Nammcesa 000034 PDF
Nammcesa 000034 PDF
Nammcesa 000034 PDF
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 54
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54-HIGHLIGHTS Page 1 of 7
REVISION NO. 48 Feb 01/10
CES
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615- 617,
619- 620,
623- 624,
627- 628,
630- 631
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A665-A667,
A672-A674,
A677-A679,
A682-A685,
A687,A689-
A691,A694-
A696,A698,
B600-B601,
B604,B606,
B608,B610,
B613-B614,
B617,B619,
B622-B624,
B627-B629,
B632-B633,
B635-B637,
B640-B645,
B647-B649
54-HIGHLIGHTS Page 3 of 7
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54-HIGHLIGHTS Page 7 of 7
REVISION NO. 48 Feb 01/10
CES
CHAPTER 54
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NACELLES/PYLONS
54-L.E.P. Page 1
Feb 01/10
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CHAPTER 54
__________
NACELLES/PYLONS
TABLE OF CONTENTS
_________________
_______
SUBJECT ________
CH/SE/SU C
_ PAGE ___________
____ EFFECTIVITY
NACELLES/PYLONS - GENERAL
_________________________ 54-00-00
DESCRIPTION AND OPERATION 1 1 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
General 1 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
Nacelles Section 1 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
Pylon 1 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
DESCRIPTION AND OPERATION 2 1 501-509, 511-526
528-599,
General 1 501-509, 511-526
528-599,
Nacelles Section 1 501-509, 511-526
528-599,
Pylon 1 501-509, 511-526
528-599,
_______________
NACELLE SECTION 54-10-00
DESCRIPTION AND OPERATION 1 1 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
General 1 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
Nacelle Section 1 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
DESCRIPTION AND OPERATION 2 1 501-509, 511-526
528-599,
General 1 501-509, 511-526
528-599,
Nacelle Section 1 501-509, 511-526
528-599,
54-CONTENTS Page 1
Feb 01/10
R
CES
CHAPTER 54
__________
NACELLES/PYLONS
TABLE OF CONTENTS
_________________
_______
SUBJECT ________
CH/SE/SU C
_ PAGE ___________
____ EFFECTIVITY
PYLONS
______ 54-50-00
DESCRIPTION AND OPERATION 1 1 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
General 1 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
Description 1 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
Pylon Structure 1 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
Systems 6 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
Compartment 6 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
Ventilation and Drainage 10 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
DESCRIPTION AND OPERATION 2 1 501-509, 511-526
528-599,
General 1 501-509, 511-526
528-599,
Description 1 501-509, 511-526
528-599,
Pylon Structure 1 501-509, 511-526
528-599,
Systems 4 501-509, 511-526
528-599,
Compartment 6 501-509, 511-526
528-599,
Ventilation and Drainage 9 501-509, 511-526
528-599,
_______
PYLONS 54-50-00
54-CONTENTS Page 2
Feb 01/10
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CES
CHAPTER 54
__________
NACELLES/PYLONS
TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ ____ ___________
PAGE EFFECTIVITY
REMOVAL/INSTALLATION 401 ALL
Removal of the Pylons 401 ALL
Installation of the Pylons 448 ALL
_______
PYLONS 54-50-00
INSPECTION/CHECK 601 ALL
General Visual Inspection of the 601 ALL
Pylon Drain System
Flow Check of Individual Drain 609 ALL
Lines of Pylon System
Inspection for Missing Fasteners 618 ALL
on the Pylon Fairing Panels
Detailed Inspection of the CAF4 629 ALL
Sealant in Pylon Cantilever ZONE
A
54-CONTENTS Page 3
Aug 01/09
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CES
CHAPTER 54
__________
NACELLES/PYLONS
TABLE OF CONTENTS
_________________
SUBJECT
_______ CH/SE/SU
________ C
_ ____ EFFECTIVITY
PAGE ___________
Doors 6 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
DESCRIPTION AND OPERATION 2 1 501-509, 511-526
528-599,
Description 1 501-509, 511-526
528-599,
Pylon Box Structure 1 501-509, 511-526
528-599,
Pylon-to-Wing Attach Fitting 1 501-509, 511-526
528-599,
Pylon-to-Engine Attach Fitting 4 501-509, 511-526
528-599,
Pylon Box Components 4 501-509, 511-526
528-599,
Doors 4 501-509, 511-526
528-599,
54-CONTENTS Page 4
Feb 01/10
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CES
CHAPTER 54
__________
NACELLES/PYLONS
TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ ____ ___________
PAGE EFFECTIVITY
Detailed Inspection of 678 ALL
Pylon-to-Wing Attach-Fitting Lugs
at RIB 4
Special Detailed Inspection of 687 ALL
Pylon-to-Wing Forward Attachment
Shackles at RIB4
Detailed Inspection of 698 ALL
Pylon-to-Wing Forward
Attachment-Shackles at RIB 4
Detailed Inspection of Shackles, A606 ALL
Sleeves and Bolts of Pylon-to-Wing
Attachment Fittings at RIB 4
Detailed Inspection of A613 ALL
Pylon-Spigot-Receptacle Upper
Surface, including Fitting Bore
and Upper Spar Surrounding Surface
Detailed Inspection of A622 ALL
Pylon-to-Wing Attach-Fitting Lugs
at RIB 10
Detailed Inspection of A631 ALL
Pylon-to-Wing Aft Attach-Fitting,
Sleeves and Bolts
Detailed Inspection of Pylon, A637 ALL
Lateral Panels, in the Areas of
Fasteners Securing the Supports of
Access Doors, between RIB 5 and
RIB 6, LH/RH
Detailed Inspection of Pylon, A646 ALL
Lateral Panels, at the Edge of
Access Door Cutouts, between RIB 5
and RIB 6, LH/RH
Detailed Inspection of Pylon, A655 ALL
Lateral Panel, in Areas of
Fasteners at Door Cutout Corners,
between RIB 2 and RIB 3, External
Surface, LH/RH
Detailed Inspection of Pylon, A664 ALL
Lower Spar, in Areas of Fasteners
at Junction with Lateral Panel,
between RIB 1 and RIB 4, LH/RH
Detailed Inspection of Pylon, A676 ALL
Upper Spar, in Areas of Fasteners
at Junction with Lateral Panel,
between RIB 4 and RIB 10, LH/RH
Detailed Inspection of Pylon, A686 ALL
Upper Spars, Upper Surface, from
54-CONTENTS Page 5
Aug 01/09
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CES
CHAPTER 54
__________
NACELLES/PYLONS
TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ PAGE ___________
____ EFFECTIVITY
Forward of RIB1 to RIB10
Detailed Inspection of Pylon, A697 ALL
Upper Spar, Lower Surface, Forward
of RIB1
Detailed Inspection of Pylon, B607 ALL
Upper Spar, Lower Surface, between
RIB 2 and RIB 3, RIB 4 and RIB 8
Special Detailed Inspection of B616 ALL
Pylon, Upper Spar, Lower Surface,
between RIB1 and RIB2, RIB3 and
RIB4, RIB8 and RIB10
Detailed Inspection of Pylon, B626 ALL
Pyramid Mating Face with the
Engine Forward Mount Fitting
Detailed Inspection of Pylon, B634 ALL
Engine Aft Attachment Beam Mating
Face with the Engine Aft Mount
Fitting
Special Detailed Inspection of B642 ALL
Pylon-to-Wing Aft
Attachment-Shackles at RIB 10
PYLON-TO-WING ATTACH FITTINGS 54-51-17
REMOVAL/INSTALLATION 401 ALL
Removal of the Pylon-to-Wing 401 ALL
Forward Attach Fitting at RIB4
Installation of Pylon-to-Wing 421 ALL
Forward Attach Fitting at RIB4
Removal of the Pylon-to-Wing Aft 432 ALL
Attach Fitting at RIB10
Installation of the Pylon-to-Wing 440 ALL
Aft Attach Fitting at RIB10
Removal of the Bearing of the 449 ALL
Pylon Rear Attachment at RIB10
Installation of the Bearing of the 455 ALL
Pylon Rear Attachment at RIB10
PYLON-TO-WING ATTACH FITTINGS 54-51-17
INSPECTION/CHECK 601 ALL
Inspection of the Pylon-to-Wing 601 ALL
Forward Attach-Fitting
Inspection of the Pylon-to-Wing 603 ALL
Aft Attach-Fitting
Inspection of the Shackles at RIB4 605 ALL
and the Spigot
Inspection of the Shackles at 628 ALL
RIB10
PYLON-TO-WING ATTACH FITTINGS 54-51-17
54-CONTENTS Page 6
Aug 01/09
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CES
CHAPTER 54
__________
NACELLES/PYLONS
TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ ____ ___________
PAGE EFFECTIVITY
REPAIRS 801 ALL
Replacement of the Bushes of the 801 ALL
Shackles at RIB10
Replacement of the Bushes of the 810 ALL
RIB4 Fittings
Reboring of the RIB4 Fittings 861 ALL
PYLON-TO-ENGINE ATTACH FITTINGS 54-51-18
REMOVAL/INSTALLATION 401 ALL
Removal of the Pylon-to-Engine Aft 401 ALL
Attach-Fittings
Installation of the 408 ALL
Pylon-to-Engine Aft
Attach-Fittings
DOORS 54-51-21
REMOVAL/INSTALLATION 401 ALL
Removal of the Pylon Lateral 401 ALL
Access-Doors
Installation of the Pylon Lateral 408 ALL
Access-Doors
MISCELLANEOUS 54-51-29
REMOVAL/INSTALLATION 401 ALL
Removal of the Hoisting Fitting 401 ALL
Installation of the Hoisting 409 ALL
Fitting
BALL JOINT - SPIGOT 54-51-41
REMOVAL/INSTALLATION 401 ALL
Removal of the Spigot Ball Joint 401 ALL
Installation of the Spigot Ball 432 ALL
Joint
54-CONTENTS Page 7
Feb 01/10
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CES
CHAPTER 54
__________
NACELLES/PYLONS
TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ ____ ___________
PAGE EFFECTIVITY
DEACTIVATION/REACTIVATION 401 ALL
Deactivation of the 401 ALL
Pressure-Relief Doors
Refer to the CDL TASK: 54-3 401 ALL
Reactivation of the 409 ALL
Pressure-Relief Doors
Refer to the CDL TASK: 54-3 409 ALL
54-CONTENTS Page 8
Feb 01/10
R
CES
CHAPTER 54
__________
NACELLES/PYLONS
TABLE OF CONTENTS
_________________
SUBJECT
_______ CH/SE/SU
________ C
_ PAGE EFFECTIVITY
____ ___________
403-499, 501-509
511-526, 528-599
CANTILEVER STRUCTURE 54-52-12
REPAIRS 801 ALL
Replacement of the Cantilever 801 ALL
54-CONTENTS Page 9
Feb 01/10
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CES
CHAPTER 54
__________
NACELLES/PYLONS
TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ PAGE EFFECTIVITY
____ ___________
Access Panels 101-149, 151-199
201-233, 236-238
301-306, 401-499
Removal of the Pylon-to-Wing 420 234-235, 239-249
Access Panels 251-299, 307-399
501-509, 511-526
528-599,
Installation of the Pylon-to-Wing 425 234-235, 239-249
Access Panels 251-299, 307-399
501-509, 511-526
528-599,
SKIN PANELS AND DOORS 54-53-11
INSPECTION/CHECK 601 ALL
Detailed Inspection of the 601 ALL
Pressure Relief Door
54-CONTENTS Page 10
Feb 01/10
R
CES
CHAPTER 54
__________
NACELLES/PYLONS
TABLE OF CONTENTS
_________________
_______
SUBJECT CH/SE/SU
________ C
_ PAGE EFFECTIVITY
____ ___________
Aft Fixed Fairing 528-599,
SKIN PANELS - AFT FIXED FAIRING 54-54-11
CLEANING/PAINTING 701 ALL
Cleaning of the Skin Panels of the 701 ALL
Aft Fixed Fairing
SEAL - AFT FIXED FAIRING 54-54-41
REPAIRS 801 ALL
Replacement of the Aft Fixed 801 ALL
Fairing Seal.
54-CONTENTS Page 11
Feb 01/10
R
CES
CHAPTER 54
__________
NACELLES/PYLONS
TABLE OF CONTENTS
_________________
SUBJECT
_______ CH/SE/SU
________ C
_ PAGE EFFECTIVITY
____ ___________
201-249, 251-299
301-399, 401-499
Description 1 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
DESCRIPTION AND OPERATION 2 1 501-509, 511-526
528-599,
Description 1 501-507,
Description 1 508-509, 511-526
528-599,
54-CONTENTS Page 12
Feb 01/10
R
CES
CHAPTER 54
__________
NACELLES/PYLONS
TABLE OF CONTENTS
_________________
_______
SUBJECT ________
CH/SE/SU C
_ PAGE ___________
____ EFFECTIVITY
PYLON-TO-NACELLE JUNCTION 54-57-00
DESCRIPTION AND OPERATION 1 1 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
Description 1 001-049, 051-099
101-149, 151-199
201-249, 251-299
301-399, 401-499
DESCRIPTION AND OPERATION 2 1 501-509, 511-526
528-599,
Description 1 501-509, 511-526
528-599,
FITTINGS 54-57-17
REMOVAL/INSTALLATION 401 ALL
Removal of the Fittings at RIB1 401 ALL
Installation of the Fittings at 410 ALL
RIB1
Removal of the Thrust Reverser 416 501-509, 511-526
Cowl Fitting at RIB3 528-599,
Installation of the Thrust 420 501-509, 511-526
Reverser Cowl Fitting at RIB3 528-599,
Removal of the Thrust Reverser 423 001-049, 051-099
Cowl Fitting at RIB 1 and RIB 2 101-149, 151-199
201-249, 251-299
301-399, 401-499
Installation of the Thrust 427 001-049, 051-099
Reverser Cowl Fitting at RIB 1 and 101-149, 151-199
RIB 2 201-249, 251-299
301-399, 401-499
SEALING 54-57-22
REMOVAL/INSTALLATION 401 ALL
Removal of the Apron Assemblies 401 ALL
Installation of the Apron 411 ALL
Assemblies
Removal of the Profiles 416 501-509, 511-526
528-599,
Installation of the Profiles 419 501-509, 511-526
528-599,
SEALING 54-57-22
INSPECTION/CHECK 601 501-509, 511-526
528-599,
Inspection of the Pylon-to-Nacelle 601 501-509, 511-526
Fairing 528-599,
54-CONTENTS Page 13
Feb 01/10
R
CES
NACELLES/PYLONS - GENERAL - DESCRIPTION AND OPERATION
_____________________________________________________
1. General
_______
A. Nacelles Section
54-10-00 Nacelle Section.
B. Pylon
54-50-00 Pylons
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-00-00
Page 1
Config-1 Nov 01/08
CES
NACELLES/PYLONS - GENERAL - DESCRIPTION AND OPERATION
_____________________________________________________
1. General
_______
A. Nacelles Section
54-10-00 Nacelle Section.
B. Pylon
54-50-00 Pylons.
R
EFF :
501-509, 511-526, 528-599, 54-00-00
Page 1
Config-2 Feb 01/10
CES
NACELLE SECTION - DESCRIPTION AND OPERATION
___________________________________________
1. General
_______
A. Nacelle Section
71-10-00 Cowling
78-30-00 Thrust Reverser
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-10-00
Page 1
Config-1 Nov 01/08
CES
NACELLE SECTION - DESCRIPTION AND OPERATION
___________________________________________
1. General
_______
A. Nacelle Section
71-10-00 Cowling
78-30-00 Thrust Reverser
R
EFF :
501-509, 511-526, 528-599, 54-10-00
Page 1
Config-2 Feb 01/10
CES
PYLONS - DESCRIPTION AND OPERATION
__________________________________
1. _______
General
The purpose of the engine pylon mounted underneath each wing is:
- to support the engine
- to transmit the engine thrust to the aircraft
- to route and support all the systems related to the engine (electrical
wiring, hydraulic and fuel lines up to the engine and all return lines).
2. Description
___________
A. Pylon Structure
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-50-00
Page 1
Config-1 Nov 01/08
CES
Engine Pylon Description
Figure 001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-50-00
Page 2
Config-1 Feb 01/08
CES
Engine Pylon Description
Figure 001A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-50-00
Page 3
Config-1 Nov 01/08
CES
Engine Pylon Stations - Description
Figure 002
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-50-00
Page 4
Config-1 Nov 01/08
CES
(5) Lower fairing
The lower fairing is a removable secondary structure situated between
the pylon box and the engine nozzle.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-50-00
Page 5
Config-1 Nov 01/08
CES
B. Systems
The pylon supports all the following systems related to the engine :
(3) Fuel
(Ref. Fig. 005)
All pylon bottom surfaces adjacent to the nacelle are fire walls.
C. Compartment
(Ref. Fig. 005)
For safety purposes the engine pylon is divided into 7 compartments, each
houses a particular type of equipment
-------------------------------------------------------------------------------
| DESIGNATION | ZONE | SYSTEMS |
|--------------------------------- |----------|-------------------------------|
|Forward | A | Flammable Fluids (Fuel, |
|Fairing | | Hydraulics) |
| | B1 | Bleed Air (High And Low |
| | | Temperatures) |
| | B2 | Electrics |
|----------------------------------|----------|-------------------------------|
|Pylon Box | C | Hydraulics Without Couplings |
| | | Extinguishers |
|----------------------------------|----------|-------------------------------|
|Rearward Secondary | D | Hydraulics |
|Structure | | Limited electrics |
|----------------------------------|----------|-------------------------------|
|Lower Fairing | E | None |
|----------------------------------|----------|-------------------------------|
|Pylon to Wing | F | Fuel (No Couplings) |
|Center Fillets | | Electrics |
| | | Bleed Air (Low Temperature) |
-------------------------------------------------------------------------------
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-50-00
Page 6
Config-1 Nov 01/08
CES
Electrical and Hydraulic Installation
Figure 003
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-50-00
Page 7
Config-1 Nov 01/08
CES
Fire Extinguishing/Detection and Air System Installation
Figure 004
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-50-00
Page 8
Config-1 Nov 01/08
CES
Fuel System and System Segregation through Compartments
Figure 005
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-50-00
Page 9
Config-1 Nov 01/08
CES
D. Ventilation and Drainage
(Ref. Fig. 006)
Each compartment is separately ventilated, separately drained overboard.
The air of each zone is renewed
(1) Compartment A
Air inlet through the edges of the removable panels (not sealed).
Air exit and overboard drain at the trailing edge.
(2) Compartment B1
Air bleed from precooler supply ducting.
Air exit through louvers fitted with an overtemperature detector.
Drain : unsealed structure.
(3) Compartment B2
Vent and drain : unsealed structure.
(4) Compartment C
Air intake incorporated in the access door located on the side of the
pylon between RIBs 2 and 3.
(5) Compartment D
Vent and drain : unsealed structure.
(6) Compartment E
Vent and drain : unsealed structure.
(7) Compartment F
Vented with the wing vent system.
Air exits through a hole in the secondary structure on the side of
the pylon panel between RIBs 5 and 7.
Air exit and overboard drain at the trailing edge.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-50-00
Page 10
Config-1 Nov 01/08
CES
Ventilation and Drainage
Figure 006
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-50-00
Page 11
Config-1 Nov 01/08
CES
PYLONS - DESCRIPTION AND OPERATION
__________________________________
1. _______
General
The purpose of the engine pylon mounted underneath each wing is:
- to support the engine
- to transmit the engine thrust to the aircraft
- to route and support all the systems related to the engine
(electrical wiring, hydraulic and fuel lines up to the engine and all
return lines).
2. ___________
Description
(Ref. Fig. 001, 002)
A. Pylon Structure
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 1
Config-2 Feb 01/10
CES
Engine Pylon Description
Figure 001
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 2
Config-2 Feb 01/10
CES
Engine Pylon Stations - Description
Figure 002
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 3
Config-2 Feb 01/10
CES
B. Systems
The pylon supports all the following systems related to the engine :
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 4
Config-2 Feb 01/10
CES
Electrical and Hydraulic Installation
Figure 003
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 5
Config-2 Feb 01/10
CES
(2) Fire extinguishing/detection and Air System
(Ref. Fig. 004)
(3) Fuel
(Ref. Fig. 005)
All pylon bottom surfaces adjacent to the nacelle are fire walls.
C. Compartment
(Ref. Fig. 005)
For safety purposes the engine pylon is divided into 7 compartments, each
houses a particular type of equipment
-------------------------------------------------------------------------------
| DESIGNATION | ZONE | SYSTEMS |
|--------------------------------- |----------|-------------------------------|
|Forward | A | Flammable Fluids (Fuel, |
|Fairing | | Hydraulics) |
| | B1 | Bleed Air (High And Low |
| | | Temperatures) |
| | B2 | Electrics |
|----------------------------------|----------|-------------------------------|
|Pylon Box | C | Hydraulics Without Couplings |
| | | Fire extinguisher bottles |
|----------------------------------|----------|-------------------------------|
|Rearward Secondary | D | Hydraulics |
|Structure | | Limited electrics |
|----------------------------------|----------|-------------------------------|
|Lower Fairing | E | None |
|----------------------------------|----------|-------------------------------|
|Pylon to Wing | F | Fuel (Zero-leakage Couplings) |
|Center Fillets | | Electrics |
| | | Bleed Air (Low Temperature) |
-------------------------------------------------------------------------------
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 6
Config-2 Feb 01/10
CES
Fire Extinguishing/Detection and Air System Installation
Figure 004
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 7
Config-2 Feb 01/10
CES
Fuel System and System Segregation through Compartments
Figure 005
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 8
Config-2 Feb 01/10
CES
D. Ventilation and Drainage
(Ref. Fig. 006)
Each compartment is separately ventilated, separately drained overboard.
The air of each zone is renewed
(1) Compartment A
Air inlet through the edges of the removable panels (not sealed).
Air exit and overboard drain at the trailing edge.
(2) Compartment B1
Air bleed from precooler supply ducting.
Air exit through louvers fitted with an overtemperature detector.
Drain : unsealed structure.
(3) Compartment B2
Vent and drain : unsealed structure.
(4) Compartment C
Air intake incorporated in the access door located on the side of the
pylon between RIBs 2 and 3.
(5) Compartment D
Vent and drain : unsealed structure.
(6) Compartment E
Vent and drain : unsealed structure.
(7) Compartment F
Vented with the wing vent system.
Air exits through a hole in the secondary structure on the side of
the pylon panel between RIBs 5 and 7.
Air exit and overboard drain at the trailing edge.
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 9
Config-2 Feb 01/10
CES
Ventilation and Drainage
Figure 006
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 10
Config-2 Feb 01/10
CES
PYLONS - REMOVAL/INSTALLATION
_____________________________
TASK 54-50-00-000-001
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 :
ALL 54-50-00
Page 401
Feb 01/10
CES
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-50-00
Page 402
Feb 01/10
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-50-00
Page 403
Feb 01/10
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-50-00
Page 404
Feb 01/10
511-526, 528-599,
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-50-00-941-050
A. Safety Precautions
R (1) Put a warning notice in position to tell persons not to start the
R engine 1(2).
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF :
ALL 54-50-00
Page 405
Feb 01/10
CES
(3) Make sure that the ON legend on the ENG/FADEC GND PWR/1(2) pushbutton
switch is off, and put a warning notice to tell persons not to use
it.
(4) Make sure that the APU BLEED pushbutton switch is released (on legend
OFF) and put a warning notice to tell persons not to use it.
(7) Obey the safety procedure of the hydraulic system (Ref. TASK 29-00-
00-910-002).
Subtask 54-50-00-865-050
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU ENGINE/2/HP FUEL SOV 1KC2 A02
49VU ENGINE/1/HP FUEL SOV 1KC1 A01
49VU ANTI ICE/PROBES/AOA/1 4DA1 D04
49VU ANTI ICE/PROBES/PHC/1 2DA1 D03
49VU ANTI ICE/PROBES/PITOT/1 3DA1 D02
121VU HYDRAULIC/HYD POWER/Y 3803GX N30
122VU ANTI ICE/ENG/2 1DN2 W10
122VU ANTI ICE/PROBES/PHC/3 2DA3 Y16
122VU ANTI ICE/PROBES/2/TAT 1DA2 Y15
122VU ANTI ICE/PROBES/2/PITOT 3DA2 Y14
122VU ANTI ICE/PROBES/2/AOA 4DA2 Y13
R 122VU ANTI ICE/PROBES/PHC/2 2DA2 Y12
122VU ANTI ICE/PROBES/2/STATIC 5DA2 Y11
122VU ANTI ICE/PROBES/3/PITOT 3DA3 Z16
122VU ANTI ICE/PROBES/3/AOA 4DA3 Z15
122VU ANTI ICE/PROBES/1/STATIC 5DA1 Z13
122VU ANTI ICE/PROBES/1/TAT 1DA1 Z12
123VU Y HYD/ELEC/PUMP 3802GX AB06
123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
EFF :
ALL 54-50-00
Page 406
Feb 01/10
CES
Subtask 54-50-00-864-050
Subtask 54-50-00-941-055
D. Get Access
Subtask 54-50-00-869-050
E. Aircraft Stability
Subtask 54-50-00-020-051
(2) Remove the thrust reverser cowl doors (Ref. TASK 78-32-11-000-002):
EFF :
ALL 54-50-00
Page 407
Nov 01/08
CES
(3) Remove the engine (Ref. TASK 71-00-00-000-042).
Subtask 54-50-00-020-051-A
(2) Remove the left thrust-reverser cowl doors (Ref. TASK 78-32-01-000-
010) (Ref. TASK 78-32-02-000-010) (Ref. TASK 78-32-03-000-010)
(Ref. TASK 78-32-04-000-010):
Subtask 54-50-00-020-054
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-50-00
Page 408
Feb 01/10
511-526, 528-599,
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
Subtask 54-50-00-020-054-A
Subtask 54-50-00-020-052
Subtask 54-50-00-020-052-A
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-50-00
Page 409
Feb 01/10
511-526, 528-599,
CES
(4) Put a container in position under the disconnected hydraulic lines.
Subtask 54-50-00-020-053
4. Procedure
_________
Subtask 54-50-00-020-055
(d) Remove and discard the lockwire from the bolts (5).
EFF :
ALL 54-50-00
Page 410
Feb 01/10
CES
Fuel System - Recirculation Check-Valve Junction
Figure 401/TASK 54-50-00-991-001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-50-00
Page 411
Feb 01/08
CES
Fuel System - Recirculation Check-Valve Junction
Figure 401A/TASK 54-50-00-991-001-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-50-00
Page 412
Nov 01/08
CES
Fuel System - Recirculation Check-Valve Junction
Figure 401B/TASK 54-50-00-991-001-B
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 413
Feb 01/10
CES
(e) Remove the bolts (5), the washers (4) and the plates (2) and (1).
(a) Remove the nut (6), the bolts (7) and the bonding braids (5).
(b) Remove the nuts (10), the bolts (9) and the clamps (1).
(e) Remove and discard the lockwire from the connector (12) and the
nuts (2) and (13).
(i) Remove the O-rings (11) and (14) and discard them.
EFF :
ALL 54-50-00
Page 414
Feb 01/10
CES
Fuel System - Pylon-to-Wing Junction
Figure 402/TASK 54-50-00-991-005
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-50-00
Page 415
Feb 01/08
CES
Fuel System - Pylon-to-Wing Junction
Figure 402A/TASK 54-50-00-991-005-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-50-00
Page 416
Nov 01/08
CES
Fuel System - Pylon-to-Wing Junction
Figure 402B/TASK 54-50-00-991-005-B
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 417
Feb 01/10
CES
(3) Removal of the pipe assembly (11):
(Ref. Fig. 403/TASK 54-50-00-991-021)
(b) Remove the bolt (8), the washer (9) and the electrical bonding
(10).
(c) Hold the pipe assembly (11) and remove the three bolts (7), the
washers (6) and the electrical bonding (5).
(d) Remove the pipe assembly (11) from the structure and disconnect
the scavenge pipe (12) from the connection (15).
(e) Remove and discard the O-rings (2) from the pipe (1).
(f) Remove and discard the O-rings (3) from the pipe assembly (11).
(g) Remove and discard the O-rings (14) from the scavenge pipe (12).
Subtask 54-50-00-020-056
(2) Loosen the clamps (22) and (24) and remove the sleeve assembly (23).
EFF :
ALL 54-50-00
Page 418
Feb 01/10
CES
Pipe Assembly
Figure 403/TASK 54-50-00-991-021
EFF :
ALL 54-50-00
Page 419
Aug 01/09
R
CES
Pneumatic System - Bleed Air - Duct Junction
Figure 404/TASK 54-50-00-991-006
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-50-00
Page 420
Feb 01/08
CES
Pneumatic System - Bleed Air - Duct Junction
Figure 404A/TASK 54-50-00-991-006-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-50-00
Page 421
Nov 01/08
CES
Pneumatic System - Bleed Air - Duct Junction
Figure 404B/TASK 54-50-00-991-006-B
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 422
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
401-499,
Subtask 54-50-00-020-057
(1) Disconnect the feeder cables from the right side of the pylon:
(b) Remove the nuts (39), the bolts (41) and the washers (40).
(c) Disconnect the tension regulator cable (32) from the engine
electrical box 401VC.
(e) Remove the nut (46), the washer (47) and the bolt (35).
(f) Disengage the cable (32) with its clamps (31), (36) from the
pylon secondary structure.
(h) Remove the lockwire from the plate (43) and discard it.
(j) Remove the nuts (44) and disconnect the four electrical feeders.
(k) Remove the nuts (51), the washers (52) and the bolts (53).
(l) Disengage the 13 cable supports (54) along the right side of the
pylon secondary structure.
(m) At RIB09, remove the bolts (57), the nuts (55) and disengage the
cable supports (56) from the pylon secondary structure.
(n) Disengage the cables from the pylon and put them on the wing.
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-50-00
Page 423
Feb 01/10
CES
Electrical System - Feeder Cable Installation
Figure 405/TASK 54-50-00-991-012- 12 (SHEET 1)
R
EFF :
ALL 54-50-00
Page 424
Nov 01/07
CES
Electrical System - Feeder Cable Installation
Figure 405/TASK 54-50-00-991-012- 22 (SHEET 2)
R
EFF :
ALL 54-50-00
Page 425
Nov 01/07
CES
(2) Disconnect the electrical connectors at RIB7A:
(a) Remove the bolts (73), the washers (74) and disengage the plate
(61).
1
_ For the left pylon:
411VC, 413VC, 415VC, 417VC, 419VC, 421VC, 423VC.
2
_ For the right pylon:
410VC, 412VC, 414VC, 416VC, 418VC, 420VC, 422VC.
(c) Remove the nut (70), the washer (69), the bolt (64), the washer
(65) and the spacer (66).
(d) Remove the clamps (63), (67), (71) and the washers (68), (72).
(f) Disengage the seven electrical connectors with the plate (61)
from the wing closing rib and put them on the pylon.
(a) Remove the bolts (82) and the bonding strips (81) around the
spigot fitting.
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-50-00
Page 426
Feb 01/10
CES
Electrical System - Connection at RIB7A
Figure 406/TASK 54-50-00-991-013
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-50-00
Page 427
Feb 01/08
CES
Electrical System - Connection at RIB7A
Figure 406A/TASK 54-50-00-991-013-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-50-00
Page 428
Nov 01/08
CES
Electrical System - Connection at RIB7A
Figure 406B/TASK 54-50-00-991-013-B
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 429
Feb 01/10
CES
Electrical System - Wing Closing Rib Connections
Figure 407/TASK 54-50-00-991-014
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-50-00
Page 430
Feb 01/08
CES
Electrical System - Wing Closing Rib Connections
Figure 407A/TASK 54-50-00-991-014-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-50-00
Page 431
Nov 01/08
CES
Electrical System - Wing Closing Rib Connections
Figure 407B/TASK 54-50-00-991-014-B
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 432
Feb 01/10
CES
Spigot at RIB5A - Electrical Bonding
Figure 408/TASK 54-50-00-991-015
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-50-00
Page 433
Feb 01/08
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
Subtask 54-50-00-020-057-A
(1) Disconnect the feeder cables from the right side of the pylon:
(b) Remove the nuts (39), the bolts (41) and the washers (40).
(c) Disconnect the tension regulator cable (32) from the engine
electrical box 401VC.
(e) Remove the nut (46), the washer (47) and the bolt (35).
(f) Disengage the cable (32) with its clamps (31), (36) from the
pylon secondary structure.
(h) Remove the lockwire from the plate (43) and discard it.
(j) Remove the nuts (44) and disconnect the four electrical feeders.
(k) Remove the nuts (51), the washers (52) and the bolts (53).
(l) Disengage the 13 cable supports (54) along the right side of the
pylon secondary structure.
(m) At RIB09, remove the bolts (57), the nuts (55) and disengage the
cable supports (56) from the pylon secondary structure.
(n) Disengage the cables from the pylon and put them on the wing.
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-50-00
Page 434
Feb 01/10
CES
(2) Disconnect the electrical connectors at RIB7A:
(a) Remove the bolts (73), the washers (74) and disengage the plate
(61).
1
_ For the left pylon:
411VC, 413VC, 415VC, 417VC, 419VC, 421VC, 423VC.
2
_ For the right pylon:
410VC, 412VC, 414VC, 416VC, 418VC, 420VC, 422VC.
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-50-00
Page 435
Feb 01/10
CES
(c) Remove the nuts (70), the washers (69), the bolts (64), and the
spacer (66).
(d) Remove the clamps (63), (71) and the washers (68), (72).
(f) Disengage the seven electrical connectors with the plate (61)
from the wing closing rib and put them on the pylon.
(a) Remove the bolts (82) and the bonding strips (81) around the
spigot fitting.
Subtask 54-50-00-480-050
EFF :
ALL 54-50-00
Page 436
Feb 01/10
CES
Spigot at RIB5A - Electrical Bonding
Figure 408A/TASK 54-50-00-991-015-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-50-00
Page 437
Nov 01/08
CES
Spigot at RIB5A - Electrical Bonding
Figure 408B/TASK 54-50-00-991-015-B
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 438
Feb 01/10
CES
Subtask 54-50-00-020-050
NOTE : During removal with the crane of the threaded pins and sleeves,
____
gradually apply a vertical force on the pylon. Apply this force
until it is possible to remove them.
(b) Lock the bolts (101) with a pin wrench of the PYLON REMOVAL-
WRENCH (98D54503000000).
Remove the nuts (105) with a pin wrench of the PYLON REMOVAL-
WRENCH (98D54503000000).
(d) Release the nuts (104), lock the sleeves (100) with a special
wrench and remove the nuts (104) with a pin wrench of the PYLON
REMOVAL-WRENCH (98D54503000000).
(f) Remove the sleeves (100) with the extractor PYLON SHAFT EXTRACTOR
RIB4-RIB10 (98D54003005000).
EFF :
ALL 54-50-00
Page 439
Feb 01/10
CES
Pylon-to-Wing Aft Attach Fitting
Figure 409/TASK 54-50-00-991-020
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-50-00
Page 440
Nov 01/08
CES
Pylon-to-Wing Aft Attach Fitting
Figure 409A/TASK 54-50-00-991-020-A
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 441
Feb 01/10
CES
(2) Remove the forward threaded pins and sleeves at RIB4:
(b) Lock the bolt (91) with a pin wrench of the PYLON REMOVAL-WRENCH
(98D54503000000) and remove the nut (95) with a pin wrench of the
PYLON REMOVAL-WRENCH (98D54503000000).
(d) Release the nut (94), lock the sleeve (92) with a special wrench
and remove the nut (94) with a pin wrench of the PYLON REMOVAL-
WRENCH (98D54503000000).
(f) Remove the sleeve (92) with the extractor PYLON SHAFT EXTRACTOR
RIB4-RIB10 (98D54003005000). Remove the sleeve at the bottom
first.
Subtask 54-50-00-020-058
(1) Lower the pylon and move it away from the wing with the crane.
EFF :
ALL 54-50-00
Page 442
Feb 01/10
CES
(5) Attach the BEAM-LIFTING AT RIB4 (98D54003003001) to the GEAR-HOISTING
PYLON (98D54003002000), attach it to the pylon with the crane and
remove the TROLLEY-PYLON R I (98D54003000000) from the pylon.
EFF :
ALL 54-50-00
Page 443
Feb 01/10
CES
Pylon-to-Wing Forward Attach Fitting
Figure 410/TASK 54-50-00-991-019- 12 (SHEET 1)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-50-00
Page 444
Nov 01/08
CES
Pylon-to-Wing Forward Attach Fitting
Figure 410/TASK 54-50-00-991-019- 22 (SHEET 2)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-50-00
Page 445
Nov 01/08
CES
Pylon-to-Wing Forward Attach Fitting
Figure 410A/TASK 54-50-00-991-019-A12 (SHEET 1)
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 446
Feb 01/10
CES
Pylon-to-Wing Forward Attach Fitting
Figure 410A/TASK 54-50-00-991-019-A22 (SHEET 2)
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 447
Feb 01/10
CES
TASK 54-50-00-400-001
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
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-50-00
Page 448
Feb 01/10
CES
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
EFF :
ALL 54-50-00
Page 449
Feb 01/08
CES
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-50-00
Page 450
Nov 01/08
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-50-00
Page 451
Feb 01/10
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-50-00
Page 452
Feb 01/10
511-526, 528-599,
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-50-00
Page 453
Feb 01/10
511-526, 528-599,
CES
R **ON A/C ALL
3. __________
Job Set-up
Subtask 54-50-00-941-056
A. Safety Precautions
(1) Make sure that the engine (1) and (2) shutdown occurred not less than
5 minutes before you do this procedure.
(2) Make sure that a warning notice in position is in the cockpit to tell
persons not to start engine.
(3) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton
switch is off, and put a warning notice to tell persons not to use
it.
(4) Make sure that the APU BLEED pushbutton switch is released (on legend
OFF) and install a warning notice to tell persons not to use it.
(5) Make sure that the fuel safety procedure instructions are obeyed
(Ref. TASK 28-00-00-910-001).
(6) Make sure that the hydraulic safety procedure instructions are obeyed
(Ref. TASK 29-00-00-910-002).
(9) Make sure that the hydraulic reservoirs are depressurized (Ref. TASK
29-14-00-614-001).
(10) Make sure that the aircraft is stable (Ref. TASK 05-57-00-200-001).
EFF :
ALL 54-50-00
Page 454
Nov 01/07
CES
Subtask 54-50-00-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU ENGINE/2/HP FUEL SOV 1KC2 A02
49VU ENGINE/1/HP FUEL SOV 1KC1 A01
49VU ANTI ICE/PROBES/AOA/1 4DA1 D04
49VU ANTI ICE/PROBES/PHC/1 2DA1 D03
49VU ANTI ICE/PROBES/PITOT/1 3DA1 D02
121VU HYDRAULIC/HYD POWER/Y 3803GX N30
122VU ANTI ICE/ENG/2 1DN2 W10
122VU ANTI ICE/PROBES/PHC/3 2DA3 Y16
122VU ANTI ICE/PROBES/2/TAT 1DA2 Y15
122VU ANTI ICE/PROBES/2/PITOT 3DA2 Y14
122VU ANTI ICE/PROBES/2/AOA 4DA2 Y13
R 122VU ANTI ICE/PROBES/PHC/2 2DA2 Y12
122VU ANTI ICE/PROBES/2/STATIC 5DA2 Y11
122VU ANTI ICE/PROBES/3/PITOT 3DA3 Z16
122VU ANTI ICE/PROBES/3/AOA 4DA3 Z15
122VU ANTI ICE/PROBES/1/STATIC 5DA1 Z13
122VU ANTI ICE/PROBES/1/TAT 1DA1 Z12
123VU Y HYD/ELEC/PUMP 3802GX AB06
123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
4. Procedure
_________
Subtask 54-50-00-480-051
EFF :
ALL 54-50-00
Page 455
Feb 01/10
CES
R (4) Disengage the pylon from the STORAGE RIG (98D54003001000) with the
BEAM-LIFTING AT RIB4 (98D54003003001) and the GEAR-HOISTING PYLON
(98D54003002000).
Subtask 54-50-00-914-050
(1) Clean the friction surfaces and the spigot ball joint with lint-free
cloth soaked with CLEANING AGENTS (Material No. 11-003).
(2) Apply COMMON GREASE (Material No. 04-004) on the spigot ball joint.
(3) Use the crane to lift in position under the wing the with the pylon
installed on it.
(4) Put the spigot fitting with precaution into its ball joint in the
pylon.
Subtask 54-50-00-420-050
NOTE : If necessary, change the value of the forces you apply to the
____
forward pylon-to-wing attach fitting, to make the installation of
the sleeves easier.
EFF :
ALL 54-50-00
Page 456
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
(a) Apply COMMON GREASE (Material No. 04-004) to the sleeves, the
spigot and all the friction surfaces.
NOTE : Put the nuts, the cotter pins and the lockwashers:
____
- for the upper attachments, in the outer side of the
pylons (always symmetrically to the pylon centerline).
- for the inner attachments, in the inner side of the
pylons (always symmetrically to the pylon centerline).
(e) Install the nut (94). Lock the sleeve (92) with a special wrench
of the PYLON REMOVAL-WRENCH (98D54503000000). TORQUE the nut (94)
to between 4 and 5 m.daN (29.49 and 36.87 lbf.ft). Use a pin
wrench of the PYLON REMOVAL-WRENCH (98D54503000000) and a torque
wrench.
(h) Lock the bolt (91) with a pin wrench of the PYLON REMOVAL-WRENCH
(98D54503000000) and install the nut (95) with a pin wrench of
the PYLON REMOVAL-WRENCH (98D54503000000) .
(i) TORQUE the nut (95) to between 4 and 5 m.daN (29.49 and 36.87
lbf.ft).
(j) Safety the nut (95) with the cotter pin (96).
EFF :
ALL 54-50-00
Page 457
Feb 01/10
CES
(2) Install the aft threaded pins and the sleeves at RIB10:
(b) Apply COMMON GREASE (Material No. 04-004) to the sleeves, the
spigot and all the friction surfaces.
(e) Install the nuts (104). Lock the sleeves (100) with a special
wrench. TORQUE the nuts (104) to between 1 and 12 m.daN (88.49
and 1061.94 lbf.in). Use a pin wrench of the PYLON REMOVAL-WRENCH
(98D54503000000) and a torque wrench.
(h) Lock the bolts (101) with a pin wrench PYLON REMOVAL-WRENCH
(98D54503000000). Install the nuts (105) with a pin wrench of the
PYLON REMOVAL-WRENCH (98D54503000000).
(i) TORQUE the nuts (105) to between 1 and 12 m.daN (88.49 and
1061.94 lbf.in).
(j) Safety the nuts (105) with the cotter pins (106).
EFF :
ALL 54-50-00
Page 458
Feb 01/10
CES
Subtask 54-50-00-420-052
Subtask 54-50-00-420-053
(1) Install the bonding strips (81) and the bolts (82).
EFF :
ALL 54-50-00
Page 459
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
401-499,
Subtask 54-50-00-420-054
NOTE : Do not cross the electrical cables in the pylon during the
____
installation.
(2) Make sure that the electrical connectors are clean and in the correct
condition.
(4) Connection of the electrical feeders on the right side of the pylon
(Ref. Fig. 405/TASK 54-50-00-991-012)
(a) Install the tension regulator cable (32) in the engine electrical
box 401VC.
(b) Install the washers (40), the bolts (41), the nuts (39) and
tighten the nuts (39).
(c) Install the plate (38) on the engine electrical box, install the
bolts (37) and tighten them.
(d) Put the clamp (36) in position on the pylon secondary structure.
(e) Install the washer (47), the bolt (35), the nut (46) and tighten
the nut (46).
(g) Install the washer (33), the bolt (34) and tighten the bolt (34).
(h) Install the four electrical feeders on the plate 400VT (43) with
the nuts (44).
(i) Install the cover (42) and the new corrosion resistant steel
lockwire 0.8 mm (0.32 in.) dia. MISCELLANEOUS (Material No. 19-
010) on this plate.
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-50-00
Page 460
Feb 01/10
CES
(j) Install the 13 cable supports (54) on the pylon secondary
structure with the washers (52), the bolts (53) and the nuts
(51).
(k) At RIB09, install the cable support (56) on the pylon secondary
structure with the bolts (57) and the nuts (55).
(a) For the left pylon, connect the connectors: 471VC, 473VC, 475VC.
(b) For the right pylon, connect the connectors: 470VC, 472VC, 474VC.
(a) Put the assembly electrical cables and plate (61) in position at
the wing closing rib.
(b) Install the washers (74), the bolts (73) and tighten the bolts
(73).
(e) Install the spacer (66), the washer (65) and the clamp (63).
(f) Install the bolt (64), the washer (69) and the nut (70).
1
_ for the left pylon: 411VC, 413VC, 415VC, 417VC, 419VC, 421VC,
423VC.
2
_ for the right pylon: 410VC, 412VC, 414VC, 416VC, 418VC, 420VC,
422VC.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-50-00
Page 461
Feb 01/08
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
Subtask 54-50-00-420-054-A
NOTE : Do not cross the electrical cables in the pylon during the
____
installation.
(2) Make sure that the electrical connectors are clean and in the correct
condition.
(4) Connection of the electrical feeders on the right side of the pylon
(Ref. Fig. 405/TASK 54-50-00-991-012)
(a) Install the tension regulator cable (32) in the engine electrical
box 401VC.
(b) Install the washers (40), the bolts (41), the nuts (39) and
tighten the nuts (39).
(c) Install the plate (38) on the engine electrical box, install the
bolts (37) and tighten them.
(d) Put the clamp (36) in position on the pylon secondary structure.
(e) Install the washer (47), the bolt (35), the nut (46) and tighten
the nut (46).
(g) Install the washer (33), the bolt (34) and tighten the bolt (34).
(h) Install the four electrical feeders on the plate 400VT (43) with
the nuts (44).
(i) Install the cover (42) and the new corrosion resistant steel
lockwire 0.8 mm (0.32 in.) dia. MISCELLANEOUS (Material No. 19-
010) on this plate.
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-50-00
Page 462
Feb 01/10
CES
(j) Install the 13 cable supports (54) on the pylon secondary
structure with the washers (52), the bolts (53) and the nuts
(51).
(k) At RIB09, install the cable support (56) on the pylon secondary
structure with the bolts (57) and the nuts (55).
(a) For the left pylon, connect the connectors: 471VC, 473VC, 475VC.
(b) For the right pylon, connect the connectors: 470VC, 472VC, 474VC.
(a) Put the assembly electrical cables and plate (61) in position at
the wing closing rib.
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-50-00
Page 463
Feb 01/10
CES
(b) Install the washers (74), the bolts (73) and tighten the bolts
(73).
(f) Install the bolts (64), the washers (69) and the nuts (70).
1
_ for the left pylon: 411VC, 413VC, 415VC, 417VC, 419VC, 421VC,
423VC.
2
_ for the right pylon: 410VC, 412VC, 414VC, 416VC, 418VC, 420VC,
422VC.
Subtask 54-50-00-420-058
EFF :
ALL 54-50-00
Page 464
Feb 01/10
CES
**ON A/C ALL
(2) Install the clamp (22), (24) and the sleeve assembly (23).
Subtask 54-50-00-420-059
NOTE : Do an electrical bonding when you install the bolt (7) and the
____
screws (6) (Ref. TASK 20-28-00-912-002).
(1) Remove the blanking plugs from the disconnected line ends.
(d) Connect the pipe assembly (11) to the pipe (1) and connect the
scavenge pipe (12) to the connection (15).
(e) Install the three bolts (7), the three washers (6) and the
electrical bonding (5) to attach the pipe assembly (11) to the
structure.
(f) Install the bolt (13), the electrical bonding (5) and the nut
(4).
EFF :
ALL 54-50-00
Page 465
Feb 01/08
CES
**ON A/C 234-235, 239-249, 251-299, 307-399,
(a) Install the new O-ring (11) and the O-ring (14).
(f) Safety the nuts (2) and (13) with corrosion-resistant steel
lockwire 0.8 mm (0.32 in.) dia. MISCELLANEOUS (Material No. 19-
010).
(i) Install the bonding braids (5), the bolts (7) and the nuts (6)
and tighten the nuts (6).
(j) Install the clamps (1), the bolts (9) and the nut (10) and
tighten the nuts (10).
EFF :
ALL 54-50-00
Page 466
Feb 01/10
CES
**ON A/C 234-235, 239-249, 251-299, 307-399,
NOTE : Do an electrical bonding when you install the bolt (6) and the
____
screws (7) (Ref. TASK 20-28-00-912-002).
(h) Install the bolts (6) and nut (7) and tighten it.
EFF :
ALL 54-50-00
Page 467
Feb 01/10
CES
Subtask 54-50-00-710-050
J. Operational Test
-------------------------------------------------------------------------------
ACTION RESULT
-------------------------------------------------------------------------------
Subtask 54-50-00-420-055
Subtask 54-50-00-420-056
EFF :
ALL 54-50-00
Page 468
Nov 01/08
CES
Subtask 54-50-00-420-057
(2) Install the thrust reverser cowl doors (Ref. TASK 78-32-11-400-002).
Subtask 54-50-00-420-056-A
Subtask 54-50-00-420-057-A
(2) Install the left thrust-reverser cowl door (Ref. TASK 78-32-01-400-
010) (Ref. TASK 78-32-02-400-010):
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-50-00
Page 469
Feb 01/10
511-526, 528-599,
CES
R (b) FOR 1000EM2
R 461AL.
R (3) Install the right thrust-reverser cowl door (Ref. TASK 78-32-03-400-
R 010) (Ref. TASK 78-32-04-400-010):
R (4) Install the fan cowl doors (Ref. TASK 71-13-11-400-010) (Ref. TASK
R 71-13-16-400-010):
Subtask 54-50-00-210-054
(1) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
(b) There are no air leakages at the bleed air duct connections.
EFF :
ALL 54-50-00
Page 470
May 01/08
CES
5. Close-up
________
Subtask 54-50-00-410-050
(a) For the left pylon: 413EL, 471AL, 471BL, 471CL, 472BR, 472AR,
414FR, 414CR, 414AR.
(b) For the right pylon: 424AR, 424CR, 424ER, 482AR, 482BR, 482CR,
423FL, 481AL, 481BL.
Subtask 54-50-00-410-050-A
(a) For the left pylon: 413CL, 413AR, 413CR 471AL, 471BL, 471CL,
471DL 471AR, 471BR, 471CR.
(b) For the right pylon: 423CL, 423AR, 423CR 481AL, 481BL, 481CL
481AR, 481BR, 481CR, 481DR.
EFF :
ALL 54-50-00
Page 471
Feb 01/10
CES
(c) For the left wing: 521BT, 521EB.
Subtask 54-50-00-865-052
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU ENGINE/2/HP FUEL SOV 1KC2 A02
49VU ENGINE/1/HP FUEL SOV 1KC1 A01
49VU ANTI ICE/PROBES/AOA/1 4DA1 D04
49VU ANTI ICE/PROBES/PHC/1 2DA1 D03
49VU ANTI ICE/PROBES/PITOT/1 3DA1 D02
121VU HYDRAULIC/HYD POWER/Y 3803GX N30
122VU ANTI ICE/ENG/2 1DN2 W10
122VU ANTI ICE/PROBES/PHC/3 2DA3 Y16
122VU ANTI ICE/PROBES/2/TAT 1DA2 Y15
122VU ANTI ICE/PROBES/2/PITOT 3DA2 Y14
122VU ANTI ICE/PROBES/2/AOA 4DA2 Y13
R 122VU ANTI ICE/PROBES/PHC/2 2DA2 Y12
122VU ANTI ICE/PROBES/2/STATIC 5DA2 Y11
122VU ANTI ICE/PROBES/3/PITOT 3DA3 Z16
122VU ANTI ICE/PROBES/3/AOA 4DA3 Z15
122VU ANTI ICE/PROBES/1/STATIC 5DA1 Z13
122VU ANTI ICE/PROBES/1/TAT 1DA1 Z12
123VU Y HYD/ELEC/PUMP 3802GX AB06
123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
Subtask 54-50-00-942-050
C. Close Access
(1) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 54-50-00
Page 472
Feb 01/10
CES
PYLONS - INSPECTION/CHECK
_________________________
TASK 54-50-00-200-001
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
-------------------------------------------------------------------------------
No specific flashlight
No specific mirror
No specific warning notice
No specific access platform 1.7 m (5 ft. 7 in.)
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-50-00
Page 601
May 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-50-00-941-051
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-50-00-040-050
EFF :
ALL 54-50-00
Page 602
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-50-00-040-050-A
Subtask 54-50-00-010-051
C. Get Access
Subtask 54-50-00-010-051-A
C. Get Access
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-50-00
Page 603
Feb 01/10
511-526, 528-599,
CES
**ON A/C ALL
4. Procedure
_________
Subtask 54-50-00-210-051
(b) Make sure that the drain inlets are not blocked. Use a flashlight
and a mirror, if necessary.
(c) Examine the lines to make sure that there are no cracks, marks,
corrosion or other damage.
5. Close-up
________
Subtask 54-50-00-440-050
EFF :
ALL 54-50-00
Page 604
Feb 01/10
CES
Pylon Drains
Figure 601/TASK 54-50-00-991-008
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-50-00
Page 605
Aug 01/09
CES
Pylon Drains
Figure 601A/TASK 54-50-00-991-008-A
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 606
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-50-00-440-050-A
Subtask 54-50-00-410-051
B. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-50-00-410-051-A
B. Close Access
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-50-00
Page 607
Feb 01/10
511-526, 528-599,
CES
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-50-00
Page 608
Feb 01/10
CES
R **ON A/C ALL
TASK 54-50-00-200-002
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.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-50-00
Page 609
Aug 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-50-00-941-053
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-50-00-040-051
EFF :
ALL 54-50-00
Page 610
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-50-00-040-051-A
Subtask 54-50-00-010-052
C. Get Access
Subtask 54-50-00-010-052-A
C. Get Access
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-50-00
Page 611
Feb 01/10
511-526, 528-599,
CES
R **ON A/C ALL
4. Procedure
_________
Subtask 54-50-00-210-052
A. Inspection
(Ref. Fig. 602/TASK 54-50-00-991-009)
(a) Pour water in the area of the drain inlets of the line (1),
located on the front upper spar between ribs 3 and 4 and on rear
spar between ribs 6 and 7.
(b) Make sure that the drain inlets are not obstructed and that the
water flows freely.
(c) Make sure that the water flows freely at the outlet of the drain
line (1) located on the lower spar of the forward fairing.
(a) Pour water in the aera of the drain inlet of the drain line (2).
(b) Make sure that the drain inlet is not obstructed and that the
water flows freely.
(c) Make sure that the water flows freely at the outlet of the drain
line (2) located on the lower spar of the forward fairing.
(3) Dry the inspected drain lines and the area of the drain inlets with
compressed air.
Subtask 54-50-00-210-053
EFF :
ALL 54-50-00
Page 612
Aug 01/09
CES
Drain system of Forward Fairing
Figure 602/TASK 54-50-00-991-009
R
EFF :
ALL 54-50-00
Page 613
Aug 01/09
CES
Drain system of Aft lower Fairing
Figure 603/TASK 54-50-00-991-010
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-50-00
Page 614
Aug 01/09
CES
R **ON A/C 501-509, 511-526, 528-599,
(1) Pour water in the drain inlet located on the aft part of the lower
spar.
(2) Make sure that the drain inlet is not obstructed and that the water
flows freely.
(3) Make sure that the water flows freely at the outlet of the drain
line, located on the trailing edge of the lower fairing.
(4) Dry the inspected drain line and the area of the drain inlet inlet
with compressed air.
5. Close-up
________
Subtask 54-50-00-440-051
Subtask 54-50-00-440-051-A
Subtask 54-50-00-410-052
B. Close Access
EFF :
ALL 54-50-00
Page 615
Feb 01/10
CES
Drain system of Aft lower Fairing
Figure 603A/TASK 54-50-00-991-010-A
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 616
Feb 01/10
CES
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-50-00-410-052-A
B. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-50-00
Page 617
Feb 01/10
511-526, 528-599,
CES
R **ON A/C ALL
TASK 54-50-00-200-003
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-50-00
Page 618
Aug 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-50-00-941-057
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
EFF :
ALL 54-50-00
Page 619
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
401-499,
Subtask 54-50-00-040-052
Subtask 54-50-00-040-052-A
Subtask 54-50-00-010-054
C. Get Access
4. Procedure
_________
Subtask 54-50-00-210-055
A. Inspection
EFF :
ALL 54-50-00
Page 620
Feb 01/10
CES
Fairing Panels - Right Pylons
Figure 604/TASK 54-50-00-991-016
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-50-00
Page 621
Aug 01/09
CES
R Fairing Panels - Right Pylons
R Figure 604A/TASK 54-50-00-991-016-B
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-50-00
Page 622
Aug 01/09
CES
R **ON A/C 501-509, 511-526, 528-599,
(a) Panels with one missing fastener permitted, under the following
conditions:
- No missing fastener permitted on the forward edge of the panel.
- At the beginning of each row, the two first fasteners must not
be missing.
5. Close-up
________
Subtask 54-50-00-440-052
EFF :
ALL 54-50-00
Page 623
Feb 01/10
CES
Fairing Panels - Right Pylons
Figure 604B/TASK 54-50-00-991-016-A
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 624
Feb 01/10
CES
Fairing Panels - Left Pylon
Figure 605/TASK 54-50-00-991-017
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-50-00
Page 625
Aug 01/09
CES
R Fairing Panels - Left Pylon
R Figure 605A/TASK 54-50-00-991-017-B
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-50-00
Page 626
Aug 01/09
CES
Fairing Panels - Left Pylon
Figure 605B/TASK 54-50-00-991-017-A
R
EFF :
501-509, 511-526, 528-599, 54-50-00
Page 627
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-50-00-440-052-A
Subtask 54-50-00-410-053
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-50-00
Page 628
Feb 01/10
CES
TASK 54-50-00-220-001
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific flashlight
No specific mirror
No specific warning notice
No specific access platform 1.7 m (5 ft. 7 in.)
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-50-00
Page 629
Aug 01/09
CES
3. __________
Job Set-up
Subtask 54-50-00-941-058
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-50-00-040-053
Subtask 54-50-00-040-053-A
Subtask 54-50-00-010-055
C. Get Access
EFF :
ALL 54-50-00
Page 630
Feb 01/10
CES
4. Procedure
_________
Subtask 54-50-00-220-050
(a) If the volume of the sealant is increased and the sealant breaks
easily, there is contamination by kerozene.
(b) If the volume of the sealant is not changed and its color is
yellow, there is contamination by hydraulic fluid.
(4) If you find contamination, repair the CAF4 sealant (Ref. TASK 54-52-
00-300-001).
5. Close-up
________
Subtask 54-50-00-440-053
Subtask 54-50-00-440-053-A
EFF :
ALL 54-50-00
Page 631
Feb 01/10
CES
CAF4 Sealant - Pylon Cantilever
Figure 606/TASK 54-50-00-991-018
EFF :
ALL 54-50-00
Page 632
Aug 01/09
CES
**ON A/C ALL
Subtask 54-50-00-410-054
B. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-50-00
Page 633
Aug 01/09
CES
PYLON BOX - DESCRIPTION AND OPERATION
_____________________________________
1. Description
___________
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-00
Page 1
Config-1 Nov 01/08
CES
Primary Structure - Materials and Protections Description
Figure 001
R
EFF : 001-049, 051-099, 101-105, 151-199,
201-220, 234-235, 239-249, 251-299, 307-399,
54-51-00
Page 2
Config-1 Nov 01/08
404-499,
CES
Primary Structure - Materials and Protections Description
Figure 001A
R
EFF :
401-403,
106-149, 221-233, 236-238, 301-306, 54-51-00
Page 3
Config-1 Feb 01/08
CES
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
R 401-499,
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-00
Page 4
Config-1 Nov 01/08
CES
Pylon-to-Wing Attach Fittings
Figure 002
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-00
Page 5
Config-1 Nov 01/08
CES
C. Pylon-to-Engine Attach Fitting
E. Doors
(Ref. Fig. 004)
The pylon box is fitted with four doors giving access to the various
systems:
- The forward access doors are located on each side of the pylon box
between RIB2 and RIB3. They are made of light alloy and are attached by
means of four screws.
- The aft access doors are located on each side of the pylon box between
RIB5 and RIB6. They are made of carbon fiber reinforced plastic and
honeycomb web sandwich type and are attached by means of four captive
screws.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-00
Page 6
Config-1 Nov 01/08
CES
Pylon to Engine Attach Fittings
Figure 003
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page 7
Config-1 Feb 01/08
CES
Pylon to Engine Attach Fittings
Figure 003A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page 8
Config-1 Nov 01/08
CES
Doors
Figure 004
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-00
Page 9
Config-1 Nov 01/08
CES
PYLON BOX - DESCRIPTION AND OPERATION
_____________________________________
1. ___________
Description
(Ref. Fig. 001)
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 1
Config-2 Feb 01/10
CES
Primary Structure - Materials and Protections Description
Figure 001
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 2
Config-2 Feb 01/10
CES
Pylon-to-Wing Attach Fittings
Figure 002
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 3
Config-2 Feb 01/10
CES
C. Pylon-to-Engine Attach Fitting
(Ref. Fig. 003)
The pylon-to-engine junction is provided by the forward attach fitting
located at the forward end of the pyramid at RIB1.
The aft attach fitting is located at RIB3.
The forward attach fitting reacts to engine thrust, vertical and side
load.
The aft attach fitting reacts to vertical and side loads, roll moments.
E. Doors
(Ref. Fig. 005)
The pylon box is fitted with four doors giving access to the various
systems:
- The forward access doors are located on each side of the pylon box
between RIB2 and RIB3. They are made of light alloy and are attached by
means of four screws.
- The aft access doors are located on each side of the pylon box between
RIB5 and RIB6. They are made of carbon fiber reinforced plastic and
honeycomb web sandwich type and are attached by means of four captive
screws.
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 4
Config-2 Feb 01/10
CES
Pylon-to-Engine Attach Fittings
Figure 003
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 5
Config-2 Feb 01/10
CES
Reverser Cowl Hinge Fittings
Figure 004
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 6
Config-2 Feb 01/10
CES
Doors
Figure 005
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 7
Config-2 Feb 01/10
CES
PYLON BOX - INSPECTION/CHECK
____________________________
TASK 54-51-00-200-001
R Special Detailed Inspection (ROTO) of Engine Forward Mount Fitting and Spigot
R Fitting
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
-------------------------------------------------------------------------------
EFF :
ALL 54-51-00
Page 601
May 01/09
CES
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-00
Page 602
May 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-00-941-050
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF :
ALL 54-51-00
Page 603
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-050
B. Get Access
Subtask 54-51-00-040-051
EFF :
ALL 54-51-00
Page 604
Nov 01/08
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-00-010-050-A
B. Get Access
Subtask 54-51-00-040-051-A
Subtask 54-51-00-020-061
EFF :
ALL 54-51-00
Page 605
Feb 01/10
CES
Fitting at RIB1
Figure 601/TASK 54-51-00-991-053
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page 606
Feb 01/08
CES
Fitting at RIB1
Figure 601A/TASK 54-51-00-991-053-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page 607
Nov 01/08
CES
R **ON A/C 501-509, 511-526, 528-599,
(1) Remove the nut (3), the bolt (1) and the washer (2).
NOTE : Do the full procedure for one hole, then do it again for each
____
hole.
Subtask 54-51-00-110-051
EFF :
ALL 54-51-00
Page 608
Feb 01/10
CES
Fitting at RIB1
Figure 601B/TASK 54-51-00-991-053-B
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 609
Feb 01/10
CES
Engine Forward Mount-Fitting and Spigot Fitting - Inspection Areas
Figure 602/TASK 54-51-00-991-057
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page 610
Feb 01/08
CES
Engine Forward Mount-Fitting and Spigot Fitting - Inspection Areas
Figure 602A/TASK 54-51-00-991-057-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page 611
Nov 01/08
CES
Engine Forward Mount-Fitting and Spigot Fitting - Inspection Areas
Figure 602B/TASK 54-51-00-991-057-B
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 612
Feb 01/10
CES
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.
NOTE : Do the full procedure for one hole, then do it again for each
____
hole.
(2) Make sure that the surface of the inspection area is clean and
smooth.
4. Procedure
_________
Subtask 54-51-00-250-051
A. Inspection
EFF :
ALL 54-51-00
Page 613
Nov 01/08
CES
R **ON A/C 501-509, 511-526, 528-599,
NOTE : Do the full procedure for one hole, then do it again for each
____
hole.
5. Close-up
________
Subtask 54-51-00-420-065
(1) Install the bolt (1) with SPECIAL MATERIALS (Material No. 05-047),
the washer (2) and the nut (3).
NOTE : Do the full procedure for one hole, then do it again for each
____
hole.
(2) TORQUE the nut (3) to between 14 and 16 m.daN (103.24 and 117.99
lbf.ft).
EFF :
ALL 54-51-00
Page 614
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
401-499,
Subtask 54-51-00-440-051
Subtask 54-51-00-410-050
C. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-51-00-440-051-A
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-00
Page 615
Feb 01/10
511-526, 528-599,
CES
Subtask 54-51-00-410-050-A
C. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 616
Feb 01/10
CES
**ON A/C ALL
TASK 54-51-00-200-002
R Special Detailed Inspection (US) of Engine Forward Mount Fitting, End of Lower
R Arms, Aft of RIB 1, Forward and Aft Attachment Bolt Holes
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 54-51-00
Page 617
May 01/09
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-00
Page 618
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-51-00-941-051
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-051
B. Get Access
EFF :
ALL 54-51-00
Page 619
May 01/09
CES
Subtask 54-51-00-040-052
Subtask 54-51-00-010-051-A
B. Get Access
Subtask 54-51-00-040-052-A
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-00
Page 620
Feb 01/10
511-526, 528-599,
CES
**ON A/C ALL
Subtask 54-51-00-110-052
(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 54-51-00
Page 621
Feb 01/10
CES
Engine Forward Mount-Fitting, Attachment Bolt Holes
Figure 603/TASK 54-51-00-991-058
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page 622
Feb 01/08
CES
Engine Forward Mount-Fitting, Attachment Bolt Holes
Figure 603A/TASK 54-51-00-991-058-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page 623
Nov 01/08
CES
Engine Forward Mount-Fitting, Attachment Bolt Holes
Figure 603B/TASK 54-51-00-991-058-B
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 624
Feb 01/10
CES
(3) Do a visual check of the inspection area for damage or
discontinuities.
4. Procedure
_________
Subtask 54-51-00-270-051
A. Inspection
EFF :
ALL 54-51-00
Page 625
Feb 01/10
CES
(b) For the hole inspection with movement 4:
Do the inspection on the internal side for the left pylon.
Do the inspection on the external side for the right pylon.
5. Close-up
________
Subtask 54-51-00-440-052
Subtask 54-51-00-410-051
B. Close Access
EFF :
ALL 54-51-00
Page 626
Nov 01/08
CES
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-51-00-440-052-A
Subtask 54-51-00-410-051-A
B. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-00
Page 627
Feb 01/10
511-526, 528-599,
CES
**ON A/C ALL
TASK 54-51-00-200-003
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 54-51-00
Page 628
Nov 01/09
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-00
Page 629
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-51-00-941-052
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-052
B. Get Access
EFF :
ALL 54-51-00
Page 630
Nov 01/08
CES
Subtask 54-51-00-040-053
Subtask 54-51-00-010-052-A
B. Get Access
Subtask 54-51-00-040-053-A
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-00
Page 631
Feb 01/10
511-526, 528-599,
CES
**ON A/C ALL
Subtask 54-51-00-110-053
(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 54-51-00-220-054
A. Inspection
EFF :
ALL 54-51-00
Page 632
Feb 01/10
CES
Engine Forward Mount-Fitting, Forward of RIB1
Figure 604/TASK 54-51-00-991-003
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page 633
Feb 01/08
CES
Engine Forward Mount-Fitting, Forward of RIB1
Figure 604A/TASK 54-51-00-991-003-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page 634
Nov 01/08
CES
Engine Forward Mount-Fitting, Forward of RIB1
Figure 604B/TASK 54-51-00-991-003-B
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 635
Feb 01/10
CES
(2) Make sure that there is no:
5. Close-up
________
Subtask 54-51-00-440-053
Subtask 54-51-00-410-052
B. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page 636
Nov 01/08
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-00-440-053-A
Subtask 54-51-00-410-052-A
B. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 637
Feb 01/10
CES
R **ON A/C ALL
TASK 54-51-00-200-004
Detailed Inspection of Pylon, Lower Spar, between RIB 1 and RIB 10, Lower
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 :
ALL 54-51-00
Page 638
Nov 01/07
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-00
Page 639
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-51-00-941-053
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-053
B. Get Access
EFF :
ALL 54-51-00
Page 640
Nov 01/08
CES
(4) Remove the access panels:
Subtask 54-51-00-020-051
Subtask 54-51-00-040-054
Subtask 54-51-00-010-053-A
B. Get Access
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-00
Page 641
Feb 01/10
511-526, 528-599,
CES
R (4) Remove the access panels
R Subtask 54-51-00-020-051-A
R Subtask 54-51-00-040-054-A
Subtask 54-51-00-110-054
(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 54-51-00
Page 642
Nov 01/07
CES
4. Procedure
_________
Subtask 54-51-00-220-055
A. Inspection
EFF :
ALL 54-51-00
Page 643
Feb 01/10
CES
Pylon Lower Spar between RIB1 and RIB10
Figure 605/TASK 54-51-00-991-004
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page 644
Feb 01/08
CES
Pylon Lower Spar between RIB1 and RIB10
Figure 605A/TASK 54-51-00-991-004-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page 645
Nov 01/08
CES
Pylon Lower Spar between RIB1 and RIB10
Figure 605B/TASK 54-51-00-991-004-B
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 646
Feb 01/10
CES
5. Close-up
________
Subtask 54-51-00-440-054
Subtask 54-51-00-420-052
Subtask 54-51-00-410-053
C. Close Access
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page 647
Nov 01/08
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-00-440-054-A
Subtask 54-51-00-420-052-A
Subtask 54-51-00-410-053-A
C. Close Access
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 648
Feb 01/10
CES
R **ON A/C ALL
TASK 54-51-00-200-027
Detailed Inspection of Pylon, Lower Spar, Upper surface, between RIB 2 and RIB
3, and RIB 4 and RIB 8
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 54-51-00
Page 649
Nov 01/07
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-00-941-054
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
EFF :
ALL 54-51-00
Page 650
Feb 01/10
CES
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-071
B. Get Access
Subtask 54-51-00-040-055
Subtask 54-51-00-040-055-A
EFF :
ALL 54-51-00
Page 651
Feb 01/10
CES
**ON A/C ALL
Subtask 54-51-00-110-055
(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 54-51-00-220-056
A. Inspection
EFF :
ALL 54-51-00
Page 652
Feb 01/10
CES
Lower Spar from RIB2 to RIB3 and from RIB4 to RIB8
Figure 606/TASK 54-51-00-991-026
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page 653
Feb 01/08
CES
Lower Spar from RIB2 to RIB3 and from RIB4 to RIB8
Figure 606A/TASK 54-51-00-991-026-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page 654
Nov 01/08
CES
Lower Spar from RIB2 to RIB3 and from RIB4 to RIB8
Figure 606B/TASK 54-51-00-991-026-B
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 655
Feb 01/10
CES
**ON A/C ALL
5. Close-up
________
Subtask 54-51-00-440-055
Subtask 54-51-00-440-055-A
EFF :
ALL 54-51-00
Page 656
Feb 01/10
CES
R **ON A/C ALL
Subtask 54-51-00-410-054
B. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page 657
Nov 01/07
CES
TASK 54-51-00-200-028
Special Detailed Inspection of Pylon Lower Spar, Upper Surface, between RIB1
and RIB2, RIB3 and RIB4, and RIB8 and RIB10
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 54-51-00
Page 658
Nov 01/07
R
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-00
Page 659
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-51-00-941-055
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-054
B. Get Access
Subtask 54-51-00-040-056
EFF :
ALL 54-51-00
Page 660
Nov 01/08
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-00-040-056-A
Subtask 54-51-00-110-056
EFF :
ALL 54-51-00
Page 661
Feb 01/10
CES
Lower Spar between RIB1 and RIB2, RIB3 and RIB4, and RIB8 and RIB10 -
Inspection Areas
Figure 607/TASK 54-51-00-991-056
R EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00 Page 662
Feb 01/08
CES
Lower Spar between RIB1 and RIB2, RIB3 and RIB4, and RIB8 and RIB10 -
Inspection Areas
Figure 607A/TASK 54-51-00-991-056-A
R EFF :
234-235, 239-249, 251-299, 307-399,
54-51-00 Page 663
Nov 01/08
CES
Lower Spar between RIB1 and RIB2, RIB3 and RIB4, and RIB8 and RIB10 -
Inspection Areas
Figure 607B/TASK 54-51-00-991-056-B
R EFF :
501-509, 511-526, 528-599,
54-51-00 Page 664
Feb 01/10
CES
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and MISCELLANEOUS (Material No. 19-003), if necessary.
(2) Make sure that the surface of the inspection area is clean and
smooth.
4. Procedure
_________
Subtask 54-51-00-250-052
A. Inspection
EFF :
ALL 54-51-00
Page 665
Feb 01/10
CES
(2) Make a report of damage after NDT inspection:
5. Close-up
________
Subtask 54-51-00-440-056
Subtask 54-51-00-440-056-A
Subtask 54-51-00-410-055
B. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page 666
Feb 01/10
CES
(3) Remove the access platform(s).
EFF :
ALL 54-51-00
Page 667
Nov 01/07
R
CES
TASK 54-51-00-200-005
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
-------------------------------------------------------------------------------
EFF :
ALL 54-51-00
Page 668
Nov 01/07
R
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-00
Page 669
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-51-00-941-056
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-055
B. Get Access
EFF :
ALL 54-51-00
Page 670
Nov 01/08
CES
Subtask 54-51-00-040-057
Subtask 54-51-00-010-055-A
B. Get Access
Subtask 54-51-00-040-057-A
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-00
Page 671
Feb 01/10
511-526, 528-599,
CES
**ON A/C ALL
Subtask 54-51-00-110-057
(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 54-51-00-220-057
A. Inspection
EFF :
ALL 54-51-00
Page 672
Feb 01/10
CES
Pylon-to-Engine Attach Fitting
Figure 608/TASK 54-51-00-991-005
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page 673
Feb 01/08
CES
Pylon-to-Engine Attach Fitting
Figure 608A/TASK 54-51-00-991-005-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page 674
Nov 01/08
CES
Pylon-to-Engine Attach Fitting
Figure 608B/TASK 54-51-00-991-005-B
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 675
Feb 01/10
CES
(2) Make sure that there is no:
5. Close-up
________
Subtask 54-51-00-440-057
Subtask 54-51-00-410-056
B. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page 676
Nov 01/08
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-00-440-057-A
Subtask 54-51-00-410-056-A
B. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 677
Feb 01/10
CES
R **ON A/C ALL
TASK 54-51-00-200-006
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 54-51-00
Page 678
Nov 01/07
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-00-941-057
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
EFF :
ALL 54-51-00
Page 679
Feb 01/10
CES
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-056
B. Get Access
Subtask 54-51-00-010-056-A
B. Get Access
EFF :
ALL 54-51-00
Page 680
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
401-499,
Subtask 54-51-00-040-058
Subtask 54-51-00-040-058-A
Subtask 54-51-00-110-058
(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 54-51-00
Page 681
Feb 01/10
CES
4. Procedure
_________
Subtask 54-51-00-220-058
A. Inspection
5. Close-up
________
Subtask 54-51-00-440-058
EFF :
ALL 54-51-00
Page 682
Feb 01/10
CES
Outer and Inner Fittings at RIB4
Figure 609/TASK 54-51-00-991-006
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-00
Page 683
Nov 01/08
CES
Outer and Inner Fittings at RIB4
Figure 609A/TASK 54-51-00-991-006-A
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 684
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-00-440-058-A
Subtask 54-51-00-410-057
B. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-51-00-410-057-A
B. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-00
Page 685
Feb 01/10
511-526, 528-599,
CES
(4) Remove the warning notice(s).
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-51-00
Page 686
Feb 01/10
CES
**ON A/C ALL
TASK 54-51-00-200-007
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 54-51-00
Page 687
Nov 01/07
R
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-00-941-058
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
EFF :
ALL 54-51-00
Page 688
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
401-499,
Subtask 54-51-00-010-057
B. Get Access
Subtask 54-51-00-010-057-A
B. Get Access
(a) For the left pylon: 471AL, 471AR, 471BL, 471BR, 521BT
(b) For the right pylon: 481AL, 481AR, 481BL, 481BR, 621BT.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-00
Page 689
Feb 01/10
511-526, 528-599,
CES
**ON A/C ALL
Subtask 54-51-00-020-052-A
(2) Disengage the cables (3) and (4) at RIB4 to get access to the
shackles.
(b) Remove the bolt (7) and the spacer (6) to disengage the clamps
(10) and (11).
(c) Remove the bolt (1) and disengage the clamps (13) and (2) from
the support (12).
(d) Loosen the bolt (9) and turn the plate (8) to get access to the
shackles.
Subtask 54-51-00-110-059
EFF :
ALL 54-51-00
Page 690
Feb 01/10
CES
Cables at RIB4
Figure 610/TASK 54-51-00-991-055
EFF :
ALL 54-51-00
Page 691
Nov 01/07
R
CES
Pylon-to-Wing Forward Attachment Shackles at RIB4 - Inspection Areas
Figure 611/TASK 54-51-00-991-059
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-00
Page 692
Nov 01/08
CES
Pylon-to-Wing Forward Attachment Shackles at RIB4 - Inspection Areas
Figure 611A/TASK 54-51-00-991-059-A
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page 693
Feb 01/10
CES
R **ON A/C ALL
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and MISCELLANEOUS (Material No. 19-003), if necessary.
(2) Make sure that the surface of the inspection area is clean and
smooth.
EFF :
ALL 54-51-00
Page 694
Nov 01/07
CES
4. Procedure
_________
Subtask 54-51-00-270-052
A. Inspection
EFF :
ALL 54-51-00
Page 695
Feb 01/10
CES
5. Close-up
________
Subtask 54-51-00-420-053-A
(a) Put the plate (8) in position and tighten the bolt (9).
(b) Install the clamps (10) and (11), the spacer (6), the plate (8)
and the bolt (7).
(d) Install the clamps (13) and (2) and the bolt (1) on the support
(12).
Subtask 54-51-00-410-058
B. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page 696
Feb 01/08
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
Subtask 54-51-00-410-058-A
B. Close Access
R (a) For the left pylon: 471AL, 471AR, 471BL, 471BR, 521BT
(b) For the right pylon: 481AL, 481AR, 481BL, 481BR, 621BT.
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-51-00
Page 697
Feb 01/10
CES
**ON A/C ALL
TASK 54-51-00-200-008
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 54-51-00
Page 698
Nov 01/07
R
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
ASRM 51110000
ASRM 51220000
3. __________
Job Set-up
Subtask 54-51-00-941-059
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
EFF :
ALL 54-51-00
Page 699
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
401-499,
Subtask 54-51-00-010-058
B. Get Access
Subtask 54-51-00-010-058-A
B. Get Access
(a) For the left pylon: 471AL, 471AR, 471BL, 471BR, 521BT
(b) For the right pylon: 481AL, 481AR, 481BL, 481BR, 621BT.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-00
Page A600
Feb 01/10
511-526, 528-599,
CES
**ON A/C ALL
Subtask 54-51-00-110-060
(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 54-51-00-220-059
A. Inspection
EFF :
ALL 54-51-00
Page A601
Feb 01/10
CES
Pylon-to-Wing Forward Attachment-Shackles at RIB4
Figure 612/TASK 54-51-00-991-007
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-00
Page A602
Nov 01/08
CES
Pylon-to-Wing Forward Attachment-Shackles at RIB4
Figure 612A/TASK 54-51-00-991-007-A
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page A603
Feb 01/10
CES
(2) Make sure that there is no:
5. Close-up
________
Subtask 54-51-00-410-059
A. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-51-00-410-059-A
A. Close Access
(a) For the left pylon: 471AL, 471BL, 471AR, 471BR, 521BT
(b) For the right pylon: 481AL, 481AR, 481BL, 481BR, 621BT.
EFF :
ALL 54-51-00
Page A604
Feb 01/10
CES
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-51-00
Page A605
Feb 01/10
CES
**ON A/C ALL
TASK 54-51-00-200-009
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
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-00
Page A606
Nov 01/07
R
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-00-941-060
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
EFF :
ALL 54-51-00
Page A607
Feb 01/10
CES
Subtask 54-51-00-010-059
B. Get Access
Subtask 54-51-00-020-054
(1) Remove the shackles, the sleeves and the bolts (Ref. TASK 54-51-17-
000-001).
Subtask 54-51-00-110-061
(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.
R
EFF :
ALL 54-51-00
Page A608
Nov 01/07
CES
4. Procedure
_________
Subtask 54-51-00-220-060
A. Inspection
5. Close-up
________
Subtask 54-51-00-420-055
(1) Install the bolts, the sleeves and the shackles (Ref. TASK 54-51-17-
400-001).
EFF :
ALL 54-51-00
Page A609
Feb 01/10
CES
Shackles, Sleeves and Bolts of the Pylon-to-Wing Attachment Fittings at RIB4
Figure 613/TASK 54-51-00-991-062
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-00
Page A610
Nov 01/08
CES
Shackles, Sleeves and Bolts of the Pylon-to-Wing Attachment Fittings at RIB4
Figure 613A/TASK 54-51-00-991-062-A
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page A611
Feb 01/10
CES
Subtask 54-51-00-410-060
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page A612
Nov 01/07
R
CES
TASK 54-51-00-200-010
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 54-51-00
Page A613
Nov 01/07
R
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-00-941-061
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF :
ALL 54-51-00
Page A614
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-060
B. Get Access
Subtask 54-51-00-010-060-A
B. Get Access
EFF :
ALL 54-51-00
Page A615
Feb 01/10
CES
R (2) Remove the access panels:
Subtask 54-51-00-110-062
(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 54-51-00-040-059
EFF :
ALL 54-51-00
Page A616
Aug 01/09
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-00-040-059-A
Subtask 54-51-00-020-062
4. Procedure
_________
Subtask 54-51-00-220-061
A. Inspection
EFF :
ALL 54-51-00
Page A617
Feb 01/10
CES
Pylon Spigot - Receptacle Fitting
Figure 614/TASK 54-51-00-991-009
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-00
Page A618
Aug 01/09
CES
Pylon Spigot - Receptacle Fitting
Figure 614A/TASK 54-51-00-991-009-A
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page A619
Feb 01/10
CES
(b) Other damage (cracks, scratches, stress, marks, dents,
bumps,...):
- If you find this type of damage, refer to the Structural Repair
Manual (Ref. ASRM 51110000) for damage classification and related
corrective action.
Subtask 54-51-00-420-062
5. Close-up
________
Subtask 54-51-00-440-059
Subtask 54-51-00-440-059-A
Subtask 54-51-00-410-061
B. Close Access
EFF :
ALL 54-51-00
Page A620
Feb 01/10
CES
(2) Install the panels:
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-51-00-410-061-A
B. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-00
Page A621
Feb 01/10
511-526, 528-599,
CES
R **ON A/C ALL
TASK 54-51-00-200-011
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.
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-00
Page A622
Aug 01/09
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-00-941-062
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
EFF :
ALL 54-51-00
Page A623
Feb 01/10
CES
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-061
B. Get Access
Subtask 54-51-00-010-061-A
B. Get Access
EFF :
ALL 54-51-00
Page A624
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
401-499,
Subtask 54-51-00-040-060
Subtask 54-51-00-040-060-A
Subtask 54-51-00-110-063
(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 54-51-00
Page A625
Feb 01/10
CES
4. Procedure
_________
Subtask 54-51-00-220-062
A. Inspection
5. Close-up
________
Subtask 54-51-00-440-060
EFF :
ALL 54-51-00
Page A626
Feb 01/10
CES
Pylon-to-Wing Attach Fitting Lugs at RIB10
Figure 615/TASK 54-51-00-991-010
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-00
Page A627
Aug 01/09
CES
Pylon-to-Wing Attach Fitting Lugs at RIB10
Figure 615A/TASK 54-51-00-991-010-A
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page A628
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-00-440-060-A
Subtask 54-51-00-410-062
B. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-51-00-410-062-A
B. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-00
Page A629
Feb 01/10
511-526, 528-599,
CES
(4) Remove the warning notice(s).
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-51-00
Page A630
Feb 01/10
CES
R **ON A/C ALL
TASK 54-51-00-200-014
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 54-51-00
Page A631
Aug 01/09
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-00-941-065
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
EFF :
ALL 54-51-00
Page A632
Feb 01/10
CES
Subtask 54-51-00-010-062
B. Get Access
(1) Put an access platform in position at the zones 415 and 425.
Subtask 54-51-00-020-055
(1) Remove the shackles, the sleeves and the bolts of the aft attach
fittings (Ref. TASK 54-51-17-000-002).
Subtask 54-51-00-110-066
(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.
4. Procedure
_________
Subtask 54-51-00-220-064
A. Inspection
EFF :
ALL 54-51-00
Page A633
Feb 01/10
CES
Sleeves of the Pylon-to-Wing Aft Attach-Fitting
Figure 616/TASK 54-51-00-991-012
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-00
Page A634
Aug 01/09
CES
Sleeves of the Pylon-to-Wing Aft Attach-Fitting
Figure 616A/TASK 54-51-00-991-012-A
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page A635
Feb 01/10
CES
**ON A/C ALL
5. Close-up
________
Subtask 54-51-00-420-056
(1) Install the shackles, the sleeves and the bolts of the aft attach
fitting (Ref. TASK 54-51-17-400-002).
Subtask 54-51-00-410-065
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page A636
Aug 01/09
R
CES
TASK 54-51-00-200-015
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 54-51-00
Page A637
Aug 01/09
R
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-00-941-066
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF :
ALL 54-51-00
Page A638
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-063
B. Get Access
Subtask 54-51-00-040-063
Subtask 54-51-00-040-063-A
EFF :
ALL 54-51-00
Page A639
Feb 01/10
CES
**ON A/C ALL
Subtask 54-51-00-110-067
(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.
4. Procedure
_________
Subtask 54-51-00-220-065
A. Inspection
EFF :
ALL 54-51-00
Page A640
Feb 01/10
CES
Supports of the Access Doors between RIB5 and RIB6
Figure 617/TASK 54-51-00-991-013
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page A641
Aug 01/09
CES
Supports of the Access Doors between RIB5 and RIB6
Figure 617A/TASK 54-51-00-991-013-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page A642
Aug 01/09
CES
Supports of the Access Doors between RIB5 and RIB6
Figure 617B/TASK 54-51-00-991-013-B
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page A643
Feb 01/10
CES
**ON A/C ALL
5. Close-up
________
Subtask 54-51-00-440-063
Subtask 54-51-00-440-063-A
EFF :
ALL 54-51-00
Page A644
Feb 01/10
CES
**ON A/C ALL
Subtask 54-51-00-410-066
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page A645
Aug 01/09
R
CES
TASK 54-51-00-200-016
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 54-51-00
Page A646
Aug 01/09
R
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-00-941-067
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
EFF :
ALL 54-51-00
Page A647
Feb 01/10
CES
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-073
B. Get Access
Subtask 54-51-00-040-064-A
Subtask 54-51-00-040-064
EFF :
ALL 54-51-00
Page A648
Feb 01/10
CES
**ON A/C ALL
Subtask 54-51-00-110-068
(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 54-51-00-220-066
A. Inspection
EFF :
ALL 54-51-00
Page A649
Feb 01/10
CES
Aft Pylon Lateral Access-Doors
Figure 618/TASK 54-51-00-991-014
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page A650
Aug 01/09
CES
Aft Pylon Lateral Access-Doors
Figure 618A/TASK 54-51-00-991-014-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page A651
Aug 01/09
CES
Aft Access Doors
Figure 618B/TASK 54-51-00-991-014-B
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page A652
Feb 01/10
CES
**ON A/C ALL
5. Close-up
________
Subtask 54-51-00-440-064-A
Subtask 54-51-00-440-064
EFF :
ALL 54-51-00
Page A653
Feb 01/10
CES
**ON A/C ALL
Subtask 54-51-00-410-067
B. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page A654
Aug 01/09
R
CES
TASK 54-51-00-200-017
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 54-51-00
Page A655
Aug 01/09
R
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-00-941-068
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF :
ALL 54-51-00
Page A656
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-064
B. Get Access
Subtask 54-51-00-040-065
Subtask 54-51-00-040-065-A
EFF :
ALL 54-51-00
Page A657
Feb 01/10
CES
**ON A/C ALL
Subtask 54-51-00-110-069
(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 54-51-00-220-067
A. Inspection
EFF :
ALL 54-51-00
Page A658
Feb 01/10
CES
Forward Access Door
Figure 619/TASK 54-51-00-991-015
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page A659
Aug 01/09
CES
Forward Access Door
Figure 619A/TASK 54-51-00-991-015-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page A660
Aug 01/09
CES
Forward Access Door
Figure 619B/TASK 54-51-00-991-015-B
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page A661
Feb 01/10
CES
**ON A/C ALL
5. Close-up
________
Subtask 54-51-00-440-065
Subtask 54-51-00-440-065-A
EFF :
ALL 54-51-00
Page A662
Feb 01/10
CES
**ON A/C ALL
Subtask 54-51-00-410-068
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page A663
Aug 01/09
R
CES
TASK 54-51-00-200-018
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 54-51-00
Page A664
Aug 01/09
R
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-00-941-069
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
EFF :
ALL 54-51-00
Page A665
Feb 01/10
CES
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-065
B. Get Access
Subtask 54-51-00-040-070
Subtask 54-51-00-040-070-A
EFF :
ALL 54-51-00
Page A666
Feb 01/10
CES
**ON A/C ALL
Subtask 54-51-00-110-070
(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.
4. Procedure
_________
Subtask 54-51-00-220-068
A. Inspection
EFF :
ALL 54-51-00
Page A667
Feb 01/10
CES
Lateral Panels between RIB1 and RIB4
Figure 620/TASK 54-51-00-991-028- 12 (SHEET 1)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page A668
Aug 01/09
CES
Lateral Panels between RIB1 and RIB4
Figure 620/TASK 54-51-00-991-028- 22 (SHEET 2)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page A669
Aug 01/09
CES
Lateral Panels between RIB1 and RIB4
Figure 620A/TASK 54-51-00-991-028-A12 (SHEET 1)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page A670
Aug 01/09
CES
Lateral Panels between RIB1 and RIB4
Figure 620A/TASK 54-51-00-991-028-A22 (SHEET 2)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page A671
Aug 01/09
CES
Lateral Panels between RIB1 and RIB4
Figure 620B/TASK 54-51-00-991-028-B12 (SHEET 1)
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page A672
Feb 01/10
CES
Lateral Panels between RIB1 and RIB4
Figure 620B/TASK 54-51-00-991-028-B22 (SHEET 2)
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page A673
Feb 01/10
CES
**ON A/C ALL
(1) Do a detailed inspection of the lower spar of the pylon between RIB1
and RIB4. This inspection is applicable to the areas of the fasteners
at the junction with the lateral panel, left and right sides.
5. Close-up
________
Subtask 54-51-00-440-070
Subtask 54-51-00-440-070-A
EFF :
ALL 54-51-00
Page A674
Feb 01/10
CES
**ON A/C ALL
Subtask 54-51-00-410-069
B. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page A675
Aug 01/09
R
CES
TASK 54-51-00-200-019
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
-------------------------------------------------------------------------------
EFF :
ALL 54-51-00
Page A676
Aug 01/09
R
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-00-941-070
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
EFF :
ALL 54-51-00
Page A677
Feb 01/10
CES
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-066
B. Get Access
(a) For the left pylon: 471AL, 471BL, 471CL, 472AR, 472BR
(b) For the right pylon: 481AL, 481BL, 482AR, 482BR, 482CR.
Subtask 54-51-00-010-066-A
B. Get Access
(a) For the left pylon: 471BL, 471CL, 471DL, 471BR, 471CR
(b) For the right pylon: 481BL, 481CL, 481BR, 481CR, 481DR.
Subtask 54-51-00-040-071
EFF :
ALL 54-51-00
Page A678
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-00-040-071-A
Subtask 54-51-00-110-071
(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 54-51-00-220-069
A. Inspection
EFF :
ALL 54-51-00
Page A679
Feb 01/10
CES
Junction Area between the Upper Spar and the Lateral Panel
Figure 621/TASK 54-51-00-991-032- 12 (SHEET 1)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-00
Page A680
Aug 01/09
CES
Junction Area between the Upper Spar and the Lateral Panel
Figure 621/TASK 54-51-00-991-032- 22 (SHEET 2)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-00
Page A681
Aug 01/09
CES
Junction Area between the Upper spar and the Lateral Panel
Figure 621A/TASK 54-51-00-991-032-A12 (SHEET 1)
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page A682
Feb 01/10
CES
Junction Area between the Upper spar and the Lateral Panel
Figure 621A/TASK 54-51-00-991-032-A22 (SHEET 2)
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page A683
Feb 01/10
CES
**ON A/C ALL
(1) Do a detailed inspection of the upper spar of the pylon between RIB4
and RIB10. This inspection is applicable to the areas of the
fasteners at the junction with the lateral panel, left and right
sides.
5. Close-up
________
Subtask 54-51-00-440-071
Subtask 54-51-00-440-071-A
EFF :
ALL 54-51-00
Page A684
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
401-499,
Subtask 54-51-00-410-070
B. Close Access
(a) For the left pylon: 471AL, 471BL, 471CL, 472AR, 472BR
(b) For the right pylon: 481AL, 481BL, 482AR, 482BR, 482CR.
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-51-00-410-070-A
B. Close Access
(a) For the left pylon: 471BL, 471CL, 471DL, 471BR, 471CR
(b) For the right pylon: 481BL, 481CL, 481BR, 481CR, 481DR.
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-00
Page A685
Feb 01/10
511-526, 528-599,
CES
R **ON A/C ALL
TASK 54-51-00-200-021
Detailed Inspection of Pylon, Upper Spars, Upper Surface, from Forward of RIB1
to RIB10
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 54-51-00
Page A686
Aug 01/09
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-00
Page A687
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-51-00-941-071
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-067
B. Get Access
(a) For the left pylon: 413CL, 413DL, 413EL, 414CR, 414FR, 471AL,
471BL, 471CL, 472AR, 472BR
(b) For the right pylon: 423CL, 423DL, 423FL, 424CR, 424ER, 481AL,
481BL, 482AR, 482BR, 482CR.
EFF :
ALL 54-51-00
Page A688
Aug 01/09
R
CES
**ON A/C 234-235, 239-249, 251-299, 307-399,
Subtask 54-51-00-010-067-A
B. Get Access
(a) For the left pylon: 413CL, 413CR, 413DT, 471AL, 471AR, 471BL,
471BR, 471CL, 471CR, 471DL
(b) For the right pylon: 423CL, 423CR, 423DT, 481AL, 481AR, 481BL,
481BR, 481CL, 481CR, 481DR
Subtask 54-51-00-010-067-B
B. Get Access
(a) For the left pylon: 413CL, 413CR, 413DT, 471AL, 471AR, 471BL,
471BR, 471CL, 471CR, 471DL
(b) For the right pylon: 423CL, 423CR, 423DT, 481AL, 481AR, 481BL,
481BR, 481CL, 481CR, 481DR
Subtask 54-51-00-020-058
EFF :
ALL 54-51-00
Page A689
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
401-499,
Subtask 54-51-00-040-066
Subtask 54-51-00-040-066-A
Subtask 54-51-00-110-072
(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.
EFF :
ALL 54-51-00
Page A690
Feb 01/10
CES
4. Procedure
_________
Subtask 54-51-00-220-070
A. Inspection
EFF :
ALL 54-51-00
Page A691
Feb 01/10
CES
Upper Surface from Forward of RIB1 to RIB10
Figure 622/TASK 54-51-00-991-036
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page A692
Aug 01/09
CES
Upper Surface from Forward of RIB1 to RIB10
Figure 622A/TASK 54-51-00-991-036-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page A693
Aug 01/09
CES
Upper Surface from Forward of RIB1 to RIB10
Figure 622B/TASK 54-51-00-991-036-B
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page A694
Feb 01/10
CES
5. Close-up
________
Subtask 54-51-00-440-066
Subtask 54-51-00-440-066-A
Subtask 54-51-00-420-059
Subtask 54-51-00-410-071
C. Close Access
(a) For the left pylon: 413CL, 413DL, 413EL, 414CR, 414FR, 471AL,
471BL, 471CL, 472AR, 472BR
(b) For the right pylon: 423CL, 423DL, 423FL, 424CR, 424ER, 481AL,
481BL, 482AR, 482BR, 482CR.
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page A695
Feb 01/10
CES
(3) Remove the access platform(s).
Subtask 54-51-00-410-071-A
C. Close Access
(a) For the left pylon: 413CL, 413CR, 413DT, 471AL, 471AR, 471BL,
471BR, 471CL, 471CR, 471DL
(b) For the right pylon: 423CL, 423CR, 423DT, 481AL, 481AR, 481BL,
481BR, 481CL, 481CR, 481DR
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-51-00-410-071-B
C. Close Access
(a) For the left pylon: 413CL, 413CR, 413DT, 471AL, 471AR, 471BL,
471BR, 471CL, 471CR, 471DL
(b) For the right pylon: 423CL, 423CR, 423DT, 481AL, 481AR, 481BL,
481BR, 481CL, 481CR, 481DR
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-00
Page A696
Feb 01/10
511-526, 528-599,
CES
**ON A/C ALL
TASK 54-51-00-200-022
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 54-51-00
Page A697
Aug 01/09
R
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-00
Page A698
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-51-00-941-072
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-068
B. Get Access
EFF :
ALL 54-51-00
Page A699
Aug 01/09
R
CES
Subtask 54-51-00-040-067
Subtask 54-51-00-010-068-A
B. Get Access
Subtask 54-51-00-040-067-A
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-00
Page B600
Feb 01/10
511-526, 528-599,
CES
**ON A/C ALL
Subtask 54-51-00-110-073
(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.
4. Procedure
_________
Subtask 54-51-00-220-071
A. Inspection
EFF :
ALL 54-51-00
Page B601
Feb 01/10
CES
Lower Surface of the Upper spar
Figure 623/TASK 54-51-00-991-037
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page B602
Aug 01/09
CES
Lower Surface of the Upper spar
Figure 623A/TASK 54-51-00-991-037-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page B603
Aug 01/09
CES
Lower Surface of the Upper spar
Figure 623B/TASK 54-51-00-991-037-B
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page B604
Feb 01/10
CES
(2) Make sure that there is no:
5. Close-up
________
Subtask 54-51-00-440-067
Subtask 54-51-00-410-072
B. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page B605
Aug 01/09
R
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-00-440-067-A
Subtask 54-51-00-410-072-A
B. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page B606
Feb 01/10
CES
**ON A/C ALL
TASK 54-51-00-200-023
Detailed Inspection of Pylon, Upper Spar, Lower Surface, between RIB 2 and RIB
3, RIB 4 and RIB 8
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
NOTE : You must do this task at the same time as MPD Task 545162-02.
____
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-00
Page B607
Aug 01/09
R
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-00-941-073
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
EFF :
ALL 54-51-00
Page B608
Feb 01/10
CES
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-074
B. Get Access
Subtask 54-51-00-110-074
(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.
R
EFF :
ALL 54-51-00
Page B609
Aug 01/09
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
401-499,
Subtask 54-51-00-040-068
Subtask 54-51-00-040-068-A
4. Procedure
_________
Subtask 54-51-00-220-072
A. Inspection
EFF :
ALL 54-51-00
Page B610
Feb 01/10
CES
Lower Surface from RIB2 to RIB3 and RIB4 to RIB8
Figure 624/TASK 54-51-00-991-038
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page B611
Aug 01/09
CES
Lower Surface from RIB2 to RIB3 and RIB4 to RIB8
Figure 624A/TASK 54-51-00-991-038-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page B612
Aug 01/09
CES
Lower Surface from RIB2 to RIB3 and RIB4 to RIB8
Figure 624B/TASK 54-51-00-991-038-B
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page B613
Feb 01/10
CES
**ON A/C ALL
5. Close-up
________
Subtask 54-51-00-440-068
Subtask 54-51-00-440-068-A
EFF :
ALL 54-51-00
Page B614
Feb 01/10
CES
**ON A/C ALL
Subtask 54-51-00-410-073
B. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page B615
Aug 01/09
R
CES
TASK 54-51-00-200-024
Special Detailed Inspection of Pylon, Upper Spar, Lower Surface, between RIB1
and RIB2, RIB3 and RIB4, RIB8 and RIB10
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
NOTE : You must do this task at the same time as MPD task 545162-01.
____
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-00
Page B616
Aug 01/09
R
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-00
Page B617
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-51-00-941-074
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-075
B. Get Access
Subtask 54-51-00-040-069
R
EFF :
ALL 54-51-00
Page B618
Aug 01/09
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-00-040-069-A
Subtask 54-51-00-110-075
EFF :
ALL 54-51-00
Page B619
Feb 01/10
CES
Pylon Upper Spar, Lower Surface Between RIB1 and RIB2, RIB3 and RIB4, RIB8 and
RIB10 - Inspection Areas
Figure 625/TASK 54-51-00-991-061
R EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00 Page B620
Aug 01/09
CES
Pylon Upper Spar, Lower Surface Between RIB1 and RIB2, RIB3 and RIB4, RIB8 and
RIB10 - Inspection Areas
Figure 625A/TASK 54-51-00-991-061-A
R EFF :
234-235, 239-249, 251-299, 307-399,
54-51-00 Page B621
Aug 01/09
CES
Pylon Upper Spar, Lower Surface Between RIB1 and RIB2, RIB3 and RIB4, RIB8 and
RIB10 - Inspection Areas
Figure 625B/TASK 54-51-00-991-061-B
R EFF :
501-509, 511-526, 528-599,
54-51-00 Page B622
Feb 01/10
CES
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004)
and MISCELLANEOUS (Material No. 19-003), if necessary.
(2) Make sure that the surface of the inspection area is clean and
smooth.
4. Procedure
_________
Subtask 54-51-00-250-053
A. Inspection
EFF :
ALL 54-51-00
Page B623
Feb 01/10
CES
**ON A/C ALL
5. Close-up
________
Subtask 54-51-00-440-069
Subtask 54-51-00-440-069-A
EFF :
ALL 54-51-00
Page B624
Feb 01/10
CES
**ON A/C ALL
Subtask 54-51-00-410-074
B. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page B625
Aug 01/09
R
CES
TASK 54-51-00-200-025
Detailed Inspection of Pylon, Pyramid Mating Face with the Engine Forward Mount
Fitting
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 54-51-00
Page B626
Aug 01/09
R
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-00-941-075
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF :
ALL 54-51-00
Page B627
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-069
B. Get Access
Subtask 54-51-00-020-059
Subtask 54-51-00-020-059-A
Subtask 54-51-00-110-076
EFF :
ALL 54-51-00
Page B628
Feb 01/10
CES
(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 54-51-00-220-073
A. Inspection
EFF :
ALL 54-51-00
Page B629
Feb 01/10
CES
Mating Face of the Pylon Pyramid
Figure 626/TASK 54-51-00-991-039
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page B630
Aug 01/09
CES
Mating Face of the Pylon Pyramid
Figure 626A/TASK 54-51-00-991-039-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page B631
Aug 01/09
CES
Mating Face of the Pylon Pyramid
Figure 626B/TASK 54-51-00-991-039-B
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page B632
Feb 01/10
CES
5. Close-up
________
Subtask 54-51-00-420-060
Subtask 54-51-00-420-060-A
Subtask 54-51-00-410-075
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page B633
Feb 01/10
CES
TASK 54-51-00-200-026
Detailed Inspection of Pylon, Engine Aft Attachment Beam Mating Face with the
Engine Aft Mount Fitting
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 54-51-00
Page B634
Aug 01/09
R
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-00-941-076
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF :
ALL 54-51-00
Page B635
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-51-00-010-070
B. Get Access
Subtask 54-51-00-020-060
Subtask 54-51-00-020-060-A
Subtask 54-51-00-110-077
EFF :
ALL 54-51-00
Page B636
Feb 01/10
CES
(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 54-51-00-220-074
A. Inspection
EFF :
ALL 54-51-00
Page B637
Feb 01/10
CES
Mating Face of the Engine Aft Attachment-Beam
Figure 627/TASK 54-51-00-991-040
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-00
Page B638
Aug 01/09
CES
Mating Face of the Engine Aft Attachment-Beam
Figure 627A/TASK 54-51-00-991-040-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-00
Page B639
Aug 01/09
CES
Mating Face of the Engine Aft Attachment-Beam
Figure 627B/TASK 54-51-00-991-040-B
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page B640
Feb 01/10
CES
5. Close-up
________
Subtask 54-51-00-420-061
Subtask 54-51-00-420-061-A
Subtask 54-51-00-410-076
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-00
Page B641
Feb 01/10
CES
TASK 54-51-00-220-001
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-00
Page B642
Feb 01/10
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
NTM 545123
3. __________
Job Set-up
Subtask 54-51-00-941-077
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
EFF :
ALL 54-51-00
Page B643
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
401-499,
Subtask 54-51-00-010-076
B. Get Access
(a) For the left pylon: 471CL, 472BR, 475AL, 475BL, 476AR, 476BR
(b) For the right pylon: 481BL, 482CR, 485AL, 485BL, 486AR, 486BR.
Subtask 54-51-00-010-076-A
B. Get Access
(a) For the left pylon: 471DL, 471CR, 475AL, 475BL, 475AR, 475BR
(b) For the right pylon: 481CL, 481DR, 485AL, 485BL, 485AR, 485BR.
Subtask 54-51-00-040-072
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-00
Page B644
Feb 01/10
511-526, 528-599,
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-00-040-072-A
Subtask 54-51-00-110-078
(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.
4. Procedure
_________
Subtask 54-51-00-220-075
A. Inspection
EFF :
ALL 54-51-00
Page B645
Feb 01/10
CES
Pylon-to-Wing Aft Attachment-Shackles at RIB10
Figure 628/TASK 54-51-00-991-063
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-00
Page B646
Aug 01/09
CES
Pylon-to-Wing Aft Attachment-Shackles at RIB10
Figure 628A/TASK 54-51-00-991-063-A
R
EFF :
501-509, 511-526, 528-599, 54-51-00
Page B647
Feb 01/10
CES
**ON A/C ALL
5. Close-up
________
Subtask 54-51-00-440-072
Subtask 54-51-00-440-072-A
EFF :
ALL 54-51-00
Page B648
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
401-499,
Subtask 54-51-00-410-077
B. Close Access
(a) For the left pylon: 471CL, 472BR, 475AL, 475BL, 476AR, 476BR
(b) For the right pylon: 481BL, 482CR, 485AL, 485BL, 486AR, 486BR.
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-51-00-410-077-A
B. Close Access
(a) For the left pylon: 471DL, 471CR, 475AL, 475BL, 475AR, 475BR
(b) For the right pylon: 481CL, 481DR, 485AL, 485BL, 485AR, 485BR.
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-00
Page B649
Feb 01/10
511-526, 528-599,
CES
PYLON-TO-WING ATTACH FITTINGS - REMOVAL/INSTALLATION
____________________________________________________
TASK 54-51-17-000-001
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.
WARNING : MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT
_______
AVAILABLE.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-17
Page 401
Nov 01/09
CES
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-17
Page 402
Feb 01/10
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-17-860-050
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF :
ALL 54-51-17
Page 403
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
(4) Obey the fuel safety procedures (Ref. TASK 28-00-00-910-001) when you
do work on the fuel system.
Subtask 54-51-17-869-050
B. Aircraft Stability
Subtask 54-51-17-581-050
C. Aircraft Lifting
NOTE : It is not necessary to lift the wheels of the aircraft off the
____
ground. Lift the aircraft sufficiently to prevent an effort
caused by the reaction of the shock absorber.
Subtask 54-51-17-020-054
D. Removal of Components
(2) Remove the thrust reverser cowl doors (Ref. TASK 78-32-11-000-002).
- FOR 1000EM1
451AL, 452AR
- FOR 1000EM2
461AL, 462AR
EFF :
ALL 54-51-17
Page 404
Aug 01/09
R
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-17-020-054-A
D. Removal of Components
(1) Remove the fan cowl doors (Ref. TASK 71-13-11-000-010), (Ref. TASK
71-13-16-000-010).
- FOR 1000EM1
437AL, 438AR
- FOR 1000EM2
447AL, 448AR
Subtask 54-51-17-010-050
(a) For the left pylon: 471AL, 472AR, 414FR 521BT, 521HB.
(b) For the right pylon: 481AL, 482AR, 423FL 621BT, 621HB.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499, 501-509,
54-51-17
Page 405
Feb 01/10
511-526, 528-599,
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
Subtask 54-51-17-010-050-A
(a) For the left pylon: 471AL, 471BL, 471AR, 471BR 521BT, 521HB.
(b) For the right pylon: 481AL, 481BL, 481AR, 481BR 621BT, 621HB.
Subtask 54-51-17-020-055
EFF :
ALL 54-51-17
Page 406
Feb 01/10
CES
Temperature Sensor and the Rods
Figure 401/TASK 54-51-17-991-001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-17
Page 407
Nov 01/08
CES
Temperature Sensor and the Rods
Figure 401A/TASK 54-51-17-991-001-A
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 408
Feb 01/10
CES
Removal of the Temperature Sensor and the Rods
Figure 402/TASK 54-51-17-991-012
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-17
Page 409
Nov 01/08
CES
Removal of the Temperature Sensor and the Rods
Figure 402A/TASK 54-51-17-991-012-A
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 410
Feb 01/10
CES
**ON A/C ALL
(4) Remove the nuts (2), the washers (3), the bolts (4) and the rods (5).
Subtask 54-51-17-020-056
(1) Remove the nut (6), the bolts (7) and the ring retainer (5).
(2) Remove the nuts (10), the bolts (9) and disconnect the bonding braids
(1).
(5) Remove the lockwire from the connector (12) discard it and loosen the
connector (12).
EFF :
ALL 54-51-17
Page 411
Feb 01/10
CES
Fuel Junction in the Pylon
Figure 403/TASK 54-51-17-991-003
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-17
Page 412
Aug 01/09
CES
R Fuel Junction in the Pylon
R Figure 403A/TASK 54-51-17-991-003-C
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-17
Page 413
Aug 01/09
CES
Fuel Junction in the Pylon
Figure 403B/TASK 54-51-17-991-003-B
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 414
Feb 01/10
CES
(6) Remove the ring-retainer (3), (4).
4. Procedure
_________
Subtask 54-51-17-481-050
(2) Put the jack in position under the attach fitting at RIB1.
Install a dynamometric cell on the jack and apply an upper force of
300 +100 -100 kg (661.3866 +220.4622 -220.4622 lb).
Subtask 54-51-17-020-057
NOTE : If the time that is necessary to finish this task is more than one
____
hour, you must install the DUMMY SHACKLES-PYLON TO WING YOKES
(98D54403000000) and the DUMMY SLEEVES-PYLON TO WING YOKES
(98D54403001000).
EFF :
ALL 54-51-17
Page 415
Feb 01/10
CES
Forward Pylon-to-Wing Attach Fitting
Figure 404/TASK 54-51-17-991-005- 12 (SHEET 1)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-17
Page 416
Nov 01/08
CES
Forward Pylon-to-Wing Attach Fitting
Figure 404/TASK 54-51-17-991-005- 22 (SHEET 2)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-17
Page 417
Nov 01/08
CES
Forward Pylon-to-Wing Attach Fitting
Figure 404A/TASK 54-51-17-991-005-A12 (SHEET 1)
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 418
Feb 01/10
CES
Forward Pylon-to-Wing Attach Fitting
Figure 404A/TASK 54-51-17-991-005-A22 (SHEET 2)
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 419
Feb 01/10
CES
(2) Lock the bolt (23) with a pin wrench of the PYLON REMOVAL-WRENCH
(98D54503000000) and remove the nut (27) with a pin wrench of the
PYLON REMOVAL-WRENCH (98D54503000000).
(4) Release the nut (26), lock the sleeve (24) with a special wrench.
Remove the nut (26) the WRENCH,HOOK-ADAPTER (98D54503001000).
R (6) Remove the sleeve (24) with the extractor PYLON SHAFT EXTRACTOR RIB4-
R RIB10 (98D54003005000). Remove the sleeve at the bottom first.
NOTE : Increase the upper force continuously and equally until you
____
can remove the sleeve.
EFF :
ALL 54-51-17
Page 420
Aug 01/09
CES
TASK 54-51-17-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-17
Page 421
Nov 01/09
CES
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-17
Page 422
Feb 01/10
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-17
Page 423
Feb 01/10
511-526, 528-599,
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-17-860-052
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
(4) Obey the fuel safety procedures (Ref. TASK 28-00-00-910-001) when you
do work on the fuel system.
Subtask 54-51-17-010-061
EFF :
ALL 54-51-17
Page 424
Aug 01/09
CES
(2) Make sure that the access panels are removed:
(a) For the left pylon: 471AL, 472AR, 414FR, 521BT, 521HB
(b) For the right pylon: 481AL, 482AR, 423FL, 621BT, 621HB.
Subtask 54-51-17-010-061-A
(a) For the left pylon: 471AL, 471BL, 471AR, 471BR ,521BT, 521HB
(b) For the right pylon: 481AL, 481BL, 481AR, 481BR ,621BT, 621HB.
4. Procedure
_________
Subtask 54-51-17-160-050
EFF :
ALL 54-51-17
Page 425
Feb 01/10
CES
**ON A/C ALL
(1) Clean the parts retained from the removed component with CLEANING
AGENTS (Material No. 11-004) and MISCELLANEOUS (Material No. 19-003).
(2) Before installation, make sure that the nuts (26) are in the correct
condition. If necessary, replace the nuts (26).
Subtask 54-51-17-420-054
(1) Apply the COMMON GREASE (Material No. 04-004) to the sleeves, the
spigot and all the friction surfaces.
EFF :
ALL 54-51-17
Page 426
Feb 01/10
CES
(3) Install the sleeves (24). Install the top sleeve first.
NOTE : You can install the sleeve more easily if you change the force
____
that the jack applies to the attach fitting.
NOTE : You must put the nuts, the cotter pins and the lockwashers:
____
- for the upper attachments, in the outer side of the pylons
(always symmetrically to the pylon centerline)
- for the inner attachments, in the inner side of the pylons
(always symmetrically to the pylon centerline).
(5) Install the nut (26). Lock the sleeve (24) with a special wrench of
the WRENCH,HOOK-ADAPTER (98D54503001000). TORQUE the nut (26) to
between 4 and 5 m.daN (29.49 and 36.87 lbf.ft). Use a pin wrench of
the WRENCH,HOOK-ADAPTER (98D54503001000) and a torque wrench.
(8) Lock the bolts (23) with a pin wrench of the PYLON REMOVAL-WRENCH
(98D54503000000) and install the nut (27) with a pin wrench of the
PYLON REMOVAL-WRENCH (98D54503000000).
(9) TORQUE the nut (27) to between 4 and 5 m.daN (29.49 and 36.87
lbf.ft).
(10) Safety the nut (27) with the cotter pins (28).
Subtask 54-51-17-081-050
R (1) Remove the force applied to the jack. Remove the JACK ADAPTOR - PYLON
R (98D07203015000) from below the attach fitting at RIB1.
EFF :
ALL 54-51-17
Page 427
Nov 01/09
CES
5. Close-up
________
Subtask 54-51-17-420-055
(4) Install the ring-retainer (3) and the ring-retainer (4) on the
connectors (12).
(10) Install the bonding braids (1), the bolts (9) and the nuts (10).
Tighten the nuts (10).
EFF :
ALL 54-51-17
Page 428
Feb 01/10
CES
(11) Install the ring retainers (5), the bolts (7) and the nut (6).
Tighten the nuts (6).
Subtask 54-51-17-420-056
(1) Install the rods (5), the bolts (4), the washers (3) and the nuts
(2). Tighten the nuts.
(2) Safety the nuts (2) with the cotter pins (1).
(3) Remove the blanking caps from the electrical connectors. Connect the
temperature sensor (6):
- For the left pylon: 6HA1
- For the right pylon: 6HA2.
Subtask 54-51-17-586-050
C. Aircraft Lowering
EFF :
ALL 54-51-17
Page 429
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
401-499,
Subtask 54-51-17-410-050
(a) For the left pylon: 471AL, 472AR, 414FR, 521BT, 521HB
(b) For the right pylon: 481AL, 482AR, 423FL, 621BT, 621HB.
Subtask 54-51-17-410-050-A
(a) For the left pylon: 471AL, 471BL, 471AR, 471BR ,521BT, 521HB
(b) For the right pylon: 481AL, 481BL, 481AR, 481BR ,621BT, 621HB.
Subtask 54-51-17-420-057
E. Installation of Components
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-17
Page 430
Feb 01/10
511-526, 528-599,
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-17-420-057-A
E. Installation of Components
(3) Install the fan cowl doors (Ref. TASK 71-13-11-400-010), (Ref. TASK
71-13-16-400-010):
- FOR 1000EM1
437AL, 438AR
- FOR 1000EM2
447AL, 448AR.
Subtask 54-51-17-942-050
F. Close Access
(1) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 54-51-17
Page 431
Feb 01/10
CES
TASK 54-51-17-000-002
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.
WARNING : MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT
_______
AVAILABLE.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-17
Page 432
Nov 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-17-860-051
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF :
ALL 54-51-17
Page 433
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
(4) Obey the fuel safety procedures (Ref. TASK 28-00-00-910-001) when you
do work on the fuel system.
Subtask 54-51-17-869-053
B. Aircraft Stability
Subtask 54-51-17-581-052
C. Aircraft Lifting
NOTE : It is not necessary to lift the wheels of the aircraft off the
____
ground. Lift the aircraft sufficiently to prevent an effort
caused by the reaction of the shock absorber.
Subtask 54-51-17-020-058
D. Removal of Components
(2) Remove the thrust reverser cowls doors (Ref. TASK 78-32-11-000-002).
- FOR 1000EM1
451AL, 452AR
- FOR 1000EM2
461AL, 462AR
EFF :
ALL 54-51-17
Page 434
Nov 01/09
R
CES
(4) Remove the aft fixed fairing (Ref. TASK 54-54-00-000-001).
Subtask 54-51-17-020-058-A
D. Removal of Components
(1) Remove the fan cowls doors (Ref. TASK 71-13-11-000-010), (Ref. TASK
71-13-16-000-010).
- FOR 1000EM1
437AL, 438AR
- FOR 1000EM2
447AL, 448AR
Subtask 54-51-17-010-051
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-17
Page 435
Feb 01/10
511-526, 528-599,
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
Subtask 54-51-17-010-051-A
4. Procedure
_________
Subtask 54-51-17-481-051
(2) Put the jack in position under the attach fitting at RIB1.
Install a dynamometric cell on the jack and apply an upper force of 0
kg (0.0000 lb) to 150 kg (330.6933 lb).
Subtask 54-51-17-020-059
EFF :
ALL 54-51-17
Page 436
Feb 01/10
CES
Pylon-to-Wing Aft Attach Fitting
Figure 405/TASK 54-51-17-991-007
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-17
Page 437
Aug 01/09
CES
R **ON A/C 501-509, 511-526, 528-599,
(2) Lock the bolt (31) with a pin wrench of the PYLON REMOVAL-WRENCH
(98D54503000000).
Remove the nut (40) with a pin wrench of the PYLON REMOVAL-WRENCH
(98D54503000000).
(4) Release the nut (41). Lock the sleeve (30) with a special wrench.
Remove the nut (41) with a pin wrench of the PYLON REMOVAL-WRENCH
(98D54503000000).
(6) Remove the sleeve (30) with the extractor PYLON SHAFT EXTRACTOR RIB4-
RIB10 (98D54003005000)
(8) Lock the bolt (33) with a pin wrench of the PYLON REMOVAL-WRENCH
(98D54503000000).
Remove the nut (37) with a pin wrench of the PYLON REMOVAL-WRENCH
(98D54503000000).
(10) Release the nut (36). Lock the sleeve (32) with a special wrench.
Remove the nut (36) with a pin wrench of the PYLON REMOVAL-WRENCH
(98D54503000000).
(12) Remove the sleeve (32) with the extractor PYLON SHAFT EXTRACTOR RIB4-
RIB10 (98D54003005000).
NOTE : Increase the upper force continuously and equally until you
____
can remove the sleeve.
EFF :
ALL 54-51-17
Page 438
Feb 01/10
CES
Pylon-to-Wing Aft Attach Fitting
Figure 405A/TASK 54-51-17-991-007-A
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 439
Feb 01/10
CES
TASK 54-51-17-400-002
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-17
Page 440
Nov 01/09
CES
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-17
Page 441
Aug 01/09
R
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-17-860-053
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
(4) Obey the fuel safety procedures (Ref. TASK 28-00-00-910-001) when you
do work on the fuel system.
EFF :
ALL 54-51-17
Page 442
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
401-499,
Subtask 54-51-17-010-063
Subtask 54-51-17-010-063-A
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-17
Page 443
Feb 01/10
511-526, 528-599,
CES
**ON A/C ALL
4. Procedure
_________
Subtask 54-51-17-160-051
(1) Clean the parts retained from the removed component with CLEANING
AGENTS (Material No. 11-004) and MISCELLANEOUS (Material No. 19-003).
(a) The lockwashers (35) and (42) and the nuts (36) and (41) at RIB10
are in the correct condition. If necessary, replace the
lockwashers (35), the lockwasher (42), the nuts (36) and the nut
(41) ((Ref. TASK 54-51-17-000-003) and (Ref. TASK 54-51-17-400-
003)).
EFF :
ALL 54-51-17
Page 444
Feb 01/10
CES
Subtask 54-51-17-420-058-A
(2) Apply the COMMON GREASE (Material No. 04-004) to the sleeves, the
spigot and all the friction surfaces.
NOTE : You can install the sleeve more easily if you change the force
____
that the jack applies to the attach fitting.
(5) Install the nut (36). Lock the sleeve (32) with a special wrench.
TORQUE the nut (36) to between 1 and 12 m.daN (88.49 and 1061.94
lbf.in). Use a pin wrench of the PYLON REMOVAL-WRENCH
(98D54503000000) and a torque wrench.
(8) Lock the bolts (33) with a pin wrench of the PYLON REMOVAL-WRENCH
(98D54503000000). Install the nut (37) with a pin wrench of the PYLON
REMOVAL-WRENCH (98D54503000000).
(9) TORQUE the nut (37) to between 1 and 12 m.daN (88.49 and 1061.94
lbf.in).
(10) Safety the nut (37) with the cotter pins (38).
EFF :
ALL 54-51-17
Page 445
Feb 01/10
CES
(11) Put the sleeve (30) in position.
(13) Install the nut (41). Lock the sleeve (30) with a special wrench.
TORQUE the nut (41) to between 1 and 12 m.daN (88.49 and 1061.94
lbf.in). Use a pin wrench of the PYLON REMOVAL-WRENCH
(98D54503000000) and a torque wrench.
(16) Lock the bolt (31) with a pin wrench of the PYLON REMOVAL-WRENCH
(98D54503000000). Install the nut (40).
(17) TORQUE the nut (40) to between 1 and 12 m.daN (88.49 and 1061.94
lbf.in).
(18) Safety the nut (40) with the cotter pins (39).
Subtask 54-51-17-081-051
R (2) Remove the JACK ADAPTOR - PYLON (98D07203015000) from below the
R attach fitting at RIB1.
5. Close-up
________
Subtask 54-51-17-586-051
A. Aircraft Lowering
EFF :
ALL 54-51-17
Page 446
Nov 01/09
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
401-499,
Subtask 54-51-17-410-051
B. Installation of Panels
Subtask 54-51-17-410-051-A
B. Installation of Panels
Subtask 54-51-17-420-059
C. Installation of Components
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-17
Page 447
Feb 01/10
511-526, 528-599,
CES
(4) Install the fan cowl doors (Ref. TASK 71-13-11-400-041):
- FOR 1000EM1
437AL, 438AR
- FOR 1000EM2
447AL, 448AR.
Subtask 54-51-17-420-059-A
C. Installation of Components
(4) Install the fan cowl doors (Ref. TASK 71-13-11-400-010), (Ref. TASK
71-13-16-400-010):
- FOR 1000EM1
437AL, 438AR
- FOR 1000EM2
447AL, 448AR.
Subtask 54-51-17-942-051
D. Close Access
(1) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 54-51-17
Page 448
Feb 01/10
CES
TASK 54-51-17-000-003
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
-------------------------------------------------------------------------------
R
EFF :
ALL 54-51-17
Page 449
Aug 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-17-941-057
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
(4) Obey the fuel safety procedures (Ref. TASK 28-00-00-910-001) when you
do work on the fuel system.
Subtask 54-51-17-040-050
EFF :
ALL 54-51-17
Page 450
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-17-040-050-A
Subtask 54-51-17-010-054
C. Get Access
(1) Put the access platform in position below the applicable pylon
rear-attachment point, zone 475 (485).
(2) Remove the applicable aft attach fitting (Ref. TASK 54-51-17-000-
002).
4. Procedure
_________
Subtask 54-51-17-020-060
CAUTION : DO NOT DAMAGE THE REAR BEARING ATTACHMENT WHEN YOU REMOVE THE
_______
BEARING.
(1) Bend the tab washer (2) to release the slotted nut (1).
EFF :
ALL 54-51-17
Page 451
Feb 01/10
CES
Pylon Rear Attachment at RIB10
Figure 406/TASK 54-51-17-991-013
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-17
Page 452
Aug 01/09
CES
Pylon Rear Attachment at RIB10
Figure 406A/TASK 54-51-17-991-013-A
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 453
Feb 01/10
CES
(2) Hold the bearing (4) with the WRENCH-CASTELLETED (98D54003006202) and
use the WRENCH-CASTELLETED (98D54003006200) to remove the nut (1).
EFF :
ALL 54-51-17
Page 454
Aug 01/09
R
CES
TASK 54-51-17-400-003
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. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-17
Page 455
Aug 01/09
R
CES
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-17
Page 456
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-51-17-941-058
A. Safety Precautions
(1) Make sure that the engine (1) and (2) shutdown occurred not less than
5 minutes before you do this procedure.
(2) Make sure that a warning notice is in position in the cockpit to tell
persons not to start engine.
(3) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton
switch is off and put a warning notice to tell persons not to use it.
(4) Make sure that the APU BLEED pushbutton switch is released (ON legend
Off) and install a warning notice to tell persons not to use it.
(5) Make sure that the fuel safety procedure instructions are obeyed
(Ref. TASK 28-00-00-910-001).
(6) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-
00-481-041).
Subtask 54-51-17-941-058-A
A. Safety Precautions
(1) Make sure that the engine (1) and (2) shutdown occurred not less than
5 minutes before you do this procedure.
(2) Make sure that a warning notice is in position in the cockpit to tell
persons not to start engine.
(3) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton
switch is off and put a warning notice to tell persons not to use it.
EFF :
ALL 54-51-17
Page 457
Feb 01/10
CES
(4) Make sure that the APU BLEED pushbutton switch is released (ON legend
Off) and install a warning notice to tell persons not to use it.
(5) Make sure that the fuel safety procedure instructions are obeyed
(Ref. TASK 28-00-00-910-001).
(6) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-
00-040-012).
4. Procedure
_________
Subtask 54-51-17-110-050
(1) Clean the parts retained from the removed component with CLEANING
AGENTS (Material No. 11-004) and MISCELLANEOUS (Material No. 19-003).
(2) Use a plastic spatula to remove unwanted material from the interface
of the pylon rear attachment.
EFF :
ALL 54-51-17
Page 458
Feb 01/10
CES
(3) Clean the interface of the bearing (4) and the pylon rear attachment
(3) with CLEANING AGENTS (Material No. 11-004) and a MISCELLANEOUS
(Material No. 19-003).
(4) Examine the pylon rear attachment and adjacent structure for:
- cracks
- damaged paint and sealant
- distortion
- correct condition of all fasteners and safety devices.
Subtask 54-51-17-420-060
(1) Apply the COMMON GREASE (Material No. 04-004) to the interface of the
bearing (4) and the pylon rear attachment.
(2) Install a new bearing (4) in the pylon rear attachment (3) with the
WRENCH-CASTELLETED (98D54003006202).
(3) Install the new tab washer tab washer (2). Make sure that the
internal tab of the washer (2) is engaged in the slot on the bearing
(4).
NOTE : You must lightly bend the tabs of the tab washer (2) before
____
you install the slotted nut (1). This will make it easier to
bend the tabs when you subsequently lock the slotted nut.
(4) Install the slotted nut (1) on the bearing (4) with the chamfered
face against the tab washer (2).
EFF :
ALL 54-51-17
Page 459
Feb 01/10
CES
(6) Safety the slotted nut (1) with the tab washer (2).
5. Close-up
________
Subtask 54-51-17-410-054
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
(2) Install the applicable aft attach fitting (Ref. TASK 54-51-17-400-
002).
Subtask 54-51-17-440-050
Subtask 54-51-17-440-050-A
Subtask 54-51-17-942-056
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
EFF :
ALL 54-51-17
Page 460
Feb 01/10
CES
PYLON-TO-WING ATTACH FITTINGS - INSPECTION/CHECK
________________________________________________
TASK 54-51-17-200-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-17-020-050
4. Procedure
_________
Subtask 54-51-17-210-050
(1) Do a visual inspection of the yokes attached to the main frame and
the wing, the fail-safe bolts, the shackles and the sleeves.
EFF :
ALL 54-51-17
Page 601
Nov 01/07
CES
-------------------------------------------------------------------------------
| | Yoke | Shackles | Fail-safe | Sleeves |
| | Pylon side | | bolts | |
| | Wing side | | | |
R -------------------------------------------------------------------------------
| Superficial | Repair, refer to | Ref. 54-51-00| Replace | Replace |
| wear | the manufacturers | P. Block 601 | | |
| | instructions | | | |
R -------------------------------------------------------------------------------
| Deformation | Repair, refer to | Replace | Replace | Replace |
| | the manufacturers | | | |
| | instructions | | | |
R -------------------------------------------------------------------------------
| Corrosion | Repair, refer to | Ref. 54-51-00| | Replace |
| | the manufacturers | P. Block 601 | | |
| | instructions | | | |
R -------------------------------------------------------------------------------
| Structural | Repair, refer to | Replace | Replace | Replace |
| defects | the manufacturers | | | |
| | instructions | | | |
R -------------------------------------------------------------------------------
| Bore | Replace the | Replace | | Replace |
| deformation | bushes | | | |
R -------------------------------------------------------------------------------
| Wear on | Replace the | Replace | | Replace |
| bore | bushes | | | |
-------------------------------------------------------------------------------
5. Close-up
________
Subtask 54-51-17-420-050
EFF :
ALL 54-51-17
Page 602
Aug 01/08
CES
TASK 54-51-17-200-002
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-17-020-051
4. Procedure
_________
Subtask 54-51-17-210-051
(1) Do a visual inspection of the yokes attached to the main frame and
the wing, the fail-safe bolts, the shackles and the sleeves.
EFF :
ALL 54-51-17
Page 603
Nov 01/07
CES
-------------------------------------------------------------------------------
| | Yoke | Shackles | Fail-safe | Sleeves |
| | Pylon side | | bolts | |
| | Wing side | | | |
R -------------------------------------------------------------------------------
| Superficial | Repair, refer to | Ref. 54-51-00| Replace | Replace |
| wear | the manufacturers | P. Block 601 | | |
| | instructions | | | |
R -------------------------------------------------------------------------------
| Deformation | Repair, refer to | Replace | Replace | Replace |
| | the manufacturers | | | |
| | instructions | | | |
R -------------------------------------------------------------------------------
| Corrosion | Repair, refer to | Ref. 54-51-00| | Replace |
| | the manufacturers | P. Block 601 | | |
| | instructions | | | |
R -------------------------------------------------------------------------------
| Structural | Repair, refer to | Replace | Replace | Replace |
| defects | the manufacturers | | | |
| | instructions | | | |
R -------------------------------------------------------------------------------
| Bore | Replace the | Replace | | Replace |
| out-of-round | bushes | | | |
R -------------------------------------------------------------------------------
| Bore wear | Replace the | Replace | | Replace |
| | bushes | | | |
R -------------------------------------------------------------------------------
5. Close-up
________
Subtask 54-51-17-420-051
EFF :
ALL 54-51-17
Page 604
Aug 01/08
CES
TASK 54-51-17-200-003
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 54-51-17
Page 605
May 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-17-941-052
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
EFF :
ALL 54-51-17
Page 606
Feb 01/10
CES
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2)
Subtask 54-51-17-040-051
Subtask 54-51-17-040-051-A
Subtask 54-51-17-020-061
Subtask 54-51-17-941-053
D. Get Access
EFF :
ALL 54-51-17
Page 607
Feb 01/10
CES
4. Procedure
_________
Subtask 54-51-17-220-068
(1) Do an inspection of the shackles for corrosion and make sure that the
corrosion damage is in the permitted limits.
EFF :
ALL 54-51-17
Page 608
Feb 01/10
CES
Permitted Corrosion on the Shackles
Figure 601/TASK 54-51-17-991-008
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-17
Page 609
Nov 01/08
CES
Permitted Corrosion on the Shackles
Figure 601A/TASK 54-51-17-991-008-A
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 610
Feb 01/10
CES
(f) If the damaged areas:
- are around the bore on the two sides and:
- Maximum dimension of the defect measured radially is less than
25 mm (0.9842 in.): the sum of the maximum depth of the defects
on the two sides must be 0.6 mm (0.0236 in.).
Subtask 54-51-17-220-050
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| A | 1.5738 | 1.5742 | | | 1.5731 | | |
| OD 1 |(39.974) |(39.984) | | |(39.956) | | |
| | | | 0.0006 | 0.0019 | | | 0.0040|
| | | | (0.015) | (0.048) | | |(0.101) |
| A | 1.5748 | 1.5757 | | | | 1.5771 | |
| ID 2 |(39.999) |(40.022) | | | |(40.058) | |
-------------------------------------------------------------------------------
EFF :
ALL 54-51-17
Page 611
Feb 01/10
CES
Forward Attach Fitting
Figure 602/TASK 54-51-17-991-009
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-17
Page 612
Nov 01/08
CES
Forward Attach Fitting
Figure 602A/TASK 54-51-17-991-009-A
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 613
Feb 01/10
CES
Subtask 54-51-17-220-051
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| A | 1.5738 | 1.5742 | | | 1.5731 | | |
| OD 1 |(39.974) |(39.984) | | |(39.956) | | |
| | | | 0.0006 | 0.0019 | | | 0.0040|
| | | | (0.015) | (0.048) | | |(0.101) |
| A | 1.5748 | 1.5757 | | | | 1.5771 | |
| ID 4 |(39.999) |(40.022) | | | |(40.058) | |
-------------------------------------------------------------------------------
Subtask 54-51-17-220-052
EFF :
ALL 54-51-17
Page 614
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| A | 1.5738 | 1.5742 | | | 1.5731 | | |
| OD 1 |(39.974) |(39.984) | | |(39.956) | | |
| | | | 0.0006 | 0.0019 | | | 0.0040|
| | | | (0.015) | (0.048) | | |(0.101) |
| A | 1.5748 | 1.5757 | | | | 1.5771 | |
| ID 3 |(39.999) |(40.022) | | | |(40.058) | |
-------------------------------------------------------------------------------
Subtask 54-51-17-220-053
EFF :
ALL 54-51-17
Page 615
Feb 01/10
CES
**ON A/C ALL
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| A | 1.7340 | 1.7346 | | | 1.7337 | | |
| OD 2 |(44.043) |(44.058) | | |(44.035) | | |
| | | | -0.0023 | -0.0007 | | | 0.0000|
| | | |-(0.058) |-(0.017) | | |(0.000) |
| A | 1.7323 | 1.7333 | | | | 1.7337 | |
| ID 7 |(44.000) |(44.025) | | | |(44.035) | |
-------------------------------------------------------------------------------
Subtask 54-51-17-220-054
EFF :
ALL 54-51-17
Page 616
Feb 01/10
CES
**ON A/C ALL
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| A | 1.7340 | 1.7346 | | | 1.7337 | | |
| OD 4 |(44.043) |(44.058) | | |(44.035) | | |
| | | | -0.0023 | -0.0007 | | | 0.0000|
| | | |-(0.058) |-(0.017) | | |(0.000) |
| A | 1.7323 | 1.7333 | | | | 1.7337 | |
| ID 5 |(44.000) |(44.025) | | | |(44.035) | |
-------------------------------------------------------------------------------
Subtask 54-51-17-220-055
EFF :
ALL 54-51-17
Page 617
Feb 01/10
CES
**ON A/C ALL
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| A | 1.7340 | 1.7346 | | | 1.7337 | | |
| OD 4 |(44.043) |(44.058) | | |(44.035) | | |
| | | | -0.0023 | -0.0007 | | | 0.0000|
| | | |-(0.058) |-(0.017) | | |(0.000) |
| A | 1.7323 | 1.7333 | | | | 1.7337 | |
| ID 6 |(44.000) |(44.025) | | | |(44.035) | |
-------------------------------------------------------------------------------
Subtask 54-51-17-220-056
EFF :
ALL 54-51-17
Page 618
Feb 01/10
CES
**ON A/C ALL
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| A | 1.7340 | 1.7346 | | | 1.7337 | | |
| OD 3 |(44.043) |(44.058) | | |(44.035) | | |
| | | | -0.0023 | -0.0007 | | | 0.0000|
| | | |-(0.058) |-(0.017) | | |(0.000) |
| A | 1.7323 | 1.7333 | | | | 1.7337 | |
| ID 5 |(44.000) |(44.025) | | | |(44.035) | |
-------------------------------------------------------------------------------
Subtask 54-51-17-220-057
EFF :
ALL 54-51-17
Page 619
Feb 01/10
CES
**ON A/C ALL
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| A | 1.7340 | 1.7346 | | | 1.7337 | | |
| OD 3 |(44.043) |(44.058) | | |(44.035) | | |
| | | | -0.0023 | -0.0007 | | | 0.0000|
| | | |-(0.058) |-(0.017) | | |(0.000) |
| A | 1.7323 | 1.7333 | | | | 1.7337 | |
| ID 6 |(44.000) |(44.025) | | | |(44.035) | |
-------------------------------------------------------------------------------
Subtask 54-51-17-220-058
EFF :
ALL 54-51-17
Page 620
Feb 01/10
CES
**ON A/C ALL
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| A | 1.5738 | 1.5742 | | | 1.5731 | | |
| OD 1 |(39.974) |(39.984) | | |(39.956) | | |
| | | | 0.0006 | 0.0020 | | | 0.0040|
| | | | (0.015) | (0.050) | | |(0.101) |
| A | 1.5748 | 1.5758 | | | | 1.5771 | |
| ID 8 |(39.999) |(40.025) | | | |(40.058) | |
-------------------------------------------------------------------------------
Subtask 54-51-17-220-059
EFF :
ALL 54-51-17
Page 621
Feb 01/10
CES
**ON A/C ALL
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| A | 1.5738 | 1.5742 | | | 1.5731 | | |
| OD 1 |(39.974) |(39.984) | | |(39.956) | | |
| | | | 0.0006 | 0.0020 | | | 0.0040|
| | | | (0.015) | (0.050) | | |(0.101) |
| A | 1.5748 | 1.5758 | | | | 1.5771 | |
| ID 9 |(39.999) |(40.025) | | | |(40.058) | |
-------------------------------------------------------------------------------
Subtask 54-51-17-220-060
EFF :
ALL 54-51-17
Page 622
Feb 01/10
CES
Spigot Attach Fitting
Figure 603/TASK 54-51-17-991-010
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-17
Page 623
Nov 01/08
CES
Spigot Attach Fitting
Figure 603A/TASK 54-51-17-991-010-A
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 624
Feb 01/10
CES
**ON A/C ALL
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| A | 2.8335 | 2.8343 | | | 2.8327 | | |
| OD 13 |(71.970) |(71.991) | | |(71.950) | | |
| | | | 0.0003 | 0.0023 | | | 0.0047|
| | | | (0.007) | (0.058) | | |(0.119) |
| A | 2.8346 | 2.8358 | | | | 2.8374 | |
| ID 12 |(71.998) |(72.029) | | | |(72.069) | |
-------------------------------------------------------------------------------
Subtask 54-51-17-220-061
EFF :
ALL 54-51-17
Page 625
Feb 01/10
CES
**ON A/C ALL
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| A | 4.3293 | 4.3307 | | | 4.3284 | | |
| OD 12 |(109.964)|(109.999)| | |(109.941)| | |
| | | | 0.0005 | 0.0027 | | | 0.0055|
| | | | (0.012) | (0.068) | | |(0.139) |
| A | 4.3312 | 4.3320 | | | | 4.3339 | |
| ID 10 |(110.012)|(110.032)| | | |(110.080)| |
-------------------------------------------------------------------------------
Subtask 54-51-17-220-062
EFF :
ALL 54-51-17
Page 626
Feb 01/10
CES
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| A | 4.3293 | 4.3307 | | | 4.3284 | | |
| OD 12 |(109.964)|(109.999)| | |(109.941)| | |
| | | | 0.0005 | 0.0027 | | | 0.0055|
| | | | (0.012) | (0.068) | | |(0.139) |
| A | 4.3312 | 4.3320 | | | | 4.3339 | |
| ID 11 |(110.012)|(110.032)| | | |(110.080)| |
-------------------------------------------------------------------------------
5. Close-up
________
Subtask 54-51-17-420-061
Subtask 54-51-17-440-051
Subtask 54-51-17-440-051-A
EFF :
ALL 54-51-17
Page 627
Feb 01/10
CES
**ON A/C ALL
TASK 54-51-17-200-004
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 54-51-17
Page 628
May 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-17-941-054
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2)
EFF :
ALL 54-51-17
Page 629
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
401-499,
Subtask 54-51-17-040-052
Subtask 54-51-17-040-052-A
Subtask 54-51-17-020-062
Subtask 54-51-17-941-055
D. Get Access
EFF :
ALL 54-51-17
Page 630
Feb 01/10
CES
4. Procedure
_________
Subtask 54-51-17-220-063
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| B | 2.1280 | 2.1288 | | | 2.1278 | | |
| OD 15 |(54.051) |(54.071) | | |(54.046) | | |
| | | | -0.0028 | -0.0008 | | | 0.0000|
| | | |-(0.071) |-(0.020) | | |(0.000) |
| B | 2.1260 | 2.1272 | | | | 2.1278 | |
| ID 14 |(54.000) |(54.030) | | | |(54.046) | |
-------------------------------------------------------------------------------
EFF :
ALL 54-51-17
Page 631
Feb 01/10
CES
Aft Attach Fitting
Figure 604/TASK 54-51-17-991-011
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-17
Page 632
Nov 01/08
CES
Aft Attach Fitting
Figure 604A/TASK 54-51-17-991-011-A
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 633
Feb 01/10
CES
Subtask 54-51-17-220-064
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| B | 1.8888 | 1.8894 | | | 1.8881 | | |
| OD 16 |(47.975) |(47.990) | | |(47.957) | | |
| | | | 0.0004 | 0.0019 | | | 0.0040|
| | | | (0.010) | (0.048) | | |(0.101) |
| B | 1.8898 | 1.8907 | | | | 1.8921 | |
| ID 15 |(48.000) |(48.023) | | | |(48.059) | |
-------------------------------------------------------------------------------
Subtask 54-51-17-220-065
(1) Do a detailed inspection of the aft attach fitting and make sure that
the dimensions are correct.
EFF :
ALL 54-51-17
Page 634
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| B | 1.8127 | 1.8133 | | | 1.8125 | | |
| OD 17 |(46.042) |(46.057) | | |(46.037) | | |
| | | | -0.0023 | -0.0007 | | | 0.0000|
| | | |-(0.058) |-(0.017) | | |(0.000) |
| B | 1.8110 | 1.8120 | | | | 1.8125 | |
| ID 14 |(45.999) |(46.024) | | | |(46.037) | |
-------------------------------------------------------------------------------
Subtask 54-51-17-220-066
EFF :
ALL 54-51-17
Page 635
Feb 01/10
CES
R **ON A/C ALL
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| B | 1.5738 | 1.5744 | | | 1.5731 | | |
| OD 18 |(39.974) |(39.989) | | |(39.956) | | |
| | | | 0.0004 | 0.0020 | | | 0.0040|
| | | | (0.010) | (0.050) | | |(0.101) |
| B | 1.5748 | 1.5758 | | | | 1.5771 | |
| ID 17 |(39.999) |(40.025) | | | |(40.058) | |
-------------------------------------------------------------------------------
Subtask 54-51-17-220-067
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| B | 1.5738 | 1.5744 | | | 1.5731 | | |
| OD 18 |(39.974) |(39.989) | | |(39.956) | | |
| | | | 0.0004 | 0.0020 | | | 0.0040|
| | | | (0.010) | (0.050) | | |(0.101) |
| B | 1.5748 | 1.5758 | | | | 1.5771 | |
| ID 19 |(39.999) |(40.025) | | | |(40.058) | |
-------------------------------------------------------------------------------
EFF :
ALL 54-51-17
Page 636
Nov 01/07
CES
5. Close-up
________
Subtask 54-51-17-420-062
Subtask 54-51-17-440-052
Subtask 54-51-17-440-052-A
Subtask 54-51-17-942-055
C. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-17
Page 637
Feb 01/10
CES
PYLON-TO-WING ATTACH FITTINGS - REPAIRS
_______________________________________
TASK 54-51-17-300-001
WARNING : MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT
_______
AVAILABLE.
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 : USE THE EQUIPMENT AND PRECAUTIONS NECESSARY FOR ENVIRONMENTAL CONTROL
_______
WHEN YOU GRIND/SAND/HONE THE BUSHES OF THE SHACKLES AT RIB10. THESE
BUSHES CONTAIN COPPER BERYLLIUM AND CAN CAUSE TOXIC BERYLLIUM DUST.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-17
Page 801
May 01/04
CES
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-17
Page 802
Nov 01/08
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-17-861-050
Subtask 54-51-17-941-059
B. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-51-17-010-055
C. Get Access
EFF :
ALL 54-51-17
Page 803
Feb 01/10
CES
Subtask 54-51-17-020-063
4. Procedure
_________
Subtask 54-51-17-020-064
(1) Remove and discard the bushes (2) and (3) from the shackles (1).
(2) Clean the shackles (1) with CLEANING AGENTS (Material No. 11-003) and
a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
Subtask 54-51-17-220-069
(2) Make sure that there is no damage and that diameters D1 and D2 of the
shackle bores are in the tolerance.
(a) Rebore the shackles (1) to the repair dimension(s) R1 and/or R2.
EFF :
ALL 54-51-17
Page 804
Feb 01/10
CES
Subtask 54-51-17-420-063
(1) Make sure that the surface of the shackle bores is clean. If
necessary, clean the surface with CLEANING AGENTS (Material No. 11-
003) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-
003).
(2) Soak the new bushes (2) and bushes (3) in nitrogen liquid.
(3) Install the bushes (2) and (3) in the shackles (1).
(4) Apply a bead of SEALANTS (Material No. 09-016B) on the shackles (1)
and the bushes (2) and (3).
(5) Rebore the bushes (2) and (3) to the diameters D3 and D4 with the
center-to-center distances X1, X2 and X3.
(6) Clean the shackles (1) with CLEANING AGENTS (Material No. 11-003) and
a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
5. Close-up
________
Subtask 54-51-17-420-064
Subtask 54-51-17-942-057
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 54-51-17-862-050
EFF :
ALL 54-51-17
Page 805
Nov 01/07
R
CES
Reboring of Bushes at RIB10
Figure 801/TASK 54-51-17-991-014- 12 (SHEET 1)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-17
Page 806
Aug 01/09
CES
Reboring of Bushes at RIB10
Figure 801/TASK 54-51-17-991-014- 22 (SHEET 2)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-51-17
Page 807
Aug 01/09
CES
Reboring of Bushes at RIB10
Figure 801A/TASK 54-51-17-991-014-A12 (SHEET 1)
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 808
Feb 01/10
CES
Reboring of Bushes at RIB10
Figure 801A/TASK 54-51-17-991-014-A22 (SHEET 2)
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 809
Feb 01/10
CES
TASK 54-51-17-300-002
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.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-17
Page 810
Feb 01/10
CES
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-17
Page 811
Feb 01/10
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-17
Page 812
Feb 01/10
511-526, 528-599,
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-17
Page 813
Feb 01/10
511-526, 528-599,
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-17-861-052
Subtask 54-51-17-941-067
B. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF :
ALL 54-51-17
Page 814
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
(4) Obey the fuel safety procedures (Ref. TASK 28-00-00-910-001) when you
do work on the fuel system.
Subtask 54-51-17-865-050
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU ENGINE/2/HP FUEL SOV 1KC2 A02
49VU ENGINE/1/HP FUEL SOV 1KC1 A01
49VU ANTI ICE/PROBES/AOA/1 4DA1 D04
49VU ANTI ICE/PROBES/PHC/1 2DA1 D03
49VU ANTI ICE/PROBES/PITOT/1 3DA1 D02
121VU HYDRAULIC/HYD POWER/Y 3803GX N30
122VU ANTI ICE/ENG/2 1DN2 W10
122VU ANTI ICE/PROBES/PHC/3 2DA3 Y16
122VU ANTI ICE/PROBES/2/TAT 1DA2 Y15
122VU ANTI ICE/PROBES/2/PITOT 3DA2 Y14
122VU ANTI ICE/PROBES/2/AOA 4DA2 Y13
R 122VU ANTI ICE/PROBES/PHC/2 2DA2 Y12
122VU ANTI ICE/PROBES/2/STATIC 5DA2 Y11
122VU ANTI ICE/PROBES/3/PITOT 3DA3 Z16
122VU ANTI ICE/PROBES/3/AOA 4DA3 Z15
122VU ANTI ICE/PROBES/1/STATIC 5DA1 Z13
122VU ANTI ICE/PROBES/1/TAT 1DA1 Z12
123VU Y HYD/ELEC/PUMP 3802GX AB06
123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
Subtask 54-51-17-864-050
(1) Make sure that the hydraulic systems are depressurized (Ref. TASK 29-
00-00-864-001).
EFF :
ALL 54-51-17
Page 815
Feb 01/10
CES
Subtask 54-51-17-020-078
E. Removal of Components
4. Procedure
_________
NOTE : This procedure is the same for the left and the right pylon.
____
Subtask 54-51-17-020-079
NOTE : The procedure that follows is given for one side and is the
____
same for the other side.
EFF :
ALL 54-51-17
Page 816
Feb 01/10
CES
(b) Put the expander (2) between the two fittings.
NOTE : You must be careful to put the stops (1) and the expander
____
(2) in position correctly to prevent damage to the
fittings during removal of the bushes.
(c) Install the washer (3) and the nut (4) on the extractor (5).
(e) Put the end of the extractor (5) in position between the two
center bushes.
(g) Remove the internal center bush (7). To do this, turn the nut
(4).
NOTE : The procedure that follows is given for one side and is the
____
same for the other side.
(a) Remove the internal bushes (10) and the external center bushes
(11):
EFF :
ALL 54-51-17
Page 817
Feb 01/10
CES
Removal of the Internal Center Bushes
Figure 802/TASK 54-51-17-991-015- 12 (SHEET 1)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-17
Page 818
Feb 01/08
CES
Removal of the Internal Center Bushes
Figure 802/TASK 54-51-17-991-015- 22 (SHEET 2)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-17
Page 819
Feb 01/08
CES
Removal of the Internal Center Bushes
Figure 802A/TASK 54-51-17-991-015-A12 (SHEET 1)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-17
Page 820
Nov 01/08
CES
Removal of the Internal Center Bushes
Figure 802A/TASK 54-51-17-991-015-A22 (SHEET 2)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-17
Page 821
Nov 01/08
CES
Removal of the Internal Center Bushes
Figure 802B/TASK 54-51-17-991-015-B12 (SHEET 1)
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 822
Feb 01/10
CES
Removal of the Internal Center Bushes
Figure 802B/TASK 54-51-17-991-015-B22 (SHEET 2)
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 823
Feb 01/10
CES
Removal of the Internal and External Center Bushes
Figure 803/TASK 54-51-17-991-016
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-17
Page 824
Feb 01/08
CES
Removal of the Internal and External Center Bushes
Figure 803A/TASK 54-51-17-991-016-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-17
Page 825
Nov 01/08
CES
Removal of the Internal and External Center Bushes
Figure 803B/TASK 54-51-17-991-016-B
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 826
Feb 01/10
CES
**ON A/C ALL
1
_ Install the push ring (12) on the screw (13).
2
_ Install the screw (13) in the fittings.
3
_ Install the washer (3) and the nut (4) on the screw (13).
4
_ Remove the internal bush (10). To do this, turn the nut (4).
5
_ Remove the nut (4) and the washer (3) from the screw (13).
6
_ Remove the screw (13) from the fittings.
7
_ Remove the internal bush (10).
8
_ Install the screw (13) in the fittings.
9
_ Install the washer (3) and the nut (4) on the screw (13).
10
__ Remove the external center bush (11). To do this, turn the nut
(4).
11
__ Remove the nut (4) and the washer (3) from the screw (13).
12
__ Remove the screw (13) from the fittings.
13
__ Remove the external center bush (11).
EFF :
ALL 54-51-17
Page 827
Feb 01/10
CES
Removal of the External Bushes
Figure 804/TASK 54-51-17-991-017
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-17
Page 828
Feb 01/08
CES
Removal of the External Bushes
Figure 804A/TASK 54-51-17-991-017-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-17
Page 829
Nov 01/08
CES
Removal of the External Bushes
Figure 804B/TASK 54-51-17-991-017-B
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 830
Feb 01/10
CES
**ON A/C ALL
1
_ Install the push ring (12) on the screw (13).
2
_ Install the screw (13) in the fittings.
3
_ Install the washer (3) and the nut (4) on the screw (13).
4
_ Remove the external bush (20). To do this, turn the nut (4).
5
_ Remove the nut (4) and the washer (3) from the screw (13).
6
_ Remove the screw (13) from the fittings.
7
_ Remove the external bushes (20).
Subtask 54-51-17-220-090
(2) Make sure that there is no damage, wear or corrosion and that the
diameter of the bore is 44 +0.0 +0.03 mm (1.7322 +0.0000 +0.0011
in.).
Subtask 54-51-17-420-078
NOTE : This procedure is given for one side and is the same for the other
____
side.
EFF :
ALL 54-51-17
Page 831
Aug 01/09
CES
Installation of the Center Bushes
Figure 805/TASK 54-51-17-991-018
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-17
Page 832
Feb 01/08
CES
**ON A/C 234-235, 239-249, 251-299, 307-399,
NOTE : This procedure is the same for the external and the internal
____
center bushes.
(a) Make sure that the surface of the fitting bores is clean. If
necessary, clean the surface with CLEANING AGENTS (Material No.
11-004) and a lint-free cotton cloth MISCELLANEOUS (Material No.
19-003).
(b) Install the centering pin (30) and expand it until it touches the
fitting bore.
(d) Install the push pin (32) in the reducer (31) without protrusion
from the reducer.
(e) Soak the new center bush (34) (or the new center bush (35)) in
liquid nitrogen for 2 minutes.
(f) Install the bush on the bush tool (33) (less than 10 seconds).
(g) Put the bush in position in front of the bore and push the bush
tool (33) with the push pin (32) (less than 10 seconds).
(h) Apply a force on the bush tool (33) with the push pin (32) for 1
minute.
(i) Remove the bush tool (33), the push pin (32), the reducer (31)
and the centering pin (30).
EFF :
ALL 54-51-17
Page 833
Feb 01/10
CES
Installation of the Center Bushes
Figure 805A/TASK 54-51-17-991-018-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-17
Page 834
Nov 01/08
CES
Installation of the Center Bushes
Figure 805B/TASK 54-51-17-991-018-B
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 835
Feb 01/10
CES
(2) Install the external and internal bushes:
NOTE : This procedure is the same for the external and the internal
____
bushes.
(a) Make sure that the surface of the fitting bores is clean. If
necessary, clean the surface with CLEANING AGENTS (Material No.
11-004) and a lint-free cotton cloth MISCELLANEOUS (Material No.
19-003).
(b) Install the centering pin (30) and expand it until it touches the
fitting bore.
(d) Install the push pin (32) in the reducer (31) without protrusion
from the reducer.
(e) Soak the new bush (36) (or the new bush (37)) in liquid nitrogen
for 2 minutes.
(f) Install the bush on the bush tool (33) (less than 10 seconds).
(g) Put the bush in position in front of the bore and push the bush
tool (33) with the push pin (32) (less than 10 seconds).
EFF :
ALL 54-51-17
Page 836
Feb 01/10
CES
Installation of the External and Internal Bushes
Figure 806/TASK 54-51-17-991-019
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-17
Page 837
Feb 01/08
CES
Installation of the External and Internal Bushes
Figure 806A/TASK 54-51-17-991-019-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-17
Page 838
Nov 01/08
CES
Installation of the External and Internal Bushes
Figure 806B/TASK 54-51-17-991-019-B
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 839
Feb 01/10
CES
(h) Apply a force on the bush tool (33) with the push pin (32) for 1
minute.
(i) Remove the bush tool (33), the push pin (32), the reducer (31)
and the centering pin (30).
Subtask 54-51-17-420-079
D. Installation for Bush Reboring of the Bell which is part of the Tool R I
RING AT RIB 4 (98D54003015000)
NOTE : The procedure that follows is given for one side and is the same
____
for the other side.
(1) Install the centering pins (51) and (52) and expand them until they
touch the bushes.
(2) Put the boring bar (53) into the fittings and the centering pins (51)
and (52).
(4) Attach the bell (50) with the 3 C presses (54).
(5) Make sure that the boring bar (53) turns freely.
EFF :
ALL 54-51-17
Page 840
Feb 01/10
CES
Subtask 54-51-17-320-050
NOTE : The procedure that follows is given for one side and is the same
____
for the other side.
(c) Put the boring bar (53) into the fittings, the centering pin
(52), the borer (55) and the bell (50).
(a) Expand the borer (55) with the adjustment nut (57).
(b) Lock the blades of the borer (55) with the locking nut (58).
EFF :
ALL 54-51-17
Page 841
Feb 01/10
CES
Installation of the Boring Bar
Figure 807/TASK 54-51-17-991-020- 12 (SHEET 1)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-17
Page 842
Feb 01/08
CES
Installation of the Boring Bar
Figure 807/TASK 54-51-17-991-020- 22 (SHEET 2)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-17
Page 843
Feb 01/08
CES
Installation of the Boring Bar
Figure 807A/TASK 54-51-17-991-020-A12 (SHEET 1)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-17
Page 844
Nov 01/08
CES
Installation of the Boring Bar
Figure 807A/TASK 54-51-17-991-020-A22 (SHEET 2)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-17
Page 845
Nov 01/08
CES
Installation of the Boring Bar
Figure 807B/TASK 54-51-17-991-020-B12 (SHEET 1)
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 846
Feb 01/10
CES
Installation of the Boring Bar
Figure 807B/TASK 54-51-17-991-020-B22 (SHEET 2)
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 847
Feb 01/10
CES
Reboring of the Bushes
Figure 808/TASK 54-51-17-991-021- 12 (SHEET 1)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-17
Page 848
Feb 01/08
CES
Reboring of the Bushes
Figure 808/TASK 54-51-17-991-021- 22 (SHEET 2)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-17
Page 849
Feb 01/08
CES
Reboring of the Bushes
Figure 808A/TASK 54-51-17-991-021-A12 (SHEET 1)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-17
Page 850
Nov 01/08
CES
Reboring of the Bushes
Figure 808A/TASK 54-51-17-991-021-A22 (SHEET 2)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-17
Page 851
Nov 01/08
CES
Reboring of the Bushes
Figure 808B/TASK 54-51-17-991-021-B12 (SHEET 1)
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 852
Feb 01/10
CES
Reboring of the Bushes
Figure 808B/TASK 54-51-17-991-021-B22 (SHEET 2)
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 853
Feb 01/10
CES
(c) Turn the boring bar (53) slowly and push it lightly with a tap
wrench to rebore the four bushes.
NOTE : You must always turn the boring bar (53) in the same
____
direction to prevent damage to the borer (55) and to the
bushes.
(d) Turn the boring bar (53) while you pull it to move back the borer
(55) between the two fittings.
NOTE : You must continue to turn the boring bar (53) in the same
____
direction (as for the reboring) to prevent damage to the
borer (55) and to the bushes.
Subtask 54-51-17-020-080
EFF :
ALL 54-51-17
Page 854
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
(1) Remove the pin (56) from the boring bar (53).
(2) Remove the boring bar (53) and the borer (55) from the fittings.
(4) Remove the 3 C presses (54) and the bell (50).
(5) Make sure that the rebored diameter is in the correct condition and
that the diameter value is in the correct tolerance.
Subtask 54-51-17-320-051
NOTE : You must deburr each side of the external bushes and the external
____
side of the center bushes.
EFF :
ALL 54-51-17
Page 855
Feb 01/10
CES
Deburring of the Bushes
Figure 809/TASK 54-51-17-991-022
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-17
Page 856
Feb 01/08
CES
Deburring of the Bushes
Figure 809A/TASK 54-51-17-991-022-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-17
Page 857
Nov 01/08
CES
Deburring of the Bushes
Figure 809B/TASK 54-51-17-991-022-B
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 858
Feb 01/10
CES
R - for the bushes (62) and for the other side of the bush (61), use
R pliers to install the knife (65) in the correct position.
R - for the bushes (63) and (64), you must change the position of
R the centering pin (60) on the other side of the fittings.
R (1) Install the centering pin (60) and expand it until it touches the
R bush.
R (5) Tighten the bar (67) on the bar (68) to keep the knife (65) in
R position.
R (6) Turn the handle of the bar (67) or (68) to deburr the bush.
R 5. Close-up
________
R Subtask 54-51-17-110-052
R (1) Clean the fitting with CLEANING AGENTS (Material No. 11-004) and a
R lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
R Subtask 54-51-17-420-080
R B. Installation of Components
EFF :
ALL 54-51-17
Page 859
Nov 01/07
CES
Subtask 54-51-17-865-051
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU ENGINE/2/HP FUEL SOV 1KC2 A02
49VU ENGINE/1/HP FUEL SOV 1KC1 A01
49VU ANTI ICE/PROBES/AOA/1 4DA1 D04
49VU ANTI ICE/PROBES/PHC/1 2DA1 D03
49VU ANTI ICE/PROBES/PITOT/1 3DA1 D02
121VU HYDRAULIC/HYD POWER/Y 3803GX N30
122VU ANTI ICE/ENG/2 1DN2 W10
122VU ANTI ICE/PROBES/PHC/3 2DA3 Y16
122VU ANTI ICE/PROBES/2/TAT 1DA2 Y15
122VU ANTI ICE/PROBES/2/PITOT 3DA2 Y14
122VU ANTI ICE/PROBES/2/AOA 4DA2 Y13
R 122VU ANTI ICE/PROBES/PHC/2 2DA2 Y12
122VU ANTI ICE/PROBES/2/STATIC 5DA2 Y11
122VU ANTI ICE/PROBES/3/PITOT 3DA3 Z16
122VU ANTI ICE/PROBES/3/AOA 4DA3 Z15
122VU ANTI ICE/PROBES/1/STATIC 5DA1 Z13
122VU ANTI ICE/PROBES/1/TAT 1DA1 Z12
123VU Y HYD/ELEC/PUMP 3802GX AB06
123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
Subtask 54-51-17-860-059
(3) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
Subtask 54-51-17-862-052
EFF :
ALL 54-51-17
Page 860
Feb 01/10
CES
TASK 54-51-17-300-003
1. __________________
Reason for the Job
This procedure is applicable to the fitting bores that you found damaged or
with incorrect dimensions after removal of the bushes.
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-17
Page 861
Aug 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-17-320-052
-------------------------------------------------------------------------------
| REPAIR SIZE | NOMINAL VALUE | TOLERANCE |
| DIAMETER | MM (in.) | mm (in.) |
|-------------------|-----------------------|---------------------------------|
| R1 | 44.2 (1.7401) | + 0.03 (+ 0.00118) |
|-------------------|-----------------------|---------------------------------|
| | | + 0 (+ 0) |
|-------------------|-----------------------|---------------------------------|
| R2 | 44.4 (1.7480) | + 0.03 (+ 0.00118) |
|-------------------|-----------------------|---------------------------------|
| | | + 0 (+ 0) |
|-------------------|-----------------------|---------------------------------|
EFF :
ALL 54-51-17
Page 862
Feb 01/10
CES
-------------------------------------------------------------------------------
| REPAIR SIZE | NOMINAL VALUE | TOLERANCE |
| DIAMETER | MM (in.) | mm (in.) |
|-------------------|-----------------------|---------------------------------|
| R3 | 44.6 (1.7559) | + 0.03 (+ 0.00118) |
|-------------------|-----------------------|---------------------------------|
| | | + 0 |
-------------------------------------------------------------------------------
4. Procedure
_________
NOTE : This procedure is the same for the left and the right pylon.
____
NOTE : The procedure that follows is given for one side and is the same for
____
the other side.
Subtask 54-51-17-420-081
A. Installation for Fitting Reboring of the Bell which is part of the Tool R
I RING AT RIB 4 (98D54003015000)
(1) Install the centering pins (51) and (52) and expand them until they
touch the fitting bores.
(2) Put the boring bar (53) into the fittings and the centering pins (51)
and (52).
EFF :
ALL 54-51-17
Page 863
Feb 01/10
CES
Installation of the Boring Bar
Figure 810/TASK 54-51-17-991-023- 12 (SHEET 1)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-17
Page 864
Feb 01/08
CES
Installation of the Boring Bar
Figure 810/TASK 54-51-17-991-023- 22 (SHEET 2)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-17
Page 865
Feb 01/08
CES
Installation of the Boring Bar
Figure 810A/TASK 54-51-17-991-023-A12 (SHEET 1)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-17
Page 866
Nov 01/08
CES
Installation of the Boring Bar
Figure 810A/TASK 54-51-17-991-023-A22 (SHEET 2)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-17
Page 867
Nov 01/08
CES
Installation of the Boring Bar
Figure 810B/TASK 54-51-17-991-023-B12 (SHEET 1)
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 868
Feb 01/10
CES
Installation of the Boring Bar
Figure 810B/TASK 54-51-17-991-023-B22 (SHEET 2)
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 869
Feb 01/10
CES
(4) Attach the bell (50) with the 3 C presses (54).
(5) Make sure that the boring bar (53) turns freely.
Subtask 54-51-17-320-053
(c) Put the boring bar (53) into the fittings, the centering pin
(52), the borer (55) and the bell (50).
EFF :
ALL 54-51-17
Page 870
Feb 01/10
CES
(2) Rebore the fittings to get the minimum applicable repair diameter. If
necessary, do the reboring procedure that follows again until you get
the correct diameter value.
(a) Expand the borer (55) with the adjustment nut (57).
(b) Lock the blades of the borer (55) with the locking nut (58).
(c) Turn the boring bar (53) slowly and push it lightly with a tap
wrench to rebore the four holes.
NOTE : You must always turn the boring bar (53) in the same
____
direction to prevent damage to the borer (55) and to the
fittings.
(d) Turn the boring bar (53) while you pull it to move back the borer
(55) between the two fittings.
NOTE : You must continue to turn the boring bar (53) in the same
____
direction (as for the reboring) to prevent damage to the
borer (55) and to the fittings.
Subtask 54-51-17-020-081
EFF :
ALL 54-51-17
Page 871
Feb 01/10
CES
Reboring of the Fitting
Figure 811/TASK 54-51-17-991-024- 12 (SHEET 1)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-17
Page 872
Feb 01/08
CES
Reboring of the Fitting
Figure 811/TASK 54-51-17-991-024- 22 (SHEET 2)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-17
Page 873
Feb 01/08
CES
Reboring of the Fitting
Figure 811A/TASK 54-51-17-991-024-A12 (SHEET 1)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-17
Page 874
Nov 01/08
CES
Reboring of the Fitting
Figure 811A/TASK 54-51-17-991-024-A22 (SHEET 2)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-17
Page 875
Nov 01/08
CES
Reboring of the Fitting
Figure 811B/TASK 54-51-17-991-024-B12 (SHEET 1)
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 876
Feb 01/10
CES
Reboring of the Fitting
Figure 811B/TASK 54-51-17-991-024-B22 (SHEET 2)
R
EFF :
501-509, 511-526, 528-599, 54-51-17
Page 877
Feb 01/10
CES
**ON A/C ALL
(1) Remove the pin (56) from the boring bar (53).
(2) Remove the boring bar (53) and the borer (55) from the fittings.
(4) Remove the 3 C presses (54) and the bell (50).
(5) Make sure that the rebored diameter is in the correct condition and
that the diameter value is in the correct tolerance.
5. Close-up
________
Subtask 54-51-17-110-053
(1) Clean the fitting with CLEANING AGENTS (Material No. 11-004) and a
lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
EFF :
ALL 54-51-17
Page 878
Aug 01/08
R
CES
PYLON-TO-ENGINE ATTACH FITTINGS - REMOVAL/INSTALLATION
______________________________________________________
TASK 54-51-18-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-18
Page 401
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
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 54-51-18-941-050
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-51-18-020-050
B. Engine Removal
EFF :
ALL 54-51-18
Page 402
Nov 01/08
CES
Subtask 54-51-18-010-050
C. Get Access
Subtask 54-51-18-020-050-A
B. Engine Removal
Subtask 54-51-18-010-050-A
C. Get Access
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-18
Page 403
Feb 01/10
511-526, 528-599,
CES
**ON A/C ALL
4. Procedure
_________
Subtask 54-51-18-020-051
(2) Remove the nuts (7) and (8), the locking plates (6), the bolts (3)
and (4) and the locking plates (5).
EFF :
ALL 54-51-18
Page 404
Feb 01/10
CES
Engine Aft Mount Upper Beam
Figure 401/TASK 54-51-18-991-001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-18
Page 405
Aug 01/09
CES
R Engine Aft Mount Upper Beam
R Figure 401A/TASK 54-51-18-991-001-D
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-18
Page 406
Aug 01/09
CES
Engine Aft Mount Upper Beam
Figure 401B/TASK 54-51-18-991-001-E
R
EFF :
501-509, 511-526, 528-599, 54-51-18
Page 407
Feb 01/10
CES
TASK 54-51-18-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-18
Page 408
Nov 01/09
CES
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-18
Page 409
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-51-18-860-051
4. Procedure
_________
Subtask 54-51-18-420-050
(1) Before installation, make sure that the bolts (3) and (4) are in the
correct condition, if necessary replace the bolt (3) and the bolt
(4).
(3) Install the bolts (3) and (4) with SPECIAL MATERIALS (Material No.
05-047).
EFF :
ALL 54-51-18
Page 410
Feb 01/10
CES
(4) Lock the bolts (3) and (4) with the lockwashers (2) and the bolts
(1).
(a) Install the nuts (7) and (8) on the bolts (3) and (4).
(b) With a torque wrench calibrated to 3.4 m.daN (25.07 lbf.ft) for
the nut (7) and calibrated to 4.5 m.daN (33.18 lbf.ft) for the
nut (8):
- Measure the running torque necessary to tighten the nuts (7)
and (8) until two threads minimum show out of the nuts (7) and
(8).
(e) With a torque wrench calibrated to 0.36 m.daN (31.85 lbf.in) for
the nut (7) and to 0.56 m.daN (49.55 lbf.in) for the nut (8):
- Measure the breakaway torque necessary to loosen the nuts (7)
and (8).
(g) Do the same for the other nut (7) and (8).
(7) Install the locking plates (6) and the nuts (7) and (8).
(8) TORQUE the nuts (7) to between 14.6 and 16.8 m.daN (107.66 and 123.89
lbf.ft) and the nuts (8) to between 25 and 29 m.daN (184.36 and
213.86 lbf.ft)
(9) Lock the nuts (7) and (8) with the lockwashers (2) and the bolts (1).
EFF :
ALL 54-51-18
Page 411
Aug 01/09
R
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
401-499,
Subtask 54-51-18-420-051
B. Engine Installation
Subtask 54-51-18-420-051-A
B. Engine Installation
5. Close-up
________
Subtask 54-51-18-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-18
Page 412
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-18-410-050-A
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
501-509, 511-526, 528-599, 54-51-18
Page 413
Feb 01/10
CES
DOORS - REMOVAL/INSTALLATION
____________________________
TASK 54-51-21-000-001
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 54-51-21
Page 401
Aug 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-21-861-050
Subtask 54-51-21-941-050
B. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
EFF :
ALL 54-51-21
Page 402
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
401-499,
Subtask 54-51-21-040-050-B
WARNING : MAKE SURE THAT THE THRUST REVERSER IS LOCKED. IF NOT, THE
_______
THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE INJURY TO
PERSONNEL AND/OR DAMAGE TO THE REVERSER.
(1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-
30-00-481-041).
Subtask 54-51-21-040-050-A
WARNING : MAKE SURE THAT THE THRUST REVERSER IS LOCKED. IF NOT, THE
_______
THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE INJURY TO
PERSONNEL AND/OR DAMAGE TO THE REVERSER.
(1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-
30-00-040-012).
Subtask 54-51-21-010-050
D. Get Access
EFF :
ALL 54-51-21
Page 403
Feb 01/10
CES
4. Procedure
_________
Subtask 54-51-21-020-050
NOTE : The procedure is the same for the pylon lateral access-doors
____
415BR, 425BL and 425BR.
(a) Hold the access-door (1) and remove the screws (3), the washers
(2) and the access-door (1).
NOTE : The procedure is the same for the pylon lateral access-doors
____
415AR, 425AL and 425AR.
(a) Hold the access-door (5) and remove the screws (4) and the
access-door (5).
Subtask 54-51-21-020-050-A
NOTE : The procedure is the same for the pylon lateral access-doors
____
415BR, 425BL and 425BR.
(a) Hold the access-door (3) and remove the screws (1) and the
washers (2).
(b) Remove the spring pin (5), the captive screw (6), the washer (4)
and the access-door (3).
EFF :
ALL 54-51-21
Page 404
Feb 01/10
CES
Pylon Lateral Access-Doors
Figure 401/TASK 54-51-21-991-001
R
EFF :
201-207,
001-049, 051-099, 101-105, 151-154, 54-51-21
Page 405
Aug 01/09
CES
Pylon Lateral Access-Doors
Figure 401A/TASK 54-51-21-991-001-A
R
EFF : 106-149, 155-199, 208-249, 251-299,
301-399, 401-499, 501-509, 511-526, 528-599,
54-51-21
Page 406
Feb 01/10
CES
(2) Remove the pylon lateral access-door 415AL.
NOTE : The procedure is the same for the pylon lateral access-doors
____
415AR, 425AL and 425AR.
(a) Hold the access-door (8) and remove the screws (7) and the
access-door (8).
R
EFF : 106-149, 155-199, 208-249, 251-299,
301-399, 401-499, 501-509, 511-526, 528-599,
54-51-21
Page 407
Feb 01/10
CES
**ON A/C ALL
TASK 54-51-21-400-001
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
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-21
Page 408
Aug 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-21-860-050
Subtask 54-51-21-040-051-B
WARNING : MAKE SURE THAT THE THRUST REVERSER IS LOCKED. IF NOT, THE
_______
THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE INJURY TO
PERSONNEL AND/OR DAMAGE TO THE REVERSER.
EFF :
ALL 54-51-21
Page 409
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-21-040-051-A
WARNING : MAKE SURE THAT THE THRUST REVERSER IS LOCKED. IF NOT, THE
_______
THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE INJURY TO
PERSONNEL AND/OR DAMAGE TO THE REVERSER.
Subtask 54-51-21-110-050
4. Procedure
_________
Subtask 54-51-21-420-050
NOTE : The procedure is the same for the pylon lateral access-doors
____
415BR, 425BL and 425BR.
(a) Put the access-door (1) in position and install the washers (2)
and the screws (3).
(b) TORQUE the screws (3) to between 0.82 and 1.06 m.daN (72.56 and
93.80 lbf.in).
EFF :
ALL 54-51-21
Page 410
Feb 01/10
CES
(2) Install the pylon lateral access-door 415AL.
NOTE : The procedure is the same for the pylon lateral access-doors
____
415AR, 425AL and 425AR.
(a) Put the access-door (5) in position and install the screws (4).
(b) TORQUE the screws (4) to between 0.82 and 1.06 m.daN (72.56 and
93.80 lbf.in).
Subtask 54-51-21-420-050-A
NOTE : The procedure is the same for the pylon lateral access-doors
____
415BR, 425BL and 425BR.
(a) Put the access-door (3) in position and install the washers (2)
and the screws (1).
(b) TORQUE the screws (1) to between 0.82 and 1.06 m.daN (72.56 and
93.80 lbf.in).
(c) Install the washer (4), the captive screw (6) and the spring pin
(5).
(d) TORQUE the captive screws (6) to between 1.79 and 2.24 m.daN
(13.20 and 16.51 lbf.ft) .
NOTE : The procedure is the same for the pylon lateral access-doors
____
415AR, 425AL and 425AR.
(a) Put the access-door (8) in position and install the screws (7).
(b) TORQUE the screws (7) to between 0.82 and 1.06 m.daN (72.56 and
93.80 lbf.in).
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-21
Page 411
Feb 01/10
511-526, 528-599,
CES
**ON A/C ALL
5. Close-up
________
Subtask 54-51-21-440-050-B
(1) Make the thrust reverser serviceable after maintenance (Ref. TASK 78-
30-00-081-041).
Subtask 54-51-21-440-050-A
(1) Make the thrust reverser serviceable after maintenance (Ref. TASK 78-
30-00-440-012).
Subtask 54-51-21-862-050
Subtask 54-51-21-410-050
C. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-21
Page 412
Feb 01/10
CES
MISCELLANEOUS - REMOVAL/INSTALLATION
____________________________________
TASK 54-51-29-000-001
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.
WARNING : MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT
_______
AVAILABLE.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-29
Page 401
Nov 01/07
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-29-941-050
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF :
ALL 54-51-29
Page 402
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put the warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-51-29-020-051
(2) Remove the thrust reverser cowl doors (Ref. TASK 78-32-11-000-002).
Subtask 54-51-29-010-050
C. Get Access
EFF :
ALL 54-51-29
Page 403
Nov 01/08
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-29-020-051-A
(1) Remove the fan cowl doors (Ref. TASK 71-13-11-000-010) (Ref. TASK 71-
13-16-000-010).
Subtask 54-51-29-010-050-A
C. Get Access
(a) At RIB3, remove the two bolts (10), the two washers (11), the
bonding strip (9) and the casing assy (12).
(b) At RIB4, remove the bolt (17), the washer (18) and the clamp
(16). Remove and discard the bushing (19).
(c) At RIB7, loosen the pipe end-fittings (1), (2) and (4) and remove
the tee (3) from the drain pipe (15). Put blanking plugs on the
disconnected line ends.
R
EFF :
501-509, 511-526, 528-599, 54-51-29
Page 404
Feb 01/10
CES
Drain Lines
Figure 401/TASK 54-51-29-991-002
R
EFF :
501-509, 511-526, 528-599, 54-51-29
Page 405
Feb 01/10
CES
(d) Remove the drain pipe (5) and the drain pipe (14) from the rear.
(a) At RIB1, remove the two bolts (7) and the two washers (6). Loosen
the pipe end-fitting (8) and put blanking plugs on the
disconnected line ends.
(b) At rib4, remove the bolt (17), the washer (18) and the clamp
(16). Remove and discard the bushing (19).
4. Procedure
_________
Subtask 54-51-29-020-050
(1) Remove the nuts (1) and discard them. Remove the washers (2).
EFF :
ALL 54-51-29
Page 406
Feb 01/10
CES
R Hoisting Fitting
R Figure 402/TASK 54-51-29-991-001-C
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-29
Page 407
Feb 01/08
CES
Hoisting Fitting
Figure 402A/TASK 54-51-29-991-001-B
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-51-29
Page 408
Feb 01/10
CES
TASK 54-51-29-400-001
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
-------------------------------------------------------------------------------
R
EFF :
ALL 54-51-29
Page 409
Feb 01/08
CES
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-29
Page 410
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-51-29-860-050
(3) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-
00-481-041).
4. Procedure
_________
Subtask 54-51-29-420-050
(2) Install the washers (2). Install the nuts (1) and tighten them
manually.
(3) Make sure that the alignment is within 0.3 mm (0.0118 in.). To do
this put a 19 mm (0.7480 in.) dia. bar
into the holes of the hoisting fittings.
(4) TORQUE the nuts (1) to between 15.5 and 18 m.daN (114.30 and 132.74
lbf.ft).
EFF :
ALL 54-51-29
Page 411
Feb 01/10
CES
(5) Remove the bar.
5. Close-up
________
Subtask 54-51-29-410-050
A. Close Access
Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-51-29-420-051
(2) Install the thrust reverser cowl doors (Ref. TASK 78-32-11-400-002).
EFF :
ALL 54-51-29
Page 412
Nov 01/08
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-51-29-410-050-A
A. Close Access
(b) At RIB1, connect the drain pipe (13) to the pipe-end fitting (8).
Do not torque the pipe-end fitting (8) at this time.
(c) Install the two washers (6) and the two bolts (7). Tighten the
two bolts (7).
(e) Install the clamp (16), the washer (18) and the bolt (17).
Tighten the bolt (17).
(f) Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-004) on the
bolts (7) and (17).
(b) At RIB3, install the casing assy (12), the bonding strip (9), the
two washers (11) and the two bolts (10). Tighten the two bolts
(10).
(d) Install the clamp (16), the washer (18) and the bolt (17).
Tighten the bolt (17).
(e) Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-004) on the
bolts (10) and (17).
R
EFF :
501-509, 511-526, 528-599, 54-51-29
Page 413
Feb 01/10
CES
(f) At RIB7, put the tee (3) in position. Connect the tee (3) to the
drain pipes (5) and (15). Do not torque the pipe-end fittings (2)
and (4) at this time.
(h) At RIB7, connect the tee (3) to the drain pipe (14). Do not
torque the pipe-end fitting (1) at this time.
(5) TORQUE the pipe-end fittings (8), (4), (1) and (2) to between 2.9 and
3.2 m.daN (21.38 and 23.59 lbf.ft).
(Ref. Fig. 401/TASK 54-51-29-991-002)
Subtask 54-51-29-420-051-A
(2) Install the thrust reverser cowl doors (Ref. TASK 78-32-01-400-010)
(Ref. TASK 78-32-02-400-010) (Ref. TASK 78-32-03-400-010) (Ref. TASK
78-32-04-400-010).
(3) Install the fan cowl doors (Ref. TASK 71-13-11-400-010) (Ref. TASK
71-13-16-400-010).
R
EFF :
501-509, 511-526, 528-599, 54-51-29
Page 414
Feb 01/10
CES
BALL JOINT - SPIGOT - REMOVAL/INSTALLATION
__________________________________________
TASK 54-51-41-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-41
Page 401
Nov 01/07
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-41
Page 402
Feb 01/10
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-41-860-050
EFF :
ALL 54-51-41
Page 403
Feb 01/10
CES
Subtask 54-51-41-941-050
B. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine
1(2).
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR 1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-51-41-040-050
Subtask 54-51-41-040-050-A
EFF :
ALL 54-51-41
Page 404
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
401-499,
Subtask 54-51-41-010-050
D. Get Access
Subtask 54-51-41-010-050-A
D. Get Access
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-41
Page 405
Feb 01/10
511-526, 528-599,
CES
R (3) Remove the access doors:
Subtask 54-51-41-020-050
E. Removal of Component
4. Procedure
_________
Subtask 54-51-41-110-050
(1) Remove the adhesive compound from the upper panel between RIB4 and
RIB5 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.
Subtask 54-51-41-020-051
EFF :
ALL 54-51-41
Page 406
Aug 01/09
CES
Spigot Ball Joint
Figure 401/TASK 54-51-41-991-001-A
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-41
Page 407
Feb 01/08
CES
**ON A/C 234-235, 239-249, 251-299, 307-399,
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-51-41
Page 408
Feb 01/10
511-526, 528-599,
CES
Spigot Ball Joint
Figure 401A/TASK 54-51-41-991-001-B
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-41
Page 409
Aug 01/09
CES
Spigot Ball Joint
Figure 401B/TASK 54-51-41-991-001-C
R
EFF :
501-509, 511-526, 528-599, 54-51-41
Page 410
Feb 01/10
CES
INTENTIONALLY BLANK
R
54-51-41
Page 411
Aug 01/09
CES
Spigot Ball Joint Removal - First Step
Figure 402/TASK 54-51-41-991-002-A12 (SHEET 1)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-41
Page 412
Aug 01/09
CES
Spigot Ball Joint Removal - First Step
Figure 402/TASK 54-51-41-991-002-A22 (SHEET 2)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-41
Page 413
Aug 01/09
CES
Spigot Ball Joint Removal - First Step
Figure 402A/TASK 54-51-41-991-002-B12 (SHEET 1)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-41
Page 414
Aug 01/09
CES
Spigot Ball Joint Removal - First Step
Figure 402A/TASK 54-51-41-991-002-B22 (SHEET 2)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-41
Page 415
Aug 01/09
CES
Spigot Ball Joint Removal - First Step
Figure 402B/TASK 54-51-41-991-002-C12 (SHEET 1)
R
EFF :
501-509, 511-526, 528-599, 54-51-41
Page 416
Feb 01/10
CES
Spigot Ball Joint Removal - First Step
Figure 402B/TASK 54-51-41-991-002-C22 (SHEET 2)
R
EFF :
501-509, 511-526, 528-599, 54-51-41
Page 417
Feb 01/10
CES
Spigot Ball Joint Removal - Second Step
Figure 403/TASK 54-51-41-991-007
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-41
Page 418
Aug 01/09
CES
Spigot Ball Joint Removal - Second Step
Figure 403A/TASK 54-51-41-991-007-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-41
Page 419
Aug 01/09
CES
Spigot Ball Joint Removal - Second Step
Figure 403B/TASK 54-51-41-991-007-B
R
EFF :
501-509, 511-526, 528-599, 54-51-41
Page 420
Feb 01/10
CES
INTENTIONALLY BLANK
R
54-51-41
Page 421
Aug 01/09
CES
Spigot Ball Joint Removal - Third Step
Figure 404/TASK 54-51-41-991-003-A12 (SHEET 1)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-41
Page 422
Aug 01/09
CES
Spigot Ball Joint Removal - Third Step
Figure 404/TASK 54-51-41-991-003-A22 (SHEET 2)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-41
Page 423
Aug 01/09
CES
**ON A/C 234-235, 239-249, 251-299, 307-399,
(1) Remove the eight bolts (1) and nuts (2) from the retaining plate (3).
Retain the bolts and nuts.
NOTE : You cannot remove two of the eight bolts (1) from the top of
____
the rear spar because they touch the spigot fitting edge on
wing side.
(2) Saw off the heads of the two bolts that you cannot remove.
(4) Get :
(b) the TOOL,R/I-SPIGOT BALL JOINT (98D54403002041) for the the right
pylon.
(5) Install the plate (26), with the two studs (24) and nuts (25) and
tighten the nuts (25).
NOTE : Use the holes of bolts (1) for the two studs (24) and nuts
____
(25).
(6) Install the two half shells (11) and (12) between the wing and the
upper panel, onto the spigot.
(9) Install the actuator mount (23), the six threaded rods (22) and the
nuts (21) in the half shells (11) and (12).
EFF :
ALL 54-51-41
Page 424
Feb 01/10
CES
INTENTIONALLY BLANK
R
54-51-41
Page 425
Aug 01/09
CES
Spigot Ball Joint Removal - Third Step
Figure 404A/TASK 54-51-41-991-003-B12 (SHEET 1)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-41
Page 426
Aug 01/09
CES
Spigot Ball Joint Removal - Third Step
Figure 404A/TASK 54-51-41-991-003-B22 (SHEET 2)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-41
Page 427
Aug 01/09
CES
Spigot Ball Joint Removal - Third Step
Figure 404B/TASK 54-51-41-991-003-C12 (SHEET 1)
R
EFF :
501-509, 511-526, 528-599, 54-51-41
Page 428
Feb 01/10
CES
Spigot Ball Joint Removal - Third Step
Figure 404B/TASK 54-51-41-991-003-C22 (SHEET 2)
R
EFF :
501-509, 511-526, 528-599, 54-51-41
Page 429
Feb 01/10
CES
(10) Tighten the nuts (21).
(11) Install the actuating cylinder. Make sure that the nut (34) is fully
loosened and that the jaws (33) are in open position.
(14) Remove the nuts (21), the actuator mount (23) and the six threaded
rods (22).
(17) Install the four half segments (51), (52), (53) and (54) between the
wing and the pylon, in the spigot ball joint bore.
(18) Install the two half shells (11) and (12) between the wing and the
upper panel.
(19) Install the bolts (13) and (14) and tighten them.
(20) Install the actuator mount (23), the six threaded rods (22) and nuts
(21) in the half shells (11) and (12).
(24) Remove the nuts (21) and the six threaded rods (22).
(27) Tighten the nut (34) so that the jaws (33) touch the spigot ball
joint.
(28) Pressurize the actuating cylinder so that the sliding rod comes out
fully.
EFF :
ALL 54-51-41
Page 430
Aug 01/09
R
CES
(29) Install the two half segments (31) and (36) between the wing and the
pylon, in the spigot ball joint bore.
(30) Depressurize the actuating cylinder and pull in the sliding rod by 40
mm (1.5748 in.).
(31) Install the shim (35) between the sliding rod end and the plate (26).
(32) Pressurize the actuating cylinder and fully remove the ball joint
(32) from its housing.
(33) Depressurize the actuating cylinder and remove the shim (35).
(34) Loosen the nuts (34) so that the jaws (33) are in the open position.
(35) Remove the actuating cylinder, the nuts (25), the plate (26) and the
studs (24).
NOTE : The two half segments (31) and (36) must stay in position in
____
the ball joint bore.
EFF :
ALL 54-51-41
Page 431
Aug 01/09
R
CES
TASK 54-51-41-400-001
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
-------------------------------------------------------------------------------
EFF :
ALL 54-51-41
Page 432
Aug 01/09
R
CES
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-51-41
Page 433
Feb 01/10
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-51-41-860-051
(1) Make sure that the ground service network is energized (Ref. TASK 24-
42-00-861-001).
(3) Make sure that the fire extinguisher bottles are removed (Ref. TASK
26-21-41-000-004).
EFF :
ALL 54-51-41
Page 434
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
401-499,
Subtask 54-51-41-040-051
(1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-
00-481-041) .
Subtask 54-51-41-040-051-A
(1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-
00-040-012) .
Subtask 54-51-41-914-050
(a) Clean the external surfaces of the spigot ball joint, the
retaining plate (3) and the bolts (1) with CLEANING AGENTS
(Material No. 11-004) and MISCELLANEOUS (Material No. 19-003).
(2) Do a visual inspection of the spigot ball joint and the spigot.
(3) Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-034) in the
housing of the spigot ball joint.
EFF :
ALL 54-51-41
Page 435
Feb 01/10
CES
4. Procedure
_________
Subtask 54-51-41-420-050
EFF :
ALL 54-51-41
Page 436
Feb 01/10
CES
Spigot Ball-Joint Installation
Figure 405/TASK 54-51-41-991-004-A
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-41
Page 437
Aug 01/09
CES
Spigot Ball-Joint Installation
Figure 405A/TASK 54-51-41-991-004-B
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-41
Page 438
Aug 01/09
CES
Spigot Ball-Joint Installation
Figure 405B/TASK 54-51-41-991-004-C
R
EFF :
501-509, 511-526, 528-599, 54-51-41
Page 439
Feb 01/10
CES
Spigot Ball Joint - Protection against Corrosion
Figure 406/TASK 54-51-41-991-005-A
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-51-41
Page 440
Aug 01/09
CES
Spigot Ball Joint - Protection against Corrosion
Figure 406A/TASK 54-51-41-991-005-B
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-51-41
Page 441
Aug 01/09
CES
R **ON A/C 501-509, 511-526, 528-599,
(3) Install the threaded rods (43) with the nuts (42) below the upper
panel.
(4) Install the nuts (41) and tighten them to hold the threaded rods (43)
in position.
(5) Install the plate (45) on the threaded rods (43) and the nuts (44).
(6) Tighten the nuts (44) continuously to install the spigot ball joint
(32) and to release the half segments (31) and (36).
(8) Remove the nuts (41) and the threaded rods (43).
(9) Apply SEALANTS (Material No. 09-018) on the surface which touches the
retaining plate (3) and the inner face of the upper spar.
(10) Install the retaining plate (3) on the lower spigot ball-joint
fitting.
(11) Install the eight bolts (1) with SEALANTS (Material No. 09-025) or
SEALANTS (Material No. 09-016) and the nuts (2).
NOTE : If you sawed the heads of the two bolts (1) during removal,
____
install new bolts (1) with the heads in the down position.
(12) Remove the unwanted sealant with CLEANING AGENTS (Material No. 11-
004) and MISCELLANEOUS (Material No. 19-003).
EFF :
ALL 54-51-41
Page 442
Feb 01/10
CES
Spigot Ball Joint - Protection against Corrosion
Figure 406B/TASK 54-51-41-991-005-C
R
EFF :
501-509, 511-526, 528-599, 54-51-41
Page 443
Feb 01/10
CES
5. Close-up
________
Subtask 54-51-41-420-051
A. Installation of Component
Subtask 54-51-41-440-050
B. Close Access
Subtask 54-51-41-440-050-A
B. Close Access
Subtask 54-51-41-410-050
C. Installation of Component
EFF :
ALL 54-51-41
Page 444
Feb 01/10
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
Subtask 54-51-41-410-050-A
C. Installation of Component
Subtask 54-51-41-942-050
D. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-51-41
Page 445
Feb 01/10
CES
FORWARD FAIRING - DESCRIPTION AND OPERATION
___________________________________________
1. Description
___________
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-52-00
Page 1
Config-1 Nov 01/08
CES
Forward Fairing
Figure 001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-52-00
Page 2
Config-1 Feb 01/08
CES
Forward Fairing
Figure 001A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-52-00
Page 3
Config-1 Nov 01/08
CES
FORWARD FAIRING - DESCRIPTION AND OPERATION
___________________________________________
1. ___________
Description
(Ref. Fig. 001)
The forward fairing is composed of :
- 9 ribs
- 2 longitudinal partitions for segregation (bulkhead)
- A visor supported by spring blades
- 1 bottom cap
- Skin
- Fan cowl hinge fittings made of titanium.
All elements except the hinge fittings are made of stainless steel.
- Compartment B1 includes 2 pressure relief doors calibrated at 200 mbars to
prevent any overpressure in case of an air duct failure.
- Compartment A includes also one pressure relief valve to prevent any
overpressure in case of an air duct failure.
- Monel rivets are used for attachment
- In some limited areas spot welding is also used.
- All the access panels are bolted.
R
EFF :
501-509, 511-526, 528-599, 54-52-00
Page 1
Config-2 Feb 01/10
CES
Forward Fairings
Figure 001
R
EFF :
501-509, 511-526, 528-599, 54-52-00
Page 2
Config-2 Feb 01/10
CES
FORWARD FAIRING - DEACTIVATION/REACTIVATION
___________________________________________
TASK 54-52-00-040-001
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-52-00
Page 401
May 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-52-00-941-053
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-52-00-040-052
EFF :
ALL 54-52-00
Page 402
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-52-00-040-052-A
Subtask 54-52-00-010-051
C. Get Access
Subtask 54-52-00-010-051-B
C. Get Access
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-52-00
Page 403
Feb 01/10
511-526, 528-599,
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-52-00-010-051-C
C. Get Access
4. Procedure
_________
Subtask 54-52-00-040-053
EFF :
ALL 54-52-00
Page 404
Feb 01/10
CES
Pressure-Relief Doors
Figure 401/TASK 54-52-00-991-003
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-52-00
Page 405
Feb 01/08
CES
R Pressure-Relief Doors
Figure 401A/TASK 54-52-00-991-003-B
EFF :
234-235, 239-249, 251-299, 307-399, 54-52-00
Page 406
Feb 01/09
CES
Pressure-Relief Doors
Figure 401B/TASK 54-52-00-991-003-A
R
EFF :
501-509, 511-526, 528-599, 54-52-00
Page 407
Feb 01/10
CES
(1) Open the pressure-relief door (1) or (2).
(4) Remove the washers (6), the pin (10) and the shims (7) and (8).
(5) Remove the nut (5), the bolt (12) and the washer (13).
(7) Remove the nut (21), the bolt (17) and the washers (16) and (18).
EFF :
ALL 54-52-00
Page 408
Feb 01/09
R
CES
TASK 54-52-00-440-001
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-52-00
Page 409
May 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-52-00-860-050
(3) Make sure that the thrust reversers are unserviceable (Ref. TASK 78-
30-00-481-041).
EFF :
ALL 54-52-00
Page 410
Feb 01/10
CES
**ON A/C 234-235, 239-249, 251-299, 307-399,
Subtask 54-52-00-860-050-A
(3) Make sure that the thrust reversers are unserviceable (Ref. TASK 78-
30-00-481-041).
Subtask 54-52-00-860-050-B
(3) Make sure that the thrust reversers are unserviceable (Ref. TASK 78-
30-00-040-012).
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-52-00
Page 411
Feb 01/10
CES
**ON A/C ALL
4. Procedure
_________
Subtask 54-52-00-440-052
(3) Install the washers (18) and (16), the bolt (17) and the nut (21).
Tighten the nut.
(5) Install the washer (13), the bolt (12) and the nut (5). Tighten the
nut.
(6) Install the shims (8) and (7), the pin (10) and the washers (6).
EFF :
ALL 54-52-00
Page 412
Feb 01/10
CES
Subtask 54-52-00-210-051
B. Test
(1) Open and close the pressure-relief doors to make sure that they are
installed correctly.
5. Close-up
________
Subtask 54-52-00-410-051
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R Subtask 54-52-00-410-051-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
EFF :
ALL 54-52-00
Page 413
Feb 01/09
CES
(4) Remove the access platform(s).
Subtask 54-52-00-410-051-C
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-52-00-040-054
Subtask 54-52-00-040-054-A
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-52-00
Page 414
Feb 01/10
511-526, 528-599,
CES
FORWARD FAIRING - INSPECTION/CHECK
__________________________________
TASK 54-52-00-200-001
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 54-52-00
Page 601
May 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-52-00-941-050
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-52-00-040-050
EFF :
ALL 54-52-00
Page 602
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-52-00-040-050-A
Subtask 54-52-00-941-051
C. Get Access
4. Procedure
_________
Subtask 54-52-00-220-050
EFF :
ALL 54-52-00
Page 603
Feb 01/10
CES
Cracks, Nicks and Scores in the Forward Fairings
Figure 601/TASK 54-52-00-991-001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-52-00
Page 604
Feb 01/08
CES
Cracks, Nicks and Scores in the Forward Fairings
Figure 601A/TASK 54-52-00-991-001-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-52-00
Page 605
Nov 01/08
CES
Cracks, Nicks and Scores in the Forward Fairings
Figure 601B/TASK 54-52-00-991-001-B
R
EFF :
501-509, 511-526, 528-599, 54-52-00
Page 606
Feb 01/10
CES
**ON A/C ALL
1
_ Do a blending or burnishing operation,
2
_ Make sure that the length and the depth of the cracks, the
nicks or the scores are in the permitted limits,
3
_ Permitted damage on corrosion resistant steel as follows:
- Zone 1 : Permitted damage without repair
- Zone 2 : Repair this damage before 6000 flights
- Zone 3 : Repair this damage before 100 flights
- Zone 4 : Repair this damage before 50 flights
limit A for the pressure relief door
limit B for all the other skins
- Zone 5 : Return to repair.
1
_ The depth of dents must not be more than 2% of the minimum
width. Maximum depth is 2 mm (0.0787 in.) and maximum area is
10 cm2 (1.55 in.2). If the dent is located near a stiffener,
make sure that there are no cracks.
2
_ Holes are not permitted.
5. Close-up
________
Subtask 54-52-00-440-050
EFF :
ALL 54-52-00
Page 607
Nov 01/08
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-52-00-440-050-A
Subtask 54-52-00-942-050
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-52-00
Page 608
Feb 01/10
CES
FORWARD FAIRING - REPAIRS
_________________________
TASK 54-52-00-300-001
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
-------------------------------------------------------------------------------
EFF :
ALL 54-52-00
Page 801
Nov 01/99
CES
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-52-00-941-052
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
EFF :
ALL 54-52-00
Page 802
May 01/09
CES
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-52-00-040-051
Subtask 54-52-00-040-051-A
Subtask 54-52-00-010-050
C. Get Access
4. Procedure
_________
Subtask 54-52-00-350-050
EFF :
ALL 54-52-00
Page 803
Feb 01/10
CES
CAF4 Sealant - Pylon Cantilever
Figure 801/TASK 54-52-00-991-002
EFF :
ALL 54-52-00
Page 804
Nov 01/99
CES
(3) Repair of the CAF4 sealant.
1
_ Use a scraper to remove the old sealant that has contamination
plus 10 mm (0.3937 in.) all around the area.
2
_ Clean with CLEANING AGENTS (Material No. 11-008).
3
_ Remove the grease with CLEANING AGENTS (Material No. 11-026).
1
_ Clean the sealant with CLEANING AGENTS (Material No. 11-008).
2
_ Remove the grease with CLEANING AGENTS (Material No. 11-026).
(c) Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-004) on the
repair areas.
5. Close-up
________
Subtask 54-52-00-440-051
Subtask 54-52-00-440-051-A
EFF :
ALL 54-52-00
Page 805
Feb 01/10
CES
R **ON A/C ALL
Subtask 54-52-00-410-050
B. Close Access
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-52-00
Page 806
Nov 01/07
CES
SKIN PANELS AND DOORS - REMOVAL/INSTALLATION
____________________________________________
TASK 54-52-11-000-001
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 54-52-11
Page 401
May 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-52-11-941-050
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF :
ALL 54-52-11
Page 402
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-52-11-040-051
Subtask 54-52-11-040-051-A
Subtask 54-52-11-010-050
C. Get Access
EFF :
ALL 54-52-11
Page 403
Feb 01/10
CES
**ON A/C 234-235, 239-249, 251-299, 307-399,
Subtask 54-52-11-010-050-A
C. Get Access
4. Procedure
_________
Subtask 54-52-11-020-050
EFF :
ALL 54-52-11
Page 404
Feb 01/10
CES
Pressure Relief Doors
Figure 401/TASK 54-52-11-991-001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-52-11
Page 405
May 01/08
CES
R Pressure Relief Doors
Figure 401A/TASK 54-52-11-991-001-A
EFF :
234-235, 239-249, 251-299, 307-399, 54-52-11
Page 406
Feb 01/09
CES
Pressure Relief Doors
Figure 401B/TASK 54-52-11-991-001-B
R
EFF :
501-509, 511-526, 528-599, 54-52-11
Page 407
Feb 01/10
CES
(2) Remove the spring (11).
(4) Remove the washers (6), the pin (10) and the shims (7) and (8).
(5) Remove the nut (5), the bolt (12) and the washer (13).
(7) Remove the nut (21), the bolt (17) and the washers (16) and (18).
Subtask 54-52-11-020-051
(2) Remove the nut (37), the bolt (35) the washer (36) and the spacer
(38).
(3) Remove the nuts (33), the bolts (31) and the spacers (32).
EFF :
ALL 54-52-11
Page 408
Feb 01/10
CES
Top Arch of the Pressure Relief Doors
Figure 402/TASK 54-52-11-991-002
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-52-11
Page 409
May 01/08
CES
Top Arch of the Pressure Relief Doors
Figure 402A/TASK 54-52-11-991-002-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-52-11
Page 410
Nov 01/08
CES
Top Arch of the Pressure Relief Doors
Figure 402B/TASK 54-52-11-991-002-B
R
EFF :
501-509, 511-526, 528-599, 54-52-11
Page 411
Feb 01/10
CES
TASK 54-52-11-400-001
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
Self Explanatory
2. ______________________
Job Set-up Information
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R B. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
EFF :
ALL 54-52-11
Page 412
May 01/08
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-52-11
Page 413
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-52-11-860-050
(3) Make sure that the thrust reversers are unserviceable (Ref. TASK 78-
30-00-481-041).
Subtask 54-52-11-860-050-A
(3) Make sure that the thrust reversers are unserviceable (Ref. TASK 78-
30-00-040-012).
4. Procedure
_________
Subtask 54-52-11-420-050
EFF :
ALL 54-52-11
Page 414
Feb 01/10
CES
**ON A/C 234-235, 239-249, 251-299, 307-399,
(2) Install the spacers (32), the bolts (31) and the nuts (33).
(3) Install the spacer (38), the washer (36), the bolt (35) and the nut
(37). Tighten the nut.
Subtask 54-52-11-420-051
EFF :
ALL 54-52-11
Page 415
Feb 01/10
CES
(3) Install the washers (18) and (16), the bolt (17) and the nut (21).
Tighten the nut.
(5) Install the washer (13), the bolt (12), the nut (5). Tighten the nut.
(6) Install the shims (8) and (7), the pin (10) and the washers (6).
Subtask 54-52-11-210-051
C. Test
(1) Open and close the pressure relief doors to make sure that they are
assembled correctly.
5. Close-up
________
Subtask 54-52-11-410-050
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-52-11
Page 416
Feb 01/10
CES
**ON A/C 234-235, 239-249, 251-299, 307-399,
Subtask 54-52-11-410-050-A
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-52-11-040-052
Subtask 54-52-11-040-052-A
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-52-11
Page 417
Feb 01/10
511-526, 528-599,
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
401-499,
TASK 54-52-11-000-002
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 54-52-11-941-051
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-52-11
Page 418
Nov 01/09
R
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
R
Subtask 54-52-11-040-053
(1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-
30-00-481-041).
R
Subtask 54-52-11-010-051
C. Get Access
4. Procedure
_________
Subtask 54-52-11-020-052
(1) Hold the panel (1) and remove the screws (3), the cup washers (2) and
the panel (1).
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-52-11
Page 419
Aug 01/09
CES
Access Panels (413AL, 414AR, 423AL and 424AR)
Figure 403/TASK 54-52-11-991-003- 12 (SHEET 1)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-52-11
Page 420
Aug 01/09
CES
Access Panels (413AL, 414AR, 423AL and 424AR)
Figure 403/TASK 54-52-11-991-003- 22 (SHEET 2)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-52-11
Page 421
Aug 01/09
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
TASK 54-52-11-000-002-A
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-52-11
Page 422
Feb 01/10
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
3. __________
Job Set-up
Subtask 54-52-11-941-060
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-52-11-040-063
(1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-
30-00-481-041).
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-52-11
Page 423
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-52-11-040-063-A
(1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-
30-00-040-013).
Subtask 54-52-11-010-056
C. Get Access
4. Procedure
_________
Subtask 54-52-11-020-058
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-52-11
Page 424
Feb 01/10
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
(1) Hold the panel (1) and remove the screws (3), the cup washers (2) and
the panel (1).
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-52-11
Page 425
Feb 01/10
CES
Access Panels (413AL, 413AR, 423AL and 423AR)
Figure 403A/TASK 54-52-11-991-003-A12 (SHEET 1)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-52-11
Page 426
Nov 01/09
CES
Access Panels (413AL, 413AR, 423AL and 423AR)
Figure 403A/TASK 54-52-11-991-003-A22 (SHEET 2)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-52-11
Page 427
Nov 01/09
CES
Access Panels (413AL, 413AR, 423AL and 423AR)
Figure 403B/TASK 54-52-11-991-003-C12 (SHEET 1)
R
EFF :
501-509, 511-526, 528-599, 54-52-11
Page 428
Feb 01/10
CES
Access Panels (413AL, 413AR, 423AL and 423AR)
Figure 403B/TASK 54-52-11-991-003-C22 (SHEET 2)
R
EFF :
501-509, 511-526, 528-599, 54-52-11
Page 429
Feb 01/10
CES
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
R 401-499,
TASK 54-52-11-400-002
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 54-52-11-941-052
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-52-11
Page 430
Nov 01/09
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-52-11-860-051
Subtask 54-52-11-040-054
(1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-
30-00-481-041).
Subtask 54-52-11-110-050
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-52-11
Page 431
Nov 01/09
CES
**ON A/C 305-306, 403-499,
Subtask 54-52-11-200-050
(1) If the seal is damaged, remove it from its support and replace it
(Ref. TASK 54-52-11-000-004).
4. Procedure
_________
Subtask 54-52-11-420-052
(1) Put the panel (1) in position and install the cup washers (2) and the
screws (3). Tighten the screws (3).
Subtask 54-52-11-220-050
(1) Make sure that the out-of-flush clearance between the access panels
is:
5. Close-up
________
Subtask 54-52-11-440-050
A. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-30-
00-081-041)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-52-11
Page 432
Nov 01/09
CES
Subtask 54-52-11-410-051
B. Close Access
(1) Remove all the fixtures, tools, test and support equipment used
during this procedure.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-52-11
Page 433
Nov 01/09
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
TASK 54-52-11-400-002-A
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-52-11
Page 434
Feb 01/10
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
3. __________
Job Set-up
Subtask 54-52-11-941-061
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-52-11-860-058
Subtask 54-52-11-040-064
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-52-11
Page 435
Feb 01/10
CES
(1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-
30-00-481-041).
Subtask 54-52-11-040-064-A
(1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-
30-00-040-013).
Subtask 54-52-11-110-054
Subtask 54-52-11-200-052
(1) If the seal is damaged, remove it from its support and replace it
(Ref. TASK 54-52-11-000-004).
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-52-11
Page 436
Feb 01/10
CES
4. Procedure
_________
Subtask 54-52-11-420-058
(1) Put the panel (1) in position and install the cup washers (2) and the
screws (3). Tighten the screws (3).
Subtask 54-52-11-220-052
(1) Make sure that the out-of-flush clearance between the access panels
is:
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-52-11
Page 437
Feb 01/10
CES
5. Close-up
________
Subtask 54-52-11-440-054
A. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-30-
00-081-041)
Subtask 54-52-11-440-054-A
A. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-30-
00-440-013)
Subtask 54-52-11-410-059
B. Close Access
(1) Remove all the fixtures, tools, test and support equipment used
during this procedure.
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-52-11
Page 438
Feb 01/10
CES
R **ON A/C 234-235, 239-249, 251-299, 305-399, 403-499, 501-509, 511-526,
R 528-599,
TASK 54-52-11-000-004
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
-------------------------------------------------------------------------------
R
EFF : 234-235, 239-249, 251-299, 305-399,
403-499, 501-509, 511-526, 528-599,
54-52-11
Page 439
Feb 01/10
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-52-11-941-053
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
R
EFF : 234-235, 239-249, 251-299, 305-399,
403-499, 501-509, 511-526, 528-599,
54-52-11
Page 440
Feb 01/10
CES
**ON A/C 234-235, 239-249, 251-299, 305-399, 403-499,
Subtask 54-52-11-040-055
(1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-
30-00-481-041).
Subtask 54-52-11-040-055-A
(1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-
30-00-040-013).
Subtask 54-52-11-010-052-A
C. Get Access
R
EFF : 234-235, 239-249, 251-299, 305-399,
403-499, 501-509, 511-526, 528-599,
54-52-11
Page 441
Feb 01/10
CES
**ON A/C 305-306, 403-499,
Subtask 54-52-11-010-052
C. Get Access
4. Procedure
_________
Subtask 54-52-11-020-053
(1) Use a sharp non-metallic spatula to remove the remaining BONDING AND
ADHESIVE COMPOUNDS (Material No. 08-018B).
R
EFF : 234-235, 239-249, 251-299, 305-399,
403-499, 501-509, 511-526, 528-599,
54-52-11
Page 442
Feb 01/10
CES
location of the Seal at Pylon Rib 5
Figure 404/TASK 54-52-11-991-004
EFF :
403-499,
234-235, 239-249, 251-299, 305-399, 54-52-11
Page 443
Nov 01/09
CES
location of the Seal at Pylon Rib 5
Figure 404A/TASK 54-52-11-991-004-A
R
EFF :
501-509, 511-526, 528-599, 54-52-11
Page 444
Feb 01/10
CES
TASK 54-52-11-400-003
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
-------------------------------------------------------------------------------
R
EFF : 234-235, 239-249, 251-299, 305-399,
403-499, 501-509, 511-526, 528-599,
54-52-11
Page 445
Feb 01/10
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-52-11-941-054
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
R
EFF : 234-235, 239-249, 251-299, 305-399,
403-499, 501-509, 511-526, 528-599,
54-52-11
Page 446
Feb 01/10
CES
Subtask 54-52-11-860-052
Subtask 54-52-11-040-056
(1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-
30-00-481-041).
Subtask 54-52-11-040-056-A
(1) Make the thrust reverser unserviceable for maintenance (Ref. TASK 78-
30-00-040-013).
R
EFF : 234-235, 239-249, 251-299, 305-399,
403-499, 501-509, 511-526, 528-599,
54-52-11
Page 447
Feb 01/10
CES
R **ON A/C 234-235, 239-249, 251-299, 305-399, 403-499, 501-509, 511-526,
R 528-599,
Subtask 54-52-11-110-051
(1) Use a lint free cloth MISCELLANEOUS (Material No. 19-003) made moist
with CLEANING AGENTS (Material No. 11-004) to clean the flange and
the front panel that touches the seal.
(2) Use a lint free cloth MISCELLANEOUS (Material No. 19-003) to dry the
area.
4. Procedure
_________
Subtask 54-52-11-420-053
(1) Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-018B) on the
flange.
(2) Engage the new seal (1) on the edge of the flange.
R
EFF : 234-235, 239-249, 251-299, 305-399,
403-499, 501-509, 511-526, 528-599,
54-52-11
Page 448
Feb 01/10
CES
5. Close-up
________
Subtask 54-52-11-410-055-A
A. Close Access
Subtask 54-52-11-410-055
A. Close Access
Subtask 54-52-11-440-051
B. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-30-
00-081-041)
Subtask 54-52-11-440-051-B
B. Make the thrust reverser serviceable after maintenance (Ref. TASK 78-30-
00-440-013)
Subtask 54-52-11-860-053
(1) Remove all the fixtures, tools, test and support equipment used
during this procedure.
R
EFF : 234-235, 239-249, 251-299, 305-399,
403-499, 501-509, 511-526, 528-599,
54-52-11
Page 449
Feb 01/10
CES
CANTILEVER STRUCTURE - REPAIRS
______________________________
TASK 54-52-12-300-001
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 54-52-12
Page 801
May 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-52-12-861-050
Subtask 54-52-12-941-050
B. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
EFF :
ALL 54-52-12
Page 802
Feb 01/10
CES
(4) Make sure that the slats are in the fully retracted position
(Ref. TASK 27-80-00-866-005).
Subtask 54-52-12-040-050
Subtask 54-52-12-040-050-A
Subtask 54-52-12-010-050
D. Get Access
EFF :
ALL 54-52-12
Page 803
Feb 01/10
CES
4. Procedure
_________
Subtask 54-52-12-010-051
Subtask 54-52-12-410-050
Subtask 54-52-12-010-051-A
EFF :
ALL 54-52-12
Page 804
Feb 01/10
CES
Cantilever Structure
Figure 801/TASK 54-52-12-991-001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-52-12
Page 805
Feb 01/08
CES
Cantilever Structure
Figure 801A/TASK 54-52-12-991-001-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-52-12
Page 806
Nov 01/08
CES
Cantilever Structure
Figure 801B/TASK 54-52-12-991-001-B
R
EFF :
501-509, 511-526, 528-599, 54-52-12
Page 807
Feb 01/10
CES
Subtask 54-52-12-410-050-A
5. Close-up
________
Subtask 54-52-12-040-051
Subtask 54-52-12-040-051-A
Subtask 54-52-12-410-051
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-52-12
Page 808
Feb 01/10
CES
PYLON-TO-WING CENTER FILLETS - DESCRIPTION AND OPERATION
________________________________________________________
1. Description
___________
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-53-00
Page 1
Config-1 Nov 01/08
CES
Pylon to Wing Center Fillets
Figure 001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-53-00
Page 2
Config-1 Feb 01/08
CES
Pylon to Wing Center Fillets
Figure 001A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-53-00
Page 3
Config-1 Nov 01/08
CES
PYLON-TO-WING CENTER FILLETS - DESCRIPTION AND OPERATION
________________________________________________________
1. ___________
Description
(Ref. Fig. 001)
The center section consists of :
- Light alloy ribs attached to the upper rearward pylon box
- Lateral access doors installed on the ribs and made of composite material
- This compartment (comparment F) includes a pressure relief door to prevent
any overpressure in case of an air duct failure
- All the access panels are bolted.
R
EFF :
501-509, 511-526, 528-599, 54-53-00
Page 1
Config-2 Feb 01/10
CES
Pylon to Wing Center Fillets
Figure 001
R
EFF :
501-509, 511-526, 528-599, 54-53-00
Page 2
Config-2 Feb 01/10
CES
PYLON-TO-WING CENTER FILLETS - DEACTIVATION/REACTIVATION
________________________________________________________
TASK 54-53-00-040-001
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-53-00
Page 401
Feb 01/07
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-53-00-941-052
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF :
ALL 54-53-00
Page 402
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-53-00-040-051
Subtask 54-53-00-040-051-A
Subtask 54-53-00-010-050
C. Get Access
4. Procedure
_________
Subtask 54-53-00-040-052
EFF :
ALL 54-53-00
Page 403
Feb 01/10
CES
Aerodynamic Seal Deactivation/Reactivation
Figure 401/TASK 54-53-00-991-002
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-53-00
Page 404
Feb 01/08
CES
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) Remove the damaged seal (3) from its support (2).
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Clean the pylon structure and the wing structure around the space
where the seal was installed, with CLEANING AGENTS (Material No. 11-
016).
(6) Put three layers of BONDING AND ADHESIVE COMPOUNDS (Material No. 08-
061) (high-speed tape) on the space where the seal was installed.
NOTE : You must attach the first layer longitudinally on the space
____
and the second and third layers diagonally to get an overlap
of the layers.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-53-00
Page 405
Feb 01/08
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
Subtask 54-53-00-040-052-A
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) Remove the damaged seals (4) and (5) from their supports (3) and (6).
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-53-00
Page 406
Feb 01/10
CES
Aerodynamic Seal Deactivation/Reactivation
Figure 401A/TASK 54-53-00-991-002-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-53-00
Page 407
Nov 01/08
CES
Aerodynamic Seal Deactivation/Reactivation
Figure 401B/TASK 54-53-00-991-002-B
R
EFF :
501-509, 511-526, 528-599, 54-53-00
Page 408
Feb 01/10
CES
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
(5) Clean the pylon structure and the wing structure, around the space
where the seal was installed, with CLEANING AGENTS (Material No. 11-
016).
(6) Put three layers of BONDING AND ADHESIVE COMPOUNDS (Material No. 08-
061) (high-speed tape) on the space where the seal was installed.
NOTE : You must attach the first layer longitudinally on the space
____
and the second and third layers diagonally to get an overlap
of the layers.
5. Close-up
________
Subtask 54-53-00-440-051
Subtask 54-53-00-440-051-A
Subtask 54-53-00-860-050
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-53-00
Page 409
Feb 01/10
CES
(4) Make an entry in the aircraft technical log to show that the
aerodynamic seal of the pylon is removed and temporarily closed with
high-speed tape.
EFF :
ALL 54-53-00
Page 410
Nov 01/07
R
CES
TASK 54-53-00-440-001
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
EFF :
ALL 54-53-00
Page 411
May 01/09
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-53-00-941-053
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF :
ALL 54-53-00
Page 412
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
Subtask 54-53-00-040-053
Subtask 54-53-00-040-053-A
Subtask 54-53-00-010-051
C. Get Access
4. Procedure
_________
Subtask 54-53-00-440-052
(1) Remove the high-speed tape from the pylon structure and the wing
structure.
EFF :
ALL 54-53-00
Page 413
Feb 01/10
CES
(2) Remove the panel (1):
- For the left pylon: 414FR.
- For the right pylon: 423FL.
Subtask 54-53-00-440-052-A
(1) Remove the high-speed tape from the pylon structure and the wing
structure.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-53-00
Page 414
Feb 01/10
511-526, 528-599,
CES
**ON A/C ALL
5. Close-up
________
Subtask 54-53-00-440-053
Subtask 54-53-00-440-053-A
Subtask 54-53-00-860-051
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-53-00
Page 415
Feb 01/10
CES
PYLON-TO-WING CENTER FILLETS - INSPECTION/CHECK
_______________________________________________
TASK 54-53-00-200-001
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 54-53-00
Page 601
Nov 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-53-00-941-050
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1 (2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1 (2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
EFF :
ALL 54-53-00
Page 602
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
401-499,
Subtask 54-53-00-040-050
(1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-
00-481-041).
Subtask 54-53-00-040-050-A
(1) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-
00-040-012).
Subtask 54-53-00-941-051
C. Get Access
4. Procedure
_________
Subtask 54-53-00-220-050
EFF :
ALL 54-53-00
Page 603
Feb 01/10
CES
Inspection of the Pylon-to-Wing Center Fillets
Figure 601/TASK 54-53-00-991-001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-53-00
Page 604
Feb 01/08
CES
**ON A/C 234-235, 239-249, 251-299, 307-399,
1
_ Make sure that the damage is in the permitted limits:
- Zone 1: Permitted damage without repair
- Zone 2: Repair this damage before 100 flights
- Zone 3: Repair this damage immediately.
2
_ For repair, refer to the SRM (Ref. ASRM 51771202) (Ref. ASRM
51771302).
1
_ Separation of 25% of the total surface is permitted with local
areas of 45 cm2 (6.97 in.2).
1
_ Holes are not permitted.
(d) For wrinkle and distortion damage on panels 482AR and 471AL:
1
_ Make sure that the damage is in the permitted limits. Refer to
the SRM (Ref. ASRM 54500001).
EFF :
ALL 54-53-00
Page 605
Feb 01/10
CES
Inspection of the Pylon-to-Wing Center Fillets
Figure 601A/TASK 54-53-00-991-001-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-53-00
Page 606
Nov 01/08
CES
Inspection of the Pylon-to-Wing Center Fillets
Figure 601B/TASK 54-53-00-991-001-B
R
EFF :
501-509, 511-526, 528-599, 54-53-00
Page 607
Feb 01/10
CES
5. Close-up
________
Subtask 54-53-00-440-050
Subtask 54-53-00-440-050-A
Subtask 54-53-00-942-050
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-53-00
Page 608
Feb 01/10
CES
SKIN PANELS AND DOORS - REMOVAL/INSTALLATION
____________________________________________
TASK 54-53-11-000-001
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.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-53-11
Page 401
Feb 01/10
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-53-11-941-050
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-53-11-010-052
B. Get Access
EFF :
ALL 54-53-11
Page 402
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
401-499,
Subtask 54-53-11-040-050
Subtask 54-53-11-040-050-A
4. Procedure
_________
Subtask 54-53-11-020-050
(4) Remove the nuts (7), the screws (4) and the washers (3).
EFF :
ALL 54-53-11
Page 403
Feb 01/10
CES
Pressure Relief Door
Figure 401/TASK 54-53-11-991-001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-53-11
Page 404
Feb 01/10
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
R Subtask 54-53-11-020-050-A
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-53-11
Page 405
Feb 01/10
CES
R Presure Relief Door
R Figure 401A/TASK 54-53-11-991-001-B
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-53-11
Page 406
Feb 01/10
CES
R Presure Relief Door
R Figure 401B/TASK 54-53-11-991-001-C
R
EFF :
501-509, 511-526, 528-599, 54-53-11
Page 407
Feb 01/10
CES
R **ON A/C ALL
TASK 54-53-11-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-53-11
Page 408
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-53-11-869-050
Subtask 54-53-11-869-050-A
4. Procedure
_________
Subtask 54-53-11-420-050
EFF :
ALL 54-53-11
Page 409
Feb 01/10
CES
(2) Install the washers (3), the screws (4), the nuts (7) and tighten
them.
(3) Install the screws (1), the nuts (8) and tighten them.
(5) Install the washers (6), the screws (5) and tighten them.
R Subtask 54-53-11-420-050-A
R (2) Install the washers (2), the screws (1) and tighten them.
5. Close-up
________
Subtask 54-53-11-440-050
R
EFF :
ALL 54-53-11
Page 410
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-53-11-440-050-A
Subtask 54-53-11-942-050
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
ALL 54-53-11
Page 411
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
401-499,
TASK 54-53-11-000-002
WARNING : YOU MUST BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE
_______
ENGINE IS SHUTDOWN. THE ENGINE PARTS CAN STAY HOT FOR ALMOST 1 HOUR.
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 : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-53-11
Page 412
Feb 01/10
CES
3. __________
Job Set-up
Subtask 54-53-11-941-056
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-53-11-010-057
B. Get Access
Subtask 54-53-11-040-057
4. Procedure
_________
Subtask 54-53-11-020-054
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-53-11
Page 413
Feb 01/10
CES
R Pylon-to-Wing Access Panels
R Figure 402/TASK 54-53-11-991-003
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-53-11
Page 414
Feb 01/10
CES
TASK 54-53-11-400-002
WARNING : YOU MUST BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE
_______
ENGINE IS SHUTDOWN. THE ENGINE PARTS CAN STAY HOT FOR ALMOST 1 HOUR.
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. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-53-11
Page 415
Feb 01/10
CES
3. __________
Job Set-up
Subtask 54-53-11-869-055
(2) Make sure that the warning notice to tell persons not to start the
engine is in position.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Make sure that the warning notice to tell persons not to energize
the FADEC 1(2) is in position.
(4) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-
00-481-041).
4. Procedure
_________
Subtask 54-53-11-420-054
(1) To make the installation easier, you can apply COMMON GREASE
(Material No. 04-012) on the seals of the pylon-to-wing access
panels.
(3) Install the washers (2) and the screws (3) and tighten them.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-53-11
Page 416
Feb 01/10
CES
R Pylon-to-Wing Access Panels
R Figure 402A/TASK 54-53-11-991-003-A
R
EFF :
501-509, 511-526, 528-599, 54-53-11
Page 417
Feb 01/10
CES
R Seal Position at Installation of Pylon-to-Wing Access Panels
R Figure 403/TASK 54-53-11-991-006
R
EFF :
ALL 54-53-11
Page 418
Feb 01/10
CES
5. Close-up
________
Subtask 54-53-11-440-056
Subtask 54-53-11-942-055
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-53-11
Page 419
Feb 01/10
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
TASK 54-53-11-000-002-A
WARNING : YOU MUST BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE
_______
ENGINE IS SHUTDOWN. THE ENGINE PARTS CAN STAY HOT FOR ALMOST 1 HOUR.
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
-------------------------------------------------------------------------------
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-53-11
Page 420
Feb 01/10
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-53-11-941-057
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-53-11-010-058
B. Get Access
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-53-11
Page 421
Feb 01/10
CES
**ON A/C 234-235, 239-249, 251-299, 307-399,
Subtask 54-53-11-040-058
Subtask 54-53-11-040-058-A
4. Procedure
_________
Subtask 54-53-11-020-055
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-53-11
Page 422
Feb 01/10
CES
R Pylon-to-Wing Access Panels
R Figure 404/TASK 54-53-11-991-004
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-53-11
Page 423
Feb 01/10
CES
R Pylon-to-Wing Access Panels
R Figure 404A/TASK 54-53-11-991-004-A
R
EFF :
501-509, 511-526, 528-599, 54-53-11
Page 424
Feb 01/10
CES
TASK 54-53-11-400-002-A
WARNING : YOU MUST BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE
_______
ENGINE IS SHUTDOWN. THE ENGINE PARTS CAN STAY HOT FOR ALMOST 1 HOUR.
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. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-53-11
Page 425
Feb 01/10
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-53-11-869-056
(2) Make sure that the warning notice to tell persons not to start the
engine is in position.
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-53-11
Page 426
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Make sure that the warning notice to tell persons not to energize
the FADEC 1(2) is in position.
(4) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-
00-481-041).
Subtask 54-53-11-869-056-A
(2) Make sure that the warning notice to tell persons not to start the
engine is in position.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Make sure that the warning notice to tell persons not to energize
the FADEC 1(2) is in position.
(4) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-
00-040-012).
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-53-11
Page 427
Feb 01/10
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
4. Procedure
_________
Subtask 54-53-11-420-055
CAUTION : MAKE SURE THAT THE SEALS OF THE ACCESS PANELS ARE IN THE
_______
CORRECT POSITION BELOW THE WING LOWER SURFACE.
YOU CAN CAUSE DAMAGE TO THE SEALS IF THEY ARE NOT IN THE
CORRECT POSITION.
(1) To make the installation easier, you can apply COMMON GREASE
(Material No. 04-012) on the seals of the pylon-to-wing access
panels.
(3) Install the washers (2) and the screws (3) and tighten them.
(4) When you install the screws (3), do the electrical bonding at the
applicable location (Ref. TASK 20-28-00-912-007).
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-53-11
Page 428
Feb 01/10
CES
R **ON A/C 501-505,
Subtask 54-53-11-420-055-A
CAUTION : MAKE SURE THAT THE SEALS OF THE ACCESS PANELS ARE IN THE
_______
CORRECT POSITION BELOW THE WING LOWER SURFACE.
YOU CAN CAUSE DAMAGE TO THE SEALS IF THEY ARE NOT IN THE
CORRECT POSITION.
(1) To make the installation easier, you can apply COMMON GREASE
(Material No. 04-012) on the seals of the pylon-to-wing access
panels.
(3) Install the washers (2) and the screws (3) and tighten them.
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-53-11
Page 429
Feb 01/10
CES
Electrical Bonding of the Pylon-to-Wing Access Panels
R Figure 405/TASK 54-53-11-991-005- 12 (SHEET 1)
EFF :
234-235, 239-249, 307-399, 54-53-11
Page 430
Feb 01/10
CES
Electrical Bonding of the Pylon-to-Wing Access Panels
R Figure 405/TASK 54-53-11-991-005- 22 (SHEET 2)
EFF :
234-235, 239-249, 307-399, 54-53-11
Page 431
Feb 01/10
CES
Electrical Bonding of the Pylon-to-Wing Access Panels
R Figure 405A/TASK 54-53-11-991-005-A12 (SHEET 1)
EFF :
501-505, 54-53-11
Page 432
Feb 01/10
CES
Electrical Bonding of the Pylon-to-Wing Access Panels
R Figure 405A/TASK 54-53-11-991-005-A22 (SHEET 2)
EFF :
501-505, 54-53-11
Page 433
Feb 01/10
CES
(4) Measure the surface electrical resistance of the installed
pylon-to-wing access panels (Ref. TASK 20-28-00-720-011).
5. Close-up
________
Subtask 54-53-11-440-057
Subtask 54-53-11-440-057-A
Subtask 54-53-11-942-056
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-53-11
Page 434
Feb 01/10
CES
SKIN PANELS AND DOORS - INSPECTION/CHECK
________________________________________
TASK 54-53-11-200-001
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.
WARNING : MAKE SURE THAT THE PNEUMATIC SYSTEM IS DEPRESSURIZED BEFORE YOU START
_______
WORK ON THE PNEUMATIC SYSTEM.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-53-11
Page 601
Nov 01/07
R
CES
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-53-11-941-051
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1 (2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF :
ALL 54-53-11
Page 602
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1 (2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2)
Subtask 54-53-11-040-051
Subtask 54-53-11-010-050
C. Get Access
R Subtask 54-53-11-010-050-A
R C. Get Access
EFF :
ALL 54-53-11
Page 603
Feb 01/10
CES
R **ON A/C ALL
4. Procedure
_________
Subtask 54-53-11-210-051
(2) Do the inspection of the bleed air duct to make sure that there is no
damage.
(3) Do the inspection of the automatic opening mechanism, the hinges, the
adjacent structure of the pressure relief door. Make sure that there
are no cracks, marks or damage.
R Subtask 54-53-11-210-051-A
R
EFF :
ALL 54-53-11
Page 604
Feb 01/10
CES
Pressure Relief Door
Figure 601/TASK 54-53-11-991-002
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-53-11
Page 605
Feb 01/10
CES
R Pressure Relief Door
R Figure 601A/TASK 54-53-11-991-002-B
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-53-11
Page 606
Feb 01/10
CES
R Pressure Relief Door
R Figure 601B/TASK 54-53-11-991-002-C
EFF :
501-509, 511-526, 528-599, 54-53-11
Page 607
Feb 01/10
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
R (2) Do the inspection of the bleed air duct to make sure that there is no
R damage.
R (3) Do the inspection of the automatic opening mechanism, the hinges, the
R adjacent structure of the pressure relief door. Make sure that there
R are no cracks, marks or damage.
5. Close-up
________
Subtask 54-53-11-410-051
Subtask 54-53-11-410-051-A
Subtask 54-53-11-440-051
EFF :
ALL 54-53-11
Page 608
Feb 01/10
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
R Subtask 54-53-11-440-051-A
Subtask 54-53-11-942-051
C. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-53-11
Page 609
Feb 01/10
CES
AFT FIXED FAIRING - DESCRIPTION AND OPERATION
_____________________________________________
1. Description
___________
The fixed fairing is attached at two points to the pylon box at RIB10 and
one point to the wing at rear false spar.
The fixed fairing is composed of:
- six ribs made of light alloy sheet
- two skin panels made of light alloy sheet
- three longitudinal members made of light alloy sheet
- two access panels made of carbon and honeycomb (sandwich panel).
All the access panels are bolted.
Standard attachement is made by aluminum alloy rivets.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-54-00
Page 1
Config-1 Nov 01/08
CES
Fixed Fairing
Figure 001 (SHEET 1)
EFF :
201-212,
001-049, 051-099, 101-105, 151-199, 54-54-00
Page 2
Config-1 Nov 01/07
CES
Fixed Fairing
Figure 001 (SHEET 2)
EFF :
201-212,
001-049, 051-099, 101-105, 151-199, 54-54-00
Page 3
Config-1 Nov 01/07
CES
Fixed Fairing
Figure 001A (SHEET 1)
R
EFF :
401-499,
106-149, 213-233, 236-238, 301-306, 54-54-00
Page 4
Config-1 Feb 01/08
CES
Fixed Fairing
Figure 001A (SHEET 2)
R
EFF :
401-499,
106-149, 213-233, 236-238, 301-306, 54-54-00
Page 5
Config-1 Feb 01/08
CES
Fixed Fairing
Figure 001B (SHEET 1)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-54-00
Page 6
Config-1 Nov 01/08
CES
Fixed Fairing
Figure 001B (SHEET 2)
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-54-00
Page 7
Config-1 Nov 01/08
CES
AFT FIXED FAIRING - DESCRIPTION AND OPERATION
_____________________________________________
1. ___________
Description
(Ref. Fig. 001)
The fixed fairing is attached by two points to the pylon box at RIB10 and
one point to the wing at rear false spar.
The fixed fairing is composed of:
- six ribs made of light alloy sheet
- two skin panels made of light alloy sheet
- three longitudinal members made of light alloy sheet
- two access panels made of carbon and honeycomb (sanwich panel).
All the access panels are bolted.
Standard attachment is made by alluminium alloy rivets.
R
EFF :
501-509, 511-526, 528-599, 54-54-00
Page 1
Config-2 Feb 01/10
CES
Fixed Fairing
Figure 001 (SHEET 1)
R
EFF :
501-509, 511-526, 528-599, 54-54-00
Page 2
Config-2 Feb 01/10
CES
Fixed Fairing
Figure 001 (SHEET 2)
R
EFF :
501-509, 511-526, 528-599, 54-54-00
Page 3
Config-2 Feb 01/10
CES
AFT FIXED FAIRING - REMOVAL/INSTALLATION
________________________________________
TASK 54-54-00-000-001
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
There is an alternative method for this procedure. This task gives one of
the methods. For the other method, refer to the other task in this page
block.
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-54-00
Page 401
Nov 01/07
R
CES
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-54-00
Page 402
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-54-00-865-050
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU HYD/HYD PWR/B WARN/& CTL 2702GJ C12
121VU HYDRAULIC/HYD POWER/Y 3803GX N30
123VU B HYD/ELEC PUMP 2701GJ AB09
123VU Y HYD/ELEC/PUMP 3802GX AB06
123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
Subtask 54-54-00-941-050
B. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
R (4) Obey the safety procedures of the hydraulic system (Ref. TASK 29-00-
00-910-002).
EFF :
ALL 54-54-00
Page 403
May 01/08
CES
Subtask 54-54-00-860-050
Subtask 54-54-00-040-051
Subtask 54-54-00-040-051-A
Subtask 54-54-00-010-050
E. Get Access
(a) For the left pylon 471CL, 475AL, 475BL, 475CL, 476AR, 476BR,
476CR.
(b) For the right pylon 481BL, 485AL, 485BL, 485CL, 482CR, 486AR,
486BR, 486CR.
EFF :
ALL 54-54-00
Page 404
Feb 01/10
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
Subtask 54-54-00-010-050-A
E. Get Access
(a) For the left pylon 471DL, 475AL, 475BL, 471CR, 475AR, 475BR.
(b) For the right pylon 481CL, 485AL, 485BL, 481DR, 485AR, 485BR.
Subtask 54-54-00-020-050
Subtask 54-54-00-020-050-A
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-54-00
Page 405
Feb 01/10
511-526, 528-599,
CES
**ON A/C ALL
Subtask 54-54-00-020-052
4. Procedure
_________
Subtask 54-54-00-020-053
EFF :
ALL 54-54-00
Page 406
Feb 01/10
CES
Installation of the Hydraulic Lines
Figure 401/TASK 54-54-00-991-001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-54-00
Page 407
Aug 01/09
CES
Installation of the Hydraulic Lines
Figure 401A/TASK 54-54-00-991-001-A
R
EFF :
501-509, 511-526, 528-599, 54-54-00
Page 408
Feb 01/10
CES
Attach Fittings on the Aft Fixed Fairing
Figure 402/TASK 54-54-00-991-002
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-54-00
Page 409
Feb 01/08
CES
Attach Fittings on the Aft Fixed Fairing
Figure 402A/TASK 54-54-00-991-002-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-54-00
Page 410
Nov 01/08
CES
R **ON A/C 501-509, 511-526, 528-599,
(3) Remove the nut (19), the washer (20) and the bolt (21).
(5) Remove the nut (17), the washer (18), the bolt (16) and the washer
(14).
NOTE : Two persons are necessary to move the aft fixed fairing.
____
EFF :
ALL 54-54-00
Page 411
Feb 01/10
CES
Attach Fittings on the Aft Fixed Fairing
Figure 402B/TASK 54-54-00-991-002-B
R
EFF :
501-509, 511-526, 528-599, 54-54-00
Page 412
Feb 01/10
CES
TASK 54-54-00-000-001- 01
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 54-54-00
Page 413
May 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-54-00
Page 414
Feb 01/10
511-526, 528-599,
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-54-00-941-054
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-54-00-040-052
Subtask 54-54-00-040-052-A
EFF :
ALL 54-54-00
Page 415
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
401-499,
Subtask 54-54-00-010-052
C. Get Access
(a) For the left pylon 471CL, 475AL, 475BL, 475CL, 476AR, 476BR,
476CR.
(b) For the right pylon 481BL, 485AL, 485BL, 485CL, 482CR, 486AR,
486BR, 486CR.
Subtask 54-54-00-010-052-A
C. Get Access
(a) For the left pylon 471DL, 475AL, 475BL, 471CR, 475AR, 475BR
(b) For the right pylon 481CL, 485AL, 485BL, 481DR, 485AR, 485BR
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-54-00
Page 416
Feb 01/10
511-526, 528-599,
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
401-499,
Subtask 54-54-00-020-055
Subtask 54-54-00-020-055-A
Subtask 54-54-00-020-060
EFF :
ALL 54-54-00
Page 417
Feb 01/10
CES
Drain Lines - Aft Fixed Fairing
Figure 403/TASK 54-54-00-991-009
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-54-00
Page 418
Nov 01/08
CES
Drain Lines - Aft Fixed Fairing
Figure 403A/TASK 54-54-00-991-009-A
R
EFF :
501-509, 511-526, 528-599, 54-54-00
Page 419
Feb 01/10
CES
Subtask 54-54-00-020-056
4. Procedure
_________
Subtask 54-54-00-020-058
EFF :
ALL 54-54-00
Page 420
Feb 01/10
CES
Plate and Fitting - Aft Fixed Fairing
Figure 404/TASK 54-54-00-991-007
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-54-00
Page 421
Aug 01/09
CES
Plate and Fitting - Aft Fixed Fairing
Figure 404A/TASK 54-54-00-991-007-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-54-00
Page 422
Aug 01/09
CES
Plate and Fitting - Aft Fixed Fairing
Figure 404B/TASK 54-54-00-991-007-B
R
EFF :
501-509, 511-526, 528-599, 54-54-00
Page 423
Feb 01/10
CES
Attach Fittings - Aft Fixed Fairing
Figure 405/TASK 54-54-00-991-008
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-54-00
Page 424
Feb 01/08
CES
Attach Fittings - Aft Fixed Fairing
Figure 405A/TASK 54-54-00-991-008-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-54-00
Page 425
Nov 01/08
CES
R **ON A/C 501-509, 511-526, 528-599,
(4) Remove the nut (16), the washer (15), the bolt (14) and the washer
(12).
NOTE : Two persons are necessary to move the aft fixed fairing.
____
EFF :
ALL 54-54-00
Page 426
Feb 01/10
CES
Attach Fittings - Aft Fixed Fairing
Figure 405B/TASK 54-54-00-991-008-B
R
EFF :
501-509, 511-526, 528-599, 54-54-00
Page 427
Feb 01/10
CES
TASK 54-54-00-400-001
1. __________________
Reason for the Job
There is an alternative method for this procedure. This task gives one of
the methods. For the other method, refer to the other task in this page
block.
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-54-00
Page 428
Nov 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-54-00
Page 429
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-54-00-860-051
(4) Make sure that the hydraulic system is depressurized (Ref. TASK 29-
00-00-864-001).
(5) Make sure that the hydraulic reservoir is depressurized (Ref. TASK
29-14-00-614-001).
(6) Make sure that you obey the safety procedures of the hydraulic system
(Ref. TASK 29-00-00-910-002).
Subtask 54-54-00-860-051-A
(4) Make sure that the hydraulic system is depressurized (Ref. TASK 29-
00-00-864-001).
(5) Make sure that the hydraulic reservoir is depressurized (Ref. TASK
29-14-00-614-001).
EFF :
ALL 54-54-00
Page 430
Feb 01/10
CES
(6) Make sure that you obey the safety procedures of the hydraulic system
(Ref. TASK 29-00-00-910-002).
Subtask 54-54-00-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and
tagged
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU HYD/HYD PWR/B WARN/& CTL 2702GJ C12
121VU HYDRAULIC/HYD POWER/Y 3803GX N30
123VU B HYD/ELEC PUMP 2701GJ AB09
123VU Y HYD/ELEC/PUMP 3802GX AB06
123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
4. Procedure
_________
Subtask 54-54-00-420-050
EFF :
ALL 54-54-00
Page 431
Feb 01/10
CES
(3) Install the washer (14), the bolt (16), the washer (18) and the nut
(17).
(5) Install the bolt (21), the washer (20) and the nut (19). Tighten the
nut.
NOTE : You must install the bolt (21) with the head down.
____
(6) TORQUE the nuts (11) and (12) to between 2.6 and 3 m.daN (19.17 and
22.12 lbf.ft).
(7) TORQUE the nut (9) to between 0.35 and 0.45 m.daN (30.97 and 39.82
lbf.in).
(8) TORQUE the nut (17) to between 3.6 and 4.1 m.daN (26.54 and 30.23
lbf.ft).
(11) Install the washer (23). Install the screw (24) and tighten it.
NOTE : You must do an electrical bonding of the screw (24) when you
____
install it (Ref. TASK 20-28-00-912-004).
Subtask 54-54-00-420-052
EFF :
ALL 54-54-00
Page 432
Feb 01/10
CES
(1) Remove the blanking plugs from the disconnected line ends.
(2) Connect the drain lines (7) and (8) (Ref. TASK 20-21-12-911-001).
(4) Install the bolt (5). Install the nut (6) and tighten it.
Subtask 54-54-00-710-050
(6) Make sure that the hydraulic lines (1), (2), (3) and (4) are sealed.
Subtask 54-54-00-710-050-A
(6) Make sure that the hydraulic lines (1), (2), (3) and (4) are sealed.
EFF :
ALL 54-54-00
Page 433
Feb 01/10
CES
**ON A/C ALL
5. Close-up
________
Subtask 54-54-00-420-053
Subtask 54-54-00-420-053-A
Subtask 54-54-00-410-050
B. Close Access
(a) For the left pylon: 471CL, 475AL, 475BL, 475CL, 476AR, 476BR,
476CR.
(b) For the right pylon: 481BL, 485AL, 485BL, 485CL, 482CR, 486AR,
486BR, 486CR.
EFF :
ALL 54-54-00
Page 434
Feb 01/10
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
Subtask 54-54-00-410-050-A
B. Close Access
(a) For the left pylon: 471DL, 475AL, 475BL, 471CR, 475AR, 475BR.
(b) For the right pylon: 481CL, 485AL, 485BL, 481DR, 485AR, 485BR.
Subtask 54-54-00-440-051
Subtask 54-54-00-440-051-A
Subtask 54-54-00-865-054
(1) Remove the safety clip(s) and the tag(s) and close this(these)
circuit breaker(s):
2701GJ, 2702GJ, 3801GX, 3802GX, 3803GX.
(2) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-54-00
Page 435
Feb 01/10
CES
(4) Remove the warning notice(s).
EFF :
ALL 54-54-00
Page 436
Aug 01/09
R
CES
TASK 54-54-00-400-001- 01
1. __________________
Reason for the Job
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-54-00
Page 437
Nov 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-54-00
Page 438
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-54-00-860-052
Subtask 54-54-00-860-052-A
4. Procedure
_________
Subtask 54-54-00-420-055
EFF :
ALL 54-54-00
Page 439
Feb 01/10
CES
**ON A/C 234-235, 239-249, 251-299, 307-399,
NOTE : Two persons are necessary to move the aft fixed fairing.
____
(2) Install the bolts (9) and the nuts (10), (7) and (8).
(3) Install the washer (12), the bolt (14), the washer (15) and the nut
(16).
(5) TORQUE the nuts (10) and (7) to between 2.6 and 3 m.daN (19.17 and
22.12 lbf.ft).
(6) TORQUE the nut (8) to between 0.35 and 0.45 m.daN (30.97 and 39.82
lbf.in).
(7) TORQUE the nut (16) to between 3.6 and 4.1 m.daN (26.54 and 30.23
lbf.ft).
(10) Install the washer (18). Install the screw (17) and tighten it.
NOTE : You must do an electrical bonding of the screw (17) when you
____
install it (Ref. TASK 20-28-00-912-004).
EFF :
ALL 54-54-00
Page 440
Feb 01/10
CES
Subtask 54-54-00-420-058
Subtask 54-54-00-420-059
EFF :
ALL 54-54-00
Page 441
Feb 01/10
CES
**ON A/C ALL
(1) Remove the blanking plugs from the disconnected line ends.
(2) Connect the two drain lines (21) and (22) (Ref. TASK 20-21-12-911-
001).
5. Close-up
________
Subtask 54-54-00-420-056
Subtask 54-54-00-420-056-A
Subtask 54-54-00-410-058
(a) For the left pylon: 471CL, 475AL, 475BL, 475CL, 476AR, 476BR,
476CR
(b) For the right pylon: 481BL, 485AL, 485BL, 485CL, 482CR, 486AR,
486BR, 486CR.
EFF :
ALL 54-54-00
Page 442
Feb 01/10
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
Subtask 54-54-00-410-058-A
(a) For the left pylon: 471DL, 475AL, 475BL, 471CR, 475AR, 475BR
(b) For the right pylon: 481CL, 485AL, 485BL, 481DR, 485AR, 485BR.
Subtask 54-54-00-440-052
Subtask 54-54-00-440-052-A
Subtask 54-54-00-410-052
D. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-54-00
Page 443
Feb 01/10
CES
AFT FIXED FAIRING - INSPECTION/CHECK
____________________________________
TASK 54-54-00-200-001
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 54-54-00
Page 601
May 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-54-00-941-052
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1 (2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1 (2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2)
EFF :
ALL 54-54-00
Page 602
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
401-499,
Subtask 54-54-00-040-050
Subtask 54-54-00-040-050-A
Subtask 54-54-00-941-053
C. Get Access
Subtask 54-54-00-020-051
D. Removal of Component
4. Procedure
_________
EFF :
ALL 54-54-00
Page 603
Feb 01/10
CES
Aft Fixed Fairing
Figure 601/TASK 54-54-00-991-003
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-54-00
Page 604
Feb 01/08
CES
**ON A/C 234-235, 239-249, 251-299, 307-399,
Subtask 54-54-00-220-050
(1) Measure the dimension of the aft fixed fairing and make sure that the
dimensions are correct.
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| E | 0.3740 | 0.3745 | | | 0.3733 | | |
| OD 1 | (9.499) | (9.512) | | | (9.481) | | |
| | | | 0.0003 | 0.0014 | | | 0.0028|
| | | | (0.007) | (0.035) | | |(0.071) |
| E | 0.3748 | 0.3754 | | | | 0.3761 | |
| ID 2 | (9.519) | (9.535) | | | | (9.552) | |
-------------------------------------------------------------------------------
Subtask 54-54-00-220-051
(1) Measure the dimension of the aft fixed fairing and make sure that the
dimensions are correct.
EFF :
ALL 54-54-00
Page 605
Feb 01/10
CES
Aft Fixed Fairing
Figure 601A/TASK 54-54-00-991-003-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-54-00
Page 606
Nov 01/08
CES
Aft Fixed Fairing
Figure 601B/TASK 54-54-00-991-003-B
R
EFF :
501-509, 511-526, 528-599, 54-54-00
Page 607
Feb 01/10
CES
Upper Forward Attach-Fitting of the Fixed Fairing
Figure 602/TASK 54-54-00-991-004
EFF :
ALL 54-54-00
Page 608
Nov 01/07
R
CES
Lower Forward Attach-Fitting of the Fixed Fairing
Figure 603/TASK 54-54-00-991-005
EFF :
ALL 54-54-00
Page 609
Nov 01/07
R
CES
Aft Attach-Fitting of the Fixed Fairing
Figure 604/TASK 54-54-00-991-006
EFF :
ALL 54-54-00
Page 610
Nov 01/07
R
CES
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| E | 0.3740 | 0.3745 | | | 0.3728 | | |
| OD 1 | (9.499) | (9.512) | | | (9.469) | | |
| | | | 0.0003 | 0.0022 | | | 0.0046|
| | | | (0.007) | (0.055) | | |(0.116) |
| E | 0.3748 | 0.3762 | | | | 0.3774 | |
| ID 3 | (9.519) | (9.555) | | | | (9.585) | |
-------------------------------------------------------------------------------
Subtask 54-54-00-220-052
(1) Measure the dimension of the aft fixed fairing and make sure that the
dimensions are correct.
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| E | 0.4718 | 0.4722 | | | 0.4711 | | |
| OD 3 |(11.983) |(11.993) | | |(11.965) | | |
| | | | 0.0002 | 0.0013 | | | 0.0028|
| | | | (0.005) | (0.033) | | |(0.071) |
| E | 0.4724 | 0.4731 | | | | 0.4739 | |
| ID 4 |(11.998) |(12.016) | | | |(12.037) | |
-------------------------------------------------------------------------------
EFF :
ALL 54-54-00
Page 611
Nov 01/07
R
CES
Subtask 54-54-00-220-053
(1) Measure the dimension of the aft fixed fairing and make sure that the
dimensions are correct.
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| F | 0.3740 | 0.3745 | | | 0.3733 | | |
| OD 5 | (9.499) | (9.512) | | | (9.481) | | |
| | | | 0.0003 | 0.0014 | | | 0.0028|
| | | | (0.007) | (0.035) | | |(0.071) |
| F | 0.3748 | 0.3754 | | | | 0.3761 | |
| ID 6 | (9.519) | (9.535) | | | | (9.552) | |
-------------------------------------------------------------------------------
Subtask 54-54-00-220-054
(1) Measure the dimension of the aft fixed fairing and make sure that the
dimensions are correct.
EFF :
ALL 54-54-00
Page 612
Nov 01/07
R
CES
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| F | 0.3740 | 0.3745 | | | 0.3728 | | |
| OD 5 | (9.499) | (9.512) | | | (9.469) | | |
| | | | 0.0003 | 0.0022 | | | 0.0046|
| | | | (0.007) | (0.055) | | |(0.116) |
| F | 0.3748 | 0.3762 | | | | 0.3774 | |
| ID 7 | (9.519) | (9.555) | | | | (9.585) | |
-------------------------------------------------------------------------------
Subtask 54-54-00-220-055
(1) Measure the dimension of the aft fixed fairing and make sure that the
dimensions are correct.
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| F | 0.4718 | 0.4722 | | | 0.4711 | | |
| OD 7 |(11.983) |(11.993) | | |(11.965) | | |
| | | | 0.0002 | 0.0013 | | | 0.0028|
| | | | (0.005) | (0.033) | | |(0.071) |
| F | 0.4724 | 0.4731 | | | | 0.4739 | |
| ID 8 |(11.998) |(12.016) | | | |(12.037) | |
-------------------------------------------------------------------------------
Subtask 54-54-00-220-056
(1) Measure the dimension of the aft fixed fairing and make sure that the
dimensions are correct.
EFF :
ALL 54-54-00
Page 613
Nov 01/07
R
CES
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| G | 0.4365 | 0.4370 | | | 0.4349 | | |
| OD 9 |(11.087) |(11.099) | | |(11.046) | | |
| | | | 0.0020 | 0.0032 | | | 0.0064|
| | | | (0.050) | (0.081) | | |(0.162) |
| G | 0.4390 | 0.4397 | | | | 0.4413 | |
| ID 12 |(11.150) |(11.168) | | | |(11.209) | |
-------------------------------------------------------------------------------
Subtask 54-54-00-220-057
(1) Measure the dimension of the aft fixed fairing and make sure that the
dimensions are correct.
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| G | 0.4365 | 0.4370 | | | 0.4346 | | |
| OD 9 |(11.087) |(11.099) | | |(11.038) | | |
| | | | 0.0020 | 0.0032 | | | 0.0078|
| | | | (0.050) | (0.081) | | |(0.198) |
| G | 0.4390 | 0.4397 | | | | 0.4424 | |
| ID 10 |(11.150) |(11.168) | | | |(11.236) | |
-------------------------------------------------------------------------------
Subtask 54-54-00-220-058
(1) Measure the dimension of the aft fixed fairing and make sure that the
dimensions are correct.
EFF :
ALL 54-54-00
Page 614
Nov 01/07
R
CES
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| G | 0.5505 | 0.5509 | | | 0.5498 | | |
| OD 10 |(13.982) |(13.992) | | |(13.964) | | |
| | | | 0.0003 | 0.0014 | | | 0.0028|
| | | | (0.007) | (0.035) | | |(0.071) |
| G | 0.5512 | 0.5519 | | | | 0.5526 | |
| ID 13 |(14.000) |(14.018) | | | |(14.036) | |
-------------------------------------------------------------------------------
Subtask 54-54-00-220-059
(1) Measure the dimension of the aft fixed fairing and make sure that the
dimensions are correct.
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| G | 0.4365 | 0.4370 | | | 0.4361 | | |
| OD 11 |(11.087) |(11.099) | | |(11.076) | | |
| | | | -0.0004 | 0.0009 | | | 0.0017|
| | | |-(0.010) | (0.022) | | |(0.043) |
| G | 0.4366 | 0.4374 | | | | 0.4378 | |
| ID 14 |(11.089) |(11.109) | | | |(11.120) | |
-------------------------------------------------------------------------------
Subtask 54-54-00-220-060
(1) Measure the dimension of the aft fixed fairing and make sure that the
dimensions are correct.
EFF :
ALL 54-54-00
Page 615
Nov 01/07
R
CES
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| G | 0.3139 | 0.3144 | | | 0.3094 | | |
| OD 11 | (7.973) | (7.985) | | | (7.858) | | |
| | | | 0.0006 | 0.0089 | | | 0.0179|
| | | | (0.015) | (0.226) | | |(0.454) |
| G | 0.3150 | 0.3228 | | | | 0.3273 | |
| ID 13 | (8.000) | (8.199) | | | | (8.313) | |
-------------------------------------------------------------------------------
Subtask 54-54-00-220-061
(1) Measure the dimension of the aft fixed fairing and make sure that the
dimensions are correct.
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| H | 0.4365 | 0.4370 | | | 0.4350 | | |
| OD 16 |(11.087) |(11.099) | | |(11.048) | | |
| | | | 0.0020 | 0.0032 | | | 0.0063|
| | | | (0.050) | (0.081) | | |(0.160) |
| H | 0.4390 | 0.4397 | | | | 0.4413 | |
| ID 15 |(11.150) |(11.168) | | | |(11.209) | |
-------------------------------------------------------------------------------
Subtask 54-54-00-220-062
(1) Measure the dimension of the aft fixed fairing and make sure that the
dimensions are correct.
EFF :
ALL 54-54-00
Page 616
Nov 01/07
R
CES
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| H | 0.3740 | 0.3745 | | | 0.3733 | | |
| OD 17 | (9.499) | (9.512) | | | (9.481) | | |
| | | | 0.0003 | 0.0014 | | | 0.0028|
| | | | (0.007) | (0.035) | | |(0.071) |
| H | 0.3748 | 0.3754 | | | | 0.3761 | |
| ID 18 | (9.519) | (9.535) | | | | (9.552) | |
-------------------------------------------------------------------------------
5. Close-up
________
Subtask 54-54-00-420-051
A. Installation of Component
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-54-00-440-050
Subtask 54-54-00-440-050-A
EFF :
ALL 54-54-00
Page 617
Feb 01/10
CES
R **ON A/C ALL
Subtask 54-54-00-942-052
C. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-54-00
Page 618
Nov 01/07
CES
R **ON A/C 501-509, 511-526, 528-599,
TASK 54-54-00-200-002
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
501-509, 511-526, 528-599, 54-54-00
Page 619
Feb 01/10
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-54-00-941-055
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC.
R
EFF :
501-509, 511-526, 528-599, 54-54-00
Page 620
Feb 01/10
CES
Subtask 54-54-00-010-053
B. Get Access
Subtask 54-54-00-020-061
Subtask 54-54-00-040-053
Subtask 54-54-00-110-050
R
EFF :
501-509, 511-526, 528-599, 54-54-00
Page 621
Feb 01/10
CES
(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 54-54-00-220-063
A. Inspection
(Ref. Fig. 605/TASK 54-54-00-991-010)
(a) Damages:
- If you find damages, refer to the Structural Repair Manual
(Ref. ASRM 54561102) and (Ref. ASRM 54541202) for corrective
action.
5. Close-up
________
Subtask 54-54-00-420-060
Subtask 54-54-00-440-053
Subtask 54-54-00-410-053
C. Close Access
R
EFF :
501-509, 511-526, 528-599, 54-54-00
Page 622
Feb 01/10
CES
Pylon Aft Fixed Fairing
Figure 605/TASK 54-54-00-991-010
R
EFF :
501-509, 511-526, 528-599, 54-54-00
Page 623
Feb 01/10
CES
(2) Close the fan cowl doors (Ref. TASK 71-13-00-410-010):
FOR 1000EM1
437AL, 438AR
FOR 1000EM2
447AL, 448AR.
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
501-509, 511-526, 528-599, 54-54-00
Page 624
Feb 01/10
CES
SKIN PANELS - AFT FIXED FAIRING - CLEANING/PAINTING
___________________________________________________
TASK 54-54-11-100-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-54-11
Page 701
Aug 01/07
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-54-11-941-050
A. Safety Precautions
(a) Put a WARNING NOTICE to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF :
ALL 54-54-11
Page 702
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a WARNING NOTICE to tell persons not to energize the FADEC.
Subtask 54-54-11-040-050
Subtask 54-54-11-040-050-A
Subtask 54-54-11-010-050
C. Get Access
(1) Put an ACCESS PLATFORM 3M (10 FT) in position at zone 470 (480).
4. Procedure
_________
Subtask 54-54-11-220-050
A. Inspection
EFF :
ALL 54-54-11
Page 703
Feb 01/10
CES
Inspection Areas for Cleaning of the Skin Panels
Figure 701/TASK 54-54-11-991-001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-54-11
Page 704
Feb 01/08
CES
Inspection Areas for Cleaning of the Skin Panels
Figure 701A/TASK 54-54-11-991-001-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-54-11
Page 705
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-54-11-110-050
(1) Apply CLEANING AGENTS (Material No. 11-001C) with a lint-free cotton
cloth MISCELLANEOUS (Material No. 19-003).
(3) Clean the dirt areas with a BRUSH - BRISTLED, FIBER, SOFT or a
lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
R
EFF :
ALL 54-54-11
Page 706
Feb 01/10
CES
Inspection Areas for Cleaning of the Skin Panels
Figure 701B/TASK 54-54-11-991-001-B
R
EFF :
501-509, 511-526, 528-599, 54-54-11
Page 707
Feb 01/10
CES
Subtask 54-54-11-220-051
C. Inspection
(2) Make sure that there is no corrosion damage, heat damage or defective
paint:
- If you find corrosion damage, heat damage or defective paint, refer
R to the Structural Repair Manual (Ref. ASRM 54541101) or (Ref. ASRM
54541102) for damage classification and corrective action.
5. Close-up
________
Subtask 54-54-11-440-050
Subtask 54-54-11-440-050-A
EFF :
ALL 54-54-11
Page 708
Feb 01/10
CES
R **ON A/C ALL
Subtask 54-54-11-860-050
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-54-11
Page 709
Nov 01/07
CES
SEAL - AFT FIXED FAIRING - REPAIRS
__________________________________
TASK 54-54-41-300-001
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. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-54-41
Page 801
May 01/05
CES
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-54-41
Page 802
May 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-54-41-865-050
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
49VU HYD/HYD PWR/B WARN/& CTL 2702GJ C12
121VU HYDRAULIC/HYD POWER/Y 3803GX N30
123VU B HYD/ELEC PUMP 2701GJ AB09
123VU Y HYD/ELEC/PUMP 3802GX AB06
123VU Y HYD/ELEC/ELEC PUMP/NORM 3801GX AB03
Subtask 54-54-41-941-050
B. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
EFF :
ALL 54-54-41
Page 803
Feb 01/10
CES
(4) Obey the safety procedures of the hydraulic system (Ref. TASK 29-00-
00-910-002)
Subtask 54-54-41-040-050
Subtask 54-54-41-040-050-A
Subtask 54-54-41-020-050
4. Procedure
_________
EFF :
ALL 54-54-41
Page 804
Feb 01/10
CES
Aft Fixed Fairing Seal
Figure 801/TASK 54-54-41-991-001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-54-41
Page 805
Feb 01/08
CES
Aft Fixed Fairing Seal
Figure 801A/TASK 54-54-41-991-001-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-54-41
Page 806
Nov 01/08
CES
Aft Fixed Fairing Seal
Figure 801B/TASK 54-54-41-991-001-B
R
EFF :
501-509, 511-526, 528-599, 54-54-41
Page 807
Feb 01/10
CES
**ON A/C ALL
Subtask 54-54-41-010-051
(1) Remove and discard the seals (1) and (2) from the retainers.
(2) Clean the retainers with CLEANING AGENTS (Material No. 11-003) and a
MISCELLANEOUS (Material No. 19-003).
Subtask 54-54-41-410-050
(1) Put the new seal (1) and the new seal (2) in position on the
retainers.
5. Close-up
________
Subtask 54-54-41-420-051
Subtask 54-54-41-440-050
EFF :
ALL 54-54-41
Page 808
Nov 01/08
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-54-41-440-050-A
Subtask 54-54-41-865-051
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s):
2701GJ, 2702GJ, 3801GX, 3802GX, 3803GX
Subtask 54-54-41-942-050
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-54-41
Page 809
Feb 01/10
CES
AFT MOVABLE FAIRING - DESCRIPTION AND OPERATION
_______________________________________________
1. Description
___________
The movable fairing is hinged at RIB14 and linked to the flap by a rod
attached to the fairing by a serrated plate system.
The movable fairing is composed of:
- an inner structure made of stainless steel and titanium alloy.
- an outer skin made of carbon and honeycomb
- one access panel.
The access panels are bolted.
Standard attachment is by aluminum alloy rivets
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-55-00
Page 1
Config-1 Nov 01/08
CES
Movable Fairing
Figure 001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 401-499,
54-55-00
Page 2
Config-1 Feb 01/08
CES
Movable Fairing
Figure 001A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-55-00
Page 3
Config-1 Nov 01/08
CES
Movable Fairing
Figure 001B
EFF :
301-306, 54-55-00
Page 4
Config-1 Nov 01/07
CES
Movable Fairing
Figure 001C
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 401-403,
54-55-00
Page 5
Config-1 Feb 01/08
CES
Movable Fairing
Figure 001D
EFF :
301-306, 54-55-00
Page 6
Config-1 Nov 01/07
CES
AFT MOVABLE FAIRING - DESCRIPTION AND OPERATION
_______________________________________________
1. ___________
Description
(Ref. Fig. 001)
The movable fairing is hinged at RIB14 and linked to the flap by a rod
attached to the fairing by a serrated plate system.
The movable fairing is composed of:
- an inner structure made of stainless steel and titanium alloy.
- an outer skin made of carbon and honeycomb
- one access panel.
The access panels are bolted.
Standard attachment is made by aluminum alloy rivets.
R
EFF :
501-509, 511-526, 528-599, 54-55-00
Page 1
Config-2 Feb 01/10
CES
Movable Fairing
Figure 001
R
EFF :
501-509, 511-526, 528-599, 54-55-00
Page 2
Config-2 Feb 01/10
CES
AFT MOVABLE FAIRING - REMOVAL/INSTALLATION
__________________________________________
TASK 54-55-00-000-001
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 54-55-00
Page 401
May 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-55-00-941-050
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
EFF :
ALL 54-55-00
Page 402
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
401-499,
Subtask 54-55-00-040-050
(2) Set the flap/slat control lever to position 2 (Ref. TASK 27-50-00-
866-008).
Subtask 54-55-00-040-050-A
(2) Set the flap/slat control lever to position 2 (Ref. TASK 27-50-00-
866-008).
Subtask 54-55-00-010-050
C. Get Access
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-55-00
Page 403
Feb 01/10
511-526, 528-599,
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
Subtask 54-55-00-010-050-A
C. Get Access
4. Procedure
_________
Subtask 54-55-00-020-050
EFF :
ALL 54-55-00
Page 404
Feb 01/10
CES
Movable Fairing Assembly
Figure 401/TASK 54-55-00-991-001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 401-499,
54-55-00
Page 405
Feb 01/08
CES
Movable Fairing Assembly
Figure 401A/TASK 54-55-00-991-001-B
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-55-00
Page 406
Nov 01/08
CES
Movable Fairing Assembly
Figure 401B/TASK 54-55-00-991-001-A
R
EFF :
301-306, 54-55-00
Page 407
Nov 01/07
CES
Movable Fairing Assembly
Figure 401C/TASK 54-55-00-991-001-C
R
EFF :
501-509, 511-526, 528-599, 54-55-00
Page 408
Feb 01/10
CES
**ON A/C ALL
(1) Remove the nut (3) and the screw (9) and release the bonding lead
(8).
(2) Remove the screw (16) and release the bonding lead (17).
NOTE : The axle head is rectangular and thus it can touch the fairing
____
panel. Turn the axle head to help removal of the bolt.
(5) Remove the nut (5), the bolt (2) and the bush (4).
NOTE : The axle head is rectangular and thus it can touch the fairing
____
panel. Turn the axle head to help removal of the bolt.
(8) Remove the nuts (14), the hollow pins (11) and the bushes (15).
EFF :
ALL 54-55-00
Page 409
May 01/09
R
CES
TASK 54-55-00-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
EFF :
ALL 54-55-00
Page 410
Aug 01/09
CES
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-55-00
Page 411
Feb 01/10
CES
**ON A/C ALL
3. __________
Job Set-up
Subtask 54-55-00-860-050
(1) Make sure that the access platform and the warning notices are in
position.
(2) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-
00-481-041).
(3) Set the flap/slat control lever to position 0 (Ref. TASK 27-50-00-
866-009).
Subtask 54-55-00-860-050-A
(1) Make sure that the access platform and the warning notices are in
position.
(3) Set the flap/slat control lever to position 0 (Ref. TASK 27-50-00-
866-009).
EFF :
ALL 54-55-00
Page 412
Feb 01/10
CES
**ON A/C ALL
4. Procedure
_________
Subtask 54-55-00-420-050
(2) Install the bushes (15), the hollow pins (11) and the nuts (14).
(3) Torque the nuts (14) to between 1.5 and 1.8 m.daN (11.06 and 13.27
lbf.ft).
(4) Install the bolts (10) and the nuts (13) and tighten them.
(5) Safety the nuts (13) with the cotter pins (12).
(6) Install the bush (4), the bolt (2) and the nut (5).
(7) Torque the nut (5) to between 1.5 and 1.8 m.daN (11.06 and 13.27
lbf.ft).
EFF :
ALL 54-55-00
Page 413
Feb 01/10
CES
(8) Install the bolt (1) and the nut (6) and tighten it.
(9) Safety the nut (6) with the cotter pin (7).
(10) Put the bonding lead (17) in position, install the screw (16) and
tighten it.
(11) Put the bonding lead (8) in position, install the bolt (9) and the
nut (3) and tighten it.
NOTE : When you install the bolt (9), do an electrical bonding of the
____
bolt (Ref. TASK 20-28-00-912-004).
Subtask 54-55-00-820-050
(1) Make sure that the clearance J1 between the inner flap and the
movable fairing (19) of the pylon is 8 +3 -3 mm (0.3149 +0.1181 -
0.1181 in.).
NOTE : You must measure the clearance J1 on the inboard and outboard
____
sides of the movable fairing (19).
EFF :
ALL 54-55-00
Page 414
Feb 01/08
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
Subtask 54-55-00-820-050-A
(1) Make sure that the clearance J1 between the inner flap and the
movable fairing (19) of the pylon is 14 +4 -3 mm (0.5511 +0.1574 -
0.1181 in.).
NOTE : You must measure the clearance J1 on the inboard and outboard
____
sides of the movable fairing (19).
5. Close-up
________
Subtask 54-55-00-440-050
(2) Set the flap/slat control lever to position 1 (Ref. TASK 27-50-00-
866-008).
EFF :
ALL 54-55-00
Page 415
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-55-00-440-050-A
(2) Set the flap/slat control lever to position 1 (Ref. TASK 27-50-00-
866-008).
Subtask 54-55-00-410-050
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-55-00-410-050-A
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-55-00
Page 416
Feb 01/10
511-526, 528-599,
CES
(3) Remove the access platform(s).
R
EFF : 234-235, 239-249, 251-299, 307-399,
501-509, 511-526, 528-599,
54-55-00
Page 417
Feb 01/10
CES
AFT MOVABLE FAIRING - INSPECTION/CHECK
______________________________________
TASK 54-55-00-200-001
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 54-55-00
Page 601
May 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-55-00-941-051
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1 (2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF :
ALL 54-55-00
Page 602
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1 (2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2)
Subtask 54-55-00-040-051
Subtask 54-55-00-040-051-A
Subtask 54-55-00-941-052
C. Get Access
Subtask 54-55-00-020-051
D. Removal of Component
EFF :
ALL 54-55-00
Page 603
Feb 01/10
CES
4. Procedure
_________
Subtask 54-55-00-220-050
EFF :
ALL 54-55-00
Page 604
Feb 01/10
CES
Forward Attach Fitting of the Aft Movable Fairing
Figure 601/TASK 54-55-00-991-002
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-55-00
Page 605
Feb 01/08
CES
Forward Attach Fitting of the Aft Movable Fairing
Figure 601A/TASK 54-55-00-991-002-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-55-00
Page 606
Nov 01/08
CES
Forward Attach Fitting of the Aft Movable Fairing
Figure 601B/TASK 54-55-00-991-002-B
R
EFF :
501-509, 511-526, 528-599, 54-55-00
Page 607
Feb 01/10
CES
Aft Attach Fitting of the Aft Movable Fairing
Figure 602/TASK 54-55-00-991-003
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499, 501-509,
54-55-00
Page 608
Feb 01/10
511-526, 528-599,
CES
Aft Attach Fitting of the Aft Movable Fairing
Figure 602A/TASK 54-55-00-991-003-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-55-00
Page 609
Nov 01/08
CES
R **ON A/C 501-509, 511-526, 528-599,
(1) Measure these dimensions of the aft movable fairing and make sure
that they are correct.
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| B | 0.2666 | 0.2672 | | | 0.2654 | | |
| OD 1 | (6.771) | (6.786) | | | (6.741) | | |
| | | | 0.0005 | 0.0025 | | | 0.0050|
| | | | (0.012) | (0.063) | | |(0.126) |
| B | 0.2677 | 0.2691 | | | | 0.2704 | |
| ID 2 | (6.799) | (6.835) | | | | (6.868) | |
-------------------------------------------------------------------------------
Subtask 54-55-00-220-059
EFF :
ALL 54-55-00
Page 610
Feb 01/10
CES
**ON A/C ALL
(1) Measure these dimensions of the aft movable fairing and make sure
that they are correct.
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| B | 0.2666 | 0.2672 | | | 0.2654 | | |
| OD 13 | (6.771) | (6.786) | | | (6.741) | | |
| | | | 0.0005 | 0.0025 | | | 0.0050|
| | | | (0.012) | (0.063) | | |(0.126) |
| B | 0.2677 | 0.2691 | | | | 0.2704 | |
| ID 14 | (6.799) | (6.835) | | | | (6.868) | |
-------------------------------------------------------------------------------
Subtask 54-55-00-220-052
(1) Measure these dimensions of the aft movable fairing and make sure
that they are correct.
EFF :
ALL 54-55-00
Page 611
Feb 01/10
CES
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| B | 0.4364 | 0.4369 | | | 0.4348 | | |
| OD 2 |(11.084) |(11.097) | | |(11.043) | | |
| | | | 0.0021 | 0.0033 | | | 0.0065|
| | | | (0.053) | (0.083) | | |(0.165) |
| D | 0.4390 | 0.4397 | | | | 0.4413 | |
| ID 3 |(11.150) |(11.168) | | | |(11.209) | |
-------------------------------------------------------------------------------
Subtask 54-55-00-220-053
(1) Measure these dimensions of the aft movable fairing and make sure
that they are correct.
EFF :
ALL 54-55-00
Page 612
Feb 01/10
CES
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| B | 0.4364 | 0.4369 | | | 0.4343 | | |
| OD 2 |(11.084) |(11.097) | | |(11.031) | | |
| | | | 0.0021 | 0.0043 | | | 0.0085|
| | | | (0.053) | (0.109) | | |(0.215) |
| C,D | 0.4390 | 0.4407 | | | | 0.4428 | |
| ID 4 |(11.150) |(11.193) | | | |(11.247) | |
-------------------------------------------------------------------------------
Subtask 54-55-00-220-060
(1) Measure these dimensions of the aft movable fairing and make sure
that they are correct.
EFF :
ALL 54-55-00
Page 613
Feb 01/10
CES
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| B | 0.4364 | 0.4369 | | | 0.4343 | | |
| OD 14 |(11.084) |(11.097) | | |(11.031) | | |
| | | | 0.0021 | 0.0043 | | | 0.0085|
| | | | (0.053) | (0.109) | | |(0.215) |
| C,D | 0.4390 | 0.4407 | | | | 0.4428 | |
| ID 4 |(11.150) |(11.193) | | | |(11.247) | |
-------------------------------------------------------------------------------
Subtask 54-55-00-220-054
(1) Measure these dimensions of the aft movable fairing and make sure
that they are correct.
EFF :
ALL 54-55-00
Page 614
Feb 01/10
CES
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| C,D | 0.5505 | 0.5509 | | | 0.5498 | | |
| OD 4 |(13.982) |(13.992) | | |(13.964) | | |
| | | | 0.0003 | 0.0014 | | | 0.0028|
| | | | (0.007) | (0.035) | | |(0.071) |
| C,D | 0.5512 | 0.5519 | | | | 0.5526 | |
| ID 5 |(14.000) |(14.018) | | | |(14.036) | |
-------------------------------------------------------------------------------
Subtask 54-55-00-220-051
(1) Measure these dimensions of the aft movable fairing and make sure
that they are correct.
EFF :
ALL 54-55-00
Page 615
Feb 01/10
CES
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| E | 0.2666 | 0.2672 | | | 0.2654 | | |
| OD 6 | (6.771) | (6.786) | | | (6.741) | | |
| | | | 0.0005 | 0.0025 | | | 0.0050|
| | | | (0.012) | (0.063) | | |(0.126) |
| E | 0.2677 | 0.2691 | | | | 0.2704 | |
| ID 7 | (6.799) | (6.835) | | | | (6.868) | |
-------------------------------------------------------------------------------
Subtask 54-55-00-220-055
(1) Measure these dimensions of the aft movable fairing and make sure
that they are correct.
EFF :
ALL 54-55-00
Page 616
Feb 01/10
CES
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| E | 0.4376 | 0.4383 | | | 0.4363 | | |
| OD 7 |(11.115) |(11.132) | | |(11.082) | | |
| | | | 0.0007 | 0.0031 | | | 0.0059|
| | | | (0.017) | (0.078) | | |(0.149) |
| E | 0.4390 | 0.4407 | | | | 0.4422 | |
| ID 8 |(11.150) |(11.193) | | | |(11.231) | |
-------------------------------------------------------------------------------
Subtask 54-55-00-220-056
(1) Measure these dimensions of the aft movable fairing and make sure
that they are correct.
EFF :
ALL 54-55-00
Page 617
Feb 01/10
CES
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| F | 0.2666 | 0.2672 | | | 0.2654 | | |
| OD 9 | (6.771) | (6.786) | | | (6.741) | | |
| | | | 0.0005 | 0.0025 | | | 0.0050|
| | | | (0.012) | (0.063) | | |(0.126) |
| F | 0.2677 | 0.2691 | | | | 0.2704 | |
| ID 10 | (6.799) | (6.835) | | | | (6.868) | |
-------------------------------------------------------------------------------
Subtask 54-55-00-220-057
(1) Measure these dimensions of the aft movable fairing and make sure
that they are correct.
EFF :
ALL 54-55-00
Page 618
Feb 01/10
CES
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| F | 0.4364 | 0.4369 | | | 0.4348 | | |
| OD 10 |(11.084) |(11.097) | | |(11.043) | | |
| | | | 0.0021 | 0.0033 | | | 0.0065|
| | | | (0.053) | (0.083) | | |(0.165) |
| F | 0.4390 | 0.4397 | | | | 0.4413 | |
| ID 12 |(11.150) |(11.168) | | | |(11.209) | |
-------------------------------------------------------------------------------
Subtask 54-55-00-220-058
(1) Measure these dimensions of the aft movable fairing and make sure
that they are correct.
EFF :
ALL 54-55-00
Page 619
Feb 01/10
CES
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| F | 0.4364 | 0.4369 | | | 0.4348 | | |
| OD 10 |(11.084) |(11.097) | | |(11.043) | | |
| | | | 0.0021 | 0.0033 | | | 0.0065|
| | | | (0.053) | (0.083) | | |(0.165) |
| F | 0.4390 | 0.4397 | | | | 0.4413 | |
| ID 11 |(11.150) |(11.168) | | | |(11.209) | |
-------------------------------------------------------------------------------
5. Close-up
________
Subtask 54-55-00-420-051
A. Installation of Component
Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-55-00-440-051
Subtask 54-55-00-440-051-A
EFF :
ALL 54-55-00
Page 620
Feb 01/10
CES
R **ON A/C ALL
Subtask 54-55-00-942-051
C. Close Access
EFF :
ALL 54-55-00
Page 621
Nov 01/07
CES
SEAL - AFT MOVABLE FAIRING - REMOVAL/INSTALLATION
_________________________________________________
TASK 54-55-41-000-001
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 54-55-41
Page 401
May 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-55-41-941-050
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
EFF :
ALL 54-55-41
Page 402
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
401-499,
Subtask 54-55-41-860-051
(2) Set the flap/slat control lever to position FULL (Ref. TASK 27-50-00-
866-008).
Subtask 54-55-41-860-051-A
(2) Set the flap/slat control lever to position FULL (Ref. TASK 27-50-00-
866-008).
Subtask 54-55-41-010-050
C. Get Access
EFF :
ALL 54-55-41
Page 403
Feb 01/10
CES
4. Procedure
_________
Subtask 54-55-41-020-050
(1) Remove and discard the seals (1), (5) and (8) from the retainers.
Subtask 54-55-41-020-050-A
(1) Remove the screws (1) and (6) from the retainers (3), (4) and (8).
(2) Remove and discard the seals (2), (5) and (7).
EFF :
ALL 54-55-41
Page 404
Feb 01/10
CES
Aft Movable-Fairing Seals
Figure 401/TASK 54-55-41-991-001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-55-41
Page 405
Feb 01/08
CES
Aft Movable-Fairing Seals
Figure 401A/TASK 54-55-41-991-001-B
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-55-41
Page 406
Nov 01/08
CES
Aft Movable-Fairing Seals
Figure 401B/TASK 54-55-41-991-001-C
R
EFF :
501-509, 511-526, 528-599, 54-55-41
Page 407
Feb 01/10
CES
Aft Movable-Fairing Seals
Figure 401C/TASK 54-55-41-991-001-A
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-403,
54-55-41
Page 408
Feb 01/08
CES
**ON A/C ALL
TASK 54-55-41-400-001
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
Self Explanatory
2. ______________________
Job Set-up Information
A. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-55-41
Page 409
Nov 01/07
R
CES
B. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
EFF :
ALL 54-55-41
Page 410
Aug 01/09
CES
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-55-41
Page 411
Feb 01/10
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-55-41-860-050
(3) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-
00-481-041).
(4) Make sure that the flap/slat control lever is in the FULL position
(Ref. TASK 27-50-00-866-008).
EFF :
ALL 54-55-41
Page 412
Nov 01/09
R
CES
(5) Make sure that the following access panels are removed:
Subtask 54-55-41-860-050-A
(3) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-
00-040-012).
(4) Make sure that the flap/slat control lever is in the FULL position
(Ref. TASK 27-50-00-866-008).
(5) Make sure that the following access panels are removed:
Subtask 54-55-41-420-051
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-55-41
Page 413
Feb 01/10
511-526, 528-599,
CES
Aft Movable-Fairing Seals - Installation of the Clips
Figure 402/TASK 54-55-41-991-002
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-55-41
Page 414
Aug 01/09
CES
Aft Movable-Fairing Seals - Installation of the Clips
Figure 402A/TASK 54-55-41-991-002-A
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-403,
54-55-41
Page 415
Aug 01/09
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
401-499,
NOTE : This procedure is applicable for the aft movable fairing on which
____
the clips are not installed.
(1) Install the clips at the end of each seal retainer with two rivets
R (Ref. ASRM 51400000).
1
_ For the seal (2), install the clip (3) and the clip (1).
2
_ For the seal (8), install the clip (9) and the clip (7).
3
_ For the seal (5), install the clip (6) and the clip (4)
1
_ For the seal (2), install the clip (3) and the clip (1).
2
_ For the seal (8), install the clip (9) and the clip (7).
3
_ For the seal (5), install the clip (6) and the clip (4).
(2) Put the new rivets through the retainer and the clip.
(4) Make sure that the rivets are flush with the surface of the retainer.
(5) Drill a 3.6 mm (0.1417 in.) dia. hole on the retainer for the seal
pin.
Subtask 54-55-41-110-050
EFF :
ALL 54-55-41
Page 416
Nov 01/09
CES
**ON A/C 234-235, 239-249, 251-299, 307-399,
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) Degrease the surface of the retainers that touches the seals with
CLEANING AGENTS (Material No. 11-003).
(a) Remove the talcum powder from the surface of the seals with hot
water and washing powder.
EFF :
ALL 54-55-41
Page 417
Feb 01/10
CES
(3) Make the surface of the retainer rough with emery cloth, grade 120 to
240.
4. Procedure
_________
Subtask 54-55-41-420-050
NOTE : Be careful that you do not cause damage to the surface of the
____
retainer.
(1) Apply on the contact surfaces of the seal and the retainer :
(a) BONDING AND ADHESIVE COMPOUNDS (Material No. 08-018) for the
seals with P/N D54530240220, P/N D54530240221 and
P/N D54530240222.
(b) BONDING AND ADHESIVE COMPOUNDS (Material No. 08-004) for the
seals with P/N D54530240224, P/N D54530240225 and
P/N D54530240222.
(2) If necessary, bend the clip lightly to engage the end of the seal
under the clip.
EFF :
ALL 54-55-41
Page 418
Aug 01/09
R
CES
R **ON A/C 234-235, 239-249, 251-299, 307-399, 501-509, 511-526, 528-599,
Subtask 54-55-41-420-050-A
(1) Apply the BONDING AND ADHESIVE COMPOUNDS (Material No. 08-018) on the
contact surfaces of the seal and the retainer.
(2) Install the seals (2), (5) and (7), the retainers (3), (4) and (8)
and the
Subtask 54-55-41-220-050
B. Inspection.
(1) Make sure that the clip holds the seal tightly.
(2) Make sure that the seal is in the correct position on the retainer.
(3) Make sure that the seal pins are perpendicular to the face of the
retainer.
EFF :
ALL 54-55-41
Page 419
Feb 01/10
CES
5. Close-up
________
Subtask 54-55-41-410-051
A. Close Access
Subtask 54-55-41-440-051
(2) Set the flap/slat control lever to position 1 (Ref. TASK 27-50-00-
866-008).
Subtask 54-55-41-440-051-A
(2) Set the flap/slat control lever to position 1 (Ref. TASK 27-50-00-
866-008).
Subtask 54-55-41-942-051
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-55-41
Page 420
Feb 01/10
CES
(3) Remove the warning notice(s).
EFF :
ALL 54-55-41
Page 421
Aug 01/09
R
CES
LOWER FAIRING - DESCRIPTION AND OPERATION
_________________________________________
1. Description
___________
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 1
Config-1 Nov 01/08
CES
Lower Fairing
Figure 001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-56-00
Page 2
Config-1 Feb 01/08
CES
Lower Fairing
Figure 001A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-56-00
Page 3
Config-1 Nov 01/08
CES
LOWER FAIRING - DESCRIPTION AND OPERATION
_________________________________________
1. ___________
Description
(Ref. Fig. 001)
The lower fairing is composed of:
- Panels made of stainless steel
- The forward section of the lower fairing is secured to the pylon througt
two 2 spigots at the front attach fitting and by four bolts under the
pylon rear attach fitting.
R 1. ___________
Description
R (Ref. Fig. 001A)
R The lower fairing is composed of:
R - Panels made of stainless steel
R - Deflectors made of stainless steel, fixed on the aft lower fairing in
R order to deviate the engine exhaust gas
R - The forward section of the lower fairing is secured to the pylon through
R two spigots at the front attach fitting and by four bolts under the pylon
R rear attach fitting.
R
EFF :
501-509, 511-526, 528-599, 54-56-00
Page 1
Config-2 Feb 01/10
CES
Lower Fairing
Figure 001
R
EFF :
501-507, 54-56-00
Page 2
Config-2 Feb 01/10
CES
R Lower Fairing
R Figure 001A
EFF :
508-509, 511-526, 528-599, 54-56-00
Page 3
Config-2 Feb 01/10
CES
LOWER FAIRING - REMOVAL/INSTALLATION
____________________________________
TASK 54-56-00-000-001
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 54-56-00
Page 401
Nov 01/08
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-56-00-941-050
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-56-00-040-056
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 402
Nov 01/08
CES
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
R 401-499,
Subtask 54-56-00-010-050
C. Get Access
R Subtask 54-56-00-010-050-A
R C. Get Access
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 403
Aug 01/09
CES
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
R 401-499,
4. Procedure
_________
Subtask 54-56-00-020-050
(2) Disengage the centering pin and remove the Forward lower fairing (3):
Subtask 54-56-00-020-051
(1) Remove the screws (11), the washers (12) and the screw supports (13).
(2) Disengage the centering pin and remove the aft lower fairing (21):
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 404
Aug 01/09
CES
Forward Lower Fairing
Figure 401/TASK 54-56-00-991-001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-56-00
Page 405
Aug 01/09
CES
Forward Lower Fairing
Figure 401A/TASK 54-56-00-991-001-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-56-00
Page 406
Aug 01/09
CES
INTENTIONALLY BLANK
R
54-56-00
Page 407
Nov 01/07
CES
Aft Lower Fairing.
Figure 402/TASK 54-56-00-991-002- 12 (SHEET 1)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 408
Nov 01/08
CES
Aft Lower Fairing.
Figure 402/TASK 54-56-00-991-002- 22 (SHEET 2)
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 409
Nov 01/08
CES
Subtask 54-56-00-020-052
(2) Disengage the centering pin and remove the center lower fairing (33):
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 410
Aug 01/09
R
CES
Center Lower Fairing
Figure 403/TASK 54-56-00-991-003
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 411
Aug 01/09
R
CES
TASK 54-56-00-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 412
Aug 01/09
R
CES
3. __________
Job Set-up
Subtask 54-56-00-860-057
(1) Make sure that the access platform and the warning notices are in
position
4. Procedure
_________
Subtask 54-56-00-420-050
(1) Put the centering pins in position and install the center lower
fairing (33):
(2) Install the bolts (32), the nuts (31) and tighten them.
Subtask 54-56-00-420-051
(1) Put the centering pin in position in the rear face of the center
fairing and install the aft lower fairing (21):.
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 413
Aug 01/09
R
CES
Subtask 54-56-00-820-050
(b) If the values of the clearances you measured are not correct you
can:
- remove the screw (18), the washers (17) and adjust with the
shims (19)
- or remove the nut (14) and the bolt (16) and adjust with the
shims (15).
NOTE : Install the bolts (16) and the nuts (14) in the fitting
____
for all the adjustement procedures.
(c) Make sure that the thickness of the parts that the screws (11)
tighten is be constant in all the adjustment procedures.
(3) Install the screw supports (13) and the screws (11) with washers
(12).
(4) TORQUE the screws (11) to between 1.6 and 1.8 m.daN (11.79 and 13.27
lbf.ft).
Subtask 54-56-00-420-052
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 414
Aug 01/09
R
CES
**ON A/C 234-235, 239-249, 251-299, 307-399,
(1) Put the centering pins in position and install the forwaed lower
fairing (3):
(2) Install the washers (1), the screws (2) and tighten.
Subtask 54-56-00-220-052
E. Check of Clearance
(Ref. Fig. 402/TASK 54-56-00-991-002)
5. Close-up
________
Subtask 54-56-00-869-051
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 415
Aug 01/09
R
CES
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-233, 236-238, 301-306,
R 401-499,
Subtask 54-56-00-410-050
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R Subtask 54-56-00-410-050-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
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 416
Aug 01/09
CES
R **ON A/C 501-509, 511-526, 528-599,
TASK 54-56-00-000-002
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.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
501-509, 511-526, 528-599, 54-56-00
Page 417
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
3. __________
Job Set-up
Subtask 54-56-00-941-053
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-56-00-040-057
Subtask 54-56-00-010-052
C. Get Access
R
EFF :
501-509, 511-526, 528-599, 54-56-00
Page 418
Feb 01/10
CES
4. Procedure
_________
Subtask 54-56-00-020-053
(2) Release the centering pins and remove the lower fairing (9):
R
EFF :
501-509, 511-526, 528-599, 54-56-00
Page 419
Feb 01/10
CES
Lower Fairing
Figure 404/TASK 54-56-00-991-005- 12 (SHEET 1)
R
EFF :
501-507, 54-56-00
Page 420
Feb 01/10
CES
Lower Fairing
Figure 404/TASK 54-56-00-991-005- 22 (SHEET 2)
R
EFF :
501-507, 54-56-00
Page 421
Feb 01/10
CES
R Lower Fairing
R Figure 404A/TASK 54-56-00-991-005-A12 (SHEET 1)
R
EFF :
508-509, 511-526, 528-599, 54-56-00
Page 422
Feb 01/10
CES
R Lower Fairing
R Figure 404A/TASK 54-56-00-991-005-A22 (SHEET 2)
R
EFF :
508-509, 511-526, 528-599, 54-56-00
Page 423
Feb 01/10
CES
TASK 54-56-00-400-002
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
501-509, 511-526, 528-599, 54-56-00
Page 424
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
3. __________
Job Set-up
Subtask 54-56-00-860-058
(1) Make sure that the access platform and the warning notices are in
position
Subtask 54-56-00-200-050
(1) Do an inspection of the pylon aft fixed fairing (Ref. TASK 54-54-00-
200-002).
4. Procedure
_________
Subtask 54-56-00-420-053
(1) Install the centering pins and install the lower fairing (9):
R
EFF :
501-509, 511-526, 528-599, 54-56-00
Page 425
Feb 01/10
CES
Subtask 54-56-00-820-051
(3) If the values of the clearances you measured are not correct you can:
- remove the bolt (6), the washer (2) and adjust with the shims (7)
- or remove the nuts (1), the nut holders (3), the bolts (5) and
adjust with the shims (4).
NOTE : For all adjustment procedure you must install the bolts (5),
____
the nuts (1) and the nut holders (3) on the fitting.
(4) Install the bolts (8) and TORQUE to between 1.6 and 1.8 m.daN (11.79
and 13.27 lbf.ft).
5. Close-up
________
Subtask 54-56-00-440-058
R
EFF :
501-509, 511-526, 528-599, 54-56-00
Page 426
Feb 01/10
CES
Subtask 54-56-00-942-053
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
501-509, 511-526, 528-599, 54-56-00
Page 427
Feb 01/10
CES
**ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
401-499,
TASK 54-56-00-000-003
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 54-56-00-941-056
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 428
Feb 01/10
R
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-56-00-040-058
Subtask 54-56-00-010-053
C. Get Access
4. Procedure
_________
Subtask 54-56-00-020-055
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 429
Feb 01/10
R
CES
Bottom Lower Fairing
Figure 405/TASK 54-56-00-991-009- 12 (SHEET 1)
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 430
Feb 01/10
R
CES
Bottom Lower Fairing
Figure 405/TASK 54-56-00-991-009- 22 (SHEET 2)
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 431
Feb 01/10
R
CES
TASK 54-56-00-400-003
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-56-00-860-059
(1) Make sure that the access platform and the warning notices are in
position
4. Procedure
_________
Subtask 54-56-00-420-055
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 432
Feb 01/10
CES
Subtask 54-56-00-820-052
(2) Measure the out-of-flush dimensions A1 and A2 between the aft lower
fairing and the bottom lower fairing.
- A1 = 0 +1 -1 mm (0.0000 +0.0393 -0.0393 in.)
- A2 = 0 +1.5 -1.5 mm (0.0000 +0.0590 -0.0590 in.)
5. Close-up
________
Subtask 54-56-00-869-061
Subtask 54-56-00-410-052
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 433
Feb 01/10
CES
LOWER FAIRING - INSPECTION/CHECK
________________________________
TASK 54-56-00-200-001
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 54-56-00
Page 601
Aug 01/09
CES
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
R 401-499,
3. __________
Job Set-up
Subtask 54-56-00-941-051
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine
1(2).
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-56-00-941-052
B. Get Access
Subtask 54-56-00-010-051
C. Removal of Component
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 602
Aug 01/09
CES
4. Procedure
_________
Subtask 54-56-00-220-050-A
(2) Make sure that the dimensions of the pins are correct.
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| A | 0.3728 | 0.3748 | | | 0.3718 | | |
| OD 1 | (9.469) | (9.519) | | | (9.443) | | |
| | | | 0.0000 | 0.0021 | | | 0.0041|
| | | | (0.000) | (0.053) | | |(0.104) |
| A | 0.3748 | 0.3749 | | | | 0.3759 | |
| ID 2 | (9.519) | (9.522) | | | | (9.547) | |
-------------------------------------------------------------------------------
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 603
Aug 01/09
CES
Lower Fairing Inspection.
Figure 601/TASK 54-56-00-991-004
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-56-00
Page 604
Aug 01/09
CES
R Lower Fairing Inspection
R Figure 601A/TASK 54-56-00-991-004-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-56-00
Page 605
Aug 01/09
CES
5. Close-up
________
Subtask 54-56-00-410-051
A. Installation of Components
Subtask 54-56-00-942-051
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-56-00
Page 606
Aug 01/09
CES
R **ON A/C 501-509, 511-526, 528-599,
TASK 54-56-00-200-002
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.
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R
EFF :
501-509, 511-526, 528-599, 54-56-00
Page 607
Feb 01/10
CES
R **ON A/C 501-509, 511-526, 528-599,
3. __________
Job Set-up
Subtask 54-56-00-941-054
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine
1(2).
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-56-00-941-055
B. Get Access
Subtask 54-56-00-020-054
C. Removal of component
R
EFF :
501-509, 511-526, 528-599, 54-56-00
Page 608
Feb 01/10
CES
4. Procedure
_________
Subtask 54-56-00-220-053
(2) Make sure that the dimensions of the pin are correct.
-------------------------------------------------------------------------------
| FIG. | ORIGINAL MANUFACTURING LIMITS | IN-SERVICE WEAR LIMITS |
| DETAIL |---------------------------------------|----------------------------|
| AND | DIMENSION | ASSEMBLY CLEARANCE| DIMENSION LIMITS | MAX. |
| ITEM | IN. (MM) | IN. (MM) | IN. (MM) | ALLOW. |
| NO. |-------------------|-------------------|---------|---------| CLEAR. |
| | MIN. | MAX. | MIN. | MAX. | MIN. | MAX. |IN. (MM)|
|--------|---------|---------|---------|---------|---------|---------|--------|
| A | 0.3098 | 0.3118 | | | 0.3090 | | |
| OD 1 | (7.868) | (7.919) | | | (7.848) | | |
| | | | 0.0002 | 0.0027 | | | 0.0052|
| | | | (0.005) | (0.068) | | |(0.132) |
| A | 0.3120 | 0.3125 | | | | 0.3142 | |
| ID 2 | (7.924) | (7.937) | | | | (7.980) | |
-------------------------------------------------------------------------------
5. Close-up
________
Subtask 54-56-00-420-054
R
EFF :
501-509, 511-526, 528-599, 54-56-00
Page 609
Feb 01/10
CES
Lower Fairing Inspection
Figure 602/TASK 54-56-00-991-006
R
EFF :
501-507, 54-56-00
Page 610
Feb 01/10
CES
R Lower Fairing Inspection
R Figure 602A/TASK 54-56-00-991-006-A
EFF :
508-509, 511-526, 528-599, 54-56-00
Page 611
Feb 01/10
CES
Subtask 54-56-00-942-054
B. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
501-509, 511-526, 528-599, 54-56-00
Page 612
Feb 01/10
CES
PYLON-TO-NACELLE JUNCTION - DESCRIPTION AND OPERATION
_____________________________________________________
1. Description
___________
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-57-00
Page 1
Config-1 Nov 01/08
CES
Pylon-to-Nacelle Junction
Figure 001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-57-00
Page 2
Config-1 Feb 01/08
CES
Pylon-to-Nacelle Junction
Figure 001A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-57-00
Page 3
Config-1 Nov 01/08
CES
Engine Cowl Hinge Fittings
Figure 002
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-57-00
Page 4
Config-1 Nov 01/08
CES
PYLON-TO-NACELLE JUNCTION - DESCRIPTION AND OPERATION
_____________________________________________________
1. ___________
Description
(Ref. Fig. 001, 002)
The pylon-to-nacelle junction is made of:
- two aprons
- a front radial firewall
- two reverse cowl fire seals
- one forward junction fairing with three cut-outs
- one rear junction fairing with one cut-out
These junction items are made of titanium.
Monel rivets and corrosion-resistant steel bolts are used for attachment.
R
EFF :
501-509, 511-526, 528-599, 54-57-00
Page 1
Config-2 Feb 01/10
CES
Pylon-to-Nacelle Junction
Figure 001
R
EFF :
501-509, 511-526, 528-599, 54-57-00
Page 2
Config-2 Feb 01/10
CES
Engine Cowl Hinge Fittings
Figure 002
R
EFF :
501-509, 511-526, 528-599, 54-57-00
Page 3
Config-2 Feb 01/10
CES
FITTINGS - REMOVAL/INSTALLATION
_______________________________
TASK 54-57-17-000-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-57-17
Page 401
May 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-57-17-941-050
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-57-17-010-050
B. Get Access
EFF :
ALL 54-57-17
Page 402
Feb 01/10
CES
(2) Open the thrust reverser doors (Ref. TASK 78-36-00-010-040)
FOR 1000EM1
451AL, 452AR
FOR 1000EM2
461AL, 462AR.
Subtask 54-57-17-040-050
Subtask 54-57-17-010-050-A
B. Get Access
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-57-17
Page 403
Feb 01/10
511-526, 528-599,
CES
Subtask 54-57-17-040-050-A
4. Procedure
_________
Subtask 54-57-17-020-050
(a) Remove the nut (7) and the bolt (9) to disconnect the tube end
(8) from the fitting (6).
(b) Remove the nut (1), the bolt (4), the washer (3), the stirrup (2)
and disconnect the cowl stop assembly (5).
(c) Remove the nuts (21), the washers (20) and the bolts (22) that
attach the fitting (6) to the bracket (23).
CAUTION : DO NOT REMOVE THE BOLTS WHICH ATTACH THE FITTING TO THE
_______
FWD PYLON-TO-ENGINE ATTACH FITTING. REMOVE THE NUTS
ONLY.
- IF YOU REMOVE THE BOLTS, YOU CAN CAUSE DAMAGE TO THE
BORES.
EFF :
ALL 54-57-17
Page 404
Nov 01/08
CES
Fitting at RIB1
Figure 401/TASK 54-57-17-991-001
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-233, 236-238, 301-306, 401-499,
54-57-17
Page 405
Feb 01/08
CES
Fitting at RIB1
Figure 401A/TASK 54-57-17-991-001-A
R
EFF :
234-235, 239-249, 251-299, 307-399, 54-57-17
Page 406
Nov 01/08
CES
(d) Remove the nuts (10) and the fitting (6).
(a) Remove the nut (15) and the bolt (13) to disconnect the tube end
(14) from the fitting (12).
(b) Remove the nut (16), the bolt (19), the washer (18), the stirrup
(17) and disconnect the cowl stop assembly (5).
(c) Remove the nuts (26), the washers (25) and the bolts (24) that
attach the fitting (12) to the bracket (23).
CAUTION : DO NOT REMOVE THE BOLTS WHICH ATTACH THE FITTING TO THE
_______
FWD PYLON-TO-ENGINE ATTACH FITTING. REMOVE THE NUTS
ONLY.
- IF YOU REMOVE THE BOLTS, YOU CAN CAUSE DAMAGE TO THE
BORES.
Subtask 54-57-17-020-050-A
(a) Remove the nut (6) and the bolt (8) to disconnect the tube end
(7) from the fitting (5).
(b) Remove the nut (1), the bolt (4), the washer (3) and the bracket
(2).
CAUTION : DO NOT REMOVE THE BOLTS WHICH ATTACH THE FITTING TO THE
_______
FWD PYLON-TO-ENGINE ATTACH FITTING. REMOVE THE NUTS
ONLY.
- IF YOU REMOVE THE BOLTS, YOU CAN CAUSE DAMAGE TO THE
BORES.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-57-17
Page 407
Feb 01/10
511-526, 528-599,
CES
Fitting at RIB1
Figure 401B/TASK 54-57-17-991-001-B
R
EFF :
501-509, 511-526, 528-599, 54-57-17
Page 408
Feb 01/10
CES
(2) Remove the fitting (11).
(a) Remove the nut (14) and the bolt (12) to disconnect the tube end
(13) from the fitting (11).
(b) Remove the nut (16), the bolt (18), the washer (17) and the
bracket (15).
CAUTION : DO NOT REMOVE THE BOLTS WHICH ATTACH THE FITTING TO THE
_______
FWD PYLON-TO-ENGINE ATTACH FITTING. REMOVE THE NUTS
ONLY.
- IF YOU REMOVE THE BOLTS, YOU CAN CAUSE DAMAGE TO THE
BORES.
R
EFF :
501-509, 511-526, 528-599, 54-57-17
Page 409
Feb 01/10
CES
**ON A/C ALL
TASK 54-57-17-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF :
ALL 54-57-17
Page 410
May 01/09
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-57-17-860-050
(3) Make sure that the thrust reversers are unserviceable (Ref. TASK 78-
30-00-481-041).
Subtask 54-57-17-860-050-A
(3) Make sure that the thrust reversers are unserviceable (Ref. TASK 78-
30-00-040-012).
EFF :
ALL 54-57-17
Page 411
Feb 01/10
CES
**ON A/C ALL
4. Procedure
_________
Subtask 54-57-17-420-050
(a) Put the fitting (6) in position and install the nuts (10).
(b) Install the bolts (22), the washers (20) and the nuts (21) to
attach the fitting (6) to the bracket (23).
(d) Install the stirrup (2), the bolt (4), the washer (3) and the nut
(1).
(e) Install the bolt (9) and the nut (7) to connect the tube end (8)
to the fitting (6).
(g) TORQUE the nuts (10) to between 14 and 16 m.daN (103.24 and
117.99 lbf.ft).
EFF :
ALL 54-57-17
Page 412
Nov 01/08
CES
(2) Install the fitting (12).
(a) Put the fitting (12) in position and install the nuts (11).
(b) Install the bolts (24), the washers (25) and the nuts (26) to
attach the fitting (12) to the bracket (23).
(d) Install the stirrup (17), the bolt (19), the washer (18) and the
nut (16).
(e) Install the bolt (13) and the nut (15) to connect the tube end
(14) to the fitting (12).
(g) TORQUE the nuts (11) to between 14 and 16 m.daN (103.24 and
117.99 lbf.ft).
Subtask 54-57-17-420-050-A
(a) Put the fitting (5) in position and install the nuts (9).
(b) Install the bracket (2), the bolt (4), the washer (3) and the nut
(1).
(c) Install the bolt (8) and the nut (6) to connect the tube end (7)
to the fitting (5).
(e) TORQUE the nuts (9) to between 14 and 16 m.daN (103.24 and 117.99
lbf.ft).
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-57-17
Page 413
Feb 01/10
511-526, 528-599,
CES
(2) Install the fitting (11).
(a) Put the fitting (11) in position and install the nuts (10).
(b) Install the bracket (15), the bolt (18), the washer (17) and the
nut (16).
(c) Install the bolt (12) and the nut (14) to connect the tube end
(13) to the fitting (11).
(e) TORQUE the nuts (10) to between 14 and 16 m.daN (103.24 and
117.99 lbf.ft).
5. Close-up
________
Subtask 54-57-17-440-050
Subtask 54-57-17-410-050
B. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-57-17
Page 414
Nov 01/08
CES
(4) Remove the access platform(s).
Subtask 54-57-17-440-050-A
Subtask 54-57-17-410-050-A
B. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-57-17
Page 415
Feb 01/10
511-526, 528-599,
CES
TASK 54-57-17-000-002
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 54-57-17-941-051
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
R
EFF :
501-509, 511-526, 528-599, 54-57-17
Page 416
Feb 01/10
CES
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-57-17-020-051
B. Removal of Components
Subtask 54-57-17-010-051
C. Get Access
R
EFF :
501-509, 511-526, 528-599, 54-57-17
Page 417
Feb 01/10
CES
4. Procedure
_________
Subtask 54-57-17-020-052
(4) Remove the thrust reverser cowl fitting (12), the fitting (13) and
the shim (14)
NOTE : Record the position of the shim (14) and the location and
____
thickness of the peel washers (17) installed on the shim (14).
Do this to put the shim (14) at the same position at the
installation.
R
EFF :
501-509, 511-526, 528-599, 54-57-17
Page 418
Feb 01/10
CES
Thrust Reverser Cowl Fitting at RIB3
Figure 402/TASK 54-57-17-991-002
R
EFF :
501-509, 511-526, 528-599, 54-57-17
Page 419
Feb 01/10
CES
TASK 54-57-17-400-002
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
A. Consumable Materials
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-57-17-860-051
(1) Make sure that the access platform and the warning notices are in
position.
R
EFF :
501-509, 511-526, 528-599, 54-57-17
Page 420
Feb 01/10
CES
4. Procedure
_________
Subtask 54-57-17-420-051
(1) Obey the location and thickness of the peel washers (17) recorded at
the removal.
(2) Put the shim (14) in the correct position on the pylon.
(3) Put the fitting (13) and the thrust reverser cowl fitting (12) in
position.
(5) Install the bolts (10) with SPECIAL MATERIALS (Material No. 05-047).
5. Close-up
________
Subtask 54-57-17-420-052
A. Installation of Components
Subtask 54-57-17-410-051
B. Close Access
R
EFF :
501-509, 511-526, 528-599, 54-57-17
Page 421
Feb 01/10
CES
(2) Remove the access platform(s).
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
501-509, 511-526, 528-599, 54-57-17
Page 422
Feb 01/10
CES
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-249, 251-299, 301-399,
R 401-499,
TASK 54-57-17-000-003
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 54-57-17-941-052
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-57-17
Page 423
Nov 01/08
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-57-17-020-053
B. Removal of Components
Subtask 54-57-17-010-052
C. Get Access
4. Procedure
_________
Subtask 54-57-17-020-054
(2) Remove the nuts (8) and (10) and the washers (7).
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-57-17
Page 424
Nov 01/08
CES
Thrust Reverser Cowl Fitting at RIB 1 and RIB 2
Figure 403/TASK 54-57-17-991-003
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-57-17
Page 425
Nov 01/08
CES
(4) Remove the thrust-reverser cowl fitting (2) and the shim (5).
NOTE : Record the position of the shim (5) and the location and
____
thickness of the peel washers (9) installed on the shim (5).
Do this to put the shim (5) in the same position for the
installation.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-57-17
Page 426
Nov 01/08
CES
TASK 54-57-17-400-003
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
-------------------------------------------------------------------------------
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-57-17
Page 427
Feb 01/09
CES
3. __________
Job Set-up
Subtask 54-57-17-860-052
(1) Make sure that the access platform and the warning notices are in
position.
4. Procedure
_________
Subtask 54-57-17-420-053
(1) Obey the location and thickness of the peel washers (9) recorded at
the removal.
(2) Put the shim (5) in the correct position on the pylon.
(5) Install the bolts (3) with SPECIAL MATERIALS (Material No. 05-047).
(6) Install the washers (7), the nut (8) and the nut (10).
(7) TORQUE the nut (8) and the nut (10) (Ref. TASK 20-21-11-991-001).
5. Close-up
________
Subtask 54-57-17-420-054
A. Installation of Components
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-57-17
Page 428
Nov 01/08
CES
Subtask 54-57-17-410-052
B. Close Access
(4) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-57-17
Page 429
Nov 01/08
CES
SEALING - REMOVAL/INSTALLATION
______________________________
TASK 54-57-22-000-001
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 54-57-22
Page 401
Nov 01/08
CES
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-57-22-941-050
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-57-22-010-050
B. Get Access
EFF :
ALL 54-57-22
Page 402
Feb 01/10
CES
(2) Open the thrust reverser doors (Ref. TASK 78-36-00-010-040).
Subtask 54-57-22-010-050-A
B. Get Access
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499, 501-509,
54-57-22
Page 403
Feb 01/10
511-526, 528-599,
CES
**ON A/C ALL
4. Procedure
_________
Subtask 54-57-22-020-050
(b) Remove the seal and retainer assemblies (41) and (44).
(a) Remove the bolts (62) the washers (63), the aft apron assemblies
(51) and (64).
(d) Remove the brackets (56) and (61) from the forward aprons.
NOTE : Do the same procedure for the removal of the right pylon.
____
EFF :
ALL 54-57-22
Page 404
Nov 01/08
CES
Seal and Retainer Assembly
Figure 401/TASK 54-57-22-991-004
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-57-22
Page 405
Nov 01/08
CES
Apron Assembly
Figure 402/TASK 54-57-22-991-005
R
EFF : 001-049, 051-099, 101-149, 151-199,
201-249, 251-299, 301-399, 401-499,
54-57-22
Page 406
Nov 01/08
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-57-22-020-050-A
(2) Removal of the welded assemblies (12), (13), (18) and (19).
(Ref. Fig. 404/TASK 54-57-22-991-002)
(b) Remove the bolts (15), the nuts (16) and the washers (14).
(c) Remove the welded assemblies (12), (13), (18) and (19).
(e) Remove the washers (30) and (22) from the front apron assemblies
(21) and (32).
(f) Remove the front apron assemblies (21) and (32) from the
structure of the pylon.
R
EFF :
501-509, 511-526, 528-599, 54-57-22
Page 407
Feb 01/10
CES
Angle Assembly
Figure 403/TASK 54-57-22-991-001
R
EFF :
501-509, 511-526, 528-599, 54-57-22
Page 408
Feb 01/10
CES
Welded Assembly
Figure 404/TASK 54-57-22-991-002
R
EFF :
501-509, 511-526, 528-599, 54-57-22
Page 409
Feb 01/10
CES
Forward Apron Assembly
Figure 405/TASK 54-57-22-991-003
R
EFF :
501-509, 511-526, 528-599, 54-57-22
Page 410
Feb 01/10
CES
**ON A/C ALL
TASK 54-57-22-400-001
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-57-22-941-051
(1) Make sure that the access platform and the warning notices are in
position.
EFF :
ALL 54-57-22
Page 411
Feb 01/10
CES
4. Procedure
_________
Subtask 54-57-22-420-050
(e) Position the brackets (56) and (61) on the forward aprons (57)
and (60).
(2) Installation of the seal and retainer assemblies (41) and (44).
(Ref. Fig. 401/TASK 54-57-22-991-004)
(a) Position the seal and retainer assemblies (41) and (44) on the
pylon structure.
EFF :
ALL 54-57-22
Page 412
Nov 01/08
CES
R **ON A/C 501-509, 511-526, 528-599,
Subtask 54-57-22-420-050-A
(a) Position the forward apron assemblies (21) and (32) on the pylon
structure.
(b) Install the washers (30) and (22) and the bolts (23) and (29) on
the forward apron assemblies.
(f) Position the front angle assemblies (24) and (31) on the forward
apron assemblies (21) and (32).
(a) Position the welded assemblies (12), (13), (18) and (19) on the
pylon box.
(b) Install the washers (14), the bolts (15) and the nuts (16).
R
EFF :
501-509, 511-526, 528-599, 54-57-22
Page 413
Feb 01/10
CES
(b) Install the washers (2) (5) and the bolts (3) (6) on the angle
assemblies (1) and (4).
5. Close-up
________
Subtask 54-57-22-410-050
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
Subtask 54-57-22-410-050-A
A. Close Access
(1) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-57-22
Page 414
Feb 01/10
CES
R (3) Close of the thrust reverser doors (Ref. TASK 78-32-00-410-010).
R FOR 1000EM1
R 451AL, 452AR
R FOR 1000EM2
R 461AL, 462AR.
Subtask 54-57-22-942-050
B. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
EFF :
ALL 54-57-22
Page 415
Nov 01/07
CES
R **ON A/C 501-509, 511-526, 528-599,
TASK 54-57-22-000-003
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 54-57-22-941-054
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
R
EFF :
501-509, 511-526, 528-599, 54-57-22
Page 416
Feb 01/10
CES
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-57-22-040-051
Subtask 54-57-22-010-052
C. Get Access
4. Procedure
_________
Subtask 54-57-22-020-051
(2) Remove the forward profiles (71), (72), (73) and (74) and the aft
profiles (75) and (76).
R
EFF :
501-509, 511-526, 528-599, 54-57-22
Page 417
Feb 01/10
CES
Profiles
Figure 406/TASK 54-57-22-991-007
R
EFF :
501-509, 511-526, 528-599, 54-57-22
Page 418
Feb 01/10
CES
TASK 54-57-22-400-003
1. __________________
Reason for the Job
Self Explanatory
2. ______________________
Job Set-up Information
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
3. __________
Job Set-up
Subtask 54-57-22-860-050
(1) Make sure that the access platform and the warning notices are in
position.
(2) Make sure that the thrust reverser is unserviceable (Ref. TASK 78-30-
00-040-012).
R
EFF :
501-509, 511-526, 528-599, 54-57-22
Page 419
Feb 01/10
CES
4. Procedure
_________
Subtask 54-57-22-420-052
(1) Put the forward profiles (71), (72), (73) and (74) and the aft
profiles (75) and (76) in position.
5. Close-up
________
Subtask 54-57-22-440-051
Subtask 54-57-22-410-052
B. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
R
EFF :
501-509, 511-526, 528-599, 54-57-22
Page 420
Feb 01/10
CES
Profiles - Backing Strip Installation
Figure 407/TASK 54-57-22-991-008
R
EFF :
501-509, 511-526, 528-599, 54-57-22
Page 421
Feb 01/10
CES
SEALING - INSPECTION/CHECK
__________________________
TASK 54-57-22-200-001
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
-------------------------------------------------------------------------------
R
EFF :
501-509, 511-526, 528-599, 54-57-22
Page 601
Feb 01/10
CES
3. __________
Job Set-up
Subtask 54-57-22-941-052
A. Safety Precautions
(a) Put a warning notice to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5
minutes before you do this procedure.
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2)
pushbutton switch is off.
(b) Put a warning notice to tell persons not to energize the FADEC
1(2).
Subtask 54-57-22-040-050
Subtask 54-57-22-941-053
C. Get Access
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4. Procedure
_________
Subtask 54-57-22-220-050
A. Inspection
(Ref. Fig. 601/TASK 54-57-22-991-006)
(1) Do the inspection of the front sections (2), (3), (4) and (5) and the
rear sections (6) and (7) of the fairing and the inspection of the
welded assy (1).
(a) If you find cracks (cracks extend parallel to the spot weld
points), refer to the Structural Repair Manual (Ref. ASRM
54571101) for damage classification and corrective action.
5. Close-up
________
Subtask 54-57-22-440-050
Subtask 54-57-22-942-051
B. Close Access
(3) Make sure that the work area is clean and clear of tool(s) and other
items.
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Pylon-to-Nacelle Fairings
Figure 601/TASK 54-57-22-991-006
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