CMM 25-27-39 Rev 8 EX-INDIGO
CMM 25-27-39 Rev 8 EX-INDIGO
CMM 25-27-39 Rev 8 EX-INDIGO
HIGHLIGHTS
This manual is revised to incorporate Service Bulletin 863708-25-3298r1, engineering changes and
to update general information.
Title (T-1) Updated to reflect revision 8. Added seat part listings from Aircraft
Installation 863706-4010 (THY A320).
Records of Revision Updated to reflect revision 8.
(RR-1)
Service Bulletin List Added Service Bulletin 863708-25-3298r1 to list.
(SB-1)
List of Effective Pages
(LEP-1-LEP-4) Updated Numeric Index to reflect changes in IPL.
Table of Contents Updated to reflect changes and additions to revision 8.
(TOC-1, TOC-2)
Introduction (Intro-2) Revised Fits & Clearances description.
Description and Revised Figure 1 to add seat part listings from Aircraft Installation
Operation (4-16) 863706-4010 (THY A320). Added Table 1A.
Cleaning (4001-4006) Revised Table 4001. Revised cleaning procedures. Added Table
4002 (Solvent Selection For Hand Cleaning).
Check (5002, 5003) Revised seat belt check procedure. Revised Table 5001.
Repair (6001-6014) Revised Tables 6001 & 6002. Revised repair procedures.
Assembly (7002-7006) Revised Table 7001.
Fits and Clearances Revised In-Arm Table adjustment procedures. Added sections for
(8006-8014) Tolerances and Hardware Installation Requirements.
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Special Tools, Fixtures, Revised Tables 9001 & 9002. Added sharp edge tester
Equipment & Consum- information.
ables (9001-9006)
Illustrated Parts List
(10004) Revised CAGE Code list.
(10005-10036) Revised Numeric Index to reflect changes in IPL.
(10037-10158) Incorporated Service Bulletin 863708-25-3298r1 by adding IPL Figs.
1A and 2A. Added IPL Figs. 4A (3” Aft-Slider Table) and IPL Fig. 15
(IFE Instl).
Revised IPL Figs. 1, 2, 7, 8, 9, 13 and 14 to incorporate engineering
updates.
Removed information for IPL Fig. 3 (Table latch sold as assembly
only).
Renumbered pages to accommodate additional information.
HIGHLIGHTS
Page H-2
25-27-39 May 11/12
COMPONENT MAINTENANCE MANUAL
WITH ILLUSTRATED PARTS LIST
PASSENGER SEAT ASSEMBLIES
Page T-2
25-27-39 May 25/11
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
RECORD OF REVISIONS
Retain this record in the front of the manual. Upon receipt of a revision, insert the revised pages
in the manual, enter the revision number, date filled, and initial.
Page RR-1
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Page RR-2
25-27-39 May 25/11
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
NOTE: Temporary revisions are printed on yellow paper with the heading TEMPORARY
REVISION.
TEMPORARY DATE OF
REVISION DATE INCORPORATION
NUMBER INTO MANUAL
Page RTR-1
25-27-39 Feb 15/06
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Page RTR-2
25-27-39 Feb 15/06
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
DATE OF
SERVICE
DATE TITLE INCORPORATION
BULLETIN
INTO MANUAL
Page SB-1
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WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Page SB-2
25-27-39 Jun 12/06
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Fits and Clearances * 8009 May 11/12 Illustrated Parts List * 10035 May 11/12
(continued) * 8010 May 11/12 (continued) * 10036 May 11/12
* 8011 May 11/12 * 10037 May 11/12
* 8012 May 11/12 * 10038 May 11/12
* 8013 May 11/12 * 10039 May 11/12
* 8014 May 11/12 * 10040 May 11/12
* 10041 May 11/12
Special Tools, Fixtures, * 9001 May 11/12 * 10042 May 11/12
Equipment and * 9002 May 11/12 * 10043 May 11/12
Consumables * 9003 May 11/12 * 10044 May 11/12
* 9004 May 11/12 * 10045 May 11/12
* 9005 May 11/12 * 10046 May 11/12
* 9006 May 11/12 * 10047 May 11/12
* 10048 May 11/12
Illustrated Parts List 10001 Feb 15/06 * 10049 May 11/12
10002 Feb 15/06 * 10050 May 11/12
10003 Sep 15/09 * 10051 May 11/12
* 10004 May 11/12 * 10052 May 11/12
* 10005 May 11/12 * 10053 May 11/12
* 10006 May 11/12 * 10054 May 11/12
* 10007 May 11/12 * 10055 May 11/12
* 10008 May 11/12 * 10056 May 11/12
* 10009 May 11/12 * 10057 May 11/12
* 10010 May 11/12 * 10058 May 11/12
* 10011 May 11/12 * 10059 May 11/12
* 10012 May 11/12 * 10060 May 11/12
* 10013 May 11/12 * 10061 BLANK
* 10014 May 11/12 * 10062 May 11/12
* 10015 May 11/12 * 10063 May 11/12
* 10016 May 11/12 * 10064 May 11/12
* 10017 May 11/12 * 10065 May 11/12
* 10018 May 11/12 * 10066 May 11/12
* 10019 May 11/12 * 10067 May 11/12
* 10020 May 11/12 * 10068 May 11/12
* 10021 May 11/12 * 10069 May 11/12
* 10022 May 11/12 * 10070 May 11/12
* 10023 May 11/12 * 10071 May 11/12
* 10024 May 11/12 * 10072 May 11/12
* 10025 May 11/12 * 10073 May 11/12
* 10026 May 11/12 * 10074 May 11/12
* 10027 May 11/12 * 10075 May 11/12
* 10028 May 11/12 * 10076 May 11/12
* 10029 May 11/12 * 10077 May 11/12
* 10030 May 11/12 * 10078 May 11/12
* 10031 May 11/12 * 10079 May 11/12
* 10032 May 11/12 * 10080 May 11/12
* 10033 May 11/12 * 10081 May 11/12
* 10034 May 11/12 * 10082 May 11/12
Illustrated Parts List * 10083 May 11/12 Illustrated Parts List * 10131 May 11/12
(continued) * 10084 May 11/12 (continued) * 10132 May 11/12
* 10085 May 11/12 * 10133 May 11/12
* 10086 May 11/12 * 10134 May 11/12
* 10087 May 11/12 * 10135 BLANK
* 10088 May 11/12 * 10136 May 11/12
* 10089 May 11/12 * 10137 May 11/12
* 10090 May 11/12 * 10138 May 11/12
* 10091 May 11/12 * 10139 BLANK
* 10092 May 11/12 * 10140 May 11/12
* 10093 May 11/12 * 10141 May 11/12
* 10094 May 11/12 * 10142 BLANK
* 10095 May 11/12 * 10143 May 11/12
* 10096 May 11/12 * 10144 May 11/12
* 10097 May 11/12 * 10145 May 11/12
* 10098 May 11/12 * 10146 May 11/12
* 10099 May 11/12 * 10147 BLANK
* 10100 May 11/12 * 10148 May 11/12
* 10101 May 11/12 * 10149 May 11/12
* 10102 May 11/12 * 10150 May 11/12
* 10103 May 11/12 * 10151 May 11/12
* 10104 BLANK * 10152 May 11/12
* 10105 May 11/12 * 10153 May 11/12
* 10106 May 11/12 * 10154 May 11/12
* 10107 May 11/12 * 10155 May 11/12
* 10108 May 11/12 * 10156 May 11/12
* 10109 BLANK * 10157 May 11/12
* 10110 May 11/12 * 10158 May 11/12
* 10111 May 11/12
* 10112 BLANK Rework 16001 Feb 15/06
* 10113 May 11/12 16002 BLANK
* 10114 May 11/12
* 10115 May 11/12
* 10116 May 11/12
* 10117 May 11/12
* 10118 May 11/12
* 10119 May 11/12
* 10120 May 11/12
* 10121 May 11/12
* 10122 May 11/12
* 10123 May 11/12
* 10124 BLANK
* 10125 May 11/12
* 10126 May 11/12
* 10127 May 11/12
* 10128 May 11/12
* 10129 BLANK
* 10130 May 11/12
Page LEP-4
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
TABLE OF CONTENTS
Subject Page
Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Intro-1
1. Scope . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Intro-1
2. Product Support Services . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Intro-1
3. Usage Guide . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Intro-1
4. Abbreviations, Acronyms and Unit Symbols . . . . . . . . . . . . . . . . . . . . . . . . . Intro-3
Description and Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
1. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
2. Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
3. Leading Particulars . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8
Testing and Fault Isolation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1001
1. Operational Checks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1001
2. Fault Isolation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1003
Schematics and Wiring Diagrams (not applicable)
Disassembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3001
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3001
2. Disassembly Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3001
Cleaning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4001
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4001
2. Cleaning Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4002
Inspection/Check . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5001
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5001
2. Inspection/Check . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5001
3. Scheduled Checks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5002
4. Maintenance Records . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5002
Repair . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6001
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6001
2. Repair Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6001
Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7001
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7001
2. Assembly Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7004
3. Storage Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7006
Fits and Clearances . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8001
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8001
2. Adjustment Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8001
3. Tolerances . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8007
4. Hardware Installation Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8010
Special Tools, Fixtures, Equipment and Consumables . . . . . . . . . . . . . . . . . . . . . . . . . 9001
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9001
Illustrated Parts List . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10001
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10001
2. Scope of Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10001
3. Equipment Designator Index . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10001
4. Numerical Index . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10001
5. Explanation of Detail Parts List Entries . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10002
6. Manufacturer Names and Addresses. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10004
Rework . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16001
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16001
2. Rework Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16001
Page TOC-1
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WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
LIST OF ILLUSTRATIONS
Figure Title Page
LIST OF TABLES
Table Title Page
Page TOC-2
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INTRODUCTION
1. Scope
Replacement parts, technical publications, and other product support services are available
from Weber Aircraft LLC. Please contact:
3. Usage Guide
(2) TESTING AND FAULT ISOLATION. This section details testing and
troubleshooting a completely assembled passenger seat.
(4) DISASSEMBLY. This section details the disassembly procedure for parts that need
to be removed to allow visual inspection of the passenger seats and for parts that
can be removed.
(5) CLEANING. This section provides a list of cleaning materials and instructions for
cleaning the passenger seats.
(7) REPAIR. This section provides a list of all materials required for the passenger
seats and repair or replacement instructions that refers to the procedure for the
removal, disassembly, repair, reassembly, and installation of all parts not listed in
DISASSEMBLY.
Page Intro-1
25-27-39 Sep 15/09
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
(8) ASSEMBLY. This section includes a list of all materials required during assembly,
and the assembly procedures for all parts disassembled in DISASSEMBLY.
REPAIR details the assembly procedure for all parts not detailed in this section.
This section also provides storage instructions for the passenger seats.
(9) FITS AND CLEARANCES. This section contains fits and clearance for the
passenger seats including torque tables, adjustments, and general installation
information. It also gives the permitted wear tolerances for in-service and the seat
manufacturer’s design wear tolerances.
(11) ILLUSTRATED PARTS LIST. This section contains a complete list of spare parts
for the passenger seats with an alphanumeric index listed in the front.
(12) REWORK. This section contains procedures to rework or modify the seat assembly
or components of the seat.
B. The sections contain a table of recommended tools and materials, when applicable.
Equivalent items can be used.
D. Verification.
Page Intro-2
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Abbreviations and unit symbols used in this manual are defined below. All weights and
measurements are given first in English standard units followed by the metric equivalent in
parentheses.
Symbol/ Symbol/
Abbr. Term Abbr. Term
Page Intro-3
25-27-39 Feb 15/06
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Symbol/ Symbol/
Abbr. Term Abbr. Term
Page Intro-4
25-27-39 Feb 15/06
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
A. General.
The passenger seats feature maximum comfort design and consist of an aluminum
frame to which are attached reclining seat backs, center armrest assemblies, armrest
food table assemblies and fully upholstered seat back and bottom cushion assemblies.
The passenger seats are installed and secured to the metal floor tracks located in the
aircraft cabin by track attachment fittings at each front and rear leg. Seat dimensions are
shown in Figure 1. Seat dimensions not shown are the same as the opposite view. Refer
to Table 2 for dimension tolerances.
B. TSO Limitations.
The conditions and tests required for TSO approval of these articles are minimum
performance standards. It is the responsibility of those desiring to install the articles
either on or within a specific type or class of aircraft to determine that the aircraft
installation conditions are within the TSO standards. If not within the TSO standards, the
articles may be installed only if further evaluation by the applicant documents an
acceptable installation and is approved by the Administrator.
C. Conformity to Certification.
The numerous requirements for demonstrating that a “seat system” meets all the static
and dynamic loads, the permanent deformation limitations, and the injury criteria, imply
that individual elements of a seat system cannot be evaluated independently from each
other. This difficulty translates into keeping the chain of structures and other essential
features affecting the performance of the “seat system” intact as certificated.
The performance of the components, the behavior of which are critical to the overall
system, are numerous. These include, but are not limited to the seat belt, the bottom
cushions, the padded back assemblies, the seat back weight and vertical center of
gravity, the impact surfaces on the back such as back mounted tables and appliances,
the total mass of the seat, any structural load path active in a primary or secondary
fashion in restraining the passenger to the seat and to the aircraft. Additionally, the seat
back upright setting, back breakover (if any and degrees), seat pitch, aircraft track, track
fitting, track adapter, angle of the seat with respect to the aircraft axis (e.g., non-constant
section), baggage bar design, IFE support installation on legs, retention of deployable
items, such as tables, video and others, all have significant impact on the certification.
Modifications by a non OEM; or the replacement of a non OEM component, will
invalidate the OEM’s TSO certification.
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WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
D. Safety Considerations.
Each back incorporates padded material to protect against head strike injury and is
contoured to fit a passenger of varied sizes yet provide optimum comfort.
The seat bottom structure (base frame assembly) is designed to eliminate any
protrusions, edges, or projections which might penetrate the various cushions during
vertical movements. All areas of passenger contact are free of projections which might
cause injury or damage to clothing.
Bottom and back cushion assemblies are covered with fireblocking covers. Life vest
assemblies are also provided.
E. Seat Backs.
Seat backs (except stretcher provisioned seats) are configured for no breakover.
The seat backs incorporate design features which provide maximum comfort with
minimum interference for ingress and egress of passengers when installed in the
aircraft. A literature pocket is located at the rear of each back assembly. Seat back
recline is hydraulically controlled.
A shrouded food table stowed on the back assembly pivots at the same pivot point as
does the back assembly.
Front row seat assemblies are equipped with an in-arm food table located in aisle and
center armrest modules where there is no seat directly in front of a passenger
placement.
I. Stretcher Provisions
The left hand seats in the last three rows of the aircraft are equipped for full breakover
for stretcher provisioning.
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WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
2. Operation
A. General.
Seat assemblies are secured to the aircraft floor and sidewall by shear pin assemblies
and anti-rattle track fittings located at the base of the leg assembly. Place seat on aircraft
floor and sidewall track and slide forward or aft direction to desired station number
location. Torque down shear pin assembly to 45±10 In./Lbs. Visually inspect to ensure
that the shear pin assembly is fully engaged with the aircraft track. Torque down front
anti-rattle assembly to 45±10 In./Lbs. and again visually inspect (refer to FITS AND
CLEARANCES, paragraph 2.D).
B. Seat Backs.
The seat back recline may be adjusted (more or less recline) to a recline position by
actuating the recline control. The seat control is located in the side of the side armrest
assembly. Seat back recline is hydraulically controlled.
Literature pockets are located on the lower, rear area of the seat backs.
This type food table is brought into use by using the food table latch assembly to unlatch
the food table. Once the table is released, allow table to come down to the use position,
Pull the table out to the fully deployed position. To secure table in the non-use position,
push table in then fold the table up and in to the back recess. Secure table with food
table latch.
The food tables are deployed by raising the armcap up, lifting the table out of the cavity
into the vertical position, then unfolding the assembly down across the seat placement.
To stow, simply reverse this procedure.
To place arm in upright position, press the discrete arm latch located under the arm
(aisle arm only). Lift the front of the arm up, rotating the arm backwards along the side
of the back assembly. To return the arm to the horizontal position, pull down on the front
of the arm by rotating it forward and down until positive engagement of the discrete arm
latch can be heard.
F. Stretcher Provisioning
To break seat back over, remove clip from the rear of the recline lock. Replace clip for
storage. To reattach recline lock, align quadrant arm in the recline lock slot and insert
pin. Secure installation by pressing clip aver barrel of recline lock.
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
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WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
3. Leading Particulars
Tables 1 and 1A provide a list of all seat assemblies contained in the seat installations
covered by this manual. Refer to the IPL portion of the manual for additional information on
particular seat assembly usage, etc.
Weber Aircraft
Description
Part No. Installation
859628-401 SEAT AY, MODEL 5600, T/C LH IAT TPL, NO ASH 859910-4010
(859910-401) RECEIVER
859628-402 SEAT AY, MODEL 5600, T/C RH IAT TPL, NO ASH 859910-4010
(859910-402) RECEIVER
855104-401 SEAT AY, MODEL 5600, T/C LH HDCP TPL, NO ASH 859910-4010
(859910-403) RECEIVER
855104-402 SEAT AY, MODEL 5600, T/C RH HDCP TPL, NO ASH 859910-4010
(859910-404) RECEIVER
860001-401 SEAT AY, MODEL 5600, T/C LH FWD EXIT HDCP TPL, 859910-4010
(859910-405) NO ASH RECEIVER, NO RECLINE
860001-402 SEAT AY, MODEL 5600, T/C RH FWD EXIT HDCP TPL, 859910-4010
(859910-406) NO ASH RECEIVER, NO RECLINE
860002-403 SEAT AY, MODEL 5600, T/C LH EXIT HDCP TPL, NO 859910-4010
(859910-413) ASH RECEIVER, NO RECLINE, NO OUTBD ARMREST
(POST SB 859910-25-2678)
860002-404 SEAT AY, MODEL 5600, T/C RH EXIT HDCP TPL, NO 859910-4010
(859910-414) ASH RECEIVER, NO RECLINE, NO OUTBD ARMREST
(POST SB 859910-25-2678)
855107-423 SEAT AY, MODEL 5600, T/C LH HDCP AFT EXIT TPL, NO 859910-4010
(859910-415) ASH RECEIVER, NO OUTBD ARMREST (POST SB
859910-25-2678)
855107-424 SEAT AY, MODEL 5600, T/C RH HDCP AFT EXIT TPL, 859910-4010
(859910-416) NO ASH RECEIVER, NO OUTBD ARMREST (POST SB
859910-25-2678)
855109-401 SEAT AY, MODEL 5600, T/C LH HDCP NARR TPL, NO 859910-4010
(859910-411) ASH RECEIVER, NO RECLINE, NO BACK TABLES
855109-402 SEAT AY, MODEL 5600, T/C RH HDCP NARR TPL, NO 859910-4010
(859910-412) ASH RECEIVER, NO RECLINE, NO BACK TABLES
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Weber Aircraft
Description
Part No. Installation
855101-411 SEAT AY, MODEL 5600, T/C LH IAT TPL, NO ASH 863706-4010
(863706-401) RECEIVER (POST SB 863708-25-3298)
855101-412 SEAT AY, MODEL 5600, T/C RH IAT TPL, NO ASH 863706-4010
(863706-402) RECEIVER (POST SB 863708-25-3298)
855104-411 SEAT AY, MODEL 5600, T/C LH HDCP TPL, NO ASH 863706-4010
(863706-403) RECEIVER (POST SB 863708-25-3298)
855104-412 SEAT AY, MODEL 5600, T/C RH HDCP TPL, NO ASH 863706-4010
(863706-404) RECEIVER (POST SB 863708-25-3298)
855105-411 SEAT AY, MODEL 5600, T/C LH FWD EXIT HDCP TPL, 863706-4010
(863706-405) NO ASH RECEIVER, NO RECLINE, AN79 STOP (POST
SB 863708-25-3298)
855105-412 SEAT AY, MODEL 5600, T/C RH FWD EXIT HDCP TPL, 863706-4010
(863706-406) NO ASH RECEIVER, NO RECLINE, AN79 STOP (POST
SB 863708-25-3298)
855106-411 SEAT AY, MODEL 5600, T/C LH EXIT HDCP TPL, NO 863706-4010
(863706-407) ASH RECEIVER, NO RECLINE, NO OUTBD ARMREST,
AN79 STOP (POST SB 863708-25-3298)
855106-412 SEAT AY, MODEL 5600, T/C RH EXIT HDCP TPL, NO 863706-4010
(863706-408) ASH RECEIVER, NO RECLINE, NO OUTBD ARMREST,
AN79 STOP (POST SB 863708-25-3298)
855107-411 SEAT AY, MODEL 5600, T/C LH HDCP AFT EXIT TPL, NO 863706-4010
(863706-409) ASH RECEIVER, NO OUTBD ARMREST, AN79 STOP
(POST SB 863708-25-3298)
855107-412 SEAT AY, MODEL 5600, T/C RH HDCP AFT EXIT TPL, 863706-4010
(863706-410) NO ASH RECEIVER, NO OUTBD ARMREST, AN79
STOP (POST SB 863708-25-3298)
855109-411 SEAT AY, MODEL 5600, T/C LH HDCP NARR TPL, NO 863706-4010
(863706-411) ASH RECEIVER, NO RECLINE, NO BACK TABLES
(POST SB 863708-25-3298)
855109-412 SEAT AY, MODEL 5600, T/C RH HDCP NARR TPL, NO 863706-4010
(863706-412) ASH RECEIVER, NO RECLINE, NO BACK TABLES
(POST SB 863708-25-3298)
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WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Tolerance Description
± 1° Seat breakover
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
(1) With all seat backs in full upright position, visually check alignment of seat backs
against each other, none should be obviously out of alignment.
(a) If the seat is on a known flat and level surface, place a plumb-bob over the top
of each seat back at the center, and measure the distance from the centerline
of the front track fitting of the seat (Ref. Fig. 1, DESCRIPTION AND
OPERATION section) to the plumb-bob; measurements shall be as indicated
on Figure 1.
(b) If the seat is not on a flat and level surface, measure the distance from the
center of the seat back to centerline of the front track fitting of the seat (Ref.
Fig. 1, DESCRIPTION AND OPERATION section) use a tool that can allow
for an unlevel condition. These tools may include, but are not limited to, a
level, square, linear scale, special templates and/or a straight edge.
(3) If dimensions measured in step (2) above are off, refer to FITS AND
CLEARANCES, paragraph 2.B or 2.C.
(4) In the recline mode, press recline control button on armrest while applying a force
(4 to 8 lbs / 1,8 to 3.6 Kg) to top of seat back assembly. Seat back shall move to
full recline position, or stop automatically at any position when the recline control
button is released.
(5) If seat back does not fully recline refer to fully reclined dimension specified in Fig.
1. Adjust in accordance with FITS AND CLEARANCES, paragraph 2.B or 2.C.
(6) With seat back in fully reclined position, remove any pressure applied to seat back,
and depress recline control button. Seat back shall automatically return to the full
upright position.
(7) If depressing recline control does not release seat back for recline adjustment,
make sure that recline control is attached to recline lock; then adjust recline control
operation so that plunger on end of recline lock is pushed in when recline lock
control button is depressed. If this adjustment does not obtain satisfactory
operation;
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
(1) Visually check position of food table in stowed position; tables shall be flush with
seat back, with no obvious protrusion.
(2) If table is not flush, refer to FITS AND CLEARANCES, paragraph 2.A.
(3) Rotate latch handle and allow food table to drop into the “in use” position. Check
that food table is level with cabin floor. Check height (refer to FITS AND
CLEARANCES, paragraph 2.A).
(1) Visually check hinged armcap assemblies and table module assemblies. There
should be no obvious misalignment.
(2) Pull table assembly out of armrest and swing into “use” position. Movement should
be smooth with no binding and table should be in a correct “in use” configuration.
(3) Adjust food table as necessary, refer to FITS AND CLEARANCES, paragraph 2.E.
(1) Visually check alignment of armrest “in use” position. There should be no obvious
misalignment with other arms.
(2) If alignment is incorrect, check all engaging parts for wear and/or obstructions that
me be preventing armrest from fully folding or permitting excessive downward
positioning. Replace any defective parts. Adjust setscrew on center support to
obtain correct height.
(3) Grasp each folding armrest at forward end and pull up to stowed position between
seat backs. Force required should be approximately 8 lbs. to prevent free fall from
stowed position.
(1) The seat assemblies should lock securely to the floor track at the lock mechanisms
and to the studs at the bottom of the leg assemblies.
(2) If the lock mechanisms or studs do not lock firmly into the floor tracks, refer to FITS
AND CLEARANCES, paragraph 2.D.
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
2. Fault Isolation
Troubles encountered with mechanical operation of the seat assembly will largely be the
result of improper adjustments. In addition, after overhaul and adjustment, mechanical
functions may be a bit “stiff”. Stiffness in operation will reduce after some “break-in” use.
Troubles likely to be encountered, together with probable causes and corrective actions are
listed in Table 1001.
Recline control will not move Broken or malfunctioning control Adjust or replace malfunctioning
or fails to unlock seat back component. (Refer to FITS AND
CLEARANCES, paragraph 2.B
or 2.C)
Control line broken Replace control line. (Refer to
REPAIR section)
Recline lock not properly Adjust lock. (Refer to FITS AND
adjusted CLEARANCES, paragraph 2.B
or 2.C)
Seat backs do not align in Improper adjustment of recline Adjust or replace malfunctioning
upright position control setting component. (Refer to FITS AND
CLEARANCES, paragraph 2.B
or 2.C)
Seat loose in floor track of Anti-rattle device or plunger on Tighten screw on anti-rattle device
aircraft rear track fitting loose or push plunger back down. (Refer
to FITS AND CLEARANCES,
paragraph 2.D)
In-Arm food tables do not Adjustment not correct Adjust as necessary. (Refer to FITS
align in “use” or “stow” AND CLEARANCES, paragraph
configurations 2.E)
Food table not at proper Adjustment of screw not Adjust screw as required. (Refer to
height in serving position properly set FITS AND CLEARANCES,
(back mounted) paragraph 2.A)
Food table will not fold flush Adjustment of screw not Adjust screw as required. (Refer to
into seat back recess (back properly set FITS AND CLEARANCES,
mounted) paragraph 2.A)
Folding arms are out of Latch assembly damaged Replace damaged component.
alignment
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WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
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WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
DISASSEMBLY
1. General
B. Partial repair of some assemblies may be performed without removing the particular
assembly from the aircraft.
2. Disassembly Procedures
A. Model 5600 Tourist Class IAT Triple Seat Assembly. (See IPL Figure 1)
(1) Remove dress appearance items and cushions. Set aside in a clean dry area with
protective covering.
(2) Refer to DISASSEMBLY paragraph 2.C for instructions pertaining to food table
latch (75, 75A), 2.D for back-mounted food table (85), 2.E for back structure (115
thru 115C), 2.F for armrest (155, 155A), 2.G for IAT module assembly (250 thru
250C), 2.H for IAT food table (265, 265A), 2.I for leg (370), 2.J for aisle spreader
(435, 435A), 2.K for center spreader (440, 440A) and 2.L for outboard spreader
(445, 445A).
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
B. Model 5600 Tourist Class Standard/Handicap/Exit Triple Seat Assembly. (See IPL
Figure 2)
(1) Remove dress appearance items and cushions. Set aside in a clean dry area with
protective covering.
(2) Refer to DISASSEMBLY paragraph 2.C for instructions pertaining to food table
latch (75, 75A), 2.D for back-mounted food table (85), 2.E for back structure (115
thru 115H), 2.M for outbd armrest (115, 155A), 2.M center and aisle armrest (210
thru 210C, 265 thru 265C), 2.I for leg (370 thru 375B), 2.J for aisle spreader (435
thru 435C), 2.K for center spreader (440 thru 440F) and 2.L for outboard spreader
(445 thru 445E).
(1) Remove table legs (10, 15) by removing applicable attaching parts.
(1) Remove literature pocket spring (40, 40A) quadrant arm (70, 70A) by removing
applicable attaching parts. Remove and replace velcro (110 thru 130) as required.
(1) Remove armcap (5), bracket (on armcap) (15), lower hinge (on armcap) (55),
upper hinge (on armcap) (40), lower hinge (55) and recline cable (65, 65A) by
removing applicable attaching parts.
(1) Remove screw (5). Remove finger lift (15, 15A), IAT link (25), paddle arm (45, 45A),
slide (65), knuckle (85, 85A) and track (100) by removing applicable attaching
parts.
(1) Remove base assembly (5) and strut (65) by removing applicable attaching parts.
(1) Remove back pivot pin (20), link (40), swivel limit bracket (part of seat belt link) (55)
and back support (95, 95A) by removing applicable attaching parts.
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
(1) Remove back pivot pin (25), link (45), swivel limit bracket (part of seat belt link) (65),
back support (100, 100A) and adapter (140, 145) by removing applicable attaching
parts.
(1) Remove back pivot pin (10), upper spreader (30 thru 35), link (60), swivel limit
bracket (part of seat belt link) (85) and support (120, 120A) by removing applicable
attaching parts.
(1) Remove base assembly (5), strut assembly (65) and adapter (125, 130) by
removing applicable attaching parts.
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
CLEANING
1. General
NOTE: Recommended cleaning agents are listed in Table 4001. Suitable substitutes
or equivalents may be used after appropriate tests are made to ensure
equivalent agents do not react with area being cleaned.
NOTE: Refer to Table 4002 for recommended solvent selections for hand cleaning.
Cleaning Materials
Table 4001
Material Identification Source
Detergent Activator For Perchloroethylene No. G84 A.L. Wilson Chem Co.
Kearny, New Jersey
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WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Cleaning Materials
Table 4001
Material Identification Source
2. Cleaning Procedures
A. Non-Upholstered Parts
(2) Clean metal parts with Aliphatic Naphtha specified in Table 4001. Dry with a clean,
lint-free cloth or allow to air dry.
(3) Remove any stains or deposits on non-electrical metal parts not removed by
Aliphatic Naphtha with a cloth moistened with Acetone (refer to Table 4001).
(4) Remove any signs of corrosion with corrosion removing compound (refer to Table
4001).
B. Upholstery
(1) Vacuum upholstery thoroughly or brush with a medium stiff bristle upholstery or
clothes brush. Do not pound or beat upholstered covers as this does not effectively
clean the upholstery and can hasten its wear.
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
(3) Oil-type grease spots are best removed with solvent-type cleaning fluid such as
DuPont Dry Cleaner (refer to Table 4001) or with solvent impregnated Powderene
powder (refer to Table 4001). Test material to be cleaned by first applying cleaning
agent to a small inconspicuous area of the material. Use cleaning agents sparingly,
without saturating fabric, to avoid spotting and damage. Apply cleaning agent with
a soft clean cloth and avoid spreading any stains by working from outer edges
toward center of stain.
(4) After using upholstery shampoo or solvent-type cleaning agent, roll a clean, turkish
towel, or other absorbent cloth, into a cylindrical shape and wipe off detergent and
dirt. Rotate rolled cloth frequently to present a clean section to the fabric surface.
NOTE: Dirt and soil are absorbed or transferred to the clean towel from the fabric.
Vigorous rubbing may be required to obtain even soil removal and to
avoid spotty or blotchy appearance after drying.
(5) Prepare seat covers for dry cleaning by covering all “velcro” hook tape with
corresponding pile tape. Heavy stains should be pretreated as outlined in steps (2)
and (3) above. Turn seat covers inside out during actual dry cleaning procedure.
(6) Dry clean seat covers in Perchloroethylene or Stoddard solvent with addition of 1/
2% commercial detergent activator. (Refer to Table 4001). Use activator per
manufacturer’s instructions. Use cleaning solvent cold in room temperature drum.
NOTE: Water content of cleaning solution must not exceed 0.8%. If water content
exceeds this proportion, there is possibility of fabric shrinkage.
(7) Dry seat covers with maximum temperature of incoming air at 55°C (130°F). After
completion of dry cleaning process, waterbound stains can be removed
secondarily with steam and detergent preparations as outlined in step (2) above.
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
C. Metal Parts.
(1) Moisten a clean, dry cloth with a chlorinated dry cleaning solvent and thoroughly
wipe metal parts completely clean. Repeat as required to remove stubborn
accumulation of dirt and grease. Dry with a fresh, clean, dry cloth.
D. Fabric-Backed Vinyls.
(1) This type of material should be cleaned with a mild soap and water solution, such
as Ivory Liquid Soap, and wiped clean and dry. Do not use solvent-type cleaners.
(1) Regular cleaning can be done simply by using a damp cloth, taking care not to soak
the leather. Wring out a soft cloth in soap suds (mild toilet soap and never a
detergent). Apply to the surface of the leather in a light, circular motion until the dirty
parts are clean. Repeat this procedure with clean cloth and clean water.
DO NOT use any spray polishes that contain silicone. Silicone will
produce an unpleasant, sticky surface.
DO NOT use any cleaning fluid which does not specifically state that
it can be used on leather.
(2) Proprietary products, made by leather manufacturers, are available. These neutral
creams or waxes are designed to restore the original sheen. These should not be
used until the leather has first been cleaned with a damp clean cloth as outlined in
step (1) above.
F. Plastic.
(1) Extreme care should be taken in cleaning all plastic. Abrasive soaps and bleaches
should never be used to clean any plastic materials. All plastic surfaces should be
cleaned with a mild soap and water solution or recommended plastic cleaner, such
as those mentioned below.
(2) Mix liquid soap or plastic cleaner with water to desired concentration, depending
on strength needed for cleaning purposes. Apply solution directly to surface and
rub with a clean, lint-free cloth to loosen dirt and debris. Wipe off with fresh, clean,
lint-free cloth or rinse with water and dry with a Turkish towel.
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
(3) To clean KYDEX 510, dust it with a soft cloth or chamois and wipe the surface
gently. Use soap and lukewarm water to remove light dirt After washing dirt. and
rinsing, be sure to dry the surface by blotting with a damp cloth or chamois. If a
cleaner must be used to remove heavier dirt or grease Janitor in a Drum and
Cascade were found to be the most effective cleaners to remove this type of dirt.
(4) Normal liquid cleaners or soap and water may not remove ground in dirt or grease.
Stains such as iodine may be safely removed with isopropyl alcohol (45%). The
higher concentration commercial grades of isopropyl alcohol will remove the stain,
but will dull the film surface. To return the gloss, wax with Simoniz wax.
(5) Light surface scratches and abrasions on KYDEX 510 can be removed by waxing
with Simoniz. Deeper scratches may be removed by lightly buffing surface with a
fine grade of rubbing compound. After application of the wax, polish the surface
lightly with a clean cotton flannel of jersey cloth. After polishing, wipe area gently
with a damp cloth to ground any electrostatic charges that may attract dust
particles.
(1) Remove any kind of soil, grease, and oil from powder-coated surfaces by
scrubbing with Spray White E (Kelite Chemical Corp.).
(2) Buff powder-coated surfaces with dry, lint-free cloth to remove residue after
cleaning.
H. IFE Equipment.
(1) IFE equipment is to be cleaned and cared for in accordance with the CMM
provided by the IFE supplier.
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Metal B B A A
Plastics: polycarbonate, C A C C
polysulfone
Rubber: silicone A A A B
Notes:
(1) A = Recommended; B = Allowed; C = Prohibited
(2) Lacquer thinners used for cleaning purposes must have vapor pressures not
greater than 45mm.Hg at 25°C.
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INSPECTION/CHECK
1. General
NOTE; Establish requirements of any service bulletins applicable to this equipment. During
check, determine which service bulletins, if any, are to be incorporated.
Replace, with a serviceable part, any part that fails to meet the requirements of check. If
defective part is repairable, note defect and assign part for repair.
2. Inspection/Check
NOTE: Conduct checks under a bright light. Use a 5X to 7X power magnifying glass to
detect surface flaws.
A. Visually check that all parts are clean and free of cracks, corrosion, deterioration, and
obvious signs of damage.
B. Check security of all clamps and straps securing leads and all other parts not removed
during disassembly.
C. Visually check all threaded parts for crossed or damaged threads. Reject part if thread
damage exceeds 50% of one thread.
NOTE: If damage to any one thread is 50% or less, note defect and assign part for
repair.
D. Check sewn seams for fraying or separation and fabric for fraying, scuffing and rips.
E. Check attaching bolts, nuts, screws and pins for tightness and floor attaching fittings for
wear or deformation.
G. Check structural parts including clips, brackets and machined parts for damage, cracks
and sharp nicks.
NOTE: Burrs are defined as material raised above the normal surface, which if not
removed would prevent complete and proper mating of parts and sealing
surfaces. Where nicks or scratches allow bare metal to show through a
protective finish, note defect and assign part for repair. Dents or other damage
must not impair finish or functional operation of any part.
H. Check paint and finishes for chipping and worn spots, and note condition of bonding on
parts and assemblies.
I. Check data plate and placards for legibility and secure attachment.
J. Check food table top shroud for nicks, cracks, stains or burns.
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
NOTE: Slight wear of the webbing is permitted however, excessive web wear that has
progressed to cut or worn edges must be replaced. Refer to following criteria
to make this determination.
(1) A limited amount of “frayed” webbing will retain sufficient strength necessary to
meet the required strength. Frayed webbing is defined as broken filaments from
either the warp (longitudinal) yarns or the filler (transverse) yarns. The number of
broken filaments should not be sufficient to obscure the identity of any yarn when
viewed from a distance of about 8 inches.
(2) Any web that is cut or torn deeper than 0.10 inches on the edge.
(3) The amount of fray should be limited to an amount that is less than 10% of the width
of the webbing and not to exceed 8 inches in length.
(4) Webbing with more than 15 broken yarns in locations other than the edge.
(5) Webbing that is frayed of distorted sufficiently to cause improper operation of any
portion of the restraint system.
L. Check cushions for wear and damage to fireblock and dress cover. Repair if there are
rips, gaps or loose seams. Cushions should be replaced at two year intervals to
guarantee maximum comfort.
CAUTION: Cushions must be replaced if they feel unstable (loose pieces, brittle,
etc.).
3. Scheduled Checks
4. Maintenance Records
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COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Scheduled Checks
Table 5001
Man-
Frequency Check Hours
per Unit
“A”, “C” and “D” Check * Check functionality and leveling on back-mounted and IAT .05
food table assemblies.
“A”, “C” and “D” Check * Check bumper strips for damage (check corners). .004
“A”, “C” and “D” Check * Check all armcaps and footbar pads for excessive wear. .008
“A”, “C” and “D” Check * Check for correct installation of bottom cushions and back .05
cushion inserts. (Refer to paragraph 2.L for inspection crite-
ria).
“A”, “C” and “D” Check * Check all video arms for proper friction. .05
“A”, “C” and “D” Check * Check cushions, fireblocking and dress covers for excessive .05
wear.
“A”, “C” and “D” Check * Check all food trays in seat backs and IAT for cracks and
delamination.
“C” and “D” Check * Check all seat belts for cut or worn edges, damaged stitching. .05
Broken fabric threads, excessive chafe marks, excessive
wear/fusing. (Refer to paragraph 2.K for inspection criteria).
“C” and “D” Check * Check all bushings (seat backs, spreaders, eyebolts etc.) for .10
excessive wear or looseness.
“C” and “D” Check * Check all wear surfaces (slides, foodtable slides, cocktail .10
trays, in arm food tables) for looseness and excessive wear.
“C” and “D” Check * Check spreaders and legs for looseness, cracks or other .05
damage.
“C” and “D” Check * Check track fitting for looseness, corrosion or other damage. .05
Page 5003
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Page 5004
25-27-39 Feb 15/06
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
REPAIR
1. General
A. Repair of the seat assemblies is generally limited to those repairs that can be effected
by standard shop practices. Major structural repairs are to be avoided since the safety-
integrity of the seat can be compromised by improper disassembly and assembly of
major structural components.
2. Repair Procedures
Abrasive cloth, 320 grit or finer Federal Specification P-C-451 Commercially available
Page 6001
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Glass cloth Style 191, finish compatible with Uniglass Industries, Inc.
epoxy resins New York, New York
A. Metal Surfaces.
(1) Polish out minor nicks and scratches on steel surfaces with crocus cloth. Polish out
minor nicks and scratches on aluminum parts with 600 to 800 grit aluminum oxide
abrasive cloth. Every effort shall be made to polish out nicks and scratches without
removing protective surfaces. Clean sanded areas as directed in paragraph 2.A,
CLEANING.
(3) With aluminum alloy parts without cladding, remove scratches or edge burrs using
a burnishing tool.
Page 6002
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
(4) 320 grit or finer, abrasive cloth with oil or soft wiping materials and polishes shall
be used for blending repaired areas. Remove oil by solvent wiping or remove polish
with water or solvent depending on type.
(6) Apply one drop of solution to the deepest portion of scratch for three minutes
maximum. The presence of a dark gray or black product of reaction indicated that
the scratch has penetrated through the cladding to the basic material. If the
reaction product is white, or faintly gray, some portion of the cladding is still intact.
Rinse test area thoroughly with water and dry, using tissues, etc.
(7) When repairs are required, apply masking tape around scratch to confine area
affected to ¼ in. or less in width.
(8) Apply chromate conversion coating Grade B to repaired area. Anodizing of clad
alloys would result in areas of difference color wherever the cladding has been
removed.
(9) Damaged anodized coatings may be satisfactorily repaired from the standpoint of
corrosion resistance by applying a chromate conversion coating.
(10) For decorative plated parts, minor scratches, stains, or other defects shall be
removed by light buffing, if it is possible to do so while maintaining required plating
thickness. Parts not repairable by light buffing should be replaced.
(1) It is not possible to repair plastic shrouds to “like-new” as the repairs will require
refinishing with paint which has different wear characteristics than the original
shroud material. In addition, the surface texture will be changed in the repaired
area and restoration is difficult, if not impossible, to achieve.
(2) (b) Shrouds which are broken into two or more pieces should be discarded unless
a fixture is devised as an external mold so that part shape will be retained during
repair reinforcement procedures outlined below.
(3) Remove shroud from structure using care not to damage or deform the parts. If
shroud is bonded to structure, a hot air-gun may be used to soften the bond line.
Use care not to exceed 150ºF temperature and not to deform the shroud while hot.
Remove adhesive with isopropyl alcohol or aliphatic naphtha.
Page 6003
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
(4) Clean shroud surfaces using a warm detergent solution, 3% detergent in warm
water at 120°F (48°C). Rinse thoroughly with clear water and dry.
(5) Clean shroud surfaces using a warm detergent solution, Refer to Cleaning for
recommended cleaning methods.
(6) Where necessary, reinforce inside surface of shroud in damaged area as follows:
(a) Roughen an area at least one inch larger than damaged area with 80 grit
abrasive cloth.
(b) Wipe bond area with Isopropyl Alcohol using clean, oil-free wipe.
(c) Coat bond area with A-1404-B EPOXY (Table 6002) adhesive.
(e) Coat glass cloth with epoxy and remove entrapped air bubbles with a roller or
squeegee.
(f) Continue laminating layers of glass cloth and epoxy resin until desired
thickness is attained. Limit the reinforcement to that thickness which will
permit reinstallation of reinforced shroud on its substructure. The necessary
number of glass cloth reinforcements may be determined as follows:
(g) Cure epoxy resin reinforcements for 24 hours at room temperature, 75°F
(23.8°C) or above. Cure may be accelerated by increasing temperature to
120°F (48.8°C) (max) which will cure resin in approximately four hours.
Page 6004
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
C G
T Typical
L R
Y Users,
A A
P Product Cured Applications,
S D
E Designation Description Color Name and Address Remarks
S E
Epoxy Adhesives
Page 6005
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
C G
T Typical
L R
Y Users,
A A
P Product Cured Applications,
S D
E Designation Description Color Name and Address Remarks
S E
I 2 A FE 7610 A/B Resin & Alum H.B. Fuller Co. Filling and
Hardener 2400 Kasota Ave. smoothing
St. Paul, MN compound
Page 6006
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
C G
T Typical
L R
Y Users,
A A
P Product Cured Applications,
S D
E Designation Description Color Name and Address Remarks
S E
Page 6007
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
C G
T Typical
L R
Y Users,
A A
P Product Cured Applications,
S D
E Designation Description Color Name and Address Remarks
S E
Cyanoacrylate Adhesives
Page 6008
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
C G
T Typical
L R
Y Users,
A A
P Product Cured Applications,
S D
E Designation Description Color Name and Address Remarks
S E
XII 1 A Aron Alpha 1 part liquid Clear McDonald & Co. Fast set,
Glendale, CA general
purpose
Ceramic Cements
XIII 1 F Utratemp 1 part Ziroconia Clear Aremco Prod. Inc. H.T. (1100°F,
516 New York City, NY 593°C)
Page 6009
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
C G
T Typical
L R
Y Users,
A A
P Product Cured Applications,
S D
E Designation Description Color Name and Address Remarks
S E
Page 6010
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
(a) Remove any excess epoxy from reinforcing operation by sanding smooth and
level.
(b) Clean repaired surface with Isopropyl Alcohol. Refer to CLEANING, Table
4002 for acceptable cleaning solvents.
(c) Fill any surface irregularities with catalyzed polyester resin filler. Catalyze only
the amount which will be immediately used since the material will begin to
harden within five minutes. An automotive body repair surfacing putty may be
used as an alternate fill material.
(d) Level fill with spatula or putty knife before filler hardens and restore texture by
stippling with a stiff-bristled brush. Texture match is achieved through trial and
error.
(e) After filler has fully hardened (10 to 15 minutes), sand area lightly to blend
repair into adjacent areas.
(8) Paint shroud using standard procedures with color matching touch-up paint. Cure
painted coating as required.
(9) Install shroud on substructure using a contact adhesive in areas where originally
adhered as follows:
(b) Allow solvents to escape from adhesive before closing assembly. Assembly is
ready to close when adhesive is almost dry with a slight tack remaining.
C. Bonding.
(1) Decals which have been removed are not repairable. To replace with a new decal,
dampen a clean, lint-free cloth in alcohol. Clean mating surfaces of dirt, grit and old
adhesive. Replace with new decal using adhesive #468 (3M). On decals too thin to
use additional adhesive, just use the preapplied adhesive.
(2) To remove grommets, pads and panels cemented to structure, apply Toluene to
edges of adhesive to soften adhesive, then pry the part free from structure. Prior to
installing new grommets, pads, or panels to structure, sand surface to remove all
traces of scale, dirt, oxides, oils and old adhesive, then wipe with a clean cloth
dampened in Aliphatic Naphtha. To cement grommets, pads and panels, apply a
coat of adhesive to both surfaces with a clean, lint-free cloth which is slightly
dampened with Toluene. Immediately press both surfaces together and allow to air-
dry for 24 hours.
Page 6011
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
(3) Rubber, metal, plastic, plastic with abrasive metal surfaces, fiberglass, fiberglass
sections and fiberglass-reinforced honeycomb panels must be clean, dry and free
from paint, rust, oil, grease or wax before bonding. Clean surfaces by sanding (240
grit) followed by wiping with alcohol or an aliphatic solvent, such as mineral spirits,
heptane or hexane.
(4) Mix Scotch-Weld No. 2216A (accelerator) with Scotch-Weld No. 2261B (base) by
weight 7 parts A to 5 parts B or by volume 3 parts A to 2 parts B.
(5) Mix components thoroughly, color should be a uniform grey. Use within one hour at
normal temperature.
(6) For maximum bond strength, apply Scotch-Weld No. 2216 A/B adhesive evenly to
both surfaces to be joined. Adhesive may be applied with brush, spatula, trowel or
air-powered sealant gun.
(7) Join the adhesive-coated surfaces and allow to cure at 65ºF or above. To keep
parts from moving during cure, contact pressure is necessary.
(8) Clean excessive adhesive from parts and equipment with an aliphatic solvent.
(9) To remove grommets, pads and panels cemented to a metal structure, apply
toluene to edges of adhesive to soften adhesive, then pry the parts free from the
structure. Prior to installing new grommets, pads or panels to structure, sand
surfaces to remove all traces of scale, dirt, oxides, oils and old adhesive. Wipe with
a clean cloth dampened with an aliphatic solvent.
(10) To cement grommets, pads, and panels, apply a coat of Scotch-Weld No. 2216
B/A adhesive in the same method as described in 2 and 3 above.
(11) Inspect bonded parts for intimate contact over full bonding area.
Page 6012
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
D. Rivets.
Permissible limitations on size of rivet holes, where rivets were drilled out on
disassembly, are controlled by standard shop-practice use of oversized replacement
rivets.
NOTE: The minimum pitch and edge distances for rivets are determined by the original
design and should be closely observed during repair.
E. Welding.
(1) To replace damaged spot-welded or tack-welded parts, cut away spot or tack in the
damaged part by spot-facing.
F. Threaded Parts.
(1) Use thread chaser or tap to repair stripped or damaged threaded parts.
G. Powder Coating.
WARNING: Conduct powder coating in well-ventilated area equipped to remove fumes and
dust from the surrounding work area. If finishes or solvents spatter into eyes,
flush with water for 15 minutes and get medical attention immediately.
NOTE: Powder coating should be done in a certified workshop with expertise in this
field.
Remove any kind of soil, grease and oil from minor nicks and scratches on powder
coated surfaces by scrubbing with Spray White E. Apply 6222-921 1 powder so the
finished product is 2-4 mm thick and bake at 400°F for 15 minutes.
Repair of minor dents and deformation of frame may be accomplished with standard
metal repair tools. An anodic coating for aluminum and zinc chromate coating for steel
will be required if the protective finish of the metal has been removed during repairs.
(1) Soak strip of Velcro tape (cemented to structure) with a commercial grade of
acetone. Peel off from any side corner.
Page 6013
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
(3) Coat metal and new Velcro tape with EC1350 or EC1099 cement or equivalent and
allow to air-dry until tacky. Press Joint of coated metal surface and new tape
together and hold briefly to ensure complete contact through entire length of tape.
J. Upholstery.
(1) Stitch dress cover open seams with 16 oz. bonded nylon (colored to match fabric)
and suitable needle.
(2) Stitch fireblocking cover open seams with spun Kevlar thread size T50 and suitable
needle.
K. Lubrication.
Lubrication reduces wear and friction between moving parts to insure proper function
and extended service life. Lubricants also provide for ease of assembly of interference
fit parts, such as bushings, pins, etc.
(1) Super Lube 41150 is the qualified lubricant to be applied to two piece sliding food
tables.
(3) If the area where the lubricant is to be applied requires cleaning, wipe down the
area with solvent cleaning procedures (See Table 4002). Apply grease to one or
both surfaces, as required, before assembling parts, especially those involving an
interference or press fit.
Page 6014
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
ASSEMBLY
1. General
A. During assembly, always use new low-cost items, such as cotter pins, screws, washers,
nuts, grommets, tie-straps, etc., when possible to prevent future maintenance
requirements due to failure of these items. Prior to initiating assembly procedures,
inspect all parts for wear and/or damage which could result in failure of the seat
assembly or any of its component assemblies.
B. Refer to Figure 7001 for a typical installation of the seat recline control buttons. The
items shown are furnished with the cable/control assembly and may vary slightly
depending upon particular part usage and manufacture; however the installation
procedure shown is generally representative.
NOTE: Ensure that all bottom cushions are installed correctly. Cushions must be held
at an angle with the aft portion placed under the back cushion assembly, then
gently lower and push forward end of bottom cushion down into place
(bottomed on front tube assembly).
EXISTING HOLE
IN ARMREST
STRUCTURE
ACTUATOR WAVE
BUTTON WASHER
ESCUTCHEON
Page 7001
25-27-39 Feb 15/06
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Epoxy W135 A/B Epoxies & Urethanes, Inc Filling of table shells voids
2406 Ludelle
Fort Worth, Texas
Page 7002
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Velcro tape (hook) (cut V200-1-(80)-100 Hartwell Corp. Applied to frame to mate
to upholstery length) 900 S. Richfield Rd. with tapes on cushions
(adhesive backed) Placentia, CA 92670
Grommet (cut to MS212661N Any approved source Protects IFE and recline
length) control cables
Page 7003
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
2. Assembly Procedures
NOTE: Refer to Table 7001 for applicable tape/pile application. The velcro tapes/piles
secure IFE and recline cables and are normally secured to base frame with a rivet
and a washer to fit.
(1) Install adapter (120, 125), strut (65) and base (5) using applicable attaching parts.
(1) Install support (120, 120A), bracket (85), link assembly (60), upper spreader (30
thru 35) and pin (10) using applicable attaching parts.
(1) Install adapter (140, 145), support (100, 100A), bracket (65), link assembly (45)
and pin (25) using applicable attaching parts.
(1) Install support (95, 95A), bracket (55), link assembly (40) and pin (20) using
applicable attaching parts.
(1) Install strut (65) and base (5) using applicable attaching parts.
(1) Install track (95), knuckle (85, 85A), slide (65), paddle (45, 45A), link (25 and finger
lift (15, 15A) using applicable attaching parts.
(1) Install recline cable (65, 65A), lower hinge (55), bracket (15) and armcap (5) using
applicable attaching parts.
Page 7004
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
(1) Replace velcro (110 thru 130) as required. Install arm assembly (70, 70A) and
spring (40, 40A) using applicable attaching parts.
(1) Install table legs (10, 15) and secure using applicable attaching parts.
(1) Install table latch (5) and secure with applicable attaching parts.
M. Model 5600 Tourist Class Standard/Handicap/Exit Triple Seat Assembly. (See IPL
Figure 2)
(1) Refer to ASSEMBLY paragraph 2.L for instructions pertaining to food table latch
(75, 75A), 2.K for back-mounted food table (85), 2.J for back structure (115 thru
115H), 2.B armrest (155, 155A, 210 thru 210C, 265 thru 265C), 2.F for leg (370 thru
375B), 2.E for aisle spreader (435 thru 435C), 2.D for center spreader (440 thru
440F) and 2.C for outboard spreader (445 thru 445E).
(2) Following assembly of upholstered items and dress covers, carefully “dress” seat
to ensure proper fit. Refer to FITS AND CLEARANCES section for final
adjustments.
NOTE Attach life vest pouch assembly (35) to velcro (450) located on front
stretcher tube. Secure using straps (40).
N. Model 5600 Tourist Class IAT Triple Seat Assembly. (See IPL Figure 1)
(1) Refer to ASSEMBLY paragraph 2.L for instructions pertaining to food table latch
(75, 75A), 2.K for back-mounted food table (85), 2.J for back structure (115 thru
115C), 2.I armrest (155, 155A), 2.H for IAT module (250 thru 250C), 2.G in-arm
food table (265, 265A), 2.F for leg (370), 2.E for aisle spreader (435, 435A), 2.D for
center spreader (440, 440A) and 2.C for outboard spreader (445, 445A).
(2) Following assembly of upholstered items and dress covers, carefully “dress” seat
to ensure proper fit. Refer to FITS AND CLEARANCES section for final
adjustments.
NOTE Attach life vest pouch assembly (35) to velcro (450) located on front
stretcher tube. Secure using straps (40).
Page 7005
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
3. Storage Procedures
A. General.
B. Procedures.
(1) Wrap seat assembly in waterproof wrapping paper (Federal Specification UU-P-
271) or equivalent, or a plastic cover. Use tape (Federal Specification JAN-P-127)
or equivalent, to secure wrapping paper or cover.
(2) Identify seat assembly part number and date of overhaul on a tag, or in a
convenient location on the seat assembly wrapper.
(3) Store seat assembly (long term) in cool, dry place, away from sunlight and heat
source at a temperature range from 4°C to 32°C (40° to 90°F). The relative
humidity should not exceed 50%. These temperature-humidity conditions meet
requirements of RTCA/DO-160D (Environmental Conditions and Test Procedures
for Airborne Equipment) to protect any sensitive electronic equipment, and reduce
any possible corrosion of metal parts and mildewing of upholstery materials.
Page 7006
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Fits and clearances for the seat assemblies are given in this section.
2. Adjustment Procedures
The setscrews located at each arm of the table assembly are provided for
adjustment of the top surface of the table assembly with respect to the aircraft floor.
To attain the desired height of 25.6 inches, adjust the setscrew (5, IPL Fig. 4)
accordingly.
(2) Surface Leveling of Table Assembly
Leveling the surface of the table can be done by adjusting two setscrews located
at both arms of the table. Alternating the adjustment of the top (25, IPL Fig. 4) and
bottom (20, IPL Fig. 4) setscrews will allow the desired leveling of the surface.
.
(2° 30’)
(25.6)
Page 8001
25-27-39 Feb 15/06
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
NOTE: Ensure that seat back and recline lock are attached correctly to seat frame
assembly, seat back, trunnion assembly and recline control assembly prior to
initiating adjustment procedure.
(1) Install one recline lock attaching nut and one washer on the rod end of recline lock.
(2) Position rod end of recline lock thru bearing (eyebolt). Install second recline lock
attaching nut and washer.
(3) Adjust recline lock attaching nuts so that seat back lines up at dimensions of seat
dimension figure, Figure 1. Tighten nuts against eyebolt assembly to maintain this
setting.
(4) Attach control assembly to recline lock using clip (4). Slide clip to fully engage
recline lock.
(5) Depress recline control button to allow seat back to travel to its fully reclined
position. This recline travel should be in accordance with dimensions of seat
dimension figure, Figure 1. If depressing button does not actuate recline lock,
adjust setscrew (2) as necessary. If locks do not provide desired recline travel,
adjust as follows:
(6) Adjust recline lock by sliding dust cover back and adjusting to desired stop (Figure
8002). Replace dust cover. Refer to seat dimension figure (Fig. 1 of DESCRIPTION
AND OPERATION section) for required dimensions.
(7) Verify proper adjustment by depressing recline control push button flush with
surface of escutcheon. The recline lock must unlock and allow free movement of
the seat back to its desired recline position. Release of recline control button shall
“lock” seat at any intermediate position. Repeat procedures (1) thru (6) as required.
Page 8002
25-27-39 Feb 15/06
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
SUPPORT
QUADRANT
RECLINE LOCK
COVER
RECLINE
LOCK PIN
BOLT
LOCK NUT
AND WASHERS
2
5 1. ACTUATOR ARM
2. SETSCREW
3. CABLE
4. CLIP
3 5. LOCK MOUNT
Page 8003
25-27-39 Feb 15/06
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
(1) In order to set lock stroke limits, extend unit in direction shown from recline arm to
eyebolt location.
(2) After moving lock into position, slide cover down over spring in direction shown to
expose stop.
(3) After stroke limits have been set on lock, reposition stop as required with cover and
retainer being repositioned to protect lock settings to ensure proper adjustment.
Page 8004
25-27-39 Feb 15/06
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
NOTE: Installation torque values for both the shear pin assembly and the anti-rattle
assembly is 45 ± 10 In./Lbs. maximum.
(1) Prior to installation, verify that both the shear pin assembly (45, IPL Fig. 9) and the
anti-rattle assembly (50, IPL Fig. 9), have been lifted out of, and are protruding
from, the base assembly (5, IPL Fig. 9) as indicated in figure 8005. This condition
will allow the seat to slide freely in the aircraft track.
(2) Locate the seat at the desired station number. The shear pin should be torqued
down into the aircraft track. Visually inspect the shear pin assembly to insure it is
fully engaged with the aircraft track.
(3) Torque down the anti-rattle assembly and again visually inspect.
ANTI-RATTLE
PIN ASSEMBLY
SHEAR PIN
ASSEMBLY
TOP OF TRACK
STUDS (65, IPL FIG. 11)
18.0
(REF)
Page 8005
25-27-39 Feb 15/06
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
(1) The In-arm food table should fold flat across the seat, touching the tray tab onto the
module. Adjust screw (90, IPL Fig. 8) on knuckle (85, 85A, IPL Fig. 8) to allow for
3° of rotation.
(2) Adjust the table by using an Allen wrench to turn the screw lock (see inset) in the
desired direction to achieve correct leveling so that the table lies flat across the seat
place.
TABLE LEAF
KNUCKLE
SCREW
LOCK
(92, IPL FIG. 8)
SPACER
(91, IPL FIG. 8)
SCREW
(REF 92,
IPL FIG. 8)
RING
(93, IPL FIG. 8)
(1) Cable tie straps can be no more than 8 inches apart, Weber places them between
2 and 6 inches apart.
• Large cable tie straps are used for securing to structural components.
• Small cable tie straps are used for securing to all other components.
(2) Cable tie straps must not be overtightened. If using a strap gun, set the tension on
the gun before use so that the strap will be snug but not overtighten.
Page 8006
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
(4) Trim excess tongue as close to head as possible with a maximum .050” excess
allowed using strap cutting tool.
(5) The tie head must be located so it will not scuff, damage, injure or be in view of the
passenger.
3. Tolerances
A. Wiring.
(a) Seat to seat and video coaxial cables can be no less than six (6) times the
diameter of the cable.
(b) All other cables and harnesses may vary between three (3) to six (6) times the
diameter of the cable.
(a) IFE and power cables are not allowed to run together, however, they may
cross.
A crease in the material caused by bending the material sharply. These “marks”
have been otherwise known as “finger nail marks” and “eyebrows”.
(2) Ding. (See Figure 8006)
A mark or an indentation of small size, typically less than .010" in diameter, and no
deeper than 10% of the material thickness.
(3) Scratch. (See Figure 8006)
Page 8007
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
A measurable defect is defined as a defect such as a scratch or dent, etc. that can
be measured with the use of any precision measuring device.
(6) Superficial Scratch.
(2) Play.
• Backs - .9” total forward and aft movement at the top of the back
(3) Noise.
(a) Sound produced by the normal operation of the seat which exceeds 65
decibels when measured at a distance of 3 feet is considered unacceptable.
(b) If the seat has multiple features that pivot (armrest, food tables), the operation
of these features is to be free of squeaks when measured at a distance of 3
feet.
Page 8008
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Page 8009
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
A. General.
(1) Minimum edge distance of bolt and screw holes shall be two bolt diameters
plus.030 inch unless a smaller distance is noted.
(2) Drill and reamed holes for bolts and screws shall meet the finish and tolerance
requirements.
(3) Areas that are prepared for fasteners after final protective finish has been applied
shall be refinished or touched up in accordance with applicable finish specification.
Painted coatings shall be touched up in accordance with drawing call-outs for
adjacent areas. (Refer to REPAIR)
(4) Lubrication, other than that applied by the manufacturer shall not be used on
fasteners.
(5) The number and type of washers under the bolt heads shall be as specified on the
engineering drawing or CMM. If unspecified, the maximum number shall be two.
(6) Where bolt head orientation is unspecified, the installation shall be with head up,
where practical and in conformance with appearance and safety requirements, to
minimize chanced of loss of bolt in case nut is loosened.
(8) Certified torque wrenches shall be used for torquing of fastener to a value
specified.
(9) Installed nuts, bolts, screws, washers and cotter pins shall be free of burrs and
sharp edges which may cause damage or injury to personnel.
(11) When necessary to protect the surface finish of adjacent structure from damage
when tightening, one standard washer shall be used, either under the nut or bolt
head, whichever is being turned.
(12) Standard spacer washers may be added under the nut to adjust grip length. A
maximum of 2 washers meeting the requirements of may be used.
(13) When washers are required and not specified, the material shall be similar to that
of the material against which the washer will bear to avoid galvanic (dissimilar
metal) corrosion. Some examples are: aluminum against aluminum, cadmium
plated steel against cadmium plated steel (or aluminum) and stainless steel against
stainless steel.
Page 8010
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
(14) Length of bolts and screws shall be such that the nut shall not bottom out on the
last thread of the bolt shank, and bolt protrusion through nut shall be in accordance
with Table 8001.
(15) For sheets and/or fittings having a combined thickness of less than .094 inch, no
threads shall be within the surfaces of the parts being bolted.
(16) In thickness greater than .094 inch, two threads including the thread run out are
allowed within the surfaces being bolted.
NOTE Torque limits listed in Table 8001 are for clean, non-lubricated bolts and
nuts and to nuts lubricated by the manufacturer.
B. Cotter Pins.
(2) There are two methods for cottering castellated nuts, Figure 8007 shows the
preferred method and the optional method which may be used where injury to
personnel, clothing, or interference with equipment are considerations. In either
case, the in shall be installed with the head parallel to the slot in the nut.
C. Gap Tolerances.
(1) Gaps between fastener heads, nuts or washers and surfaces being fastened shall
be subject to the following controls:
(a) The gap shall not exceed 0.004 inch between the bolt head and the surface
provided no more than 40% of the head periphery has a gap.
(b) A 0.004 inch feeler gauge shall not contain the shank of bolt or screw when
used for checking.
(c) Allowable gap for installed nut shall be per Table 8002 provided no more than
40% of nut base periphery has a gap.
(2) When dimples or countersinks are used, bolt or screw heads shall seat firmly in the
dimples or countersinks. Gaps under the head which will permit the insertion of a
.005 inch feeler gauge to the shank are unacceptable, however, gaps which permit
the insertion of a .004 inch feeler gauge to the shank are acceptable provided no
more than 40% of the circumference has such a gap.
D. Self-Locking Nuts.
(1) Self locking nuts may not be reused unless they meet the breakaway torque
requirements listed in Table 8003.
Page 8011
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Bolt Strength 125,000 PSI Min. 125,000 PSI Min. 160,000 PSI Min. 62,000 PSI Min. 220,000 PSI Min.
Thread Size Range Max.* Range Max.* Range Range Max.* Range
1 3/8-12 7000-
9000
1 1/2-12 10000-
12000
* Maximum torque allowed for alignment of nut and hole for cotter pin or other safety device insertion
Page 8012
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
PREFERRED OPTIONAL
METHOD METHOD
Gap Tolerances
Table 8002
1/4 0.005
5/16 0.006
3/8 0.007
7/16 0.008
1/2 0.009
9/16 0.010
5/8 0.011
3/4 0.012
Page 8013
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Gap Tolerances
Table 8002 (Continued)
7/8 0.013
1 0.015
1 1/8 0.017
1 1/4 0.019
8/32 1.5
10-32 2.0
1/4-28 3.5
5/16-24 6.5
3/8-24 9.5
7/16-20 14.0
1/2-20 18.0
9/16-18 24.0
5/8-18 32.0
3/4-16 50.0
7/8-14 70.0
1-14 92.0
1 1/8-13 117.0
Page 8014
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
A. The following tools and equipment are required to perform the procedures detailed in
this maintenance manual. There are no other special fixtures, tools, test, or support
equipment required to perform maintenance procedures.
B. The Sharp Edge Tester Model SET-50 will be utilized to provide an objective means for
judging the sharpness of an edge on the seat assembly. (See Figure 9001)
(1) Slide the Tape Cap all the way on to the pressure head of the Sharp Edge Tester
with the black center guide line and the uncovered portion of the red plastic cap
facing up.
(2) Position the tape covered pressure head on the edge of the item to be checked for
sharpness. Holding the clam shell base in your hand, press down on the tape
covered head until the arm and the tool form a straight line.
(3) Move the pressure head two inches along the edge and then back again to the
starting point. Then withdraw the tool from the edge. The total distance of
engagement between the edge and the tape-covered head is therefore 4 inches.
(4) Examine the tape cap to determine whether or not penetration has occurred
through the two-sensing layers. If penetration has occurred, the black indicating
tape will be visible through the resulting cut. The application of the Sharp Edge
Tester to an edge with acceptable sharpness will not result in the cutting through
the two outer layers of the sensing tape.
Page 9001
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Page 9002
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
C. The recommended consumables for the seat assembly are given in Table 9002.
Consumables
Table 9002 (Sheet 1 of 4)
Page 9003
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Consumables
Table 9002 (Sheet 2 of 4)
Page 9004
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Consumables
Table 9002 (Sheet 3 of 4)
Page 9005
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Consumables
Table 9002 (Sheet 4 of 4)
Page 9006
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
This section lists, describes, and illustrates all component assemblies, subassemblies, and
parts required for maintenance of the seat assembly.
2. Scope of Information
A. General
Each assembly is listed and immediately followed by a listing of its detail parts. The
listing is indentured to show the relationship between each part and its next higher
assembly. Item numbers in the parts list correspond to the item numbers of the
accompanying illustration (figure).
(1) When the part number is known: Find the part number in the numerical index and
note the figure and item number. Find the item number in the applicable parts list
and illustration to get the necessary information. The search function on the
interactive (electronic) version of this manual can also be used to locate the known
part number.
(2) When the part number is not known: Review the illustrations to identify the part by
physical appearance and location. Refer to the accompanying parts list to get the
part number, nomenclature, effectivity, and quantity.
(3) The effectivity code shows the part usage relative to the next higher assembly.
When the EFFECTIVITY CODE column is blank, the part usage applies to all next-
higher-assembly versions unless otherwise specified in the NOMENCLATURE
column.
The Equipment Designator Index (if applicable) is an aid to find the parts in the Detail Parts
List by equipment designator. The equipment designator, the part number, the figure number,
and the item number are given for each entry.
The equipment designator are sorted one character at a time, from left to right. The correct
sequence is (1) dash, (2) letters A through Z, and (3) numerals 0 through 9.
4. Numerical Index
The Numerical Index is an aid to find parts in the Detail Parts List by part number. The figure
number, the item number, and the total quantity required are given for each entry.
The part numbers are sorted one character at a time, from left to right. The correct sequence
is (1) dash, (2) letters A through Z, and (3) numerals 0 through 9.
Page 10001
25-27-39 Feb 15/06
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
The Detail Parts List is arranged in general sequence of disassembly. The parts are
illustrated in an exploded-view illustration and listed in the related parts list.
(1) The first number at the top of each FIG. ITEM column is the figure number of the
exploded-view illustration. The number given opposite each part number is the item
number assigned to the part in the illustration.
(2) A dash (-) in front of an item number means the part is not illustrated.
(3) Alpha-variants A through Z (except I and O) are assigned to item numbers when
necessary to identify added parts, alternate parts, and parts modified by service
bulletins.
This column gives the part number of the manufacturer for each part, as modified to
meet the requirements of ATA 200/2000. The modifications can include:
(1) Removal of blank spaces and special characters, with the possible exception of
dashes. Dashes are permitted only between numeric characters.
(2) Insertion of a reference part number compatible with ATA 200/2000 if the part
number is longer than 15 characters. In these cases, the full part number is given
in the NOMENCLATURE column.
C. INDENTure Column
The indenture column is used to show the relationship of one part to another as found
on the original engineering drawings. A typical indenture relationship is as follows:
Page 10002
25-27-39 Feb 15/06
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
D. NOMENCLATURE Column
(1) This column contains descriptive nomenclature for each part, and can also give the
CAGE code of the manufacturer (if the part is not made by Weber Aircraft LLC), the
part number (if it is longer than 15 digits or modified to ATA 200/2000), any service
bulletin that affect the part, and any obsolete part numbers. The column also
provides figure references for NHA and details, and additional descriptive
information as required.
(3) The terms defined below are used when applicable to indicate the
interchangeability of parts.
This column contains effectivity codes (A, B, etc.) to indicate the alternate models or
configurations of the end items to which the parts apply. This column is left blank when
the parts apply to all models or configurations in the parts list.
Page 10003
25-27-39 Sep 15/09
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
The quantity shown in this column is the units required for one next higher assembly
(NHA). The abbreviation RF (reference) means the end item or assembly is shown
completely assembled in the figure referenced in the NOMENCLATURE column.
The CAGE codes for the manufacturers of the parts, special tools, test equipment, and
materials referenced in the manual are given below. The five digit code is preceded by the
letter V. The codes are taken from Cataloging Handbook H4/H8. No code in the
NOMENCLATURE column means the part is made by Weber Aircraft LLC.
Page 10004
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
NUMERICAL INDEX
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10005
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10006
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10007
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10008
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10009
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
NAS1191E08P4L SCREW 8 50 1
NAS1351-3-14P SCREW 10 25 1
NAS1351-3-14P SCREW 11 30 1
NAS1351-3-14P SCREW 12 15 1
NAS1351-3-8P SCREW 10 5 1
NAS1351-3-8P SCREW 11 5 1
NAS1515H3L WASHER 1 405 2
R NAS1515H3L WASHER 1A 405 2
NAS1515H3L WASHER 2 405 2
R NAS1515H3L WASHER 2A 405 2
NAS1515H6H WASHER 4 30 2
NAS43DD4-10 SPACER 10 85 1
NAS43DD4-10 SPACER 11 95 2
NAS43DD4-10 SPACER 11 95A 1
NAS43DD4-25 SPACER 11 95B 1
NAS43HT4-14 SPACER 10 75 1
NAS43HT4-14 SPACER 11 85 1
NAS43HT4-14 SPACER 12 105 1
NAS514P1032-10 SCREW 8 5 2
NAS514P1032-4 SCREW 8 105 3
NAS514P1032-5 SCREW 8 70 2
NAS514P632-6 SCREW 8 20 2
NAS514P632-7 SCREW 1 140 2
R NAS514P632-8 SCREW 1A 246A 4
NAS514P832-10 SCREW 1 225 2
NAS514P832-10 SCREW 1 235 2
R NAS514P832-10 SCREW 1A 225 2
R NAS514P832-10 SCREW 1A 235 2
NAS514P832-4 SCREW 7 10 4
NAS514P832-4 SCREW 7 20 4
NAS514P832-4 SCREW 7 60 4
NAS514P832-8P SCREW 1 80 2
R NAS514P832-8P SCREW 1A 80 2
NAS514P832-8P SCREW 2 80 2
R NAS514P832-8P SCREW 2A 80 2
R NAS517-3-17 SCREW 8 90 1
NAS517-3-2 SCREW 1 395 2
R NAS517-3-2 SCREW 1A 395 2
Page 10010
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10011
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10012
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10013
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10014
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10015
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10016
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10017
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10018
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10019
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10020
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10021
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10022
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
R 854683-001 DELETED 13 60 D
R 854683-007 SPACER, RECL BUTTON 13 60A 1
854684-001 INSERT 1 175 2
R 854684-001 INSERT 1A 175 2
854684-001 INSERT 2 175 2
854684-001 INSERT 2 230 2
854684-001 INSERT 2 280 2
R 854684-001 INSERT 2A 175 2
R 854684-001 INSERT 2A 230 2
R 854684-001 INSERT 2A 280 2
R 854685-005 PLATE, RJU 1A 135 1
R 854685-005 PLATE, RJU 2A 135 3
R 854685-005 PLATE, RJU 2A 135A 3
854686-001 PIN, HDCP PIVOT 1 180 1
R 854686-001 PIN, HDCP PIVOT 1A 180 1
854686-001 PIN, HDCP PIVOT 2 180 1
R 854686-001 PIN, HDCP PIVOT 2A 180 1
854686-001 PIN-LOCK 13 40 1
854687-405 BACK STRUCTURE AY 2 115E 1
854687-405 BACK STRUCTURE AY 2 115H 2
R 854687-405 BACK STRUCTURE AY 2A 115E 1
R 854687-405 BACK STRUCTURE AY 2A 115H 2
854687-405 BACK STRUCTURE AY 5 1 1
854687-406 BACK STRUCTURE AY 2 115F 2
854687-406 BACK STRUCTURE AY 2 115G 1
R 854687-406 BACK STRUCTURE AY 2A 115F 2
R 854687-406 BACK STRUCTURE AY 2A 115G 1
854687-406 BACK STRUCTURE AY 5 1A 1
854687-407 BACK STRUCTURE AY 1 115 1
854687-407 BACK STRUCTURE AY 1 115C 2
R 854687-407 BACK STRUCTURE AY 1A 115 1
R 854687-407 BACK STRUCTURE AY 1A 115C 2
854687-407 BACK STRUCTURE AY 2 115 1
854687-407 BACK STRUCTURE AY 2 115C 2
R 854687-407 BACK STRUCTURE AY 2A 115 1
R 854687-407 BACK STRUCTURE AY 2A 115C 2
854687-407 BACK STRUCTURE AY 5 1B 1
854687-408 BACK STRUCTURE AY 1 115A 2
854687-408 BACK STRUCTURE AY 1 115B 1
Page 10023
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10024
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10025
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10026
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10027
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10028
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10029
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10030
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10031
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
855109-402 SEAT AY 2 2J 1
R 855109-411 SEAT AY 2A 2H 1
R 855109-412 SEAT AY 2A 2J 1
R 855160-001A LINK 8 41 2
855164-001 WASHER-PLASTIC 8 35 4
855165-001 PIN, FOOD TABLE, IAT 8 115 1
R 855625-001 BRACKET, SEB SUPPORT 1A 485 1
R 855625-001 BRACKET, SEB SUPPORT 2A 495 1
R 855649-401 IFE INSTL 1A 555 1
R 855649-401 IFE INSTL 15 1 RF
R 855649-402 IFE INSTL 1A 555A 1
R 855649-402 IFE INSTL 15 1A RF
R 855649-403 IFE INSTL 2A 565 1
R 855649-403 IFE INSTL 15 1B RF
R 855649-404 IFE INSTL 2A 565A 1
R 855649-404 IFE INSTL 15 1C RF
R 855649-405 IFE INSTL 2A 565D 1
R 855649-405 IFE INSTL 15 1D RF
R 855649-406 IFE INSTL 2A 565E 1
R 855649-406 IFE INSTL 15 1E RF
R 855649-419 IFE INSTL 2A 565B 1
R 855649-419 IFE INSTL 15 1F RF
R 855649-420 IFE INSTL 2A 565C 1
R 855649-420 IFE INSTL 15 1G RF
R 855649-425 IFE INSTL 2A 565F 1
R 855649-425 IFE INSTL 15 1H RF
R 855649-426 IFE INSTL 2A 565G 1
R 855649-426 IFE INSTL 15 1J RF
856258-201G DRESS COVER AY 1 95 1
R 856258-201G DRESS COVER AY 1A 95 1
856258-201G DRESS COVER AY 2 95 1
R 856258-201G DRESS COVER AY 2A 95 1
856258-203N DRESS COVER AY 2 95A 1
R 856258-203N DRESS COVER AY 2A 95B 1
856258-211F DRESS COVER AY 1 100 1
R 856258-211F DRESS COVER AY 1A 100 1
856258-211F DRESS COVER AY 2 100 1
R 856258-211F DRESS COVER AY 2A 100 1
856258-213M DRESS COVER AY 2 100A 1
Page 10032
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10033
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10034
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10035
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
AIRLINE
IPL TOTAL
PART NUMBER PART NOMENCLATURE ITEM
FIGURE REQ
NUMBER
Page 10036
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
75
115A
135
95
105
80 140
90°ROTATED
115A 155
115 D
145
460
460A
250B
150
255A 250B
260
85
100 E
25
250 265
LL
PU 35
220
270 255
260
300
360
PU
LL
365
F
245
PU
LL
A 240
(CTR 235
340 15 ONLY)
241
20
859628-401 SHOWN
Page 10037
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
A B
C
440
45
B
385
3 PLACES C 445
440
450
C (1 PIECE)
B
435
380
46
40 455
430
370
425
420
40
450
30 30A 35 370
(REF)
B AISLE (SHOWN)
OUTBD (OPPOSITE VIEW)
(AISLE) 115
(OUTBD) 115A
(REF)
85
(REF) 120
125
Page 10038
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
C CTR
120
115A (CTR)
(REF) 85
(REF) 115A (CTR)
125 (REF)
125
85 70
(REF)
68 440
120 (REF)
60
50
65 55
D OUTBD E OUTBD
170
155 165
(REF)
165 445
(REF)
160
295
290 415
405
175 415
280 395
315
290A
285
175 310
185
180 ROTATED 90°
405
310
305 300 395
(REF)
Page 10039
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
435
(REF)
190
195
200 410
400
195
400
390
215
210
215
385
(REF)
195
205
400 215
390 380
(REF) 320
330
355 325
350
340
(REF)
350
345
Page 10040
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
1
–1 859910-401 0 SEAT AY, MODEL 5600, T/C LH IAT A RF
TPL, NO ASH RECEIVER
–1A 859910-402 0 SEAT AY, MODEL 5600, T/C RH B RF
IAT TPL, NO ASH RECEIVER
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
1
R 75 854745-409A 2 LATCH AY, FOOD TABLE A 3
R –75A 854745-410A 2 LATCH AY, FOOD TABLE B 3
ATTACHING PARTS
80 NAS514P832-8P 2 SCREW 2
---*---
85 854710-407B 2 TABLE AY, FOOD (BACK 3
MOUNTED) (SEE IPL FIG. 4 FOR
DETS)
–90 854605-437 2 CUSHION AY, BACK 3
95 856258-201G 3 DRESS COVER AY 1
100 856258-211F 3 DRESS COVER AY (LIT POCKET) 1
R 105 851708-401 3 DELETED (SUPSD BY ITEM 105A) D
R –105A 864212-401 3 CUSHION AY, BACK (FBLK) 1
(SUPSDS ITEM 105)
–110 NOT USED
115 854687-407 2 BACK AY (AISLE) (SEE IPL FIG. 5 A 1
FOR DETS)
115A 854687-408 2 BACK AY (CTR & OUTBD) A 2
(SEE IPL FIG. 5 FOR DETS)
–115B 854687-408 2 BACK AY (AISLE) (SEE IPL FIG. 5 B 1
FOR DETS)
–115C 854687-407 2 BACK AY (CTR & OUTBD) SEE IPL B 2
FIG. 5 FOR DETS)
ATTACHING PARTS
120 MS3215-4050 2 RING, RETAINING 2
125 854663-001 2 SPACER, TABLE LEG 2
---*---
–130 NOT USED
135 859032-401D 2 ESCUTCHEON AY (OUTBD) 1
ATTACHING PARTS
140 NAS514P632-7 2 SCREW 2
---*---
145 854676-401A 2 ARMCAP (OUTBD) 1
150 WA5335-500-101 2 PLUG (OUTBD) 1
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
1
155 856714-454C 2 ARMREST AY-5600 (OUTBD) A 1
(SEE IPL FIG. 6 FOR DETS)
–155A 856714-453C 2 ARMREST AY-5600 (OUTBD) B 1
(SEE IPL FIG. 6 FOR DETS)
ATTACHING PARTS
160 NAS6204-17 2 BOLT 1
165 NAS1149F0432P 2 WASHER 2
170 MS21042-4 2 NUT 1
175 854684-001 2 INSERT 2
---*---
180 854686-001 2 PIN, HDCP PIVOT (OUTBD) 1
ATTACHING PARTS
185 MS3215-4025 2 RING, RETAINING 1
---*---
190 854810-402A 2 BUMPER AY A 1
–190A 854810-401A 2 BUMPER AY B 1
ATTACHING PARTS
195 NAS602-10P 2 SCREW 3
---*---
200 854811-403A 2 STEP AY, ATTENDANT 1
ATTACHING PARTS
205 NAS602-10P 2 SCREW (FWD & CTR OF STEP) 2
210 NAS602-20P 2 SCREW (AFT OF STEP) 1
215 NAS1149FN832P 2 WASHER 3
---*---
220 854774-401A 2 ESCUTCHEON AY (AISLE) 1
ATTACHING PARTS
–225 NAS514P832-10 2 SCREW 2
---*---
–230 854773-401F 2 ESCUTCHEON AY (CTR) A 2
–230A 854773-402F 2 ESCUTCHEON AY (CTR) B 2
ATTACHING PARTS
235 NAS514P832-10 2 SCREW 2
---*---
240 854778-401G 3 SUPPORT AY 1
ATTACHING PARTS
241 NAS602-5P 3 SCREW 2
---*---
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
1
245 854774-403A 3 ESCUTCHEON AY (U/O 854773 1
-401)
–245A 854774-404A 3 ESCUTCHEON AY (U/O 854773 1
-402)
250 854760-416A 2 MODULE AY, IAT (AISLE) (SEE IPL A 1
FIG. 7 FOR DETS)
–250A 854760-415A 2 MODULE AY, IAT (AISLE) (SEE IPL B 1
FIG. 7 FOR DETS)
250B 854760-414A 2 MODULE AY, IAT (CTR) (SEE IPL A 2
FIG. 7 FOR DETS)
–250C 854760-413A 2 MODULE AY, IAT (CTR) (SEE IPL B 2
FIG. 7 FOR DETS)
ATTACHING PARTS
255 NAS6204-18 2 BOLT (FWD) 1
255A NAS6204-14 2 BOLT (AFT) 1
260 NAS1149F0432P 2 WASHER (1 FWD, 1 AFT) 2
---*---
265 854777-411B 2 TABLE AY, FOOD (IN-ARM) A 3
(SEE IPL FIG. 8 FOR DETS)
–265A 854777-412B 2 TABLE AY, FOOD (IN-ARM) B 3
(SEE IPL FIG. 8 FOR DETS)
ATTACHING PARTS
270 854779-001 2 PIN-IAT 1
---*---
–275 855021-401A 2 BASEFRAME AY A 1
–275A 855021-402A 2 BASEFRAME AY B 1
280 300050-003 3 BRACKET, BAGGAGE BAR 1
ATTACHING PARTS
285 NAS623-3-36 3 SCREW 1
290 NAS1149F0363P 3 WASHER (AFT) 1
290A NAS1149F0332P 3 WASHER (FWD) 1
295 22NKM02 3 NUT (V22599) 1
---*---
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
1
300 854813-003A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (OUTBD)
(U/O 855021-401)
–300A 854813-004A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (OUTBD)
(U/O 855021-402)
ATTACHING PARTS
305 NAS623-3-16 3 SCREW 1
310 NAS1149F0332P 3 WASHER 2
315 22NKM02 3 NUT 1
---*---
320 854817-001 3 TUBE, MOUNTING 1
ATTACHING PARTS
325 NAS602-12P 3 SCREW 1
330 NAS1149FN832P 3 WASHER 1
–335 NOT USED
---*---
340 854812-007A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (INBD)
(U/O 855021-401)
–340A 854812-008A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (INBD)
(U/O 855021-402)
ATTACHING PARTS
345 NAS623-2-8 3 SCREW 1
350 NAS1149FN816P 3 WASHER 2
355 22NKM82 3 NUT (V22599) 1
---*---
360 854814-001 3 INSERT, BAGGAGE BAR 1
ATTACHING PARTS
365 AD42BS 3 RIVET (V07707) 4
---*---
370 115010-005 3 LEG AY-MACHINED, STRAIGHT 2
(SEE IPL FIG. 9 FOR DETS)
–375 NOT USED
380 854940-449 3 TUBE AY (FWD) (U/O 855021 1
-401)
–380A 854940-450 3 TUBE AY (FWD) (U/O 855021 1
-402)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
1
385 854940-451 3 TUBE AY (AFT) (U/O 855021 1
-401)
–385A 854940-452 3 TUBE AY (AFT) (U/O 855021 1
-402)
ATTACHING PARTS
390 AN3-23A 3 BOLT (INBD) 2
395 NAS517-3-2 3 SCREW (OUTBD) 2
400 NAS1149F0332P 3 WASHER (INBD) (1 FWD, 2 AFT) 3
405 NAS1515H3L 3 WASHER (OUTBD) 2
410 MS21042-3 3 NUT (INBD) (AFT ONLY) 1
415 MS21042-3 3 NUT (OUTBD) 2
---*---
420 854752-401 3 DIAPHRAGM AY (AISLE) (RVT) 1
(U/O 855021-401)
–420A 854752-402 3 DIAPHRAGM AY (AISLE) (RVT) 1
(U/O 855021-402)
425 854752-726 3 DIAPHRAGM AY (CTR) (RVT) 1
(U/O 855021-401)
R –425A 854752-725 3 DIAPHRAGM AY (CTR) (RVT) 1
(U/O 855021-402)
430 854752-410 3 DIAPHRAGM AY (OUTBD) (RVT) 1
(U/O 855021-401)
–430A 854752-409 3 DIAPHRAGM AY (OUTBD) (RVT) 1
(U/O 855021-402)
435 854650-406A 3 SPREADER AY (AISLE) (SEE IPL 1
FIG. 10 FOR DETS) (U/O 855021
-401)
–435A 854650-405A 3 SPREADER AY (AISLE) (SEE IPL 1
FIG. 10 FOR DETS) (U/O 855021
-402)
440 854651-408A 3 SPREADER AY (CTR) (SEE IPL 2
FIG. 11 FOR DETS) (U/O 855021
-401)
–440A 854651-407A 3 SPREADER AY (CTR) (SEE IPL 2
FIG. 11 FOR DETS) (U/O 855021
-402)
445 854652-401A 3 SPREADER AY (OUTBD) (SEE IPL 1
FIG. 12 FOR DETS) (U/O 855021
-401)
–445A 854652-402A 3 SPREADER AY (OUTBD) (SEE IPL 1
FIG. 12 FOR DETS) (U/O 855021
-402)
450 WA9658-2000-102 2 VELCRO-HOOK AR
455 WA9659-2000-112 2 VELCRO-LOOP AR
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
1
460 854709-059A 2 PLACARD, SAFETY (USE SEAT 3
BOTTOM CUSHION FOR
FLOTATION)
460A 854709-061A 2 PLACARD, SAFETY (NO 3
SMOKING)
75
115
ROTATED 90°
95
115A
105 80
E
115A
220
460
F
250
D 85
100
15
20
340
35
40
25
G A
855101-411 SHOWN
360
365
300
Page 10048
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
A B 445
C
440
B
C
505
440 450
C
450 385
B (1 PIECE)
435
430
45A
450
40 (3 PL)
510B
45
380
370
3 PLACES
425
420
40
30 30A 35 370
(REF)
INBD (SHOWN)
B INBD (SHOWN)
CTR & OUTBD (OPP)
C CTR & OUTBD (OPP)
BACK AY
(REF)
BACK AY
(REF)
TABLE ARM
(REF)
125
120
TABLE ARM
70A
(REF)
70 (OPP)
125
120
65
60
50
(REF)
65
66
Page 10049
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
D OUTBD 145
160
130 180 165
155
135
140
165
170
175
150
(REF) 185 175
445
(REF)
295
290A 415
405
415
280 395
290 315
285
310
405
310
305 300
(REF) 395
Page 10050
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
435
(REF)
190
195
200 410
400
195
400
390
215
215 210
385
(REF)
195 205
400 215
390 380
320
(REF)
330
355 325
350
340
(REF) 350
345
Page 10051
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
F CTR
255A
265
260
245
240
270 246A
255 235
241
260
ROTATED FOR CLARITY
250B
246
248
247
249
480
G 475
525 490
510 480
515
475
505 195
475
470
475
470
535
540
470 475
550
510 545
515 370
(REF)
540
530
Page 10052
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
1A
R –1 863706-401 0 SEAT AY, MODEL 5600, T/C LH IAT A RF
TPL, NO ASH RECEIVER (POST
SB 863708-25-3298)
R –1A 863706-402 0 SEAT AY, MODEL 5600, T/C RH B RF
IAT TPL, NO ASH RECEIVER
(POST SB 863708-25-3298)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
1A
R 75 854745-409A 2 LATCH AY, FOOD TABLE A 3
R –75A 854745-410A 2 LATCH AY, FOOD TABLE B 3
ATTACHING PARTS
R 80 NAS514P832-8P 2 SCREW 2
---*---
R 85 854710-407B 2 TABLE AY, FOOD (BACK 3
MOUNTED) (SEE IPL FIG. 4 FOR
DETS)
R –90 854605-437 2 CUSHION AY, BACK 3
R 95 856258-201G 3 DRESS COVER AY 1
R 100 856258-211F 3 DRESS COVER AY (LIT POCKET) 1
R 105 864212-401 3 CUSHION AY, BACK (FBLK) 1
–110 NOT USED
R 115 854687-407 2 BACK STRUCTURE AY (AISLE) A 1
(SEE IPL FIG. 5 FOR DETS)
R 115A 854687-408 2 BACK STRUCTURE AY (CTR & A 2
OUTBD) (SEE IPL FIG. 5 FOR
DETS)
R –115B 854687-408 2 BACK STRUCTURE AY (AISLE) B 1
(SEE IPL FIG. 5 FOR DETS)
R –115C 854687-407 2 BACK STRUCTURE AY (CTR & B 2
OUTBD) SEE IPL FIG. 5 FOR
DETS)
ATTACHING PARTS
R 120 MS3215-4050 2 RING, RETAINING 2
R 125 854663-001 2 SPACER, TABLE LEG 2
---*---
R 130 854675-405A 2 ESCUTCHEON AY (OUTBD) 1
(ATTACHED WITH CAPTIVE
SCREW) (POST SB 863708-25-
3298)
R 135 854685-005 2 PLATE, RJU (OUTBD) (POST SB 1
863708-25-3298)
ATTACHING PARTS
R 140 NAS601-7P 2 SCREW 2
---*---
R 145 854676-401A 2 ARMCAP (OUTBD) 1
R 150 WA5335-500-101 2 PLUG (OUTBD) 1
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
1A
R 155 854670-401A 2 ARMREST AY-5600 (OUTBD) A 1
(SEE IPL FIG. 13 FOR DETS)
(POST SB 863708-25-3298)
R –155A 854670-402A 2 ARMREST AY-5600 (OUTBD) B 1
(SEE IPL FIG. 13 FOR DETS)
(POST SB 863708-25-3298)
ATTACHING PARTS
R 160 NAS6204-17 2 BOLT 1
R 165 NAS1149F0432P 2 WASHER 2
R 170 MS21042-4 2 NUT 1
R 175 854684-001 2 INSERT 2
---*---
R 180 854686-001 2 PIN, HDCP PIVOT (OUTBD) 1
ATTACHING PARTS
R 185 MS3215-4025 2 RING, RETAINING 1
---*---
R 190 854810-402A 2 BUMPER AY A 1
R –190A 854810-401A 2 BUMPER AY B 1
ATTACHING PARTS
R 195 NAS602-10P 2 SCREW 3
---*---
R 200 854811-403A 2 STEP AY, ATTENDANT 1
ATTACHING PARTS
R 205 NAS602-10P 2 SCREW (FWD & CTR OF STEP) 2
R 210 NAS602-20P 2 SCREW (AFT OF STEP) 1
R 215 NAS1149FN832P 2 WASHER 3
---*---
R 220 854774-401A 2 ESCUTCHEON AY (AISLE) 1
ATTACHING PARTS
R –225 NAS514P832-10 2 SCREW 2
---*---
R –230 854773-401F 2 ESCUTCHEON AY (CTR) A 2
R –230A 854773-402F 2 ESCUTCHEON AY (CTR) B 2
ATTACHING PARTS
R 235 NAS514P832-10 2 SCREW 2
---*---
R 240 854778-401G 3 SUPPORT AY 1
ATTACHING PARTS
R 241 NAS602-5P 3 SCREW 2
---*---
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
1A
R 245 854774-403A 3 ESCUTCHEON AY (U/O 854773 1
-401)
R –245A 854774-404A 3 ESCUTCHEON AY (U/O 854773 1
-402)
R 246 854771-401A 2 PLATE AY, CLOSEOUT (CTR 2
MODULES) (POST SB 863708
-25-3298)
ATTACHING PARTS
R 246A NAS514P632-8 2 SCREW 4
---*---
R 247 854769-001 2 BRACKET, RJU (CTR MODULES) 2
(POST SB 863708-25-3298)
ATTACHING PARTS
R 248 NAS601-7P 2 SCREW 2
R 249 NAS1149FN632P 2 WASHER 2
---*---
R 250 854760-414A 2 MODULE AY, IAT (AISLE) (SEE IPL A 1
FIG. 7 FOR DETS)
R –250A 854760-413A 2 MODULE AY, IAT (AISLE) (SEE IPL B 1
FIG. 7 FOR DETS)
R 250B 854760-404A 2 MODULE AY, IAT (CTR) (SEE IPL A 2
FIG. 7 FOR DETS) (POST SB
863708-25-3298)
R –250C 854760-403A 2 MODULE AY, IAT (CTR) (SEE IPL B 2
FIG. 7 FOR DETS) (POST SB
863708-25-3298)
ATTACHING PARTS
R 255 NAS6204-18 2 BOLT (FWD) 1
R 255A NAS6204-14 2 BOLT (AFT) 1
R 260 NAS1149F0432P 2 WASHER (1 FWD, 1 AFT) 2
---*---
R 265 854777-411B 2 TABLE AY, FOOD (IN-ARM) A 3
(SEE IPL FIG. 8 FOR DETS)
R –265A 854777-412B 2 TABLE AY, FOOD (IN-ARM) B 3
(SEE IPL FIG. 8 FOR DETS)
ATTACHING PARTS
R 270 854779-001 2 PIN-IAT 1
---*---
R –275 855021-401A 2 BASEFRAME AY A 1
R –275A 855021-402A 2 BASEFRAME AY B 1
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
1A
R 280 300050-003 3 BRACKET, BAGGAGE BAR 1
ATTACHING PARTS
R 285 NAS623-3-36 3 SCREW 1
R 290 NAS1149F0363P 3 WASHER (AFT) 1
R 290A NAS1149F0332P 3 WASHER (FWD) 1
R 295 22NKM02 3 NUT (V22599) 1
---*---
R 300 854813-003A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (OUTBD)
(U/O 855021-401)
R –300A 854813-004A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (OUTBD)
(U/O 855021-402)
ATTACHING PARTS
R 305 NAS623-3-16 3 SCREW 1
R 310 NAS1149F0332P 3 WASHER 2
R 315 22NKM02 3 NUT 1
---*---
R 320 854817-001 3 TUBE, MOUNTING 1
ATTACHING PARTS
R 325 NAS602-12P 3 SCREW 1
R 330 NAS1149FN832P 3 WASHER 1
–335 NOT USED
---*---
R 340 854812-007A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (INBD)
(U/O 855021-401)
R –340A 854812-008A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (INBD)
(U/O 855021-402)
ATTACHING PARTS
R 345 NAS623-2-8 3 SCREW 1
R 350 NAS1149FN816P 3 WASHER 2
R 355 22NKM82 3 NUT (V22599) 1
---*---
R 360 854814-001 3 INSERT, BAGGAGE BAR 1
ATTACHING PARTS
R 365 AD42BS 3 RIVET (V07707) 4
---*---
R 370 115010-005 3 LEG AY-MACHINED, STRAIGHT 2
(SEE IPL FIG. 9 FOR DETS)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
1A
–375 NOT USED
R 380 854940-449 3 TUBE AY (FWD) (U/O 855021 1
-401)
R –380A 854940-450 3 TUBE AY (FWD) (U/O 855021 1
-402)
R 385 854940-451 3 TUBE AY (AFT) (U/O 855021 1
-401)
R –385A 854940-452 3 TUBE AY (AFT) (U/O 855021 1
-402)
ATTACHING PARTS
R 390 AN3-23A 3 BOLT (INBD) 2
R 395 NAS517-3-2 3 SCREW (OUTBD) 2
R 400 NAS1149F0332P 3 WASHER (INBD) (1 FWD, 2 AFT) 3
R 405 NAS1515H3L 3 WASHER (OUTBD) 2
R 410 MS21042-3 3 NUT (INBD) (AFT ONLY) 1
R 415 MS21042-3 3 NUT (OUTBD) 2
---*---
R 420 854752-401 3 DIAPHRAGM AY (AISLE) (RVT) 1
(U/O 855021-401)
R –420A 854752-402 3 DIAPHRAGM AY (AISLE) (RVT) 1
(U/O 855021-402)
R 425 854752-726 3 DIAPHRAGM AY (CTR) (RVT) 1
(U/O 855021-401)
R –425A 854752-725 3 DIAPHRAGM AY (CTR) (RVT) 1
(U/O 855021-402)
R 430 854752-410 3 DIAPHRAGM AY (OUTBD) (RVT) 1
(U/O 855021-401)
R –430A 854752-409 3 DIAPHRAGM AY (OUTBD) (RVT) 1
(U/O 855021-402)
R 435 854650-406A 3 SPREADER AY (AISLE) (SEE IPL 1
FIG. 10 FOR DETS) (U/O 855021
-401)
R –435A 854650-405A 3 SPREADER AY (AISLE) (SEE IPL 1
FIG. 10 FOR DETS) (U/O 855021
-402)
R 440 854651-408A 3 SPREADER AY (CTR) (SEE IPL 2
FIG. 11 FOR DETS) (U/O 855021
-401)
R –440A 854651-407A 3 SPREADER AY (CTR) (SEE IPL 2
FIG. 11 FOR DETS) (U/O 855021
-402)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
1A
R 445 854652-401A 3 SPREADER AY (OUTBD) (SEE IPL 1
FIG. 12 FOR DETS) (U/O 855021
-401)
R –445A 854652-402A 3 SPREADER AY (OUTBD) (SEE IPL 1
FIG. 12 FOR DETS) (U/O 855021
-402)
R 450 WA9658-2000-102 2 VELCRO-HOOK AR
R 455 WA9659-2000-112 2 VELCRO-LOOP AR
R 460 854709-105A 2 PLACARD, SAFETY (FASTEN 3
SEAT BELT WHILE SEATED)
R –465 856274-401 2 BRACKET AY (POST SB 863708 1
-25-3298)
ATTACHING PARTS
R 470 NAS603-6P 2 SCREW 3
R 475 NAS1149F0332P 2 WASHER 6
R 480 22NKTM02 2 NUT 3
---*---
R 485 855625-001 3 BRACKET, SEB SUPPORT 1
R 490 WA9659-2000-112 3 VELCRO, LOOP BEIGE (1.4”) 1
R 495 WA9659-1000-112 3 VELCRO, LOOP BEIGE (2”) 2
R –500 856682-402G 2 SHROUD AY, SEB (POST SB A 1
863708-25-3298)
R –500A 856682-401G 2 SHROUD AY, SEB (POST SB B 1
863708-25-3298)
R 505 856685-002G 3 SHROUD (U/O 856682-402) 1
R –505A 856685-001G 3 SHROUD (U/O 856682-401) 1
ATTACHING PARTS
R 510 AJ4-35 3 STUD (V3L478) 4
R 515 GH4 3 GROMMET (V3L478) 4
---*---
R –520 WA5489-100-100 3 GROMMET AR
R 525 856683-402 2 SUPPORT AY, SEB (POST SB A 1
863708-25-3298)
R –525A 856683-401 2 SUPPORT AY, SEB (POST SB B 1
863708-25-3298)
ATTACHING PARTS
R 530 NAS623-3-20 2 SCREW 1
R 535 22NKTM02 2 NUT 1
R 540 NAS1149F0316P 2 WASHER 2
R 545 856369-001 2 SPACER 1
R 550 856409-001 2 PLATE 1
---*---
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
1A
R –555 855649-401 1 IFE INSTL (SEE IPL FIG. 15 FOR A 1
DETS)
R –555A 855649-402 1 IFE INSTL (SEE IPL FIG. 15 FOR B 1
DETS)
Page 10061
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
210
75 115A
F 140
95
105
(REF)
210
115A
80 F
155
90°ROTATED
D
115
455 145
455A
145
140 150
47
25
145
85
140 150
47 E
100 145
140 150 LL
PU 35
47A
315
365
PU
LL
150 366
G
265
PU
LL
855104-401 SHOWN
15
A 20
345
Page 10062
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
A B
C 470
(860002-401, -402,
440
45 855107-401, -402
C VARIATION)
460
385
3 PLACES C 465
445
440
C 450
460 (1 PIECE)
B 465
435
286 380
46
287 40 450
430
370
425
420
40
370
30 30A 35
(REF)
AISLE (SHOWN)
B OUTBD (OPPOSITE VIEW)
866001-401, -402
866002-402, -404
855107-423, -424
VARIATION
(AISLE) 115
(OUTBD) 115A 120
(REF)
85
(REF) 120
125 130
135
125
137
135
136
(REF)
Page 10063
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
C CTR
120
(AISLE) 115
(CTR) 115A
(REF) 85
(REF) 115A (CTR)
125 115A (OUTBD)
125
85 70
(REF)
68 440
120 (REF)
60
50
65 55
D OUTBD E OUTBD
170
155 165
(REF)
165
445
160 (REF)
310
305 410
175 405
410
295 395
305A 330
175 300
185 325
180
ROTATED 90°
405
325
320 315 395
(REF)
Page 10064
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
F CTR
225
210 220
(REF)
220 195
215 200
190
(RECL CABLE)
230
195
230
200
190
440
(REF)
Page 10065
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
G
285
265
(REF)
275
270
280
235
(RECL CABLE)
400
390
190
400 200
410 195
260
255
260
385
(REF)
240
250
400 260 335
390 380
341
(REF) 360 340
355
345
(REF)
355
350
Page 10066
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2
–1 859910-403 0 SEAT AY, MODEL 5600, T/C LH A RF
HDCP TPL, NO ASH RECEIVER
–1A 859910-404 0 SEAT AY, MODEL 5600, T/C RH B RF
HDCP TPL, NO ASH RECEIVER
–1B 859910-405 0 SEAT AY, MODEL 5600, T/C LH C RF
FWD EXIT HDCP TPL, NO ASH
RECEIVER, NO RECLINE
–1C 859910-406 0 SEAT AY, MODEL 5600, T/C RH D RF
FWD EXIT HDCP TPL, NO ASH
RECEIVER, NO RECLINE
–1D 859910-413 0 SEAT AY, MODEL 5600, T/C LH E RF
EXIT HDCP TPL, NO ASH
RECEIVER, NO RECLINE, NO
OUTBD ARMREST (POST SB
859910-25-2678)
–1E 859910-414 0 SEAT AY, MODEL 5600, T/C RH F RF
EXIT HDCP TPL, NO ASH
RECEIVER, NO RECLINE, NO
OUTBD ARMREST (POST SB
859910-25-2678)
–1F 859910-415 0 SEAT AY, MODEL 5600, T/C LH G RF
HDCP AFT EXIT TPL, NO ASH
RECEIVER, NO OUTBD
ARMREST (POST SB 859910-25-
2678)
–1G 859910-416 0 SEAT AY, MODEL 5600, T/C RH H RF
HDCP AFT EXIT TPL, NO ASH
RECEIVER, NO OUTBD
ARMREST (POST SB 859910-25-
2678)
–1H 859910-411 0 SEAT AY, MODEL 5600, T/C LH J RF
HDCP NARR TPL, NO ASH
RECEIVER, NO RECLINE, NO
AFT TABLE
–1J 859910-412 0 SEAT AY, MODEL 5600, T/C RH K RF
HDCP NARR TPL, NO ASH
RECEIVER, NO RECLINE, NO
AFT TABLE
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2
–2C 860001-402 1 SEAT AY, MODEL 5600, T/C RH D 1
FWD EXIT HDCP TPL, NO ASH
RECEIVER, NO RECLINE
–2D 860002-403 1 SEAT AY, MODEL 5600, T/C LH E 1
EXIT HDCP TPL, NO ASH
RECEIVER, NO RECLINE, NO
OUTBD ARMREST (POST SB
859910-25-2678)
–2E 860002-404 1 SEAT AY, MODEL 5600, T/C RH F 1
EXIT HDCP TPL, NO ASH
RECEIVER, NO RECLINE, NO
OUTBD ARMREST (POST SB
859910-25-2678)
–2F 855107-423 1 SEAT AY, MODEL 5600, T/C LH G 1
HDCP AFT EXIT TPL, NO ASH
RECEIVER, NO OUTBD
ARMREST (POST SB 859910-25-
2678)
–2G 855107-424 1 SEAT AY, MODEL 5600, T/C RH H 1
HDCP AFT EXIT TPL, NO ASH
RECEIVER, NO OUTBD
ARMREST (POST SB 859910-25-
2678)
–2H 855109-401 1 SEAT AY, MODEL 5600, T/C LH J 1
HDCP NARR TPL, NO ASH
RECEIVER, NO RECLINE, NO
AFT TABLE
–2J 855109-402 1 SEAT AY, MODEL 5600, T/C RH K 1
HDCP NARR TPL, NO ASH
RECEIVER, NO RECLINE, NO
AFT TABLE
–5 859911 1 TRIM AND FINISH RF
–10 854604-401 2 CUSHION AY, BTM A-D 3
–10A 854604-401 2 CUSHION AY, BTM (AISLE/CTR) E-H 2
–10B 854604-467 2 CUSHION AY, BTM (OUTBD) E-H 1
–10C 854604-403 2 CUSHION AY, BTM J,K 3
15 854704-401P 3 DRESS COVER AY (BTM) 1
(U/O 854604-401)
–15A 854704-403AD 3 DRESS COVER AY (BTM) 1
(U/O 854604-403)
–15B 854704-415J 3 DRESS COVER AY (BTM) 1
(U/O 854604-467)
R 20 851707-401 3 DELETED (SUPSD BY ITEM 20D) D
R –20A 851707-403 3 DELETED (SUPSD BY ITEM 20E) D
–20B 851707-415 3 DELETED (SUPSD BY ITEM 20C) 1
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2
R –20C 851707-427 3 DELETED (SUPSD BY ITEM 20F) D
R –20D 864210-401 3 CUSHION AY, BTM (FBLK) 1
(U/O 854604-401) (SUPSDS
ITEM 20)
R –20E 864210-403 3 CUSHION AY, BTM (FBLK) 1
(U/O 854604-403) (SUPSDS
ITEM 20A)
R –20F 864210-409 3 CUSHION AY, BTM (FBLK) 1
(U/O 854604-467) (SUPSDS
ITEM 20C)
25 2010-1-511-2855 2 SEAT BELT AY (V35FB9) 3
R –25A 2011-1-511-2855 2 SEAT BELT AY (V35FB9) (ALT 3
ITEM 25)
30 840304-23 2 NAMEPLATE NP
30A 840304-35 2 NAMEPLATE (INTEGRATION) NP
35 119096-015D 2 POUCH AY, LIFEVEST 3
ATTACHING PARTS
40 MS3367-3-9 2 STRAP (WA5047-256-200) 4
---*---
45 MS3367-2-9 2 STRAP (WA5047-264-201) AR
46 MS3367-3-9 2 STRAP (WA5047-256-200) AR
47 830941-403 2 CABLE, RECL (CTR) A,B,G,H 2
47A 830941-407 2 CABLE, RECL (AISLE) A,B,G,H 1
50 849900-409 2 LOCK AY, RECL 3
55 115091-001 2 PIN, RECL LOCK 3
ATTACHING PARTS
60 AN316-6R 2 NUT 2
65 MS35333-42 2 WASHER 2
R –66 NAS601-20P 2 DELETED (SUPSD BY ITEM 68) D
R –67 MS21042-06 2 DELETED (SUPSD BY ITEM 68) D
---*---
R 68 NAS561P5-16 2 PIN-SPRING (SUPSDS ITEMS66, 3
67)
70 QUACECLIP635 2 DELETED (SUPSD BY ITEMS 70A D
THRU 70D)
–70A 860636-401 2 CLIP AY (LH) (SUPSDS ITEM 70) A,C,E, 2
G,J
–70B 860636-402 2 CLIP AY (RH) (SUPSDS ITEM 70) A,C,E, 1
G,J
–70C 860636-402 2 CLIP AY (RH) (SUPSDS ITEM 70) B,D,F, 2
H,K
–70D 860636-401 2 CLIP AY (LH) (SUPSDS ITEM 70) B,D,F, 1
H,K
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2
R 75 854745-409A 2 LATCH AY, FOOD TABLE A,D,F, 3
G,J
R –75A 854745-410A 2 LATCH AY, FOOD TABLE B,C,E, 3
H,K
ATTACHING PARTS
80 NAS514P832-8P 2 SCREW 2
---*---
85 854710-407B 2 TABLE AY, FOOD (BACK A-H 3
MOUNTED) (SEE IPL FIG. 4 FOR
DETS)
–90 854605-437 2 CUSHION AY, BACK A-D 3
–90A 854605-437 2 CUSHION AY, BACK (AISLE/CTR) E-H 2
–90B 854605-439 2 CUSHION AY, BACK (AISLE/CTR) J,K 3
–90C 854605-447 2 CUSHION AY, BACK (OUTBD) E-H 1
95 856258-201G 3 DRESS COVER AY (BACK) 1
(U/O 854605-437)
–95A 856258-203N 3 DRESS COVER AY (BACK) 1
(U/O 854605-439)
–95B 856258-221F 3 DRESS COVER AY (BACK) 1
(U/O 854605-447)
100 856258-211F 3 DRESS COVER AY (LIT POCKET) 1
(U/O 854605-437)
–100A 856258-213M 3 DRESS COVER AY (LIT POCKET) 1
(U/O 854605-439)
–100B 856258-223E 3 DRESS COVER AY (LIT POCKET) 1
(U/O 854605-447)
R 105 851708-401 3 DELETED (SUPSD BY ITEM 105C) D
R –105A 851708-403 3 DELETED (SUPSD BY ITEM 105D) D
R –105B 851708-421 3 DELETED (SUPSD BY ITEM 105E) D
R –105C 864212-401 3 CUSHION AY, BACK (FBLK) 1
(U/O 854605-437) (SUPSDS
ITEM 105)
R –105D 864212-403 3 CUSHION AY, BACK (FBLK) 1
(U/O 854605-439) (SUPSDS
ITEM 105A)
R –105E 864212-439 3 CUSHION AY, BACK (FBLK) 1
(U/O 854605-447) (SUPSDS
ITEM 105B)
R –110 MS27983-3 2 STUD (AFT SIDE OF BACK) (RVT) E,F,G,H 9
115 854687-407 2 BACK STRUCTURE AY (AISLE) A 1
(SEE IPL FIG. 5 FOR DETS)
115A 854687-408 2 BACK STRUCTURE AY (OUTBD & A 2
CTR) (SEE IPL FIG. 5 FOR DETS)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2
–115B 854687-408 2 BACK STRUCTURE AY (AISLE) B 1
(SEE IPL FIG. 5 FOR DETS)
–115C 854687-407 2 BACK STRUCTURE AY (OUTBD & B 2
CTR) (SEE IPL FIG. 5 FOR DETS)
–115D 854687-413 2 BACK STRUCTURE AY (SEE IPL C-H 3
FIG. 5 FOR DETS)
–115E 854687-405 2 BACK STRUCTURE AY (AISLE) J 1
(SEE IPL FIG. 5 FOR DETS)
–115F 854687-406 2 BACK STRUCTURE AY (OUTBD & J 2
CTR) (SEE IPL FIG. 5 FOR DETS)
–115G 854687-406 2 BACK STRUCTURE AY (AISLE) K 1
(SEE IPL FIG. 5 FOR DETS)
–115H 854687-405 2 BACK STRUCTURE AY (CTR/ K 2
OUTBD) (SEE IPL FIG. 5 FOR
DETS)
ATTACHING PARTS
120 MS3215-4050 2 RING, RETAINING 2
125 854663-001 2 SPACER,TABLE LEG A-H 2
---*---
R 130 NAS6204-18 2 BOLT C-H 3
R 135 NAS1149F0432P 2 WASHER C-H 6
R 136 MS21042L4 2 NUT C-H 3
R 137 NAS77-4-085 2 BUSHING C-H 3
140 854675-401A 2 ESCUTCHEON AY (ATTACHED A-D,J,K 4
WITH CAPTIVE SCREWS)
–140A 854675-401A 2 ESCUTCHEON AY (ATTACHED E-H 3
WITH CAPTIVE SCREWS)
145 854676-401A 2 ARMCAP A-D,J,K 4
–145A 854676-401A 2 ARMCAP E-H 3
150 WA5335-500-101 2 PLUG A-D,J,K 4
–150A WA5335-500-101 2 PLUG E-H 3
155 854670-401A 2 ARMREST AY-5600 (OUTBD) A,C,J 1
(SEE IPL FIG. 13 FOR DETS)
–155A 854670-402A 2 ARMREST AY-5600 (OUTBD) B,D,K 1
(SEE IPL FIG. 13 FOR DETS)
ATTACHING PARTS
160 NAS6204-17 2 BOLT 1
165 NAS1149F0432P 2 WASHER 2
170 MS21042-4 2 NUT 1
175 854684-001 2 INSERT 2
---*---
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2
180 854686-001 2 PIN, HDCP PIVOT (OUTBD) A-D,J,K 1
ATTACHING PARTS
185 MS3215-4025 2 RING, RETAINING 1
---*---
190 MS25281-F3 2 “P” CLAMP (CTR & AISLE ARMS) A,B,G,H 6
ATTACHING PARTS
195 NAS602-8P 2 SCREW 1
200 NAS1149FN832P 2 WASHER 1
–205 NOT USED
---*---
210 854670-406A 2 ARMREST AY-5600 (CTR) A,G 2
(SEE IPL FIG. 13 FOR DETS)
–210A 854670-405A 2 ARMREST AY-5600 (CTR) B,H 2
(SEE IPL FIG. 13 FOR DETS)
–210B 854670-402A 2 ARMREST AY-5600 (CTR) C,F,J 2
(SEE IPL FIG. 13 FOR DETS)
–210C 854670-401A 2 ARMREST AY-5600 (CTR) D,E,K 2
(SEE IPL FIG. 13 FOR DETS)
ATTACHING PARTS
215 NAS6204-17 2 BOLT 1
220 NAS1149F0432P 2 WASHER 2
225 MS21042-4 2 NUT 1
230 854684-001 2 INSERT 2
---*---
235 854810-402A 2 BUMPER AY (AISLE) A,C,E, 1
G,J
–235A 854810-401A 2 BUMPER AY (AISLE) B,D,F, 1
H,K
ATTACHING PARTS
240 NAS602-10P 2 SCREW 3
---*---
245 854811-401A 2 STEP AY, ATTENDANT 3
ATTACHING PARTS
250 NAS602-10P 2 SCREW (FWD & CTR OF STEP) 2
255 NAS602-20P 2 SCREW (AFT OF STEP) 1
260 NAS1149FN832P 2 WASHER 3
---*---
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2
265 854670-408A 2 ARMREST AY-5600 (AISLE) A,G 1
(SEE IPL FIG. 13 FOR DETS)
–265A 854670-407A 2 ARMREST AY-5600 (AISLE) B,H 1
(SEE IPL FIG. 13 FOR DETS)
–265B 854670-404A 2 ARMREST AY-5600 (AISLE) C,E,J 1
(SEE IPL FIG. 13 FOR DETS)
–265C 854670-403A 2 ARMREST AY-5600 (AISLE) D,F,K 1
(SEE IPL FIG. 13 FOR DETS)
ATTACHING PARTS
270 NAS6204-17 2 BOLT 1
275 NAS1149F0432P 2 WASHER 1
280 854684-001 2 INSERT 2
---*---
285 854678-402B 2 COVER AY (AISLE) A,C,E, 1
G,J
–285A 854678-401D 2 COVER AY (AISLE) B,D,F, 1
H,K
286 856393-001 2 ANGLE, AISLE DIAPHRAGM 1
(RVT)
287 WA9654-137-101 2 TAPE, ADHESIVE BACKED AR
(TAPE EDGES OF ITEM 286)
R –288 856760-401 2 CLOSURE AY, EXIT SEAT E,G 1
R –288A 856760-402 2 CLOSURE AY, EXIT SEAT F,H 1
–290 855024-401A 2 BASEFRAME AY A 1
–290A 855024-402A 2 BASEFRAME AY B 1
–290B 855025-401A 2 BASEFRAME AY C 1
–290C 855025-402A 2 BASEFRAME AY D 1
–290D 855026-401A 2 BASEFRAME AY E,G 1
–290E 855026-402A 2 BASEFRAME AY F,H 1
–290F 855029-401A 2 BASEFRAME AY G 1
–290G 855029-402A 2 BASEFRAME AY H 1
295 300050-003 3 BRACKET, BAGGAGE BAR 1
ATTACHING PARTS
300 NAS623-3-36 3 SCREW 1
305 NAS1149F0363P 3 WASHER (AFT) 1
305A NAS1149F0332P 3 WASHER (FWD) 1
310 22NKM02 3 NUT (V22599) 1
---*---
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2
315 854813-003A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (OUTBD)
(U/O 855024-401, 855025-401,
855026-401)
–315A 854813-004A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (OUTBD)
(U/O 855024-402, 855025-402,
855026-402)
–315B 854813-011A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (OUTBD)
(U/O 855029-401)
–315C 854813-012A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (OUTBD)
(U/O 855029-402)
ATTACHING PARTS
320 NAS623-3-16 3 SCREW 1
325 NAS1149F0332P 3 WASHER 2
330 22NKM02 3 NUT 1
---*---
335 854817-001 3 TUBE, MOUNTING 1
ATTACHING PARTS
340 NAS602-12P 3 SCREW 1
341 NAS1149FN832P 3 WASHER 1
---*---
345 854812-007A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (INBD)
(U/O 855024-401, 855025-401,
855026-401, 855029-401)
–345A 854812-008A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (INBD)
(U/O 855024-402, 855025-402,
855026-402, 855029-402)
ATTACHING PARTS
350 NAS623-2-8 3 SCREW 1
355 NAS1149FN816P 3 WASHER 1
360 22NKTM82 3 NUT (V22599) 1
---*---
365 854814-001 3 INSERT, BAGGAGE BAR 1
ATTACHING PARTS
366 AD42BS 3 RIVET (V07707) 4
---*---
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2
370 115010-005 3 LEG AY-MACHINED, STRAIGHT 2
(SEE IPL FIG. 9 FOR DETS)
(U/O 855024-401, -402, 855029
-401, -402)
–375 115010-005 3 LEG AY-MACHINED, STRAIGHT 1
(SEE IPL FIG. 9 FOR DETS)
(U/O 855025-401, -402, 855026
-401, -402)
–375A 854611-409A 3 LEG AY-MACHINED, OFFSET 1
(SEE IPL FIG. 14 FOR DETS)
(U/O 855025-401, 855026-401)
–375B 854611-410A 3 LEG AY-MACHINED, OFFSET 1
(SEE IPL FIG. 14 FOR DETS)
(U/O 855025-402, 855026-402)
380 854940-449 3 TUBE AY (FWD) (U/O 855024-401) 1
–380A 854940-450 3 TUBE AY (FWD) (U/O 855024-402) 1
–380B 854940-489 3 TUBE AY (FWD) (U/O 855025-401) 1
–380C 854940-490 3 TUBE AY (FWD) (U/O 855025-402) 1
–380D 854940-465 3 TUBE AY (FWD) (U/O 855026-401) 1
–380E 854940-466 3 TUBE AY (FWD) (U/O 855026-402) 1
–380F 854940-453 3 TUBE AY (FWD) (U/O 855029-401) 1
–380G 854940-454 3 TUBE AY (FWD) (U/O 855029-402) 1
385 854940-451 3 TUBE AY (AFT) (U/O 855024-401) 1
–385A 854940-452 3 TUBE AY (AFT) (U/O 855024-402) 1
–385B 854940-491 3 TUBE AY (AFT) (U/O 855025-401) 1
–385C 854940-492 3 TUBE AY (AFT) (U/O 855025-402) 1
–385D 854940-467 3 TUBE AY (AFT) (U/O 855026-401) 1
–385E 854940-468 3 TUBE AY (AFT) (U/O 855026-402) 1
–385F 854940-455 3 TUBE AY (AFT) (U/O 855029-401) 1
–385G 854940-456 3 TUBE AY (AFT) (U/O 855029-402) 1
ATTACHING PARTS
390 AN3-23A 3 BOLT (INBD) 2
395 NAS517-3-2 3 SCREW (OUTBD) 2
400 NAS1149F0332P 3 WASHER (INBD) 4
405 NAS1515H3L 3 WASHER (OUTBD) 2
410 MS21042-3 3 NUT 2
–415 NOT USED
---*---
420 854752-401 3 DIAPHRAGM AY (AISLE) (RVT) 1
(U/O 855024-401, 855029-401)
–420A 854752-402 3 DIAPHRAGM AY (AISLE) (RVT) 1
(U/O 855024-402, 855029-402)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2
–420B 854752-407 3 DIAPHRAGM AY (AISLE) (RVT) 1
(U/O 855025-401, 855026-401)
–420C 854752-408 3 DIAPHRAGM AY (AISLE) (RVT) 1
(U/O 855025-402, 855026-402)
425 854752-402 3 DIAPHRAGM AY (CTR) (RVT) 1
(U/O 855024-401)
–425A 854752-401 3 DIAPHRAGM AY (CTR) (RVT) 1
(U/O 855024-402)
–425B 854752-474 3 DIAPHRAGM AY (CTR) (RVT) 1
(U/O 855025-401, 855026-401)
–425C 854752-473 3 DIAPHRAGM AY (CTR) (RVT) 1
(U/O 855025-402, 855026-402)
–425D 854752-410 3 DIAPHRAGM AY (CTR) (RVT) 1
(U/O 855029-401)
–425E 854752-409 3 DIAPHRAGM AY (CTR) (RVT) 1
(U/O 855029-402)
430 854752-410 3 DIAPHRAGM AY (OUTBD) (RVT) 1
(U/O 855024-401, 855025-401)
–430A 854752-409 3 DIAPHRAGM AY (OUTBD) (RVT) 1
(U/O 855024-402, 855025-402)
–430B 854752-404 3 DIAPHRAGM AY (OUTBD) (RVT) 1
(U/O 855026-401)
–430C 854752-403 3 DIAPHRAGM AY (OUTBD) (RVT) 1
(U/O 855026-402)
–430D 854752-454 3 DIAPHRAGM AY (OUTBD) (RVT) 1
(U/O 855029-401)
–430E 854752-453 3 DIAPHRAGM AY (OUTBD) (RVT) 1
(U/O 855029-402)
435 854650-402A 3 SPREADER AY (AISLE) (SEE IPL 1
FIG. 10 FOR DETS) (U/O 858024
-401, 855029-401)
–435A 854650-401A 3 SPREADER AY (AISLE) (SEE IPL 1
FIG. 10 FOR DETS) (U/O 858024
-402, 855029-402)
–435B 854650-420A 3 SPREADER AY (AISLE) (SEE IPL 1
FIG. 10 FOR DETS) (U/O 855025
-401, 855026-401)
–435C 854650-419A 3 SPREADER AY (AISLE) (SEE IPL 1
FIG. 10 FOR DETS) (U/O 855025
-402, 855026-402)
440 854651-406A 3 SPREADER AY (CTR) (SEE IPL 2
FIG. 11 FOR DETS) (U/O 855024
-401)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2
–440A 854651-405A 3 SPREADER AY (CTR) (SEE IPL 2
FIG. 11 FOR DETS)
(U/O 855024-402)
–440B 854651-406A 3 SPREADER AY (INBD-CTR) 1
(SEE IPL FIG. 11 FOR DETS)
(U/O 855025-401, 855026-401,
855029-401)
–440C 854651-405A 3 SPREADER AY (INBD-CTR) (SEE 1
IPL FIG. 11 FOR DETS)
(U/O 855025-402, 855026-402,
855029-402)
–440D 854651-413A 3 SPREADER AY (OUTBD-CTR) 1
(SEE IPL FIG. 11 FOR DETS)
(U/O 855025-401, 855026-401)
–440E 854651-414A 3 SPREADER AY (OUTBD-CTR) 1
(SEE IPL FIG. 11 FOR DETS)
(U/O 855025-402, 855026-402)
–440F 854651-401A 3 SPREADER AY (OUTBD-CTR) 1
(SEE IPL FIG. 11 FOR DETS)
(U/O 855029-401, -402)
445 854652-401A 3 SPREADER AY (OUTBD) (SEE IPL 1
FIG. 12 FOR DETS) (U/O 855024
-401, 855029-401)
–445A 854652-402A 3 SPREADER AY (OUTBD) (SEE IPL 1
FIG. 12 FOR DETS) (U/O 855024
-402, 855029-402)
–445B 854652-411A 3 SPREADER AY (OUTBD) (SEE IPL 1
FIG. 12 FOR DETS) (U/O 856025
-401)
–445C 854652-412A 3 SPREADER AY (OUTBD) (SEE IPL 1
FIG. 12 FOR DETS) (U/O 856025
-402)
–445D 854652-413B 3 SPREADER AY (OUTBD) (SEE IPL 1
FIG. 12 FOR DETS) (U/O 856026
-401)
–445E 854652-414B 3 SPREADER AY (OUTBD) (SEE IPL 1
FIG. 12 FOR DETS) (U/O 856026
-402)
450 WA9658-2000-102 2 VELCRO-HOOK AR
455 854709-059A 2 PLACARD, SAFETY (USE SEAT A-H 3
BOTTOM CUSHION FOR
FLOTATION)
455A 854709-061A 2 PLACARD, SAFETY A-H 3
(NO SMOKING)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2
460 849592-27 2 CLOSEOUT (CTR SPREADERS) 2
ATTACHING PARTS
465 MS3367-2-9 2 STRAP (WA5047-264-201) 2
---*---
470 856263-029 2 PLACARD (RVT) E-H 1
75
115
ROTATED 90°
95
115A
105
80
F
115
E
455
D 85
100
15
20
345
35
40
25
G A
855104-411 SHOWN 365
366
315
Page 10079
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
A B 445
465
460 C
440
B
C 470
855106-411, -412
865107-411, -412
440 VARIATION
C
450 385
B (1 PIECE)
435
430
45A
286 450
40 (3 PL)
287
45
380
370
3 PLACES
425
420
40
30 30A 35 370
(REF)
B INBD (SHOWN)
CTR & OUTBD (OPPOSITE VIEW) 855105-411, -412
855106-411, -412
855107-411, -412
VARIATION
BACK AY 120
(REF)
TABLE ARM
(REF) 130
125 126
127
135
129
127
128
(REF)
Page 10080
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
C INBD (SHOWN)
CTR & OUTBD (OPP)
BACK AY
(REF)
125
TABLE ARM
70A
(REF)
70 (OPP)
120
66
(REF)
60
50
145
55
65
D OUTBD
160
180 165
130A 155
135
140
165
170
175
150
(REF)
185 175
445
(REF)
310
305A 410
405
410
295 395
300 330
300
325
405
325
320 315 395
(REF)
Page 10081
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
145
E CTR
215
220
130A
210
220
225
47 230
(REF) 150
230
190
200
195
(RECLINE CABLE)
440
(REF)
190
200 195
Page 10082
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
F
145
285
130 265
275
270
235 280
435 280 240
(REF)
190
245 410 200
400 240 195
390
190
200
195
260
255
260
385
(REF)
24 250
335
400 260
355350
345
(REF)
Page 10083
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
G
490
485
505 485
490
495
535 500
520 490
525
485
515
505
485
480
485
480
545
550
480 485
560
520 555
525 370
(REF)
550
540
Page 10084
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2A
R –1 863706-403 0 SEAT AY, MODEL 5600, T/C LH A RF
HDCP TPL, NO ASH RECEIVER
(POST SB 863708-25-3298)
R –1A 863706-404 0 SEAT AY, MODEL 5600, T/C RH B RF
HDCP TPL, NO ASH RECEIVER
(POST SB 863708-25-3298)
R –1B 863706-405 0 SEAT AY, MODEL 5600, T/C LH C RF
FWD EXIT HDCP TPL, NO ASH
RECEIVER, NO RECLINE (POST
SB 863708-25-3298)
R –1C 863706-406 0 SEAT AY, MODEL 5600, T/C RH D RF
FWD EXIT HDCP TPL, NO ASH
RECEIVER, NO RECLINE (POST
SB 863708-25-3298)
R –1D 863706-407 0 SEAT AY, MODEL 5600, T/C LH E RF
EXIT HDCP TPL, NO ASH
RECEIVER, NO RECLINE, NO
OUTBD ARMREST (POST SB
863708-25-3298)
R –1E 863706-408 0 SEAT AY, MODEL 5600, T/C RH F RF
EXIT HDCP TPL, NO ASH
RECEIVER, NO RECLINE, NO
OUTBD ARMREST (POST SB
863708-25-3298)
R –1F 863706-409 0 SEAT AY, MODEL 5600, T/C LH G RF
HDCP AFT EXIT TPL, NO ASH
RECEIVER, NO OUTBD
ARMREST (POST SB 863708-25-
3298)
R –1G 863706-410 0 SEAT AY, MODEL 5600, T/C RH H RF
HDCP AFT EXIT TPL, NO ASH
RECEIVER, NO OUTBD
ARMREST (POST SB 863708-25-
3298)
R –1H 863706-411 0 SEAT AY, MODEL 5600, T/C LH J RF
HDCP NARR TPL, NO ASH
RECEIVER, NO RECLINE, NO
AFT TABLE, NO AFT TABLE
(POST SB 863708-25-3298)
R –1J 863706-412 0 SEAT AY, MODEL 5600, T/C RH K RF
HDCP NARR TPL, NO ASH
RECEIVER, NO RECLINE (POST
SB 863708-25-3298)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2A
R –2 855104-411 1 SEAT AY, MODEL 5600, T/C LH A 1
HDCP TPL, NO ASH RECEIVER
R –2A 855104-412 1 SEAT AY, MODEL 5600, T/C RH B 1
HDCP TPL, NO ASH RECEIVER
R –2B 855105-411 1 SEAT AY, MODEL 5600, T/C LH C 1
FWD EXIT HDCP TPL, NO ASH
RECEIVER, NO RECLINE
R –2C 855105-412 1 SEAT AY, MODEL 5600, T/C RH D 1
FWD EXIT HDCP TPL, NO ASH
RECEIVER, NO RECLINE
R –2D 855106-411 1 SEAT AY, MODEL 5600, T/C LH E 1
EXIT HDCP TPL, NO ASH
RECEIVER, NO RECLINE, NO
OUTBD ARMREST
R –2E 855106-412 1 SEAT AY, MODEL 5600, T/C RH F 1
EXIT HDCP TPL, NO ASH
RECEIVER, NO RECLINE, NO
OUTBD ARMREST
R –2F 855107-411 1 SEAT AY, MODEL 5600, T/C LH G 1
HDCP AFT EXIT TPL, NO ASH
RECEIVER, NO OUTBD
ARMREST
R –2G 855107-412 1 SEAT AY, MODEL 5600, T/C RH H 1
HDCP AFT EXIT TPL, NO ASH
RECEIVER, NO OUTBD
ARMREST
R –2H 855109-411 1 SEAT AY, MODEL 5600, T/C LH J 1
HDCP NARR TPL, NO ASH
RECEIVER, NO RECLINE, NO
AFT TABLE
R –2J 855109-412 1 SEAT AY, MODEL 5600, T/C RH K 1
HDCP NARR TPL, NO ASH
RECEIVER, NO RECLINE, NO
AFT TABLE
R –5 863707 1 TRIM AND FINISH RF
R –10 854604-401 2 CUSHION AY, BTM A-D 3
R –10A 854604-401 2 CUSHION AY, BTM (AISLE/CTR) E-H 2
R –10B 854604-467 2 CUSHION AY, BTM (OUTBD) E-H 1
R –10C 854604-403 2 CUSHION AY, BTM J,K 3
R 15 854704-401P 3 DRESS COVER AY (BTM) 1
(U/O 854604-401)
R –15A 854704-403AD 3 DRESS COVER AY (BTM) 1
(U/O 854604-403)
R –15B 854704-415J 3 DRESS COVER AY (BTM) 1
(U/O 854604-467)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2A
R 20 864210-401 3 CUSHION AY, BTM (FBLK) 1
(U/O 854604-401)
R –20A 864210-403 3 CUSHION AY, BTM (FBLK) 1
(U/O 854604-403)
R –20B 864210-409 3 CUSHION AY, BTM (FBLK) 1
(U/O 854604-467)
R 25 2010-1-511-2855 2 SEAT BELT AY (V35FB9) 3
R –25A 2011-1-511-2855 2 SEAT BELT AY (V35FB9) (ALT 3
ITEM 25)
R 30 840304-23 2 NAMEPLATE (TSO) NP
R 30A 861615-019 2 NAMEPLATE (INTEGRATION) NP
R –30B 861615-003 2 NAMEPLATE (MODIFICATION) NP
(POST SB 863708-25-3298)
R –30C 861615-007 2 NAMEPLATE (MODIFICATION) NP
(POST SB 863708-25-3298)
R 35 119096-015D 2 POUCH AY, LIFEVEST 3
ATTACHING PARTS
R 40 MS3367-3-9 2 STRAP (WA5047-256-200) 4
---*---
R 45 MS3367-3-9 2 STRAP (WA5047-256-200) A,B,G,H 3
R 45A MS3367-2-9 2 STRAP (WA5047-264-201) A,B,G,H AR
R 47 830941-403 2 CABLE, RECL (CTR) A,B,G,H 2
R 47A 830941-407 2 CABLE, RECL (AISLE) A,B,G,H 1
R 50 849900-409 2 LOCK AY, RECL 3
ATTACHING PARTS
R 55 AN316-6R 2 NUT 2
R 60 MS35333-42 2 WASHER 2
---*---
R 65 NAS561P5-16 2 PIN-SPRING 3
R 66 115091-001 2 PIN, RECL LOCK 3
R 70 860636-401 2 CLIP AY (LH) A,C,E, 2
G,J
R 70A 860636-402 2 CLIP AY (RH) A,C,E, 1
G,J
R –70B 860636-402 2 CLIP AY (RH) B,D,F, 2
H,K
R –70C 860636-401 2 CLIP AY (LH) B,D,F, 1
H,K
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2A
R 75 854745-409A 2 LATCH AY, FOOD TABLE A,D,F, 3
G,J
R –75A 854745-410A 2 LATCH AY, FOOD TABLE B,C,E, 3
H,K
ATTACHING PARTS
R 80 NAS514P832-8P 2 SCREW 2
---*---
R 85 854710-407B 2 TABLE AY, FOOD (BACK A,B,G,H 3
MOUNTED) (SEE IPL FIG. 4 FOR
DETS)
R –85A 854713-407B 2 TABLE AY, FOOD (3” AFT-SLIDER) C,D,E,F 3
(SEE IPL FIG. 4A FOR DETS)
R –90 854605-437 2 CUSHION AY, BACK A-D 3
R –90A 854605-437 2 CUSHION AY, BACK (AISLE/CTR) E-H 2
R –90B 854605-447 2 CUSHION AY, BACK (OUTBD) E-H 1
R –90C 854605-439 2 CUSHION AY, BACK (AISLE/CTR) J,K 3
R 95 856258-201G 3 DRESS COVER AY (BACK) 1
(U/O 854605-437)
R –95A 856258-221F 3 DRESS COVER AY (BACK) 1
(U/O 854605-447)
R –95B 856258-203N 3 DRESS COVER AY (BACK) 1
(U/O 854605-439)
R 100 856258-211F 3 DRESS COVER AY (LIT POCKET) 1
(U/O 854605-437)
R –100A 856258-223E 3 DRESS COVER AY (LIT POCKET) 1
(U/O 854605-447)
R –100B 856258-213M 3 DRESS COVER AY (LIT POCKET) 1
(U/O 854605-439)
R 105 864212-401 3 CUSHION AY, BACK (FBLK) 1
(U/O 854605-437)
R –105A 864212-403 3 CUSHION AY, BACK (FBLK) 1
(U/O 854605-439)
R –105B 864212-439 3 CUSHION AY, BACK (FBLK) 1
(U/O 854605-447)
R –110 MS27983-3 2 STUD (AFT SIDE OF BACK) (RVT) E,F,G,H 9
R 115 854687-407 2 BACK STRUCTURE AY (AISLE) A 1
(SEE IPL FIG. 5 FOR DETS)
R 115A 854687-408 2 BACK STRUCTURE AY (OUTBD & A 2
CTR) (SEE IPL FIG. 5 FOR DETS)
R –115B 854687-408 2 BACK STRUCTURE AY (AISLE) B 1
(SEE IPL FIG. 5 FOR DETS)
R –115C 854687-407 2 BACK STRUCTURE AY (OUTBD & B 2
CTR) (SEE IPL FIG. 5 FOR DETS)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2A
R –115D 854687-413 2 BACK STRUCTURE AY (SEE IPL C-H 3
FIG. 5 FOR DETS)
R –115E 854687-405 2 BACK STRUCTURE AY (AISLE) J 1
(SEE IPL FIG. 5 FOR DETS)
R –115F 854687-406 2 BACK STRUTURE AY (OUTBD & J 2
CTR)
(SEE IPL FIG. 5 FOR DETS)
R –115G 854687-406 2 BACK STRUCTURE AY (AISLE) K 1
(SEE IPL FIG. 5 FOR DETS)
R –115H 854687-405 2 BACK STRUCTURE AY (CTR/ K 2
OUTBD) (SEE IPL FIG. 5 FOR
DETS)
ATTACHING PARTS
R 120 MS3215-4050 2 RING, RETAINING 2
R 125 854663-001 2 SPACER,TABLE LEG A-H 2
---*---
R 126 NAS6204-18 2 BOLT C-H 3
R 127 NAS1149F0432P 2 WASHER C-H 6
R 128 MS21042L4 2 NUT C-H 3
R 129 NAS77-4-085 2 BUSHING C-H 3
R 130 854675-401A 2 ESCUTCHEON AY (INBD) A-D,J,K 1
(ATTACHED WITH CAPTIVE
SCREWS)
R 130A 854675-405A 2 ESCUTCHEON AY (OUTBD/CTR) A-D,J,K 3
(ATTACHED WITH CAPTIVE
SCREW) (POST SB 863708-25-
3298)
R –130B 854675-405A 2 ESCUTCHEON AY (INBD/CTR) E-H 3
(ATTACHED WITH CAPTIVE
SCREW) (POST SB 863708-25-
3298)
R 135 854685-005 2 PLATE, RJU (OUTBD/CTR) (POST A-D,J,K 3
SB 863708-25-3298)
R –135A 854685-005 2 PLATE, RJU (INBD/CTR) (POST E-H 3
SB 863708-25-3298)
ATTACHING PARTS
R 140 NAS601-7P 2 SCREW 2
---*---
R 145 854676-401A 2 ARMCAP A-D,J,K 4
R –145A 854676-401A 2 ARMCAP (INBD/CTR) E-H 3
R 150 WA5335-500-101 2 PLUG A-D,J,K 4
R –150A WA5335-500-101 2 PLUG (INBD/CTR) E-H 3
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2A
R 155 854670-401A 2 ARMREST AY-5600 (OUTBD) A,C,J 1
(SEE IPL FIG. 13 FOR DETS)
R –155A 854670-402A 2 ARMREST AY-5600 (OUTBD) B,D,K 1
(SEE IPL FIG. 13 FOR DETS)
ATTACHING PARTS
R 160 NAS6204-17 2 BOLT 1
R 165 NAS1149F0432P 2 WASHER 2
R 170 MS21042-4 2 NUT 1
R 175 854684-001 2 INSERT 2
---*---
R 180 854686-001 2 PIN, HDCP PIVOT (OUTBD) A-D,J,K 1
ATTACHING PARTS
R 185 MS3215-4025 2 RING, RETAINING 1
---*---
R 190 MS25281-F3 2 “P” CLAMP (CTR & AISLE ARMS) A,B,G,H 6
ATTACHING PARTS
R 195 NAS602-8P 2 SCREW 1
R 200 NAS1149FN832P 2 WASHER 1
–205 NOT USED
---*---
R 210 854670-406A 2 ARMREST AY-5600 (CTR) A,G 2
(SEE IPL FIG. 13 FOR DETS)
R –210A 854670-405A 2 ARMREST AY-5600 (CTR) B,H 2
(SEE IPL FIG. 13 FOR DETS)
R –210B 854670-401A 2 ARMREST AY-5600 (CTR) C,F,J 2
(SEE IPL FIG. 13 FOR DETS)
R –210C 854670-402A 2 ARMREST AY-5600 (CTR) D,E,K 2
(SEE IPL FIG. 13 FOR DETS)
ATTACHING PARTS
R 215 NAS6204-17 2 BOLT 1
R 220 NAS1149F0432P 2 WASHER 2
R 225 MS21042-4 2 NUT 1
R 230 854684-001 2 INSERT 2
---*---
R 235 854810-402A 2 BUMPER AY (AISLE) A,C,E, 1
G,J
R –235A 854810-401A 2 BUMPER AY (AISLE) B,D,F, 1
H,K
ATTACHING PARTS
R 240 NAS602-10P 2 SCREW 3
---*---
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2A
R 245 854811-401A 2 STEP AY, ATTENDANT 3
ATTACHING PARTS
R 250 NAS602-10P 2 SCREW (FWD & CTR OF STEP) 2
R 255 NAS602-20P 2 SCREW (AFT OF STEP) 1
R 260 NAS1149FN832P 2 WASHER 3
---*---
R 265 854670-408A 2 ARMREST AY-5600 (AISLE) A,G 1
(SEE IPL FIG. 13 FOR DETS)
R –265A 854670-407A 2 ARMREST AY-5600 (AISLE) B,H 1
(SEE IPL FIG. 13 FOR DETS)
R –265B 854670-404A 2 ARMREST AY-5600 (AISLE) C,E,J 1
(SEE IPL FIG. 13 FOR DETS)
R –265C 854670-403A 2 ARMREST AY-5600 (AISLE) D,F,K 1
(SEE IPL FIG. 13 FOR DETS)
ATTACHING PARTS
R 270 NAS6204-17 2 BOLT 1
R 275 NAS1149F0432P 2 WASHER 1
R 280 854684-001 2 INSERT 2
---*---
R 285 854678-402B 2 COVER AY (AISLE) A,C,E, 1
G,J
R –285A 854678-401D 2 COVER AY (AISLE) B,D,F, 1
H,K
R 286 856393-001 2 ANGLE, AISLE DIAPHRAGM 1
(RVT)
R 287 WA9654-137-101 2 TAPE, ADHESIVE BACKED AR
(TAPE EDGES OF ITEM 286)
R –288 856760-401 2 CLOSURE AY, EXIT SEAT E,G 1
R –288A 856760-402 2 CLOSURE AY, EXIT SEAT F,H 1
R –290 855024-401A 2 BASEFRAME AY A 1
R –290A 855024-402A 2 BASEFRAME AY B 1
R –290B 855025-401A 2 BASEFRAME AY C 1
R –290C 855025-402A 2 BASEFRAME AY D 1
R –290D 855026-401A 2 BASEFRAME AY E,G 1
R –290E 855026-402A 2 BASEFRAME AY F,H 1
R –290F 855029-401A 2 BASEFRAME AY G 1
R –290G 855029-402A 2 BASEFRAME AY H 1
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2A
R 295 300050-003 3 BRACKET, BAGGAGE BAR 1
ATTACHING PARTS
R 300 NAS623-3-36 3 SCREW 1
R 305 NAS1149F0363P 3 WASHER (AFT) 1
R 305A NAS1149F0332P 3 WASHER (FWD) 1
R 310 22NKM02 3 NUT (V22599) 1
---*---
R 315 854813-003A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (OUTBD)
(U/O 855024-401, 855025-401,
855026-401)
R –315A 854813-004A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (OUTBD)
(U/O 855024-402, 855025-402,
855026-402)
R –315B 854813-011A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (OUTBD)
(U/O 855029-401)
R –315C 854813-012A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (OUTBD)
(U/O 855029-402)
ATTACHING PARTS
R 320 NAS623-3-16 3 SCREW 1
R 325 NAS1149F0332P 3 WASHER 2
R 330 22NKM02 3 NUT 1
---*---
R 335 854817-001 3 TUBE, MOUNTING 1
ATTACHING PARTS
R 340 NAS602-12P 3 SCREW 1
R 341 NAS1149FN832P 3 WASHER 1
---*---
R 345 854812-007A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (INBD)
(U/O 855024-401, 855025-401,
855026-401, 855029-401)
R –345A 854812-008A 3 TUBE, BAGGAGE BAR, 1
POWDERCOAT (INBD)
(U/O 855024-402, 855025-402,
855026-402, 855029-402)
ATTACHING PARTS
R 350 NAS623-2-8 3 SCREW 1
R 355 NAS1149FN816P 3 WASHER 1
R 360 22NKTM82 3 NUT (V22599) 1
---*---
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2A
R 365 854814-001 3 INSERT, BAGGAGE BAR 1
ATTACHING PARTS
R 366 AD42BS 3 RIVET (V07707) 4
---*---
R 370 115010-005 3 LEG AY-MACHINED, STRAIGHT 2
(SEE IPL FIG. 9 FOR DETS)
(U/O 855024-401, -402, 855029
-401, -402)
R –375 115010-005 3 LEG AY-MACHINED, STRAIGHT 1
(SEE IPL FIG. 9 FOR DETS)
(U/O 855025-401, -402, 855026
-401, -402)
R –375A 854611-409A 3 LEG AY-MACHINED, OFFSET 1
(SEE IPL FIG. 14 FOR DETS)
(U/O 855025-401, 855026-401)
R –375B 854611-410A 3 LEG AY-MACHINED, OFFSET 1
(SEE IPL FIG. 14 FOR DETS)
(U/O 855025-402, 855026-402)
R 380 854940-449 3 TUBE AY (FWD) (U/O 855024-401) 1
R –380A 854940-450 3 TUBE AY (FWD) (U/O 855024-402) 1
R –380B 854940-489 3 TUBE AY (FWD) (U/O 855025-401) 1
R –380C 854940-490 3 TUBE AY (FWD) (U/O 855025-402) 1
R –380D 854940-465 3 TUBE AY (FWD) (U/O 855026-401) 1
R –380E 854940-466 3 TUBE AY (FWD) (U/O 855026-402) 1
R –380F 854940-453 3 TUBE AY (FWD) (U/O 855029-401) 1
R –380G 854940-454 3 TUBE AY (FWD) (U/O 855029-402) 1
R 385 854940-451 3 TUBE AY (AFT) (U/O 855024-401) 1
R –385A 854940-452 3 TUBE AY (AFT) (U/O 855024-402) 1
R –385B 854940-491 3 TUBE AY (AFT) (U/O 855025-401) 1
R –385C 854940-492 3 TUBE AY (AFT) (U/O 855025-402) 1
R –385D 854940-467 3 TUBE AY (AFT) (U/O 855026-401) 1
R –385E 854940-468 3 TUBE AY (AFT) (U/O 855026-402) 1
R –385F 854940-455 3 TUBE AY (AFT) (U/O 855029-401) 1
R –385G 854940-456 3 TUBE AY (AFT) (U/O 855029-402) 1
ATTACHING PARTS
R 390 AN3-23A 3 BOLT (INBD) 2
R 395 NAS517-3-2 3 SCREW (OUTBD) 2
R 400 NAS1149F0332P 3 WASHER (INBD) 4
R 405 NAS1515H3L 3 WASHER (OUTBD) 2
R 410 MS21042-3 3 NUT 2
---*---
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2A
–415 NOT USED
R 420 854752-401 3 DIAPHRAGM AY (AISLE) (RVT) 1
(U/O 855024-401, 855029-401)
R –420A 854752-402 3 DIAPHRAGM AY (AISLE) (RVT) 1
(U/O 855024-402, 855029-402)
R –420B 854752-407 3 DIAPHRAGM AY (AISLE) (RVT) 1
(U/O 855025-401, 855026-401)
R –420C 854752-408 3 DIAPHRAGM AY (AISLE) (RVT) 1
(U/O 855025-402, 855026-402)
R 425 854752-402 3 DIAPHRAGM AY (CTR) (RVT) 1
(U/O 855024-401)
R –425A 854752-401 3 DIAPHRAGM AY (CTR) (RVT) 1
(U/O 855024-402)
R –425B 854752-474 3 DIAPHRAGM AY (CTR) (RVT) 1
(U/O 855025-401, 855026-401)
R –425C 854752-473 3 DIAPHRAGM AY (CTR) (RVT) 1
(U/O 855025-402, 855026-402)
R –425D 854752-410 3 DIAPHRAGM AY (CTR) (RVT) 1
(U/O 855029-401)
R –425E 854752-409 3 DIAPHRAGM AY (CTR) (RVT) 1
(U/O 855029-402)
R 430 854752-410 3 DIAPHRAGM AY (OUTBD) (RVT) 1
(U/O 855024-401, 855025-401)
R –430A 854752-409 3 DIAPHRAGM AY (OUTBD) (RVT) 1
(U/O 855024-402, 855025-402)
R –430B 854752-404 3 DIAPHRAGM AY (OUTBD) (RVT) 1
(U/O 855026-401)
R –430C 854752-403 3 DIAPHRAGM AY (OUTBD) (RVT) 1
(U/O 855026-402)
R –430D 854752-454 3 DIAPHRAGM AY (OUTBD) (RVT) 1
(U/O 855029-401)
R –430E 854752-453 3 DIAPHRAGM AY (OUTBD) (RVT) 1
(U/O 855029-402)
R 435 854650-402A 3 SPREADER AY (AISLE) (SEE IPL 1
FIG. 10 FOR DETS) (U/O 858024
-401, 855029-401)
R –435A 854650-401A 3 SPREADER AY (AISLE) (SEE IPL 1
FIG. 10 FOR DETS) (U/O 858024
-402, 855029-402)
R –435B 854650-420A 3 SPREADER AY (AISLE) (SEE IPL 1
FIG. 10 FOR DETS) (U/O 855025
-401, 855026-401)
R –435C 854650-419A 3 SPREADER AY (AISLE) (SEE IPL 1
FIG. 10 FOR DETS) (U/O 855025
-402, 855026-402)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2A
R 440 854651-406A 3 SPREADER AY (CTR) (SEE IPL 2
FIG. 11 FOR DETS) (U/O 855024
-401)
R –440A 854651-405A 3 SPREADER AY (CTR) (SEE IPL 2
FIG. 11 FOR DETS)
(U/O 855024-402)
R –440B 854651-406A 3 SPREADER AY (INBD-CTR) 1
(SEE IPL FIG. 11 FOR DETS)
(U/O 855025-401, 855026-401,
855029-401)
R –440C 854651-405A 3 SPREADER AY (INBD-CTR) (SEE 1
IPL FIG. 11 FOR DETS)
(U/O 855025-402, 855026-402,
855029-402)
R –440D 854651-413A 3 SPREADER AY (OUTBD-CTR) 1
(SEE IPL FIG. 11 FOR DETS)
(U/O 855025-401, 855026-401)
R –440E 854651-414A 3 SPREADER AY (OUTBD-CTR) 1
(SEE IPL FIG. 11 FOR DETS)
(U/O 855025-402, 855026-402)
R –440F 854651-401A 3 SPREADER AY (OUTBD-CTR) 1
(SEE IPL FIG. 11 FOR DETS)
(U/O 855029-401, -402)
R 445 854652-401A 3 SPREADER AY (OUTBD) (SEE IPL 1
FIG. 12 FOR DETS) (U/O 855024
-401, 855029-401)
R –445A 854652-402A 3 SPREADER AY (OUTBD) (SEE IPL 1
FIG. 12 FOR DETS) (U/O 855024
-402, 855029-402)
R –445B 854652-411A 3 SPREADER AY (OUTBD) (SEE IPL 1
FIG. 12 FOR DETS) (U/O 856025
-401)
R –445C 854652-412A 3 SPREADER AY (OUTBD) (SEE IPL 1
FIG. 12 FOR DETS) (U/O 856025
-402)
R –445D 854652-413B 3 SPREADER AY (OUTBD) (SEE IPL 1
FIG. 12 FOR DETS) (U/O 856026
-401)
R –445E 854652-414B 3 SPREADER AY (OUTBD) (SEE IPL 1
FIG. 12 FOR DETS) (U/O 856026
-402)
R 450 WA9658-2000-102 2 VELCRO-HOOK AR
R 455 854709-105A 2 PLACARD, SAFETY (FASTEN A-H 3
SEAT BELT WHILE SEATED)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2A
R 460 849592-27 2 CLOSEOUT (CTR SPREADERS) 2
ATTACHING PARTS
R 465 MS3367-2-9 2 STRAP (WA5047-264-201) 2
---*---
R 470 856263-029 2 PLACARD, EXIT SEAT (RVT) E-H 1
R –475 856274-401 2 BRACKET AY (POST SB 863708 1
-25-3298)
ATTACHING PARTS
R 480 NAS603-6P 2 SCREW 3
R 485 NAS1149F0332P 2 WASHER 6
R 490 22NKTM02 2 NUT 3
---*---
R 495 855625-001 3 BRACKET, SEB SUPPORT 1
R 500 WA9659-2000-112 3 VELCRO, LOOP BEIGE (1.4”) 1
R 505 WA9659-1000-112 3 VELCRO, LOOP BEIGE (2”) 2
R –510 856682-402G 2 SHROUD AY, SEB (POST SB A,C,E, 1
863708-25-3298) G,J
R –510A 856682-401G 2 SHROUD AY, SEB (POST SB B,D,F, 1
863708-25-3298) H,K
R 515 856685-002G 3 SHROUD (U/O 856682-402) 1
R –515A 856685-001G 3 SHROUD (U/O 856682-401) 1
ATTACHING PARTS
R 520 AJ4-35 3 STUD (V3L478) 4
R 525 GH4 3 GROMMET (V3L478) 4
---*---
R –530 WA5489-100-100 3 GROMMET AR
R 535 856683-402 2 SUPPORT AY, SEB (POST SB A,C,E, 1
863708-25-3298) G,J
R –535A 856683-401 2 SUPPORT AY, SEB (POST SB B,D,F, 1
863708-25-3298) H,K
ATTACHING PARTS
R 540 NAS623-3-20 2 SCREW 1
R 545 22NKTM02 2 NUT 1
R 550 NAS1149F0316P 2 WASHER 2
R 555 856369-001 2 SPACER 1
R 560 856409-001 2 PLATE 1
---*---
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
2A
R –565 855649-403 1 IFE INSTL (SEE IPL FIG. 15 FOR A 1
DETS)
R –565A 855649-404 1 IFE INSTL (SEE IPL FIG. 15 FOR B 1
DETS)
R –565B 855649-419 1 IFE INSTL (SEE IPL FIG. 15 FOR C 1
DETS)
R –565C 855649-420 1 IFE INSTL (SEE IPL FIG. 15 FOR D 1
DETS)
R –565D 855649-405 1 IFE INSTL (SEE IPL FIG. 15 FOR E,G 1
DETS)
R –565E 855649-406 1 IFE INSTL (SEE IPL FIG. 15 FOR F,H 1
DETS)
R –565F 855649-425 1 IFE INSTL (SEE IPL FIG. 15 FOR J 1
DETS)
R –565G 855649-426 1 IFE INSTL (SEE IPL FIG. 15 FOR K 1
DETS)
DELETED
Page 10098
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
3
R –1 854745-409A 0 DELETED RF
R –1A 854745-410A 0 DELETED RF
R –5 854746-403 1 DELETED D
ATTACHING PARTS
R –10 MS171435 1 DELETED D
R –15 NAS1149D0332J 1 DELETED D
R –20 LC-047F1 1 DELETED D
---*---
R –25 854749-003 1 DELETED D
R –25A 854749-004 1 DELETED D
45
15 25
30
25
20
50
30
35
25
25
20
10
854710-407 SHOWN 5
Page 10100
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
4
–1 854710-407B 0 TABLE AY, FOOD (BACK RF
MOUNTED) (SEE IPL FIGS. 1,
1A, 2 AND 2A FOR NHA)
90
75
10
80
A 10 75
95
80
A
35
30
30 65A
50
25 55
35 60
45
40
20
65
20
45
50 35
60
25
30A
35
40
Page 10102
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
4A
R –1 854713-407B 0 TABLE AY, FOOD (3” AFT SLIDER) RF
(SEE IPL FIG. 2A FOR NHA)
Page 10104
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
130
115
130
135
130
125
110
65
145
150
A
125
120
100 100
120
85 80
854687-405 SHOWN 75
80
95 90
Page 10105
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
45
55
40
45
55
50
60
50
60
Page 10106
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
5
–1 854687-405 0 BACK STRUCTURE AY (SEE IPL A 1
FIGS. 2 AND 2A FOR NHA)
–1A 854687-406 0 BACK STRUCTURE AY (SEE IPL B 1
FIGS. 2 AND 2A FOR NHA)
–1B 854687-407 0 BACK STRUCTURE AY (SEE IPL C 1
FIGS. 1, 1A, 2 AND 2A FOR NHA)
–1C 854687-408 0 BACK STRUCTURE AY (SEE IPL D 1
FIGS. 1, 1A, 2 AND 2A FOR NHA)
–1D 854687-413 0 BACK STRUCTURE AY (SEE IPL E 1
FIGS. 2 AND 2S FOR NHA)
–5 NOT USED
THRU
–35 NOT USED
40 854918-009 1 SPRING, LIT POCKET A,B 1
–40A 854918-011 1 SPRING, LIT POCKET C,D 1
–40B 854918-019 1 SPRING, LIT POCKET E 1
ATTACHING PARTS
45 NAS517-3-4 1 SCREW 2
50 NAS1149D0332J 1 WASHER 2
55 NAS1169-10L 1 WASHER-DIMPLED 2
60 22NKM02 1 NUT 2
---*---
65 854926-009 1 DOUBLER, LIT SPRING (RVT) A,B 1
–65A 854926-011 1 DOUBLER, LIT SPRING (RVT) C,D,E 1
–70 854693-401 1 ARM AY, QUADRANT A,C 1
–70A 854693-401 1 ARM AY, QUADRANT B,D,E 2
ATTACHING PARTS
75 NAS6204-10 1 BOLT 1
80 NAS1149D0432J 1 WASHER 2
85 MS21042-4 1 NUT 1
---*---
90 NAS75-4-008 2 BUSHING 1
95 854699-001 2 ARM 1
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
5
100 NAS77-8-080 1 BUSHING 2
–105 WA5135-102-101 1 CLIPNUT 2
110 WA9658-2000-102 1 VELCRO-HOOK, 2 IN. BEIGE AR
115 WA9658-1000-101 1 VELCRO-HOOK, 1 IN. BEIGE AR
120 WA9658-500-105 1 VELCRO-HOOK, 0.5 IN. BEIGE AR
125 WA9659-2000-112 1 VELCRO-LOOP, 2 IN. BEIGE AR
130 WA9659-1000-112 1 VELCRO-LOOP, 1 IN. BEIGE AR
135 854696-005 1 PAN, REAR (RVT) A,B 1
–135A 854696-007 1 PAN, REAR (RVT) C,D,E 1
–140 854967-005 1 PAN (RVT) A,B 1
–140A 854967-007 1 PAN (RVT) C,D,E 1
145 854688-005 1 DIAPHRAGM, BACK (RVT) A,B 1
–145A 854688-007 1 DIAPHRAGM, BACK (RVT) C,D,E 1
150 854691-405 1 FRAME AY A 1
–150A 854691-406 1 FRAME AY B 1
–150B 854691-407 1 FRAME AY C 1
–150C 854691-408 1 FRAME AY D 1
–150D 854691-413 1 FRAME AY E 1
Page 10109
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
25
20A
20
30
10
859714-453 SHOWN
ARMREST ASSEMBLY
IPL FIGURE 6
Page 10110
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
6
–1 856714-453C 0 ARMREST AY-5600 (STD) A RF
(SEE IPL FIG. 1 FOR NHA)
–1A 856714-454C 0 ARMREST AY-5600 (STD) B RF
(SEE IPL FIG. 1 FOR NHA)
Page 10112
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
85
55 80
75
60
10
65
10
80
100 70
854760-413 SHOWN
Page 10113
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
37
45 40A
15
50
20
36
35
30
Page 10114
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
7
–1 854760-413A 0 MODULE AY-IAT (CTR) (SEE IPL A RF
FIGS. 1 AND 1A FOR NHA)
–1A 854760-414A 0 MODULE AY-IAT (CTR) (SEE IPL B RF
FIGS. 1 AND 1A FOR NHA)
–1B 854760-415A 0 MODULE AY-IAT (AISLE) (SEE IPL C RF
FIG. 1 FOR NHA)
–1C 854760-416A 0 MODULE AY-IAT (AISLE) (SEE IPL D RF
FIG. 1 FOR NHA)
R –1D 854760-403A 0 MODULE AY-IAT (AISLE) (SEE IPL E RF
FIG. 1A FOR NHA)
R –1E 854760-404A 0 MODULE AY-IAT (AISLE) (SEE IPL F RF
FIG. 1A FOR NHA)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
7
R 65 830941-403 1 CABLE, RECL A,B,E, 1
F
–65A 830941-409 1 CABLE, RECL C,D 1
70 854762-401C 1 PANEL AY-IAT A,C 1
–70A 854762-402C 1 PANEL AY-IAT B,D 1
R –70B 854762-403A 1 PANEL AY-IAT E 1
R –70C 854762-404A 1 PANEL AY-IAT F 1
75 854763-408A 1 PANEL AY-IAT A,C 1
–75A 854763-407A 1 PANEL AY-IAT B,D 1
R –75B 854763-406A 1 PANEL AY-IAT A,C 1
R –75C 854763-405A 1 PANEL AY-IAT B,D 1
80 NAS561P6-16 1 PIN-ROLL 2
85 WA9659-2000-112 1 VELCRO-LOOP, 2 IN. BEIGE (25”) 1
–90 WA9659-500-106 1 VELCRO-LOOP, 5 IN. BEIGE (36”) 1
–95 WA9659-750-1111 1 VELCRO-LOOP,.75 IN. BEIGE 1
(24”)
R 100 WA5489-100-100 1 GROMMET (BND) (3.85” PIECE) 1
94
ROTATED FOR CLARITY
92
91
92 93
(REF)
85
90
A 55
50
60
100 (2 PL)
105
B
130
117
135
116
20 35
30
125
854777-411 SHOWN 15
Page 10117
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
A 70
65 70
75
65
75
80
B
40
41
40
40
40
Page 10118
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
8
–1 854777-411B 0 TABLE AY, FOOD (IN-ARM) A RF
(SEE IPL FIG. 1 FOR NHA)
–1A 854777-412B 0 TABLE AY, FOOD (IN-ARM) B RF
(SEE IPL FIG. 1 FOR NHA)
5 NAS514P1032-10 1 SCREW 2
–10 854782-411B 1 FOOD TABLE AY A 1
–10A 854782-412B 1 FOOD TABLE AY B 1
15 852388-1A 2 LIFT, FINGER (U/O 854782-411) 1
–15A 852388-2A 2 LIFT, FINGER (U/O 854782-412) 1
ATTACHING PARTS
20 NAS514P632-6 2 SCREW 2
---*---
–25 854795-401A 2 LINK AY, IAT 1
ATTACHING PARTS
30 818830-17 2 PIN-HINGE, TABLE ARM 4
35 855164-001 2 WASHER-PLASTIC 4
---*---
40 91255A191 3 DELETED (SUPSD BY ITEM 40A) D
–40A NAS1191E06P3L 3 SCREW (SUPSDS ITEM 40) 4
–40B NAS1191E06T3L 3 SCREW (ALT ITEM 40A) 4
R 41 855160-001A 3 LINK 2
–45 854785-403A 2 PADDLE ARM AY (U/O 854782 1
-411)
–45A 854785-404A 2 PADDLE ARM AY (U/O 854782 1
-412)
ATTACHING PARTS
50 NAS1191E08P4L 2 SCREW 1
55 NAS1191E02P3L 2 SCREW 2
60 5610-22-20 2 WASHER 2
---*---
65 854794-001 3 SLIDE-IAT 2
ATTACHING PARTS
70 NAS514P1032-5 3 SCREW 2
75 MS21209F1-10 3 INSERT-HELICOIL 2
---*---
80 854786-003A 3 PADDLE ARM (U/O 854785-403) 1
–80A 854786-004A 3 PADDLE ARM (U/O 854785-404) 1
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
8
R –85 854791-001 2 DELETED (SUPSD BY ITEM 85B) D
R –85A 854791-002 2 DELETED (SUPSD BY ITEM 85C) D
R –85B 862080-403 2 KNUCKLE AY-IAT (U/O 854782 1
-411) (SUPSDS ITEM 85)
R –85C 862080-404 2 KNUCKLE AY-IAT (U/O 854782 1
-412) (SUPSDS ITEM 85A)
ATTACHING PARTS
R 90 NAS517-3-17 2 SCREW 1
---*---
R 91 865052-001 3 KNUCKLE SPACER 1
ATTACHING PARTS
R 92 115018-011 3 SCREW-LOCK 1
R 93 5103-18 3 RING-RETAINING (V07382) 1
---*---
R 94 862081-003 3 KNUCKLE (U/O 862080-403) 1
R –94A 862081-004 3 KNUCKLE (U/O 862080-404) 1
R –95 3408320018 2 DELETED D
100 854792-001 2 TRACK-IAT 2
ATTACHING PARTS
105 NAS514P1032-4 2 SCREW 3
---*---
–110 854783-401E 2 FOOD TABLE AY (U/O 854782 1
-411)
–110A 854783-402E 2 FOOD TABLE AY (U/O 854782 1
-412)
–115 855165-001 3 PIN, FOOD TABLE, IAT 1
R 116 854789-001E 3 INSERT (BND) (U/O 854783 1
-401)
R –116A 854789-002E 3 INSERT (BND) (U/O 854783 1
-402)
R 117 854787-001B 3 TABLE (U/O 854783-401) 1
R –117A 854787-002B 3 TABLE (U/O 854783-402) 1
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
8
–120 854784-411B 2 FOOD TABLE AY (U/O 854782 1
-411)
–120A 854784-412B 2 FOOD TABLE AY (U/O 854782 1
-412)
R 125 854790-005C 3 INSERT (BND) (U/O 854784-411) 1
R –125A 854790-006C 3 INSERT (BND) (U/O 854784-412) 1
R 130 854793-011C 3 INSERT (BND) (U/O 854784-411) 1
R –130A 854793-012C 3 INSERT (BND) (U/O 854784-412) 1
R 135 854788-011A 3 TABLE (U/O 854784-411) 1
R –135A 854788-012A 3 TABLE (U/O 854784-412) 1
95
105A
105A
80
110A
75
110
85
100 75
90
70
105
65
115
120
25
20
25 20
20 15
30 20
55
10
35 45
60
35
50
LEG ASSEMBLY
IPL FIGURE 9
Page 10122
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
9
–1 115010-005 0 LEG AY-AI (SEE IPL FIGS. 1 AND 2 RF
FOR NHA)
–5 115014-001 1 BASE AY 1
ATTACHING PARTS
R 10 AN4-12A 1 BOLT (AFT) 1
R 15 AN4-15A 1 BOLT (FWD) 1
20 NAS1149F0463P 1 WASHER (FWD & AFT) 4
R 25 42NKE048 1 NUT (FWD & AFT) 2
---*---
30 115024-001 1 BUSHING (AFT) 1
35 115022-001 2 STUD 3
–40 NOT USED
R 45 115017-003 2 PIN AY, SHEAR 1
50 115020-001 2 PIN AY, ANTI-RATTLE 1
55 115023-001 2 BUSHING 1
60 115015-001 2 BASE AY 1
65 115025-003 1 STRUT AY 1
ATTACHING PARTS
70 AN4-13A 1 BOLT 1
75 NAS1149F0463P 1 WASHER 2
R 80 42NKE048 1 NUT 1
85 115024-003 1 BUSHING 1
---*---
R 90 NAS6604-15 1 BOLT (FWD) 1
R 95 NAS6604-25 1 BOLT (AFT) 1
100 NAS1149F0463P 1 WASHER (FWD-UNDER HEAD) 1
R 105 NAS1149F0463P 1 WASHER (FWD-UNDER NUT) 1
R 105A NAS1149F0463P 1 WASHER (AFT) 2
R 110 MS21042-4 1 NUT (FWD) 1
R 110A 42NKE048 1 NUT (FWD) 1
115 AN565B8H4 1 SETSCREW 1
120 115011-001 1 LEG AY, (RVT) 1
Page 10124
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
10
25
30
120
85
15
20
115 35
90 130
85
50
115
45
70
75
65
60
854650-401 SHOWN
ROTATED FOR 55
CLARITY 80
Page 10125
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
10
25
30
120
85
15
20
115 35
90
130D
85
95
110
115
50
45A
105
100
70
75
65
60 854650-419 SHOWN
ROTATED FOR 55
CLARITY 80
Page 10126
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
10
–1 854650-401A 0 SPREADER AY, AISLE (SEE IPL A RF
FIG. 2 FOR NHA)
–1A 854650-402A 0 SPREADER AY, AISLE (SEE IPL B RF
FIG. 2 FOR NHA)
–1B 854650-405A 0 SPREADER AY, AISLE (SEE IPL C RF
FIG. 1 FOR NHA)
–1C 854650-406A 0 SPREADER AY, AISLE (SEE IPL D RF
FIG. 1 FOR NHA)
–1D 854650-419A 0 SPREADER AY, AISLE (SEE IPL E RF
FIG. 2 FOR NHA)
–1E 854650-420A 0 SPREADER AY, AISLE (SEE IPL F RF
FIGS. 2 FOR NHA)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
10
95 854631-003 1 SUPPORT-BACK, MACHINED E 1
–95A 854631-004 1 SUPPORT-BACK, MACHINED F 1
ATTACHING PARTS
100 NAS6203-8 1 BOLT 1
105 NAS1149D0332J 1 WASHER 1
---*---
110 MS21209F1-20 1 HELICOIL E,F 2
115 MS21209C0820 1 HELICOIL 3
120 MS21209C0615 1 HELICOIL A,B,E, 1
F
–125 MS21209F1-20 1 HELICOIL C,D 1
130 854653-001A 1 SPREADER, AISLE A 1
–130A 854653-002A 1 SPREADER, AISLE B 1
–130B 854653-005A 1 SPREADER, AISLE C 1
–130C 854653-006A 1 SPREADER, AISLE D 1
130D 854653-015A 1 SPREADER, AISLE E 1
–130E 854653-016A 1 SPREADER, AISLE F 1
Page 10129
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
10
155
40
35
155
55
60
185 30
20
40
25
185
95 95
120 190
130 50
135
130 55
130
125 80
180 85
75
130
70
135
ROTATED FOR 65
854651-401 SHOWN CLARITY 90
Page 10130
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
80
85
75
70
ROTATED FOR 65
CLARITY 90
5
10
60
55 40
35 30
20
40
165
165 95B
25
160
155
95A
170
170
180 55
160
155
170 50A
145
190B
175
155
140
155
170 150
150
175
854651-405 SHOWN
Page 10131
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
10
40
35
60 55
115
30
45
110 95
20
100
40 25
95
120 45
190
55
130
135
50B
130
130
110
105
125
180
80
85
75
130
135
70
Page 10132
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
11
–1 854651-401A 0 SPREADER AY, CTR (SEE IPL FIG. A RF
2 FOR NHA)
–1A 854651-405A 0 SPREADER AY, CTR (SEE IPL B RF
FIG. 2 FOR NHA)
–1B 854651-406A 0 SPREADER AY, CTR (SEE IPL FIG. C RF
2 FOR NHA)
–1C 854651-407A 0 SPREADER AY, CTR (SEE IPL FIG. D RF
1 FOR NHA)
–1D 854651-408A 0 SPREADER AY, CTR (SEE IPL FIG. E RF
1 FOR NHA)
–1E 854651-413A 0 SPREADER AY, CTR (SEE IPL FIG. F RF
2 FOR NHA)
–1F 854651-414A 0 SPREADER AY, CTR (SEE IPL FIG. G RF
2 FOR NHA)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
11
65 851199-003 2 BRACKET, SWIVEL LIMIT 1
ATTACHING PARTS
70 NAS623-4-6 2 SCREW 1
75 MS21042-4 2 NUT 1
80 5710-58-30 2 WASHER 1
85 NAS43HT4-14 2 SPACER 1
---*---
90 856693-001 2 LINK, SEAT BELT 1
95 NAS43DD4-10 1 SPACER A,E-G 2
95A NAS43DD4-10 1 SPACER B,C 1
95B NAS43DD4-25 1 SPACER B,C 1
100 854631-003 1 SUPPORT-BACK, MACHINED F 1
–100A 854631-004 1 SUPPORT-BACK, MACHINED G 1
ATTACHING PARTS
105 NAS6203-24 1 BOLT 1
110 NAS1149D0332J 1 WASHER 2
115 MS21042L3 1 NUT 1
---*---
120 NAS6604-20 1 BOLT (FWD) A,D-G 1
125 NAS6604-14 1 BOLT (AFT) A,D-G 1
130 NAS1149F0432P 1 WASHER A,D-G 4
135 MS21042-4 1 NUT A,D-G 2
140 854657-001A 1 ADAPTER, FRONT, OFFSET B-E 1
145 854658-001A 1 ADAPTER, REAR, OFFSET B-E 1
ATTACHING PARTS
150 NAS6604-25 1 BOLT 3
155 NAS1149F0432P 1 WASHER 6
160 MS21042-4 1 NUT 3
---*---
165 NAS6604-22 1 BOLT B,C 2
170 NAS1149F0432P 1 WASHER B,C 4
175 MS21042-4 1 NUT B,C 2
180 300041-001 1 TRUNNION, RECLINE LOCK 1
185 MS21209C0820 1 HELICOIL 4
190 854654-001B 1 SPREADER-CTR A,F,G 1
–190A 854654-007A 1 SPREADER-CTR D,E 1
190B 854654-005A 1 SPREADER-CTR B,C 1
Page 10135
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
30 -413 VARIATION
35
15 20
50
5
45
10 25
55
80
45
110
40
60
105 135 115
85
75
65
125
130
125
125
95
105
100 120
130
Page 10136
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
12
–1 854652-401A 0 SPREADER AY, OUTBD (SEE IPL A RF
FIGS. 1 AND 2 FOR NHA)
–1A 854652-402A 0 SPREADER AY, OUTBD (SEE IPL B RF
FIGS. 1 AND 2 FOR NHA)
–1B 854652-411A 0 SPREADER AY, OUTBD (SEE IPL C RF
FIG. 2 FOR NHA)
–1C 854652-412A 0 SPREADER AY, OUTBD (SEE IPL D RF
FIG. 2 FOR NHA)
–1D 854652-413B 0 SPREADER AY, OUTBD-EXIT E RF
(SEE IPL FIG. 2 FOR NHA)
–1E 854652-414B 0 SPREADER AY, OUTBD-EXIT F RF
(SEE IPL FIG. 2 FOR NHA)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
12
85 851199-003 2 BRACKET, SWIVEL LIMIT 1
ATTACHING PARTS
–90 NAS623-4-6 2 SCREW 1
95 MS21042-4 2 NUT 1
100 5710-58-30 2 WASHER 1
105 NAS43HT4-14 2 SPACER 1
---*---
110 856693-001 2 LINK, SEAT BELT 1
115 854626-001 1 BUSHING C-F 1
120 854631-003 1 SUPPORT, BACK, MACHINED C,F 1
–120A 854631-004 1 SUPPORT, BACK, MACHINED D 1
ATTACHING PARTS
125 NAS6203-17 1 BOLT 1
130 NAS1149D0332J 1 WASHER 2
135 MS21042-3 1 NUT 1
---*---
–140 NAS6204-21 1 BOLT 1
–145 NAS6204-15 1 BOLT 1
–150 NAS1149F0432P 1 WASHER 4
–155 MS21042-4 1 NUT 2
–160 854655-001 1 SPREADER, OUTBD A,C,E, 1
F
–160A 854655-002 1 SPREADER, OUTBD B,D 1
Page 10139
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
25
20A
20
40
45 30
50 55
60
(-407, -408 VARIATION) 10
854670-401 SHOWN
ARMREST ASSEMBLY
IPL FIGURE 13
Page 10140
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
13
–1 854670-401A 0 ARMREST AY-5600 (SEE IPL A 1
FIGS. 1A AND 2 FOR NHA)
–1A 854670-402A 0 ARMREST AY-5600 (SEE IPL B 1
FIGS. 1A AND 2 FOR NHA)
–1B 854670-405A 0 ARMREST AY-5600 (SEE IPL C 1
FIGS. 2 AND 2A FOR NHA)
–1C 854670-406A 0 ARMREST AY-5600 (SEE IPL D 1
FIGS. 2 AND 2A FOR NHA)
–1D 854670-407A 0 ARMREST AY-5600 (SEE IPL E 1
FIGS. 2 AND 2A FOR NHA)
–1E 854670-408A 0 ARMREST AY-5600 (SEE IPL F 1
FIGS. 2 AND 2A FOR NHA)
–1F 854670-403A 0 ARMREST AY-5600 (SEE IPL G 1
FIGS. 2 AND 2A FOR NHA)
–1G 854670-404A 0 ARMREST AY-5600 (SEE IPL H 1
FIGS. 2 AND 2A FOR NHA)
Page 10142
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
80
75
A
85
A 75
70
65
120
155
25
20A
25 20
20A 15
30 20
55
10
35 45
60
35 854611-409 SHOWN
50
Page 10143
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
A
95 105 130
105
135
140 115
150
135
140
140
145
150
155
(REF)
110
100
140
100 145
90
125
Page 10144
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
14
–1 854611-409A 0 LEG AY, OFFSET (SEE IPL FIG. 2 A RF
FOR NHA)
–1A 854611-410A 0 LEG AY, OFFSET (SEE IPL FIG. 2 B RF
FOR NHA)
–5 115014-001 1 BASE AY 1
ATTACHING PARTS
R 10 NAS6604-14 1 BOLT (AFT) 1
R 15 NAS6604-19 1 BOLT (FWD) 1
20 NAS1149F0463P 1 WASHER (AFT) 2
20A NAS1149F0432P 1 WASHER (FWD) 2
R 25 42NKE048 1 NUT (FWD & AFT) 1
30 115024-001 1 BUSHING (AFT) 1
---*---
35 115022-001 2 STUD 3
–40 NOT USED
R 45 115017-003 2 PIN AY, SHEAR 1
50 115020-001 2 PIN AY, ANTI-RATTLE 1
55 115023-001 2 BUSHING 1
60 115015-001 2 BASE AY 1
65 115025-003 1 STRUT AY 1
ATTACHING PARTS
R 70 NAS6604-17 1 BOLT 1
75 NAS1149F0463P 1 WASHER 2
R 80 42NKE048 1 NUT 1
---*---
85 115024-003 1 BUSHING 1
R 90 NAS6604-23 1 BOLT (FWD) 1
R 95 NAS6605-27 1 BOLT (AFT) 1
100 NAS1149F0463P 1 WASHER (FWD) 2
105 NAS1149F0563P 1 WASHER (AFT) 2
R 110 42KNE048 1 NUT (FWD) 1
R 115 42NKE054 1 NUT (AFT) 1
120 AN565B8H4 1 SETSCREW 1
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
14
125 115546-001 1 ADAPTER, LEG, POWDERCOAT 1
(FWD)
130 115548-001 1 ADAPTER, LEG, POWDERCOAT 1
(AFT)
ATTACHING PARTS
R 135 NAS6605-28 1 BOLT 5
140 NAS1149F0532P 1 WASHER 10
R 145 42NKE054 1 NUT 5
---*---
150 116558-001 1 BUSHING 5
155 854616-403A 1 V-LEG AY 1
Page 10147
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
5
15
20 70
80 70 80
70
70 70
-401 SHOWN
-402 OPPOSITE
E E F F
D C
B 90
85
A
855649-402 INSTL (RH IAT TPL) 855649-401 INSTL (LH IAT TPL)
IFE INSTALLATION
IPL FIGURE 15 (SHEET 1 OF 9)
Page 10148
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
5
15
20
80 (-403, -404)
70 80 (-403, -404) 70 80A (-425, -426)
80A (-425, -426) 70
70
H H G G
D C
B 95 95 A
855649-404 INSTL (RH STD HDCP TPL) 855649-403 INSTL (LH STD HDCP TPL)
855649-426 INSTL (LH AFT HDCP TPL) 855649-425 INSTL (LH AFT HDCP TPL)
IFE INSTALLATION
IPL FIGURE 15 (SHEET 2 OF 9)
Page 10149
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
70 70
80 70
80
70
70 -405 SHOWN
-406 OPPOSITE
H K J G
M L
105 100
P N
855649-406 INSTL (RH EXIT HDCP TPL) 855649-405 INSTL (LH EXIT HDCP TPL)
IFE INSTALLATION
IPL FIGURE 15 (SHEET 3 OF 9)
Page 10150
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
5C
15C 70
20C 80 70
80
70
T
70
-419 SHOWN
-420 OPPOSITE 70
K H G J
D C
P 110 110 N
855649-420 INSTL (RH FWD EXIT HDCP TPL) 855649-419 INSTL (LH FWD EXIT HDCP TPL)
IFE INSTALLATION
IPL FIGURE 15 (SHEET 4 OF 9)
Page 10151
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
A
5
B OPPOSITE 15 (REF 856683-401, -402
20 SUPPORT AY)
125
5
15
20
(TA1S8-M - P/O
856683
SUPPORT AY) (REF 856682-401, -402
2 PL IFE SHROUD AY)
C
(TA1S8-M TIE HOLDER
D OPPOSITE V REF 5, IPL FIGS. 6 & 13)
70
60 (N/S)
120
55 (N/S)
30 (N/S)
10 40 (F/S)
70 55 (F/S)
15
70
60 (N/S)
50 (N/S)
30 (N/S)
35 (F/S)
50 (F/S)
15
IFE INSTALLATION
IPL FIGURE 15 (SHEET 5 OF 9)
Page 10152
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
E
F OPPOSITE
120
115
(TA1S8-M
P/O IAT PANEL
REF IPL FIG. 7)
70
70
5 5
10 10
20 20
115
30A 10
45 70
55
15
(IFE HARNESS
N/S)
5
10 (RECLINE CABLE)
20 F/S)
IFE INSTALLATION
IPL FIGURE 15 (SHEET 6 OF 9)
Page 10153
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
J
(TA1S8-M TIE HOLDER
K OPPOSITE REF 5, IPL FIGS. 6 & 13) U
120
30A
45
10
55 (IFE HARNESS 70
15 N/S)
5
70 15
20
L
V
M OPPOSITE
10
70 30B
45
5 55
15 15
20
70
W
IFE INSTALLATION
IPL FIGURE 15 (SHEET 7 OF 9)
Page 10154
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
N
5
15
P OPPOSITE
20
(REF 856683-401, -402
SUPPORT AY)
125
5
15
20
(TA1S8-M - P/O
856683
SUPPORT AY) (REF 856682-401, -402
2 PL IFE SHROUD AY)
IFE INSTALLATION
IPL FIGURE 15 (SHEET 8 OF 9)
Page 10155
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
T U
(BTM
DIAPHRAGM) V OPPOSITE
(CLOSE) 80
80A
(REF)
120
(OPEN)
115
W X (RECLINE CABLE)
70
(IFE CABLE) 5
5
5
70
10
10 10 (IFE
10 CABLE)
5
5
IFE INSTALLATION
IPL FIGURE 15 (SHEET 9 OF 9)
Page 10156
25-27-39 May 11/12
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
15
R –1 855649-401 0 IFE INSTL (SEE IPL FIG. 1A FOR A RF
NHA)
R –1A 855649-402 0 IFE INSTL (SEE IPL FIG. 1A FOR B RF
NHA)
R –1B 855649-403 0 IFE INSTL (SEE IPL FIG. 2A FOR C RF
NHA)
R –1C 855649-404 0 IFE INSTL (SEE IPL FIG. 2A FOR D RF
NHA)
R –1D 855649-405 0 IFE INSTL (SEE IPL FIG. 2A FOR E RF
NHA)
R –1E 855649-406 0 IFE INSTL (SEE IPL FIG. 2A FOR F RF
NHA)
R –1F 855649-419 0 IFE INSTL (SEE IPL FIG. 2A FOR G RF
NHA)
R –1G 855649-420 0 IFE INSTL (SEE IPL FIG. 2A FOR H RF
NHA)
R –1H 855649-425 0 IFE INSTL (SEE IPL FIG. 2A FOR J RF
NHA)
R –1J 855649-426 0 IFE INSTL (SEE IPL FIG. 2A FOR K RF
NHA)
INDENT
AIRLINE UNITS
FIG PART EFF
PART NOMENCLATURE PER
ITEM NUMBER CODE
NO ASSY
15
R 80 851633-003 1 RACEWAY * A-H 2
R 80A 851633-005 1 RACEWAY * J,K 1
R –80B 851633-009 1 RACEWAY * J,K 1
R 85 RDAM7902-19 1 HARNESS AY (V0FF57) ** A 1
R 90 RDAM7902-20 1 HARNESS AY (V0FF57) ** B 1
R 95 RDAM7902-58 1 HARNESS AY (V0FF57) ** C,D,J, 1
K
R 100 RDAM7902-17 1 HARNESS AY (V0FF57) ** E 1
R 105 RDAM7902-18 1 HARNESS AY (V0FF57) ** F 1
R 110 RDAM7902-38 1 HARNESS AY (V0FF57) ** G,H 1
R 115 RDAX6733-58 1 DPCU (V0FF57) ** 3
R 120 RD-AX6421-20 1 RJU (V0FF57) ** 3
R 125 RD-AX4332-01 1 SEB (V0FF57) ** 1
* INDICATED EQUIPMENT IS
COVERED UNDER WEBER
AIRCRAFT LLC TSO
** INDICATED EQUIPMENT IS
NOT COVERED UNDER WEBER
AIRCRAFT LLC TSO
REWORK
1. General
2. Rework Procedures
Page 16001
25-27-39 Feb 15/06
WEBER AIRCRAFT
COMPONENT MAINTENANCE MANUAL
PART NO. 855104, 855107, 855109, 859628, 860001, 860002
Page 16002
25-27-39 Feb 15/06
WEBER AIRCRAFT LP
SERVICE BULLETIN
1. PLANNING INFORMATION
A. Effectivity
This service bulletin is effective for the following tourist class passenger seats manufactured by
Weber Aircraft LP for AIR INDIGO, A320 airplanes.
B. Reason
This service bulletin is being generated to provide compliant type III exit seat bottom cushions.
C. Description
This service bulletin provides instructions to remove old outboard cushion assembly and install
new outboard cushion assembly.
Return removed fireblocking assembly to Weber Aircraft LP at 2000 Weber Drive, Gainesville,
Texas 76240.
D. Approval
The seats as modified by this service bulletin continue to meet the requirements of TSO-C127a.
Approval of the installation aspects of the seat assembly as modified by this service bulletin is the
responsibility of the installer.
Under seat TSO approval, optional equipment (IFE, Telephones, etc.) is approved only for that
equipment’s mass attributes and means of attachment to the seat. All other attributes of the
optional equipment are outside the scope of the seat TSO approval. It is the responsibility of the
installer of the seat into the aircraft to obtain the necessary approval and to insure
that optional equipment installed on the seat does not violate the TSO approval.
To be determined.
Contact Weber Aircraft LP, 2000 Weber Drive, Gainesville, Texas 76240, Customer Service
Department. ¯ Phone: (940) 668-4100 ¯ Fax: (940) 668-4195.
None.
Not affected.
I. References
Weber Aircraft LP Component Maintenance Manual with Illustrated Parts List 25 ---27 ---39
2. GENERAL INSTRUCTIONS
A. See the applicable reference from the above References section for disassembly and assembly
instructions and component identification not shown in this service bulletin.
B. The seats to be modified must be inspected for serviceability prior to modification. Seat integrity
after modification must meet or exceed the condition prior to modification.
C. All nonmetallic material shall meet the flame resistance requirements of 14 CFR 25.853(a) (AMDT.
25---83) unless otherwise noted.
D. It is recommended that the seat not be disassembled any further than is absolutely necessary to
accomplish instructions listed in this document.
(1) Remove existing cushion assembly. Remove and retain dress cover assembly. See Figures
1 and 2.
Return fireblocking assembly to Weber Aircraft LP.
B. Modification
(1) Using an indelible marker, remark 856263---XXX (special bottom diaphragm) placard with
new cushion assembly number as shown on new fireblocking cushion assembly placard
(854604---XXX). Cover with clear tape.
(2) Reidentify Fabric Reference with data from AC Installation BP Cushion Placard Data Block.
(1) Dress new fireblocking assembly using retained dress cover assembly.
4. REIDENTIFICATION
(1) Using the new 840304---25 modification nameplate provided in each kit, apply the following:
855xxx--- 4xx
5600
859910
859910--- 4xx
5600
5. MATERIAL INFORMATION
Figure 1
Figure 2
Approved by:
Engineering
Certification
Quality Assurance
SERVICE BULLETIN
1. PLANNING INFORMATION
A. Effectivity
This service bulletin is effective for the following tourist class passenger seats manufactured by
Weber Aircraft LLC for GEF/THY A320 airplanes, tail number MSN 3259 and MSN 3308:
B. Reason
This service bulletin is being generated to convert existing seats to GEF THY seats.
C. Description
This service bulletin provides instructions for SEB bracket and IFE installation.
D. Compliance
E. Approval
The seats as modified by this service bulletin continue to meet the requirements of original seat
TSO. Approval of the installation aspects of the seat assembly as modified by this service bulletin
is the responsibility of the installer.
Under seat TSO approval, optional equipment (IFE, Telephones, etc.) is approved only for that
equipment’s mass attributes and means of attachment to the seat. All other attributes of the
optional equipment are outside the scope of the seat TSO approval. It is the responsibility of the
installer of the seat into the aircraft to obtain the necessary approval and to ensure
that optional equipment installed on the seat does not violate the TSO approval.
F. Manpower
Contact Weber Aircraft LLC, 2000 Weber Drive, Gainesville, Texas 76240, Customer Service
Department. ¯ Phone: (940) 668-4100 ¯ Fax: (940) 668-4195.
None.
Not affected.
J. References
Weber Aircraft LLC Component Maintenance Manual with Illustrated Parts List 25 ---27 ---20 and
25 ---27 ---39
25---27---20
25---27---39
2. GENERAL INSTRUCTIONS
A. See the applicable reference from the above References section for disassembly and assembly
instructions and component identification not shown in this service bulletin.
B. The seats to be modified must be inspected for serviceability prior to modification. Seat integrity
after modification must meet or exceed the condition prior to modification.
C. All nonmetallic material shall meet the flame resistance requirements of 14 CFR 25.853(a) (AMDT.
25---83).
D. It is recommended that the seat not be disassembled any further than is absolutely necessary to
accomplish instructions listed in this document.
3. ACCOMPLISHMENT INSTRUCTIONS
(2) Retain mounting hardware, recline cables, escutcheons and armcaps (standard seats only)
for reuse with new arms.
(1) On IAT seats, install newly provided arms, using retained hardware. Reattach applicable
recline cables and escutcheons.
(2) On Standard seats, install newly provided arms, using retained hardware. Wait to reinstall
armcaps and escutcheons until IFE installation has been completed.
(1) Install SEB bracket assembly as shown in Figure 1. Bracket assembly is located on inboard
side of outboard leg.
D. IFE Installation
(2) After testing IFE equipment, install shroud assembly and applicable armcaps and
escutcheons.
4. REIDENTIFICATION
(1) Using the new 861615---003/007 modification nameplates (placards) provided in each kit,
apply the following:
S If applicable, Revision Level of Service Bulletin and Revision Date (directly below
“MODIFIED BY SERVICE BULLETIN XXXXXX---25---XXXX”)
S Weber Model No.
S Weber TSO Part No.
S Serial No. (as taken from the original nameplate)
S Modified By (organization doing the modification) / Repair Station No.: TQKY144F
S Modification Date
(2) Apply new nameplate(s) to seat baseframe as close to original nameplate as possible. Do not
remove or damage original nameplate.
5. MATERIAL INFORMATION
FIGURE 1
(SEB Bracket Assy Install)
Approved by:
Wayne Lindsey
Product Support Manager
Jimmie McGahey
Project Engineer
Will Bezner
Certification
Ken Kniss
Quality Assurance Manager