) Remove the right upper sidewall panels 252PW, 252LW, 252HW (Ref. TASK
25-23-43-000-001).
(2) Remove the insulation blankets from the inspection area (Ref. TASK
25-80-00-000-001).
(3) Clean the inspection area with the CLEANING AGENTS (Material No. 11-
026) and a clean lint free cloth MISCELLANEOUS (Material No. 19-003).
4. Procedure
_________
Subtask 53-41-00-210-068
A. Inspection
(1) Examine the frame splices at FR53 thru FR56 for cracks.
5. Close-up
________
Subtask 53-41-00-410-082
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the right upper sidewall panels 252PW, 252LW, 252HW
(Ref. TASK 25-23-43-400-001).
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page 659
Feb 01/08
R
IAC
Frame Splice at FR53 thru FR56
Figure 610/TASK 53-41-00-991-013
EFF :
ALL 53-41-00
Page 660
Feb 01/08
R
IAC
TASK 53-41-00-210-012
Detailed Visual Inspection of AFT Cargo Door Lock Fittings and Surrounding
Structure between Stringer 41 RH to Door Sill (6 places)
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page 661
Feb 01/08
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-087
A. Get Access
(3) If installed, remove the rear additional center tank (Ref. AMM
28-11-27, Page Block 401).
EFF :
ALL 53-41-00
Page 662
Feb 01/08
R
IAC
(5) Remove the insulation blankets from the inspection area (Ref. TASK
25-80-00-000-001).
Subtask 53-41-00-010-087-A
A. Get Access
(3) If installed, remove the rear additional center tank (Ref. AMM
28-11-27, Page Block 401).
(5) Remove the insulation blankets from the inspection area (Ref. TASK
25-80-00-000-001).
Subtask 53-41-00-110-069
B. Cleaning
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
R
EFF :
ALL 53-41-00
Page 663
Feb 01/08
IAC
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-070
(1) Do a detailed visual inspection of the lock fittings and the adjacent
structure around the aft cargo-compartment door. Do this between FR53
and FR55A.
(a) Look for corrosion and other damage to the metal parts and to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion-protection data.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
(b) Refer to the ASRM (Ref. ASRM 51-11-11-001) for the allowable
damage limits.
(c) Repair the minor damage (Ref. AMM 517311300001) or (Ref. AMM
517311300004).
(d) If you find other damage to the metal parts, that is more than
the limits for minor damage, you must:
1
_ Refer to the ASRM for the material details, the item
identification and the action/repair data:
- for the skin plates, refer to the ASRM (Ref. ASRM 53-41-11-
001)
- for the frames, refer to the ASRM (Ref. ASRM 53-41-12-001)
EFF :
ALL 53-41-00
Page 664
Feb 01/08
R
IAC
Lock Fittings and Adjacent Structure at the AFT Cargo-Compartment Door
Figure 611/TASK 53-41-00-991-015
EFF :
ALL 53-41-00
Page 665
Feb 01/08
R
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- for the stringers, refer to the ASRM (Ref. ASRM 53-41-13-
001).
Subtask 53-41-00-210-070-A
(1) Do a detailed visual inspection of the lock fittings and the adjacent
structure around the aft cargo-compartment door. Do this between FR56
and FR58A.
(a) Look for corrosion and other damage to the metal parts and to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion-protection data.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
(b) Refer to the ASRM (Ref. ASRM 51-11-11-001) for the allowable
damage limits.
(c) Repair the minor damage (Ref. AMM 517311300001) or (Ref. AMM
517311300004).
(d) If you find other damage to the metal parts, that is more than
the limits for minor damage, you must:
1
_ Refer to the ASRM for the material details, the item
identification and the action/repair data:
- for the skin plates, refer to the ASRM (Ref. ASRM 53-41-11-
001)
- for the frames, refer to the ASRM (Ref. ASRM 53-41-12-001)
- for the stringers, refer to the ASRM (Ref. ASRM 53-41-13-
001).
EFF :
ALL 53-41-00
Page 666
Feb 01/08
R
IAC
**ON A/C ALL
5. Close-up
________
Subtask 53-41-00-916-053
Subtask 53-41-00-410-087
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) If removed, install the rear additional center tank (Ref. AMM
28-11-27, Page Block 401).
(7) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page 667
Feb 01/08
R
IAC
**ON A/C 901-999,
Subtask 53-41-00-410-087-A
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) If removed, install the rear additional center tank (Ref. AMM
28-11-27, Page Block 401).
(7) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
901-999, 53-41-00
Page 668
Feb 01/08
IAC
**ON A/C ALL
TASK 53-41-00-210-014
Detailed Visual Inspection of Fuselage Internal Structure between FR46 and FR65
including AFT Face of Pressure Bulkhead from STGR 38 LH/RH to Bottom CenterLine
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-41-00
Page 669
Feb 01/08
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-090
A. Get Access
R
EFF :
ALL 53-41-00
Page 670
Feb 01/08
IAC
(4) Remove the fixed partition at FR47 (Ref. TASK 25-55-11-000-001).
(5) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-071
A. Inspection.
R
EFF :
ALL 53-41-00
Page 671
Feb 01/08
IAC
Fuselage Internal Structure FR46 thru FR65
Figure 612/TASK 53-41-00-991-016
R
EFF :
ALL 53-41-00
Page 672
Feb 01/08
IAC
5. Close-up
________
Subtask 53-41-00-914-054
Subtask 53-41-00-916-055
Subtask 53-41-00-410-091
C. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
ALL 53-41-00
Page 673
Feb 01/08
IAC
**ON A/C 001-012, 014-099,
TASK 53-41-00-210-016
Detailed Visual Inspection of Visible Part of Windows Forgings between FR47 and
FR65 LH/RH, External Surface
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
001-012, 014-099, 53-41-00
Page 674
Feb 01/08
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-941-058
A. Get Access
(1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position adjacent
to the window forging.
(2) Carefully clean the inspection area with the CLEANING AGENTS
(Material No. 11-026) and a clean lint-free cloth MISCELLANEOUS
(Material No. 19-003).
4. Procedure
_________
Subtask 53-41-00-210-072
A. Inspection
(1) Examine the window forgings at FR47 thru FR65 for cracks.
5. Close-up
________
Subtask 53-41-00-942-073
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
001-012, 014-099, 53-41-00
Page 675
Feb 01/08
R
IAC
Window Forgings FR47 thru FR65
Figure 613/TASK 53-41-00-991-017
R
EFF :
001-012, 014-099, 53-41-00
Page 676
Feb 01/08
IAC
Window Forgings FR47 thru FR64
Figure 613A/TASK 53-41-00-991-017-A
EFF :
101-199, 53-41-00
Page 677
Feb 01/08
R
IAC
Window Forgings FR47/51 thru FR65
Figure 613B/TASK 53-41-00-991-017-B
R
EFF :
901-999, 53-41-00
Page 678
Feb 01/08
IAC
Window Forgings - Permitted Damage
Figure 614/TASK 53-41-00-991-030
R
EFF :
001-012, 014-099, 53-41-00
Page 679
Feb 01/08
IAC
(3) Remove the warning notice(s).
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
001-012, 014-099, 53-41-00
Page 680
Feb 01/08
IAC
**ON A/C 101-199,
TASK 53-41-00-210-016-A
Detailed Visual Inspection of Visible Part of Windows Forgings between FR47 and
FR64 LH/RH, External Surface
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
101-199, 53-41-00
Page 681
Feb 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-941-087
A. Get Access
(1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position adjacent
to the window forging.
(2) Carefully clean the inspection area with the CLEANING AGENTS
(Material No. 11-026) and a clean lint-free cloth MISCELLANEOUS
(Material No. 19-003).
4. Procedure
_________
Subtask 53-41-00-210-144
A. Inspection
(1) Examine the window forgings at FR47 thru FR64 for cracks.
(2) Ifyou find cracks, refer to the ASRM (Ref. ASRM 53-00-29-101) for the
correct repair procedure.
5. Close-up
________
Subtask 53-41-00-942-107
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
101-199, 53-41-00
Page 682
Feb 01/08
IAC
Window Forgings - Permitted Damage
Figure 614A/TASK 53-41-00-991-030-A
R
EFF :
101-199, 53-41-00
Page 683
Feb 01/08
IAC
**ON A/C 901-999,
TASK 53-41-00-210-016-B
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
901-999, 53-41-00
Page 684
Feb 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-941-086
A. Get Access
(1) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position adjacent
to the window forging.
(2) Carefully clean the inspection area with the CLEANING AGENTS
(Material No. 11-026) and a clean lint-free cloth MISCELLANEOUS
(Material No. 19-003).
4. Procedure
_________
Subtask 53-41-00-210-143
A. Inspection
(1) Examine the window forgings at FR47/51 thru FR65 for cracks.
(2) If you find cracks, refer to the ASRM (Ref. ASRM 53-00-29-101) for
the correct repair procedure.
5. Close-up
________
Subtask 53-41-00-942-106
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
901-999, 53-41-00
Page 685
Feb 01/08
IAC
Window Forgings - Permitted Damage
Figure 614B/TASK 53-41-00-991-030-B
R
EFF :
901-999, 53-41-00
Page 686
Feb 01/08
IAC
**ON A/C ALL
TASK 53-41-00-210-018
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page 687
Feb 01/08
R
IAC
3. __________
Job Set-up
Subtask 53-41-00-010-091
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(1) Remove the vertical stabilizer fairings 323AL and 323AR (Ref. TASK
53-55-11-000-001).
(2) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-074
EFF :
ALL 53-41-00
Page 688
Feb 01/08
R
IAC
Circumferential Skin Splice FR70
Figure 615/TASK 53-41-00-991-018
EFF :
ALL 53-41-00
Page 689
Feb 01/08
R
IAC
- the external surface,
for cracks.
5. Close-up
________
Subtask 53-41-00-410-092
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the vertical stabilizer fairings 323AL and 323AR (Ref. TASK
53-55-11-400-001).
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page 690
Feb 01/08
R
IAC
TASK 53-41-00-210-019
Detailed Visual Inspection of Skin around VHF-3 Antenna Cutout between Stringer
1 LH/RH, External Surface
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page 691
Feb 01/08
R
IAC
3. __________
Job Set-up
Subtask 53-41-00-010-092
A. Get Access
(2) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-075
(a) Look for corrosion and other damage to the metal parts and to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion-protection data.
EFF :
ALL 53-41-00
Page 692
Feb 01/08
R
IAC
Skin Cutout of the VHF 3 Antenna
Figure 616/TASK 53-41-00-991-019
EFF :
ALL 53-41-00
Page 693
Feb 01/08
R
IAC
(b) Repair the corroded areas (Ref. AMM 517411300001).
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
(b) Refer to the ASRM (Ref. ASRM 51-11-11-001) for the allowable
damage limits.
(c) Repair the minor damage (Ref. AMM 517311300001) or (Ref. AMM
517311300004).
(d) If you find other damage to the metal parts, that is more than
the limits for minor damage, you must:
1
_ Refer to the ASRM for the material details, the item
identification and the action/repair data:
- for the skin plates, refer to the ASRM (Ref. ASRM 53-41-11-
001)
- for the frames, refer to the ASRM (Ref. ASRM 53-41-12-001)
- for the stringers, refer to the ASRM (Ref. ASRM 53-41-13-
001).
Subtask 53-41-00-210-075-A
(a) Make sure that you examine the frames, the stringers and the
internal surface of the fuselage skin.
(b) Look for corrosion and other damage to the metal parts and to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion-protection data.
EFF :
ALL 53-41-00
Page 694
Feb 01/08
R
IAC
(3) If you find other damage to the metal parts:
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
(b) Refer to the ASRM (Ref. ASRM 51-11-11-001) for the allowable
damage limits.
(c) Repair the minor damage (Ref. AMM 517311300001) or (Ref. AMM
517311300004).
(d) If you find other damage to the metal parts, that is more than
the limits for minor damage, you must:
1
_ Refer to the ASRM for the material details, the item
identification and the action/repair data:
- for the skin plates, refer to the ASRM (Ref. ASRM 53-41-11-
001)
- for the frames, refer to the ASRM (Ref. ASRM 53-41-12-001)
- for the stringers, refer to the ASRM (Ref. ASRM 53-41-13-
001).
5. Close-up
________
Subtask 53-41-00-410-093
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page 695
Feb 01/08
R
IAC
TASK 53-41-00-210-020
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page 696
Feb 01/08
R
IAC
3. __________
Job Set-up
Subtask 53-41-00-941-059
A. Get Access
(2) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-076
A. Inspection
(1) Examine the circumferential skin splice FR64 between STGR10 LH and
STGR10 RH for cracks.
EFF :
ALL 53-41-00
Page 697
Feb 01/08
R
IAC
Circumferential Skin Splice FR64
Figure 617/TASK 53-41-00-991-020
EFF :
ALL 53-41-00
Page 698
Feb 01/08
R
IAC
5. Close-up
________
Subtask 53-41-00-942-076
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page 699
Feb 01/08
R
IAC
TASK 53-41-00-210-021
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-093
A. Get Access
(1) Remove the corner scuff plates at the AFT passenger/crew doors
(Ref. TASK 53-45-15-000-001).
4. Procedure
_________
Subtask 53-41-00-210-078
A. Inspection:
(1) Examine the fuselage skin below the scuff plate for:
- corrosion,
- cracks,
- loose or missing rivets,
- skin distortion.
EFF :
ALL 53-41-00
Page A600
Feb 01/08
R
IAC
Bottom Corners of the Aft Passenger/Crew Door-Cutouts
Figure 618/TASK 53-41-00-991-021
EFF :
ALL 53-41-00
Page A601
Feb 01/08
R
IAC
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for
____
the correct repair procedure.
5. Close-up
________
Subtask 53-41-00-410-094
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the corner scuff plates at the AFT passenger/crew doors
(Ref. TASK 53-45-15-400-001).
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
ALL 53-41-00
Page A602
Feb 01/08
IAC
TASK 53-41-00-210-025
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-096
A. Get Access
R
EFF :
ALL 53-41-00
Page A603
Feb 01/08
IAC
4. Procedure
_________
Subtask 53-41-00-210-080
(2) If you find a defective eccentric bolt, you must replace it.
Subtask 53-41-00-210-080-A
(2) If you find a defective eccentric bolt, you must replace it.
5. Close-up
________
Subtask 53-41-00-410-097
A. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
ALL 53-41-00
Page A604
Feb 01/08
IAC
Eccentric Bolts on the Locking Mechanism Fittings at the AFT Cargo-Compartment
Door
Figure 619/TASK 53-41-00-991-023
R EFF :
ALL
53-41-00 Page A605
Feb 01/08
IAC
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
ALL 53-41-00
Page A606
Feb 01/08
IAC
**ON A/C 101-199,
TASK 53-41-00-210-026
Detailed Visual Inspection of Bulk Cargo Door Stop Fittings and Back-up
Structure at FR60 and FR62 (10 places)
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
101-199, 53-41-00
Page A607
Feb 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-099
A. Get Access
(1) Remove the sidewall panels 162BW, 162EW (Ref. TASK 25-55-11-000-001).
(2) Remove the floor panels 162GF, 162HF, 162KF, 162LF (Ref. TASK 53-42-
17-000-001).
(3) Remove the insulation blankets from around the BULK cargo-compartment
door (Ref. TASK 25-80-00-000-001).
(4) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth.
R
EFF :
101-199, 53-41-00
Page A608
Feb 01/08
IAC
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______
MATERIALS ONLY WITH A GOOD SUPPLY OF AIR.
OBEY THE MANUFACTURERS INSTRUCTIONS.
PUT ON PROTECTIVE CLOTHING.
DO NOT GET THEM IN YOUR MOUTH.
DO NOT SMOKE.
DO NOT BREATHE THE GAS.
THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT.
GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
4. Procedure
_________
Subtask 53-41-00-210-084
A. Inspection
(1) Examine the stop fittings at the BULK cargo-compartment door for:
- cracks,
- deformation.
(2) Examine the internal and the external structure adjacent to the stop
fittings at the BULK cargo-compartment door for:
- cracks,
- corrosion,
- deformation.
5. Close-up
________
Subtask 53-41-00-916-066
Subtask 53-41-00-410-100
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
101-199, 53-41-00
Page A609
Feb 01/08
IAC
Stop Fittings at the BULK Cargo-Compartment Door and the Adjacent Structure
Figure 620/TASK 53-41-00-991-024
EFF :
101-199, 53-41-00
Page A610
Feb 01/08
R
IAC
(3) Install the floor panels 162GF, 162HF, 162KF and 162LF (Ref. TASK 53-
42-17-400-001).
(4) Install the sidewall panels 162BW and 162EW (Ref. TASK 25-55-11-400-
001).
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
101-199, 53-41-00
Page A611
Feb 01/08
R
IAC
**ON A/C ALL
TASK 53-41-00-210-027
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-41-00
Page A612
Feb 01/08
IAC
3. __________
Job Set-up
Subtask 53-41-00-941-051
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(2) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-052
A. Inspection
5. Close-up
________
Subtask 53-41-00-942-051
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
ALL 53-41-00
Page A613
Feb 01/08
IAC
Lap Joint FR47 thru FR70
Figure 621/TASK 53-41-00-991-002
EFF :
ALL 53-41-00
Page A614
Feb 01/08
R
IAC
**ON A/C 101-199,
TASK 53-41-00-210-028
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
101-199, 53-41-00
Page A615
Feb 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-079
A. Get Access
(1) Remove the sidewall panels 162BW, 162EW (Ref. TASK 25-55-11-000-001).
(2) Remove the floor panel 162HF, 162LF, 162GF, 162KF (Ref. TASK 53-42-
17-000-001).
(3) Remove the insulation blankets from the inspection area (Ref. TASK
25-80-00-000-001).
R
EFF :
101-199, 53-41-00
Page A616
Feb 01/08
IAC
(5) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-085
A. Inspection
(1) Examine the internal fuselage skin around the BULK cargo-compartment
door-cutout from FR59 thru FR63 and from STGR24 thru STGR32 for:
- cracks,
- corrosion.
5. Close-up
________
Subtask 53-41-00-916-059
Subtask 53-41-00-410-078
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the floor panels 162HF, 162LF, 162GF and 162KF (Ref. TASK 53-
42-17-400-001).
(4) Install the sidewall panels 162BW and 162EW (Ref. TASK 25-55-11-400-
001).
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
101-199, 53-41-00
Page A617
Feb 01/08
IAC
Internal Fuselage Skin around the Bulk Cargo-Compartment Door-Cutout
Figure 622/TASK 53-41-00-991-011
R
EFF :
101-199, 53-41-00
Page A618
Feb 01/08
IAC
**ON A/C ALL
TASK 53-41-00-210-029
Detailed Visual Inspection of Door Stop Fittings on FR66 and FR68, LH/RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page A619
Feb 01/08
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-104
A. Get Access
(2) Remove the thermal and acoustical insulation blankets (Ref. TASK 25-
80-00-000-001).
(3) Cleaning.
(a) Clean the door stop fittings with CLEANING AGENTS (Material No.
11-004) and a lint-free cloth.
EFF :
ALL 53-41-00
Page A620
Feb 01/08
R
IAC
4. Procedure
_________
Subtask 53-41-00-210-087
A. Inspection
5. Close-up
________
Subtask 53-41-00-410-103
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the thermal and acoustical insulation blankets (Ref. TASK 25-
80-00-400-001).
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page A621
Feb 01/08
R
IAC
Door Stop Fittings
Figure 623/TASK 53-41-00-991-026
EFF :
ALL 53-41-00
Page A622
Feb 01/08
R
IAC
TASK 53-41-00-210-030
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page A623
Feb 01/08
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-106
A. Get Access
(2) Put the access platform below the AFT cargo-compartment door.
(3) Remove the partition access panels 161DW, 162DW at FR65 (Ref. TASK
25-55-12-000-001).
(4) Remove the thermal and acoustical insulation blankets (Ref. TASK 25-
80-00-000-001) and identify the blankets for installation.
EFF :
ALL 53-41-00
Page A624
Feb 01/08
R
IAC
Subtask 53-41-00-110-115
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Use a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) and
the CLEANING AGENTS (Material No. 11-003) to clean the inspection
area.
4. Procedure
_________
Subtask 53-41-00-210-089
A. Inspection
(1) Examine the fuselage internal structure below the cabin floor panels
together with the floor structure from FR65 thru FR70 for:
- corrosion,
- cracks.
EFF :
ALL 53-41-00
Page A625
Feb 01/08
R
IAC
Fuselage Internal Structure and the Floor Structure between FR65 thru FR70
Figure 624/TASK 53-41-00-991-027
EFF :
ALL 53-41-00
Page A626
Feb 01/08
R
IAC
5. Close-up
________
Subtask 53-41-00-916-057
Subtask 53-41-00-410-107
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the thermal and acoustical insulation blankets (Ref. TASK 25-
80-00-400-001).
(3) Install the partition access panels 161DW, 162DW at FR65 (Ref. TASK
25-55-12-400-001).
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page A627
Feb 01/08
R
IAC
TASK 53-41-00-210-031
Detailed Visual Inspection of AFT Cargo Door Cutout Upper and Lower Corners,
External Surface
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page A628
Feb 01/08
R
IAC
3. __________
Job Set-up
Subtask 53-41-00-010-105
A. Get Access
(1) Put the access platform below the AFT cargo-compartment door.
(3) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-088
A. Inspection
EFF :
ALL 53-41-00
Page A629
Feb 01/08
R
IAC
AFT Cargo Compartment Door Cutout
Figure 625/TASK 53-41-00-991-028
EFF :
ALL 53-41-00
Page A630
Feb 01/08
R
IAC
5. Close-up
________
Subtask 53-41-00-410-104
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page A631
Feb 01/08
R
IAC
TASK 53-41-00-210-036
Detailed Visual Inspection of Upper Segment of FR70, Fin to Fuselage FWD Attach
Fittings and Area between FR69 and FR70 from STGR6 LH/RH to Crown Center Line
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page A632
Feb 01/08
R
IAC
3. __________
Job Set-up
Subtask 53-41-00-010-109
A. Get Access
(3) Remove the insulation blankets from the rear pressure bulkhead
(Ref. TASK 25-80-00-000-001).
(4) Cleaning.
4. Procedure
_________
Subtask 53-41-00-210-090
A. Inspection
(1) Examine the upper section of FR70, the fin to fuselage FWD
attach-fittings and the area between FR69 to FR70 and from STGR6
LH/RH to the crown centerline for:
- cracks,
- corrosion.
EFF :
ALL 53-41-00
Page A633
Feb 01/08
R
IAC
The Upper Section of FR70 and the Vertical-Stabilizer Forward Attach-Fittings
Figure 626/TASK 53-41-00-991-029
EFF :
ALL 53-41-00
Page A634
Feb 01/08
R
IAC
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-17-001) and
____
(Ref. ASRM 53-51-16-001) for the correct repair procedures.
5. Close-up
________
Subtask 53-41-00-410-108
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
ALL 53-41-00
Page A635
Feb 01/08
IAC
TASK 53-41-00-210-037
Detailed Visual Inspection of Cabin Floor Structure, below and 0.5m around
Galleys and Toilets, from FR47/54 (318), FR47/51 (319), FR47 (320/321) to FR70
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-41-00
Page A636
Feb 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page A637
Feb 01/08
R
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-41-00-010-112
A. Get Access:
(5) Remove the floor panels (Ref. TASK 53-32-12-000-002), (Ref. TASK 53-
42-12-000-001) and (Ref. TASK 53-42-12-000-002).
(6) Cleaning
(a) Clean the inspection area with CLEANING AGENTS (Material No. 11-
003) and a lint free cloth.
EFF :
ALL 53-41-00
Page A638
Feb 01/08
R
IAC
4. Procedure
_________
Subtask 53-41-00-210-091
A. Inspection:
(1) Examine the cabin floor structure, below and 0.5m around the galley
and toilet areas for corrosion. If necessary, refer to the ASRM (Ref.
ASRM 53-43-00-001) for the correct repair procedure.
NOTE : The door entrance area between FR66 and FR68 is not examined
____
in this procedure.
5. Close-up
________
Subtask 53-41-00-916-075
EFF :
ALL 53-41-00
Page A639
Feb 01/08
R
IAC
Cabin Floor Structure - FR47 thru FR70
Figure 627/TASK 53-41-00-991-031
R
EFF :
001-012, 014-099, 101-199, 53-41-00
Page A640
Feb 01/08
IAC
Cabin Floor Structure - FR47/51 thru FR70
Figure 627A/TASK 53-41-00-991-031-A
R
EFF :
901-999, 53-41-00
Page A641
Feb 01/08
IAC
Subtask 53-41-00-410-110
B. Close Access:
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the floor panels (Ref. TASK 53-32-12-400-002), (Ref. TASK 53-
42-12-400-001) and (Ref. TASK 53-42-12-400-002).
EFF :
ALL 53-41-00
Page A642
Feb 01/08
R
IAC
TASK 53-41-00-210-038
General Visual Inspection of AFT Cargo Door Lock Fittings and Surrounding
Structure, External Portion (6 places)
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page A643
Feb 01/08
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-113
A. Get Access:
(3) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint free cloth.
4. Procedure
_________
Subtask 53-41-00-210-092
A. Examine the AFT cargo door lock fittings and the adjacent structure
between FR53 and FR55A, external part (6 places) for:
- corrosion,
- cracks
- and other damage.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-46-11-101) for the
____
correct repair procedure.
EFF :
ALL 53-41-00
Page A644
Feb 01/08
R
IAC
AFT Cargo Door Lock Fittings
Figure 628/TASK 53-41-00-991-032
EFF :
ALL 53-41-00
Page A645
Feb 01/08
R
IAC
**ON A/C 901-999,
Subtask 53-41-00-210-092-A
A. Examine the AFT cargo door lock fittings and the adjacent structure
between FR56 and FR58A, external part (6 places) for:
- corrosion,
- cracks
- and other damage.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-46-11-101) for the
____
correct repair procedure.
Subtask 53-41-00-916-082
R NOTE : The step that follows is only necessary for the Corrosion
____
R Prevention and Control Program (CPCP).
R (1) Apply the STORAGE PRESERVATION (Material No. 15-005) or the STORAGE
R PRESERVATION (Material No. 15-005A) or the STORAGE PRESERVATION
R (Material No. 15-006) to the inspection area as necessary.
5. Close-up
________
Subtask 53-41-00-410-111
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
ALL 53-41-00
Page A646
Feb 01/08
IAC
TASK 53-41-00-210-041
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-41-00
Page A647
Feb 01/08
IAC
3. __________
Job Set-up
Subtask 53-41-00-010-123
A. Get Access
(2) Open the aft passenger/crew doors (Ref. TASK 52-10-00-010-001), from
the outside.
(3) Remove the scuff-plates (Ref. TASK 53-45-15-000-001), from the aft
passenger/crew doors.
Subtask 53-41-00-110-085
B. Cleaning Procedure
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint free cloth, if necessary. Make sure that the area is dry
before you continue.
R
EFF :
ALL 53-41-00
Page A648
Feb 01/08
IAC
4. Procedure
_________
Subtask 53-41-00-210-094
5. Close-up
________
Subtask 53-41-00-410-120
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Close the aft passenger/crew doors (Ref. TASK 52-10-00-410-001), from
the outside.
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
ALL 53-41-00
Page A649
Feb 01/08
IAC
AFT Passenger/Crew Door Cutout, Underneath the Scuff-Plate, LH/RH
Figure 629/TASK 53-41-00-991-038
R
EFF :
ALL 53-41-00
Page A650
Feb 01/08
IAC
**ON A/C 101-199,
TASK 53-41-00-210-042
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
101-199, 53-41-00
Page A651
Feb 01/08
R
IAC
3. __________
Job Set-up
Subtask 53-41-00-010-125
A. Get Access
(1) Put the warning notice in position to tell persons not to operate the
flight controls.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(2) Put the access platform in position adjacent to FR47.5 LH and RH.
(3) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-095
A. Inspection
5. Close-up
________
Subtask 53-41-00-410-123
A. Close Access
EFF :
101-199, 53-41-00
Page A652
Feb 01/08
R
IAC
Frame Splice at FR47.5 Stringer 16 LH and RH to Crown Center Line
Figure 630/TASK 53-41-00-991-039
EFF :
101-199, 53-41-00
Page A653
Feb 01/08
R
IAC
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
101-199, 53-41-00
Page A654
Feb 01/08
R
IAC
TASK 53-41-00-210-044
Detailed Visual Inspection of the Aft Emergency Skin Cutouts Upper and Lower
Corners, External Surface LH/RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
101-199, 53-41-00
Page A655
Feb 01/08
R
IAC
3. __________
Job Set-up
Subtask 53-41-00-010-128
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(1) Put the adjustable platform in position below the emergency exit.
(2) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-097
A. Inspection
(1) Examine the skin cutouts at the upper and lower corners of the aft
emergency exit for:
- cracks,
- corrosion,
- skin distortion,
- surface damage.
EFF :
101-199, 53-41-00
Page A656
Feb 01/08
R
IAC
5. Close-up
________
Subtask 53-41-00-410-126
A. Close Access
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
101-199, 53-41-00
Page A657
Feb 01/08
R
IAC
TASK 53-41-00-210-045
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
101-199, 53-41-00
Page A658
Feb 01/08
R
IAC
3. __________
Job Set-up
Subtask 53-41-00-010-129
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(2) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-098
A. Inspection
(1) Examine the skin cutouts at the upper and lower corners of the
emergency-exit escape chute compartment cutouts for:
- cracks,
- corrosion.
EFF :
101-199, 53-41-00
Page A659
Feb 01/08
R
IAC
5. Close-up
________
Subtask 53-41-00-410-127
A. Close Access
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
101-199, 53-41-00
Page A660
Feb 01/08
R
IAC
TASK 53-41-00-210-046
Detailed Visual Inspection of the Skin at the Window Cutout between FR47 and
FR47.2 from Stringer 14 to Stringer 18, External Surface LH/RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
101-199, 53-41-00
Page A661
Feb 01/08
R
IAC
3. __________
Job Set-up
Subtask 53-41-00-010-130
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(2) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-099
A. Inspection
EFF :
101-199, 53-41-00
Page A662
Feb 01/08
R
IAC
5. Close-up
________
Subtask 53-41-00-410-128
A. Close Access
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
101-199, 53-41-00
Page A663
Feb 01/08
R
IAC
TASK 53-41-00-210-048
Detailed Visual Inspection of the Door Stop Fittings on FR47.2A and FR47.4, LH
and RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
101-199, 53-41-00
Page A664
Feb 01/08
R
IAC
3. __________
Job Set-up
Subtask 53-41-00-010-133
A. Get Access
(1) Open the applicable emergency exit doors (Ref. TASK 52-22-00-010-
001).
(a) Clean the door stop fittings with CLEANING AGENTS (Material No.
11-003) and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-101
A. Inspection
(Ref. Fig. 631/TASK 53-41-00-991-041)
EFF :
101-199, 53-41-00
Page A665
Feb 01/08
R
IAC
Door Stop Fittings
Figure 631/TASK 53-41-00-991-041
EFF :
101-199, 53-41-00
Page A666
Feb 01/08
R
IAC
5. Close-up
________
Subtask 53-41-00-410-131
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
101-199, 53-41-00
Page A667
Feb 01/08
R
IAC
TASK 53-41-00-210-047
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
101-199, 53-41-00
Page A668
Feb 01/08
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-131
A. Get Access
(2) Remove the door frame linings in the inspection area (Ref. TASK 25-
23-47-000-010).
(3) Remove the insulation blankets in the inspection area (Ref. TASK 25-
80-00-000-001).
(4) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth.
R
EFF :
101-199, 53-41-00
Page A669
Feb 01/08
IAC
4. Procedure
_________
Subtask 53-41-00-210-100
A. Inspection
5. Close-up
________
Subtask 53-41-00-916-074
A. Protective Treatment
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
Subtask 53-41-00-410-129
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
101-199, 53-41-00
Page A670
Feb 01/08
IAC
TASK 53-41-00-210-049
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
101-199, 53-41-00
Page A671
Feb 01/08
IAC
3. __________
Job Set-up
Subtask 53-41-00-010-134
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(3) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-102
A. Inspection
R
EFF :
101-199, 53-41-00
Page A672
Feb 01/08
IAC
NOTE : If necessary,refer to the ASRM (Ref. ASRM 53-41-11-101) for
____
the correct repair procedure.
5. Close-up
________
Subtask 53-41-00-916-077
Subtask 53-41-00-410-132
B. Close Access
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
101-199, 53-41-00
Page A673
Feb 01/08
IAC
**ON A/C ALL
TASK 53-41-00-210-801
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page A674
Feb 01/08
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-135
A. Get Access
(1) Remove the necessary floor panels (Ref. TASK 53-42-12-000-001) and
(Ref. TASK 53-42-12-000-002).
Subtask 53-41-00-110-086
B. Cleaning Procedure
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
EFF :
ALL 53-41-00
Page A675
Feb 01/08
R
IAC
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint free cloth.
4. Procedure
_________
Subtask 53-41-00-210-103
A. Inspection
(1) Inspect the cabin floor structure, without the areas below the
galleys, the toilets and the door entrance areas, from FR47 to FR70
for:
- corrosion,
- cracks
Subtask 53-41-00-916-078
5. Close-up
________
Subtask 53-41-00-410-133
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the floor panels (Ref. TASK 53-42-12-400-001) and (Ref. TASK
53-42-12-400-002).
EFF :
ALL 53-41-00
Page A676
Feb 01/08
R
IAC
Cabin Floor Structure - FR47 to FR70
Figure 632/TASK 53-41-00-991-043
EFF :
ALL 53-41-00
Page A677
Feb 01/08
R
IAC
TASK 53-41-00-210-802
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page A678
Feb 01/08
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-136
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(2) Put a warning notice on the slat/flap control lever to tell persons
not to operate the slats/flaps.
EFF :
ALL 53-41-00
Page A679
Feb 01/08
R
IAC
Subtask 53-41-00-110-087
B. Cleaning Procedure
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint free cloth.
4. Procedure
_________
Subtask 53-41-00-210-104
A. Inspection
(1) Examine the the fuselage external surface and the belly fairing
support structure between FR30 thru FR53, under the belly fairing
for:
- corrosion,
- cracks
- and other damage.
EFF :
ALL 53-41-00
Page A680
Feb 01/08
R
IAC
Fuselage External Surface inside the Belly Fairing and Belly Fairing Support
Structure
Figure 633/TASK 53-41-00-991-044
EFF :
ALL
53-41-00 Page A681
Feb 01/08
R
IAC
**ON A/C 101-199,
Subtask 53-41-00-210-104-B
A. Inspection
(1) Examine the the fuselage external surface and the belly fairing
support structure between FR35.3 thru FR48, under the belly fairing
for:
- corrosion,
- cracks
- and other damage.
Subtask 53-41-00-210-104-A
A. Examine the the fuselage external surface and the belly fairing support
structure between FR27 and FR57, under the belly fairing for:
- corrosion,
- cracks
- and other damage.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-45-12-201) for the
____
correct repair procedure.
Subtask 53-41-00-916-079
EFF :
ALL 53-41-00
Page A682
Feb 01/08
R
IAC
5. Close-up
________
Subtask 53-41-00-410-134
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page A683
Feb 01/08
R
IAC
TASK 53-41-00-210-803
General Visual Inspection of AFT Cargo Door Cutout, Visible Part of Lateral
Frames
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-41-00
Page A684
Feb 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-137
A. Get Access
(2) Put the access platform adjacent to the AFT cargo-compartment door.
Subtask 53-41-00-110-088
B. Cleaning Procedure
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint free cloth.
R
EFF :
ALL 53-41-00
Page A685
Feb 01/08
IAC
4. Procedure
_________
Subtask 53-41-00-210-105
A. Inspection
(1) Examine the lateral FR52A and FR56 that you can see at the AFT cargo
door cutout for:
- corrosion,
- cracks
- and any other damage.
Subtask 53-41-00-210-105-A
A. Inspection
(1) Examine the lateral FR55A and FR59 that you can see at the AFT cargo
door cutout for:
- corrosion,
- cracks
- and any other damage.
R
EFF :
ALL 53-41-00
Page A686
Feb 01/08
IAC
AFT Cargo Door Cutout - Lateral
Figure 634/TASK 53-41-00-991-045
R
EFF :
ALL 53-41-00
Page A687
Feb 01/08
IAC
**ON A/C ALL
Subtask 53-41-00-916-080
R NOTE : The step that follows is only necessary for the Corrosion
____
R Prevention and Control Program (CPCP).
R (1) Apply the STORAGE PRESERVATION (Material No. 15-005) or the STORAGE
R PRESERVATION (Material No. 15-005A) or the STORAGE PRESERVATION
R (Material No. 15-006) or an equivalent to the inspection area as
R necessary.
5. Close-up
________
Subtask 53-41-00-410-135
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
ALL 53-41-00
Page A688
Feb 01/08
IAC
**ON A/C 101-199,
TASK 53-41-00-210-804
General Visual Inspection of Sealing Profile of Bulk Cargo Door Cutout at Upper
Corners
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
101-199, 53-41-00
Page A689
Feb 01/08
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-138
A. Get Access
(1) Put the access platform adjacent to the BULK cargo compartment door.
(2) Open the BULK cargo compartment door (Ref. TASK 52-30-00-860-006).
Subtask 53-41-00-110-089
B. Cleaning Procedure
(1) Clean the inspection area with the CLEANING AGENTS (Material No. 11-
026) and a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
4. Procedure
_________
Subtask 53-41-00-210-106
A. Inspection
(1) Inspect the seealing profile of the bulk cargo door cutout at the
upper corners for:
- corrosion,
- cracks
- and any other damage.
EFF :
101-199, 53-41-00
Page A690
Feb 01/08
R
IAC
Sealing Profile of the Bulk Cargo Door Cutout at the Upper Corners
Figure 635/TASK 53-41-00-991-046
R
EFF :
101-199, 53-41-00
Page A691
Feb 01/08
IAC
Subtask 53-41-00-916-081
NOTE : The steps that follow are only necessary for the Corrosion
____
Prevention and Control Program (CPCP).
(1) Apply the STORAGE PRESERVATION (Material No. 15-005) or the STORAGE
PRESERVATION (Material No. 15-005A) or the STORAGE PRESERVATION
(Material No. 15-006) or equivalent to the inspection area as
necessary.
5. Close-up
________
Subtask 53-41-00-410-136
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Close the BULK cargo compartment door (Ref. TASK 52-30-00-860-008).
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
101-199, 53-41-00
Page A692
Feb 01/08
IAC
TASK 53-41-00-210-805
General Visual Inspection of Bulk Cargo Door Stop Fittings and Back-Up
Structure, at FR60 and FR62 (10 Places)
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
A. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
101-199, 53-41-00
Page A693
Feb 01/08
IAC
3. __________
Job Set-up
Subtask 53-41-00-010-139
A. Get Access
(2) Remove the sidewall panels 162BW and 162EW (Ref. TASK 25-55-11-000-
001).
(3) Remove the floor panels 162GF, 162HF, 162KF and 162LF (Ref. TASK 53-
42-17-000-001).
(4) Remove the insulation blankets from around the bulk-cargo compartment
door (Ref. TASK 25-80-00-000-001).
(5) Clean the inspection area with the CLEANING AGENTS (Material No. 11-
026) and a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
4. Procedure
_________
Subtask 53-41-00-210-107
A. Inspection
(1) Examine the stop fittings of the bulk cargo-compartment door for:
- Cracks
- Deformation.
(2) Examine the internal and external structure adjacent to the stop
fittings at the bulk cargo-compartment door. Examine the structure
that you can see for:
- Cracks
- Corrosion
- Deformation.
R
EFF :
101-199, 53-41-00
Page A694
Feb 01/08
IAC
Subtask 53-41-00-916-083
B. Temporary Protection
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1) Apply the STORAGE PRESERVATION (Material No. 15-005) or the STORAGE
PRESERVATION (Material No. 15-006) to the inspection area.
5. Close-up
________
Subtask 53-41-00-410-137
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the floor panels 162GF, 162HF, 162KF and 162LF (Ref. TASK 53-
42-17-400-001).
(4) Install the sidewall panels 162BW and 162EW (Ref. TASK 25-55-11-400-
001).
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
101-199, 53-41-00
Page A695
Feb 01/08
IAC
**ON A/C ALL
TASK 53-41-00-210-806
Detailed Visual Inspection of the Fuselage Skin External Surface between FR64
and FR70 from Stringer 6 to Crown Center Line LH and RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page A696
Feb 01/08
R
IAC
3. __________
Job Set-up
Subtask 53-41-00-010-140
A. Get Access
(2) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-41-00-210-108
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
EFF :
ALL 53-41-00
Page A697
Feb 01/08
R
IAC
Fuselage External Surface - FR64 to FR70 from Stringer 6 to Crown Center Line
Figure 636/TASK 53-41-00-991-049
EFF :
ALL 53-41-00
Page A698
Feb 01/08
R
IAC
(c) If you find other types of damage:
- Refer to the ASRM (Ref. ASRM 51-73-00-001) for the repair of
the minor damage.
5. Close-up
________
Subtask 53-41-00-410-138
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page A699
Feb 01/08
R
IAC
TASK 53-41-00-210-807
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
R
R Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page B600
May 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-941-069
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
(2) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in the applicable
position.
Subtask 53-41-00-110-090
B. Cleaning Procedure
(1) Clean the area with the CLEANING AGENTS (Material No. 11-026) and a
lint-free cotton cloth MISCELLANEOUS (Material No. 19-003). Let the
area dry.
4. Procedure
_________
Subtask 53-41-00-210-109
A. Inspection
(1) Examine the area that follows for scratches, dents and cracks:
- The upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 6, LH/RH between FR 47 and FR 70.
(2) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for the
permitted damage limits.
EFF :
ALL 53-41-00
Page B601
Feb 01/08
R
IAC
Upper Skin of longitudinal Lap Joints including Crack Stopper Areas at Stringer
6, External Surface
Figure 637/TASK 53-41-00-991-050
EFF :
ALL
53-41-00 Page B602
Feb 01/08
R
IAC
(3) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for the
correct repair procedure.
Subtask 53-41-00-210-109-A
A. Inspection
(1) Examine the following area for scratches, dents and cracks:
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 6, LH/RH between FR 47/51 and FR 70.
5. Close-up
________
Subtask 53-41-00-942-091
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-41-00
Page B603
Feb 01/08
R
IAC
TASK 53-41-00-210-808
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
1. __________________
Reason for the Job
R
R Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page B604
May 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-157
A. Get Access
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
EFF :
ALL 53-41-00
Page B605
Feb 01/08
R
IAC
**ON A/C 101-199,
Subtask 53-41-00-010-157-B
A. Get Access
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
Subtask 53-41-00-010-157-A
A. Get Access
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
Subtask 53-41-00-110-091
B. Cleaning Procedure
EFF :
ALL 53-41-00
Page B606
Feb 01/08
R
IAC
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material
No. 19-003) and the CLEANING AGENTS (Material No. 11-004), and let
the area dry.
4. Procedure
_________
Subtask 53-41-00-210-110
A. Inspection
(1) Examine the following areas for scratches, dents and cracks:
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 32 LH between FR 47 and FR 53, external
surface.
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 41 RH between FR 47 and FR 51, external
surface.
EFF :
ALL 53-41-00
Page B607
Feb 01/08
R
IAC
Upper Skin of Longitudinal Lap Joints including Crack Stopper Areas at Stringer
32LH, External Surface
Figure 638/TASK 53-41-00-991-051
R EFF :
ALL
53-41-00 Page B608
Feb 01/08
IAC
Upper Skin of Longitudinal Lap Joints including Crack Stopper Areas at Stringer
32RH, External Surface
Figure 639/TASK 53-41-00-991-070
R EFF :
101-199,
53-41-00 Page B609
Feb 01/08
IAC
Upper Skin of Longitudinal Lap Joints including Crack Stopper Areas at Stringer
41RH, External Surface
Figure 640/TASK 53-41-00-991-081
EFF :
ALL
53-41-00 Page B610
Feb 01/08
R
IAC
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for
____
the allowable damage limits.
Subtask 53-41-00-210-110-B
A. Inspection
(1) Examine the following areas for scratches, dents and cracks:
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 32 LH between FR 47 and FR 48, external
surface.
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 32 RH between FR 47 and FR 47.5, external
surface.
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 41 RH between FR 47 and FR 47.4, external
surface.
Subtask 53-41-00-210-110-A
A. Inspection
(1) Examine the following areas for scratches, dents and cracks:
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 32 LH between FR 47/51 and FR 57,
external surface.
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 41 RH between FR 47/51 and FR 55,
external surface.
EFF :
ALL 53-41-00
Page B611
Feb 01/08
R
IAC
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for
____
the correct repair procedure.
5. Close-up
________
Subtask 53-41-00-410-155
A. Close Access
Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 53-41-00-410-155-B
A. Close Access
Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-41-00
Page B612
Feb 01/08
R
IAC
**ON A/C 901-999,
Subtask 53-41-00-410-155-A
A. Close Access
Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
901-999, 53-41-00
Page B613
Feb 01/08
IAC
**ON A/C ALL
TASK 53-41-00-210-809
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
R
R Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page B614
May 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
ASRM 53-41-11-101
ASRM 53-41-11-201
AMM 53-73-11-300-001 (for corrective action)
ASRM 53-41-11-101 (for corrective action)
ASRM 53-41-11-201 (for corrective action)
53-41-00-991-053 Fig. 641
53-41-00-991-071 Fig. 642
53-41-00-991-072 Fig. 643
3. __________
Job Set-up
Subtask 53-41-00-941-070
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
(2) Put the ACCESS PLATFORM 1M(3 FT) in the applicable position.
Subtask 53-41-00-110-092
B. Cleaning Procedure
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material
No. 19-003) and the CLEANING AGENTS (Material No. 11-026), and let
the area dry.
EFF :
ALL 53-41-00
Page B615
Feb 01/08
R
IAC
4. Procedure
_________
Subtask 53-41-00-210-111
A. Inspection
(1) Examine the areas that follow for scratches, dents and cracks:
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 32 LH between FR 53 and FR 70, external
surface
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 32 RH between FR 58 and FR 70, external
surface
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 41 RH between FR 51 and FR 70, external
surface.
(2) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for the
permitted damage limits.
(3) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for the
correct repair procedure.
Subtask 53-41-00-210-111-B
A. Inspection
(1) Examine the areas that follow for scratches, dents and cracks:
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 32 LH between FR 48 and FR 70, external
surface
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 32 RH between FR 47.5 and FR 70, external
surface
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 41 RH between FR 47.4 and FR 70, external
surface.
EFF :
ALL 53-41-00
Page B616
Feb 01/08
R
IAC
Upper Skin of Longitudinal Lap Joints including Crack Stopper Areas, Stringer
32 LH, External Surface
Figure 641/TASK 53-41-00-991-053
EFF :
ALL
53-41-00 Page B617
Feb 01/08
R
IAC
Upper Skin of Longitudinal Lap Joints including Crack Stopper Areas, Stringer
32 RH, External Surface
Figure 642/TASK 53-41-00-991-071
EFF :
ALL
53-41-00 Page B618
Feb 01/08
R
IAC
Upper Skin of Longitudinal Lap Joints including Crack Stopper Areas, Stringer
41 LH, External Surface
Figure 643/TASK 53-41-00-991-072
EFF :
ALL
53-41-00 Page B619
Feb 01/08
R
IAC
(2) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for the
permitted damage limits.
(3) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for the
correct repair procedure.
Subtask 53-41-00-210-111-A
A. Inspection
(1) Examine the areas that follow for scratches, dents and cracks:
- The upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 32 LH. Do this between FR57 and FR70,
external surface
- The upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 32 RH. Do this between FR64 and FR70,
external surface
- The upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 41 RH. Do this between FR55 and FR70,
external surface.
(2) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for the
permitted damage limits.
(3) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for the
repair data.
(4) Refer to the AMM (Ref. AMM 53-73-11-300-001) for the correct repair
procedure.
5. Close-up
________
Subtask 53-41-00-942-092
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
ALL 53-41-00
Page B620
Feb 01/08
IAC
(3) Remove the access platform(s).
R
EFF :
ALL 53-41-00
Page B621
Feb 01/08
IAC
TASK 53-41-00-210-810
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-41-00
Page B622
Feb 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-941-068
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
(2) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in the required
position.
Subtask 53-41-00-110-093
B. Cleaning Procedure
EFF :
ALL 53-41-00
Page B623
Feb 01/08
R
IAC
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material
No. 19-003) and the CLEANING AGENTS (Material No. 11-004), and let
the area dry.
4. Procedure
_________
Subtask 53-41-00-210-112
A. Inspection
(1) Examine the following area for scratches, dents and cracks:
- the fuselage external surface between FR47 and FR70, from stringer
23 LH/RH to bottom centerline, exept the area that is covered by
the belly fairing.
EFF :
ALL 53-41-00
Page B624
Feb 01/08
R
IAC
Fuselage external Surface from STGR 23 RH/LH toBottom Centerline
Figure 644/TASK 53-41-00-991-056
R
EFF :
001-012, 014-099, 53-41-00
Page B625
Feb 01/08
IAC
Fuselage external Surface from STGR 23 RH/LH toBottom Centerline
Figure 644A/TASK 53-41-00-991-056-B
R
EFF :
101-199, 53-41-00
Page B626
Feb 01/08
IAC
Fuselage external Surface from STGR 23 RH/LH toBottom Centerline
Figure 644B/TASK 53-41-00-991-056-A
R
EFF :
901-999, 53-41-00
Page B627
Feb 01/08
IAC
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for
____
the allowable damage limits.
Subtask 53-41-00-210-112-A
A. Inspection
(1) Examine the following area for scratches, dents and cracks:
- the fuselage external surface between FR47/51 and FR70, from
stringer 23 LH/RH to bottom centerline, exept the area that is
covered by the belly fairing.
5. Close-up
________
Subtask 53-41-00-942-090
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
ALL 53-41-00
Page B628
Feb 01/08
IAC
TASK 53-41-00-210-811
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
R
R Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page B629
May 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-941-071
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
(2) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in the applicable
position.
Subtask 53-41-00-110-094
B. Cleaning Procedure
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material
No. 19-003) and the CLEANING AGENTS (Material No. 11-026), and let
the area dry.
EFF :
ALL 53-41-00
Page B630
Feb 01/08
R
IAC
4. Procedure
_________
Subtask 53-41-00-210-113
A. Inspection
(1) Examine the areas that follow for scratches, dents and cracks:
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 18, LH/RH between FR 47 and FR 64,
external surface.
(2) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for the
permitted damage limits.
(3) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for the
correct repair procedure.
Subtask 53-41-00-210-113-B
A. Inspection
(1) Examine the areas that follow for scratches, dents and cracks:
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 18, LH/RH between FR 47.5 and FR 64,
external surface.
EFF :
ALL 53-41-00
Page B631
Feb 01/08
R
IAC
Upper Skin of longitudinal Lap Joints, including Crack Stopper Areas at
Stringer 18, LH/RH to Bottom Centerline, External Surface
Figure 645/TASK 53-41-00-991-060
R EFF :
001-012, 014-099,
53-41-00 Page B632
Feb 01/08
IAC
Upper Skin of longitudinal Lap Joints, including Crack Stopper Areas at
Stringer 18, LH/RH to Bottom Centerline, External Surface
Figure 645A/TASK 53-41-00-991-060-B
R EFF :
101-199,
53-41-00 Page B633
Feb 01/08
IAC
Upper Skin of longitudinal Lap Joints, including Crack Stopper Areas at
Stringer 18, LH/RH to Bottom Centerline, External Surface
Figure 645B/TASK 53-41-00-991-060-A
R EFF :
901-999,
53-41-00 Page B634
Feb 01/08
IAC
(2) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for the
permitted damage limits.
(3) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for the
correct repair procedure.
Subtask 53-41-00-210-113-A
A. Inspection
(1) Examine the areas that follow for scratches, dents and cracks:
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 18, LH/RH between FR 47/51 and FR 64,
external surface.
5. Close-up
________
Subtask 53-41-00-942-093
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
ALL 53-41-00
Page B635
Feb 01/08
IAC
TASK 53-41-00-210-812
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
R
R Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page B636
May 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-941-072
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
(2) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in the applicable
position.
Subtask 53-41-00-110-095
B. Cleaning Procedure
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material
No. 19-003) and the CLEANING AGENTS (Material No. 11-026), and let
the area dry.
EFF :
ALL 53-41-00
Page B637
Feb 01/08
R
IAC
4. Procedure
_________
Subtask 53-41-00-210-114
A. Inspection
(1) Examine the areas that follow for scratches, dents and cracks:
- the lower skin of the longitudinal lap joints in the crack stopper
areas at stringer 18, LH/RH between FR 47 and FR 64, external
surface.
(2) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for the
permitted damage limits.
(3) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for the
correct repair procedure.
Subtask 53-41-00-210-114-B
A. Inspection
(1) Examine the areas that follow for scratches, dents and cracks:
- the lower skin of the longitudinal lap joints in the crack stopper
areas at stringer 18, LH/RH between FR 47.5 and FR 64, external
surface.
EFF :
ALL 53-41-00
Page B638
Feb 01/08
R
IAC
Lower Skin of longitudinal Lap Joints in Crack Stopper Areas at Stringer 18,
LH/RH, External Surface
Figure 646/TASK 53-41-00-991-063
R EFF :
001-012, 014-099,
53-41-00 Page B639
Feb 01/08
IAC
Lower Skin of longitudinal Lap Joints in Crack Stopper Areas at Stringer 18,
LH/RH, External Surface
Figure 646A/TASK 53-41-00-991-063-B
R EFF :
101-199,
53-41-00 Page B640
Feb 01/08
IAC
Lower Skin of longitudinal Lap Joints in Crack Stopper Areas at Stringer 18,
LH/RH, External Surface
Figure 646B/TASK 53-41-00-991-063-A
R EFF :
901-999,
53-41-00 Page B641
Feb 01/08
IAC
(2) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for the
permitted damage limits.
(3) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for the
correct repair procedure.
Subtask 53-41-00-210-114-A
A. Inspection
(1) Examine the areas that follow for scratches, dents and cracks:
- the lower skin of the longitudinal lap joints in the crack stopper
areas at stringer 18, LH/RH between FR 47/51 and FR 64, external
surface.
(2) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for the
permitted damage limits.
(3) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for the
correct repair procedure.
5. Close-up
________
Subtask 53-41-00-942-094
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
ALL 53-41-00
Page B642
Feb 01/08
IAC
TASK 53-41-00-210-813
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
R
R Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page B643
May 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-941-073
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
(2) Put the ACCESS PLATFORM 1M(3 FT) in the applicable position.
Subtask 53-41-00-110-096
B. Cleaning Procedure
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material
No. 19-003) and the CLEANING AGENTS (Material No. 11-026), and let
the area dry.
EFF :
ALL 53-41-00
Page B644
Feb 01/08
R
IAC
4. Procedure
_________
Subtask 53-41-00-210-115
A. Inspection
(1) Examine the areas that follow for scratches, dents and cracks:
- the lower skin of the longitudinal lap joints in the crack stopper
areas at stringer 32, LH/RH between FR 53 and FR 70, external
surface.
(2) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for the
permitted damage limits.
(3) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for the
correct repair procedure.
Subtask 53-41-00-210-115-B
A. Inspection
(1) Examine the areas that follow for scratches, dents and cracks:
- the lower skin of the longitudinal lap joints in the crack stopper
areas at stringer 32, LH/RH between FR 48 and FR 70, external
surface.
EFF :
ALL 53-41-00
Page B645
Feb 01/08
R
IAC
Lower Skin of longitudinal Lap Joints in Crack Stopper Areas at Stringer 32,
LH/RH, External Surface
Figure 647/TASK 53-41-00-991-066
R EFF :
001-012, 014-099,
53-41-00 Page B646
Feb 01/08
IAC
Lower Skin of longitudinal Lap Joints in Crack Stopper Areas at Stringer 32,
LH/RH, External Surface
Figure 647A/TASK 53-41-00-991-066-B
R EFF :
101-199,
53-41-00 Page B647
Feb 01/08
IAC
Lower Skin of longitudinal Lap Joints in Crack Stopper Areas at Stringer 32,
LH/RH, External Surface
Figure 647B/TASK 53-41-00-991-066-A
R EFF :
901-999,
53-41-00 Page B648
Feb 01/08
IAC
(2) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for the
permitted damage limits.
(3) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for the
correct repair procedure.
Subtask 53-41-00-210-115-A
A. Inspection
(1) Examine the areas that follow for scratches, dents and cracks:
- the lower skin of the longitudinal lap joints in the crack stopper
areas at stringer 32, LH/RH between FR 57 and FR 70, external
surface.
(2) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for the
permitted damage limits.
(3) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for the
correct repair procedure.
5. Close-up
________
Subtask 53-41-00-942-095
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-41-00
Page B649
Feb 01/08
R
IAC
TASK 53-41-00-210-814
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page B650
Feb 01/08
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-941-074
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
(2) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in the required
position.
Subtask 53-41-00-110-097
B. Cleaning Procedure
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material
No. 19-003) and the CLEANING AGENTS (Material No. 11-004), and let
the area dry.
EFF :
ALL 53-41-00
Page B651
Feb 01/08
R
IAC
4. Procedure
_________
Subtask 53-41-00-210-116
A. Inspection
(1) Examine the following area for scratches, dents and cracks:
- the fuselage skin around the AFT passenger/crew door cutouts
between FR 65 and FR 70 and from stringer 6 to stringer 26,
external surface, LH/RH.
NOTE : This does not include the area under the scuff plates.
____
5. Close-up
________
Subtask 53-41-00-942-096
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-41-00
Page B652
Feb 01/08
R
IAC
Fuselage Skin around AFT Passenger/Crew Door Cutouts
Figure 648/TASK 53-41-00-991-069
EFF :
ALL 53-41-00
Page B653
Feb 01/08
R
IAC
TASK 53-41-00-210-815
General Visual Inspection of Fuselage Skin around Outflow Valve Cutout, between
FR 65 and FR 66 and from Stringer 26 to Stringer 31, RH, External Surface
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page B654
Feb 01/08
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-941-075
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
(2) Put the ACCESS PLATFORM 1M(3 FT) in the required position.
Subtask 53-41-00-110-098
B. Cleaning Procedure
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material
No. 19-003) and the CLEANING AGENTS (Material No. 11-004), and let
the area dry.
EFF :
ALL 53-41-00
Page B655
Feb 01/08
R
IAC
4. Procedure
_________
Subtask 53-41-00-210-117
A. Inspection
(1) Examine the following area for scratches, dents and cracks:
- the external fuselage skin around the cutout for the fuselage
outflow valve between FR 65 and FR 66 and from stringer 26 to
stringer 31, RH.
5. Close-up
________
Subtask 53-41-00-942-097
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-41-00
Page B656
Feb 01/08
R
IAC
External Fuselage Skin around the Cutout for the Fuselage Outflow Valve
Figure 649/TASK 53-41-00-991-073
EFF :
ALL 53-41-00
Page B657
Feb 01/08
R
IAC
TASK 53-41-00-210-816
General Visual Inspection of Fuselage Skin around Water Service Panel Cutout
between FR 65 and FR 66 and from STGR 37 to STGR 43, LH, External Surface
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page B658
Feb 01/08
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-941-076
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
(2) Put the ACCESS PLATFORM 1M(3 FT) in the required position.
Subtask 53-41-00-110-099
B. Cleaning Procedure
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material
No. 19-003) and the CLEANING AGENTS (Material No. 11-004), and let
the area dry.
EFF :
ALL 53-41-00
Page B659
Feb 01/08
R
IAC
4. Procedure
_________
Subtask 53-41-00-210-118
A. Inspection
(1) Examine the following area for scratches, dents and cracks:
- the external fuselage skin around the cutout for the potable water
service door between FR 65 and FR 66 and from stringer 37 to
stringer 43, LH.
5. Close-up
________
Subtask 53-41-00-942-098
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-41-00
Page B660
Feb 01/08
R
IAC
External Fuselage Skin around the Cutout for the Potable Water Service Door
Figure 650/TASK 53-41-00-991-074
EFF :
ALL 53-41-00
Page B661
Feb 01/08
R
IAC
TASK 53-41-00-210-817
General Visual Inspection of Fuselage Skin around Waste Service Panel Cutout
between FR 65 and FR 66 and from STGR 33 to STGR 40, RH, External Surface
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page B662
Feb 01/08
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-941-077
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
(2) Put the ACCESS PLATFORM 1M(3 FT) in the required position.
Subtask 53-41-00-110-100
B. Cleaning Procedure
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material
No. 19-003) and the CLEANING AGENTS (Material No. 11-026), and let
the area dry.
4. Procedure
_________
Subtask 53-41-00-210-119
A. Inspection
(1) Examine the following area for scratches, dents and cracks:
- the external fuselage skin around the cutout for the lavatory
(waste) service door between FR 65 and FR 66 and from stringer 33
to stringer 40, RH.
EFF :
ALL 53-41-00
Page B663
Feb 01/08
R
IAC
External Fuselage Skin around the Cutout for the Lavatory (Waste) Service Door
Figure 651/TASK 53-41-00-991-075
R
EFF :
ALL 53-41-00
Page B664
Feb 01/08
IAC
5. Close-up
________
Subtask 53-41-00-942-099
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
ALL 53-41-00
Page B665
Feb 01/08
IAC
TASK 53-41-00-210-818
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
R
R Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page B666
May 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-941-078
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
(2) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in the required
position.
Subtask 53-41-00-110-101
B. Cleaning Procedure
EFF :
ALL 53-41-00
Page B667
Feb 01/08
R
IAC
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material
No. 19-003) and the CLEANING AGENTS (Material No. 11-004), and let
the area dry.
4. Procedure
_________
Subtask 53-41-00-210-120
A. Inspection
(1) Examine the following area for scratches, dents and cracks:
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 41 RH between FR 51 and FR 58.
EFF :
ALL 53-41-00
Page B668
Feb 01/08
R
IAC
Upper Skin of the Longitudinal Lap Joint at STGR 41 RH
Figure 652/TASK 53-41-00-991-076
R
EFF :
001-012, 014-099, 101-199, 53-41-00
Page B669
Feb 01/08
IAC
Upper Skin of the Longitudinal Lap Joint at STGR 41 RH
Figure 652A/TASK 53-41-00-991-076-A
R
EFF :
901-999, 53-41-00
Page B670
Feb 01/08
IAC
**ON A/C 901-999,
Subtask 53-41-00-210-120-A
A. Inspection
(1) Examine the following area for scratches, dents and cracks:
- the upper skin of the longitudinal lap joints, including the crack
stopper areas at stringer 41 RH between FR 47/51 and FR 58.
5. Close-up
________
Subtask 53-41-00-942-100
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-41-00
Page B671
Feb 01/08
R
IAC
TASK 53-41-00-210-819
General Visual Inspection of AFT Cargo Door Actuator Attach Bracket, between
Floor Beams
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page B672
Feb 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-153
A. Get Access
(1) Open the AFT cargo compartment door (Ref. TASK 52-30-00-860-001).
(2) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in the required
position.
(3) If installed, remove the ACT2 from the AFT cargo compartment
(Ref. TASK 28-11-27-000-001)
(4) Remove the access panel 151CC in the ceiling of the AFT Cargo
Compartment.
EFF :
ALL 53-41-00
Page B673
Feb 01/08
IAC
**ON A/C 101-199,
Subtask 53-41-00-010-153-B
A. Get Access
(1) Open the AFT cargo compartment door (Ref. TASK 52-30-00-860-001).
(2) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in the required
position.
(3) If installed, remove the ACT2 from the AFT cargo compartment
(Ref. TASK 28-11-27-000-001)
(4) Remove the access panel 151CC in the ceiling of the AFT Cargo
Compartment.
Subtask 53-41-00-010-153-A
A. Get Access
(1) Open the AFT cargo compartment door (Ref. TASK 52-30-00-860-001).
(2) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in the required
position.
(3) If installed, remove the ACT3 from the AFT cargo compartment
(Ref. TASK 28-11-27-000-004)
(4) If installed, remove the ACT2 from the AFT cargo compartment
(Ref. TASK 28-11-27-000-003)
(5) Remove the access panel 151GC in the ceiling of the AFT Cargo
Compartment.
R
EFF :
101-199, 901-999, 53-41-00
Page B674
Feb 01/08
IAC
**ON A/C ALL
Subtask 53-41-00-110-102
B. Cleaning Procedure
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material
R No. 19-003) and the CLEANING AGENTS (Material No. 11-026), and let
the area dry.
4. Procedure
_________
Subtask 53-41-00-210-121
R A. Inspection
R
R (a) Make sure that you examine the floor beams and the actuator
R attach-bracket.
R
EFF :
ALL 53-41-00
Page B675
Feb 01/08
IAC
AFT Cargo Door Actuator Attach Bracket
Figure 653/TASK 53-41-00-991-077
R
EFF :
ALL 53-41-00
Page B676
Feb 01/08
IAC
R (b) Look for corrosion and other damage to the metal parts.
R (a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
R corrosion-protection data.
R (a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
R damage.
R (b) Refer to the ASRM (Ref. ASRM 51-11-11-001) for the permitted
R damage limits.
R (c) Repair the minor damage (Ref. AMM 51-73-11-300-001) or (Ref. AMM
R 51-73-11-300-004).
R (d) If you find other damage to the metal parts, that is more than
R the limits for minor damage, you must:
R 1
_ Refer to the ASRM for the material details, the item
R identification and the action/repair data:
R - For the floor beams refer to the ASRM (Ref. ASRM 53-41-49-
R 001).
Subtask 53-41-00-210-121-A
(a) Make sure that you examine the floor beams and the actuator
attach-bracket.
(b) Look for corrosion and other damage to the metal parts.
R
EFF :
ALL 53-41-00
Page B677
Feb 01/08
IAC
(2) If you find corrosion damage:
R (a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion-protection data.
R (a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
R damage.
R (b) Refer to the ASRM (Ref. ASRM 51-11-11-001) for the permitted
R damage limits.
(c) Repair the minor damage (Ref. AMM 51-73-11-300-001) or (Ref. AMM
51-73-11-300-004).
(d) If you find other damage to the metal parts, that is more than
the limits for minor damage, you must:
1
_ Refer to the ASRM for the material details, the item
identification and the action/repair data:
R - For the floor beams refer to the ASRM (Ref. ASRM 53-41-49-
R 001).
5. Close-up
________
Subtask 53-41-00-410-151
A. Close Access
(1) Install the access panel 151CC in the ceiling of the AFT Cargo
Compartment.
(2) If removed, install the ACT2 in the AFT cargo compartment (Ref. TASK
28-11-27-400-001)
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
ALL 53-41-00
Page B678
Feb 01/08
IAC
(4) Remove the access platform(s).
(5) Close the AFT cargo compartment door (Ref. TASK 52-30-00-860-002).
Subtask 53-41-00-410-151-B
A. Close Access
(1) Install the access panel 151CC in the ceiling of the AFT Cargo
Compartment.
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Close the AFT cargo compartment door (Ref. TASK 52-30-00-860-002).
Subtask 53-41-00-410-151-A
A. Close Access
(1) Install the access panel 151GC in the ceiling of the AFT Cargo
Compartment.
(2) If removed, install the ACT2 in the AFT cargo compartment (Ref. TASK
28-11-27-400-003)
(3) If removed, install the ACT3 in the AFT cargo compartment (Ref. TASK
28-11-27-400-004)
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
(6) Close the AFT cargo compartment door (Ref. TASK 52-30-00-860-002).
R
EFF :
ALL 53-41-00
Page B679
Feb 01/08
IAC
**ON A/C 101-199,
TASK 53-41-00-210-820
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
101-199, 53-41-00
Page B680
Feb 01/08
IAC
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-941-079
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
(2) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in the required
position.
Subtask 53-41-00-110-103
B. Cleaning Procedure
R
EFF :
101-199, 53-41-00
Page B681
Feb 01/08
IAC
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material
No. 19-003) and the CLEANING AGENTS (Material No. 11-004), and let
the area dry.
4. Procedure
_________
Subtask 53-41-00-210-122
A. Inspection
(1) Examine the following area for scratches, dents and cracks:
- the circumferential joint above the AFT emergency exit door at FR
47.3 from stringer 6 to stringer 12, external surface, LH/RH.
5. Close-up
________
Subtask 53-41-00-942-101
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
101-199, 53-41-00
Page B682
Feb 01/08
IAC
Circumferential Joint above the AFT Emergency Door
Figure 654/TASK 53-41-00-991-078
R
EFF :
101-199, 53-41-00
Page B683
Feb 01/08
IAC
(3) Remove the access platform(s).
R
EFF :
101-199, 53-41-00
Page B684
Feb 01/08
IAC
**ON A/C ALL
TASK 53-41-00-210-823
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-41-00
Page B685
Feb 01/08
IAC
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-41-00
Page B686
Feb 01/08
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-41-00-941-081
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
(2) Put the ACCESS PLATFORM 8M (26 FT) - ADJUSTABLE in the required
position.
Subtask 53-41-00-110-106
B. Cleaning Procedure
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material
No. 19-003) and the CLEANING AGENTS (Material No. 11-004), and let
the area dry.
4. Procedure
_________
EFF :
ALL 53-41-00
Page B687
Feb 01/08
R
IAC
External Surface from STGR23 LH/RH to Crown Centerline
Figure 655/TASK 53-41-00-991-082
R
EFF :
001-012, 014-099, 53-41-00
Page B688
Feb 01/08
IAC
**ON A/C 101-199,
Subtask 53-41-00-210-125
A. Inspection
(1) Examine the following areas for scratches, dents and cracks:
- the external surface of the fuselage between FR47 and FR 70 from
STGR 23LH to the crown centerline and from STGR 23RH to the crown
centerline.
Subtask 53-41-00-210-125-A
A. Inspection
(1) Examine the following areas for scratches, dents and cracks:
- the external surface of the fuselage between FR47/51 and FR 70 from
STGR 23LH to the crown centerline and from STGR 23RH to the crown
centerline.
EFF :
ALL 53-41-00
Page B689
Feb 01/08
R
IAC
External Surface from STGR23 LH/RH to Crown Centerline
Figure 655A/TASK 53-41-00-991-082-B
R
EFF :
101-199, 53-41-00
Page B690
Feb 01/08
IAC
External Surface from STGR23 LH/RH to Crown Centerline
Figure 655B/TASK 53-41-00-991-082-A
R
EFF :
901-999, 53-41-00
Page B691
Feb 01/08
IAC
**ON A/C ALL
5. Close-up
________
Subtask 53-41-00-942-102
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
ALL 53-41-00
Page B692
Feb 01/08
IAC
TASK 53-41-00-210-824
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-41-00
Page B693
Feb 01/08
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-41-00
Page B694
Feb 01/08
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-41-00-010-159
A. Get Access
(1) Remove the AFT Galley (Ref. TASK 25-33-41-000-001) or (Ref. TASK 25-
33-41-000-002) or (Ref. TASK 25-33-45-000-001).
(4) Remove the linings (Ref. TASK 25-23-41-000-001), (Ref. TASK 25-23-42-
000-001), (Ref. TASK 25-23-43-000-001), (Ref. TASK 25-23-44-000-001),
(Ref. TASK 25-23-46-000-002) and (Ref. TASK 25-23-47-000-001).
Subtask 53-41-00-110-107
B. Clean the inspection area with CLEANING AGENTS (Material No. 11-003) and
a lint-free cloth.
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
EFF :
ALL 53-41-00
Page B695
Feb 01/08
R
IAC
4. Procedure
_________
Subtask 53-41-00-210-126
A. Inspection
(1) Examine the following areas for scratches, dents and cracks:
- the internal structure of the fuselage between FR47 and FR 70 above
the cabin floor level.
Subtask 53-41-00-210-126-A
A. Inspection
(1) Examine the following areas for scratches, dents and cracks:
- the internal structure of the fuselage between FR47/51 and FR 70
above the cabin floor level.
EFF :
ALL 53-41-00
Page B696
Feb 01/08
R
IAC
Internal Structure above Cabin Floor
Figure 656/TASK 53-41-00-991-083
R
EFF :
001-012, 014-099, 53-41-00
Page B697
Feb 01/08
IAC
Internal Structure above Cabin Floor
Figure 656A/TASK 53-41-00-991-083-B
R
EFF :
101-199, 53-41-00
Page B698
Feb 01/08
IAC
Internal Structure above Cabin Floor
Figure 656B/TASK 53-41-00-991-083-A
R
EFF :
901-999, 53-41-00
Page B699
Feb 01/08
IAC
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-12-201) and
____
(Ref. ASRM 53-41-13-201) for the correct repair procedure.
5. Close-up
________
Subtask 53-41-00-410-156
A. Close Access
(2) Install the linings (Ref. TASK 25-23-41-400-001), (Ref. TASK 25-23-
42-400-001), (Ref. TASK 25-23-43-400-001), (Ref. TASK 25-23-44-400-
001), (Ref. TASK 25-23-46-400-002) and (Ref. TASK 25-23-47-400-001).
(5) Install the AFT Galley (Ref. TASK 25-33-41-400-001) or (Ref. TASK 25-
33-41-400-002) or (Ref. TASK 25-33-45-400-001).
(6) Make sure that the work area is clean and clear of tool(s) and other
items.
(7) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page C600
Feb 01/08
R
IAC
TASK 53-41-00-210-825
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-41-00
Page C601
Feb 01/08
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-41-00
Page C602
Feb 01/08
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-160
A. Get Access
(1) Open the AFT Cargo Compartment Door (Ref. TASK 52-30-00-860-001).
(4) Remove the linings (Ref. TASK 25-55-11-000-001), (Ref. TASK 25-55-12-
000-001), (Ref. TASK 25-55-11-000-002), (Ref. TASK 25-55-11-000-003),
(Ref. TASK 25-55-12-000-002) and (Ref. TASK 25-55-12-000-003).
R
EFF :
ALL 53-41-00
Page C603
Feb 01/08
IAC
**ON A/C 901-999,
Subtask 53-41-00-010-160-A
A. Get Access
(1) Open the AFT Cargo Compartment Door (Ref. TASK 52-30-00-860-001).
(6) Remove the linings (Ref. TASK 25-55-11-000-001), (Ref. TASK 25-55-12-
000-001), (Ref. TASK 25-55-11-000-002), (Ref. TASK 25-55-11-000-003),
(Ref. TASK 25-55-12-000-002) and (Ref. TASK 25-55-12-000-003).
Subtask 53-41-00-110-108
B. Clean the inspection area with CLEANING AGENTS (Material No. 11-003) and
a lint-free cloth.
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
EFF :
ALL 53-41-00
Page C604
Feb 01/08
R
IAC
4. Procedure
_________
Subtask 53-41-00-210-127
A. Inspection
(1) Examine the following areas for scratches, dents and cracks:
- the internal structure of the fuselage between FR46 and FR 65,
between the cabin floor panels and the cargo compartment floor
including the cabin floor structure.
R
EFF :
ALL 53-41-00
Page C605
Feb 01/08
IAC
Internal Structure between Cabin Floor and Cargo Compartment Floor
Figure 657/TASK 53-41-00-991-084
R
EFF :
001-012, 014-099, 53-41-00
Page C606
Feb 01/08
IAC
Internal Structure between Cabin Floor and Cargo Compartment Floor
Figure 657A/TASK 53-41-00-991-084-B
EFF :
101-199, 53-41-00
Page C607
Feb 01/08
R
IAC
Internal Structure between Cabin Floor and Cargo Compartment Floor
Figure 657B/TASK 53-41-00-991-084-A
R
EFF :
901-999, 53-41-00
Page C608
Feb 01/08
IAC
5. Close-up
________
Subtask 53-41-00-410-157
A. Close Access
(2) Install the linings (Ref. TASK 25-55-11-400-001), (Ref. TASK 25-55-
12-400-001), (Ref. TASK 25-55-11-400-002), (Ref. TASK 25-55-11-400-
003), (Ref. TASK 25-55-12-400-002) and (Ref. TASK 25-55-12-400-003).
(5) Make sure that the work area is clean and clear of tool(s) and other
items.
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
(8) Close the AFT Cargo Compartment Door (Ref. TASK 52-30-00-860-004).
Subtask 53-41-00-410-157-A
A. Close Access
(2) Install the linings (Ref. TASK 25-55-11-400-001), (Ref. TASK 25-55-
12-400-001), (Ref. TASK 25-55-11-400-002), (Ref. TASK 25-55-11-400-
003), (Ref. TASK 25-55-12-400-002) and (Ref. TASK 25-55-12-400-003).
R
EFF :
ALL 53-41-00
Page C609
Feb 01/08
IAC
(6) If removed, install the ACT3 (Ref. TASK 28-11-27-400-004).
(7) Make sure that the work area is clean and clear of tool(s) and other
items.
(8) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
(10) Close the AFT Cargo Compartment Door (Ref. TASK 52-30-00-860-004).
R
EFF :
901-999, 53-41-00
Page C610
Feb 01/08
IAC
**ON A/C 101-199,
TASK 53-41-00-210-826
General Visual Inspection of AFT Emergency Exit Skin Cutouts, Upper and Lower
Corners, External Surface, LH/RH
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
101-199, 53-41-00
Page C611
Feb 01/08
IAC
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-941-082
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
(2) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in the required
position.
Subtask 53-41-00-110-109
B. Cleaning Procedure
R
EFF :
101-199, 53-41-00
Page C612
Feb 01/08
IAC
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material
No. 19-003) and the CLEANING AGENTS (Material No. 11-004), and let
the area dry.
4. Procedure
_________
Subtask 53-41-00-210-128
A. Inspection
(1) Examine the following areas for scratches, dents and cracks:
- the external surface of the the upper and lower skin cutouts of the
AFT Emergency Exit, LH and RH.
5. Close-up
________
Subtask 53-41-00-942-103
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
101-199, 53-41-00
Page C613
Feb 01/08
IAC
Upper and Lower Corners of the AFT Emergency Skin Cutouts
Figure 658/TASK 53-41-00-991-085
R
EFF :
101-199, 53-41-00
Page C614
Feb 01/08
IAC
(3) Remove the access platform(s).
R
EFF :
101-199, 53-41-00
Page C615
Feb 01/08
IAC
**ON A/C ALL
TASK 53-41-00-220-003
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page C616
Feb 01/08
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-860-050
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(2) Put the warning notice on the slat/flap control lever to tell persons
not to operate the flaps.
Subtask 53-41-00-941-053
B. Get Access
(1) Put the adjustable access platform in position below the inspection
area.
EFF :
ALL 53-41-00
Page C617
Feb 01/08
R
IAC
Subtask 53-41-00-860-051
(1) Make sure that the surfaces of the inspection areas are clean and
smooth.
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR
MOUTH OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10
AND 15 MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS,
FLAMMABLE AND SKIN IRRITANTS.
(2) If necessary, clean the inspection areas with the CLEANING AGENTS
(Material No. 11-004) and a MISCELLANEOUS (Material No. 19-003). Make
sure the inspection areas are dry before you continue.
(3) If necessary, make the surface of the inspection areas smooth with
the abrasive cloth, grade 280.
(4) Do a visual inspection of the inspection areas. Look for damage and
defects in the shape of the external surface.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
EFF :
ALL 53-41-00
Page C618
Feb 01/08
R
IAC
(c) If you find other types of damage:
- Refer to the ASRM (Ref. ASRM 51-73-00-001) for the repair of
the minor damage.
4. Procedure
_________
Subtask 53-41-00-250-051
(2) Write a report if you find damage during the inspection procedure.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
EFF :
ALL 53-41-00
Page C619
Feb 01/08
R
IAC
**ON A/C 901-999,
Subtask 53-41-00-250-051-A
A. Inspection
(2) Write a report if you find damage during the inspection procedure.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
5. Close-up
________
Subtask 53-41-00-370-051
EFF :
ALL 53-41-00
Page C620
Feb 01/08
R
IAC
Subtask 53-41-00-942-053
B. Close Access
Subtask 53-41-00-860-052
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page C621
Feb 01/08
R
IAC
TASK 53-41-00-220-004
Special Detailed Inspection of Frame Splices and Adjacent Area from FR53 to
FR60, located above Stringer 18 RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page C622
Feb 01/08
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-085
A. Get Access
(1) Remove the right upper sidewall panels 252PW, 252LW, 252HW (Ref. TASK
25-23-43-000-001) and the right lower sidewall panels 252NW, 252KW
(Ref. TASK 25-23-44-000-001).
(2) Remove the insulation blankets from the inspection area (Ref. TASK
25-80-00-000-001).
Subtask 53-41-00-860-053
(1) Make sure that the surfaces of the inspection areas are clean and
smooth.
(2) If necessary, clean the inspection areas with the CLEANING AGENTS
(Material No. 11-026) and a MISCELLANEOUS (Material No. 19-003). Make
sure the inspection areas are dry before you continue.
EFF :
ALL 53-41-00
Page C623
Feb 01/08
R
IAC
(3) If necessary, make the surface of the inspection areas smooth with
the abrasive cloth, grade 280.
(4) Do a visual inspection of the inspection areas. Look for damage and
defects in the shape of the external surface.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
damage.
4. Procedure
_________
Subtask 53-41-00-220-052
(1) Do the special detailed inspection of the frame splices at FR53 thru
FR56, above the STGR18 RH (Ref. NTM 534106-Part.4).
(2) Write a report if you find damage during the inspection procedure.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
damage.
EFF :
ALL 53-41-00
Page C624
Feb 01/08
R
IAC
(c) If you find other types of damage:
- refer to the ASRM (Ref. ASRM 51-73-00-001) for the repair of
the minor damage
- refer to the ASRM (Ref. ASRM 53-00-12-201) for the correct
repair procedure.
5. Close-up
________
Subtask 53-41-00-370-052
Subtask 53-41-00-410-084
B. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Install the right upper sidewall panels 252PW, 252LW, 252HW
(Ref. TASK 25-23-43-400-001) and the right lower sidewall panels
252NW, 252KW (Ref. TASK 25-23-44-400-001).
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
ALL 53-41-00
Page C625
Feb 01/08
IAC
TASK 53-41-00-220-005
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
ALL 53-41-00
Page C626
Feb 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page C627
Feb 01/08
R
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-41-00-860-054
(2) Put the warning notice on the slat/flap control lever to tell persons
not to operate the flaps.
Subtask 53-41-00-010-081
B. Get Access
(1) Remove the belly-fairing access panels 197BB and 197GB (Ref. TASK 53-
35-13-000-001) (Ref. TASK 53-35-13-000-002).
(2) Remove the sidewall panels in the AFT cargo-compartment (Ref. TASK
25-55-11-000-003).
(3) Remove the necessary insulation to get access to the inspection areas
(Ref. TASK 25-80-00-000-001).
Subtask 53-41-00-010-081-A
B. Get Access
(1) Remove the belly-fairing access panels 197KB and 197GB (Ref. TASK 53-
35-13-000-001) (Ref. TASK 53-35-13-000-002).
(2) Remove the sidewall panels in the AFT cargo-compartment (Ref. TASK
25-55-11-000-003).
(3) Remove the necessary insulation to get access to the inspection areas
(Ref. TASK 25-80-00-000-001).
EFF :
ALL 53-41-00
Page C628
Feb 01/08
R
IAC
**ON A/C ALL
Subtask 53-41-00-860-055
(1) Make sure that the surfaces of the inspection areas are clean and
smooth.
(2) If necessary, clean the inspection areas with the CLEANING AGENTS
(Material No. 11-026) and a MISCELLANEOUS (Material No. 19-003). Make
sure the inspection areas are dry before you continue.
(3) If necessary, make the surface of the inspection areas smooth with
the abrasive cloth, grade 280.
(4) Do a visual inspection of the inspection areas. Look for damage and
defects in the shape of the external surface.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
damage.
4. Procedure
_________
EFF :
ALL 53-41-00
Page C629
Feb 01/08
R
IAC
**ON A/C 001-012, 014-099,
Subtask 53-41-00-220-050
(2) Write a report if you find damage during the inspection procedure.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
damage.
R
EFF :
001-012, 014-099, 53-41-00
Page C630
Feb 01/08
IAC
**ON A/C 101-199,
Subtask 53-41-00-220-050-B
(2) Write a report if you find damage during the inspection procedure.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
damage.
Subtask 53-41-00-220-050-A
(2) Write a report if you find damage during the inspection procedure.
R
EFF :
101-199, 901-999, 53-41-00
Page C631
Feb 01/08
IAC
(3) If you find damage:
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the class of
damage.
5. Close-up
________
Subtask 53-41-00-370-053
Subtask 53-41-00-410-080
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the sidewall panels in the AFT cargo-compartment (Ref. TASK
25-55-11-400-003).
EFF :
ALL 53-41-00
Page C632
Feb 01/08
R
IAC
(4) Install the belly-fairing access panels 197BB and 197GB (Ref. TASK
53-35-13-400-001) (Ref. TASK 53-35-13-400-002).
Subtask 53-41-00-410-080-A
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the sidewall panels in the AFT cargo-compartment (Ref. TASK
25-55-11-400-003).
(4) Install the belly-fairing access panels 197KB and 197GB (Ref. TASK
53-35-13-400-001) (Ref. TASK 53-35-13-400-002).
Subtask 53-41-00-860-056
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page C633
Feb 01/08
R
IAC
TASK 53-41-00-220-006
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page C634
Feb 01/08
R
IAC
3. __________
Job Set-up
Subtask 53-41-00-010-089
A. Get Access
4. Procedure
_________
Subtask 53-41-00-220-053
A. Inspection
5. Close-up
________
Subtask 53-41-00-410-090
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-41-00
Page C635
Feb 01/08
R
IAC
(5) Close the AFT cargo-compartment door (Ref. TASK 52-30-00-860-002).
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page C636
Feb 01/08
R
IAC
TASK 53-41-00-220-007
Special Detailed Inspection of Internal Doubler Forward and AFT Water Service
Panel Cutout between STGR38 and STGR42 LH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page C637
Feb 01/08
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-084
Subtask 53-41-00-860-060
(1) Make sure that the outer surface of the inspection area is clean and
smooth.
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR
MOUTH OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10
AND 15 MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS,
FLAMMABLE AND SKIN IRRITANTS.
(2) If necessary, clean the outer surface of the inspection area with the
CLEANING AGENTS (Material No. 11-004) and a MISCELLANEOUS (Material
No. 19-003).
(3) If necessary, make the outer surface of the inspection area smooth
with the abrasive cloth, grade 280. Make sure the inspection area is
dry before you continue.
EFF :
ALL 53-41-00
Page C638
Feb 01/08
R
IAC
Internal Doubler of the Cutout at the AFT Water Service-Panel
Figure 659/TASK 53-41-00-991-014
EFF :
ALL 53-41-00
Page C639
Feb 01/08
R
IAC
(4) Do a visual inspection of the outer surface of the inspection area.
Look for damage, and defects in the shape of the surface.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
4. Procedure
_________
Subtask 53-41-00-220-051
(2) Write a report about the damage you find during the inspection
procedure.
EFF :
ALL 53-41-00
Page C640
Feb 01/08
R
IAC
5. Close-up
________
Subtask 53-41-00-370-057
Subtask 53-41-00-410-083
(2) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page C641
Feb 01/08
R
IAC
TASK 53-41-00-220-008
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page C642
Feb 01/08
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-094
A. Get Access
(1) Remove the forward and aft scuff plates at the AFT passenger/crew
doors (Ref. TASK 53-45-15-000-001).
(2) Remove the necessary frame linings and the insulation, to get access
to the inner surfaces of the inspection areas (Ref. TASK 25-23-45-
000-003) and (Ref. TASK 25-23-45-000-004).
Subtask 53-41-00-860-058
(1) Make sure that the inner and outer surfaces of the inspection areas
are clean and smooth.
EFF :
ALL 53-41-00
Page C643
Feb 01/08
R
IAC
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR
MOUTH OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10
AND 15 MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS,
FLAMMABLE AND SKIN IRRITANTS.
(2) Clean the inner and outer surfaces of the inspection areas with the
CLEANING AGENTS (Material No. 11-004) and a MISCELLANEOUS (Material
No. 19-003).
(4) Make the inner and outer surfaces of the inspection areas smooth with
the abrasive cloth, grade 280.
(5) Make sure you remove the damaged paint and the paint runs from the
surfaces.
(6) Make sure the inspection areas are clean and dry before you continue.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
EFF :
ALL 53-41-00
Page C644
Feb 01/08
R
IAC
(c) If you find other types of damage:
- refer to the ASRM (Ref. ASRM 53-41-11-101) for the necessary
data.
4. Procedure
_________
Subtask 53-41-00-220-054
(3) Write a report about the damage you find during the inspection
procedure.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
EFF :
ALL 53-41-00
Page C645
Feb 01/08
R
IAC
5. Close-up
________
Subtask 53-41-00-370-055
Subtask 53-41-00-410-095
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the insulation and the frame linings you removed for access
(Ref. TASK 25-23-45-400-008) and (Ref. TASK 25-23-45-400-005).
(3) Install the corner scuff plates at the AFT passenger/crew doors
(Ref. TASK 53-45-15-400-001).
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page C646
Feb 01/08
R
IAC
TASK 53-41-00-220-009
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page C647
Feb 01/08
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-095
Subtask 53-41-00-860-059
(1) Make sure that the outer surface of the inspection area is clean and
smooth.
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR
MOUTH OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10
AND 15 MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS,
FLAMMABLE AND SKIN IRRITANTS.
(2) If necessary, clean the outer surface of the inspection area with the
CLEANING AGENTS (Material No. 11-004) and a MISCELLANEOUS (Material
No. 19-003).
(3) If necessary, make the outer surface of the inspection area smooth
with the abrasive cloth, grade 280. Make sure the inspection area is
dry before you continue.
EFF :
ALL 53-41-00
Page C648
Feb 01/08
R
IAC
Internal Doubler of the Cutout at the Waste Service Panel
Figure 660/TASK 53-41-00-991-022
EFF :
ALL 53-41-00
Page C649
Feb 01/08
R
IAC
(4) Do a visual inspection of the outer surface of the inspection area.
Look for damage, and defects in the shape of the surface.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
4. Procedure
_________
Subtask 53-41-00-220-055
(2) Write a report about the damage you find during the inspection
procedure.
EFF :
ALL 53-41-00
Page C650
Feb 01/08
R
IAC
5. Close-up
________
Subtask 53-41-00-370-056
Subtask 53-41-00-410-096
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page C651
Feb 01/08
R
IAC
TASK 53-41-00-220-010
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page C652
Feb 01/08
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-121
A. Get Access
Subtask 53-41-00-860-057
(1) Make sure that the outer surface of the inspection area is clean and
smooth.
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR
MOUTH OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10
AND 15 MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS,
FLAMMABLE AND SKIN IRRITANTS.
(2) If necessary, clean the outer surface of the inspection area with the
CLEANING AGENTS (Material No. 11-004) and a MISCELLANEOUS (Material
No. 19-003). Make sure the inspection area is dry before you
continue.
(3) If necessary, make the outer surface of the inspection area smooth
with the abrasive cloth, grade 280.
EFF :
ALL 53-41-00
Page C653
Feb 01/08
R
IAC
Circumferential Skin Splice at FR64, from STGR10 LU/RH to Crown Centerline
Figure 661/TASK 53-41-00-991-047
EFF :
ALL 53-41-00
Page C654
Feb 01/08
R
IAC
(4) Do a visual inspection of the outer surface of the inspection area.
Look for damage, and defects in the shape of the external surface.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
4. Procedure
_________
Subtask 53-41-00-220-058
(2) Write a report about the damage you find during the inspection
procedure.
5. Close-up
________
Subtask 53-41-00-370-054
EFF :
ALL 53-41-00
Page C655
Feb 01/08
R
IAC
Subtask 53-41-00-410-118
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page C656
Feb 01/08
R
IAC
TASK 53-41-00-220-011
Special Detailed Inspection of Aft Cargo Door Lock Fitting and Surrounding
Structure between FR53 and FR55A, from STGR41 RH to Door Sill (6 Places)
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page C657
Feb 01/08
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-122
A. Get Access
(3) If installed, remove the rear additional center tank (Ref. AMM
28-11-27, Page Block 401).
(5) Remove the insulation blankets from the inspection area (Ref. TASK
25-80-00-000-001).
EFF :
ALL 53-41-00
Page C658
Feb 01/08
R
IAC
**ON A/C 901-999,
Subtask 53-41-00-010-122-A
A. Get Access
(3) If installed, remove the rear additional center tank (Ref. AMM
28-11-27, Page Block 401).
(5) Remove the insulation blankets from the inspection area (Ref. TASK
25-80-00-000-001).
Subtask 53-41-00-860-061
(1) Make sure that the surfaces of the inspection areas are clean and
smooth.
R
EFF :
ALL 53-41-00
Page C659
Feb 01/08
IAC
Lock Fittings of the Aft Cargo Compartment Door
Figure 662/TASK 53-41-00-991-048
R
EFF :
ALL 53-41-00
Page C660
Feb 01/08
IAC
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR
MOUTH OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10
AND 15 MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS,
FLAMMABLE AND SKIN IRRITANTS.
(2) If necessary, clean the surfaces of the inspection areas with the
CLEANING AGENTS (Material No. 11-004) and a MISCELLANEOUS (Material
No. 19-003).
(4) If necessary, make the surfaces of the inspection areas smooth with
the abrasive cloth, grade 280.
(5) Make sure the inspection areas are clean and dry before you continue.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
R
EFF :
ALL 53-41-00
Page C661
Feb 01/08
IAC
4. Procedure
_________
Subtask 53-41-00-220-059
(1) Do the special detailed inspection of the aft cargo door lock
fittings, and the surrounding structure. Do this from STGR41 RH to
the internal part of the door sill, at 6 places (Ref. NTM 534156-
Part.6).
(2) Write a report about the damage you find during the inspection
procedure.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
R
EFF :
ALL 53-41-00
Page C662
Feb 01/08
IAC
5. Close-up
________
Subtask 53-41-00-370-058
Subtask 53-41-00-410-121
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) If removed, install the rear additional center tank (Ref. AMM
28-11-27, Page Block 401).
(7) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 53-41-00-410-121-A
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
ALL 53-41-00
Page C663
Feb 01/08
IAC
(3) Install the AFT cargo-compartment floor-panels 151VG and 151ZG
(Ref. TASK 53-42-14-400-001).
(4) If removed, install the rear additional center tank (Ref. AMM
28-11-27, Page Block 401).
(7) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
901-999, 53-41-00
Page C664
Feb 01/08
IAC
**ON A/C 101-199,
TASK 53-41-00-220-012
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
101-199, 53-41-00
Page C665
Feb 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
ASRM 51-11-00-001
ASRM 51-22-00-001
ASRM 51-73-00-001
ASRM 51-74-00-001
NTM 53-41-45 P.B. 601
ASRM 53-00-12-201 (for corrective action)
51-73-11-300-003 Repair of Dents in Skin Panels (for corrective
action)
51-74-11-300-001 Repair of Corroded Areas (for corrective action)
53-41-00-991-039 Fig. 630
3. __________
Job Set-up
Subtask 53-41-00-010-124
A. Get Access
(1) Put the warning notice in position to tell persons not to operate the
flight controls.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(2) Put the access platform in position adjacent to FR47.5 LH and RH.
R
EFF :
101-199, 53-41-00
Page C666
Feb 01/08
IAC
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR
MOUTH OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10
AND 15 MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS,
FLAMMABLE AND SKIN IRRITANTS.
(3) If necessary, clean the surfaces of the inspection area with CLEANING
AGENTS (Material No. 11-004) and a MISCELLANEOUS (Material No. 19-
003).
(4) Make sure that the inspection areas are clean and dry before you
continue.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
R
EFF :
101-199, 53-41-00
Page C667
Feb 01/08
IAC
4. Procedure
_________
Subtask 53-41-00-220-060
A. Inspection
(2) Record the damage that you find during the inspection procedure.
(a) Refer to the AMM for the classification of the damage (Ref. TASK
51-73-11-300-003).
(d) If necessary, refer to the ASRM for the correct repair procedure
(Ref. ASRM 53-00-12-201).
5. Close-up
________
Subtask 53-41-00-410-122
A. Close Access
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
101-199, 53-41-00
Page C668
Feb 01/08
IAC
**ON A/C 001-010,
TASK 53-41-00-220-017
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
001-010, 53-41-00
Page C669
Feb 01/08
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-860-065
Subtask 53-41-00-010-168
B. Get Access
(2) Open the left or right AFT passenger/crew door (Ref. TASK 52-10-00-
010-001).
(3) Remove the door frame linings (Ref. TASK 25-23-45-000-003) (Ref. TASK
25-23-45-000-004).
(Ref. Fig. 663/TASK 53-41-00-991-093)
(4) Remove the fasteners that secure the gusset plates to frame 66 at
stringer positions 18, 20 and 22 (Ref. ASRM 51-42-11-001).
R
EFF :
001-010, 53-41-00
Page C670
Feb 01/08
IAC
Gusset Plate Attachment Holes on FR66 at STGR Positions 18, 20, 2
Figure 663/TASK 53-41-00-991-093
R
EFF :
001-010, 53-41-00
Page C671
Feb 01/08
IAC
Subtask 53-41-00-110-119
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Make sure that the surfaces of the inspection areas are clean.
(2) If necessary, clean the inspection areas with the CLEANING AGENTS
(Material No. 11-026) and a lint-free cotton cloth MISCELLANEOUS
(Material No. 19-003).
4. Procedure
_________
Subtask 53-41-00-220-065
(1) Do the special detailed inspection (Ref. NTM 511001) of the gusset
plate attachment holes on FR66 at stringer positions 18, 20 and 22.
(2) Write a report about the damage you find during the inspection
procedure.
R
EFF :
001-010, 53-41-00
Page C672
Feb 01/08
IAC
5. Close-up
________
Subtask 53-41-00-410-165
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the fasteners that secure the gusset plates to frame 66 a
stringer positions 18, 20 and 22 (Ref. ASRM 51-42-11-001).
(4) Close the left or right AFT passenger/crew door (Ref. TASK 52-10-00-
410-001).
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 53-41-00-862-058
R
EFF :
001-010, 53-41-00
Page C673
Feb 01/08
IAC
**ON A/C 001-012, 014-019,
TASK 53-41-00-220-018
Special Detailed Inspection of Former Junction Fastener Holes and Tooling Hole
on FR68, LH/RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
001-012, 014-019, 53-41-00
Page C674
Feb 01/08
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-861-060
Subtask 53-41-00-010-169
B. Get Access
(2) Open the left or right AFT passenger/crew door (Ref. TASK 52-10-00-
010-001).
(3) Remove the door frame linings (Ref. TASK 25-23-45-000-003) (Ref. TASK
25-23-45-000-004).
(Ref. Fig. 664/TASK 53-41-00-991-094)
(4) Remove the fasteners that secure the former junction on frame 68,
LH/RH (Ref. ASRM 51-42-11-001).
R
EFF :
001-012, 014-019, 53-41-00
Page C675
Feb 01/08
IAC
Former Junction Fastener Holes and Tooling Hole on FR68, LH/RH
Figure 664/TASK 53-41-00-991-094
R
EFF :
001-012, 014-019, 53-41-00
Page C676
Feb 01/08
IAC
Subtask 53-41-00-110-120
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Make sure that the surfaces of the inspection areas are clean.
(2) If necessary, clean the inspection areas with the CLEANING AGENTS
(Material No. 11-026) and a lint-free cotton cloth MISCELLANEOUS
(Material No. 19-003).
4. Procedure
_________
Subtask 53-41-00-220-066
(2) Write a report about the damage you find during the inspection
procedures.
R
EFF :
001-012, 014-019, 53-41-00
Page C677
Feb 01/08
IAC
- you must contact AIRBUS INDUSTRIE for the necessary
corrective action procedure.
5. Close-up
________
Subtask 53-41-00-410-166
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the fasteners that secure the former junction to frame 68,
LH/RH (Ref. ASRM 51-42-11-001).
(4) Close the left or right AFT passenger/crew door (Ref. TASK 52-10-00-
410-001).
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 53-41-00-862-059
R
EFF :
001-012, 014-019, 53-41-00
Page C678
Feb 01/08
IAC
**ON A/C ALL
TASK 53-41-00-210-834
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
A. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page C679
Feb 01/08
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-170
Subtask 53-41-00-860-069
Subtask 53-41-00-010-171
C. Get Access
(1) Remove the door frame linings of the aft passenger/crew doors
(Ref. TASK 25-23-45-000-003) and (Ref. TASK 25-23-45-000-004).
EFF :
ALL 53-41-00
Page C680
Feb 01/08
R
IAC
Subtask 53-41-00-110-121
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
4. Procedure
_________
Subtask 53-41-00-210-135
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion-protection data.
EFF :
ALL 53-41-00
Page C681
Feb 01/08
R
IAC
Lower-Corners Internal-Structure of the AFT Passenger/Crew Door-Cutouts
Figure 665/TASK 53-41-00-991-095
R
EFF :
ALL 53-41-00
Page C682
Feb 01/08
IAC
(b) Repair the corroded areas (Ref. TASK 51-74-11-300-001).
(b) Refer to the ASRM (Ref. ASRM 51-11-11-001) for the allowable
damage limits.
Subtask 53-41-00-916-088
5. Close-up
________
Subtask 53-41-00-410-167
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Install the door frame linings of the aft passenger/crew doors
(Ref. TASK 25-23-45-400-008) and (Ref. TASK 25-23-45-400-005).
R
EFF :
ALL 53-41-00
Page C683
Feb 01/08
IAC
TASK 53-41-00-210-835
Detailed Visual Inspection of Cabin Floor Structure and Structure below AFT
Entrance Area, between FR66 and FR68 and Lateral Shear Plates FR68 and FR70
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
A. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page C684
Feb 01/08
R
IAC
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page C685
Feb 01/08
R
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-172
A. Get Access
(1) If necessary, remove the cabin attendant seat(s) (Ref. TASK 25-22-41-
000-001) or (Ref. TASK 25-22-42-000-001).
(2) Remove the applicable floor panels between FR66 and FR68 (Ref. TASK
53-42-12-000-002).
NOTE : The removal of the aft galley is only necessary if you cannot
____
get access to the lateral shear plates.
(6) Clean the inspection area with the CLEANING AGENTS (Material No. 11-
026) and a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
4. Procedure
_________
EFF :
ALL 53-41-00
Page C686
Feb 01/08
R
IAC
Cabin Floor Structure - FR66 thru FR70
Figure 666/TASK 53-41-00-991-096
R
EFF :
001-012, 014-099, 53-41-00
Page C687
Feb 01/08
IAC
Cabin Floor Structure - FR66 thru FR70
Figure 666A/TASK 53-41-00-991-096-A
EFF :
101-199, 901-999, 53-41-00
Page C688
Feb 01/08
R
IAC
**ON A/C ALL
Subtask 53-41-00-210-136
(1) Do a detailed visual inspection of the cabin floor structure and the
structure below the aft entrance area. Do this between FR66 and FR68
and the lateral shear plates between FR68 and FR70.
(b) Look for corrosion and other damage to the metal parts.
(4) If you find other damage to the metal parts that is more than the
limits for minor damage, you must:
(a) Refer to the ASRM for the material details, the item
identification and the action/repair data:
- For the floor structure, refer to the ASRM (Ref. ASRM 53-41-14-
001-001).
5. Close-up
________
Subtask 53-41-00-916-089
A. Corrosion Protection
R
EFF :
ALL 53-41-00
Page C689
Feb 01/08
IAC
Lateral Shear Plates - Inspection Area
Figure 667/TASK 53-41-00-991-098
R
EFF :
ALL 53-41-00
Page C690
Feb 01/08
IAC
(2) Apply STORAGE PRESERVATION (Material No. 15-007) or STORAGE
PRESERVATION (Material No. 15-008) or equivalent to the cabin floor
structure (Ref. TASK 51-75-13-916-002).
Subtask 53-41-00-410-168
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Install the applicable floor panels between FR66 to FR68 (Ref. TASK
53-42-12-400-002).
(6) If necessary, install the cabin attendant seat(s) (Ref. TASK 25-22-
41-400-001) (Ref. TASK 25-22-42-400-001).
R
EFF :
ALL 53-41-00
Page C691
Feb 01/08
IAC
**ON A/C 101-199, 901-999,
TASK 53-41-00-210-836
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
R
R Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
EFF :
101-199, 901-999, 53-41-00
Page C692
May 01/08
IAC
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
101-199, 901-999, 53-41-00
Page C693
Feb 01/08
R
IAC
**ON A/C 101-199, 901-999,
3. __________
Job Set-up
Subtask 53-41-00-010-173-A
A. Get Access
(2) Put the WARNING NOTICE on the flap/slat control lever to tell persons
not to operate the flap/slats.
(4) Remove the belly-fairing access panels 198GB (Ref. TASK 53-35-13-000-
001) and 198KB (Ref. TASK 53-35-13-000-002).
Subtask 53-41-00-010-173
A. Get Access
(2) Put the WARNING NOTICE on the flap/slat control lever to tell persons
not to operate the flap/slats.
(4) Remove the belly-fairing access panels 198MB (Ref. TASK 53-35-13-000-
001) and 198BB (Ref. TASK 53-35-13-000-002).
R
EFF :
101-199, 901-999, 53-41-00
Page C694
Feb 01/08
IAC
**ON A/C 101-199, 901-999,
Subtask 53-41-00-110-122
B. Cleaning
(1) Clean the inspection area with the CLEANING AGENTS (Material No. 11-
026) and a clean lint-free cloth MISCELLANEOUS (Material No. 19-003).
4. Procedure
_________
Subtask 53-41-00-210-137-A
A. Inspection
(3) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for the
correct repair procedure.
R
EFF :
101-199, 901-999, 53-41-00
Page C695
Feb 01/08
IAC
Inspection Area of the Longitudinal Butt Joint at STGR30, RH between FR47 and
FR64
Figure 668/TASK 53-41-00-991-097-A
EFF :
101-199,
53-41-00 Page C696
Feb 01/08
IAC
Inspection Area of the Longitudinal Butt Joint at STGR30, RH between FR47/51
and Fr64
Figure 668A/TASK 53-41-00-991-097
EFF :
901-999,
53-41-00 Page C697
Feb 01/08
IAC
**ON A/C 901-999,
Subtask 53-41-00-210-137
A. Inspection
(3) If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for the
correct repair procedure.
5. Close-up
________
Subtask 53-41-00-410-169-A
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the belly-fairing access panels 198GB (Ref. TASK 53-35-13-
400-001) and 198KB (Ref. TASK 53-35-13-400-002).
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
101-199, 901-999, 53-41-00
Page C698
Feb 01/08
IAC
**ON A/C 901-999,
Subtask 53-41-00-410-169
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the belly-fairing access panels 198MB (Ref. TASK 53-35-13-
400-001) and 198BB (Ref. TASK 53-35-13-400-002).
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
901-999, 53-41-00
Page C699
Feb 01/08
IAC
Keel Beam Bottom Panel at the FR46/STGR37 Intersection, LH/RH
Figure 669/TASK 53-41-00-991-091
EFF :
001-012, 014-019, 53-41-00
Page D600
Feb 01/08
IAC
MAIN STRUCTURE - CLEANING/PAINTING
__________________________________
TASK 53-41-00-916-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page 701
May 01/06
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-117
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(2) Put the warning notice on the slat/flap control lever to tell persons
not to operate the slats/flaps.
Subtask 53-41-00-110-079
B. Cleaning Procedure
EFF :
ALL 53-41-00
Page 702
May 01/06
IAC
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Remove the old temporary protection compound from the area to be
treated with a non metallic scraper, and clean with CLEANING AGENTS
(Material No. 11-004) and a lint free cloth. Make sure that the area
is dry before you continue.
4. Procedure
_________
Subtask 53-41-00-916-069
EFF :
ALL 53-41-00
Page 703
May 01/06
IAC
R Fuselage External Surface, contained in the Belly Fairing, and Belly Fairing
Support Structure zone 190
Figure 701/TASK 53-41-00-991-034
EFF :
ALL
53-41-00 Page 704
Nov 01/96
IAC
R **ON A/C 101-199,
R Subtask 53-41-00-916-069-B
Subtask 53-41-00-916-069-A
5. Close-up
________
Subtask 53-41-00-410-114
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-41-00
Page 705
Feb 01/07
IAC
(4) Remove the warning notice(s).
(6) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page 706
Feb 01/07
R
IAC
R **ON A/C 101-199,
R TASK 53-41-00-916-002
R 1. __________________
Reason for the Job
R Self Explanatory
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R
EFF :
101-199, 53-41-00
Page 707
Feb 01/07
IAC
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R 3. __________
Job Set-up
R Subtask 53-41-00-010-118
R A. Get Access
R (1) Put the access platform adjacent to the BULK cargo compartment door.
R (2) Open the BULK cargo compartment door (Ref. TASK 52-30-00-860-006).
R Subtask 53-41-00-110-080
R B. Cleaning Procedure
R WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
R AREA WHEN YOU USE SPECIAL MATERIALS.
R IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
R OR IN YOUR EYES :
R -FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
R MINUTES.
R -GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
R DO NOT BREATHE THE FUMES FROM THE MATERIAL.
R DO NOT SMOKE WHEN YOU USE THE MATERIAL.
R DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
R HEAT.
R THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
R AND SKIN IRRITANTS.
R (1) Remove the old temporary protection compound from the area to be
R treated with a non metallic scraper, and clean with CLEANING AGENTS
R (Material No. 11-004) and a lint free cloth. Make sure that the area
R is dry before you continue.
R
EFF :
101-199, 53-41-00
Page 708
Feb 01/07
IAC
R 4. Procedure
_________
R Subtask 53-41-00-916-070
R 5. Close-up
________
R Subtask 53-41-00-410-115
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Close the BULK cargo compartment door (Ref. TASK 52-30-00-860-008).
R (4) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
R
EFF :
101-199, 53-41-00
Page 709
Feb 01/07
IAC
R Sealing Profile of Bulk Cargo Cutout at Upper Corners.
R Figure 702/TASK 53-41-00-991-035
R
EFF :
101-199, 53-41-00
Page 710
Feb 01/07
IAC
R **ON A/C ALL
TASK 53-41-00-916-003
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page 711
Feb 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-861-050
Subtask 53-41-00-010-119
B. Get Access
(1) Remove the necessary equipment and furnishing to get access to the
cabin floor panels.
(2) Remove the necessary floor panels (Ref. TASK 53-32-12-000-002) and
(Ref. TASK 53-42-12-000-001).
Subtask 53-41-00-110-081
C. Cleaning Procedure
EFF :
ALL 53-41-00
Page 712
Feb 01/07
IAC
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Remove the old temporary protection compound from the area to be
treated with a non metallic scraper, and clean with CLEANING AGENTS
(Material No. 11-004) and a lint free cloth. Make sure that the area
is dry before you continue.
4. Procedure
_________
Subtask 53-41-00-916-071
EFF :
ALL 53-41-00
Page 713
Feb 01/07
IAC
Cabin Floor Structure, FR47 to FR70.
R Figure 703/TASK 53-41-00-991-036
EFF :
ALL 53-41-00
Page 714
Feb 01/07
IAC
R **ON A/C 901-999,
Subtask 53-41-00-916-071-A
5. Close-up
________
Subtask 53-41-00-410-116
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the floor panels (Ref. TASK 53-32-12-400-002) and (Ref. TASK
53-42-12-400-001).
(3) Install the equipment and furnishing, removed to get access to the
cabin floor panels.
Subtask 53-41-00-862-050
EFF :
ALL 53-41-00
Page 715
Feb 01/07
IAC
TASK 53-41-00-916-004
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-41-00
Page 716
Feb 01/07
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-41-00-010-120
A. Get Access
(1) Open the AFT cargo compartment door (Ref. TASK 52-30-00-860-001).
(2) Put the access platform adjacent to the AFT cargo compartment door.
Subtask 53-41-00-110-082
B. Cleaning Procedure
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
EFF :
ALL 53-41-00
Page 717
Feb 01/07
IAC
(1) Remove the old temporary protection compound from the area to be
treated with a non metallic scraper, and clean with CLEANING AGENTS
(Material No. 11-004) and a lint free cloth. Make sure that the area
is dry before you continue.
4. Procedure
_________
Subtask 53-41-00-916-072
Subtask 53-41-00-916-072-A
EFF :
ALL 53-41-00
Page 718
Feb 01/07
IAC
Aft Cargo Door Cutout, Visible Part of Lateral FR52A and FR56.
R Figure 704/TASK 53-41-00-991-037
EFF :
ALL 53-41-00
Page 719
Feb 01/07
IAC
**ON A/C ALL
5. Close-up
________
Subtask 53-41-00-410-117
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Close the Aft cargo compartment door (Ref. TASK 52-30-00-860-002).
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-41-00
Page 720
Feb 01/07
IAC
FLOOR PANELS - DESCRIPTION AND OPERATION
________________________________________
1. General
_______
2. Component
__________________
Location
R (Ref. Fig. 001)
EFF :
ALL 53-42-00
Page 1
Nov 01/04
IAC
Floor Panels - Component Location
Figure 001
EFF :
ALL 53-42-00
Page 2
Feb 01/96
IAC
PANELS - CABIN FLOOR - REMOVAL/INSTALLATION
___________________________________________
TASK 53-42-12-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-42-12
Page 401
Nov 01/07
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-42-12-010-050
A. Get access:
(3) Remove the textile floor covering, as necessary (Ref. TASK 25-28-41-
000-001).
(4) Remove the nontextile floor covering, as necessary (Ref. TASK 25-28-
42-000-001).
4. Procedure
_________
EFF :
ALL 53-42-12
Page 402
Nov 01/07
IAC
Cabin Floor Panel Installation - FR47 thru FR64
Figure 401/TASK 53-42-12-991-001
R
EFF :
001-012, 014-099, 53-42-12
Page 403
May 01/06
IAC
R Cabin Floor Panel Installation - FR47 thru FR64
R Figure 401A/TASK 53-42-12-991-001-C
EFF :
101-199, 53-42-12
Page 404
Nov 01/07
IAC
Cabin Floor Panel Installation - FR47/51 thru FR64
Figure 401B/TASK 53-42-12-991-001-A
R
EFF :
901-901, 53-42-12
Page 405
Nov 01/07
IAC
R Cabin Floor Panel Installation - FR47/51 thru FR64
R Figure 401C/TASK 53-42-12-991-001-D
R
EFF :
902-999, 53-42-12
Page 406
Nov 01/07
IAC
R **ON A/C 001-012, 014-099, 901-901,
Subtask 53-42-12-020-050
(1) Pull the cord (1) up to remove the sealant from between the floor
panel joints.
NOTE : Identify the floor panels. This will help with the
____
installation.
R Subtask 53-42-12-020-050-A
R (1) Pull the cord (4) up, to remove the sealant from between the floor
R panel joints.
R NOTE : Identify the floor panels (1). This will help with the
____
R installation procedure.
EFF :
ALL 53-42-12
Page 407
Nov 01/07
IAC
**ON A/C ALL
TASK 53-42-12-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-42-12
Page 408
Feb 01/08
IAC
R C. Expendable Parts
R -------------------------------------------------------------------------------
R FIG.ITEM |DESIGNATION |IPC-CSN
R -------------------------------------------------------------------------------
R D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-42-12
Page 409
Nov 01/07
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-42-12-860-050
(1) Make sure that the passenger seats are removed in the area as
necessary (Ref. TASK 25-21-41-000-001).
(2) Make sure that the partitions are removed (Ref. TASK 25-26-42-000-
001).
(3) Make sure that the textile floor covering is removed as necessary
(Ref. TASK 25-28-41-000-001).
(4) Make sure that the nontextile floor covering is removed as necessary
(Ref. TASK 25-28-42-000-001).
4. Procedure
_________
EFF :
ALL 53-42-12
Page 410
Nov 01/07
IAC
R **ON A/C 001-012, 014-099, 901-901,
Subtask 53-42-12-160-051
(1) Remove any old sealant from the floor panels with a nonmetallic
scraper.
(2) Clean the component interface and the adjacent area with CLEANING
AGENTS (Material No. 11-003) and lint free cloth.
(3) Make sure that the parts retained from the removed component are
clean and in the correct condition.
Subtask 53-42-12-420-050
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
001-012, 014-099, 901-901, 53-42-12
Page 411
Nov 01/07
IAC
(3) Apply the SPECIAL MATERIALS (Material No. 05-002) to the screws (3).
(4) Install the screws (3) and TORQUE to 0.42 m.daN (37.16 lbf.in).
(5) Install the cord (1) MISCELLANEOUS (Material No. 19-027) in the gap
between the floor panels.
NOTE : Make a loop at the end of the cord, this will help the next
____
removal procedure.
(6) Apply the SEALANTS (Material No. 09-016) in the gap between the floor
panels.
R Subtask 53-42-12-160-051-A
R (1) Remove the used sealant from the floor panels (1) with a SCRAPER -
R NON METALLIC.
R (a) Clean the component interface and the adjacent area with the
R CLEANING AGENTS (Material No. 11-026) and a clean lint-free
R cotton cloth MISCELLANEOUS (Material No. 19-003).
R (3) Make sure that the parts retained from the removed component are
R clean and in the correct condition.
R (5) Make sure that the clipnuts (5) are clean and in the correct
R condition. If necessary, replace the defective clipnuts (5).
R (6) Make sure that the self-adhesive foam tapes (3) are in the correct
R condition. If necessary:
R (b) Clean the surfaces of the self-adhesive foam tapes (3) with the
R CLEANING AGENTS (Material No. 11-026) and a lint-free cotton
R cloth MISCELLANEOUS (Material No. 19-003).
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R Subtask 53-42-12-420-050-A
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (3) Apply the zinc chromate putty SPECIAL MATERIALS (Material No. 05-002)
R to the screws (2).
R (4) Install the screws (2) and TORQUE to 0.42 m.daN (37.16 lbf.in).
R (5) Install the cord (4) MISCELLANEOUS (Material No. 19-027) in the
R clearance between the floor panels (1). Make a loop at the end of the
R cord. This will help with the subsequent removal procedure.
R (6) Apply the SEALANTS (Material No. 09-016) in the space between the
R floor panels (1).
5. Close-up
________
Subtask 53-42-12-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the nontextile floor covering, if removed (Ref. TASK 25-28-
42-400-001).
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(7) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
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Page 414
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TASK 53-42-12-000-002
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 415
May 01/08
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-42-12-010-051
A. Get access:
(1) Remove the AFT galley (Ref. TASK 25-33-41-000-001) and/or (Ref. TASK
25-33-41-000-002).
(2) Remove the lavatory (Ref. TASK 25-43-41-000-001) and/or (Ref. TASK
25-43-42-000-001) and/or (Ref. TASK 25-43-43-000-001).
(4) Remove the nontextile floor covering, as necessary (Ref. TASK 25-28-
42-000-001).
(5) Remove the textile floor covering, as necessary (Ref. TASK 25-28-41-
000-001).
4. Procedure
_________
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Typical Cabin Floor Panel Installation - FR64 thru FR70
Figure 402/TASK 53-42-12-991-003
R
EFF :
001-012, 014-099, 53-42-12
Page 417
Nov 01/07
IAC
R Cabin Floor Panels FR64 thru FR70
R Figure 402A/TASK 53-42-12-991-003-E
R
EFF :
101-199, 53-42-12
Page 418
Nov 01/07
IAC
R Cabin Floor Panels FR64 thru FR70
R Figure 402B/TASK 53-42-12-991-003-B
R
EFF :
901-901, 53-42-12
Page 419
May 01/08
IAC
Cabin Floor Panels FR64 thru FR70
R Figure 402C/TASK 53-42-12-991-003-D
R
EFF :
902-999, 53-42-12
Page 420
May 01/08
IAC
**ON A/C 001-012, 014-099, 901-901,
Subtask 53-42-12-020-052
(1) If you must remove the floor panels adjacent the door-threshold floor
panels, you must do this:
(2) Pull the cord (1) up to remove the sealant from between the floor
panels.
NOTE : Identify the floor panels. This will help with the
____
installation.
(a) Pull the cord (1) up to remove the sealant from between the
door-threshold floor panels and the door sills.
Subtask 53-42-12-020-052-A
(1) If you must remove the floor panels adjacent to the door-threshold
floor panels (6), do the steps that follow:
R
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Page 421
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(2) Pull the cord (4) up, to remove the sealant from between the floor
panels (1).
NOTE : Identify the floor panels (1). This will help with the
____
installation procedure.
(a) Pull the cord (4) up, to remove the sealant from between the
door-threshold floor panels (6) and the door sills.
R
EFF :
101-199, 902-999, 53-42-12
Page 422
May 01/08
IAC
**ON A/C ALL
TASK 53-42-12-400-002
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 423
May 01/08
R
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C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 424
May 01/08
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**ON A/C ALL
3. __________
Job Set-up
Subtask 53-42-12-860-051
(1) Make sure that the AFT galley is removed (Ref. TASK 25-33-41-000-001)
and/or (Ref. TASK 25-33-41-000-002).
(2) Make sure that the lavatory is removed (Ref. TASK 25-43-41-000-001)
and/or (Ref. TASK 25-43-42-000-001) and/or (Ref. TASK 25-43-43-000-
001).
(3) Make sure that the passenger seats are removed in the area as
necessary (Ref. TASK 25-21-41-000-001).
(4) Make sure that the textile floor covering is removed as necessary
(Ref. TASK 25-28-41-000-001).
(5) Make sure that the nontextile floor covering is removed as necessary
(Ref. TASK 25-28-42-000-001).
4. Procedure
_________
R
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**ON A/C 001-012, 014-099,
Subtask 53-42-12-160-050
(1) Remove any old sealant from the floor panels with a nonmetallic
scraper.
(2) Clean the component interface and the adjacent area with CLEANING
AGENTS (Material No. 11-026) and a lint free cloth.
(3) Make sure that the parts retained from the removed component are
clean and in the correct condition.
Subtask 53-42-12-160-050-B
(1) Remove the used sealant from the floor panels with a SCRAPER - NON
METALLIC.
(2) Clean the component interface and the adjacent area with the CLEANING
AGENTS (Material No. 11-026) and a lint-free cotton cloth
MISCELLANEOUS (Material No. 19-003).
(3) Make sure that the parts retained from the removed component are
clean and in the correct condition.
(5) Make sure that the clipnuts (5) are clean and in the correct
condition. If necessary, replace the defective clipnuts.
(6) Make sure that the self-adhesive foam tapes (3) are in the correct
condition. If necessary:
R
EFF :
001-012, 014-099, 101-199, 902-999, 53-42-12
Page 426
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(b) Clean the surfaces of the self-adhesive foam tapes (3) with the
CLEANING AGENTS (Material No. 11-026) and a lint-free cotton
cloth MISCELLANEOUS (Material No. 19-003).
(c) Install the new self-adhesive foam tapes BONDING AND ADHESIVE
COMPOUNDS (Material No. 08-005B) (3).
Subtask 53-42-12-160-050-A
(1) Remove the used sealant from the floor panels with a SCRAPER - NON
METALLIC.
(a) Clean the component interface and the adjacent area with the
CLEANING AGENTS (Material No. 11-026) and a lint-free cotton
cloth, MISCELLANEOUS (Material No. 19-003).
(3) Make sure that the parts retained from the removed component are
clean and in the correct condition.
(5) Make sure that the self-adhesive foam tapes (2) are in the correct
condition. If necessary:
1
_ Clean the contact surfaces of the self-adhesive foam tapes (2)
with the CLEANING AGENTS (Material No. 11-026) and a lint-free
cotton cloth, MISCELLANEOUS (Material No. 19-003).
(c) Install the new self-adhesive foam tapes BONDING AND ADHESIVE
COMPOUNDS (Material No. 08-005B) (2).
R
EFF :
101-199, 901-999, 53-42-12
Page 427
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IAC
**ON A/C 001-012, 014-099, 901-901,
Subtask 53-42-12-420-051
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Apply the SPECIAL MATERIALS (Material No. 05-002) to the screws (3).
(4) Install the screws (3) and TORQUE to 0.42 m.daN (37.16 lbf.in).
(5) Install the cord (1) MISCELLANEOUS (Material No. 19-027) in the gap
between the floor panels.
NOTE : Make a loop at the end of the cord, this will help the next
____
removal procedure.
(6) Apply the SEALANTS (Material No. 09-016) in the gap between the floor
panels.
Subtask 53-42-12-420-051-A
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Apply the zinc chromate putty SPECIAL MATERIALS (Material No. 05-002)
to the screws (2).
(4) Install the screws (2) and TORQUE to 0.42 m.daN (37.16 lbf.in).
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(5) Install the cord (4) MISCELLANEOUS (Material No. 19-027) in the
spaces between the floor panels (1). Make a loop at the end of the
cord. This will help with the subsequent removal procedure.
(8) If neccessary, install the inner cover-plate (7) and the screws (8)
and (9).
(9) Apply the SEALANTS (Material No. 09-016) in the spaces between the
floor panels (1) and between the door-threshold floor panels (6).
5. Close-up
________
Subtask 53-42-12-410-052
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the lavatory (Ref. TASK 25-43-41-400-001) and/or (Ref. TASK
25-43-42-400-001) and/or (Ref. TASK 25-43-43-400-001).
(4) Install the galley (Ref. TASK 25-33-41-400-001) and/or (Ref. TASK 25-
33-41-400-002).
(7) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
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FLOOR PANELS - AFT CARGO COMPARTMENT ZONE 150 - REMOVAL/INSTALLATION
____________________________________________________________________
TASK 53-42-14-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 401
Feb 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-42-14-861-050
Subtask 53-42-14-010-050
B. Get Access
(1) Open the AFT cargo compartment door (Ref. TASK 52-30-00-860-001).
(2) Put the access platform in position adjacent to the AFT cargo
compartment door.
(3) Set the AFT CARGO COMPT light switch 8LU to ON.
4. Procedure
_________
Subtask 53-42-14-020-050
(2) Pull the cord (7) up to remove the sealant from between the floor
panels (1).
(3) Remove the sealant from between the cutouts and the tiedown positions
with a non metallic scraper.
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R AFT Cargo Compartment Floor Panels - Zone 150
Figure 401/TASK 53-42-14-991-001
EFF :
001-012, 014-019, 53-42-14
Page 403
May 01/97
IAC
(4) Remove the screws (2), and if installed the washers (8) and nuts (9).
NOTE : Identify the length of the screws (2), and if installed the
____
position of the washers (8) and the nuts (9). This will help
with the installation procedure.
(5) Remove the floor panels (1) and the section hoses (3), (4), (5) and
(6).
NOTE : Identify the floor panels (1) and the section hoses (3), (4),
____
(5) and (6). This will help with the installation procedure.
Subtask 53-42-14-020-050-A
(2) Pull the cord (7) up to remove the sealant from between the floor
panels (1).
(3) Remove the sealant from between the cutouts and the tiedown positions
with a non metallic scraper.
EFF :
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Page 404
Feb 01/07
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R AFT Cargo Compartment Floor Panels - Zone 150
R Figure 401A/TASK 53-42-14-991-001-D
EFF :
020-099, 53-42-14
Page 405
Feb 01/07
IAC
AFT Cargo Compartment Floor Panels - Zone 150
R Figure 401B/TASK 53-42-14-991-001-B
EFF :
101-199, 53-42-14
Page 406
Feb 01/07
IAC
AFT Cargo Compartment Floor Panels - Zone 150
R Figure 401C/TASK 53-42-14-991-001-C
R
EFF :
901-999, 53-42-14
Page 407
Feb 01/07
IAC
(4) Remove the screws (2), and if installed the washers (8) and the nuts
(9).
NOTE : Identify the length of the screws (2), and if installed the
____
position of the washers (8) and the nuts (9). This will help
with the installation procedure.
(5) Remove the floor panels (1) and the section hoses (3) and (6).
NOTE : Identify the floor panels (1) and the section hoses (3) and
____
(6). This will help with the installation procedure.
R
EFF :
020-099, 101-199, 901-999, 53-42-14
Page 408
Feb 01/07
IAC
**ON A/C ALL
TASK 53-42-14-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 409
Feb 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-42-14-860-050
(1) Make sure that the AFT cargo compartment door is opened (Ref. TASK
52-30-00-860-001).
(2) Make sure that the access platform is in position adjacent to the AFT
cargo compartment door.
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(3) Make sure that the AFT CARGO COMPT light switch 8LU is set to ON.
Subtask 53-42-14-110-052
B. Cleaning Procedure
(1) Remove the old sealant from the floor panels with a non metallic
scraper.
(2) Clean the component interface and the adjacent area with CLEANING
AGENTS (Material No. 11-026) and a lint free cloth. Make sure that
the area is dry before you continue.
4. Procedure
_________
Subtask 53-42-14-420-050
R (3) Make sure that the parts retained from the removed component are
clean and in the correct condition.
R (4) Put the floor panels (1) and the section hoses (3) thru (6) in
R position.
R (5) Apply the SEALANTS (Material No. 09-005) in the holes at the end of
each seal.
R (6) Make sure that all the seal intersections are flush with each other.
R (7) Apply the zinc chromate putty SPECIAL MATERIALS (Material No. 05-002)
to the screws (2).
R (8) Install the screws (2) and, if removed, the washers (8) and the nuts
(9).
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R (9) TORQUE the screws (2) to 0.42 m.daN (37.16 lbf.in).
R (10) Position the cord (7) FIBER GLASS CORD 1.1MM DIA. (DAN107-1) in the
spaces between the floor panels (1).
R (11) Make sure that the cord (7) comes out at both ends:
- Approximately 100.0 mm (3.9370 in.) between the sloped floor panels
(1)
- Approximately 200.0 mm (7.8740 in.) between the flat floor panels
(1).
R (12) Apply the SEALANTS (Material No. 09-005) in the spaces between the
floor panels (1) and the cutouts of the tiedown positions.
R (13) Make a loop of the cord ends (7) and press into the sealant. This
will help with the subsequent removal procedure.
Subtask 53-42-14-420-050-A
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R (3) Make sure that the parts retained from the removed component are
clean and in the correct condition.
R (4) Put the floor panels (1) and the section hoses (3) and (6) in
position.
R (5) Apply the SEALANTS (Material No. 09-005) in the holes at the end of
each seal.
R (6) Make sure that all the seal intersections are flush with each other.
R (7) Apply the zinc chromate putty SPECIAL MATERIALS (Material No. 05-002)
to the screws (2).
R (8) Install the screws (2) and, if removed, the washers (8) and the nuts
(9).
R (10) Position the cord (7) FIBER GLASS CORD 1.1MM DIA. (DAN107-1) in the
spaces between the floor panels (1).
R (11) Make sure that the cord (7) comes out at both ends:
- Approximately 100.0 mm (3.9370 in.) between the sloped floor panels
(1)
- Approximately 200.0 mm (7.8740 in.) between the flat floor panels
(1).
R (12) Apply the SEALANTS (Material No. 09-005) in the spaces between the
floor panels (1) and the cutouts of the tiedown positions.
R (13) Make a loop of the cord ends (7) and press into the sealant. This
will help with the subsequent removal procedure.
EFF :
020-099, 101-199, 901-999, 53-42-14
Page 413
Nov 01/07
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**ON A/C ALL
5. Close-up
________
Subtask 53-42-14-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Set the AFT CARGO COMPT light switch 8LU to OFF.
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
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May 01/07
R
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FLOOR PANELS - AFT CARGO COMPARTMENT ZONE 160 - REMOVAL/INSTALLATION
____________________________________________________________________
TASK 53-42-17-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 401
Feb 01/07
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-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-42-17-010-050
A. Get Access
(2) Put the access platform in position below the AFT cargo-compartment
door.
R Subtask 53-42-17-010-050-A
R A. Get Access
R (1) Put the access platform in position below the BULK cargo-compartment
R door.
4. Procedure
_________
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Page 402
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BULK Cargo-Compartment Floor-Panels Zone 160
Figure 401/TASK 53-42-17-991-001
EFF :
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Page 403
Feb 01/96
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**ON A/C 020-099,
Subtask 53-42-17-020-051
(2) Pull the cord up to remove the sealant from between the floor panels
(1).
(3) Remove the sealant from between the cutouts and the tiedown positions
with a nonmetal scraper.
(5) Remove the floor panels (1) and the seals (3), (4), (5) and (6).
Subtask 53-42-17-020-051-A
(2) Pull the cord up to remove the sealant from between the floor panels
(1).
R
EFF :
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Page 404
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BULK Cargo-Compartment Floor-Panels Zone 160
Figure 401A/TASK 53-42-17-991-001-A
R
EFF :
020-099, 53-42-17
Page 405
Feb 01/07
IAC
R BULK Cargo-Compartment Floor-Panels Zone 160
R Figure 401B/TASK 53-42-17-991-001-C
R
EFF :
101-199, 53-42-17
Page 406
Feb 01/07
IAC
BULK Cargo-Compartment Floor-Panels Zone 160
R Figure 401C/TASK 53-42-17-991-001-B
R
EFF :
901-999, 53-42-17
Page 407
Feb 01/07
IAC
(3) Remove the sealant from between the cutouts and the tiedown positions
with a nonmetal scraper.
(5) Remove the floor panels (1) and the seals (3) and (6).
R Subtask 53-42-17-020-051-B
R (1) Remove the screws (8) and (11), the washers (9) and (10) and the
R panel (12).
R (3) Pull the cord up to remove the sealant from between the floor panels
R (1).
R (4) Remove the sealant from between the cutouts and the tiedown positions
R with a nonmetal scraper.
R (6) Remove the floor panels (1) and the seals (3) and (7).
R
EFF :
020-099, 101-199, 901-999, 53-42-17
Page 408
Feb 01/07
IAC
**ON A/C ALL
TASK 53-42-17-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-42-17
Page 409
Feb 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-42-17-860-050
(1) Make sure that the aircraft is in the same configuration as for the
removal task.
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4. Procedure
_________
Subtask 53-42-17-916-050
R (1) Remove the used sealant from the floor panels with a SCRAPER - NON
R METALLIC.
R (2) Clean the component interface and the adjacent area with the CLEANING
R AGENTS (Material No. 11-026) and a clean lint-free cloth
R MISCELLANEOUS (Material No. 19-003).
(3) Make sure that the parts retained from the removed component are
clean and in the correct condition.
EFF :
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Page 411
Nov 01/07
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**ON A/C 001-012, 014-019,
Subtask 53-42-17-420-050
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Put the floor panels (1) and the seals (3), (4), (5) and (6) in
position.
(3) Apply the SEALANTS (Material No. 09-005) in the holes at the end of
each seal.
(4) Make sure that all the seal intersections are flush with each other.
(5) Apply the zinc chromate putty SPECIAL MATERIALS (Material No. 05-002)
to the screws (2).
(6) Install the screws (2) and TORQUE to 0.42 m.daN (37.16 lbf.in).
(7) Install the cord (7) FIBER GLASS CORD 1.1MM DIA. (DAN107-1) in the
spaces between the floor panels (1).
(8) Make a loop at the end of the cord. This will help with the
subsequent removal procedure.
(9) Apply the SEALANTS (Material No. 09-005) in the spaces between the
floor panels (1) and the cutouts of the tiedown positions.
Subtask 53-42-17-420-050-A
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Put the floor panels (1) and the seals (3) and (6) in position.
(3) Apply the SEALANTS (Material No. 09-005) in the holes at the end of
each seal.
EFF :
001-012, 014-099, 901-999, 53-42-17
Page 412
Nov 01/07
R
IAC
R (4) Make sure that all the seal intersections are flush with each other.
R (5) Apply the zinc chromate putty SPECIAL MATERIALS (Material No. 05-002)
R to the screws (2).
R (6) Install the screws (2) and TORQUE to 0.42 m.daN (37.16 lbf.in).
R (7) Install the cord (7) FIBER GLASS CORD 1.1MM DIA. (DAN107-1) in the
R spaces between the floor panels (1).
R
R (8) Make a loop at the end of the cord. This will help with the
R subsequent removal procedure.
R (9) Apply the SEALANTS (Material No. 09-005) in the spaces between the
R floor panels (1) and the cutouts of the tiedown positions.
Subtask 53-42-17-420-050-B
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Put the floor panels (1) and the seals (3) and (7) in position.
R (3) Apply the SEALANTS (Material No. 09-005) in the holes at the end of
R each seal.
R (4) Make sure that all the seal intersections are flush with each other.
R (5) Apply the zinc chromate putty SPECIAL MATERIALS (Material No. 05-002)
R to the screws (2), (8) and (11).
R (6) Install the screws (2) and TORQUE to 0.42 m.daN (37.16 lbf.in).
R (7) Install the cord (4) FIBER GLASS CORD 1.1MM DIA. (DAN107-1) in the
R spaces between the floor panels (1).
R
R (8) Make a loop at the end of the cord. This will help with the
R subsequent removal procedure.
EFF :
020-099, 101-199, 901-999, 53-42-17
Page 413
May 01/07
IAC
R (9) Apply the SEALANTS (Material No. 09-005) in the spaces between the
R floor panels (1) and the cutouts of the tiedown positions.
R (10) Put the panel (12) in position and install and tighten the screws (8)
and (11) and the washers (9) and (10).
R (11) Apply the SEALANTS (Material No. 09-005) around the edges of the
R panel (12).
5. Close-up
________
Subtask 53-42-17-410-052
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 53-42-17-410-052-A
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-42-17
Page 414
May 01/07
IAC
SUPPORT STRUTS - DESCRIPTION AND OPERATION
__________________________________________
1. _______
General
Support struts are made of extruded aluminum (or composite material). The
support struts of the cabin floor structure have a H-Cross-section profile.
They are installed in the different underfloor compartments and sections to
make the floor structure stronger. The sidewall panels of the cargo
compartments are attached to the support struts.
2. __________________
Component Location
3. Description
___________
(1) The support struts under the cabin floor structure are generally
riveted to the cross-beams and to the frames. The support struts in
the cargo compartments make a lateral channel left and right of the
cargo compartments sidewall. In the left-hand channel different
aircraft systems are installed.
(2) To get access to the different aircraft systems (for removal and
installation) some of the support struts are removable. The removable
struts in the aft cargo compartments are installed at, frame 50/51,
56/57, 61/62 and the center support strut at frame 65.
EFF :
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Page 1
Feb 01/07
IAC
Support Struts - Location
Figure 001
R
EFF :
001-012, 014-099, 101-199, 53-43-00
Page 2
Feb 01/07
IAC
Support Struts - Location
Figure 001A
R
EFF :
901-999, 53-43-00
Page 3
Feb 01/07
IAC
STRUTS - REMOVAL/INSTALLATION
_____________________________
TASK 53-43-11-000-001
NOTE : Applicable to FR50 and FR51, FR56 and FR57, FR61 and FR62 left side and
____
the partition center support strut at FR65.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 401
Feb 01/07
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-43-11-010-050
A. Get Access
(4) Remove the partition panels 161DW, 162DW at FR65 (Ref. TASK 25-55-12-
000-001).
(5) Remove the sealant from around the attach area of the support struts
(1) with a nonmetal scraper.
4. Procedure
_________
Subtask 53-43-11-020-051
(1) Remove all attach items from the support struts (1).
(2) Remove and discard the screws (3), the bolts (4), the nuts (5) and
the washers (6).
EFF :
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IAC
Removable Support Struts
Figure 401/TASK 53-43-11-991-001
R
EFF :
001-012, 014-099, 101-199, 53-43-11
Page 403
Feb 01/07
IAC
Removable Support Struts
Figure 401A/TASK 53-43-11-991-001-A
R
EFF :
901-999, 53-43-11
Page 404
Feb 01/07
IAC
(4) Remove the quick release pins (7) from the support struts (2).
EFF :
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Page 405
May 01/06
R
IAC
TASK 53-43-11-400-001
NOTE : Applicable to FR50 and FR51, FR56 and FR57, FR61 and FR62 left side and
____
the partition center support strut at FR65.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
A. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
B. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
EFF :
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R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-43-11-860-050
(1) Make sure that the aircraft is in the same configuration as for the
removal task.
(2) Clean the support struts (1) and the mating surfaces with CLEANING
AGENTS (Material No. 11-003).
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WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______
MATERIALS ONLY WITH A GOOD SUPPLY OF AIR.
OBEY THE MANUFACTURERS INSTRUCTIONS.
PUT ON PROTECTIVE CLOTHING.
DO NOT GET THEM IN YOUR MOUTH.
DO NOT SMOKE.
DO NOT BREATHE THE GAS.
THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT.
GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
(3) Make sure that the parts retained from the removed component are
clean and in the correct condition.
4. Procedure
_________
Subtask 53-43-11-916-050
(b) The threads of the screws (3) and the bolts (4).
EFF :
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Page 408
Feb 01/07
IAC
Subtask 53-43-11-420-050
(2) Install the new screws (3), the new bolts (4) and bolts (4), the new
nuts (5) and the new washers (6).
(5) Seal all the bolt heads, the nuts and the attachment area of the
support struts with SEALANTS (Material No. 09-005).
(6) Install any attach items removed from the support struts.
5. Close-up
________
Subtask 53-43-11-410-050
A. Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the partition panels 161DW, 162DW at FR65 (Ref. TASK 25-55-
12-400-001).
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-43-11
Page 409
May 01/06
IAC
FAIRINGS - DESCRIPTION AND OPERATION
____________________________________
1. _______
General
The dorsal fin 321AL is made of layers of glassfiber reinforced plastic over
a honeycomb core. It is installed at the leading edge of the vertical
stabilizer to fuselage joint. The dorsal fin helps the directional stability
of the aircraft. It also makes the air flow smoothly around the joint and
keeps turbulance to a minimum. The removal of the dorsal fin gives access to
the HF and VOR antenna connections.
2. Component
__________________
Location
(Ref. Fig. 001)
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Page 1
Feb 01/96
IAC
Dorsal Fin - Component Location
Figure 001
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Page 2
Feb 01/96
IAC
DORSAL FIN - REMOVAL/INSTALLATION
_________________________________
TASK 53-45-11-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 401
Feb 01/08
IAC
3. __________
Job Set-up
Subtask 53-45-11-865-050
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17
121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
Subtask 53-45-11-010-050
B. Get Access
R (1) Put the ACCESS PLATFORM 6M (20 FT) in position at Zone 321.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
R (2) Remove and discard the self-adhesive disc from the lift point (1).
R (3) Remove the lift lug (2) from the lift point (1).
R (4) Install the lift lug (2) in the lift point (1) with the eye-end out.
R (6) Attach the SLING - DORSAL FIN, LEADING EDGES, END CAP
R (98D55307531000) or the SLING - UNIVERSAL, TAIL PLAN (98A55308440000)
R to the lift lug (2).
EFF :
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Page 402
Feb 01/08
IAC
R Dorsal Fin 321AL.
Figure 401/TASK 53-45-11-991-001
EFF :
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Page 403
May 01/97
IAC
**ON A/C 020-099, 101-199, 901-999,
Subtask 53-45-11-010-050-A
B. Get Access
R (1) Put the ACCESS PLATFORM 6M (20 FT) in position at Zone 321.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
R (2) Remove and discard the self-adhesive disc from the lift point (1).
R (3) Remove and keep the plastic plug from the lift point (1).
R (4) Install the lift lug (2) in the lift point (1) with the eye-end out.
R (6) Attach the SLING - DORSAL FIN, LEADING EDGES, END CAP
R (98D55307531001) or the SLING - UNIVERSAL, TAIL PLAN (98A55308440000)
R to the lift lug (2).
4. Procedure
_________
Subtask 53-45-11-020-050
A. Removal:
(1) Remove the screws (3) from the dorsal fin (4).
(2) With the aid of the crane, carefully disengage and lift the dorsal
fin (4) from the aircraft.
EFF :
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IAC
(3) Lower the dorsal fin (4) on to a satisfactory support.
EFF :
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Nov 01/97
R
IAC
TASK 53-45-11-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 406
Feb 01/08
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-45-11-865-051
A. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17
121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
Subtask 53-45-11-869-050
(1) Make sure that the aircraft is in the same configuration as for the
removal task.
(2) Make sure that the warning notice is in position to tell persons not
to operate the flight controls.
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R
IAC
4. Procedure
_________
Subtask 53-45-11-914-050
(1) Remove the old sealant from the dorsal fin and the aircraft mating
surfaces with a SCRAPER - NON METALLIC.
(2) Clean the dorsal fin and aircraft mating surfaces with CLEANING
AGENTS (Material No. 11-003) and a lint-free cotton cloth
MISCELLANEOUS (Material No. 19-003).
(3) Apply SEALANTS (Material No. 09-018) to the dorsal fin and aircraft
mating surfaces (Ref. TASK 51-76-11-300-001).
Subtask 53-45-11-420-050
R B. Installation
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R (2) Attach the SLING - DORSAL FIN, LEADING EDGES, END CAP
R (98D55307531000) or the SLING - UNIVERSAL, TAIL PLAN (98A55308440000)
R to the crane and the lift lug (2).
EFF :
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Page 408
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IAC
(3) Lift the dorsal fin (4) with the CRANE HEIGHT 10 M (33 FT) and put it
in the installation position on the aircraft.
(4) Install the screws (3) and TORQUE to 0.3 m.daN (26.54 lbf.in).
(5) Make sure that the clearances at points a, b and c are as
follows:
R - Point a is 10.0 +3.5 -3.5 mm (0.3937 +0.1377 -0.1377 in.)
R - Point b is 1.0 +1.0 -1.0 mm (0.0393 +0.0393 -0.0393 in.)
R - Point c is 3.5 +0.5 -0.5 mm (0.1377 +0.0196 -0.0196 in.).
R (7) Remove the lift lug (2) from the lift point (1). Apply the zinc
R chromate putty SPECIAL MATERIALS (Material No. 05-002) to the lift
R lug threads.
R (8) Install the lift lug (2) in the lift point (1) with its eye-end
R inboard.
R
R (9) Install a new self-adhesive PVC disk SPECIAL MATERIALS (Material No.
R 05-052) on the lift point (1).
R (10) Apply a bead of the SEALANTS (Material No. 09-016) along the joints
R of the dorsal fin (4) (Ref. TASK 51-76-11-300-001).
Subtask 53-45-11-420-050-A
R B. Installation
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R (2) Attach the SLING - DORSAL FIN, LEADING EDGES, END CAP
R (98D55307531001) or the SLING - UNIVERSAL, TAIL PLAN (98A55308440000)
R to the crane and the lift lug (2).
(3) Lift the dorsal fin (4) with the CRANE HEIGHT 10 M (33 FT) and put it
in the installation position on the aircraft.
(4) Install the screws (3) and TORQUE to 0.3 m.daN (26.54 lbf.in).
EFF :
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Page 409
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IAC
(5) Make sure that the clearances at points a, b and c are as
follows:
R - Point a is 10.0 +3.5 -3.5 mm (0.3937 +0.1377 -0.1377 in.)
R - Point b is 1.0 +1.0 -1.0 mm (0.0393 +0.0393 -0.0393 in.)
R - Point c is 3.5 +0.5 -0.5 mm (0.1377 +0.0196 -0.0196 in.).
R (7) Remove the lift lug (2) from the lift point (1).
R (9) Install a new self-adhesive PVC disk SPECIAL MATERIALS (Material No.
R 05-052) on the lift point (1).
R (10) Apply a bead of the SEALANTS (Material No. 09-016) along the joints
R of the dorsal fin (4) (Ref. TASK 51-76-11-300-001).
5. Close-up
________
Subtask 53-45-11-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the safety clip(s) and the tag(s) and close this(these)
circuit breaker(s):
19CE1, 19CE2, 19CE3, 15CE1, 15CE2, 16CE1, 16CE2
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-45-11
Page 410
Feb 01/08
IAC
SCUFF PLATES - DOOR ENTRANCE - REMOVAL/INSTALLATION
___________________________________________________
TASK 53-45-15-000-001
1. __________________
Reason for the Job
R
R Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-45-15-010-050
A. Get Access
(1) Put the access platform in position at the AFT passenger/crew door.
EFF :
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Page 401
May 01/06
IAC
4. Procedure
_________
Subtask 53-45-15-020-050
R NOTE : The scuff plates can become damaged during the subsequent removal
____
R procedure.
(2) Remove the sealant from around the scuff plate sections (3), (4) and
(5) with a nonmetallic scraper.
(3) Apply a hot air blower to the scuff plate sections (3), (4) and (5).
NOTE : Do not let the temperature of the scuff plates increase more
____
than 100 +50 -0 deg.C (212.00 +90.00 -0.00 deg.F).
CAUTION : MAKE SURE THAT YOU DO NOT DAMAGE THE FUSELAGE WHEN YOU
_______
REMOVE THE SCUFF PLATES.
(5) Remove the scuff plate sections (3), (4) and (5).
EFF :
ALL 53-45-15
Page 402
Nov 01/01
IAC
Scuff Plates of the AFT Passenger/Crew Doors
Figure 401/TASK 53-45-15-991-001
EFF :
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Page 403
Feb 01/96
IAC
TASK 53-45-15-400-001
1. __________________
Reason for the Job
R
R Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-45-15
Page 404
May 01/06
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-45-15-860-050
(1) Make sure that the aircraft is in the same configuration as for the
removal task.
4. Procedure
_________
Subtask 53-45-15-916-050
(1) Clean the mating surfaces of the scuff plate sections and the
fuselage skin with CLEANING AGENTS (Material No. 11-026) and a clean
lint-free cloth.
EFF :
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Page 405
Nov 01/07
IAC
Scuff Plates Attachment
Figure 402/TASK 53-45-15-991-002
EFF :
ALL 53-45-15
Page 406
Nov 01/07
R
IAC
Application of Sealant and Release Agent to the Scuff Plates
R Figure 403/TASK 53-45-15-991-006
EFF :
ALL 53-45-15
Page 407
Nov 01/07
IAC
(2) Make sure that the parts retained from the removed component are
clean and in the correct condition.
(4) Make sure that the scuff plate sections are in the correct condition
and are not damaged. If necessary, replace the damaged scuff plate
sections.
(5) Make sure that the scuff plate sections are correctly installed.
Subtask 53-45-15-420-050
(1) Apply the adhesive tape to the contour of the scuff plate sections on
the fuselage skin.
(2) Apply the adhesive tape approximately 15 mm (0.5905 in.) wide to the
inner edges of the scuff plate sections.
(4) Apply a layer of the release agent, SPECIAL MATERIALS (Material No.
05-013A) to the remaining inner areas of the scuff plate sections.
NOTE : The correct application of the release agent makes sure that
____
the scuff plate sections are not damaged during the subsequent
removal procedure.
(5) Apply a thin layer of the SEALANTS (Material No. 09-005) to the
mating area of the scuff plate sections at the fuselage skin
(Ref. TASK 51-76-11-300-001).
(6) Apply the SEALANTS (Material No. 09-005) to the screws (1) (Ref. TASK
51-76-11-300-001).
(7) If necessary, apply the SEALANTS (Material No. 09-005) to the inner
surface of the scuff plate sections.
(8) Remove the adhesive tape from the scuff plate sections.
(9) Put the scuff plate sections (3), (4) and (5) in position.
R
EFF :
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(10) Align the scuff plate sections and install and tighten the screws (1)
and the washers (2).
(11) Remove all unwanted sealant from around the scuff plates.
(13) Apply the SEALANTS (Material No. 09-030) (6) around and approximately
30 mm (1.1811 in.) from the edges of the scuff plates.
(14) Install a sheet of porous felt (7) over the scuff plates.
(15) Attach the porous felt (7) with the BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-065) to the scuff plates.
(16) Attach the vacuum valve (9) to the vacuum foil SPECIAL MATERIALS
(Material No. 05-068) (8).
(17) Put the vacuum foil SPECIAL MATERIALS (Material No. 05-068) (8) in
position on the scuff plates.
(18) Make sure that the vacuum foil SPECIAL MATERIALS (Material No. 05-
068) has an overlap of the seal tape by approximately 30 mm (1.1811
in.).
(19) Connect the VACUUM EQUIPMENT 0 TO 1 BAR (15 PSI) to the vacuum valve
(9).
(20) Operate the vacuum equipment and increase the vacuum around the scuff
plate to 0 bar (0.0000 psi).
(21) Operate the vacuum equipment for as long as necessary. Refer to the
environmental temperature shown in the table:
-------------------------------------------------------------------------------
TEMPERATURE TIME
-------------------------------------------------------------------------------
R
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(23) Remove the vacuum foil SPECIAL MATERIALS (Material No. 05-068) (8).
(24) Remove the vacuum valve (9) from the vacuum foil SPECIAL MATERIALS
(Material No. 05-068) (8).
(27) Clean the scuff plates and the adjacent area with the CLEANING AGENTS
(Material No. 11-026) and a clean lint-free cloth.
(28) Apply the SEALANTS (Material No. 09-005) around the edges of the
scuff plates and in the area of the door sill. Let the sealant dry
(Ref. TASK 51-76-11-300-001).
(29) Apply the STRUCTURE PAINTS (Material No. 16-021) to the sealant
around the door sill and to the sealant around the edges of the scuff
plates (Ref. TASK 51-75-12-300-003).
5. Close-up
________
Subtask 53-45-15-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-45-15
Page 410
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R
IAC
**ON A/C 101-199,
TASK 53-45-15-000-002
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-45-15-010-051
A. Get Access
(3) Remove the floor panel 162JF at the entrance to the BULK
cargo-compartment (Ref. TASK 53-42-17-000-001).
R
EFF :
101-199, 53-45-15
Page 411
Nov 01/07
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4. Procedure
_________
Subtask 53-45-15-020-051
NOTE : The scuff plates can become damaged during the subsequent removal
____
procedure.
(1) Remove the sealant from around the scuff plates with a nonmetallic
scraper.
(3) Apply a hot air blower to the scuff plate sections (1) and (4).
NOTE : Do not let the temperature of the scuff plates increase more
____
than 100 +50 -0 deg.C (212.00 +90.00 -0.00 deg.F).
(4) Loosen the scuff plate sections (1) and (4) with a nonmetallic wedge.
CAUTION : MAKE SURE THAT YOU DO NOT DAMAGE THE FUSELAGE WHEN YOU
_______
REMOVE THE SCUFF PLATES.
NOTE : You must install new scuff plates if the scuff plates you
____
remove were not installed with a release agent. (The release
agent provides for easier removal).
R
EFF :
101-199, 53-45-15
Page 412
Nov 01/07
IAC
Scuff Plate of the BULK Cargo-Compartment Door
R Figure 404/TASK 53-45-15-991-003
R
EFF :
101-199, 53-45-15
Page 413
Nov 01/07
IAC
TASK 53-45-15-400-002
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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Page 414
Nov 01/07
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IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-45-15-860-051
(1) Make sure that the aircraft is in the same configuration as for the
removal task.
4. Procedure
_________
Subtask 53-45-15-916-051
(1) Clean the scuff plate mating surface of the fuselage skin with
CLEANING AGENTS (Material No. 11-003).
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Scuff Plate Attachment
R Figure 405/TASK 53-45-15-991-004
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101-199, 53-45-15
Page 416
Nov 01/07
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Installation and Application of Sealant to the Scuff Plates
R Figure 406/TASK 53-45-15-991-005
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Page 417
Nov 01/07
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WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE
_______
SPECIAL MATERIAL.
THIS MATERIAL IS DANGEROUS.
(2) Make sure that the scuff plates are in the correct condition and are
not damaged. If necessary, replace the damaged scuff plates.
(3) Before you install new, or the removed scuff plates, you must treat
the scuff plates (1) and (4) as follows:
(a) Clean the mating surface of each plate with CLEANING AGENTS
(Material No. 11-003).
(b) Sand blast the inner areas of both scuff plate sections.
(c) Apply STRUCTURE PAINTS (Material No. 16-001) to the sand blasted
areas.
(4) Make sure that the scuff plates are in the correct condition and that
they fit satisfactorily.
(6) Put the vacuum equipment adjacent the BULK cargo-compartment door.
NOTE : The use of a strong vacuum pump for the attachment of the
____
scuff plates is recommended.
Subtask 53-45-15-420-051
(2) Around the inner areas of the scuff plate screw holes, apply the
adhesive tape to a radius of approximately 20 mm (0.7874 in.).
(3) Apply a layer of the release agent, SPECIAL MATERIALS (Material No.
05-013A) to the remaining inner areas of the scuff plates (1) and
(4).
NOTE : The correct application of the release agent makes sure that
____
the scuff plates are not damaged during the next removal
procedure.
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(4) Apply a thin layer of SEALANTS (Material No. 09-013) to the scuff
plate mating area of the fuselage skin (Ref. TASK 51-76-11-300-001).
(6) Remove the adhesive tape from the scuff plates and put the scuff
plate sections (1) and (4) in position.
(7) Align the scuff plate sections (1) and (4) and install and tighten
the screws (2) and the washers (3).
(8) Remove any unwanted sealant from around the scuff plates.
(10) Attach the SEALANTS (Material No. 09-030) (11) around and
approximately 30 mm (1.1811 in.) from the edges of the scuff plates.
(12) Attach the porous felt (12) with BONDING AND ADHESIVE COMPOUNDS
(Material No. 08-065) to the scuff plates.
(13) Attach the vacuum valve (14) to the SPECIAL MATERIALS (Material No.
05-068) (13).
(14) Put the SPECIAL MATERIALS (Material No. 05-068) (13) in position on
the scuff plates.
NOTE : Make sure that the SPECIAL MATERIALS (Material No. 05-068)
____
make an overlap of the seal tape by approximately 30 mm
(1.1811 in.).
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INTENTIONALLY BLANK
R
53-45-15
Page 420
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R (16) Operate the vacuum pump for as long as necessary. Refer to the
R environmental temperature shown in the table:
R -------------------------------------------------------------------------------
R TEMPERATURE TIME
R -------------------------------------------------------------------------------
R (19) Remove the vacuum valve (14) from the SPECIAL MATERIALS (Material No.
R 05-068) (13).
R (22) Clean the scuff plates and adjacent area with CLEANING AGENTS
R (Material No. 11-003).
R (23) Apply SEALANTS (Material No. 09-013) around the edges of the scuff
R plates, to the anchor nuts (5) and (6) and around the door sill. Let
R the sealant dry (Ref. TASK 51-76-11-300-001).
R (24) Apply STRUCTURE PAINTS (Material No. 16-003) to the sealant around
R the door sill, around the edges of the scuff plates and to the anchor
R nuts (5) and (6) (Ref. TASK 51-75-12-300-003).
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R 5. Close-up
________
R Subtask 53-45-15-410-051
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (2) Install the floor panel 162JF at the entrance to the BULK
R cargo-compartment (Ref. TASK 53-42-17-400-001).
R (5) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
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FITTINGS - DESCRIPTION AND OPERATION
____________________________________
1. General
_______
Fittings are made of forged aluminum alloy, or aluminum alloy sheet. They
are riveted to the structure.
2. Component
__________________
Location
(Ref. Fig. 001)
3. ___________
Description
Fittings make it possible to connect components to the structure, such as
the attachment for the AFT cargo-compartment door.
Fittings are also installed in the main structure to connect the main
structures together. The fittings are installed with sealant to prevent
corrosion.
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Fittings
Figure 001 (SHEET 1)
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Page 2
Feb 01/96
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Fittings
Figure 001 (SHEET 2)
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MISCELLANEOUS (EG : DRAINS) - DESCRIPTION AND OPERATION
_______________________________________________________
1. _______
General
Drains are installed in the rear fuselage structure of the aircraft at or
near to the lowest points in an area. The drains let water and condensation
drain out so that they do not cause corrosion.
2. Component
__________________
Location
R (Ref. Fig. 001)
3. ___________
Description
Drain valves are installed in the rear fuselage shell. When the cabin
pressurizes, the valves, preset to operate when cabin pressurization reaches
2 psi (0.1378 bar), close to prevent loss of cabin pressure. As the cabin
pressure decreases below the preset value (normally after the aircraft has
landed), the valves open (under spring tension) to allow any water that has
collected to drain away. You can remove the drain valves, for inspection or
replacement, with an allen key from outside the aircraft.
Drain valves are also installed in the door structure of the aft cargo
compartment.
In other structures (doors, door frames, stringers, brackets and fittings)
holes are drilled at the lowest points to make sure that water and
condensation drain to the drain valves.
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Rear Fuselage Drains
Figure 001
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Feb 01/96
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DRAINS - REAR FUSELAGE - REMOVAL/INSTALLATION
_____________________________________________
TASK 53-49-21-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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May 01/06
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C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-49-21-010-050
A. Get Access
(2) Open the AFT cargo-compartment door 826 (Ref. TASK 52-30-00-860-001).
(3) In the AFT cargo compartment, remove the applicable floor panels
(Ref. TASK 53-42-14-000-001).
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4. Procedure
_________
Subtask 53-49-21-020-050
(1) Remove the drain valve (5) from the valve retainer (3).
(2) Remove the sealant with CLEANING AGENTS (Material No. 11-004), a
lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) and a
SCRAPER - NON METALLIC from the collar (1).
(3) Remove and discard the collars (1) and the pins (4) (Ref. ASRM 51-42-
11-001).
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Drain Valve
Figure 401/TASK 53-49-21-991-001
R
EFF :
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Page 404
May 01/06
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R Drain Valve
R Figure 401A/TASK 53-49-21-991-001-B
EFF :
101-199, 53-49-21
Page 405
Feb 01/07
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Drain Valve
R Figure 401B/TASK 53-49-21-991-001-A
R
EFF :
901-999, 53-49-21
Page 406
Feb 01/07
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(4) Remove the strap (2).
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TASK 53-49-21-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
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Aug 01/07
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D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-49-21-860-050
(1) Make sure that the ACCESS PLATFORM 2M (6 FT) is in position at the
AFT cargo-compartment door 826.
(2) Make sure that the AFT cargo-compartment door 826 is open (Ref. TASK
52-30-00-860-001).
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(3) Make sure that the applicable floor panels in the AFT
cargo-compartment are removed (Ref. TASK 53-42-14-000-001).
(4) Make sure that the the insulation blankets are removed as necessary
(Ref. TASK 25-80-00-000-001).
4. Procedure
_________
Subtask 53-49-21-860-051
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
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(1) Remove the remaining sealant with CLEANING AGENTS (Material No. 11-
004), a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003)
and a SCRAPER - NON METALLIC from the strap (2), the valve retainer
(3) and the structure.
(2) Make sure that the parts retained from the removed component are
clean and in the correct condition.
Subtask 53-49-21-420-050
(1) Put the valve retainer (3) and the strap (2) in the installation
position.
(2) Install the valve retainer (3) and the strap (2) with the pins (4)
and the collars (1) (Ref. ASRM 51-42-11-001).
(3) Install the drain valve (5) in the valve retainer (3).
(4) Apply a bead of SEALANTS (Material No. 09-016) to the collars (1).
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5. Close-up
________
Subtask 53-49-21-410-050
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the floor panels in the AFT cargo-compartment (Ref. TASK 53-
42-14-400-001).
EFF :
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Feb 01/07
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CONE/REAR FUSELAGE - DESCRIPTION AND OPERATION
______________________________________________
1. _______
General
The cone/rear fuselage extends from FR70 to FR77.
2. Component
__________________
Location
(Ref. Fig. 001)
3. ___________
Description
(Ref. Fig. 001)
(2) A glass fibre cover protects the rear face of the rear pressure
bulkhead. The cover is installed adjacent to the access door 312AR.
(2) An aluminum cover protects the rear face of the rear pressure
bulkhead. The cover is installed adjacent to the access door 312AR.
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R Cone/Rear Fuselage
Figure 001
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(3) A work platform is installed at the lower forward part of the
cone/rear fuselage.
C. Jacking Point
R (1) A jacking point, installed between FR73 and FR74 at STR34, helps to
R support the aircraft when it is lifted on jacks during maintenance.
R (3) Part of the APU air-intake structure is installed between FR76 and
R FR77, between STR32 and STR34, left and right.
R (1) The attachment fittings for the horizontal stabilizer are installed
R at FR77. Diagonal struts, tie beams and edge beams make the fuselage
R structure stronger.
(2) The six vertical stabilizer attachment fittings are installed in this
R area. They are installed in pairs at FR70, FR72 and FR74. The top
R part of the frames are made stronger and are also the fittings.
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MAIN STRUCTURE - DESCRIPTION AND OPERATION
__________________________________________
1. _______
General
The main structure of the cone/rear fuselage are the frames, the stringers
and the skin plates. They are made of aluminum-alloy and they are riveted
together to make the fuselage shell. The support struts, the ties and the
edge beams make the fuselage shell stronger.
2. Component
__________________
Location
(Ref. Fig. 001)
3. Description
___________
A. Frames
(1) The frames are the stiffeners that go around the cone/rear fuselage
shell. They are made of aluminum-alloy and are machined or formed.
The FR70 is fully machined and it carries the aluminum sheet sections
which make the rear pressure bulkhead.
(2) The top sections of FR72 and FR74 are machined and are made stronger
to carry the load of the vertical stabilizer. The lower sections are
made of aluminum-alloy sheets which are formed.
(3) The frames in the area of the horizontal stabilizer cut-outs are made
in segments. A system of diagonal struts and edge beams make these
frames stronger.
(2) Skin stiffeners make the skin stronger in areas where there are no
stringers. The skin stiffeners are riveted to the skin plates.
C. Skin Plates
The skin plates are made of aluminum-alloy sheets and the stringers which
are riveted to them make them stronger. The skin plates are preformed to
the contour of the fuselage before they are riveted to the frames.
D. Support Struts
The support struts make the frames stronger in the areas where the frames
have to carry heavy loads. The diagonal support struts at FR77 are
adjustable.
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Main Structure Cone/Rear Fuselage
Figure 001
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E. Fittings
(1) The attachment fittings for the vertical stabilizer are made of
aluminum-alloy and are machined. The attachment fittings are riveted
in pairs to the top part of FR70, FR72 and FR74.
(2) The attachment fittings for the horizontal stabilizer are made of
aluminum-alloy. Bolts are used to attach these fittings to the upper
and the lower section of FR77.
(3) The diagonal struts support the fittings and the hinge bearings of
the horizontal stabilizer.
(4) The attachment fittings for the tail-cone are at the aft side of
FR77. They are machined and are part of FR77. The working platform in
the cone/rear fuselage is between FR71 and FR73. It has an
aluminum-alloy frame work and a honeycomb top panel.
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MAIN STRUCTURE - INSPECTION/CHECK
_________________________________
TASK 53-51-00-210-001
Detailed Visual Inspection of Rear Pressure Bulkhead AFT Face and Fuselage
Internal Structure, FR70 and FR71, from STGR 26 LH/RH to Bottom Center Line
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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Page 601
May 01/06
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C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-51-00-010-051
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1) Put the access platform below the access door 312AR.
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R
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(5) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth .
R
4. Procedure
_________
Subtask 53-51-00-210-050
A. Inspection.
(1) Examine the levelling compound/sealant around the drain pipe. Check
that any fluid in the area will flow out of the drain pipe.
5. Close-up
________
Subtask 53-51-00-914-050
(1) Carefully remove the levelling compound/sealant from around the drain
pipe with a nonmetallic scraper.
(2) Apply SEALANTS (Material No. 09-013) to the area around the drain
pipe.
EFF :
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Page 603
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R Pressure Bulkhead and FR70-71
Figure 601/TASK 53-51-00-991-001
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Page 604
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Subtask 53-51-00-916-050
Subtask 53-51-00-410-050
C. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
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Page 605
May 01/97
IAC
TASK 53-51-00-210-002
Detailed Visual Inspection of Rear Pressure Bulkhead Forward Face below Cabin
Floor Level
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 606
Nov 01/04
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-51-00-010-057
A. Get Access
R WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
R BEFORE YOU START A TASK ON OR NEAR:
R - THE FLIGHT CONTROLS
R - THE FLIGHT CONTROL SURFACES
R - THE LANDING GEAR AND THE RELATED DOORS
R - COMPONENTS THAT MOVE.
R WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
R MATERIAL.
R THIS MATERIAL IS DANGEROUS.
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(1) Open the AFT cargo-compartment door (Ref. TASK 52-30-00-860-001) or
(Ref. TASK 52-30-00-860-003).
(4) Clean the inspection area with CLEANING AGENTS (Material No. 11-003).
R
4. Procedure
_________
Subtask 53-51-00-210-055
A. Inspection:
(1) Examine the forward face of the rear pressure bulkhead below the
cabin floor for corrosion.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 535116000) for the
____
correct repair procedure.
5. Close-up
________
Subtask 53-51-00-916-061
Subtask 53-51-00-410-056
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
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Page 608
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Rear Pressure-Bulkhead Forward-Face below the Cabin Floor
Figure 602/TASK 53-51-00-991-004
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R
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R (5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
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TASK 53-51-00-210-003
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 611
Nov 01/04
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3. __________
Job Set-up
Subtask 53-51-00-010-058
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1) Put the access platform below the access door 312AR.
(4) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth.
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R
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4. Procedure
_________
Subtask 53-51-00-210-057
A. Inspection:
R (1) Examine the ring frame at the circumferential joint of the rear
R pressure-bulkhead skin at FR70 for:
- corrosion,
- cracks.
5. Close-up
________
Subtask 53-51-00-916-051
Subtask 53-51-00-410-057
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
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Page 613
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Circumferential Joint of the Rear Pressure-Bulkhead Skin
Figure 603/TASK 53-51-00-991-005
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R
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TASK 53-51-00-210-004
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
A. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-51-00-010-056
A. Get Access
R WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
R BEFORE YOU START A TASK ON OR NEAR:
R - THE FLIGHT CONTROLS
R - THE FLIGHT CONTROL SURFACES
R - THE LANDING GEAR AND THE RELATED DOORS
R - COMPONENTS THAT MOVE.
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4. Procedure
_________
Subtask 53-51-00-210-054
A. Inspection:
(1) Examine the fuselage skin at the THS forward corner cutouts for:
- cracks,
- skin distortion.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 535111000) for the
____
correct repair procedure.
5. Close-up
________
Subtask 53-51-00-410-055
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
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R
IAC
THS Forward Corner Cutouts
Figure 604/TASK 53-51-00-991-003
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R
IAC
TASK 53-51-00-210-005
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 618
Nov 01/04
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3. __________
Job Set-up
Subtask 53-51-00-010-054
A. Get Access
R WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
R BEFORE YOU START A TASK ON OR NEAR:
R - THE FLIGHT CONTROLS
R - THE FLIGHT CONTROL SURFACES
R - THE LANDING GEAR AND THE RELATED DOORS
R - COMPONENTS THAT MOVE.
R WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
R MATERIAL.
R THIS MATERIAL IS DANGEROUS.
(1) Put the access platform in position below the access door 312AR.
R
(4) Clean the inspection area with CLEANING AGENTS (Material No. 11-003).
R
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4. Procedure
_________
Subtask 53-51-00-210-053
A. Inspection:
NOTE : If necessary, refer to the ASRM (Ref. ASRM 535113000) for the
____
correct repair procedure.
5. Close-up
________
Subtask 53-51-00-916-059
Subtask 53-51-00-410-053
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
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R
IAC
FR74 Splices at Stringers 12 and 19
Figure 605/TASK 53-51-00-991-002
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Page 621
May 01/97
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TASK 53-51-00-210-007
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-51-00
Page 622
Nov 01/97
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3. __________
Job Set-up
Subtask 53-51-00-010-061
A. Get Access
R WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
R BEFORE YOU START A TASK ON OR NEAR:
R - THE FLIGHT CONTROLS
R - THE FLIGHT CONTROL SURFACES
R - THE LANDING GEAR AND THE RELATED DOORS
R - COMPONENTS THAT MOVE.
R WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
R MATERIAL.
R THIS MATERIAL IS DANGEROUS.
(1) Put the access platform in position below the access door 312AR.
(2) Put the access platform in position below the access door 314AR.
(3) Put a warning notice in position to tell persons not to operate the
APU.
(5) Carefully clean the THS attachment and back-up structure with
CLEANING AGENTS (Material No. 11-004) and a lint-free cloth.
R
EFF :
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Page 623
May 01/99
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4. Procedure
_________
Subtask 53-51-00-210-060
A. Inspection:
NOTE : If necessary, refer to the ASRM (Ref. ASRM 535300000) for the
____
correct repair procedure.
5. Close-up
________
Subtask 53-51-00-916-052
Subtask 53-51-00-410-060
B. Close Access
(1) Make sure that the electrical connectors are clean and in the correct
condition.
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
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Page 624
Nov 01/97
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THS Attachment and Back-up Structure at FR77 between STGR8 and STGR21
Figure 606/TASK 53-51-00-991-008
EFF :
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Page 625
May 01/97
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TASK 53-51-00-210-008
Detailed Visual Inspection of Rear Pressure Bulkhead Forward Face above Cabin
Floor Level
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
R A. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 626
May 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
R Subtask 53-51-00-010-063-A
R A. Get Access
R (2) Remove the insulation blankets from the rear pressure bulkhead
R (Ref. TASK 25-80-00-000-001).
R Subtask 53-51-00-010-063-B
R A. Get Access
R (3) Remove the insulation blankets from the rear pressure bulkhead
R (Ref. TASK 25-80-00-000-001).
EFF :
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Page 627
May 01/07
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**ON A/C ALL
Subtask 53-51-00-110-056
R B. Cleaning
R
R (1) Carefully clean the inspection area with CLEANING AGENTS (Material
R No. 11-026) and a clean lint-free cloth MISCELLANEOUS (Material No.
R 19-003).
R
4. Procedure
_________
Subtask 53-51-00-210-061
A. Inspection:
(1) Examine the forward face of the rear pressure bulkhead for corrosion.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 535116000) for the
____
correct repair procedure.
5. Close-up
________
Subtask 53-51-00-916-053
R Subtask 53-51-00-410-062-A
R B. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
EFF :
ALL 53-51-00
Page 628
May 01/07
IAC
Rear Pressure-Bulkhead Forward-Face above the Cabin Floor
Figure 607/TASK 53-51-00-991-009
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Page 629
May 01/97
R
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R (3) Install the aft galley (Ref. TASK 25-33-41-400-002).
R (4) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
R Subtask 53-51-00-410-062-B
R B. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
R (5) Remove the ground support and maintenance equipment, the special and
R standard tools and all other items.
R
EFF :
ALL 53-51-00
Page 630
May 01/07
IAC
R **ON A/C ALL
TASK 53-51-00-210-009
Detailed Visual Inspection of Tail Cone Attachment Fittings at FR77 and FR78
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-51-00
Page 631
May 01/06
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-51-00-010-065
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1) Put the access platform in position below the access door 314AR.
(2) Put a warning notice in position to tell persons not to operate the
APU.
EFF :
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Page 632
May 01/06
R
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(5) Clean the fittings with a nonmetallic scraper.
(6) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint-free cloth.
4. Procedure
_________
Subtask 53-51-00-210-062
A. Inspection:
NOTE : If necessary:
____
- refer to the ASRM (Ref. ASRM 53-51-12-001) for the tail-cone
attachment fittings at FR77
- refer to the ASRM (Ref. ASRM 53-56-11-001) and (Ref. ASRM
53-56-11-101) for the tail-cone attachment fittings at FR78
for the correct repair procedure.
5. Close-up
________
Subtask 53-51-00-916-062
Subtask 53-51-00-410-063
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-51-00
Page 633
May 01/06
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Tail-Cone Attachment Fittings
Figure 608/TASK 53-51-00-991-010
EFF :
ALL 53-51-00
Page 634
May 01/06
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TASK 53-51-00-210-010
Detailed Visual Inspection of Fin to Fuselage MID and AFT Attach Fittings
inside Fuselage, in Areas of Attachment to Fuselage Skin and to FR72 and FR74
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 635
May 01/06
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3. __________
Job Set-up
Subtask 53-51-00-010-066
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1) Put the access platform in position below the access door 312AR.
(4) Carefully clean the inspection area with CLEANING AGENTS (Material
No. 11-004) and a lint-free cloth.
EFF :
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Page 636
May 01/06
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4. Procedure
_________
Subtask 53-51-00-210-064
A. Inspection:
NOTE : If necessary, refer to the ASRM (Ref. ASRM 535600000) for the
____
correct repair procedure.
5. Close-up
________
Subtask 53-51-00-916-054
Subtask 53-51-00-410-064
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-51-00
Page 637
May 01/06
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Internal Fin to Fuselage Attachment Fittings at FR72 and FR74
Figure 609/TASK 53-51-00-991-011
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Page 638
May 01/06
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TASK 53-51-00-210-011
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 639
May 01/06
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3. __________
Job Set-up
Subtask 53-51-00-010-067
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1) Put the access platform in position below the access door 312AR.
(4) Carefully clean the inspection area with CLEANING AGENTS (Material
No. 11-002) and a lint-free cloth.
EFF :
ALL 53-51-00
Page 640
May 01/06
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4. Procedure
_________
Subtask 53-51-00-210-065
A. Inspection:
5. Close-up
________
Subtask 53-51-00-916-055
Subtask 53-51-00-410-065
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-51-00
Page 641
May 01/06
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THS Actuator Attachment Fittings
Figure 610/TASK 53-51-00-991-012
EFF :
ALL 53-51-00
Page 642
May 01/06
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TASK 53-51-00-210-012
Detailed Visual Inspection of Fin to Fuselage FWD, MID and AFT Attach Fittings,
Outside Fuselage, LH/RH
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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Page 643
May 01/06
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3. __________
Job Set-up
Subtask 53-51-00-010-059
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(2) Carefully clean the inspection area with CLEANING AGENTS (Material
No. 11-004) and a lint-free cloth.
4. Procedure
_________
Subtask 53-51-00-210-059
A. Inspection:
NOTE : If necessary, refer to the ASRM (Ref. ASRM 535500000) for the
____
correct repair procedure.
EFF :
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Page 644
May 01/06
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External Fin to Fuselage Attachment Fittings
Figure 611/TASK 53-51-00-991-006
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Page 645
May 01/06
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5. Close-up
________
Subtask 53-51-00-916-060
Subtask 53-51-00-410-058
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-51-00
Page 646
May 01/06
R
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TASK 53-51-00-210-014
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-51-00
Page 647
May 01/06
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3. __________
Job Set-up
Subtask 53-51-00-010-068
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1) Put the access platform in position below the access door 312AR.
(4) Carefully clean the inspection area with CLEANING AGENTS (Material
No. 11-004) and a lint-free cloth.
EFF :
ALL 53-51-00
Page 648
May 01/06
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4. Procedure
_________
Subtask 53-51-00-210-066
A. Inspection:
(1) Examine the reinforcement splice of the rear pressure bulkhead at the
fin forward attachment for:
- cracks.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 535116000) for the
____
correct repair procedure.
5. Close-up
________
Subtask 53-51-00-916-056
Subtask 53-51-00-410-066
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-51-00
Page 649
May 01/06
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Reinforcement Splice of the Rear Pressure Bulkhead at the Fin Forward
Attachment
Figure 612/TASK 53-51-00-991-013
EFF :
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53-51-00 Page 650
May 01/06
R
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TASK 53-51-00-210-015
Detailed Visual Inspection of Rear Pressure Bulkhead, Skin Splices AFT Face
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-51-00
Page 651
May 01/06
R
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3. __________
Job Set-up
Subtask 53-51-00-010-069
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1) Put the access platform in position below the access door 312AR.
(4) Carefully clean the inspection area with CLEANING AGENTS (Material
No. 11-004) and a lint-free cloth.
EFF :
ALL 53-51-00
Page 652
May 01/06
R
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4. Procedure
_________
Subtask 53-51-00-210-067
A. Inspection:
NOTE : If necessary, refer to the ASRM (Ref. ASRM 535100000) for the
____
correct repair procedure.
5. Close-up
________
Subtask 53-51-00-916-057
Subtask 53-51-00-410-067
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-51-00
Page 653
May 01/06
R
IAC
Rear Pressure Bulkhead, Aft Face Skin Splices
Figure 613/TASK 53-51-00-991-014
EFF :
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Page 654
May 01/06
R
IAC
TASK 53-51-00-210-016
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-51-00
Page 655
May 01/06
R
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3. __________
Job Set-up
Subtask 53-51-00-010-070
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : OBEY THE MANUFACTURERS INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1) Put the access platform in position below the access door 312AR.
(4) Carefully clean the inspection area with CLEANING AGENTS (Material
No. 11-004) and a lint-free cloth.
EFF :
ALL 53-51-00
Page 656
May 01/06
R
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4. Procedure
_________
Subtask 53-51-00-210-068
A. Inspection:
(1) Examine the cutouts of the aft face of the rear pressure bulkhead
for:
- cracks.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 535100000) for the
____
correct repair procedure.
5. Close-up
________
Subtask 53-51-00-916-058
Subtask 53-51-00-410-068
B. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-51-00
Page 657
May 01/06
R
IAC
Rear Pressure Bulkhead Cutouts
Figure 614/TASK 53-51-00-991-015
EFF :
ALL 53-51-00
Page 658
May 01/06
R
IAC
TASK 53-51-00-210-017
Detailed Visual Tnspection of Shear Ties and Frame Clips at FR72 and FR74,
between Stringer 3 and Stringer 9, LH/RH, Internal Structure
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific flashlight
No specific lint free cloth
No specific access platform 3 m (9 ft. 10 in.)
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
ASRM 53-00-12-201
53-51-00-991-017 Fig. 615
EFF :
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Page 659
May 01/06
R
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3. __________
Job Set-up
Subtask 53-51-00-010-073
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(1) Put the access platform in position below the access door 312AR.
Subtask 53-51-00-110-064
B. Cleaning Procedure
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and a lint free cloth , if necessary. Make sure the area is dry
before you continue.
EFF :
ALL 53-51-00
Page 660
May 01/06
R
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4. Procedure
_________
Subtask 53-51-00-210-069
(1) Do a detailed visual inspection of the shear ties and the frame clips
at FR72 and FR74, between stringer 3 and stringer 9, LH and RH,
internal structure for cracks.
5. Close-up
________
Subtask 53-51-00-410-071
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-51-00
Page 661
May 01/06
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Shear Ties and Frame Clips at FR72 and FR74, between Stringer 3 and Stringer 9,
LH/RH
Figure 615/TASK 53-51-00-991-017
EFF :
ALL
53-51-00 Page 662
May 01/06
R
IAC
TASK 53-51-00-210-019
General Visual Inspection of Fuselage Skin around Cutout for Tail Compartment
Access Door, between FR 70 and FR 73, STGR 25 RH and Bottom Center Line
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-51-00
Page 663
May 01/06
R
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-51-00-941-066
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
(2) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in the required
position.
Subtask 53-51-00-110-066
B. Cleaning Procedure
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material
No. 19-003) and the CLEANING AGENTS (Material No. 11-004), and let
the area dry.
EFF :
ALL 53-51-00
Page 664
May 01/06
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4. Procedure
_________
Subtask 53-51-00-210-071
A. Inspection
(1) Examine the following area for scratches, dents and cracks:
- the fuselage skin around the cutout for the tail compartment access
door between FR 70 and FR 73 and from stringer 25 RH to bottom
centerline, external surface.
NOTE : This does not include the area under the scuff plates.
____
5. Close-up
________
Subtask 53-51-00-942-069
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-51-00
Page 665
May 01/06
R
IAC
Fuselage Skin around Cutout for Tail Compartment Acces Door
Figure 616/TASK 53-51-00-991-019
EFF :
ALL 53-51-00
Page 666
May 01/06
R
IAC
TASK 53-51-00-210-018
General Visual Inspection of the Fuselage External Surface and the Vertical
Stabilizer Attachment Fitting, below the Vertical Stabilizer/Fuselage Fairings
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-51-00
Page 667
May 01/06
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C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-51-00-010-074
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
(3) Remove the vertical stabilizer fairings 323AL, 323AR (Ref. TASK 53-
55-11-000-001).
Subtask 53-51-00-110-065
B. Cleaning Procedure
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WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______
AREA WHEN YOU USE SPECIAL MATERIALS.
IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH
OR IN YOUR EYES :
-FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15
MINUTES.
-GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS.
DO NOT BREATHE THE FUMES FROM THE MATERIAL.
DO NOT SMOKE WHEN YOU USE THE MATERIAL.
DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF
HEAT.
THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE
AND SKIN IRRITANTS.
(2) Clean the area with a lint-free cloth and the CLEANING AGENTS
(Material No. 11-004), and let the area dry.
4. Procedure
_________
Subtask 53-51-00-210-070
A. Inspection
NOTE : If necessary, refer to the ASRM (Ref. ASRM 535100000) for the
____
correct repair procedure.
EFF :
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Page 669
May 01/06
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Fuselage External Surface and Vertical Stabilizer Attachment Fittings Below
Vertical Stabilizer/Fuselage Fairings
Figure 617/TASK 53-51-00-991-018
EFF :
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May 01/06
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5. Close-up
________
Subtask 53-51-00-916-064
Subtask 53-51-00-410-072
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the vertical stabilizer fairings 323AL, 323AR (Ref. TASK 53-
55-11-400-001).
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-51-00
Page 671
May 01/06
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TASK 53-51-00-210-020
General Visual Inspection of the Rear Fuselage Internal Structure, between FR70
and FR77
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-51-00
Page 672
May 01/06
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C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-51-00-010-076
A. Get Access
(1) Put a WARNING NOTICE in position to tell persons not to operate the
APU.
(2) Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in position below the
access door 312AR.
(3) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position below the
access door 314AR.
Subtask 53-51-00-110-067
(1) Make sure that the surface of the inspection area is clean.
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(2) If necessary, clean the inspection area with a lint-free cotton
cloth, MISCELLANEOUS (Material No. 19-003) and the CLEANING AGENTS
(Material No. 11-004).
4. Procedure
_________
Subtask 53-51-00-210-072
A. Inspection Procedure
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint coating of the aircraft.
(b) Repair the damage to the paint system (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
5. Close-up
________
Subtask 53-51-00-410-074
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 53-51-00
Page 674
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Inspection Areas of the Rear Fuselage, between FR70 and FR77
Figure 618/TASK 53-51-00-991-020
EFF :
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(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-51-00
Page 676
May 01/06
R
IAC
TASK 53-51-00-210-021
General Visual Inspection of the Rear Fuselage External Surface, between FR70
and FR87
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE CLEAR.
_______
MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR
DAMAGE.
WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
FALL CAN INJURE OR KILL YOU.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-51-00
Page 677
May 01/06
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IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-51-00-941-067
(1) Put a WARNING NOTICE in position to tell persons not to operate the
APU.
(2) Put the ACCESS PLATFORM 8M (26 FT) - ADJUSTABLE in position at the
inspection area.
EFF :
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Page 678
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Subtask 53-51-00-110-068
(1) Make sure that the surface of the inspection area is clean.
4. Procedure
_________
Subtask 53-51-00-210-073
A. Inspection Procedure
(a) Look for scratches, dents, cracks, corrosion and damage to the
surface protection.
(a) Refer to the ASRM (Ref. ASRM 51-11-00-001) for the classification
of the damage.
(b) Refer to the ASRM (Ref. ASRM 53-51-11-101) for the allowable
damage limits for this structure.
(c) Repair the scratches which are in the limits (Ref. TASK 51-73-11-
300-001) or (Ref. TASK 51-73-11-300-004), as necessary.
(d) Repair the dents which are in the limits (Ref. TASK 51-73-11-300-
003).
EFF :
ALL 53-51-00
Page 679
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Inspection Areas of the Rear Fuselage and the Tail Cone, between FR70 and FR87
Figure 619/TASK 53-51-00-991-021
EFF :
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Page 680
May 01/06
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(e) For damage that is more than the limits for minor damage, refer
to the ASRM (Ref. ASRM 53-51-11-201) for the correct repair data.
(a) Refer to the ASRM (Ref. ASRM 51-22-00-001) for the general
corrosion data.
(a) Refer to the ASRM (Ref. ASRM 51-23-11-001) for the general data
about the paint coating of the aircraft.
(b) Repair the damage to the paint system (Ref. TASK 51-75-12-300-
001) or (Ref. TASK 51-75-12-300-003), as necessary.
5. Close-up
________
Subtask 53-51-00-942-070
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
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Page 681
May 01/06
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MAINTENANCE PLATFORM - REMOVAL/INSTALLATION
___________________________________________
TASK 53-51-17-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-51-17-010-050
A. Get Access
EFF :
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Page 401
Feb 01/96
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4. Procedure
_________
Subtask 53-51-17-020-050
EFF :
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Page 402
Feb 01/96
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Maintenance Platform Panels
Figure 401/TASK 53-51-17-991-001
EFF :
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Page 403
Feb 01/96
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TASK 53-51-17-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-51-17
Page 404
Feb 01/08
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3. __________
Job Set-up
Subtask 53-51-17-860-050
(1) Make sure that the aircraft is in the same configuration as for the
removal task.
4. Procedure
_________
Subtask 53-51-17-110-050
(1) Clean the component interface and the adjacent area with CLEANING
AGENTS (Material No. 11-004) and a clean cloth.
(2) Make sure that the parts retained from the removed component are
clean and in the correct condition.
Subtask 53-51-17-420-050
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
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Page 405
Feb 01/96
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(3) Apply SPECIAL MATERIALS (Material No. 05-002) to the screws (1).
(5) Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-064) to the
panels, if necessary.
5. Close-up
________
Subtask 53-51-17-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-51-17
Page 406
Feb 01/96
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SUPPORT STRUTS - DESCRIPTION AND OPERATION
__________________________________________
1. General
_______
The support struts in the cone/rear fuselage make the structure in this
section stronger. The support struts are part of the main structure. Some of
the support struts are removable and the others are rivited to the
structure. The removable support struts are divided into three groups:
- the upper V support struts,
- the lower V support struts,
- the diagonal support struts.
2. Component
__________________
Location
(Ref. Fig. 001)
3. ___________
Description
The upper and lower V support struts are installed between FR74 and FR77.
The support struts are made of extruded aluminum.
All of the upper V support struts are removable and they are adjustable.
Only two of the lower V support struts are removable.
The removable diagonal support struts at FR77 are adjustable. They support
the horizontal stabilizer attach fittings. The diagonal support struts are
also used to center the horizontal stabilizer.
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Feb 01/96
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Support Struts
Figure 001
EFF :
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Page 2
Feb 01/96
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SUPPORT STRUTS - REMOVAL/INSTALLATION
_____________________________________
TASK 53-53-11-000-001
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
NOTE : The removal of one support strut is given. The procedure is the same for
____
the other support struts.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 401
Aug 01/06
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3. __________
Job Set-up
Subtask 53-53-11-010-050
A. Get Access
(1) Put the warning notice in position to tell persons not to operate the
flight controls.
Subtask 53-53-11-864-052
B. Depressurize the Green, Yellow and Blue hydraulic systems (Ref. TASK 29-
10-00-864-001), (Ref. TASK 29-10-00-864-002) and (Ref. TASK 29-10-00-864-
003).
Subtask 53-53-11-865-050
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
105VU FLT CTL/SEC1/STBY SPLY 22CE B01
121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20
121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19
121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17
121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
EFF :
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Page 402
Aug 01/06
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R **ON A/C ALL
4. Procedure
_________
Subtask 53-53-11-020-050
A. Removal:
(1) Remove the nut (5), the screw (2) and the washer (3).
(6) Remove the bolts (9), the washers (8) and the support strut (1).
EFF :
ALL 53-53-11
Page 403
May 01/06
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R Horizontal Support Struts
Figure 401/TASK 53-53-11-991-001
EFF :
ALL 53-53-11
Page 404
May 01/06
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TASK 53-53-11-400-001
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
NOTE : The installation of one support strut is given. The procedure is the
____
same for the other support struts.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 405
Feb 01/08
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C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-53-11-860-050
(1) Make sure that the aircraft is in the same configuration as for the
removal task.
(2) Make sure that the warning notice is in position to tell persons not
to move the flight controls
Subtask 53-53-11-864-053
B. Make sure that the Green, Yellow and Blue hydraulic systems are
depressurized (Ref. TASK 29-10-00-864-001), (Ref. TASK 29-10-00-864-002)
and (Ref. TASK 29-10-00-864-003).
EFF :
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Page 406
Feb 01/08
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Subtask 53-53-11-865-052
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
105VU FLT CTL/SEC1/STBY SPLY 22CE B01
121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20
121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19
121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17
121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
4. Procedure
_________
Subtask 53-53-11-916-051
EFF :
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Page 407
Aug 01/06
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R (3) Protective treatment.
R (a) Apply SPECIAL MATERIALS (Material No. 05-002) to the bolts (9)
R and the bushes (6) and (7).
Subtask 53-53-11-420-050
B. Installation:
(2) Put the support strut (1) in position and install the washers (8) and
the bolts (9).
(4) TORQUE the nuts (12) to between 2.0 and 2.2 m.daN (14.74 and 16.22
lbf.ft).
(5) Safety the nuts (12) with the new cotter pins (11).
R (6) Put the bonding straps (4) in position and install the screws (2),
R the washers (3) and the nuts (5) (Ref. TASK 20-28-00-912-004).
(7) Apply STORAGE PRESERVATION (Material No. 15-007) to the work area
(Ref. TASK 51-75-13-916-002).
5. Close-up
________
Subtask 53-53-11-865-051
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
15CE1, 15CE2, 16CE1, 16CE2, 19CE1, 19CE2, 19CE3, 20CE1, 20CE2, 21CE1,
21CE2, 21CE3, 22CE.
EFF :
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Page 408
May 01/06
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Subtask 53-53-11-410-050
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-53-11
Page 409
May 01/06
R
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TASK 53-53-11-000-002
R WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
R START A TASK ON OR NEAR:
R - THE FLIGHT CONTROLS
R - THE FLIGHT CONTROL SURFACES
R - THE LANDING GEAR AND THE RELATED DOORS
R - COMPONENTS THAT MOVE.
NOTE : The removal of one support strut is given. The procedure is the same for
____
the other support struts.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-53-11
Page 410
May 01/06
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3. __________
Job Set-up
Subtask 53-53-11-010-051
A. Get Access
(1) Make sure that the Trimmable Horizontal Stabilizer (THS) is in the
zero position (Ref. TASK 27-41-00-220-003).
(2) Put the warning notice in position to tell persons not to operate the
flight controls.
Subtask 53-53-11-864-050
B. Depressurize the Blue, Green and Yellow hydraulic systems (Ref. TASK 29-
10-00-864-001), (Ref. TASK 29-10-00-864-002) and (Ref. TASK 29-10-00-864-
003).
Subtask 53-53-11-865-053
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
105VU FLT CTL/SEC1/STBY SPLY 22CE B01
121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20
121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19
121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17
EFF :
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Page 411
Aug 01/06
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-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
4. Procedure
_________
Subtask 53-53-11-020-051
A. Removal:
(1) Remove the nuts (9), the washers (7) and the screws (6).
EFF :
ALL 53-53-11
Page 412
Aug 01/06
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R Diagonal Support Struts
Figure 402/TASK 53-53-11-991-002
EFF :
ALL 53-53-11
Page 413
Aug 01/06
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TASK 53-53-11-400-002
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
NOTE : The installation for one support strut is given. The procedure is the
____
same for the other support struts.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 414
Aug 01/06
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C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-53-11-860-051
(1) Make sure that the aircraft is in the same configuration as for the
removal task.
(2) Make sure that the warning notice is in position to tell persons not
to move the flight controls.
Subtask 53-53-11-864-051
B. Make sure that the Green, Yellow and Blue hydraulic systems are
depressurized (Ref. TASK 29-10-00-864-001), (Ref. TASK 29-10-00-864-002),
(Ref. TASK 29-10-00-864-003).
EFF :
ALL 53-53-11
Page 415
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IAC
Subtask 53-53-11-865-054
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
105VU FLT CTL/SEC1/STBY SPLY 22CE B01
121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20
121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19
121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17
121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
4. Procedure
_________
Subtask 53-53-11-916-050
(3) Apply COMMON GREASE (Material No. 04-004) to the bolts (1).
Subtask 53-53-11-420-053
B. Installation
(1) Put the support strut (5) in position and install the bolts (1).
(2) Install the washers (2) and the nuts (3). Do not tighten the nuts (3)
at this time.
EFF :
ALL 53-53-11
Page 416
Aug 01/06
IAC
Adjustment of the THS
Figure 403/TASK 53-53-11-991-003
EFF :
ALL 53-53-11
Page 417
Aug 01/06
R
IAC
(3) Make sure that the clearance X is 14.5 +2.5 -2.5 mm (0.5708 +0.0984
-0.0984 in.) between the THS attach support and the inner attach
fitting.
(4) Do a check of the clearance Y at the left and the right attach
fittings:
(a) The value of the clearance Y must be equal at the left and the
right fittings. A tolerance of +/- 0.2 mm (0.0078 in.) is
permitted.
(5) Make sure that the dimension Z between the bolt and the sleeve is a
minimum of 0.5 mm (0.0196 in.).
(6) If the clearances X, Y and Z are correct, do the steps that
follow:
(a) TORQUE the locknuts (11) to between 11.00 and 13.00 m.daN (81.12
and 95.87 lbf.ft).
(c) TORQUE the tubes of the support struts (5), in the correct
direction, as follows:
- The top tubes to between 3.25 and 3.59 m.daN (23.96 and 26.47
lbf.ft).
- The bottom tubes to between 2.78 and 3.08 m.daN (20.50 and
22.71 lbf.ft).
(d) TORQUE the nuts (3) to between 1.20 and 1.35 m.daN (106.19 and
119.46 lbf.in).
(e) Safety the nuts (3) with the new cotter pins (4).
(f) Install the bonding straps (8) and (10) with the screws (6), the
washers (7) and the nuts (9) (Ref. TASK 20-28-00-912-004).
(g) Apply the STORAGE PRESERVATION (Material No. 15-007) to the area
(Ref. TASK 51-75-13-916-002).
(7) If one or more of the clearances X, Y and Z is(are) not
correct, do the adjustment of the THS (Refer to Para. 4.C.).
EFF :
ALL 53-53-11
Page 418
Aug 01/06
R
IAC
Subtask 53-53-11-820-051
(3) Remove the two support struts at the side where the clearance Y has
the highest value.
(4) Adjust the two remaining support struts until the value of the
clearance Y is equal at the left and the right fittings. A
tolerance of +/- 0.2 mm (0.0078 in.) is permitted.
(5) Make sure that the clearance X is 14.5 +2.5 -2.5 mm (0.5708 +0.0984
-0.0984 in.) between the THS attach support and the inner fitting.
(6) Make sure that the dimension Z between the bolt and the sleeve is a
minimum of 0.5 mm (0.0196 in.).
Subtask 53-53-11-420-054
(1) TORQUE the locknuts (11) to between 11.00 and 13.00 m.daN (81.12 and
95.87 lbf.ft).
(2) Safety the locknuts (11) with the lockwire, MISCELLANEOUS (Material
No. 19-010)
(3) TORQUE the tubes of the support struts (5), in the correct direction,
as follows:
- The top tubes to between 3.25 and 3.59 m.daN (23.96 and 26.47
lbf.ft).
- The bottom tubes to between 2.78 and 3.08 m.daN (20.50 and 22.71
lbf.ft).
(4) TORQUE the nuts (3) to between 1.20 and 1.35 m.daN (106.19 and 119.46
lbf.in).
(5) Safety the nuts (3) with the new cotter pins (4).
(6) Install the bonding straps (8) and (10) with the screws (6), the
washers (7) and the nuts (9) (Ref. TASK 20-28-00-912-004).
EFF :
ALL 53-53-11
Page 419
Aug 01/06
R
IAC
(7) Apply the STORAGE PRESERVATION (Material No. 15-007) to the area
(Ref. TASK 51-75-13-916-002).
5. Close-up
________
Subtask 53-53-11-865-055
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
15CE1, 15CE2, 16CE1, 16CE2, 19CE1, 19CE2, 19CE3, 20CE1, 20CE2, 21CE1,
21CE2, 21CE3, 22CE.
Subtask 53-53-11-410-051
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(7) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-53-11
Page 420
Aug 01/06
R
IAC
FAIRINGS - DESCRIPTION AND OPERATION
____________________________________
1. _______
General
The fairings 323AL, 323AR, 325AL and 325AR are made of layers of glassfiber
reinforced plastic over a honeycomb core. They are installed at the vertical
stabilizer to the aircraft joint. The fairings make sure that the airflow
around the joint is smooth and this keeps the turbulance to a minimum.
2. Component
__________________
Location
(Ref. Fig. 001)
EFF :
ALL 53-55-00
Page 1
Feb 01/96
IAC
Fairings - Component Location
Figure 001
EFF :
ALL 53-55-00
Page 2
Feb 01/96
IAC
FAIRINGS - VERTICAL STABILIZER - REMOVAL/INSTALLATION
_____________________________________________________
TASK 53-55-11-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-55-11
Page 401
May 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-55-11-941-050
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
Subtask 53-55-11-864-050
B. De-pressurize the Green, Yellow and Blue hydraulic systems. (Ref. TASK
29-10-00-864-001) (Ref. TASK 29-10-00-864-002) (Ref. TASK 29-10-00-864-
003).
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES
_______
ARE CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC
SYSTEM.
Subtask 53-55-11-865-050
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
49VU AUTO FLT/FAC1/28VDC 5CC1 B04
49VU AUTO FLT/FAC1/26VAC 14CC1 B03
105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
105VU FLT CTL/SEC1/STBY SPLY 22CE B01
EFF :
ALL 53-55-11
Page 402
Aug 01/06
IAC
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20
121VU AUTO FLT/FAC2/28VDC 5CC2 M19
121VU AUTO FLT/FAC2/26VAC 14CC2 M18
121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19
121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17
121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
4. Procedure
_________
Subtask 53-55-11-020-050
A. Removal:
EFF :
ALL 53-55-11
Page 403
May 01/06
IAC
R Vertical Stabilizer Fairings 323AL/323AR
Figure 401/TASK 53-55-11-991-001
EFF :
ALL 53-55-11
Page 404
Aug 01/96
IAC
TASK 53-55-11-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-55-11
Page 405
May 01/05
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-55-11-860-050
(1) Make sure that the aircraft is in the same configuration as for the
removal task.
(2) Make sure the warning notices are in position to tell persons not to
operate the flight controls.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
Subtask 53-55-11-864-051
B. Make sure that the Green, Yellow and Blue hydraulic systems are
depressurized. (Ref. TASK 29-10-00-864-001) (Ref. TASK 29-10-00-864-002)
(Ref. TASK 29-10-00-864-003)
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES
_______
ARE CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC
SYSTEM.
EFF :
ALL 53-55-11
Page 406
Feb 01/96
IAC
Subtask 53-55-11-865-051
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
49VU AUTO FLT/FAC1/28VDC 5CC1 B04
49VU AUTO FLT/FAC1/26VAC 14CC1 B03
105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
105VU FLT CTL/SEC1/STBY SPLY 22CE B01
121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20
121VU AUTO FLT/FAC2/28VDC 5CC2 M19
121VU AUTO FLT/FAC2/26VAC 14CC2 M18
121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19
121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17
121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
4. Procedure
_________
Subtask 53-55-11-914-050
(1) Clean the mating surfaces of the fairing with a nonmetallic scraper,
CLEANING AGENTS (Material No. 11-003) and a lintfree cloth.
EFF :
ALL 53-55-11
Page 407
Aug 01/06
IAC
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______
MATERIALS ONLY WITH A GOOD SUPPLY OF AIR.
OBEY THE MANUFACTURERS INSTRUCTIONS.
PUT ON PROTECTIVE CLOTHING.
DO NOT GET THEM IN YOUR MOUTH.
DO NOT SMOKE.
DO NOT BREATHE THE GAS.
THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT.
GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
(4) Apply SPECIAL MATERIALS (Material No. 05-013A) and SEALANTS (Material
No. 09-018) to the mating surfaces of the fairing (2).
Subtask 53-55-11-420-050
B. Installation:
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the screws (1) and TORQUE to 0.3 m.daN (26.54 lbf.in).
(4) Make sure that the clearance a is 1.0 +1.0 -1.0 mm (0.0393 +0.0393-
0.0393 in.) between the fairing (2), the dorsal fin (3) and the
rudder fairing (4).
(5) Make sure that the clearance c is 10.0 +3.5 -3.5 mm (0.3937 +0.1377
-0.1377 in.) between the fairing (2) and the fuselage.
(6) Apply a bead of SEALANTS (Material No. 09-016A) to the edges of the
fairing (2).
5. Close-up
________
Subtask 53-55-11-410-051
A. Close Access
EFF :
ALL 53-55-11
Page 408
Feb 01/96
IAC
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 53-55-11-865-052
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
5CC1, 5CC2, 14CC1, 14CC2, 15CC, 15CE1, 15CE2, 16CE1, 16CE2, 19CE1, 19CE2,
19CE3, 21CE1, 21CE2, 21CE3, 22CE.
EFF :
ALL 53-55-11
Page 409
Feb 01/96
IAC
FAIRINGS - RUDDER - REMOVAL/INSTALLATION
________________________________________
TASK 53-55-12-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-55-12
Page 401
Feb 01/07
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-55-12-941-050
(1) Put the warning notices in the cockpit to tell persons not to operate
the flight controls.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
Subtask 53-55-12-864-050
B. Depressurize the Green, Yellow and Blue hydraulic systems (Ref. TASK 29-
10-00-864-001) (Ref. TASK 29-10-00-864-002) (Ref. TASK 29-10-00-864-003).
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES
_______
ARE CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC
SYSTEM.
Subtask 53-55-12-865-050
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
49VU AUTO FLT/FAC1/28VDC 5CC1 B04
49VU AUTO FLT/FAC1/26VAC 14CC1 B03
105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
105VU FLT CTL/SEC1/STBY SPLY 22CE B01
121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20
121VU AUTO FLT/FAC2/28VDC 5CC2 M19
EFF :
ALL 53-55-12
Page 402
Feb 01/07
R
IAC
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
121VU AUTO FLT/FAC2/26VAC 14CC2 M18
121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19
121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17
121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
4. Procedure
_________
Subtask 53-55-12-020-050
A. Removal:
EFF :
ALL 53-55-12
Page 403
Feb 01/07
IAC
R Rudder Fairing - Removal/Installation
Figure 401/TASK 53-55-12-991-001
EFF :
001-010, 53-55-12
Page 404
Nov 01/02
IAC
Rudder Fairing - Removal/Installation
Figure 401A/TASK 53-55-12-991-001-A
R
EFF :
011-012, 014-099, 101-199, 901-999, 53-55-12
Page 405
Feb 01/07
IAC
TASK 53-55-12-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-55-12
Page 406
May 01/05
IAC
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-55-12-860-050
(1) Make sure that the aircraft is in the same configuration as for the
removal task.
(2) Make sure the warning notice is in position to tell persons not to
operate the flight controls.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
EFF :
ALL 53-55-12
Page 407
Feb 01/07
IAC
Subtask 53-55-12-864-051
B. Make sure the Green, Yellow and Blue hydraulic systems are depressurized
(Ref. TASK 29-10-00-864-001) (Ref. TASK 29-10-00-864-002) (Ref. TASK 29-
10-00-864-003).
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES
_______
ARE CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC
SYSTEM.
Subtask 53-55-12-865-051
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
49VU AUTO FLT/FAC1/28VDC 5CC1 B04
49VU AUTO FLT/FAC1/26VAC 14CC1 B03
105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
105VU FLT CTL/SEC1/STBY SPLY 22CE B01
121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20
121VU AUTO FLT/FAC2/28VDC 5CC2 M19
121VU AUTO FLT/FAC2/26VAC 14CC2 M18
121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19
121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17
121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
4. Procedure
_________
Subtask 53-55-12-914-050
(1) Clean the mating surfaces of the fairing with a nonmetallic scraper,
CLEANING AGENTS (Material No. 11-003) and a lintfree cloth.
EFF :
ALL 53-55-12
Page 408
Feb 01/07
R
IAC
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______
MATERIALS ONLY WITH A GOOD SUPPLY OF AIR.
OBEY THE MANUFACTURERS INSTRUCTIONS.
PUT ON PROTECTIVE CLOTHING.
DO NOT GET THEM IN YOUR MOUTH.
DO NOT SMOKE.
DO NOT BREATHE THE GAS.
THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT.
GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
(4) Apply SPECIAL MATERIALS (Material No. 05-013A) and SEALANTS (Material
No. 09-018) to the mating surfaces of the fairings.
Subtask 53-55-12-420-050
B. Installation:
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Install the screws (1) and TORQUE to 0.3 m.daN (26.54 lbf.in).
(4) Make sure that the clearance a is 1.0 +1.0 -1.0 mm (0.0393 +0.0393-
0.0393 in.) between the fairing (2) and the vertical stabilizer
fairing (3), and the fairing and the vertical stabilizer (4).
(5) Make sure that the clearance c is 10.0 +3.5 -3.5 mm (0.3937 +0.1377
-0.1377 in.) between the fairing and the fuselage.
(6) Apply a bead of SEALANTS (Material No. 09-016) to the edges of the
fairing (2).
5. Close-up
________
EFF :
ALL 53-55-12
Page 409
Feb 01/07
R
IAC
R **ON A/C 011-012, 014-099, 101-199, 901-999,
Subtask 53-55-12-410-051
A. Close Access
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 53-55-12-865-052
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
5CC1, 5CC2, 14CC1, 14CC2, 15CC, 15CE1, 15CE2, 16CE1, 16CE2, 19CE1, 19CE2,
19CE3, 21CE1, 21CE2, 21CE3, 22CE.
EFF :
ALL 53-55-12
Page 410
Feb 01/07
IAC
FAIRINGS - TRIMMABLE HORIZONTAL STABILIZER - REMOVAL/INSTALLATION
_________________________________________________________________
TASK 53-55-13-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-55-13
Page 401
May 01/06
R
IAC
3. __________
Job Set-up
Subtask 53-55-13-941-050
(1) Put a warning notice in position to tell persons not to operate the
flight controls.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
(2) Put the access platform in position at Zones 311 and 312.
Subtask 53-55-13-864-050
B. Depressurize the Green, Yellow and Blue hydraulic systems (Ref. TASK 29-
10-00-864-001) (Ref. TASK 29-10-00-864-002) (Ref. TASK 29-10-00-864-003).
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES
_______
ARE CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC
SYSTEM.
Subtask 53-55-13-865-050
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
49VU AUTO FLT/FAC1/28VDC 5CC1 B04
49VU AUTO FLT/FAC1/26VAC 14CC1 B03
105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
105VU FLT CTL/SEC1/STBY SPLY 22CE B01
121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20
121VU AUTO FLT/FAC2/28VDC 5CC2 M19
121VU AUTO FLT/FAC2/26VAC 14CC2 M18
121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19
EFF :
ALL 53-55-13
Page 402
Aug 01/06
IAC
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17
121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
Subtask 53-55-13-010-050
D. Get Access
4. Procedure
_________
Subtask 53-55-13-020-050
A. Removal:
EFF :
ALL 53-55-13
Page 403
Aug 01/06
IAC
R Fittings of the THS Fairing
Figure 401/TASK 53-55-13-991-001
EFF :
ALL 53-55-13
Page 404
Aug 01/96
IAC
TASK 53-55-13-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-55-13
Page 405
Nov 01/04
IAC
3. __________
Job Set-up
Subtask 53-55-13-860-050
(1) Make sure that the aircraft is in the same configuration as for the
removal task.
(2) Make sure that the warning notice is in position to tell persons not
to operate the flight controls.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
Subtask 53-55-13-864-051
B. Make sure that the Green, Yellow and Blue hydraulic systems are
depressurized. (Ref. TASK 29-10-00-864-001) (Ref. TASK 29-10-00-864-002)
(Ref. TASK 29-10-00-864-003)
WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES
_______
ARE CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC
SYSTEM.
Subtask 53-55-13-865-051
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
49VU AUTO FLT/FAC1/28VDC 5CC1 B04
49VU AUTO FLT/FAC1/26VAC 14CC1 B03
105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
105VU FLT CTL/SEC1/STBY SPLY 22CE B01
121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20
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Page 406
Aug 01/06
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-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
121VU AUTO FLT/FAC2/28VDC 5CC2 M19
121VU AUTO FLT/FAC2/26VAC 14CC2 M18
121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19
121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17
121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
4. Procedure
_________
Subtask 53-55-13-914-050
(1) Clean the mating surfaces of the fairing with a nonmetallic scraper,
CLEANING AGENTS (Material No. 11-003) and a lint-free cloth.
(4) Apply SEALANTS (Material No. 09-018) to the fairing interface and the
screws (1).
EFF :
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Page 407
Aug 01/06
IAC
Subtask 53-55-13-420-050
B. Installation:
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
5. Close-up
________
Subtask 53-55-13-410-050
A. Close Access
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 53-55-13-865-052
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
5CC1, 5CC2, 14CC1, 14CC2, 15CC, 15CE1, 15CE2, 16CE1, 16CE2, 19CE1, 19CE2,
19CE3, 21CE1, 21CE2, 21CE3, 22CE.
EFF :
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Aug 01/06
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IAC
FITTINGS - DESCRIPTION AND OPERATION
____________________________________
1. General
_______
2. Component
__________________
Location
(Ref. Fig. 001)
3. Description
___________
EFF :
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Page 1
Feb 01/96
IAC
Fittings
Figure 001
EFF :
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Page 2
Feb 01/96
IAC
FITTINGS - TRIMMABLE HORIZONTAL STABILIZER - REMOVAL/INSTALLATION
_________________________________________________________________
TASK 53-56-11-000-001
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 401
Aug 01/06
R
IAC
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-56-11-865-050
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
105VU FLT CTL/SEC1/STBY SPLY 22CE B01
121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20
121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19
121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17
121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
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Feb 01/07
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-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
Subtask 53-56-11-010-050
B. Get Access
(1) Put the THS to the zero position (Ref. TASK 27-41-00-220-003).
(2) Put the warning notice in position to tell persons not to operate the
flight controls.
(6) Open the trailing edge panels 334AB, 344AB, 334AT, 344AT (Ref. TASK
55-13-11-000-001).
4. Procedure
_________
EFF :
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Feb 01/07
IAC
Trimmable Horizontal Stabilizer-Fittings
Figure 401/TASK 53-56-11-991-001- 12 (SHEET 1)
R
EFF :
001-012, 014-099, 53-56-11
Page 404
May 01/06
IAC
Trimmable Horizontal Stabilizer-Fittings
Figure 401/TASK 53-56-11-991-001- 22 (SHEET 2)
R
EFF :
001-012, 014-099, 53-56-11
Page 405
May 01/06
IAC
Trimmable Horizontal Stabilizer-Fittings
Figure 401A/TASK 53-56-11-991-001-A12 (SHEET 1)
R
EFF :
101-199, 901-999, 53-56-11
Page 406
Feb 01/07
IAC
Trimmable Horizontal Stabilizer-Fittings
Figure 401A/TASK 53-56-11-991-001-A22 (SHEET 2)
R
EFF :
101-199, 901-999, 53-56-11
Page 407
Feb 01/07
IAC
**ON A/C 001-012, 014-099,
Subtask 53-56-11-020-050
NOTE : The removal procedures given are for the left Support Fittings.
____
The removal procedures for the right Support Fittings are almost
the same.
(a) If the bolt (16) is safetied with a STA-LOK nut (Ref. TASK 20-22-
00-000-001):
1
_ Use the TOOL - EXTRACTION, TAB WASHERS STA-LOK NSA5454 (SL90-
314-4375) and remove the tab washer (35) with the spring ring
(36).
2
_ Use the WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 (SL90-
374-4375) and remove the slotted nut (14) from the bolt (16).
3
_ Remove the bush (15) and the bolt (16).
1
_ Remove and discard the cotter pin (43).
2
_ Remove the locking cap (42), the nut (41) and the washer (40).
3
_ Remove the bush (15) and the bolt (16).
(a) Put the distance struts in position between the left and the
right upper and lower cross beam sections at FR77.
NOTE : Make sure the sleeve (18) is not loaded, turn the movable
____
spindle unit to make any necessary adjustments.
R
EFF :
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Page 408
Aug 01/06
IAC
(4) Install the EXTRACTOR - CENTERING BUSH, THS (98D27407505000) and
remove the sleeve (18).
(a) Open the closed edges of the lockwasher (2) and the tabwasher
(7).
(b) Remove the nut (1) and remove and discard the lockwasher (2).
(e) Remove the nut (30), the screw (28) and the washers (29).
(j) Remove the retaining ring (3) and the sleeve (6).
(a) Open the closed edges of the lockwasher (2) and the tabwasher
(7).
(b) Remove the nut (1) and remove and discard the lockwasher (2).
(e) Remove the nut (30), the screw (28) and the washers (29).
R
EFF :
001-012, 014-099, 53-56-11
Page 409
Aug 01/06
IAC
(h) Remove the nut (9) and the washer (11).
(j) Remove the retaining ring (3) and the washer (21).
(k) Carefully pull the sleeve (6) out of the link assembly and remove
the bushes (20) and the washer (21).
(b) Remove the nut (25), the bolt (24) and the washers (10).
Subtask 53-56-11-020-050-A
NOTE : The removal procedures given are for the left Support Fittings.
____
The removal procedures for the right Support Fittings are almost
the same.
(2) Remove the locking cap (42), the nut (41) and the washer (40).
(a) Put the distance struts in position between the left and the
right upper and lower cross beam sections at FR77.
EFF :
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IAC
(c) Attach the adapter to the horizontal stabilizer and to the
distance strut.
(d) Make sure that there is no load on sleeve (18). Turn the movable
spindle unit to make all necessary adjustments.
(a) Open the closed edges of the lockwasher (2) and the tabwasher
(7).
(b) Remove the nut (1) and remove and discard the lockwasher (2).
(e) Remove the nut (30), the screw (28) and the washers (29).
(j) Remove the retaining ring (3) and the sleeve (6).
(a) Open the closed edges of the lockwasher (2) and the tabwasher
(7).
(b) Remove the nut (1) and remove and discard the lockwasher (2).
R
EFF :
101-199, 901-999, 53-56-11
Page 411
Feb 01/07
IAC
(e) Remove the nut (30), the screw (28) and the washers (29).
(j) Remove the retaining ring (3) and the washer (21).
(k) Carefully pull the sleeve (6) out of the link assembly and remove
the bushes (20) and the washer (21).
(b) Remove the nut (25), the bolt (24) and the washers (10).
R
EFF :
101-199, 901-999, 53-56-11
Page 412
Feb 01/07
IAC
R **ON A/C ALL
TASK 53-56-11-400-001
R WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
R START A TASK ON OR NEAR:
R - THE FLIGHT CONTROLS
R - THE FLIGHT CONTROL SURFACES
R - THE LANDING GEAR AND THE RELATED DOORS
R - COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
R
R Self Explanatory
EFF :
ALL 53-56-11
Page 413
May 01/06
IAC
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
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Page 414
May 01/06
IAC
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-56-11
Page 415
Feb 01/07
IAC
**ON A/C ALL
3. __________
Job Set-up
Subtask 53-56-11-860-050
(1) Make sure that the aircraft is in the same configuration as for the
removal task.
(2) Make sure that the warning notice is in position to tell persons not
to move the flight controls.
Subtask 53-56-11-865-052
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02
105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01
105VU FLT CTL/SEC1/STBY SPLY 22CE B01
121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20
121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19
121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17
121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
4. Procedure
_________
EFF :
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Page 416
Feb 01/07
R
IAC
R **ON A/C 101-199, 901-999,
Subtask 53-56-11-914-050
(1) Remove the sealant from the links with a non-metallic scraper.
(2) Clean the links, component interface and the adjacent area with
CLEANING AGENTS (Material No. 11-026).
(4) Apply COMMON GREASE (Material No. 04-004) to the new O-rings (31) and
put them in position in the sleeve (18).
(5) Apply COMMON GREASE (Material No. 04-004) to the bushes (4), the
sleeves (6), the Y-bolt (17), the sleeve (18), the bushes (20), the
washers (21) and the bolt (24).
Subtask 53-56-11-420-050
NOTE : The installation procedures given are for the left Support
____
Fittings. The installation procedures for the right Support
Fittings are almost the same.
(3) Apply the SEALANTS (Material No. 09-013) to the surfaces of the
spacer (13) and the washers (10).
EFF :
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Feb 01/07
IAC
(4) Install one of the washers (10) on the bolt (24) and push the bolt
(24) through:
- the link (19), the spacer (13) the link (23).
(5) Install the washer (10) and the nut (25). Do not tighten the nut.
(c) Install the washer (21) and the retaining ring (3).
(a) Install the bushes (4) in the links (19) and (23).
(8) Apply the SEALANTS (Material No. 09-013) to the new tab-washers (7).
(10) Install the washers (11), the nuts (9) and the new cotter pins (12).
(11) Install the bolts (5), the cupwashers (22) and the new lockwashers
(2).
(13) TORQUE the nuts (1) to between 4.5 and 5.5 m.daN (33.18 and 40.56
lbf.ft) with the HOOK WRENCH - ADAPTER (98AMS172327000).
(14) Safety the bolts (5) and the sleeves (6) with the tab-washers (7).
(15) TORQUE the nut (25) to between 5.5 and 6.6 m.daN (40.56 and 48.67
lbf.ft).
(16) Safety the nut (25) with a new cotter pin (26).
EFF :
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Page 418
Aug 01/06
R
IAC
(19) Install the Y-bolt (17).
(a) If the bolt (16) is safetied with a STA-LOK nut (Ref. TASK 20-22-
00-400-001):
1
_ Install the slotted nut (14) on the bolt (16).
2
_ Use the WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 (SL90-
374-4375) and TORQUE the slotted nut (14) to between 2.00 and
3.00 m.daN (14.74 and 22.12 lbf.ft).
3
_ Use the TOOL - INSTALLATION, TAB-WASHERS STA-LOK NSA5454
(SL90-313-4375) and install the tab-washer (35) with the
spring ring (36) on the slotted nut (14).
4
_ Make sure that the distance between the lower side of the bolt
head and the bracket is between 3.8 mm (0.1496 in.) and 5.4 mm
(0.2125 in.).
(Ref. Fig. 401/TASK 53-56-11-991-001)
5
_ Make sure that the distance between the slotted nut (14) and
the bracket is a minimum of 1.7 mm (0.0669 in.).
(Ref. Fig. 401/TASK 53-56-11-991-001)
1
_ Install the washer (40) and the nut (41) on the bolt (16).
2
_ TORQUE the nut (41) to between 2.00 and 3.00 m.daN (14.74 and
22.12 lbf.ft).
3
_ Install the locking cap (42) with a new cotter pin (43).
4
_ Make sure that the distance between the lower side of the bolt
head and the bracket is between 3.8 mm (0.1496 in.) and 5.4 mm
(0.2125 in.).
(Ref. Fig. 401/TASK 53-56-11-991-001)
5
_ Make sure that the distance between the washer (40) and the
bracket is a minimum of 1.7 mm (0.0669 in.).
(Ref. Fig. 401/TASK 53-56-11-991-001)
EFF :
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Page 419
Aug 01/06
R
IAC
(21) Put the bonding jumpers (27) in position and install the screws (28),
the washers (29) and the nuts (30) (Ref. TASK 20-28-00-912-004).
(22) Lubricate the bolts (5) and the Y-bolt (17) (Ref. TASK 12-22-53-640-
001).
(24) Apply the STORAGE PRESERVATION (Material No. 15-007) to the cadmium
plated parts (Ref. TASK 51-75-13-916-002).
Subtask 53-56-11-420-050-A
NOTE : The installation procedures given are for the left Support
____
Fittings. The installation procedures for the right Support
Fittings are almost the same.
(3) Apply the SEALANTS (Material No. 09-013) to the surfaces of the
spacer (13) and the washers (10).
(4) Install one of the washers (10) on the bolt (24) and push the bolt
(24) through:
- the link (19), the spacer (13) and the link (23).
(5) Install the washer (10) and the nut (25). Do not tighten the nut.
(c) Install the washer (21) and the retaining ring (3).
EFF :
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Feb 01/07
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(7) Install the lower floating-bearing assembly:
(a) Install the bushes (4) in the links (19) and (23).
(8) Apply the SEALANTS (Material No. 09-013) to the new tabwashers (7).
(10) Install the washers (11), the nuts (9) and the new cotter pins (12).
(11) Install the bolts (5), the cupwashers (22) and the new lockwashers
(2).
(13) TORQUE the nuts (1) to between 4.5 and 5.5 m.daN (33.18 and 40.56
lbf.ft) with the HOOK WRENCH - ADAPTER (98AMS172327000).
(14) Safety the bolts (5) and the sleeves (6) with the tab-washers (7).
(15) TORQUE the nut (25) to between 5.5 and 6.6 m.daN (40.56 and 48.67
lbf.ft).
(16) Safety the nut (25) with a new cotter pin (26).
(20) Make sure that the Y-bolt (identified with an L) is installed on
the left side and the Y-bolt (identified with an R) is installed on
the right side.
(22) Install the washer (40) and the nut (41) on the bolt (16).
(23) TORQUE the nut (41) to between 2.00 and 3.00 m.daN (14.74 and 22.12
lbf.ft).
(24) Install the locking cap (42) with a new cotter pin (43).
R
EFF :
101-199, 901-999, 53-56-11
Page 421
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(25) Make sure that the distance between the lower side of the bolt head
and the bracket is between 3.8 mm (0.1496 in.) and 5.4 mm (0.2125
in.).
(Ref. Fig. 401A/TASK 53-56-11-991-001-A)
(26) Make sure that the minimum distance between the washer (40) and the
bracket is 1.7 mm (0.0669 in.).
(Ref. Fig. 401A/TASK 53-56-11-991-001-A)
(27) Put the bonding jumpers (27) in position and install the screws (28),
the washers (29) and the nuts (30) (Ref. TASK 20-28-00-912-004).
(28) Lubricate the bolts (5) and the Y-bolt (17) (Ref. TASK 12-22-53-640-
001).
(30) Apply the STORAGE PRESERVATION (Material No. 15-007) to the cadmium
plated parts (Ref. TASK 51-75-13-916-002).
5. Close-up
________
Subtask 53-56-11-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Close the trailing edge panels 334AB, 344AB, 334AT, 344AT (Ref. TASK
55-13-11-400-001).
(8) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
R
EFF :
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Page 422
Aug 01/06
IAC
Subtask 53-56-11-865-051
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
15CE1, 15CE2, 16CE1, 16CE2, 19CE1, 19CE2, 19CE3, 20CE1, 20CE2, 21CE1,
21CE2, 21CE3, 22CE.
EFF :
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IAC
TAIL CONE (APU COMPARTMENT) - DESCRIPTION AND OPERATION
_______________________________________________________
1. _______
General
The tail cone is made of aluminum alloy, and makes up the rear part of the
fuselage from FR78 to FR86.
2. Component
__________________
Location
(Ref. Fig. 001)
3. Description
___________
A. General
The tail cone is made of frames, stringers and skin plates which are
riveted together. The access door beams and the support struts increase
its structural strength. The tail cone has an inspection compartment and
an Auxiliary Power Unit (APU) compartment. You can remove the tail cone
from the aircraft as a single unit. It is not pressurized during flight.
B. Component Description
(1) Fittings
The tail cone has:
- four main attachment fittings, with two diagonal support struts,
installed on the forward frame FR78. These fittings connect the
tail cone to the fuselage,
- two framework fittings on the forward frame FR78. These permit the
inspection of the horizontal stabilizer bearings with the tail cone
installed,
- a fail-safe fitting on the top side of the forward frame FR78. This
takes the load if one of the main attachment fittings fail,
- seven APU attachment fittings for the installation of the APU and
its related equipment,
- hoisting points for the removal and installation of the tailcone.
(2) Firewalls
The APU compartment is a specified fire zone and firewalls close the
compartment on all sides. The firewalls are made of titanium sheets.
The firewalls have cutouts for the APU related components and
equipment.
EFF :
ALL 53-58-00
Page 1
Feb 01/96
IAC
Tail Cone - Component Location
Figure 001
EFF :
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Page 2
Feb 01/96
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(4) Maintenance and Access Doors
A maintenance door (314AR) and two access doors (315AL and 316AR) are
installed in the lower surface of the tailcone. They give access to
the APU and its related components.
EFF :
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Page 3
Feb 01/96
IAC
TAIL CONE - REMOVAL/INSTALLATION
________________________________
TASK 53-58-11-000-006
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-58-11
Page 401
May 01/08
IAC
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-58-11
Page 402
Feb 01/07
IAC
3. __________
Job Set-up
Subtask 53-58-11-864-052
A. Depressurize the Green, Yellow and Blue hydraulic systems (Ref. TASK 29-
10-00-864-001), (Ref. TASK 29-10-00-864-002), (Ref. TASK 29-10-00-864-
003).
Subtask 53-58-11-865-052
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU APU/FUEL/BLOW OFF/PUMP 2QC B14
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
49VU AUTO FLT/FAC1/28VDC 5CC1 B04
49VU AUTO FLT/FAC1/26VAC 14CC1 B03
EFF :
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Page 403
Feb 01/07
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-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
121VU AUTO FLT/FAC2/28VDC 5CC2 M19
121VU AUTO FLT/FAC2/26VAC 14CC2 M18
121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19
121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17
121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
Subtask 53-58-11-865-054
-------------------------------------------------------------------------------
PANEL SERVICE IDENT. LOCATION
-------------------------------------------------------------------------------
2001VU LIGHT APU 2LJ D08
Subtask 53-58-11-581-054
EFF :
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Page 404
Feb 01/07
R
IAC
Subtask 53-58-11-010-056
E. Get Access
(2) Put the warning notice in position to tell persons not to operate the
flight controls.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
WARNING : LOCK THE MECHANISM OF THE ACCESS DOOR 316AR WITH THE PIP
_______
PIN WHEN YOU OPEN THE ACCESS DOOR. THIS WILL PREVENT
INJURY.
4. Procedure
_________
EFF :
ALL 53-58-11
Page 405
Feb 01/07
IAC
Electrical Harnesses
Figure 401/TASK 53-58-11-991-008
EFF :
001-012, 014-019, 53-58-11
Page 406
Feb 01/96
IAC
Electrical Harnesses
Figure 401A/TASK 53-58-11-991-008-A
R
EFF :
020-099, 101-199, 901-999, 53-58-11
Page 407
Feb 01/07
IAC
Electrical Harnesses APU
Figure 402/TASK 53-58-11-991-009
EFF :
ALL 53-58-11
Page 408
Feb 01/96
IAC
INTENTIONALLY BLANK
53-58-11
Page 409
Feb 01/96
IAC
APU Bleed Air Duct
Figure 403/TASK 53-58-11-991-010- 12 (SHEET 1)
R
EFF :
001-012, 014-099, 901-999, 53-58-11
Page 410
Feb 01/07
IAC
APU Bleed Air Duct
Figure 403/TASK 53-58-11-991-010- 22 (SHEET 2)
R
EFF :
001-012, 014-099, 901-999, 53-58-11
Page 411
Feb 01/07
IAC
R **ON A/C 101-199,
Subtask 53-58-11-020-065
A. Removal:
EFF :
ALL 53-58-11
Page 412
Feb 01/07
IAC
(f) Remove the clamps from the electrical harnesses 4213VB/1M and
4207VB/1M up to FR77.
(g) Remove and discard the lockwire from the firewall seal 7138VC/3E
at the APU firewall FR80.
(i) Remove the clamps from the electrical harness 4210VB/3E between
FR80 thru FR77.
(o) Disconnect the connector 7527VC and remove the clamps up to FR77.
(a) Remove the overheat sensing element 19HF (Ref. TASK 36-22-17-000-
001).
(b) Remove the insulating sleeve (2), the insulation lock sleeve (12)
and the insulating sleeve (11).
(c) Remove the nuts (5), the washers (6) and the bolts (7) and
disconnect the rod assembly (8) from the bleed air duct (13).
(d) Remove the nuts (17), the washers (16), the screws (15) and the
bonding strap (14) from the bleed air duct (13).
(e) Remove the V-clamp (1) and move the bleed air duct (4) forward.
R
EFF :
001-012, 014-099, 901-999, 53-58-11
Page 413
Feb 01/07
IAC
R APU Bleed Air Duct
R Figure 403A/TASK 53-58-11-991-010-A12 (SHEET 1)
R
EFF :
101-199, 53-58-11
Page 414
Feb 01/07
IAC
R APU Bleed Air Duct
R Figure 403A/TASK 53-58-11-991-010-A22 (SHEET 2)
R
EFF :
101-199, 53-58-11
Page 415
Feb 01/07
IAC
Hydraulic Hoses
Figure 404/TASK 53-58-11-991-016
EFF :
ALL 53-58-11
Page 416
Feb 01/07
R
IAC
APU Fuel Line
Figure 405/TASK 53-58-11-991-011
EFF :
ALL 53-58-11
Page 417
Feb 01/07
R
IAC
APU Vent and Drain Valve
Figure 406/TASK 53-58-11-991-012
EFF :
ALL 53-58-11
Page 418
Feb 01/07
R
IAC
Tail Cone Hoisting
Figure 407/TASK 53-58-11-991-013
EFF :
ALL 53-58-11
Page 419
Feb 01/07
R
IAC
Tail Cone Attachment
Figure 408/TASK 53-58-11-991-014
EFF :
ALL 53-58-11
Page 420
Feb 01/07
R
IAC
(f) Remove and discard the air seals (9) and (10) from the bleed air
duct (4).
(g) Put the blanking covers on the open ends of the bleed air ducts.
(3) Disconnect the hydraulic hoses 1102GM, 1103GM, 3102GM and 3103GM:
(Ref. Fig. 404/TASK 53-58-11-991-016)
(a) Put a container below the APU vent and drain valve (87) and
prepare to drain the unwanted fuel.
(b) Remove the cap (86) from the vent and drain valve (87) and
install the ADAPTER - VENT AND DRAIN VALVE, APU (85).
NOTE : Fuel will stay in the APU feed hose (upstream of the drain
____
valve, AFT of FR80) after you drain the fuel from the
drain valve.
(a) Remove the nuts (49), the washers (44) and the bolts (43) and
remove the bonding straps (32), (46) and (53).
(b) Remove and discard the lockwire from the retaining rings (34) and
remove the retaining rings.
R
EFF :
001-012, 014-099, 901-999, 53-58-11
Page 421
Feb 01/07
IAC
(c) Remove the bolts (40), nuts (41) and washers (42) and remove the
clamp (52).
(d) Move the sleeve (54) forward over the shroud (38).
(e) Disconnect the nut (35) from the union (36) and install the SLIDE
CONE - APU FUEL (98D28207510000).
(f) Remove the sleeve (54) and the shroud (38) from the fuel hose
(37).
(g) Remove and discard the O-rings (51) from the shrouds (38) and
(33).
(a) Disconnect the ball-bearing control cable from the APU intake
flap diverter (Ref. TASK 49-16-41-000-001).
(b) Remove the APU air intake flap (Ref. TASK 49-16-43-000-001).
R (a) Attach the SLING - UNIVERSAL, TAIL PLAN to the crane and put the
crane in position.
(b) Remove the self-adhesive discs which cover the tail-cone hoisting
points.
EFF :
001-012, 014-099, 901-999, 53-58-11
Page 422
May 01/08
IAC
(c) Remove the hoisting lugs from the hoisting points and install the
lugs eye end out of the tail cone structure.
(a) Remove the screws (68) and the access covers (69).
(b) Remove the nuts (74), the bolts (75) and the washers (76) and
disconnect the bonding strap (71).
(c) Make sure the tail cone is held by the hoist and that the weight
is not on the attach bolts.
(e) Remove the nuts (72) from the attach bolts (70).
NOTE : Remove the lower attach bolts before you remove the upper
____
attach bolts.
R
EFF :
001-012, 014-099, 901-999, 53-58-11
Page 423
Feb 01/07
IAC
R **ON A/C 101-199,
R Subtask 53-58-11-020-065-A
R A. Removal:
R (Ref. Fig. 401A/TASK 53-58-11-991-008-A, 402/TASK 53-58-11-991-009)
R (f) Remove the clamps from the electrical harnesses 4213VB/1M and
R 4207VB/1M up to FR77.
R (g) Remove and discard the lockwire from the firewall seal 7138VC/3E
R at the APU firewall FR80.
R (i) Remove the clamps from the electrical harness 4210VB/3E between
R FR80 thru FR77.
R (o) Disconnect the connector 7527VC and remove the clamps up to FR77.
R
EFF :
101-199, 53-58-11
Page 424
Feb 01/07
IAC
R (p) Disconnect the cable lugs of the electrical harness 4622VB/3G
R from the terminal block 7508VT and remove the clamps between FR77
R and FR79.
R (a) Remove the overheat sensing element 19HF (Ref. TASK 36-22-17-000-
R 001).
R (b) Remove the insulating sleeve (2), the insulation lock sleeve (12)
R and the insulating sleeve (11).
R (c) Remove the nuts (5), the washers (6) and the bolts (7) and
R disconnect the rod assembly (8) from the bleed air duct (13).
R (d) Remove the nuts (17), the washers (16), the screws (15) and the
R bonding strap (14) from the bleed air duct (13).
R (e) Remove the V-clamp (1) and move the bleed air duct (4) forward.
R (f) Remove and discard the air seal (9) from the bleed air duct (4).
R (g) Put the CAP - BLANKING on the open ends of the bleed air ducts.
R (3) Disconnect the hydraulic hoses 1102GM, 1103GM, 3102GM and 3103GM:
R
EFF :
101-199, 53-58-11
Page 425
Feb 01/07
IAC
R (a) Put a CONTAINER - STAINLESS STEEL, APPLICABLE CAPACITY below the
R APU vent and drain valve (87) and prepare to drain the unwanted
R fuel.
R (b) Remove the cap (86) from the vent and drain valve (87) and
R install the ADAPTER - VENT AND DRAIN VALVE, APU (85).
R NOTE : Fuel will stay in the APU feed hose (upstream of the drain
____
R valve, AFT of FR80) after you drain the fuel from the
R drain valve.
R (a) Remove the nuts (49), the washers (44) and the bolts (43) and
R remove the bonding straps (32), (46) and (53).
R (b) Remove and discard the lockwire from the retaining rings (34) and
R remove the retaining rings.
R (c) Remove the bolts (40), nuts (41) and washers (42) and remove the
R clamp (52).
R (d) Move the sleeve (54) forward over the shroud (38).
R (e) Disconnect the nut (35) from the union (36) and install the SLIDE
R CONE - APU FUEL (98D28207510000).
R (f) Remove the sleeve (54) and the shroud (38) from the fuel hose
R (37).
R (g) Remove and discard the O-rings (51) from the shrouds (38) and
R (33).
R
EFF :
101-199, 53-58-11
Page 426
Feb 01/07
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(6) Remove the APU Air-Intake Flap:
(Ref. Fig. 401A/TASK 53-58-11-991-008-A)
(a) Disconnect the ball-bearing control cable from the APU intake
flap diverter (Ref. TASK 49-16-41-000-001).
R (a) Attach the SLING - UNIVERSAL, TAIL PLAN to the crane and put the
crane in position.
(b) Remove the self-adhesive discs which cover the tail-cone hoisting
points.
(c) Remove the hoisting lugs from the hoisting points and install the
lugs with their eye-ends out of the tail cone structure.
(a) Remove the screws (68) and the access covers (69).
(b) Remove the nuts (74), the bolts (75) and the washers (76) and
disconnect the bonding strap (71).
(c) Make sure that the tail cone is held by the hoist and that the
weight is not on the attach bolts.
(e) Remove the nuts (72) from the attach bolts (70).
EFF :
101-199, 53-58-11
Page 427
May 01/08
IAC
NOTE : Remove the lower attach bolts before you remove the upper
____
attach bolts.
EFF :
101-199, 53-58-11
Page 428
May 01/08
R
IAC
**ON A/C ALL
TASK 53-58-11-400-007
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-58-11
Page 429
May 01/08
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-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-58-11
Page 430
Nov 01/07
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-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 53-58-11
Page 431
Feb 01/07
IAC
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-58-11-864-053
A. Make sure that the Green, Yellow and Blue hydraulic systems are
depressurized (Ref. TASK 29-10-00-864-001), (Ref. TASK 29-10-00-864-002),
(Ref. TASK 29-10-00-864-003).
Subtask 53-58-11-865-053
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU APU/FUEL/BLOW OFF/PUMP 2QC B14
49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11
49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09
49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08
49VU AUTO FLT/FAC1/28VDC 5CC1 B04
49VU AUTO FLT/FAC1/26VAC 14CC1 B03
EFF :
ALL 53-58-11
Page 432
Feb 01/07
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-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
121VU APU/FUEL/BLOW OFF/CTL 1QC K39
121VU APU/FIRE AND OVHT/DET/LOOP B 2WG L44
121VU APU/FIRE AND OVHT/DET/LOOP A 1WG L43
121VU APU/APU/CTL 2KD L42
121VU APU/ECB/SPLY 1KD L41
121VU APU/AUTO/EXTIG/GND/TEST 30WF L40
121VU APU/FIRE/EXTIG/SQUIB/B 2WF L39
121VU APU/FIRE/EXTIG/SQUIB/A 1WF L38
121VU APU/FIRE/LP VALVE/NORM 4WF M42
121VU APU/FIRE/LP VALVE/STBY 3WF M41
121VU APU/FUEL/LP VALVE/CTL 1QF M40
121VU APU/FUEL/LP VALVE/SPLY 2QF M39
121VU APU/FUEL/PUMP/CTL 3QC M38
121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20
121VU AUTO FLT/FAC2/28VDC 5CC2 M19
121VU AUTO FLT/FAC2/26VAC 14CC2 M18
121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19
121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18
121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17
121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16
121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
EFF :
ALL 53-58-11
Page 433
Feb 01/07
R
IAC
Subtask 53-58-11-865-055
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL SERVICE IDENT. LOCATION
-------------------------------------------------------------------------------
2001VU LIGHT APU 2LJ D08
Subtask 53-58-11-869-053
(1) Make sure that the aircraft is in the same configuration as for the
removal task.
(2) Make sure that the warning notice is in position to tell persons not
to move the flight controls.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
4. Procedure
_________
EFF :
ALL 53-58-11
Page 434
Feb 01/07
IAC
**ON A/C 001-012, 014-099, 901-999,
Subtask 53-58-11-210-059
(4) Make sure that the parts retained from the removed component are
clean and in the correct condition.
Subtask 53-58-11-420-052
B. Installation
(c) Attach the sling to the hoisting lugs on the tail cone.
EFF :
ALL 53-58-11
Page 435
May 01/08
IAC
(e) Make sure that the tail cone bearing (67) aligns with the
fuselage spigot (66).
(f) Remove the installation adaptors (77) from the EXTRACTOR - ATTACH
BOLTS, TAIL CONE (98A53407566005) kit and install the adaptors on
the attach bolts (70).
(g) Apply the COMMON GREASE (Material No. 04-004) to the attach bolts
(70).
(h) Install the attach bolts (70) in the upper attach fittings.
(i) Remove the installation adaptors from the upper attach bolts (70)
and install the nuts (72).
(j) Install the attach bolts (70) in the lower attach fittings.
(k) Remove the installation adaptors from the lower attach bolts (70)
and install the nuts (72).
(l) TORQUE the nuts (72) to between 1.40 and 1.75 m.daN (10.32 and
12.90 lbf.ft).
(m) Safety the nuts (72) with the new cotter pins (73).
(n) Apply the STORAGE PRESERVATION (Material No. 15-007) to the bare
threads of the bolts (Ref. TASK 51-75-13-916-002).
EFF :
001-012, 014-099, 901-999, 53-58-11
Page 436
Feb 01/07
IAC
- Apply the zinc chromate putty SPECIAL MATERIALS (Material No.
05-002) to the screws (68).
(p) Put the access covers (69) in position and install and tighten
the screws (68).
(q) Put the bonding straps (71) in position and install and tighten
the nuts (74), the bolts (75) and the washers (76) (Ref. TASK 20-
28-00-912-004).
- Remove the hoisting lugs from the tail cone and apply the zinc
chromate putty SPECIAL MATERIALS (Material No. 05-002) to the
lugs.
(t) Install the hoisting lugs in the hoisting points eye end.
(u) Install the SPECIAL MATERIALS (Material No. 05-052) over the
hoisting points.
(a) Apply the COMMON GREASE (Material No. 04-012) to the new O-rings
(51) and install them on the shrouds (38) and (33).
(b) Install the shroud (38) with the sleeve (54) over the fuel hose
(37).
(c) Remove the SLIDE CONE - APU FUEL and connect the nut (35) to the
fitting (36).
EFF :
001-012, 014-099, 901-999, 53-58-11
Page 437
Feb 01/07
IAC
(d) Tighten the nut (35) (Ref. TASK 20-21-12-911-001) and safety with
the lockwire MISCELLANEOUS (Material No. 19-010).
(e) Slide the sleeve (54) over the shroud (38) and the shroud (33).
(f) Install the retaining springs (34) and safety with the lockwire
MISCELLANEOUS (Material No. 19-018).
(g) Align the shroud (38) with the sleeve (54) and the shroud (33).
Install the clamp (52).
(h) Put the bonding straps (32), (46) and (53) in position. Install
and tighten the bolts (43), the washers (44) and the nuts (49)
(Ref. TASK 20-28-00-912-004).
(a) Remove the blanking covers from the bleed air ducts and install:
- A new air seal (9) and a new air seal (10) in the bleed air
duct (4).
(b) Put the bleed air duct (4) over the bleed air duct (13) and move
it rearward.
(c) Move the bleed air duct (4) forward and align it with the bleed
air duct (3).
(f) Install and tighten the bolts (7), the washers (6) and the nuts
(5).
(g) Make sure that the bleed air duct (4) is correctly aligned and
TORQUE the V-clamp (1) to between 0.46 and 0.57 m.daN (40.70 and
50.44 lbf.in).
(h) Put the bonding strap (14) in position and tighten the screws
(15), the washers (16) and the nuts (17) (Ref. TASK 20-28-00-912-
004).
EFF :
001-012, 014-099, 901-999, 53-58-11
Page 438
Feb 01/07
IAC
(i) Install the overheat sensing element 19HF (Ref. TASK 36-22-17-
400-001).
(j) Install the sleeve (2), the sleeve (11) and the lock sleeve (12).
(6) Connect the hydraulic hoses 1102GM, 1103GM, 3102GM and 3103GM:
(Ref. Fig. 404/TASK 53-58-11-991-016)
(b) Connect the hoses (Ref. TASK 20-21-12-911-001) and paint a red
mark on the connections.
(7) Remove the blanking caps and connect the electrical equipment:
(c) Put the electrical harness 4210VB/3E in position and install and
tighten the clamps.
EFF :
001-012, 014-099, 901-999, 53-58-11
Page 439
Feb 01/07
IAC
(g) Connect the electrical connectors 11WF-A and 12WF-A.
(8) Apply the STORAGE PRESERVATION (Material No. 15-007) to the inside of
the tail cone (Ref. TASK 51-75-13-916-002).
Subtask 53-58-11-420-052-A
B. Installation
EFF :
ALL 53-58-11
Page 440
May 01/08
IAC
R (c) Attach the sling to the hoisting lugs on the tail cone.
R (e) Make sure that the tail cone bearing (67) aligns with the
R fuselage spigot (66).
R (f) Remove the installation adaptors (77) from the EXTRACTOR - ATTACH
R BOLTS, TAIL CONE (98A53407566005) kit and install the adaptors on
R the attach bolts (70).
R (g) Apply the COMMON GREASE (Material No. 04-004) to the attach bolts
R (70).
R (h) Install the attach bolts (70) in the upper attach fittings.
R (i) Remove the installation adaptors from the upper attach bolts (70)
R and install the nuts (72).
R (j) Install the attach bolts (70) in the lower attach fittings.
R (k) Remove the installation adaptors from the lower attach bolts (70)
R and install the nuts (72).
R (l) TORQUE the nuts (72) to between 1.40 and 1.75 m.daN (10.32 and
R 12.90 lbf.ft).
R (m) Safety the nuts (72) with the new cotter pins (73).
R (n) Apply the STORAGE PRESERVATION (Material No. 15-007) to the bare
R threads of the bolts (Ref. TASK 51-75-13-916-002).
EFF :
101-199, 53-58-11
Page 441
Feb 01/07
IAC
R (o) Protective treatment
R 1
_ Apply the zinc chromate putty SPECIAL MATERIALS (Material No.
R 05-002) to the screws (68).
R (p) Put the access covers (69) in position and install and tighten
R the screws (68).
R (q) Put the bonding straps (71) in position and install and tighten
R the nuts (74), the bolts (75) and the washers (76) (Ref. TASK 20-
R 28-00-912-004).
R 1
_ Remove the hoisting lugs from the tail cone and apply the zinc
R chromate putty SPECIAL MATERIALS (Material No. 05-002) to the
R lugs.
R (t) Install the hoisting lugs in the hoisting points with the eye
R ends.
R (u) Apply the SPECIAL MATERIALS (Material No. 05-052) on the hoisting
R points.
EFF :
101-199, 53-58-11
Page 442
Feb 01/07
IAC
R (2) Connect the APU fuel line:
R (Ref. Fig. 405/TASK 53-58-11-991-011)
R (a) Apply the COMMON GREASE (Material No. 04-012) to the new O-rings
R (51) and install them on the shrouds (38) and (33).
R (b) Install the shroud (38) with the sleeve (54) over the fuel hose
R (37).
R (c) Remove the SLIDE CONE - APU FUEL and connect the nut (35) to the
R fitting (36).
R (d) Tighten the nut (35) (Ref. TASK 20-21-12-911-001) and safety it
R with the lockwire MISCELLANEOUS (Material No. 19-018).
R (e) Install the shroud (38) in the sleeve (54). Slide the sleeve (54)
R on the shroud (38) and the shroud (33).
R (f) Install the retaining springs (34) and safety them with the
R lockwire, MISCELLANEOUS (Material No. 19-018).
R (g) Align the shroud (38) with the sleeve (54) and the shroud (33)
R and install the clamp (52).
R (h) Put the bonding straps (32), (46) and (53) in position. Install
R and tighten the bolts (43), the washers (44) and the nuts (49)
R (Ref. TASK 20-28-00-912-004).
R (a) Remove the blanking covers from the bleed air ducts and install a
R new air seal (9) in the bleed air duct (4).
R (b) Put the bleed air duct (4) on the bleed air duct (13) and move it
R rearward.
R (c) Move the bleed air duct (4) forward and align it with the bleed
R air duct (3).
EFF :
101-199, 53-58-11
Page 443
Feb 01/07
IAC
R (e) Put the rod assembly (8) in position.
R (f) Install and tighten the bolts (7), the washers (6) and the nuts
R (5).
R (g) Make sure that the bleed air duct (4) is correctly aligned and
R TORQUE the V-clamp (1) to between 0.46 and 0.57 m.daN (40.70 and
R 50.44 lbf.in).
R (h) Put the bonding strap (14) in position and tighten the screws
R (15), the washers (16) and the nuts (17) (Ref. TASK 20-28-00-912-
R 004).
R (i) Install the overheat sensing element 19HF (Ref. TASK 36-22-17-
R 400-001).
R (j) Install the sleeve (2), the sleeve (11) and the lock sleeve (12).
R (6) Connect the hydraulic hoses 1102GM, 1103GM, 3102GM and 3103GM:
R (Ref. Fig. 404/TASK 53-58-11-991-016)
R (b) Connect the hoses (Ref. TASK 20-21-12-911-001) and paint a red
R mark on the connections.
R (c) Remove the hydraulic fluid leakage if necessary (Ref. TASK 51-78-
R 00-615-002).
R (7) Remove the blanking caps and connect the electrical equipment:
R (Ref. Fig. 401A/TASK 53-58-11-991-008-A, 402/TASK 53-58-11-991-009)
R (a) Make sure that the electrical connectors are clean and in the
R correct condition.
R (d) Put the electrical harness 4210VB/3E in position and install and
R tighten the clamps.
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R (g) Connect the electrical wiring to the switch 8QC.
R (8) Apply the STORAGE PRESERVATION (Material No. 15-007) to the internal
R surfaces of the tail cone (Ref. TASK 51-75-13-916-002).
Subtask 53-58-11-710-052-A
C. Do these Tests:
EFF :
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(2) Do the operational test of the APU fire detection system (Ref. TASK
26-13-00-710-001).
(3) Do the operational test of the APU air-intake flap (Ref. TASK 49-16-
00-710-001).
(4) Do the operational test of the APU fuel system (Ref. TASK 28-22-00-
710-001) and examine the APU fuel line for leaks.
(6) Do the operational test of the APU bleed-air system (Ref. TASK 36-12-
00-710-001).
(7) Do the operational test of the APU compartment lighting (Ref. TASK
33-31-00-710-001).
(8) Do the operational test of the navigation lights (Ref. TASK 33-41-00-
710-001).
Subtask 53-58-11-710-052-B
C. Do these Tests:
(2) Do the operational test of the APU fire detection system (Ref. TASK
26-13-00-710-001).
(3) Do the operational test of the APU air-intake flap (Ref. TASK 49-16-
00-710-003).
(4) Do the operational test of the APU fuel system (Ref. TASK 28-22-00-
710-001) and examine the APU fuel line for leaks.
(6) Do the operational test of the APU bleed-air system (Ref. TASK 36-12-
00-710-001).
EFF :
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(7) Do the operational test of the APU compartment lighting (Ref. TASK
33-31-00-710-001).
(8) Do the operational test of the navigation lights (Ref. TASK 33-41-00-
710-001).
5. Close-up
________
Subtask 53-58-11-410-057
A. Make sure that the work area is clean and clear of tool(s) and other
items.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 53-58-11
Page 447
Feb 01/07
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MISCELLANEOUS (EG : DRAINS) - DESCRIPTION AND OPERATION
_______________________________________________________
1. General
_______
A. Drains
Drains are installed in the cone rear-fuselage structure of the aircraft
at or near to the lowest points in an area. The drains let water and
condensation drain out so that they do not cause corrosion.
2. Component
__________________
Location
(Ref. Fig. 001)
3. ___________
Description
At FR70, a drain pipe near the rear pressure bulkhead lets water and
condensation drain out.
At FR80, a hole in the skin lets water and condensation drain into the drain
mast.
At FR84, two drain holes in the skin let water and condensation drain out.
The airflow removes condensation and water from the drain pipe, drain mast
and drain holes.
In other structures (doors, door frames, stringers, brackets and fittings)
holes are drilled at the lowest points. This makes sure that water and
condensation drain to the drain pipe, drain mast and drain holes.
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Page 1
Feb 01/96
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Cone Rear-Fuselage Drains
Figure 001
EFF :
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Feb 01/96
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MISCELLANEOUS (EG : DRAINS) - INSPECTION/CHECK
______________________________________________
TASK 53-59-00-210-001
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
R
No specific access platform 2.0 m (6 ft. 7 in.)
R No specific 1 PROBE - NON METALLIC, FLEXIBLE
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
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R C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 53-59-00-010-050
A. Get Access
(1) Put the access platform below the drain pipe at FR70.
4. Procedure
_________
Subtask 53-59-00-210-050
R A. Inspection Procedure
R (1) Do the operational check of the single drain pipe aft of the FR70
R from the outside
R
R (a) Clean the area around the drain pipe with a lint-free cotton
R cloth MISCELLANEOUS (Material No. 19-003) and the CLEANING AGENTS
R (Material No. 11-001A).
R
R (b) Use a PROBE - NON METALLIC, FLEXIBLE to make sure that the drain
R pipe is not blocked.
R
R (c) If the drain hole is blocked, you must remove the blockage.
EFF :
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Cone-Rear Fuselage Drains
Figure 601/TASK 53-59-00-991-001
EFF :
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Feb 01/96
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5. Close-up
________
Subtask 53-59-00-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
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Nov 01/03
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R **ON A/C 101-199,
R TASK 53-59-00-210-002
R Operational Check of Rubber Flap Drain Valve at Bulk Cargo Compartment Door
R from Outside
R 1. __________________
Reason for the Job
R 2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R 3. __________
Job Set-up
R Subtask 53-59-00-010-051
R A. Get Access
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R 4. Procedure
_________
R Subtask 53-59-00-280-050
R (1) Clean the area around the drain hole with the clean cloth.
R (3) If the drain hole is blocked, you must remove the blockage.
R (4) Carefully push a nonmetallic probe through the drain hole and make
R sure that the rubber flap moves freely.
R 5. Close-up
________
R Subtask 53-59-00-410-051
R A. Close Access
R (1) Make sure that the work area is clean and clear of tool(s) and other
R items.
EFF :
101-199, 53-59-00
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R Rubber Flap Drain Valve - Bulk Cargo Compartment Door
R Figure 602/TASK 53-59-00-991-002
EFF :
101-199, 53-59-00
Page 607
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