COMPONENT MAINTENANCE MANUAL

C41XXXX
5701 BOLSA AVE, HUNTINGTON BEACH, CA 92647 (CAGE NO. 56135)

REVISION TRANSMITTAL LETTER

TO:

Holders of Component Maintenance Manual (CMM) 50-11-05, revision No. 11, dated Jul 17/20.

GENERAL:

This transmittal letter is attached to the revision No. 12 of CMM 50-11-05, dated Oct 09/23.

The pages which are changed with this revision are shown in the List of Effective Pages (LEP). The type of
change is shown in the list as follows:

R This page has been revised (replaced)

D This page has been erased (removed)

N This page is new (put into the CMM)

This is a complete CMM package. Discard the previous issue and replace it with this issue, revision No. 12,
dated Oct 09/23.

REASON FOR ISSUE:

This manual has been revised to incorporate the latest design changes and update information.

The attached highlights give details of these changes.

TL

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 COMPONENT MAINTENANCE MANUAL
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HIGHLIGHTS

Revision No.12 - Oct 09/23

Pages which have been added, revised or deleted are outlined below together with the Highlights of the
Revision.

LOCATIONS DESIGNATION DESCRIPTION OF CHANGE

TITLE PAGE R

LIST OF EFFECTIVE PAGES R

INTRODUCTION R Updated Abbreviations and Unit Symbols

information.

DISASSEMBLY R Disassembly procedures revised to reflect the

changes made into the IPL section.

REPAIR R Revised Table 6001 to reflect updates.

ASSEMBLY R Assembly procedures revised to reflect the

changes made into the IPL section.

SPECIAL TOOLS, FIXTURES, R Revised Table 9002 to reflect changes made into
EQUIPMENT, AND CONSUMABLES the tables of the Cleaning and Repair sections.

DETAILED PARTS LIST

FIGURE 1 R Revised to reflect the latest engineering changes.

FIGURE 1A R Revised to update information.

FIGURE 1B R Revised to reflect the latest engineering changes.

FIGURE 1F R Revised the artwork to incorporate updates.

Revised to reflect the latest engineering changes
and update information.

FIGURE 1H R Revised to reflect the latest engineering changes

and update information.

FIGURE 1J R Revised to update information.

FIGURE 1K R Revised to reflect the latest engineering changes

and update information.

FIGURE 1L R Revised to reflect the latest engineering changes

and update information.

HLTS

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LOCATIONS DESIGNATION DESCRIPTION OF CHANGE

FIGURE 1N R Revised to reflect the latest engineering changes

and update information.

FIGURE 1Q R Revised to reflect the latest engineering changes

and update information.

FIGURE 1U R Revised to reflect the latest engineering changes

and update information.

FIGURE 1W R Revised to reflect the latest engineering changes

and update information.

FIGURE 1X R Revised to reflect the latest engineering changes

and update information.

HLTS

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SAFRAN CABIN INC.
5701 Bolsa Ave
Huntington Beach, CA 92647
USA
Telephone +1 714-934-0000
www.safran-cabin.com

(56135)

COMPONENT MAINTENANCE MANUAL

WITH
ILLUSTRATED PARTS LIST

SIDEWALL PANEL ASSEMBLY

Part Number
C411051-159 C411151-101
C411051-160 C411151-103
C411051-161 C411151-105
C411051-162 C411151-107
C411051-163 C411151-109
C411051-165 C411151-113
C411051-171
C411051-173

The technical data in this document is controlled for export under the Export Administration Regulations
(EAR), 15 CFR Parts 730-774, ECCN: 9E991. Violations of these laws can be subject to fines and
penalties under the Export Administration Act.

Copyright © 2023 Safran Cabin Inc.

This document contains proprietary information of Safran Cabin Inc., or contains proprietary
information of others, and is issued in strict confidence. Except for rights expressly granted by
contract, this document can not, in whole or in part, be duplicated, reproduced electronically or
mechanically, disclosed, or used for design or manufacturing purposes without written authorization
from Safran Cabin Inc.

WARNING: ANY WARRANTY OFFERED BY SAFRAN CABIN INC. WILL BE DEEMED NULL AND
VOID IF ITS PRODUCTS ARE USED IN AN UNINTENDED MANNER OR SHOW INDICATIONS
THAT THEY HAVE BEEN ALTERED IN ANYWAY, INCLUDING, BUT NOT LIMITED TO, USE OF
REPLACEMENT PARTS OR MAINTENANCE ACTIONS NOT PERFORMED AS OUTLINED IN THIS
MANUAL AT THE TIME AND IN THE MANNER SPECIFIED HEREIN.

TP1

Initial Issue: Nov 30/07 50-11-05 Revision No. 12

Oct 09/23
 Part Number
C411151-115 C412409-121
C411151-117 C412409-139
C411151-129 C412409-143
C411151-131 C412409-147
C411151-133 C412409-159
C411151-135 C412409-161
C411151-139 C412409-173
C411151-143 C412410-079
C411151-145 C412410-081
C411151-147 C412410-085
C411151-149 C412410-089
C411151-153 C412416-103
C411151-155 C412416-104
C411151-159 C412416-105
C411151-179 C412416-107
C411151-183 C412416-109
C411152-161 C412416-119
C411152-163 C412416-125
C411152-165 C412416-127
C411152-167 C412416-129
C411152-169 C412416-131
C411152-171 C412416-133
C411162-111 C412416-135
C411162-127 C412416-141
C411162-137 C412416-145
C412409-101 C412416-163
C412409-111 C412416-165
C412409-113 C412417-139
C412409-115 C412417-145
C412409-117 C412417-147
C412409-118
(cont.)

TP2

Initial Issue: Nov 30/07 50-11-05 Revision No. 12

Oct 09/23
 Part Number
C412418-101 C419051-101
C412418-103 C419051-102
C412418-105 C419051-103
C412418-107 C419051-104
C412418-109 C419051-105
C412418-111 C419051-106
C412418-113 C419151-143
C412418-119 C419151-155
C412418-121 C419401-153
C414051-101 C419401-157
C414051-102 C419401-159
C414151-123 C419401-171
C414401-143 C419408-101
C414408-101 C419408-103
C414408-105 C419408-105
C414408-107 C419408-107
C414408-109 C419408-109

TP 3

Initial Issue: Nov 30/07 50-11-05 Revision No. 12

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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RECORD OF REVISIONS

INSERTED INSERTED
REV. ISSUE REV. ISSUE
No. DATE DATE BY No. DATE DATE BY

Initial Issue Nov 30/07

1 Mar 10/08
2 Mar 15/09
3 Nov 05/09
4 Jul 06/10
5 Nov 18/10
6 Oct 31/11
7 Set 16/13
8 Jun 11/14
9 Apr 08/16
10 Jul 22/17
11 Jul 17/ 20
12 Oct 09/23

ROR

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RECORD OF TEMPORARY REVISIONS

TEMP. REV. INSERTED REMOVED DATE

ISSUE
No. INCORPO-
DATE
DATE BY DATE BY RATED

RTR

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SERVICE BULLETIN LIST

SERVICE BULLETIN INCORPORATION INTO CMM TITLE

Number Rev Date Rev

SBL

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LIST OF EFFECTIVE PAGES

SUBJECT PAGE DATE SUBJECT PAGE DATE

TITLE PAGE DESCRIPTION AND OPERATION -
1 R Oct 09/23 1 Jul 17/20
2 R Oct 09/23 2 Jul 17/20
3 R Oct 09/23 3 Jul 17/20
4 R Oct 09/23 4 Jul 17/20
5 Jul 17/20
RECORD OF REVISIONS 6 Jul 17/20
1 Sep 16/13 7 Jul 17/20
2 Blank Sep 16/13 8 Jul 17/20
9 Jul 17/20
RECORD OF TEMPORARY REVISIONS 10 Jul 17/20
1 Sep 16/13 11 Jul 17/20
2 Blank Sep 16/13 12 Jul 17/20
13 Jul 17/20
SERVICE BULLETIN LIST 14 Jul 17/20
1 Sep 16/13 15 Jul 17/20
2 Blank Sep 16/13 16 Jul 17/20
17 Jul 17/20
LIST OF EFFECTIVE PAGES 18 Jul 17/20
1 R Oct 09/23 19 Jul 17/20
2 R Oct 09/23 20 Jul 17/20
3 R Oct 09/23 21 Jul 17/20
4 R Oct 09/23 22 Jul 17/20
5 R Oct 09/23 23 Jul 17/20
6 R Oct 09/23 24 Jul 17/20
25 Jul 17/20
TABLE OF CONTENTS 26 Jul 17/20
1 R Oct 09/23 27 Jul 17/20
2 R Oct 09/23 28 Jul 17/20
3 R Oct 09/23 29 Jul 17/20
4 Blank Oct 09/23 30 Jul 17/20

LIST OF ILLUSTRATIONS DISASSEMBLY -

1 Oct 09/23 3001 R Oct 09/23
2 Oct 09/23 3002 R Oct 09/23
3003 R Oct 09/23
LIST OF TABLES 3004 R Oct 09/23
1 Oct 09/23 3005 R Oct 09/23
2 Blank Oct 09/23 3006 R Oct 09/23
3007 R Oct 09/23
INTRODUCTION 3008 R Oct 09/23
1 R Oct 09/23 3009 R Oct 09/23
2 R Oct 09/23 3010 R Oct 09/23
3 R Oct 09/23 3011 R Oct 09/23
4 R Oct 09/23 3012 R Oct 09/23
5 R Oct 09/23 3013 R Oct 09/23
6 Blank Oct 09/23 3014 R Oct 09/23

LEP

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LIST OF EFFECTIVE PAGES (Continued)

SUBJECT PAGE DATE SUBJECT PAGE DATE

3015 R Oct 09/23 6024 R Oct 09/23
3016 R Oct 09/23 6025 R Oct 09/23
3017 R Oct 09/23 6026 R Oct 09/23
3018 R Oct 09/23 6027 R Oct 09/23
6028 R Oct 09/23
CLEANING - 6029 R Oct 09/23
4001 Jul 17/20 6030 R Oct 09/23
4002 Jul 17/20 6031 R Oct 09/23
4003 Jul 17/20 6032 R Oct 09/23
4004 Jul 17/20 6033 R Oct 09/23
4005 Jul 17/20 6034 R Oct 09/23
4006 Jul 17/20 6035 R Oct 09/23
4007 Jul 17/20 6036 R Oct 09/23
4008 Jul 17/20 6037 R Oct 09/23
4009 Jul 17/20 6038 R Oct 09/23
4010 Jul 17/20 6039 R Oct 09/23
4011 Jul 17/20 6040 R Oct 09/23
4012 Blank Jul 17/20 6041 R Oct 09/23
6042 R Oct 09/23
INSPECTION/CHECK - 6043 R Oct 09/23
5001 Jul 17/20 6044 R Oct 09/23
5002 Blank Jul 17/20 6045 R Oct 09/23
6046 R Oct 09/23
REPAIR - 6047 R Oct 09/23
6001 R Oct 09/23 6048 R Oct 09/23
6002 R Oct 09/23 6049 R Oct 09/23
6003 R Oct 09/23 6050 Blank Oct 09/23
6004 R Oct 09/23
6005 R Oct 09/23 ASSEMBLY -
6006 R Oct 09/23 7001 R Oct 09/23
6007 R Oct 09/23 7002 R Oct 09/23
6008 R Oct 09/23 7003 R Oct 09/23
6009 R Oct 09/23 7004 R Oct 09/23
6010 R Oct 09/23 7005 R Oct 09/23
6011 R Oct 09/23 7006 R Oct 09/23
6012 R Oct 09/23 7007 R Oct 09/23
6013 R Oct 09/23 7008 R Oct 09/23
6014 R Oct 09/23 7009 R Oct 09/23
6015 R Oct 09/23 7010 R Oct 09/23
6016 R Oct 09/23 7011 R Oct 09/23
6017 R Oct 09/23 7012 R Oct 09/23
6018 R Oct 09/23 7013 R Oct 09/23
6019 R Oct 09/23 7014 R Oct 09/23
6020 R Oct 09/23 7015 R Oct 09/23
6021 R Oct 09/23 7016 R Oct 09/23
6022 R Oct 09/23 7017 R Oct 09/23
6023 R Oct 09/23 7018 R Oct 09/23

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LIST OF EFFECTIVE PAGES (Continued)

SUBJECT PAGE DATE SUBJECT PAGE DATE

SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND 10026 R Oct 09/23
CONSUMABLES - 10027 R Oct 09/23
9001 R Oct 09/23 10028 R Oct 09/23
9002 R Oct 09/23 10029 R Oct 09/23
9003 R Oct 09/23 10030 R Oct 09/23
9004 R Oct 09/23 10031 R Oct 09/23
9005 R Oct 09/23 10032 R Oct 09/23
9006 R Oct 09/23 10033 R Oct 09/23
9007 R Oct 09/23 10034 R Oct 09/23
9008 R Oct 09/23 10035 R Oct 09/23
9009 R Oct 09/23 10036 R Oct 09/23
9010 Blank Oct 09/23 10037 R Oct 09/23
10038 R Oct 09/23
STORAGE (INCLUDING TRANSPORTATION) - 10039 R Oct 09/23
15001 Sep 16/13 10040 R Oct 09/23
15002 Blank Sep 16/13 10041 R Oct 09/23
10042 R Oct 09/23
ILLUSTRATED PARTS LIST (IPL) 10043 R Oct 09/23
10001 R Oct 09/23 10044 R Oct 09/23
10002 Blank Oct 09/23 10045 R Oct 09/23
10046 R Oct 09/23
INTRO IPL 10047 R Oct 09/23
10003 R Oct 09/23 10048 R Oct 09/23
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10005 R Oct 09/23 10050 R Oct 09/23
10006 R Oct 09/23 10051 R Oct 09/23
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10060 R Oct 09/23
ALPHA/NUMERIC INDEX 10061 R Oct 09/23
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10017 R Oct 09/23 10064 R Oct 09/23
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10136 R Oct 09/23
DETAILED PARTS LIST 10137 R Oct 09/23
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 COMPONENT MAINTENANCE MANUAL
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TABLE OF CONTENTS
PAGE
INTRODUCTION .............................................................................................................................. INTRO 1
1. Scope ........................................................................................................................................ INTRO 1
2. Product Support Services ......................................................................................................... INTRO 1
3. Usage Guide ............................................................................................................................. INTRO 2
4. Abbreviations and Unit Symbols ............................................................................................... INTRO 2
5. Dates of Shop Verification by Actual Performance ................................................................... INTRO 5

DESCRIPTION AND OPERATION - ............................................................................................... 1

1. Description ................................................................................................................................ 1
A. Sidewall Panel Assembly ................................................................................................... 1
2. Leading Particulars ................................................................................................................... 2
3. Operation .................................................................................................................................. 30

TESTING AND FAULT ISOLATION ................................................................................ NOT APPLICABLE

SCHEMATIC AND WIRING DIAGRAMS ........................................................................ NOT APPLICABLE

DISASSEMBLY - ............................................................................................................................. 3001

1. General ..................................................................................................................................... 3001
2. Disassembly Procedures .......................................................................................................... 3001
A. Shroud Assembly (IPL Figure 1) ........................................................................................ 3001
B. Shroud Assembly (IPL Figure 1A) ..................................................................................... 3001
C. Sloping Sidewall Liner Assembly (IPL Figure 1B) .............................................................. 3002
D. Bulk Sloping Sidewall Panel Assembly (IPL Figure 1C) .................................................... 3002
E. Bulk Sloper Bracket Assembly (IPL Figure 1D) ................................................................. 3003
F. Bulk Endwall Assembly (IPL Figure 1E) - Deleted Figure .................................................. 3003
G. Vertical Sidewall Panel Assembly (IPL Figure 1F) ............................................................. 3003
H. Vertical Sidewall Panel Assembly (IPL Figure 1G) ............................................................ 3004
I. Vertical Sidewall Panel Assembly (IPL Figure 1H) ............................................................ 3004
J. Vertical Sidewall Panel Assembly (IPL Figure 1J) ............................................................. 3005
K. Vertical Sidewall Panel Assembly (IPL Figure 1K) ............................................................. 3006
L. Vertical Sidewall Panel Assembly (IPL Figure 1L) ............................................................. 3007
M. Vertical Sidewall Panel Assembly (IPL Figure 1M) ............................................................ 3008
N. Vertical Sidewall Panel Assembly (IPL Figure 1N) ............................................................ 3008
O. Vertical Sidewall Panel Assembly (IPL Figure 1P) ............................................................. 3010
P. Vertical Sidewall Panel Assembly (IPL Figure 1Q) ............................................................ 3011
Q. Vertical Sidewall Panel Assembly (IPL Figure 1R) ............................................................ 3012
R. Vertical Sidewall Panel Assembly (IPL Figure 1S) ............................................................. 3012
S. Vertical Sidewall Vent Liner Assembly (IPL Figure 1T) ...................................................... 3012
T. Vertical Sidewall Panel Assembly (IPL Figure 1U) ............................................................ 3013
U. Vertical Sidewall Panel Assembly (IPL Figure 1V) ............................................................. 3014
V. Vertical Sidewall Panel Assembly (IPL Figure 1W) ............................................................ 3015
W. Vertical Sidewall Panel Assembly (IPL Figure 1X) ............................................................. 3016
X. Vertical Sidewall Panel Assembly (IPL Figure 1Y) ............................................................. 3017
Y. Vertical Sidewall Panel Assembly (IPL Figure 1Z) ............................................................. 3018

CLEANING - .................................................................................................................................... 4001

1. General ..................................................................................................................................... 4001

TOC

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TABLE OF CONTENTS (Continued)
PAGE
2. Safety Precautions .................................................................................................................... 4003
3. Cleaning Procedures ................................................................................................................. 4003
A. General Surface Cleaning (Including Vinyl-Decor Covered Panels) .................................. 4003
B. Cleaning Instructions and Material Specifications for Metal Parts ..................................... 4006
C. Cleaning Instructions for Adhesives .................................................................................. 4009
4. Metal Preservation and Corrosion Inhibition ............................................................................. 4010

INSPECTION/CHECK - ................................................................................................................... 5001

1. General ..................................................................................................................................... 5001
2. Component Inspection/Checks ................................................................................................. 5001

REPAIR - ......................................................................................................................................... 6001

1. General ..................................................................................................................................... 6001
2. Replace or Install Bonded Components .................................................................................... 6008
3. Replace Potted Inserts .............................................................................................................. 6010
4. Fill and Relocate the Insert Holes ............................................................................................. 6015
5. Replace Adhesive-Backed Rubstrip or Placard ........................................................................ 6016
6. Repair Corrosion and Restore Metal ......................................................................................... 6017
7. Repair Fiberglass Composite Panel .......................................................................................... 6027
8. Fill Edge Holes in Honeycomb Panels ...................................................................................... 6043
9. Fill and Fair out Procedures for Panel ....................................................................................... 6043
10. Paint and Prime the Composite Panels .................................................................................... 6045

ASSEMBLY - ................................................................................................................................... 7001

1. General ..................................................................................................................................... 7001
2. Assembly Procedures ............................................................................................................... 7001
A. Shroud Assembly (IPL Figure 1) ........................................................................................ 7001
B. Shroud Assembly (IPL Figure 1A) ..................................................................................... 7001
C. Sloping Sidewall Liner Assembly (IPL Figure 1B) .............................................................. 7002
D. Bulk Sloping Sidewall Panel Assembly (IPL Figure 1C) .................................................... 7002
E. Bulk Sloper Bracket Assembly (IPL Figure 1D) ................................................................. 7003
F. Bulk Endwall Assembly (IPL Figure 1E) - Deleted Figure .................................................. 7003
G. Vertical Sidewall Panel Assembly (IPL Figure 1F) ............................................................. 7003
H. Vertical Sidewall Panel Assembly (IPL Figure 1G) ............................................................ 7004
I. Vertical Sidewall Panel Assembly (IPL Figure 1H) ............................................................ 7004
J. Vertical Sidewall Panel Assembly (IPL Figure 1J) ............................................................. 7005
K. Vertical Sidewall Panel Assembly (IPL Figure 1K) ............................................................. 7006
L. Vertical Sidewall Panel Assembly (IPL Figure 1L) ............................................................. 7007
M. Vertical Sidewall Panel Assembly (IPL Figure 1M) ............................................................ 7008
N. Vertical Sidewall Panel Assembly (IPL Figure 1N) ............................................................ 7008
O. Vertical Sidewall Panel Assembly (IPL Figure 1P) ............................................................. 7010
P. Vertical Sidewall Panel Assembly (IPL Figure 1Q) ............................................................ 7011
Q. Vertical Sidewall Panel Assembly (IPL Figure 1R) ............................................................ 7012
R. Vertical Sidewall Panel Assembly (IPL Figure 1S) ............................................................. 7012
S. Vertical Sidewall Vent Liner Assembly (IPL Figure 1T) ...................................................... 7012
T. Vertical Sidewall Panel Assembly (IPL Figure 1U) ............................................................ 7013
U. Vertical Sidewall Panel Assembly (IPL Figure 1V) ............................................................. 7014
V. Vertical Sidewall Panel Assembly (IPL Figure 1W) ............................................................ 7015

TOC

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TABLE OF CONTENTS (Continued)
PAGE
W. Vertical Sidewall Panel Assembly (IPL Figure 1X) ............................................................. 7016
X. Vertical Sidewall Panel Assembly (IPL Figure 1Y) ............................................................. 7017
Y. Vertical Sidewall Panel Assembly (IPL Figure 1Z) ............................................................. 7018

FITS AND CLEARANCES ............................................................................................... NOT APPLICABLE

SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES - ......................................... 9001

1. General ..................................................................................................................................... 9001

STORAGE (INCLUDING TRANSPORTATION) - ............................................................................ 15001

1. Storage Instructions .................................................................................................................. 15001

ILLUSTRATED PARTS LIST (IPL) ................................................................................................... 10001

1. General ..................................................................................................................................... 10003
2. Scope of Information ................................................................................................................. 10003
3. Equipment Designator Index ..................................................................................................... 10003
4. Numerical Index ........................................................................................................................ 10003
5. Explanation of Detailed Parts List Entries ................................................................................. 10004
6. Manufacturer's Names and Addresses ..................................................................................... 10006

Manufacturer’s Names and Addresses ..................................................................................... 10007

Alpha/Numeric Index ................................................................................................................. 10015

Detailed Parts List ..................................................................................................................... 10091

TOC

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LIST OF ILLUSTRATIONS

FIGURE TITLE PAGE

1 Sidewall Panel Assembly ............................................................................................ 21
6001 Insert Installation with Potting Compound .................................................................. 6014
6002 Fill and Relocate the Insert holes ............................................................................... 6016
6003 Damage in Honeycomb Panels .................................................................................. 6028
6004 Potting Compound or Solid Repair ............................................................................. 6038
6005 Scarf Repair Procedure .............................................................................................. 6038
6006 Taper Scarf Repair ...................................................................................................... 6042
6007 Criss-Cross Pattern .................................................................................................... 6047
6008 1- ½+ Criss-Cross Pattern .......................................................................................... 6049

Detailed Parts List

1 Shroud Assembly ........................................................................................................ 10092

1A Shroud Assembly ........................................................................................................ 10102
1B Sloping Sidewall Liner Assembly ................................................................................ 10106
1C Bulk Sloping Sidewall Panel Assembly ....................................................................... 10116
1D Bulk Sloper Bracket Assembly .................................................................................... 10122
1E Bulk Endwall Assembly ............................................................................................... 10124
1F Vertical Sidewall Panel Assembly ............................................................................... 10130
1G Vertical Sidewall Panel Assembly ............................................................................... 10134
1H Vertical Sidewall Panel Assembly ............................................................................... 10140
1J Vertical Sidewall Panel Assembly ............................................................................... 10146
1K Vertical Sidewall Panel Assembly ............................................................................... 10152
1L Vertical Sidewall Panel Assembly ............................................................................... 10158
1M Vertical Sidewall Panel Assembly ............................................................................... 10162
1N Vertical Sidewall Panel Assembly ............................................................................... 10166
1P Vertical Sidewall Panel Assembly ............................................................................... 10174
1Q Vertical Sidewall Panel Assembly ............................................................................... 10180
1R Vertical Sidewall Panel Assembly ............................................................................... 10188
1S Vertical Sidewall Panel Assembly ............................................................................... 10192
1T Vertical Sidewall Vent Liner Assembly ........................................................................ 10196
1U Vertical Sidewall Panel Assembly ............................................................................... 10200
1V Vertical Sidewall Panel Assembly ............................................................................... 10206
1W Vertical Sidewall Panel Assembly ............................................................................... 10210
1X Vertical Sidewall Panel Assembly ............................................................................... 10216
1Y Vertical Sidewall Panel Assembly ............................................................................... 10222
1Z Vertical Sidewall Panel Assembly ............................................................................... 10226
2 Vertical Sidewall Panel Assembly ............................................................................... 10230
2A Vertical Sidewall Panel Assembly ............................................................................... 10234
2B Sloping Sidewall Liner Assembly ................................................................................ 10238
2C Section 41 Vertical Sidewall Assembly ....................................................................... 10240
2D Section 41 Vertical Sidewall Assembly ....................................................................... 10244
2E Section 41 Vertical Sidewall Assembly ....................................................................... 10248
2F Section 41 Vertical Sidewall Assembly ....................................................................... 10252
2G Section 43 Vertical Sidewall Assembly ....................................................................... 10256
2H Section 43 Vertical Sidewall Assembly ....................................................................... 10258
2J Section 43 Vertical Sidewall Assembly ....................................................................... 10262
2K Section 43 Vertical Sidewall Assembly ....................................................................... 10266

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LIST OF ILLUSTRATIONS (Continued)

FIGURE TITLE PAGE

2L Section 43 Vertical Sidewall Assembly ....................................................................... 10270
2M Section 43 Vertical Sidewall Assembly ....................................................................... 10274
2N Section 43 Vertical Sidewall Assembly ....................................................................... 10278
2P Section 43 Vertical Sidewall Assembly ....................................................................... 10282
2Q Section 41 Vertical Sidewall Assembly ....................................................................... 10284
2R Section 41 Vertical Sidewall Assembly ....................................................................... 10288
2S Section 46 Vertical Sidewall Assembly ....................................................................... 10292
2T Vertical Sidewall Panel Assembly ............................................................................... 10296
2U Section 46 Vertical Sidewall Assembly ....................................................................... 10300
2V Vertical Sidewall Panel Assembly ............................................................................... 10304
2W Section 46 Vertical Sidewall Assembly ....................................................................... 10306
2X Vertical Sidewall Panel Assembly ............................................................................... 10310
2Y Vertical Sidewall Panel Assembly ............................................................................... 10312
2Z Vertical Sidewall Panel Assembly ............................................................................... 10316
3 Vertical Sidewall Panel Assembly ............................................................................... 10320
3A Vertical Sidewall Panel Assembly ............................................................................... 10324
3B Vertical Sidewall Panel Assembly ............................................................................... 10328
3C Sloping Sidewall Panel Assembly ............................................................................... 10332
3D Vertical Sidewall Panel Assembly ............................................................................... 10334
3E Vertical Sidewall Panel Assembly ............................................................................... 10338
3F Vertical Sidewall Panel Assembly ............................................................................... 10342
3G Vertical Sidewall Panel Assembly ............................................................................... 10346

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LIST OF TABLES

TABLE TITLE PAGE

1 Leading Particulars ..................................................................................................... 2
4001 Cleaning Tools and Materials ...................................................................................... 4001
5001 Inspection/Check Procedures ..................................................................................... 5001
6001 Repair Materials .......................................................................................................... 6002
6002 Adhesive Cure Time ................................................................................................... 6012
6003 Properties of Corrosion-Inhibition Compound (CIC) Materials ................................... 6025
9001 Special Tools, Fixtures, and Equipment ...................................................................... 9001
9002 Consumables .............................................................................................................. 9002

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INTRODUCTION

TASK 50-11-05-99F-801-A01
1. Scope

A. This Component Maintenance Manual (CMM) contains maintenance instructions and lists
replacement parts for the Sidewall Panel Assembly, PNs C411051-159, C411051-160, C411051-161,
C411051-162, C411051-163, C411051-165, C411051-171, C411051-173, C411151-101,
C411151-103, C411151-105, C411151-107, C411151-109, C411151-113, C411151-115, C411151-117,
C411151-129, C411151-131, C411151-133, C411151-135, C411151-139,C411151-143, C411151-145,
C411151-147, C411151-149, C411151-153, C411151-155, C411151-159, C411151-179, C411151-183,
C411152-161, C411152-163, C411152-165, C411152-167, C411152-169, C411152-171, C411162-111,
C411162-127, C411162-137, C412409-101, C412409-111, C412409-113, C412409-115,
C412409-117, C412409-118, C412409-121, C412409-139, C412409-143, C412409-147,
C412409-159, C412409-161, C412409-173, C412410-079, C412410-081, C412410-085,
C412410-089, C412416-103, C412416-104, C412416-105, C412416-107, C412416-109,
C412416-119, C412416-125, C412416-127, C412416-129, C412416-131, C412416-133,
C412416-135, C412416-141, C412416-145, C412416-163, C412416-165, C412417-139,
C412417-145, C412417-147, C412418-101, C412418-103, C412418-105, C412418-107,
C412418-109, C412418-111, C412418-113, C412418-119, C412418-121, C414051-101,
C414051-102, C414151-123, C414401-143, C414408-101, C414408-105, C414408-107,
C414408-109, C419051-101, C419051-102, C419051-103, C419051-104, C419051-105,
C419051-106, C419151-143,C419151-155, C419401-153, C419401-157, C419401-159,
C419401-171, C419408-101, C419408-103, C419408-105, C419408-107, and C419408-109.

B. This document agrees with the AIR TRANSPORT ASSOCIATION of AMERICA, and shows the
newest data.

C. This manual uses the task and subtask identification of the Maintenance Task Oriented Support
System (MTOSS). The maintenance tasks and other data have special MTOSS numbers for the use
of Electronic Data Processing (EDP).

TASK 50-11-05-99F-802-A01
2. Product Support Services

Replacement parts, technical publications, and other product support services are available from Safran
Cabin Inc. Please refer to:

Safran Cabin Inc. Telephone: (657) 227-5505

7330 Lincoln Way
Garden Grove, CA 92841
USA
(V56135)

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TASK 50-11-05-99F-803-A01
3. Usage Guide

A. Refer to the TABLE OF CONTENTS to find the applicable maintenance procedures or other data.

(1) DESCRIPTION AND OPERATION section gives the function, primary components, operation,
and properties of the Sidewall Panel Assembly.

(2) DISASSEMBLY section gives special procedures to disassemble the Sidewall Panel Assembly
for the repair or parts replacement.

(3) CLEANING section gives procedures to clean the components of the Sidewall Panel Assembly.

(4) INSPECTION/CHECK section gives procedures to examine parts for damaged or worn parts..

(5) REPAIR section gives procedures to replace potted inserts, replace bonded components, and
make other repairs.

(6) ASSEMBLY section gives special procedures to assemble the Sidewall Panel Assembly.

(7) SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES section gives the
recommended special tools, fixtures, test equipment and consumable materials used in this
manual.

(8) ILLUSTRATED PARTS LIST (IPL) section contains the data necessary to order the replacement
parts. An equipment designator index, a numerical index, and exploded-view illustrations agree
to the parts lists to help find and identify the parts. The introduction gives more data.

(9) STORAGE (INCLUDING TRANSPORTATION) section gives the special procedures to storage
the Sidewall Panel Assembly.

B. The sections give a table of recommended tools and materials, when applicable. Use of equivalent
items is possible.

TASK 50-11-05-99F-804-A01
4. Abbreviations and Unit Symbols

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 / Term
Abbreviation

% Percent

– Not Illustrated

° Degrees

°C Degrees Celsius

°F Degrees Fahrenheit

< Less than

INTRO

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> Greater than

± Plus or Minus

© Copyright Sign

® Registered Sign

™ Trade Mark

(-) Negative charge

ALT Alternate

AR As Required

ASSY Assembly

ATA Air Transport Association

CAGE Commercial And Government Entity

CAS Chemical Abstracts Service

CFM Cubic Feet per Minute

CIC Corrosion Inhibiting Compounds

cm Centimeter (1 cm = 0.394 in)

CMM Component Maintenance Manual

Co. Company

Corp. Corporation

CT Crew Terminal

DET Detail

Div. Division

EAR Export Administration Regulations

ECCN Export Control Classification Number

EDP Electronic Data Processing

EFFECT Effectivity

ESD Electrostatic Discharge

FDA Food and Drug Administration

Fed. Federal

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FIG. Figure

FR Fluid Resistant

FWD Forward

g Grams (1 g = 0.002 lb)

H.V.L.P. High Volume Low Pressure

Hrs Hours

ID Identification

in Inch

INBD Inboard

Inc. Incorporated

IPL Illustrated Parts List

kg Kilogram (1 kg = 2.205 lb)

kPa Kilopascal (1 kPa = 0.145 psi)

LAV Lavatory

lb Pound

lbf-in Pound Force Inch

LLC Limited Liability Company

Ltd. Limited Company

MEK Methyl Ethyl Ketone

Mfg. Manufacturing

MIL Military

min Minutes

ml Milliliter (1 ml = 0.034 oz)

MSDS Material Safety Data Sheets

MTOSS Maintenance Task Oriented Support System

N/A Not Applicable

NHA Next Higher Assembly

N-m Newton Meter

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No. Number

OPT Optional

OUTBD Outboard

oz Ounces

PN Part Number

psi Pound per Square Inch

REQ'D Required

REV. Revision

RF Reference

RPLD Replaced

RPLS Replaces

SB Service Bulletin

SEC Section

Spec. Specification

STA Station

SUBASSY Subassembly

SUPSD Superseded

SUPSDS Supersedes

TEMP. Temporary

USDA United States Department of Agriculture

TASK 50-11-05-99F-805-A01
5. Dates of Shop Verification by Actual Performance

Testing and Fault Isolation Not Applicable

Disassembly Verified Oct 04/23
Assembly Verified Oct 04/23
Engineering Technical Review Completed Oct 04/23

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DESCRIPTION AND OPERATION

TASK 50-11-05-870-801-A01
1. Description

A. Sidewall Panel Assembly

(1) The Figure 1 gives the arrangements of the Sidewall Panel Assemblies. The Sidewall Panel
contains the items given below:

(a) Sidewall Extrusion.

(b) Plastic Spacer.

(c) Cover Strip.

(d) Vertical Sidewall Liner.

(e) Doubler Strip.

(f) Quarter Turn Fastener Assembly.

(g) Hook Fastener.

(h) Loop Fastener.

(i) Reinforcement Strip.

(j) Clip-on Nuts.

(k) Foam Seal.

(l) Liner Strip Sidewall.

(m) Ball Latch Assembly.

(n) Angle.

(o) Decompression Panel Assembly.

(p) Nutplate.

(q) Water dam liner.

(2) Install the Sidewall Panel Panels with attaching parts.

(3) The Sidewall Panel Assemblies are made of lightweight panels bonded together with aerospace
adhesive. Brackets, doublers, and other fittings give added structural strength. Most of the
components are attached with standard hardware threaded into inserts potted in the panels.
Other components are bonded to the panels with aerospace adhesive.

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TASK 50-11-05-870-802-A01
2. Leading Particulars

A. Table 1 gives the technical properties of the Sidewall Panel Assembly.

Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01

Property Specification
Description
Manufacturer Safran Cabin Inc. (CAGE 56135)
Nomenclature Sidewall Panel Assembly
Part Number C411051-159
Overall Dimensions
Weight 0.25 lb (0.11 kg)
Length 9.5 in (24.13 cm)
Width 5.75 in (14.61 cm)
Part Number C411051-160
Overall Dimensions
Weight 0.25 lb (0.11 kg)
Length 9.21 in (23.39 cm)
Width 5.76 in (14.63 cm)
Part Number C411051-161
Overall Dimensions
Weight 0.45 lb (0.2 kg)
Length 8.16 in (20.73 cm)
Width 4.21 in (10.69 cm)
Part Number C411051-162
Overall Dimensions
Weight 0.45 lb (0.2 kg)
Length 8.29 in (21.06 cm)
Width 4.21 in (10.69 cm)
Part Number C411051-163
Overall Dimensions
Weight 1.29 lb (0.59 kg)
Length 12.6 in (32 cm)
Width 10.99 in (27.91 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C411051-165
Overall Dimensions
Weight 1.26 lb (0.57 kg)
Length 12.6 in (32 cm)
Width 11.13 in (28.27 cm)
Part Number C411051-171
Overall Dimensions
Weight 0.08 lb (0.04 kg)
Length 4.71 in (11.96 cm)
Width 3.85 in (9.78 cm)
Part Number C411051-173
Overall Dimensions
Weight 0.05 lb (0.02 kg)
Length 4.48 in (11.38 cm)
Width 3.74 in (9.5 cm)
Part Number C411151-101
Overall Dimensions
Weight 1.97 lb (0.89 kg)
Length 128.38 in (326.09 cm)
Width 29.33 in (74.5 cm)
Part Number C411151-103
Overall Dimensions
Weight 1.56 lb (0.71 kg)
Length 98.82 in (251 cm)
Width 24.22 in (61.52 cm)
Part Number C411151-105
Overall Dimensions
Weight 1.56 lb (0.71 kg)
Length 98.78 in (250.9 cm)
Width 24.35 in (61.85 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C411151-107
Overall Dimensions
Weight 1.56 lb (0.71 kg)
Length 98.76 in (250.85 cm)
Width 24.31 in (61.75 cm)
Part Number C411151-109
Overall Dimensions
Weight 1.28 lb (0.58 kg)
Length 85.25 in (216.54 cm)
Width 24.34 in (61.82 cm)
Part Number C411151-113
Overall Dimensions
Weight 1.19 lb (0.54 kg)
Length 74.78 in (189.94 cm)
Width 24.34 in (61.82 cm)
Part Number C411151-115
Overall Dimensions
Weight 1.58 lb (0.72 kg)
Length 98.76 in (250.86 cm)
Width 24.34 in (61.82 cm)
Part Number C411151-117
Overall Dimensions
Weight 1.28 lb (0.58 kg)
Length 85.24 in (216.51 cm)
Width 24.31 in (61.75 cm)
Part Number C411151-129
Overall Dimensions
Weight 2.44 lb (1.11 kg)
Length 98.79 in (250.93 cm)
Width 24.27 in (61.65 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C411151-131
Overall Dimensions
Weight 1.6 lb (0.73 kg)
Length 98.79 in (250.93 cm)
Width 24.19 in (61.44 cm)
Part Number C411151-133
Overall Dimensions
Weight 1.26 lb (0.57 kg)
Length 77.5 in (196.85 cm)
Width 24.86 in (63.14 cm)
Part Number C411151-135
Overall Dimensions
Weight 1.28 lb (0.58 kg)
Length 81.89 in (208 cm)
Width 28.2 in (71.63 cm)
Part Number C411151-139
Overall Dimensions
Weight 0.68 lb (0.31 kg)
Length 37.54 in (95.35 cm)
Width 25.07 in (63.68 cm)
Part Number C411151-143
Overall Dimensions
Weight 1.11 lb (0.5 kg)
Length 39.69 in (100.81 cm)
Width 24.36 in (61.87 cm)
Part Number C411151-145
Overall Dimensions
Weight 1.05 lb (0.48 kg)
Length 39.43 in (100.16 cm)
Width 24.26 in (61.62 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C411151-147
Overall Dimensions
Weight 1.07 lb (0.49 kg)
Length 37.92 in (96.32 cm)
Width 24.93 in (63.32 cm)
Part Number C411151-149
Overall Dimensions
Weight 1.07 lb (0.49 kg)
Length 38.03 in (96.6 cm)
Width 24.88 in (63.2 cm)
Part Number C411151-153
Overall Dimensions
Weight 0.42 lb (0.19 kg)
Length 28.16 in (71.53 cm)
Width 25.4 in (64.52 cm)
Part Number C411151-155
Overall Dimensions
Weight 0.32 lb (0.15 kg)
Length 25.98 in (65.99 cm)
Width 16.74 in (42.52 cm)
Part Number C411151-159
Overall Dimensions
Weight 26.35 lb (11.95 kg)
Length 109.62 in (278.43 cm)
Width 32.22 in (81.84 cm)
Part Number C411151-179
Overall Dimensions
Weight 1.7 lb (0.77 kg)
Length 39.17 in (99.49 cm)
Width 23.94 in (60.81 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C411151-183
Overall Dimensions
Weight 1.61 lb (0.73 kg)
Length 39.13 in (99.39 cm)
Width 23.81 in (60.48 cm)
Part Number C411152-161
Overall Dimensions
Weight 0.44 lb (0.2 kg)
Length 25.65 in (65.15 cm)
Width 3.32 in (8.43 cm)
Part Number C411152-163
Overall Dimensions
Weight 0.58 lb (0.26 kg)
Length 30.8 in (78.23 cm)
Width 3.56 in (9.04 cm)
Part Number C411152-165
Overall Dimensions
Weight 0.63 lb (0.29 kg)
Length 36.4 in (92.46 cm)
Width 3.62 in (9.19 cm)
Part Number C411152-167
Overall Dimensions
Weight 0.49 lb (0.22 kg)
Length 26.16 in (66.45 cm)
Width 4.99 in (12.67 cm)
Part Number C411152-169
Overall Dimensions
Weight 0.56 lb (0.25 kg)
Length 30.56 in (77.62 cm)
Width 3.2 in (8.13 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C411152-171
Overall Dimensions
Weight 0.64 lb (0.29 kg)
Length 36.24 in (92.05 cm)
Width 3.42 in (8.69 cm)
Part Number C411162-111
Overall Dimensions
Weight 0.85 lb (0.39 kg)
Length 55.5 in (140.97 cm)
Width 20.81 in (52.86 cm)
Part Number C411162-127
Overall Dimensions
Weight 1.25 lb (0.57 kg)
Length 81.88 in (207.98 cm)
Width 28.6 in (72.64 cm)
Part Number C411162-137
Overall Dimensions
Weight 0.9 lb (0.41 kg)
Length 50.5 in (128.27 cm)
Width 24.89 in (63.22 cm)
Part Number C412409-101
Overall Dimensions
Weight 4.97 lb (2.26 kg)
Length 49.55 in (125.86 cm)
Width 55.79 in (141.71 cm)
Part Number C412409-111
Overall Dimensions
Weight 4.2 lb (1.9 kg)
Length 73 in (185.42 cm)
Width 49.69 in (126.21 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C412409-113
Overall Dimensions
Weight 4.15 lb (1.88 kg)
Length 73 in (185.42 cm)
Width 49.55 in (125.86 cm)
Part Number C412409-115
Overall Dimensions
Weight 8.44 lb (3.83 kg)
Length 74.01 in (187.99 cm)
Width 49.55 in (125.86 cm)
Part Number C412409-117
Overall Dimensions
Weight 1.36 lb (0.62 kg)
Length 36.5 in (92.71 cm)
Width 49.55 in (125.86 cm)
Part Number C412409-118
Overall Dimensions
Weight 1.35 lb (0.61 kg)
Length 36.49 in (92.69 cm)
Width 49.55 in (125.86 cm)
Part Number C412409-121
Overall Dimensions
Weight 1.04 lb (0.47 kg)
Length 19 in (48.26 cm)
Width 50.65 in (128.66 cm)
Part Number C412409-139
Overall Dimensions
Weight 6.37 lb (2.89 kg)
Length 54 in (137.16 cm)
Width 48.84 in (124.06 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C412409-143
Overall Dimensions
Weight 4.43 lb (2.01 kg)
Length 49 in (124.46 cm)
Width 49.62 in (126.03 cm)
Part Number C412409-147
Overall Dimensions
Weight 1.02 lb (0.46 kg)
Length 18.54 in (47.09 cm)
Width 49.85 in (126.62 cm)
Part Number C412409-159
Overall Dimensions
Weight 0.89 lb (0.4 kg)
Length 25.05 in (63.63 cm)
Width 50.7 in (128.78 cm)
Part Number C412409-161
Overall Dimensions
Weight 1.06 lb (0.48 kg)
Length 26 in (66.04 cm)
Width 50.65 in (128.65 cm)
Part Number C412409-173
Overall Dimensions
Weight 1.01 lb (0.46 kg)
Length 19 in (48.26 cm)
Width 50.65 in (128.65 cm)
Part Number C412410-079
Overall Dimensions
Weight 0.16 lb (0.073 kg)
Length 13.19 in (33.5 cm)
Width 26 in (66.04 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C412410-081
Overall Dimensions
Weight 0.14 lb (0.06 kg)
Length 12.51 in (31.78 cm)
Width 25.95 in (65.91 cm)
Part Number C412410-085
Overall Dimensions
Weight 0.17 lb (0.08 kg)
Length 13.34 in (33.88 cm)
Width 27 in (68.58 cm)
Part Number C412410-089
Overall Dimensions
Weight 0.16 lb (0.07 kg)
Length 13.34 in (33.88 cm)
Width 26 in (66.04 cm)
Part Number C412416-103
Overall Dimensions
Weight 1.45 lb (0.66 kg)
Length 50.71 in (128.8 cm)
Width 30.37 in (77.14 cm)
Part Number C412416-104
Overall Dimensions
Weight 1.46 lb (0.66 kg)
Length 50.68 in (128.73 cm)
Width 30.31 in (76.99 cm)
Part Number C412416-105
Overall Dimensions
Weight 5.05 lb (2.29 kg)
Length 75.66 in (192.18 cm)
Width 50.66 in (128.68 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C412416-107
Overall Dimensions
Weight 3 lb (1.36 kg)
Length 73.02 in (185.47 cm)
Width 50.66 in (128.68 cm)
Part Number C412416-109
Overall Dimensions
Weight 1.42 lb (0.64 kg)
Length 50.71 in (128.8 cm)
Width 30.31 in (76.99 cm)
Part Number C412416-119
Overall Dimensions
Weight 6.38 lb (2.89 kg)
Length 55.79 in (141.71 cm)
Width 49.55 in (125.86 cm)
Part Number C412416-125
Overall Dimensions
Weight 4.96 lb (2.25 kg)
Length 76.16 in (193.45 cm)
Width 49.5 in (125.73 cm)
Part Number C412416-127
Overall Dimensions
Weight 3.36 lb (1.52 kg)
Length 75.66 in (192.18 cm)
Width 49.55 in (125.86 cm)
Part Number C412416-129
Overall Dimensions
Weight 3.2 lb (1.45 kg)
Length 75.66 in (192.18 cm)
Width 49.55 in (125.86 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C412416-131
Overall Dimensions
Weight 6.51lb (2.95 kg)
Length 80.96 in (205.64 cm)
Width 49.65 in (126.11 cm)
Part Number C412416-133
Overall Dimensions
Weight 4.17 lb (1.89 kg)
Length 52.16 in (132.49 cm)
Width 49.66 in (126.14 cm)
Part Number C412416-135
Overall Dimensions
Weight 5.55 lb (2.52 kg)
Length 71.87 in (182.55 cm)
Width 49.11 in (124.74 cm)
Part Number C412416-141
Overall Dimensions
Weight 5.28 lb (2.39 kg)
Length 80.99 in (205.71 cm)
Width 49.66 in (126.14 cm)
Part Number C412416-145
Overall Dimensions
Weight 1.55 lb (0.7 kg)
Length 50.69 in (128.75 cm)
Width 30.3 in (76.96 cm)
Part Number C412416-163
Overall Dimensions
Weight 3.71 lb (1.68 kg)
Length 46.85 in (119 cm)
Width 28.81 in (73.18 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C412416-165
Overall Dimensions
Weight 3.8 lb (1.72 kg)
Length 43.24 in (109.83 cm)
Width 33.53 in (85.17 cm)
Part Number C412417-139
Overall Dimensions
Weight 6.4 lb (2.9 kg)
Length 54.02 in (137.21 cm)
Width 50.33 in (127.84 cm)
Part Number C412417-145
Overall Dimensions
Weight 1.57 lb (0.71 kg)
Length 52.01 in (132.11 cm)
Width 30.3 in (76.96 cm)
Part Number C412417-147
Overall Dimensions
Weight 1.07 lb (0.49 kg)
Length 51.26 in (130.2 cm)
Width 19.04 in (48.36 cm)
Part Number C412418-101
Overall Dimensions
Weight 5 lb (2.27 kg)
Length 55.79 in (141.71 cm)
Width 49.06 in (124.61 cm)
Part Number C412418-103
Overall Dimensions
Weight 5.04 lb (2.29 kg)
Length 73 in (185.42 cm)
Width 50.66 in (128.68 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C412418-105
Overall Dimensions
Weight 4.23 lb (1.92 kg)
Length 73 in (185.42 cm)
Width 49.55 in (125.86 cm)
Part Number C412418-107
Overall Dimensions
Weight 4.19 lb (1.9 kg)
Length 73 in (185.42 cm)
Width 49.55 in (125.86 cm)
Part Number C412418-109
Overall Dimensions
Weight 8.48 lb (3.85 kg)
Length 74 in (187.96 cm)
Width 49.29 in (125.2 cm)
Part Number C412418-111
Overall Dimensions
Weight 4.96 lb (2.25 kg)
Length 76.16 in (193.45 cm)
Width 49.53 in (125.81 cm)
Part Number C412418-113
Overall Dimensions
Weight 4.16 lb (1.89 kg)
Length 52.16 in (132.49 cm)
Width 49.64 in (126.09 cm)
Part Number C412418-119
Overall Dimensions
Weight 6.41 lb (2.91 kg)
Length 54 in (137.16 cm)
Width 49.15 in (124.84 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C412418-121
Overall Dimensions
Weight 5.27 lb (2.39 kg)
Length 81 in (205.74 cm)
Width 49.64 in (126.09 cm)
Part Number C414051-101
Overall Dimensions
Weight 0.22 lb (0.1 kg)
Length 11.5 in (29.21 cm)
Width 3.77 in (9.58 cm)
Part Number C414051-102
Overall Dimensions
Weight 0.22 lb (0.1 kg)
Length 11.5 in (29.21 cm)
Width 3.77 in (9.58 cm)
Part Number C414151-123
Overall Dimensions
Weight 22.09 lb (10.02 kg)
Length 106.06 in (269.39 cm)
Width 31.46 in (79.91 cm)
Part Number C414401-143
Overall Dimensions
Weight 6.48 lb (21.28 kg)
Length 32.03 in (81.36 cm)
Width 46.92 in (119.18 cm)
Part Number C414408-101
Overall Dimensions
Weight 0.17 lb (0.08 kg)
Length 26 in (66.04 cm)
Width 13.56 in (34.44 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C414408-105
Overall Dimensions
Weight 0.02 lb (0.07 kg)
Length 27 in (68.58 cm)
Width 13.56 in (34.44 cm)
Part Number C414408-107
Overall Dimensions
Weight 0.17 lb (0.08 kg)
Length 26 in (66.04 cm)
Width 13.56 in (34.44 cm)
Part Number C414408-109
Overall Dimensions
Weight 0.33 lb (0.15 kg)
Length 26 in (66.04 cm)
Width 13.56 in (34.44 cm)
Part Number C419051-101
Overall Dimensions
Weight 0.44 lb (0.2 kg)
Length 9.03 in (22.93 cm)
Width 8.5 in (21.59 cm)
Part Number C419051-102
Overall Dimensions
Weight 0.44 lb (0.2 kg)
Length 9.03 in (22.93 cm)
Width 8.5 in (21.59 cm)
Part Number C419051-103
Overall Dimensions
Weight 1.34 lb (0.61 kg)
Length 14.12 in (35.86 cm)
Width 9.51 in (24.15 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C419051-104
Overall Dimensions
Weight 1.34 lb (0.61 kg)
Length 14.12 in (35.86 cm)
Width 9.51 in (24.15 cm)
Part Number C419051-105
Overall Dimensions
Weight 0.52 lb (0.23 kg)
Length 10.42 in (26.47 cm)
Width 8.97 in (22.79 cm)
Part Number C419051-106
Overall Dimensions
Weight 0.52 lb (0.23 kg)
Length 10.42 in (26.47 cm)
Width 8.97 in (22.79 cm)
Part Number C419151-143
Overall Dimensions
Weight 22.09 lb (10.02 kg)
Length 106.81 in (271.3 cm)
Width 33.86 in (86 cm)
Part Number C419151-155
Overall Dimensions
Weight 1.95 lb (0.88 kg)
Length 77.79 in (197.58 cm)
Width 19.29 in (49 cm)
Part Number C419401-153
Overall Dimensions
Weight 2.61 lb (1.18 kg)
Length 73.5 in (186.69 cm)
Width 49.73 in (126.31 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C419401-157
Overall Dimensions
Weight 9.34 lb (4.24 kg)
Length 95.22 in (241.86 cm)
Width 51.09 in (129.77 cm)
Part Number C419401-159
Overall Dimensions
Weight 6.48 lb (2.94 kg)
Length 32.03 in (81.36 cm)
Width 46.19 in (117.32 cm)
Part Number C419401-171
Overall Dimensions
Weight 6.48 lb (2.94 kg)
Length 32.03 in (81.36 cm)
Width 46.92 in (119.18 cm)
Part Number C419408-101
Overall Dimensions
Weight 6.47 lb (2.93 kg)
Length 46.92 in (119.18 cm)
Width 32.03 in (81.36 cm)
Part Number C419408-103
Overall Dimensions
Weight 5.21 lb (2.36 kg)
Length 51.7 in (131.32 cm)
Width 46.53 in (118.19 cm)
Part Number C419408-105
Overall Dimensions
Weight 3.73 lb (1.69 kg)
Length 43.06 in (109.37 cm)
Width 33.03 in (83.9 cm)

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Leading Particulars
Table 1/TABLE 50-11-05-870-001-A01 (continued)

Property Specification
Part Number C419408-107
Overall Dimensions
Weight 0.33 lb (0.15 kg)
Length 26 in (66.04 cm)
Width 13.56 in (34.44 cm)
Part Number C419408-109
Overall Dimensions
Weight 0.17 lb (0.077 kg)
Length 26 in (66.04 cm)
Width 13.56 in (34.44 cm)

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FOAM SEAL

SHROUD
C411051−159
FOAM SEAL
C411051−160

FOAM SEAL

C411051−161 FOAM SEAL

C411051−162

SHROUD
FOAM SEAL

FOAM SEAL

SHROUD

C411051−163
C411051−165
C419051−103
501105DO01

FOAM SEAL C419051−104

Sidewall Panel Assembly

(Sheet 1 of 9)
Figure 1/GRAPHIC 50-11-05-870-001-A01

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 COMPONENT MAINTENANCE MANUAL
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FOAM SEAL

C414051−101
C414051−102

FOAM SEAL
SHROUD

FOAM SEAL

FOAM SEAL

C419051−101
C419051−102

FOAM SEAL

SHROUD

FOAM SEAL

FOAM SEAL

C419051−105
C419051−106

FOAM SEAL
501105DO02

SHROUD

Sidewall Panel Assembly

(Sheet 2 of 9)
Figure 1/GRAPHIC 50-11-05-870-001-A01

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 COMPONENT MAINTENANCE MANUAL
C41XXXX

CLIP−ON NUT

C411051−171

C411051−173

SHROUD

SLOPING SIDEWALL
LINER ASSY

C411151−149
C411151−101 C411151−129
C411151−153
C411151−103 C411151−131
C411151−155
C411151−105 C411151−133
C411151−179
C411151−107 C411151−135
C411151−183
C411151−109 C411151−139
REINFORCEMENT C411162−111
STRIP C411151−113 C411151−143
C411162−127
C411151−115 C411151−145
C411162−137
501105DO03

C411151−117 C411151−147
C419151−155

Sidewall Panel Assembly

(Sheet 3 of 9)
Figure 1/GRAPHIC 50-11-05-870-001-A01

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 COMPONENT MAINTENANCE MANUAL
C41XXXX

PANEL ASSY

CLIP−ON NUT

C411151−159

C414151−123 BULK SLOPING

SIDEWALL SUB ASSY
C419151−143

LINER STRIP
SIDEWALL

C411152−161

C411152−163

C411152−165
NUTPLATE C411152−167

C411152−169

C411152−171
BULK SLOPER
BRACKET ASSY
501105DO04

Sidewall Panel Assembly

(Sheet 4 of 9)
Figure 1/GRAPHIC 50-11-05-870-001-A01

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VERTICAL
SIDEWALL LINER

C412409−101

C412418−101

COVER
SIDEWALL
STRIP
EXTRUSION

VERTICAL
SIDEWALL LINER DOUBLER
STRIP

C412409−161

LINER

QUARTER
TURN
SIDEWALL
EXTRUSION

C412416−103

C412416−104
VERTICAL
SIDEWALL LINER C412416−109

C412416−145

C412417−145
501105DO05

QUARTER
TURN

Sidewall Panel Assembly

(Sheet 5 of 9)
Figure 1/GRAPHIC 50-11-05-870-001-A01

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SIDEWALL VERTICAL
EXTRUSION SIDEWALL LINER
ACCESS PANEL
LINER

C412416−107

C412416−127

C412416−129

DOUBLER
QUARTER STRIP SIDEWALL
TURN EXTRUSION

BLOW IN PANEL

VERTICAL
SIDEWALL LINER
C412409−111
C412409−113
C412418−105
C412418−107
VERTICAL
SIDEWALL LINER
COVER
STRIP

SIDEWALL
EXTRUSION

VERTICAL BLOW IN PANEL

SIDEWALL LINER

C412409−115
C412418−109
501105DO06

BLOW IN PANEL

COVER
STRIP

Sidewall Panel Assembly

(Sheet 6 of 9)
Figure 1/GRAPHIC 50-11-05-870-001-A01

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SIDEWALL
EXTRUSION

C412409−117
VERTICAL
SIDEWALL LINER C412409−118

SIDEWALL ACCESS PANEL

EXTRUSION LINER

DOUBLER
STRIP

C412416−125 BLOW IN PANEL

C412418−111

QUARTER
TURN

VERTICAL
SIDEWALL SIDEWALL LINER
EXTRUSION

C412416−131

QUARTER
TURN
501105DO07

VERTICAL
SIDEWALL LINER

Sidewall Panel Assembly

(Sheet 7 of 9)
Figure 1/GRAPHIC 50-11-05-870-001-A01

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SIDEWALL
EXTRUSION

DOUBLER
STRIP

C412409−139

C412417−139

C412418−119

VERTICAL SIDEWALL
PANEL ASSY

SIDEWALL
EXTRUSION

C412409−143

VERTICAL
SIDEWALL SIDEWALL LINER
EXTRUSION

C412409−121
C412409−147
C412409−159
C412409−173
C412417−147
501105DO08

VERTICAL
SIDEWALL LINER

Sidewall Panel Assembly

(Sheet 8 of 9)
Figure 1/GRAPHIC 50-11-05-870-001-A01

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C412410−079 C414408−109
C412410−081 C419408−101
C412410−085 C419408−103
C412410−089 C419408−105
C414408−101 C419408−107
C414408−105 C419408−109
C414408−107
VERTICAL
SIDEWALL LINER

SIDEWALL
EXTRUSION
VERTICAL
SIDEWALL LINER

C412416−105

C412416−135

C412418−103

QUARTER
SIDEWALL TURN
EXTRUSION

VERTICAL
SIDEWALL LINER

C412416−119
501105DO09

QUARTER
TURN

Sidewall Panel Assembly

(Sheet 9 of 9)
Figure 1/GRAPHIC 50-11-05-870-001-A01

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 COMPONENT MAINTENANCE MANUAL
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TASK 50-11-05-870-004-A01
3. Operation

NOTE: Not applicable.

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DISASSEMBLY

TASK 50-11-05-99F-806-A01
1. General

A. This section contains special instructions and notes needed to prevent damage to components and
possible injury during disassembly of the Sidewall Panel Assembly.

NOTE: Disassembly sequence can be changed.

B. To use this section, first refer to DESCRIPTION AND OPERATION and INSPECTION/CHECK
sections to identify the damaged and worn parts. Then refer to paragraph 2, below, for any special
disassembly instructions.

C. Refer to REPAIR section or replace all bonded components, adhesive-backed placards, and potted
inserts. Remove the attaching parts given in the IPL to remove all other components.

TASK 50-11-05-000-801-A01
2. Disassembly Procedures

CAUTION: THE MONUMENT HAS DECORATIVE SURFACES THAT ARE EASILY DAMAGED.
COVER THE SURFACES AND BE CAREFUL WITH UNIT TO PREVENT DAMAGE.

SUBTASK 50-11-05-040-001-A01
A. Shroud Assembly (IPL Figure 1)

(1) Refer to REPAIR section to replace the bonded foam seal (5, -5A, 5B, or 5C).

(2) Refer to REPAIR section to replace the bonded foam seal (10, -10A, 10B, -10C , 10D, or -10E).

(3) Refer to REPAIR section to replace the bonded foam seal (15, -15A, 15B, -15E, -15F, 15G,
or -15H).

(4) Refer to REPAIR section to replace the bonded foam seal (20).

(5) Refer to REPAIR section to replace the bonded foam seal (22 or -22A).

(6) Remove the shroud (25, -25A, 25B, -25C, 25D, -25E, 25F, -25G, 25H, -25J, -25J, -25K, -25L,
25M, or -25N).

SUBTASK 50-11-05-040-002-A01
B. Shroud Assembly (IPL Figure 1A)

(1) Remove the clip-on nut (5 or -5A).

(2) Remove the rivets (15) to release the shroud doubler assembly (10). Disassemble the shroud
doubler assembly (10) as follows:

(a) Remove the rivets (25) to release the nutplates (20).

(b) Remove the shroud doubler (30).

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 COMPONENT MAINTENANCE MANUAL
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(3) Remove the shroud (35 or -35A).

SUBTASK 50-11-05-040-003-A01
C. Sloping Sidewall Liner Assembly (IPL Figure 1B)

(1) Remove the clip-on nuts (-5).

(2) Refer to REPAIR section to replace the bonded reinforcement strip (10, -10A, or -10B).

(3) Refer to REPAIR section to replace the bonded reinforcement strip (-12).

(4) Refer to REPAIR section to replace the bonded doubler (15, -15A, -15B, -15C, -15D, -15E, -15F,
-15G, -15H, -15J, -15K, -15L, -15M, -15N, -15P, -15Q, -15R, or -15S).

(5) Refer to REPAIR section to replace the bonded transfer tape (-17 or -17A).

(6) Refer to REPAIR section to replace the bonded placard (20B, -20C, -20D, -20E, or -20F).

(7) Refer to REPAIR section to replace the bonded placard (25, -25A, -25B, -25C, -25D, -25E,
-25F, -25G, -25H, -25J, -25K, -25L, -25M, -25N, -25P, -25Q, -25R, -25S, -25T, -25U, -25V,
-25W, -25X, -26, -26A, -26B, -26C, -26C, -26D, -26E, -26E, -26F, -26G, -26H, -26J, -26K, -26L,
-26M, -26N, -26P, -26Q, or -26R).

(8) Refer to REPAIR section to replace the bonded placard (30, -30A, -30B, or -30C).

(9) Remove the sloping sidewall liner (35, -35A, -35B, -35C, -35D, -35E, -35F, -35G, -35H, -35J,
-35K, -35L, -35M, -35N, -35P, -35Q, -35R, -35S, -35T, -35U, -35V, -35W, -35X, -35Y, or -35Z).

SUBTASK 50-11-05-040-004-A01
D. Bulk Sloping Sidewall Panel Assembly (IPL Figure 1C)

(1) Remove the clip-on nuts (5 or -5A).

(2) Remove the screws (15 or -15A) to release the net fitting closeout (10 or -10A).

(3) Remove the screws (25) to release the net fitting closeout (20).

(4) Remove the screw (35 or -35A) to release the sidewall liner strip (30, -30A, or -30B). Refer to
REPAIR section to replace the bonded sidewall liner strip (30, -30A, or -30B).

(5) Refer to REPAIR section to replace the bonded foam filler (40).

(6) Refer to REPAIR section to replace the bonded placard (45).

(7) Refer to REPAIR section to replace the bonded placard (50).

(8) Refer to REPAIR section to replace the bonded placard (55).

(9) Refer to REPAIR section to replace the glass cloth tape (-57).

(10) Remove and disassemble the sidewall panel assembly (60, -60B, or -60C) as follows:

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(a) Remove the sidewall panel (-65, -65B, or -65C).

SUBTASK 50-11-05-040-005-A01
E. Bulk Sloper Bracket Assembly (IPL Figure 1D)

(1) Remove the rivets (10 or -10A) to release the nutplates (5 or -5A).

(2) Remove the bulk sloper bracket (15, -15A, -15B, -15C, -15D, or -15E).

SUBTASK 50-11-05-040-006-A01
F. Bulk Endwall Assembly (IPL Figure 1E) - Deleted Figure

SUBTASK 50-11-05-040-007-A01
G. Vertical Sidewall Panel Assembly (IPL Figure 1F)

(1) Remove the nuts (10A), washers (15), and screws (20) to release the sidewall extrusion (5).
Refer to REPAIR section to replace the bonded sidewall extrusion (5).

(2) Refer to REPAIR section to replace the bonded spacer (-25A).

(3) Refer to REPAIR section to replace the bonded cover strip (30).

(4) Refer to REPAIR section to replace the bonded cover strip (35).

(5) Refer to REPAIR section to replace the bonded cover strip (40).

(6) Refer to REPAIR section to replace the bonded silicone foam tape (-42A).

(7) Refer to REPAIR section to replace the bonded glass cloth tape (-43A).

(8) Refer to REPAIR section to replace the bonded transfer tape (-44 or -44A).

(9) Remove the blow in panel (45).

(10) Refer to REPAIR section to replace the bonded vertical sidewall liner (50).

(11) Remove the grill (55).

(12) Refer to REPAIR section to replace the bonded placard (60 or -60A).

(13) Refer to REPAIR section to replace the bonded placard (65 or -65A).

(14) Refer to REPAIR section to replace the bonded placard (70 or -70A).

(15) Refer to REPAIR section to replace the bonded placard (75 or -75A).

(16) Disassemble the decompression blow subassembly (-80) as follows:

(a) Refer to REPAIR section to replace the bonded placard (-85 or -85A).

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(b) Remove the blow in panel (-90).

SUBTASK 50-11-05-040-008-A01
H. Vertical Sidewall Panel Assembly (IPL Figure 1G)

(1) Refer to REPAIR section to replace the bonded silicone foam tape (-3).

(2) Remove the nuts (10E), washers (15), and screws (20) to release the sidewall extrusion (5E).

(3) Refer to REPAIR section to replace the bonded insulation panel (30A).

(4) Remove the liner (70F).

(5) Refer to REPAIR section to replace the bonded transfer tape (-73 or -73A).

(6) Refer to REPAIR section to replace the bonded placard (75E or -75F).

(7) Refer to REPAIR section to replace the bonded placard (80E or -80F).

(8) Refer to REPAIR section to replace the bonded placard (85C).

(9) Refer to REPAIR section to replace the bonded placard (90B or -90C).

SUBTASK 50-11-05-040-009-A01
I. Vertical Sidewall Panel Assembly (IPL Figure 1H)

(1) Refer to REPAIR section to replace the bonded silicone foam tape (-3).

(2) Remove the nuts (10), washers (15), and screws (20) to release the sidewall extrusion (5). Refer
to REPAIR section to replace the bonded sidewall extrusion (5).

(3) Refer to REPAIR section to replace the bonded water dam liner (-22).

(4) Remove the rivet (30) and nylon washers (35) to release the cargo access panel lanyard (25).

(5) Refer to REPAIR section to replace the bonded hook fastener (40).

(6) Remove and disassemble the quarter turn fastener assembly (45 or -45A) as follows:

(a) Remove the sleeve (-50).

(b) Remove the stud (-55).

(7) Remove the retainers (-60, -60A, 60B, -60C, or -60D).

(8) Refer to REPAIR section to replace the bonded doubler strip (65, -65A, -65B, or -65C).

(9) Refer to REPAIR section to replace the bonded doubler strip (70, -70A, -70B, or -70C).

(10) Refer to REPAIR section to replace the bonded doubler strip (75, -75A, -75B, or -75C).

(11) Refer to REPAIR section to replace the bonded silicone foam tape (-80A).

(12) Refer to REPAIR section to replace the bonded placard (85, -85A, -85B, -85C, -85D, -85E,
-85F, or -85G).

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(13) Refer to REPAIR section to replace the bonded placard (90 or -90A).

(14) Refer to REPAIR section to replace the bonded placard (95, -95A, -95B, or -95C).

(15) Refer to REPAIR section to replace the bonded placard (100 or -100A).

(16) Refer to REPAIR section to replace the bonded placard (-105, -105A, -105B, or -105C).

(17) Refer to REPAIR section to replace the bonded placard (-110).

(18) Refer to REPAIR section to replace the bonded placard (-115 or -115A).

(19) Refer to REPAIR section to replace the bonded tape (-120A).

(20) Refer to REPAIR section to replace the bonded tape (-122A).

(21) Remove the vertical sidewall liner (125, -125A, -125B, or -125C).

SUBTASK 50-11-05-040-010-A01
J. Vertical Sidewall Panel Assembly (IPL Figure 1J)

(1) Remove the cargo access panel lanyards (5 or -5A).

(2) Remove the rivets (15 or -15A) and nylon washers (20 or -20A) to release the cargo access
panel lanyard (10).

(3) Refer to REPAIR section to replace the bonded hook fasteners (25 or -25A).

(4) Refer to REPAIR section to replace the bonded silicone foam tape (-28).

(5) Remove the nuts (35 or -35A), washers (40 or -40A), and screws (45 or -45A) to release the
sidewall extrusion (30, -30A, or -30B). Refer to REPAIR section to replace the bonded sidewall
extrusion (30, -30A, or -30B).

(6) Remove and disassemble the quarter turn fastener assemblies(50, -50A, or -50B) as follows:

(a) Remove the sleeve (-55).

(b) Remove the stud (-60).

(7) Remove the retainers (-65, -65A, -65B, 65C, -65D, or -65E).

(8) Refer to REPAIR section to replace the bonded transfer tape (-68 or -68A).

(9) Refer to REPAIR section to replace the bonded doubler strip (70, -70A, or -70B).

(10) Refer to REPAIR section to replace the bonded doubler strip (75).

(11) Refer to REPAIR section to replace the bonded doubler strip (80 or -80A).

(12) Refer to REPAIR section to replace the bonded doubler strip (85, -85A, or -85B).

(13) Refer to REPAIR section to replace the bonded doubler strip (-90 or -90A).

(14) Refer to REPAIR section to replace the bonded doubler strip (-95).

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(15) Refer to REPAIR section to replace the bonded silicone foam tape (-100A).

(16) Refer to REPAIR section to replace the bonded placard (105, -105A, -105B, -105C, -105D,
or -105E).

(17) Refer to REPAIR section to replace the bonded placard (110, -110A, -110B, or -110C).

(18) Refer to REPAIR section to replace the bonded placard (115, -115A, -115B, -115C, -115D,
or -115E).

(19) Refer to REPAIR section to replace the bonded placard (120).

(20) Refer to REPAIR section to replace the bonded placard (125 or -125A).

(21) Refer to REPAIR section to replace the bonded placard (130).

(22) Refer to REPAIR section to replace the bonded placard (135).

(23) Refer to REPAIR section to replace the bonded placard (140).

(24) Refer to REPAIR section to replace the bonded placard (-145, -145A, -145B, or -145C).

(25) Refer to REPAIR section to replace the bonded placard (-150).

(26) Refer to REPAIR section to replace the bonded glass cloth tape (-155A).

(27) Refer to REPAIR section to replace the bonded vertical sidewall liner (160).

(28) Remove the access panel liner (165, -165A, or -165B).

SUBTASK 50-11-05-040-011-A01
K. Vertical Sidewall Panel Assembly (IPL Figure 1K)

(1) Remove the nuts (10A), washers (15), and screws (20) to release the sidewall extrusion (5 or
-5A). Refer to REPAIR section to replace the bonded sidewall extrusion (5 or -5A).

(2) Refer to REPAIR section to replace the bonded transfer tape (-22 or -22A).

(3) Refer to REPAIR section to replace the bonded cover strip (25).

(4) Refer to REPAIR section to replace the bonded cover strip (30).

(5) Refer to REPAIR section to replace the bonded cover strip (35 or -35A).

(6) Refer to REPAIR section to replace the bonded silicone foam tape (-37A).

(7) Refer to REPAIR section to replace the bonded glass cloth tape (-38A).

(8) Remove the blow in panel (40, -40A, -40B, or -40D).

(9) Refer to REPAIR section to replace the bonded vertical sidewall liner (45 or -45A).

(10) Remove the grill (50 or -50A).

(11) Refer to REPAIR section to replace the bonded vertical sidewall liner (55 or -55A).

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(12) Refer to REPAIR section to replace the bonded placard (60, -60A, -60B, or -60C).

(13) Refer to REPAIR section to replace the bonded placard (65, -65A, -65B, or -65C).

(14) Refer to REPAIR section to replace the bonded placard (70 or -70A).

(15) Refer to REPAIR section to replace the bonded placard (75, -75A, or -75B).

(16) Refer to REPAIR section to replace the bonded placard (80, -80A, or -80B).

(17) Refer to REPAIR section to replace the bonded placard (85, -85A, or -85B).

(18) Disassemble the decompression blow subassembly (-90) as follows:

(a) Refer to REPAIR section to replace the bonded placard (-95 or -95A).

(b) Refer to REPAIR section to replace the bonded placard (-100).

(c) Refer to REPAIR section to replace the bonded placard (-105).

(d) Remove the blow in panel (-110).

SUBTASK 50-11-05-040-012-A01
L. Vertical Sidewall Panel Assembly (IPL Figure 1L)

(1) Remove the nuts (10A), washers (15), and screws (20) to release the sidewall extrusion (5).
Refer to REPAIR section to replace the bonded sidewall extrusion (5).

(2) Refer to REPAIR section to replace the bonded cover strip (25).

(3) Refer to REPAIR section to replace the bonded cover strip (30).

(4) Refer to REPAIR section to replace the bonded cover strip (35).

(5) Refer to REPAIR section to replace the bonded cover strip (40).

(6) Refer to REPAIR section to replace the bonded cover strip (45).

(7) Refer to REPAIR section to replace the bonded cover strip (50).

(8) Refer to REPAIR section to replace the bonded transfer tape (-51 or -51A).

(9) Refer to REPAIR section to replace the bonded silicone foam tape (-52A).

(10) Refer to REPAIR section to replace the bonded glass cloth tape (-53A).

(11) Remove the blow in panel (55).

(12) Remove the blow in panel (60).

(13) Remove the blow out panel (65).

(14) Refer to REPAIR section to replace the bonded vertical sidewall liner (70).

(15) Refer to REPAIR section to replace the bonded placard (75 or -75A).

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(16) Refer to REPAIR section to replace the bonded placard (80 or -80A).

(17) Refer to REPAIR section to replace the bonded placard (85).

(18) Refer to REPAIR section to replace the bonded placard (90 or -90A).

(19) Disassemble the decompression blow subassembly (-95) as follows:

(a) Refer to REPAIR section to replace the bonded placard (-100 or -100A).

(b) Remove the blow in panel (-105).

(20) Disassemble the decompression blow subassembly (-110) as follows:

(a) Refer to REPAIR section to replace the bonded placard (-115 or -115A).

(b) Refer to REPAIR section to replace the bonded placard (-120).

(c) Remove the blow in panel (-125).

SUBTASK 50-11-05-040-013-A01
M. Vertical Sidewall Panel Assembly (IPL Figure 1M)

(1) Refer to REPAIR section to replace the bonded silicone foam tape (-3).

(2) Remove the nuts (10A), washers (15), and screws (20) to release the sidewall extrusion (5 or
-5A). Refer to REPAIR section to replace the bonded sidewall extrusion (5 or -5A).

(3) Refer to REPAIR section to replace the bonded doubler strip (25 or -25A).

(4) Refer to REPAIR section to replace the bonded transfer tape (-27 or -27A).

(5) Remove the vertical sidewall liner (30 or -30A).

(6) Refer to REPAIR section to replace the bonded placard (35, -35A, -35B, or -35C).

(7) Refer to REPAIR section to replace the bonded placard (40 or -40A).

(8) Refer to REPAIR section to replace the bonded placard (45 or -45A).

(9) Refer to REPAIR section to replace the bonded placard (-50 or -50A).

SUBTASK 50-11-05-040-014-A01
N. Vertical Sidewall Panel Assembly (IPL Figure 1N)

(1) Remove the rivets (10) and nylon washers (15) to release the cargo access panel lanyards (5).

(2) Refer to REPAIR section to replace the bonded hook fasteners (20).

(3) Remove the nuts (30), washers (35), and screws (40) to release the sidewall extrusion (25).
Refer to REPAIR section to replace the bonded sidewall extrusion (25).

(4) Remove and disassemble the quarter turn fasteners Assembly (45) as follows:

(a) Remove the sleeve (-50).

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(b) Remove the stud (-55).

(5) Remove the retainers (-60 or 60A).

(6) Refer to REPAIR section to replace the bonded doubler strip (65).

(7) Refer to REPAIR section to replace the bonded doubler strip (70).

(8) Refer to REPAIR section to replace the bonded doubler strip (75).

(9) Refer to REPAIR section to replace the bonded cover strip (80).

(10) Refer to REPAIR section to replace the bonded cover strip (85).

(11) Refer to REPAIR section to replace the bonded cover strip (90).

(12) Refer to REPAIR section to replace the bonded silicone foam tape (-95A).

(13) Refer to REPAIR section to replace the bonded placard (100 or -100A).

(14) Refer to REPAIR section to replace the bonded placard (105 or -105A).

(15) Refer to REPAIR section to replace the bonded placard (110 or -110A).

(16) Refer to REPAIR section to replace the bonded placard (115 or -115A).

(17) Refer to REPAIR section to replace the bonded placard (120 or -120A).

(18) Refer to REPAIR section to replace the bonded placard (125).

(19) Refer to REPAIR section to replace the bonded placard (130).

(20) Refer to REPAIR section to replace the bonded glass cloth tape (-135A).

(21) Refer to REPAIR section to replace the bonded transfer tape (-137A).

(22) Remove the decompression grill (140).

(23) Remove the blow in panel (145).

(24) Remove the access panel liner (150).

(25) Disassemble the decompression blow subassembly (-155) as follows:

(a) Refer to REPAIR section to replace the bonded placard (-160).

(b) Refer to REPAIR section to replace the bonded placard (-165 or -165A).

(c) Refer to REPAIR section to replace the bonded placard (-170 or -170A).

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(d) Remove the blow in panel (-175).

SUBTASK 50-11-05-040-015-A01
O. Vertical Sidewall Panel Assembly (IPL Figure 1P)

(1) Remove the rivet (10) and nylon washers (15) to release the cargo access panel lanyard (5).

(2) Refer to REPAIR section to replace the bonded hook fastener (20).

(3) Refer to REPAIR section to replace the bonded silicone foam tape (-22).

(4) Remove the nuts (30), washers (35), and screws (40) to release the sidewall extrusion (25).
Refer to REPAIR section to replace the bonded sidewall extrusion (25).

(5) Remove and disassemble the quarter turn fastener assemblies (45) as follows:

(a) Remove the sleeve (-50).

(b) Remove the stud (-55).

(6) Remove the retainers (-60 or 60A).

(7) Refer to REPAIR section to replace the bonded transfer tape (-63 or -63A).

(8) Refer to REPAIR section to replace the bonded doubler strip (65).

(9) Refer to REPAIR section to replace the bonded doubler strip (70).

(10) Refer to REPAIR section to replace the bonded doubler strip (75).

(11) Refer to REPAIR section to replace the bonded silicone foam tape (-80A).

(12) Refer to REPAIR section to replace the bonded placard (85 or -85A).

(13) Refer to REPAIR section to replace the bonded placard (90).

(14) Refer to REPAIR section to replace the bonded placard (95).

(15) Refer to REPAIR section to replace the bonded placard (100 or -100A).

(16) Refer to REPAIR section to replace the bonded placard (105 or -105A).

(17) Refer to REPAIR section to replace the bonded placard (110).

(18) Refer to REPAIR section to replace the bonded glass cloth tape (-115A).

(19) Remove the outboard decompression vent panel (120).

(20) Remove the vertical sidewall liner (125).

(21) Remove the vertical sidewall liner (130).

(22) Remove the vertical sidewall liner (135).

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(23) Remove the vertical sidewall liner (140).

SUBTASK 50-11-05-040-016-A01
P. Vertical Sidewall Panel Assembly (IPL Figure 1Q)

(1) Remove the nuts (10), washers (15), and screws (20) to release the sidewall extrusion (5). Refer
to REPAIR section to replace the bonded sidewall extrusion (5).

(2) Refer to REPAIR section to replace the bonded water dam liner (22).

(3) Refer to REPAIR section to replace the bonded cover strip (25).

(4) Refer to REPAIR section to replace the bonded doubler strip (30).

(5) Refer to REPAIR section to replace the bonded cover strip (35).

(6) Refer to REPAIR section to replace the bonded decompression panel assembly (40 or -40A).
Disassemble the decompression panel assembly (40 or -40A) as follows:

(a) Refer to REPAIR section to replace the bonded insulation panel (45).

(b) Refer to REPAIR section to replace the bonded insulation panel (-46 or -46A).

(c) Refer to REPAIR section to replace the bonded insulation panel (-47 or -47A).

(d) Refer to REPAIR section to replace the bonded insulation panel (-48).

(e) Remove the inboard decompression vent panel (50 or -50A).

(f) Refer to REPAIR section to replace the bonded transfer tape (-53 or -53A).

(7) Refer to REPAIR section to replace the bonded decompression panel assembly (55).
Disassemble the decompression panel assembly (55) as follows:

(a) Refer to REPAIR section to replace the bonded insulation panel (60).

(b) Remove the outboard decompression vent panel (65).

(c) Refer to REPAIR section to replace the bonded transfer tape (-67 or -67A).

(8) Remove the panel grill (70).

(9) Refer to REPAIR section to replace the bonded placard (75 or -75A).

(10) Refer to REPAIR section to replace the bonded placard (80 or -80A).

(11) Refer to REPAIR section to replace the bonded placard (85).

(12) Refer to REPAIR section to replace the bonded silicone foam tape (-90A).

(13) Refer to REPAIR section to replace the bonded glass cloth tape (-95A).

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(14) Refer to REPAIR section to replace the bonded transfer tape (-100A or -100B).

SUBTASK 50-11-05-040-017-A01
Q. Vertical Sidewall Panel Assembly (IPL Figure 1R)

(1) Refer to REPAIR section to replace the bonded silicone foam tape (-3).

(2) Remove the nuts (10A), washers (15), and screws (20) to release the sidewall extrusion (5).
Refer to REPAIR section to replace the bonded sidewall extrusion (5).

(3) Remove the outboard decompression vent panel (25).

(4) Refer to REPAIR section to replace the bonded vertical sidewall liner (30).

(5) Refer to REPAIR section to replace the bonded vertical sidewall liner (35).

(6) Refer to REPAIR section to replace the bonded transfer tape (-37 or -37A).

(7) Refer to REPAIR section to replace the bonded placard (40 or -40A).

(8) Refer to REPAIR section to replace the bonded placard (45).

(9) Refer to REPAIR section to replace the bonded placard (50).

SUBTASK 50-11-05-040-018-A01
R. Vertical Sidewall Panel Assembly (IPL Figure 1S)

(1) Remove the nuts (10 or -10A), washers (15 or -15A), and screws (20 or -20A) to release the
sidewall extrusion (5 or -5A). Refer to REPAIR section to replace the bonded sidewall extrusion
(5 or -5A).

(2) Refer to REPAIR section to replace the bonded water dam liner (25).

(3) Refer to REPAIR section to replace the bonded doubler strip (30, -30A, or -30B).

(4) Refer to REPAIR section to replace the bonded transfer tape (-33, -33A, or -33B).

(5) Remove the vertical sidewall liner (35, -35A, -35B, or -35C).

(6) Refer to REPAIR section to replace the bonded placard (40, -40A, -40B, -40C, -40E, -40F,
or -40G).

(7) Refer to REPAIR section to replace the bonded placard (45, -45A, -45B, -45C, -45D, -45D,
or -45E).

(8) Refer to REPAIR section to replace the bonded placard (-50).

(9) Refer to REPAIR section to replace the bonded silicone foam tape (-55A).

SUBTASK 50-11-05-040-019-A01
S. Vertical Sidewall Vent Liner Assembly (IPL Figure 1T)

(1) Refer to REPAIR section to replace the bonded placard (5, -5A, -5B, -5C, -5D, -5E, -5F, -5G,
-5H, -5J, -5K, -5L, -5M, or -5N).

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(2) Remove the vertical sidewall liner panel (10, -10A, -10B, -10C, or -10D).

SUBTASK 50-11-05-040-020-A01
T. Vertical Sidewall Panel Assembly (IPL Figure 1U)

(1) Remove the rivet (10) and nylon washers (15A) to release the cargo access panel lanyard (5).

(2) Refer to REPAIR section to replace the bonded hook fastener (20).

(3) Refer to REPAIR section to replace the bonded silicone foam tape (-23).

(4) Remove the nuts (30), washers (35), and screws (40) to release the sidewall extrusion (25).
Refer to REPAIR section to replace the bonded sidewall extrusion (25).

(5) Remove and disassemble the quarter turn fastener assemblies (45 or -45A) as follows:

(a) Remove the sleeve (-50).

(b) Remove the stud (-55).

(6) Remove the retainers (-60, -60A, or 60B).

(7) Refer to REPAIR section to replace the bonded doubler strip (65, -65A, or -65B).

(8) Refer to REPAIR section to replace the bonded doubler strip (70 or -70A).

(9) Refer to REPAIR section to replace the bonded cover strip (75 or -75A).

(10) Refer to REPAIR section to replace the bonded cover strip (80 or -80A).

(11) Refer to REPAIR section to replace the bonded cover strip (85 or -85A).

(12) Refer to REPAIR section to replace the bonded silicone foam tape (-90A).

(13) Refer to REPAIR section to replace the bonded transfer tape (-92 or -92A).

(14) Refer to REPAIR section to replace the bonded placard (95, -95A, -95B, or -95C).

(15) Refer to REPAIR section to replace the bonded placard (100, -100A, or -100B).

(16) Refer to REPAIR section to replace the bonded placard (105).

(17) Refer to REPAIR section to replace the bonded placard (110 or -110A).

(18) Refer to REPAIR section to replace the bonded placard (115 or -115A).

(19) Refer to REPAIR section to replace the bonded placard (120 or -120A).

(20) Refer to REPAIR section to replace the bonded placard (125 or -125A).

(21) Refer to REPAIR section to replace the bonded placard (130 or -130A).

(22) Refer to REPAIR section to replace the bonded placard (135).

(23) Refer to REPAIR section to replace the bonded placard (-140).

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(24) Refer to REPAIR section to replace the bonded placard (-145).

(25) Refer to REPAIR section to replace the bonded glass cloth tape (-150A).

(26) Refer to REPAIR section to replace the bonded vertical sidewall liner (155 or -155A).

(27) Refer to REPAIR section to replace the bonded vertical sidewall liner (160 or -160A).

(28) Remove the decompression grill (165 or -165A).

(29) Remove the blow in panel (170 or -170A).

(30) Disassemble the decompression blow subassembly (-175) as follows:

(a) Refer to REPAIR section to replace the bonded placard (-180).

(b) Refer to REPAIR section to replace the bonded placard (-185 or -185A).

(c) Refer to REPAIR section to replace the bonded placard (-190 or -190A).

(d) Remove the blow in panel (-195).

SUBTASK 50-11-05-040-021-A01
U. Vertical Sidewall Panel Assembly (IPL Figure 1V)

(1) Remove the rivet (10) and nylon washers (15) to release the cargo access panel lanyard (5).

(2) Refer to REPAIR section to replace the bonded hook fastener (20).

(3) Refer to REPAIR section to replace the bonded silicone foam tape (-22).

(4) Remove the nuts (30), washers (35), and screws (40) to release the sidewall extrusion (25).
Refer to REPAIR section to replace the bonded sidewall extrusion (25).

(5) Refer to REPAIR section to replace the bonded spacer (45).

(6) Remove and disassemble the quarter turn fastener assemblies (50) as follows:

(a) Remove the sleeve (-55).

(b) Remove the stud (-60).

(7) Remove the retainers (-65 or 65A).

(8) Refer to REPAIR section to replace the bonded doubler strip (70).

(9) Refer to REPAIR section to replace the bonded doubler strip (75).

(10) Refer to REPAIR section to replace the bonded silicone foam tape (-80A).

(11) Refer to REPAIR section to replace the bonded placard (85 or -85A).

(12) Refer to REPAIR section to replace the bonded placard (90 or -90A).

(13) Refer to REPAIR section to replace the bonded placard (95).

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(14) Refer to REPAIR section to replace the bonded placard (100).

(15) Refer to REPAIR section to replace the bonded placard (105).

(16) Refer to REPAIR section to replace the bonded placard (110).

(17) Refer to REPAIR section to replace the bonded glass cloth tape (-115A).

(18) Refer to REPAIR section to replace the bonded transfer tape (-117 or -117A).

(19) Remove the blow out panel (120).

(20) Refer to REPAIR section to replace the bonded vertical sidewall liner (125).

(21) Refer to REPAIR section to replace the bonded vertical sidewall liner (130).

(22) Remove the access panel liner (135).

SUBTASK 50-11-05-040-022-A01
V. Vertical Sidewall Panel Assembly (IPL Figure 1W)

(1) Remove the rivet (10) and nylon washers (15) to release the cargo access panel lanyard (5).

(2) Refer to REPAIR section to replace the bonded hook fastener (20).

(3) Refer to REPAIR section to replace the bonded silicone foam tape (-22).

(4) Remove the nuts (30), washers (35), and screws (40) to release the sidewall extrusion (25).
Refer to REPAIR section to replace the bonded sidewall extrusion (25).

(5) Remove and disassemble the quarter turn fastener assemblies (45) as follows:

(a) Remove the sleeve (-50).

(b) Remove the stud (-55).

(6) Remove the retainers (-60 or 60B).

(7) Refer to REPAIR section to replace the bonded doubler strip (65).

(8) Refer to REPAIR section to replace the bonded doubler strip (70).

(9) Refer to REPAIR section to replace the bonded doubler strip (75).

(10) Refer to REPAIR section to replace the bonded cover strip (80).

(11) Refer to REPAIR section to replace the bonded cover strip (85).

(12) Refer to REPAIR section to replace the bonded cover strip (90).

(13) Refer to REPAIR section to replace the bonded silicone foam tape (-95A).

(14) Refer to REPAIR section to replace the bonded placard (100 or -100B).

(15) Refer to REPAIR section to replace the bonded placard (105 or -105A).

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(16) Refer to REPAIR section to replace the bonded placard (110).

(17) Refer to REPAIR section to replace the bonded placard (115).

(18) Refer to REPAIR section to replace the bonded placard (120 or -120A).

(19) Refer to REPAIR section to replace the bonded glass cloth tape (-145A).

(20) Refer to REPAIR section to replace the bonded transfer tape (-147 or -147A).

(21) Remove the decompression grill (150).

(22) Remove the inboard decompression vent panel (155).

(23) Remove the access panel liner (160).

(24) Disassemble the decompression blow subassembly (-165) as follows:

(a) Refer to REPAIR section to replace the bonded placard (-170).

(b) Remove the blow in panel (-175).

SUBTASK 50-11-05-040-023-A01
W. Vertical Sidewall Panel Assembly (IPL Figure 1X)

(1) Remove the rivets (10) and nylon washers (15A) to release the cargo access panel lanyards (5).

(2) Refer to REPAIR section to replace the bonded hook fastener (20).

(3) Refer to REPAIR section to replace the bonded silicone foam tape (-22).

(4) Remove the nuts (30), washers (35), and screws (40) to release the sidewall extrusion (25).
Refer to REPAIR section to replace the bonded sidewall extrusion (25).

(5) Remove and disassemble the quarter turn fastener assemblies(45) as follows:

(a) Remove the sleeve (-50).

(b) Remove the stud (-55).

(6) Remove the retainers (-60 or 60A).

(7) Refer to REPAIR section to replace the bonded doubler strip (65).

(8) Refer to REPAIR section to replace the bonded doubler strip (70).

(9) Refer to REPAIR section to replace the bonded doubler strip (75).

(10) Refer to REPAIR section to replace the bonded cover strip (80).

(11) Refer to REPAIR section to replace the bonded cover strip (85).

(12) Refer to REPAIR section to replace the bonded cover strip (90).

(13) Refer to REPAIR section to replace the bonded silicone foam tape (-95A).

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(14) Refer to REPAIR section to replace the bonded placard (100).

(15) Refer to REPAIR section to replace the bonded placard (105).

(16) Refer to REPAIR section to replace the bonded placards (110).

(17) Refer to REPAIR section to replace the bonded placard (115).

(18) Refer to REPAIR section to replace the bonded placards (120 or -120A).

(19) Refer to REPAIR section to replace the bonded placards (125).

(20) Refer to REPAIR section to replace the bonded placards (130 or -130A).

(21) Refer to REPAIR section to replace the bonded placards (135).

(22) Refer to REPAIR section to replace the bonded placards (140).

(23) Refer to REPAIR section to replace the bonded glass cloth tape (-145A).

(24) Refer to REPAIR section to replace the bonded transfer tape (-147 or -147A).

(25) Remove the decompression grill (150).

(26) Remove the vertical sidewall liner (155).

(27) Remove the inboard decompression vent panel (160).

(28) Remove the vertical sidewall liner (165).

(29) Disassemble the decompression blow subassembly (-170) as follows:

(a) Refer to REPAIR section to replace the bonded placard (-175 or -175A).

(b) Refer to REPAIR section to replace the bonded placard (-180).

(c) Remove the blow in panel (-185).

SUBTASK 50-11-05-040-024-A01
X. Vertical Sidewall Panel Assembly (IPL Figure 1Y)

(1) Remove and disassemble the quarter turn fastener assemblies (5, -5A, or -5B) as follows:

(a) Remove the sleeve (-10).

(b) Remove the stud (-15).

(2) Remove the retainers (-20, -20A, -20B, or 20C).

(3) Refer to REPAIR section to replace the bonded doubler strip (25 or -25A).

(4) Refer to REPAIR section to replace the bonded doubler strip (30 or -30A).

(5) Refer to REPAIR section to replace the bonded doubler strip (35 or -35A).

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(6) Refer to REPAIR section to replace the bonded doubler strip (40, -40A, or -40B).

(7) Refer to REPAIR section to replace the bonded silicone foam tape (-45).

(8) Refer to REPAIR section to replace the bonded placard (50, -50A, or -50B).

(9) Refer to REPAIR section to replace the bonded placard (55).

(10) Refer to REPAIR section to replace the bonded placard (60).

(11) Refer to REPAIR section to replace the bonded placard (65, -65A, or -65B).

(12) Refer to REPAIR section to replace the bonded glass cloth tape (-70A).

(13) Remove the vertical sidewall liner (75, -75A, or -75B).

SUBTASK 50-11-05-040-025-A01
Y. Vertical Sidewall Panel Assembly (IPL Figure 1Z)

(1) Remove and disassemble the quarter turn fastener assemblies (5 or -5A) as follows:

(a) Remove the sleeve (-10).

(b) Remove the stud (-15).

(2) Remove the retainers (-20, -20A, or 20B).

(3) Refer to REPAIR section to replace the bonded doubler strip (25 or -25A).

(4) Refer to REPAIR section to replace the bonded doubler strip (30 or -30A).

(5) Refer to REPAIR section to replace the bonded doubler strip (35 or -35A).

(6) Refer to REPAIR section to replace the bonded doubler strip (40 or -40A).

(7) Refer to REPAIR section to replace the bonded silicone foam tape (-45).

(8) Refer to REPAIR section to replace the bonded placard (50 or -50A).

(9) Refer to REPAIR section to replace the bonded placard (55).

(10) Refer to REPAIR section to replace the bonded glass cloth tape (-60A).

(11) Remove the vertical sidewall liner (65 or -65A).

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CLEANING

TASK 50-11-05-99F-807-A01
1. General

A. This section provides cleaning instructions for passenger cabin interior equipment manufactured by
Safran Cabin Inc. Correct use of the materials and equipment will provide acceptable cleaning,
minimize hazards to personnel, and prevent possible damage to the equipment.

NOTE: The companies that make the cleaning materials can change the formula. Therefore, always
follow the instructions given on the container. The instructions to mix and use the cleaning
materials, given on or provided with the container, supersede the instructions given here.

Paragraph Cleaning Procedures

3.A General Surface Cleaning (Including Vinyl-Decor Covered Panels)
3.B Cleaning Instructions and Material Specifications for Metal Parts
3.C Cleaning Instructions for Adhesives

B. The recommended cleaning materials are given in Table 4001.

NOTE: Refer to applicable cleaning instructions for other materials not included in this Table.

NOTE: Equivalent items can be used.

Cleaning Tools and Materials

Table 4001/TABLE 50-11-05-940-006-A01

Nomenclature Part or Specification Number Source (CAGE)*

Apron N/A Commercially Available
Cotton Cloths (lint-free) (clean and N/A Commercially Available
dry)
Protective eyewear or safety N/A Commercially Available
goggles
Rubber Gloves or Latex N/A Commercially Available
Soft-bristled brush NSN 0038 Industries For The Blind and
Visually Impaired Inc. (V9U362)
Solvent, cleaning Adhesive Acetone Commercially Available
removal CAS No. 67-64-1
MEK (Methyl Ethyl Ketone) Commercially Available
CAS No. 78-93-3
(Fed. MIL Spec. TT-M-261)
(metal parts only)
BRULIN 815MX Brulin Holding Co. Inc. (V94058)
* Refer to the IPL, paragraph 6, for the address.

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Cleaning Tools and Materials
Table 4001/TABLE 50-11-05-940-006-A01 (continued)

Nomenclature Part or Specification Number Source (CAGE)*

Solvent, cleaning Adhesive CALLA 301-A LEMON Andpak Ema Inc. (V68491)
removal
General overall surface cleaning Mild household detergent Commercially Available
(including decor) (Mild Detergents)
BRULIN 815MX Brulin Holding Co. Inc. (V94058)
CALLA 301-A LEMON Andpak Ema Inc. (V68491)
Metal cleaning Solvent, Federal Specification Optional
P-D-680, Type III
MEK (Methyl Ethyl Ketone) Commercially Available
CAS No. 78-93-3
(Fed. MIL Spec. TT-M-261)
(metal parts only)
BRULIN 815MX Brulin Holding Co. Inc. (V94058)
CALLA 301-A LEMON Andpak Ema Inc. (V68491)
Sodium Bicarbonate NaHCO3 Commercially Available
CAS No. 144-55-8
Metal Preservation, Corrosion VCI-416 Cleaner Corrosion Cortec Corp. (V44695)
Inhibitors/Cleaners Inhibitor
Corwipe 300 Cortec Corp. (V44695)
Plastic Blade Scraper or Spatula N/A Commercially Available
Sponges (clean and dry) Non-Scratch Scrub Sponge 3M Company (V04963)
(Scotch-Brite)
Spray bottles N/A Commercially Available
Solvents - outside surfaces Isopropyl Alcohol Commercially Available
CAS No. 67-63-0
Solvents - outside surfaces Acetone Commercially Available
CAS No. 67-64-1
Vacuum Model# VK811SIWD / 125 CFM Cleva North America (V70A87)
(or equivalent)
* Refer to the IPL, paragraph 6, for the address.

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TASK 50-11-05-100-801-A01
2. Safety Precautions

A. All cleaning materials have some hazard related to their use. Follow the safety warnings given below
to make surethat the personnel are safe and to prevent damage to the equipment.

WARNING: METHYL ETHYL KETONE (MEK) AND ACETONE ARE POISONOUS AND
FLAMMABLE. PREVENT EYE AND SKIN CONTACT AND DO NOT BREATHE
THE VAPORS. KEEP AWAY FROM HEAT AND OPEN FLAME. USE IN A WELL
VENTILATED AREA. DO NOT TAKE INTERNALLY. WEAR GLOVES AND USE
DISCRETION TO AVOID VAPOR CONTACT WITH EYES AND NOSE. USE OF
RESPIRATOR AND GOGGLES IS ADVISED.

BRULIN 815MX CONTAINS 2-AMINOETHANOL. DIRECT CONTACT CAN CAUSE

EYE IRRITATION. LONG CONTACT CAN CAUSE SKIN IRRITATION. WEAR
ADEQUATE AND DISCRETIONARY PROTECTION TO PREVENT AND MINIMIZE
SKIN CONTACT AND EYE IRRITATION.

ALL HOUSEHOLD DETERGENTS, SOAPS, AND OTHER CLEANING AGENTS

NORMALLY ARE ALKALINE SOLUTIONS. EYE IRRITATIONS AND SKIN
SENSITIVITY IS POSSIBLE. WEAR ADEQUATE AND DISCRETIONARY
PROTECTION TO PREVENT AND MINIMIZE HAZARDS.

CAUTION: ALL DISSIMILAR METALS ARE ISOLATED TO PREVENT GALVANIC CORROSION.

IF REPAIR OR REPLACEMENT IS REQUIRED, THE MAINTENANCE MECHANICS
MUST REMOVE AND REPLACE ALL SEALS AND INSULATING BARRIERS. ALL
PARTS MUST BE DISASSEMBLED AND REASSEMBLED AS SHOWN IN THE
DISASSEMBLY AND ASSEMBLY SECTIONS IN THIS CMM. ANY STRUCTURAL
DAMAGE MUST BE REPAIRED AS DESCRIBED IN THE REPAIR SECTION IN THIS
CMM.

TASK 50-11-05-100-802-A01
3. Cleaning Procedures

A. General Surface Cleaning (Including Vinyl-Decor Covered Panels)

CAUTION: THE DECORATIVE LAMINATE SURFACE OF VARIOUS INTERIOR COMPONENTS

CAN BE DAMAGED BY THE USE OF INCORRECT CLEANING MATERIALS AND
EQUIPMENT, OR INCORRECT MIXING OF THE SPECIFIED CLEANING MATERIALS.

DO NOT USE ABRASIVE MATERIALS ON THE DECORATIVE SURFACES. DO NOT

SCRAPE THE SURFACES WITH SHARP TOOLS.

(1) Use of Mild Household Detergent

CAUTION: DO NOT USE BRULIN 815MX CLEANER UNDILUTED. SOLUTIONS

STRONGER THAN SPECIFIED CAN DAMAGE THE DECORATIVE SURFACES.

(a) Prepare a solution of mild household detergent (Table 4001) with warm water (90°F -
120°F) (32ºC - 49ºC). Solution must be 1 part of detergent to 50 parts of water by volume.
Apply the solution to the surface with a sponge or cotton cloth (lint-free).

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(b) On porous surfaces, the cloth or sponge (Table 4001) should be lightly dampened with the
solution and the surfaces should be cleaned using circular swipes. Do not allow excess
solution to be forced from the sponge or cloth into the surface. Push lightly.

(c) On non-porous surfaces, such as Tedlar or vinyl, surfaces can be scrubbed with a wet
sponge or cloth. Do not allow excess to run off onto adjoining surfaces. Make sure that
excess does not come into contact with porous surfaces.

(d) For all surfaces, scrub soiled areas as necessary, and repeat applications of mild
detergent to remove contamination. Use a soft-bristled brush to clean heavily textured
surfaces or crevices. Rinse the surfaces with clean water, or use a fresh sponge or cloth
dampened with clean water to remove residue. Dry the surfaces with a clean, dry cotton
cloth (lint-free).

(2) Use of BRULIN 815MX

(a) Prepare a solution of BRULIN 815MX (Table 4001) with cool or warm water (90°F - 120°F)
(32ºC - 49ºC). Solution must be 1 part of BRULIN 815MX to 64 parts of water by volume
for light soil. Solution can be increased up to 1 part of BRULIN 815MX to 10 parts of
water by volume. The solution can be applied using a spray bottle, soft-bristled brush,
sponge, or cotton cloth (lint-free).

NOTE: Cool water works best with normal dirt and dust. Warm water works best with
oily surfaces.

(b) On porous surfaces, do not use spray bottles. Cloth or sponge should be lightly dampened
with the solution, and the surfaces should be cleaned using circular swipes. Do not allow
excess solution to be forced from the sponge or cloth into the surface. Push lightly.

(c) On non-porous surfaces, such as Tedlar or vinyl, surfaces can be scrubbed with a wet
sponge or cloth, or the material can be sprayed onto the surfaces and scrubbed with a
clean sponge or cloth. Do not allow excess to run off onto adjoining surfaces. Make sure
that excess does not come into contact with porous surfaces.

(d) For all surfaces, scrub soiled areas as necessary, and repeat as necessary to remove
contamination. Use a soft-bristled brush to clean heavily textured surfaces or crevices.
Rinse the surfaces with clean water, or use a fresh sponge or cloth dampened with clean
water to remove residue. Dry the surfaces with a clean, dry cotton cloth (lint-free).

(3) Use of CALLA 301-A LEMON

(a) Prepare a solution of CALLA 301-A LEMON (Table 4001) with cool or warm water (90°F -
120°F) (32ºC - 49ºC). Solution must be 1 part of CALLA 301-A LEMON to 4-8 parts of
water by volume for normal cleaning. For concentrated dirt, or spots, use full strength. The
solution can be applied using a spray bottle, soft-bristled brush, or cotton cloth (lint-free).

NOTE: Cool water works best with normal dirt and dust. Warm water works best with
oily surfaces.

(b) On porous surfaces, do not use spray bottles. Cloth or sponge should be lightly dampened
with the solution, and the surfaces should be cleaned using circular swipes. Do not allow
excess solution to be forced from the sponge or cloth into the surface. Push lightly.

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(c) On non-porous surfaces, such as Tedlar or vinyl, surfaces can be scrubbed with a
soft-bristled brush or wet sponge or cloth, or the material can be sprayed onto the
surfaces and scrubbed with the soft-bristled brush, a clean sponge or cloth. Do not
allow excess to run off onto adjoining surfaces. Make sure that excess does not come
into contact with porous surfaces.

(d) For all surfaces, scrub soiled areas as necessary, and repeat as necessary to remove
contamination. Use a soft-bristled brush to clean heavily textured surfaces or crevices.
Rinse the surfaces with clean water, or use a fresh sponge or cloth dampened with clean
water to remove residue. Dry the surfaces with a clean, dry cotton cloth (lint-free).

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B. Cleaning Instructions and Material Specifications for Metal Parts

CAUTION: DO NOT LET SOLVENTS TOUCH THE DECOR MATERIAL OR PLASTIC

COMPONENTS. MEK AND ACETONE CAN DAMAGE SOME COMPONENTS AND
MATERIALS.

DO NOT SATURATE CLOTH WITH SOLVENT BY PLACING THE CLOTH OVER THE
CONTAINER’S MOUTH AND TURNING THE CONTAINER TO WET THE CLOTH.
THIS CAN CAUSE CONTAMINATION OF THE SOLVENT SOURCE. DO NOT USE
OPEN CONTAINERS OR PLUNGER-TYPE SOLVENT DISPENSERS IN CLEANING
SOLUTIONS. ALWAYS POUR THE SOLVENT ONTO THE CLOTH OR USE A
DISPENSER CAN WHICH IS DESIGNED TO ISOLATE CONTAMINATION.

DO NOT SCOUR OR ABRADE SURFACES WITH LIGHT AL-O2 CORROSION.

CORROSION PROTECTION IS NORMALLY A THIN LAYER OF ANODIZING OR
ORGANIC AGENT. ABRASION CAN REMOVE THE PROTECTIVE FILM COATING.

DO NOT TOUCH THE CLEANED SURFACES. MAKE SURE TO WEAR GLOVES

AND AVOID VAPOR DURING CLEANING.

USE A SHEET LEXAN MAT OVER THE FLOORING FIXED WITH DOUBLE-COATED
ADHESIVE TO REDUCE THE IMPACT, GOUGING AND CORROSION.

COURTAULDS PRC ADHESIVE (PS 1776) IS A POLYSULFIDE, 2-PART FUEL TANK

SEALANT. IT HAS EXTREMELY HIGH PEEL ON METAL BUT MINIMAL IMPACT
ON CERTIFICATION OR BURN.

SOLVENT/CLEANER MUST NOT DAMAGE THE BASE MATERIAL AND CHEMICAL

SURFACE TREATMENT/PLATING, AND MUST NOT LEAVE A RESIDUE ON THE
SURFACE. DO NOT LET THE SOLVENT DRY ON THE SURFACE.

THE CLOTHS USED IN CLEANING MUST NOT CONTAIN ANY OIL, GREASE,
SILICONE COMPOUNDS, OR ANY OTHER RESIDUE THAT CAN AFFECT THE
ADHESION OF THE PRIMER.

NOTE: It is recommended that regardless of cleaning method employed, that metal surfaces should
be treated with a corrosion inhibitor. Metal surfaces are normally treated or anodized to
prevent corrosion. Normal wear and abnormal abuse affect corrosion, and it is always
a factor in aircraft.

NOTE: Calla 301-A Lemon and Brulin 815MX used as described in this section are mild corrosion
inhibitors. These are pH base materials which can neutralize the weak organic acids in real
coffee and orange flavored drink.

NOTE: Cortec VCI-416 and all Cortec products are specifically designed for corrosion.

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(1) Use of Solvents

(a) Dampen a clean dry cotton cloth (lint-free) with the solvent by pouring the solvent onto
the cloth. Wipe the metal surfaces with the solvent. Repeat applications as necessary to
remove all dirt. Dry the parts with a clean, dry cotton cloth (lint-free). Do not allow solvent
to evaporate on surface. Do not re-use cloth as this can redeposit contamination on the
surface. For oxidation, powdery white corrosion, use corrosion inhibitor/cleaner.

(2) Use of BRULIN 815MX

(a) Prepare a solution of BRULIN 815MX (Table 4001) with cool or warm water (90°F - 120°F)
(32ºC - 49ºC). Solution must be 1 part of BRULIN 815MX to 64 parts of water by volume,
for light soil. Solution can be increased up to 1 part of BRULIN 815MX to 10 parts of
water by volume. The solution can be applied using a spray bottle, soft-bristled brush,
sponge or cotton cloth (lint-free).

NOTE: Cool water works best with normal dirt and dust. Warm water works best with
oily surfaces.

(b) Surfaces can be scrubbed with a wet sponge or cloth, or the material can be sprayed
onto the surfaces and scrubbed with a clean sponge or cloth or soft-bristled brush. Do
not allow excess to run off onto adjoining surfaces. Make sure that excess does not
come into contact with porous surfaces.

(c) For all surfaces, scrub soiled areas as necessary, and repeat applications as necessary to
remove contamination. Use a soft-bristled brush to clean heavily soiled areas or crevices.
Rinse the surfaces with clean water, or use a fresh sponge or cloth dampened with clean
water to remove residue. Dry the surfaces with a clean, dry cotton cloth (lint-free).

(3) Use of CALLA 301-A LEMON

(a) Prepare a solution of CALLA 301-A LEMON (Table 4001) with cool or warm water (90°F -
120°F) (32ºC - 49ºC). Solution must be 1 part of CALLA 301-A LEMON to 4-8 parts of
water by volume for normal soil. Use full strength for heavy soil. The solution can be
applied using a spray bottle, soft-bristled brush, sponge, or cotton cloth (lint-free).

NOTE: Cool water works best with normal dirt and dust. Warm water works best with
oily surfaces.

(b) Surfaces can be scrubbed with a wet sponge or cloth, or the material can be sprayed
onto the surfaces and scrubbed with a clean sponge or cloth or soft-bristled brush. Do
not allow excess to run off onto adjoining surfaces. Make sure that excess does not
come into contact with porous surfaces.

(c) For all surfaces, scrub soiled areas as necessary, and repeat applications as necessary to
remove contamination. Use a soft-bristled brush to clean heavily soiled areas or crevices.
Rinse the surfaces with clean water, or use a fresh sponge or cloth dampened with clean
water to remove residue. Dry the surfaces with a clean, dry cotton cloth (lint-free).

(4) Use of VCI-416 (Recommended BEST)

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(a) Prepare a solution of VCI-416 (Table 4001) with cool or warm water (90°F - 120°F) (32ºC -
49ºC). Solution must be 1 part of VCI-416 to 50 parts of water by volume for light soil.
Solution can be increased up to 1 part of VCI-416 to 10 parts of water by volume for
heavy soil. The solution can be applied using a spray bottle, soft-bristled brush, sponge,
or cotton cloth (lint-free).

NOTE: Cool water works best with normal dirt and dust. Warm water works best with
oily surfaces.

(b) Surfaces can be scrubbed with a wet sponge or cloth, or the material can be sprayed onto
the surfaces and scrubbed with a clean sponge or cloth. Do not allow excess to run off
onto adjoining surfaces. Make sure that excess does not come into contact with porous
surfaces.

(c) For all surfaces, scrub soiled areas as necessary, and repeat as necessary to remove
contamination. Use a soft-bristled brush to clean heavily textured surfaces or crevices.
No rinsing is necessary. Allow metal surfaces to remain wet for a minimum of 1 minute
prior to drying. Dry the surfaces with a clean, dry cotton cloth (lint-free).

(5) Use of Sodium Bicarbonate Cleaners and Strippers

(a) Equipment that uses Sodium Bicarbonate stripping compounds can be used to remove
White-aluminum oxide corrosion, and can be capable of removing limited crevice or
granular corrosion products. Use of Wet bicarbonate should be inspected and make sure
coating thickness of anodize to make sure its integrity. Restore protection per REPAIR
section as needed.

(b) Dry Bicarbonate used as a grit-blast media can also be used.

(c) Regardless of wet or dry application, remove all remnants of Sodium Bicarbonate by
rinsing with clean water. Dry the surfaces using either solvent or dry shop wipe. Do not
allow the water to evaporate on the surfaces.

(6) Use of Cortec Corwipe 300

(a) Corwipe 300 Wipes are impregnated with corrosion inhibitors and offer mild cleaning.
These wipes can be used after final wipe down of surfaces with a clean, dry shop wipe.
When used as the final wipe down they will give added corrosion resistance to metal
surfaces.

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C. Cleaning Instructions for Adhesives

CAUTION: DO NOT LET SOLVENTS TOUCH THE DECOR MATERIAL OR PLASTIC

COMPONENTS. MEK AND ACETONE CAN DAMAGE SOME COMPONENTS, AND
MATERIALS.

DO NOT SATURATE CLOTH WITH SOLVENT BY PLACING THE CLOTH OVER THE
CONTAINER’S MOUTH AND TURNING THE CONTAINER TO WET THE CLOTH.
THIS CAN CAUSE CONTAMINATION OF THE SOLVENT SOURCE. ALWAYS POUR
THE SOLVENT ONTO THE CLOTH OR USE A DISPENSER CAN DESIGNED TO
ISOLATE CONTAMINATION.

NOTE: It is recommended that regardless of cleaning method employed; that metal surfaces should
be treated with a corrosion inhibitor. Metal surfaces are normally treated or anodized to
prevent corrosion. Normal wear and abnormal abuse affect corrosion, and it is always
a factor in aircraft.

(1) Use of Solvents

(a) To remove adhesive tape or adhesive residue from metal parts, dampen a clean dry
cotton cloth (lint-free) with the solvent by pouring the solvent onto the cloth. Wipe onto
the adhesive residue or tape. Peel as much tape from the surface as possible. Use of
a plastic scraper or spatula to remove as much solid material is recommended. Do not
scratch surfaces, this reduces corrosion protection. Do not use metal scrapers, as this
increases damage risk.

(b) Repeat solvent applications as necessary to remove all residues. Dry the parts with a
clean, dry cotton cloth (lint-free). Do not allow solvent to evaporate on surface.

(2) Use of BRULIN 815MX

(a) Prepare a solution of BRULIN 815MX (Table 4001) with warm water (90°F - 120°F) (32ºC
- 49ºC). Solution must be 1 part of BRULIN 815MX to 10 parts of water by volume. The
solution can be applied using a sponge or cotton cloth (lint-free).

NOTE: Warm water works best with most adhesive residues.

(b) Surfaces can be wiped with a wet sponge or cloth, or the material can be sprayed onto
the surfaces and wiped with a clean sponge or cloth or soft-bristled brush. Do not allow
excess to run off onto adjoining surfaces. Make sure that excess does not come into
contact with porous surfaces.

(c) For all surfaces, scrub soiled areas as necessary, and repeat applications as necessary to
remove contamination. Use a soft-bristled brush to clean heavily soiled areas or crevices.
Rinse the surfaces with clean water, or use a fresh sponge or cloth dampened with clean
water to remove residue. Dry the surfaces with a clean, dry cotton cloth (lint-free).

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(3) Use of CALLA 301-A LEMON

(a) Prepare a solution of CALLA 301-A LEMON (Table 4001). Use full strength. The solution
can be applied using a spray bottle, soft-bristled brush, sponge, or cotton cloth (lint-free).
Surfaces can be wiped with a wet sponge or cloth, or the material can be sprayed onto
the surfaces and scrubbed with a clean sponge or cloth or soft-bristled brush. Do not
allow excess to run off onto adjoining surfaces. Make sure that excess does not come
into contact with porous surfaces.

(b) For all surfaces, scrub soiled areas as necessary, and repeat applications as necessary to
remove contamination. Use a soft-bristled brush to clean heavily soiled areas or crevices.
Rinse the surfaces with clean water, or use a fresh sponge or cloth dampened with clean
water to remove residue. Dry the surfaces with a clean, dry cotton cloth (lint-free).

(4) Use of VCI-416

(a) For use on Metal surfaces with adhesive tape or residue. Prepare a solution of VCI-416
(Table 4001) with warm water (90°F - 120°F) (32ºC - 49ºC). Solution must be 1 part of
VCI-416 to 10 parts of water by volume. The solution can be applied using a spray bottle,
soft-bristled brush, sponge, or cotton cloth (lint-free).

NOTE: Warm water works best with most adhesive residue.

(b) Surfaces can be scrubbed with a wet sponge or cloth, or the material can be sprayed onto
the surfaces and scrubbed with a clean sponge or cloth. Do not allow excess to run off
onto adjoining surfaces. Make sure that excess does not come into contact with porous
surfaces.

(c) Scrub soiled areas as necessary, and repeat as necessary to remove contamination.
Use a soft-bristled brush to clean heavily textured surfaces or crevices. No rinsing is
necessary. Allow metal surfaces to remain wet for 1 minute. Dry the surfaces with a
clean, dry cotton cloth (lint-free).

TASK 50-11-05-100-803-A01
4. Metal Preservation and Corrosion Inhibition

A. General Surface Cleaning and Preservation Metal Surfaces. Cortec VCI-416 is non-toxic and USDA
Approved for metal surfaces. Removes oxidation as well as normal dirt and contamination. It is
recommended for use, to make sure that the metal preservation.

(1) To Use Cortec VCI-416

(a) Cortec VCI-416 Cleaner, Corrosion Inhibitor can be purchased in 16 oz (473.18 ml) spray
bottles or purchased in concentrated form. For use as a cleaner: heavy soil/ cleaning
use concentrate at 1 part VCI-416 to 10 parts water. For Light Duty Cleaning, use 1
part VCI-416 to 50 parts water.

(b) Cortec VCI-416 use as Corrosion Inhibitor: if other cleaners are used, spray metal
surfaces with Cortec VCI-416 or apply with a damp cloth. Wipe surfaces with a dry clean
cloth to remove any residue from cleaning process. Spray or apply a second coat of
Cortec VCI-416. Leave wet for a minimum of 1 minute. Follow with a clean dry, cloth.

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(c) If Cortec VCI-416 was used as cleaner, make sure that the surfaces remain wet for
1 minute prior to drying.

(2) To Use Cortec Corwipe 300

(a) Corwipe 300 Wipes are impregnated with corrosion inhibitors and offer mild cleaning.
These wipes can be used after final wipe down of surfaces with a clean dry shop wipe.

(b) When used as the final wipe down they will give added corrosion resistance to metal
surfaces.

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INSPECTION/CHECK

TASK 50-11-05-99F-808-A01
1. General

A. Refer to paragraph 2 to do a general visual inspection of the Sidewall Panel Assembly for damaged or
worn parts.

B. For the extent of damage allowed to be repaired, refer to REPAIR section to repair minor damage. If
the damage is major or beyond simple repair, replace the part.

TASK 50-11-05-210-801-A01
2. Component Inspection/Checks

A. Component inspection of the Sidewall Panel Assembly are given in Table 5001.

Inspection/Check Procedures
Table 5001/TABLE 50-11-05-210-001-A01

Component Check For Corrective Action

Sidewall Panel Assembly Punctures, scratches, or gouges Repair the damage to panel per
in the Sidewall Panel Assembly; REPAIR section; the individual
separation between the bonded panel cannot be replaced.
panel.
Bent or damaged spacer. Replace the spacer.
Loose, bent, cracked or damaged Repair/replace the cover per
cover. REPAIR section.
Loose, deteriorated, chipped, If loose, tighten with attaching
gouged, or worn doubler. hardware. If damaged,
repair/replace the doubler per
REPAIR section.
Loose, bent, cracked or damaged If loose, tighten with attaching
¼-turn retainer. hardware. If damaged, replace the
¼-turn retainer.
Deteriorated, chipped, gouged or Replace the loop fastener.
worn loop fastener.
Placard not readable or lost. Refer to REPAIR section to replace
the bonded placard.

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REPAIR

TASK 50-11-05-99F-809-A01
1. General

A. This section contains procedures for the general repairs given below:

Paragraph Repair Action

2 Replace or Install Bonded Components
3 Replace Potted Inserts
4 Fill and Relocate the Insert Holes
5 Replace Adhesive-Backed Rubstrip or Placard
6 Repair Corrosion and Restore Metal
7 Repair Fiberglass Composite Panel
8 Fill Edge Holes in Honeycomb Panels
9 Fill and Fair out Procedures for Panel
10 Paint and Prime the Composite Panels

WARNING: REFER TO CURRENT “MATERIAL SAFETY DATA SHEETS” (MSDS). THE COMPOUND
MANUFACTURER GIVES THE MSDS FOR HEALTH AND SAFETY DATA.

B. The recommended materials are given in Table 6001.

NOTE: You can apply the materials shown in Table 6001. If you would like assistance regarding
the applicable materials you can contact Safran Cabin Inc. Table 6001 does not give all the
recommended materials shown in the repair procedures (see the applicable procedures for
material specifications). Refer to the Engineering Specifications for specific materials and
other approved equivalent materials (potting compound, adhesives, solvents, primers, and
other very necessary materials).

NOTE: Equivalent items can be used.

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Repair Materials
Table 6001/TABLE 50-11-05-940-010-A01

Nomenclature Part or Specification Number Source (CAGE)*

Miscellaneous Tools:
Sealant Gun, Pneumatic Model 250 PRC - Desoto International Inc.
(PPG Aerospace) (V5HCF1)
Putty Knife N/A Commercially Available
Razor Blade N/A Commercially Available
Pliers or Router N/A Commercially Available
Heat Gun HL1920E or similar TE Connectivity Corp. (V06090)
N/A Commercially Available
Pneumatic Wrench
Soldering Iron N/A Commercially Available
Vacuum Model# VK811SIWD / 125 CFM (or Cleva North America (V70A87)
equivalent)
Pressure Spray Gun #FX tip and needle #765 air cap DeVilbiss Co. (ITW Inc.)
(JGA-502 Gun) (or equivalent) (V0GAZ6)
Siphon Cup Gun #FX tip and needle #765 air cap DeVilbiss Co. (ITW Inc.)
(JGA-502 Cup) (or equivalent) (V0GAZ6)
Cloth, Milled Glass Fibers MIL-C-9084, Hammer Milled Commercially Available
0.03125 in (0.0793 cm) length or
less.
Polyester tapes, used for Flashbreaker™ Polyester Airtech International Inc. (Airtech
multipurpose lay-up at 400°F Pressure-Sensitive Adhesive Advanced Materials Group)
(202°C). Silicone or rubber based and Release Tape (V53912)
Polyester tapes, used for Flashbreaker™ Pressure-Sensitive Airtech International Inc. (Airtech
multipurpose lay-up Adhesive Masking and Release Advanced Materials Group)
Tape (V53912)
Conformal Coating, Brush Military Spec MIL-I-46058, Class C Commercially Available or Chase
Application or Humiseal 1A33 Corp. (V99109)
Abrasive-Cloth, Aluminum-Oxide, Federal Specification P-C-451 Commercially Available
Medium-Grit
Scotch-Brite Pad Aircraft Cleaning Pad 3M Company (V04963)
Ultra Fine Hand Pad 7448 3M Company (V04963)
Sandpaper 100-400 grit Commercially Available
120-240 grit
180-220 grit
200-400 grit
Sanding Pad 320 grit Commercially Available
* Refer to the IPL, paragraph 6, for the address.

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Repair Materials
Table 6001/TABLE 50-11-05-940-010-A01 (continued)

Nomenclature Part or Specification Number Source (CAGE)*

Adhesives:
Scotch-Weld™ #30 3M Company (V04963)
Decor Bonding adhesive (Formerly Fast-Bond™ #30)
Scotch-Weld™ #30 NF 3M Company (V04963)
(Formerly Fast-Bond™ #30-NF)
Edge Wrap Aerobond 1801 Aerocell Corp. (V1SX35)
Aquabind Alternative Materials Tech Inc.
(Akzo Nobel Coatings) (V0ZXD0)
Sealant/Adhesive (stainless steel) DEVCON Aluminum Filled Epoxy ITW Polymers Adhesives NA
Per MMM-A-132 Type I or (V0RZG3)
equivalent
Henkel Loctite EA 9394 Adhesive Henkel Corp. (V1N6B3)
or equivalent
Adhesives Epibond 1210-A (Resin) Huntsman Advanced Materials
9615-B (Hardener) GmbH (V1532N)
Epibond 1559-1 A/B
Epocast 1618 D/B
Epocast 1628 A/B
L-301 A/B Cytec Industries Inc. (Solvay
Group) (V0V7G8)
Versilok 506 Accelerator #4 Lord Corp. (Chemical Products
Div.) (V30676)
Scotch-Weld™ #5 3M Company (V04963)
(Formerly Scotch-Grip #5)
DP420 3M Company (V04963)
DP190
EC-3524
Fill and Fair Compounds, Akemi #7 Standard Filler AXSON North America Inc. (Sika
Polyester Based Advanced Resins) (V3VPY6)
Akemi #4 Faster Version AXSON North America Inc. (Sika
Advanced Resins) (V3VPY6)
Micro-Ultra Filler #15-3 Adtech Plastic Systems Corp. Inc.
(V09AU0)
Fire Retardant Reducer #15-3 Adtech Plastic Systems Corp. Inc.
(V09AU0)
* Refer to the IPL, paragraph 6, for the address.

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Repair Materials
Table 6001/TABLE 50-11-05-940-010-A01 (continued)

Nomenclature Part or Specification Number Source (CAGE)*

Fill and Fair Compounds, Araldite 252, 2-part Paste Adhesive Huntsman Advanced Materials
Filler GmbH (V1532N)
Epoxy Based
DP110 3M Company (V04963)
Edge Fill L-306 Cytec Industries Inc. (Solvay
Group) (V0V7G8)
Magnolia Plastics 128-135 A/B Magnolia Advanced Materials Inc.
(V22121)
Potting Compound L-318 Kit Form Cytec Industries Inc. (Solvay
Group) (V0V7G8)
Epibond 1559-1 A/B Huntsman Advanced Materials
Epibond 420 or Redux 420 GmbH (V1532N)
Epocast 1618 D/B
Epocast 89670-A/B
1631-A/B
1632-A/B
Magnobond 92-1 A/B Magnolia Advanced Materials Inc.
(V22121)
DP420 3M Company (V04963)
Polystrate #14270 - 5 min epoxy ITW Polymers Adhesives NA
(V0RZG3)
EY-3009 A/B or EY-3010 A/B H.B. Fuller North America
7160 A/B (V26348)
7176
Aerobond 1507-A/B or 1508-A/B Aerocell Corp. (V1SX35)
Aerofill 1504-A/B
DAPCO 3040-A/B Cytec Industries Inc.(Solvay
Group) (V0V7G8)
Potting Adhesive, Epoxy Based L-318 Cytec Industries Inc.(Solvay
Group) (V0V7G8)
Structural Adhesive, Epoxy Based L-301 A/B Cytec Industries Inc.(Solvay
Group) (V0V7G8)
Core Sealer-Edge Seal, Epoxy L-306 FRHT (Alternate: Araldite Cytec Industries Inc.(Solvay
Based 252 A-B, 2-part paste or Epocast Group) (V0V7G8)
1628 A-B from Huntsman)
DAPCO 3008 A/B Cytec Industries Inc.(Solvay
DAPCO 3303 Group) (V0V7G8)
* Refer to the IPL, paragraph 6, for the address.

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Repair Materials
Table 6001/TABLE 50-11-05-940-010-A01 (continued)

Nomenclature Part or Specification Number Source (CAGE)*

Core Sealer-Edge Seal, Epoxy Magnolia 85-3 A/B Magnolia Advanced Materials Inc.
Based (V22121)
Laminating Resin Epoxy Epon 828 Resin Epikure 3223 Resolution Performance Products
DETA Catalyst LLC (Hexion Inc.) (V3FBZ6)
Epocast 50A1 (100 Parts by Huntsman Advanced Materials
weight) GmbH (V1532N)
9816 Catalyst (15 Parts by weight) Huntsman Advanced Materials
or 946 Catalyst (15 Parts by GmbH (V1532N)
weight)
Hysol ® EA 956 A/B Henkel Corp. (V1N6B3)
Sealant, Silicone (white) RTV102 Momentive Performance Materials
Dow Corning 7130 Inc. (General Electric Co.)
GE 160 (V01139)
GE 5242
Sealant/Adhesive PR 1775/1776 Class A or B Courtaulds Aerospace (PPG
Aerospace) (V05027)
P/S 890 Class A or B Sealants and Coatings
Technologies Inc. (V45DF3)
Metal Surface Protection: VCI-416 Cleaner Corrosion Cortec Corp. (V44695)
Metal Preservation, Corrosion Inhibitor
Inhibitors/Cleaners
Corwipe 300 Cortec Corp. (V44695)
Organic Coating for Aluminum VCI-386 Topcoat and VCI-393 / VCI Products are FDA and USDA
Surfaces VCI-395 Primer approved
Alodine 600/1200 Henkel Corp. (V1N6B3)
White 44-W-7 Primer A/B* Deft Inc. (PPG Aerospace)
(V33461)
Light Gray 44-W-18 Primer A/B* Deft Inc. (PPG Aerospace)
(V33461)
White 44-W-7 and 44-W-18 Deft Inc. (PPG Aerospace)
NOTE: DO NOT HAVE (V33461)
CHROMATE
Organic Epoxy Mastic M45/M46 Reduce with M95 Benjamin Moore and Co. Ltd.
Coating - Topcoat (V09585)
M62-01 Epoxy Gloss Coating Certified for Food Processing and
FDA Approved for Food Service
* Refer to the IPL, paragraph 6, for the address.

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Repair Materials
Table 6001/TABLE 50-11-05-940-010-A01 (continued)

Nomenclature Part or Specification Number Source (CAGE)*

Fluid Resistant Primers: KOROPON Courtaulds Aerospace (PPG
515-700 PAINT Aerospace) (V05027)
910-704 CATALYST
463-12-8 PAINT Dexter Corp. Polymer System
CA-116 CATALYST (V1JB33)
10-P4-7 PAINT Courtaulds Aerospace (PPG
EC-131 CATALYST Aerospace) (V05027)
515X391 PAINT Courtaulds Aerospace (PPG
910c780 CATALYST Aerospace) (V05027)
010x326 THINNER
MIL-P-23377 primer Ty II ClC C&C VenturesLLC (Randolph
MIL-T-81772B REDUCER (Green Products Co.) (V77672)
Primer)
MIL-P-23377 primer Ty II ClC C&C VenturesLLC (Randolph
MIL-T-81772B REDUCER (Yellow Products Co.) (V77672)
Primer)
Topcoats: #442-3 (GLOSS COLOR) Bostik Inc. (Arkema) (V5W425)
#X-304 CATALYST
#453-3 (FLAT COLOR) Bostik Inc. (Arkema) (V5W425)
#CA-118 CATALYST
#980- (GLOSS COLOR) WLS Coatings Inc. (V0YY71)
#982- (SEMI-GLOSS)
Sher Will Enamel F63 or H99 Sherwin-Williams Co. (V1JRP1)
V66V29 catalyst. R7KB29 or
R7K84 or R99KY29 (REDUCER)
(03Y091) Topcoat Deft Inc. (PPG Aerospace)
(03Y091) Catalyst (V33461)
MIL-T-81772 Type I Reducer
MIL-PRF-85285C, Type I Deft Inc. (PPG Aerospace)
Polyurethane (V33461)
#343-55 (Filler) Mankiewicz Gebr. & Co.
#345-15 (Hardener) (VD2603)
#346-65 (Topcoat)
#345-19 (Hardener)
Acceptable CIC Materials: NYCOTE 7-11 Nycote Laboratories Corp.
(V05803) or Chemetall Chemical
Products Inc. (V02CA7)
* Refer to the IPL, paragraph 6, for the address.

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Repair Materials
Table 6001/TABLE 50-11-05-940-010-A01 (continued)

Nomenclature Part or Specification Number Source (CAGE)*

Acceptable CIC Materials: DINITROL / ARDROX AV Series Chemetall Oakite Inc. (V0L040)
Compounds
DINITROL AV 8
DINITROL AV 15
DINITROL AV 25
DINITROL AV 30
SOCOPAC 65H Socomore (VF6892)
Solvents: Isopropyl Alcohol Commercially Available
CAS No. 67-63-0
Acetone Commercially Available
CAS No. 67-64-1
MEK (Methyl Ethyl Ketone) Commercially Available
CAS No. 78-93-3
(Fed. MIL Spec. TT-M-261)
Ethyl Alcohol (Ethanol) Commercially Available
CAS No. 64-17-5
Thinner Humiseal #33 Chase Corp. (V99109)
* Refer to the IPL, paragraph 6, for the address.

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TASK 50-11-05-300-801-A01
2. Replace or Install Bonded Components

NOTE: Refer to Table 6001 for the recommended materials. For Structural Bonding reference “Structural
Adhesives – Joints and Aluminum Doubler Bonding“ section.

WARNING: APPROVED SOLVENTS (MEK, ACETONE, ALCOHOL) ARE FLAMMABLE AND SHOULD
BE USED WITH PROPER PRECAUTIONS. ALL SOLVENTS AND ADHESIVES SHOULD
BE MIXED AND USED PER THESE INSTRUCTIONS AND/OR THE MANUFACTURER’S
RECOMMENDED PROCEDURES.

SHOULD A CONFLICT BETWEEN THESE INSTRUCTIONS AND MANUFACTURER’S

INSTRUCTIONS OCCUR, THE MANUFACTURERS’ INSTRUCTIONS WILL TAKE
PRECEDENCE, BUT NOTIFY SAFRAN CABIN INC., DIRECTOR OF MATERIALS AS
SOON AS POSSIBLE.

USE THESE ITEMS IN A WELL VENTILATED AREA AND AWAY FROM OPEN FLAMES.
IF ADHESIVES OR SOLVENT MATERIALS SHOULD COME IN CONTACT WITH SKIN
OR EYES; FLUSH AREA WITH CLEAN WATER AND SEEK MEDICAL ATTENTION
AS NEEDED.

THE USE OF PROPER PERSONAL PROTECTIVE GEAR IS REQUIRED. AT A MINIMUM:

GLOVES ARE RECOMMENDED FOR HANDLING PARTS, AND SHOULD BE WORN
WHENEVER HANDLING CHEMICALS OR SOLVENTS. GOGGLES SHOULD BE WORN
WHEN A SPLASH COULD OCCUR.

WHEN SANDING OR ABRADING PART SURFACES; A DUST OR PARTICULATE MASK

SHOULD BE WORN.

WHEN MIXING CHEMICALS OR USING SOLVENTS, AN ORGANIC VAPOR

RESPIRATOR IS RECOMMENDED, ALONG WITH GOOD VENTILATION AND
ADEQUATE LIGHTING.

A. Prior to bonding, remove any loose or damaged components. Partially bonded Metallic details and
composite parts can be removed from other panels using heat and care. Heat the bond-line to 160°F
- 180°F (71°C - 82°C) using a heat gun or similar tool until softened. Place the part in shear or peel or
tap with a rubber or plastic mallet to dislodge the parts.

B. After separation, Inspect the parts and make sure that they are sound and can be re-bonded. If
the part condition will not allow re-use, consult with Components Manual and resource new parts
(panels, doublers, etc) as needed.

C. Remove any loose debris from the surfaces of the loosened part.

D. Wipe down dirty or oily parts with a clean shop wipe or rag dampened with approved solvent from
Table 6001, and follow with a clean dry shop wipe. This will remove any film or oil from the surface to
be bonded.

E. Once the part is free of oil or film, to make sure that a satisfactory bond can be achieved, it is
recommended that the bonding surface be abraded using a medium-grit (aluminum oxide or silicone
oxide) sanding medium to remove any surface gloss. Do not sand prior to solvent wipe (step C). This
abrasive cloth will remove the loose particles and will make a uniform-grain pattern on the surfaces.

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F. Follow sanding operation with a clean, lint-free cloth dampened with approved solvent. Follow the
wipe-down process with a clean, lint-free cloth to dry. Do not allow solvent to evaporate on surface of
the part. Do not handle clean parts with bare skin.

G. For metallic parts-consult metal surface preparation section to make sure that the corrosion inhibition
prior to bonding.

H. Mix approved adhesives (two-part resin/catalyst) per the requirements of the manufacturer. Mix
no more than you can use during the pot life of the adhesive. Mix the components fully but not
excessively. Do not whip air into the mixture during the mixing process.

CAUTION: SOME CATALYZED ADHESIVES WILL EXOTHERM (GENERATE HEAT) IN MODERATE

MASS OR IF MIXED TOO AGGRESSIVELY.

I. Apply adhesive to both sides of the part(s) to be bonded to make sure uniform wet-out. It is
recommended that an adhesive comb or pneumatic sealant gun be used to make sure that a uniform
coat is applied.

– If using a sealant gun, apply a bead over the area that can be spread as appropriate to make
sure uniform coverage. A spatula or similar tool can be used for this. When applying adhesive
to both sides, spread one side lengthwise and spread the facing side width-wise so that the
two would crisscross when pressed together.

– If using a comb, spread using at a minimum teeth with 1/16 x 1/16 spread (0.125 in (0.3175 cm)
comb is preferred). When applying adhesive to both sides, spread one side lengthwise and
spread the facing side width-wise so that the two would crisscross when pressed together.

J. Push the parts together. For large areas, begin at one end and work down slowly to make sure that
no air is entrapped. Work quickly per the work-life requirements of the adhesive.

K. Remove unwanted or excess adhesive from the part using a clean spatula or similar tool. Use of a
radius gauge or similar tool to provide a neat fillet is recommended. The dry tool is useful for removing
the bulk of squeeze-out or excess adhesive. When large excess is removed, a cloth or cotton swab
dipped in acetone, isopropyl alcohol or other approved solvent can be used to remove and residual
excess away from the bond line. Do not soak or apply excess solvent to the bond line.

L. Clamp or fixture the parts as needed for a minimum of 2 hours at room temperature prior to attempting
to accelerate the cure.

1. If accelerated cure is required – gently heat the part to 120°F - 140°F (49°C - 60°C) for a
minimum of two hours. Do not heat above 160°F (71°C).

2. If Room Temperature Cure is acceptable, allow to set a minimum of 48 hours at room temperature
(62°F (17°C) minimum).

M. Physical Inspection: Use a 6 in (15.24 cm) by 0.5 in (1.27 cm) scale or similar tool as a probe to follow
adhesive bond lines. Make sure that the scale does not penetrate the bond-line greater than a depth
of 0.0625 in (0.1587 cm) in any one area, these are not flaws, but where the resin has shrunk into the
gaps. Inspect for gaps up 1 in (2.54 cm) in length and greater than 0.0625 in (0.1587 cm) in depth
but no more than one-half the thickness of the base panel. These flaws can be corrected. See
Touch-ups. Gaps greater than that defined here require that the detail be removed and re-bonded as
the excess can compromise the part.

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N. Touch-up: mix additional adhesive as needed to fill small gaps and inject into part areas as needed.
Clean and form a fillet using the adhesive and a grout or radius gauge as necessary. Allow correction
materials a minimum of 24 hours at room temperature to set, or two hours at 120°F (49°C).

O. Parts that require separation and cleaning prior to re-bonding should begin with paragraph A.

P. Seal the corners and clearances with white RTV102 Sealant as required.

TASK 50-11-05-300-802-A01
3. Replace Potted Inserts

NOTE: Refer to Table 6001 for the recommended materials. For replacing potted inserts reference
“Insert Potting Compounds“ section.

NOTE: Use these instructions to replace inserts installed with potting compounds in the honeycomb
panel. For repair of the fiberglass facings see below and referenced sections as appropriate.

WARNING: APPROVED SOLVENTS (MEK, ACETONE, ALCOHOL) ARE FLAMMABLE AND SHOULD
BE USED WITH PROPER PRECAUTIONS. ALL SOLVENTS AND ADHESIVES SHOULD
BE MIXED AND USED PER THESE INSTRUCTIONS AND/OR THE MANUFACTURER’S
RECOMMENDED PROCEDURES.

SHOULD A CONFLICT BETWEEN THESE INSTRUCTIONS AND MANUFACTURERS’

INSTRUCTIONS OCCUR, THE MANUFACTURERS’ INSTRUCTIONS WILL TAKE
PRECEDENCE, BUT NOTIFY SAFRAN CABIN INC., DIRECTOR OF MATERIALS AS
SOON AS POSSIBLE.

USE THESE ITEMS IN A WELL VENTILATED AREA AND AWAY FROM OPEN FLAMES.
IF ADHESIVES OR SOLVENT MATERIALS SHOULD COME IN CONTACT WITH SKIN
OR EYES; FLUSH AREA WITH CLEAN WATER AND SEEK MEDICAL ATTENTION
AS NEEDED.

THE USE OF PROPER PERSONAL PROTECTIVE GEAR IS REQUIRED.

AT A MINIMUM: GLOVES ARE RECOMMENDED FOR HANDLING PARTS, AND

SHOULD BE WORN WHENEVER HANDLING CHEMICALS OR SOLVENTS.

GOGGLES SHOULD BE WORN WHEN A SPLASH COULD OCCUR.

WHEN SANDING OR ABRADING PART SURFACES; A DUST OR PARTICULATE MASK

SHOULD BE WORN.

WHEN MIXING CHEMICALS OR USING SOLVENTS, AN ORGANIC VAPOR

RESPIRATOR IS RECOMMENDED, ALONG WITH GOOD VENTILATION AND
ADEQUATE LIGHTING.

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A. Inspect suspect or damaged insert and panel surround. If the Fiberglass panel is not damaged
consult with Paragraph 4 for the removal of the insert.

B. If the fiberglass panel is damaged:

– Damage is less than 1.5D (1.5x the Outside Diameter of the insert and flange):

a) Fill hole with potting compound and fair surface.

– Damage is greater than 1.5D and lower than 2.5D:

a) Mix laminating resin and prepare chopped glass fibers to fill the damaged area.

b) Mask the area outside the damage, and cut flashbreaker tape to match the hole in panel.

c) Use milled glass or chop glass fibers from woven or roving so that the glass is 0.0625 in
(0.1587 cm) or 0.25 in (0.635 cm) in length.

d) Add some dry fibers inside insert hole, and inject a small amount of laminating resin
over them – filling hole about ¼ of the way. Mix additional fibers with adhesive selection
(10% by weight) and push/fill damaged area in panel to near flush. Add some additional
unfilled resin to top and fill flush with surrounding panel. Allow to cure then sand flush
prior to insert installation.

– If damaged area is greater than 2.5D it is recommended that skin restoration with either a
wet lay-up or pre-cured fiberglass plug be accomplished prior to insert replacement. Consult
Paragraph 7for wet lay-up.

a) If adding a pre-cured fiberglass plug over the damaged area, first clean surrounding area
and smooth surfaces with an angle motor or sanding disk.

b) Wipe down surface with isopropyl alcohol or other approved solvent.

c) Pre-cured Fiberglass skin repair must overlap surrounding skins by a minimum of 0.25 in
(0.635 cm) on all sides.

d) Remove one cell (0.125 in (0.3175 cm) of core) from around the ID hole.

e) Fill hole with structural adhesive or potting compound and bond pre-cured skin plug over
the location. Make sure that the structural adhesive or potting compound adhesive fills the
additional 0.125 in (0.3175 cm) area also.

f) Allow a minimum of 24 hours to set prior to additional sanding operations.

g) Fill and fair the step out of the panel surface per other sections of this specification.

C. After insert is removed per paragraph 4 or skin is restored per paragraph 3.B.; drill hole for new insert
as needed. The hole only has to large enough to install the insert and allow the flange to be flush.

D. Inject potting compound into hole in the panel and fill a minimum of ¼ way.

E. Clean new or restored inserts by either vapor degrease or solvent cleaning. Wipe down surfaces with
a solvent damp rag, then clean and dry with a lint-free shop wipe.

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F. Do not handle degreased surfaces with bare hands.

G. Install insert in location. Can inserts are designed with an adhesive backed temporary fixing tab to
make suret that a flush installation with panel surface. The tab is larger than the flange on the insert,
and allows it to seat on the panel skin surface and hold the insert in place. Consult with source and
use the tab(s) and alignment tools as needed to make sure that the alignment is as required.

H. Alignment tools are at the discretion of the repair shop, and not a requirement.

I. Inject potting compound into one of the tabs on top of insert and make sure that the adhesive
push-out from the opposite side hole.

J. Allow adhesive to set prior to loading inserts. See Table 6002 for when part can be loaded (Green
Strength). Any adhesive not listed in Table 6002 should be cured for a minimum of 24 hours prior to
applying a load.

Adhesive Cure Time

Table 6002/TABLE 50-11-05-940-011-A01

WorkLife / Cure Time

Manufacturer Material Description
(Green strength)
Aerocell Corp. Inc. Aerobond 1507N A/B 30 minutes at 70°F+ (21°C+)
8 hours at 70°F+ (21°C+)
ITW Polymers Adhesives NA #14270 Polystrate 4-5 minutes at 70°F+ (21°C+)
1.5 hours at 30°F+ (-1°C+)
Plastic Welder II 20 minutes at 70°F+ (21°C+)
1.5 hours at 35°F+ (2°C+)
Huntsman Advanced Materials Epocast 1544 A/C 20 minutes at 70°F (21°C)
GmbH 24 hours at 70°F (21°C)
Epibond 1544 A71/D 20 minutes at 70°F (21°C)
Epocast 1544 A42/D 24 hours at 70°F (21°C)
Epocast 1544 A82/D
Epibond 1559-1 A/B 6 minutes at 70°F (21°C)
1 hour at 70°F (21°C)
Epocast 1632 A/B 45 minutes
4 hours at 70°F (21°C)
Epocast 1633 A/B 5 minutes at 70°F (21°C)
1 hour at 70°F (21°C)
Araldite 2043 5 minutes at 70°F (21°C)
1 hour at 70°F (21°C)
Araldite 2012 4 minutes at 70°F (21°C)
AW 2104 + HW 2934 1 hour at 70°F (21°C)
Epocast 1618 A/B 17 minutes at 70°F (21°C)
Epocast 1618 D/B 4 hours at 70°F (21°C)
Fastweld 10 3-4 minutes at 70°F (21°C)
1 hour at 70°F (21°C)

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Adhesive Cure Time
Table 6002/TABLE 50-11-05-940-011-A01 (continued)

WorkLife / Cure Time

Manufacturer Material Description
(Green strength)
Huntsman Advanced Materials EPIBOND 420 A/B 80 minutes at 72°F (22°C)
GmbH REDUX 420 A/B
H.B. Fuller North America FR 7162 A/B 10 minutes at 70°F (21°C)
8 hours at 70°F (21°C)
FR 7176 A/B 10 minutes at 70°F (21°C)
8 hours at 70°F (21°C)
Magnolia Advanced Materials Magnobond 92-1 A/B 10 minutes at 70°F (21°C)
Inc. 8 hours at 70°F (21°C)
3M Company DP420 20 minutes at 70°F (21°C)
4 hours at 70°F (21°C)
DP460 60 minutes at 70°F (21°C)
4 hours at 70°F (21°C)
EC-2216 A/B 30 minutes at 70°F (21°C)
4 hours at 70°F (21°C)
EC-3333 B/A 30 minutes at 70°F (21°C)
4 hours at 70°F (21°C)

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HONEYCOMB PANEL
INSERT CAVITY

1. PREPARE THE HOLE FOR THE INSERT.

2. INCREASE THE HOLE BENEATH SKIN.
INITIAL CAVITY IS SHOWN NET SIZE.
REMOVE 1 CELL WIDTH (MIN).
IS NECESSARY TO REMOVE ONE CELL WIDTH CORE.
ADD POTTING COMPOUND (RECOMMENDED
ON PANELS WITH 2−PLY OR MORE SKINS).

ADHESIVE BACKED PLASTIC

OR METAL TAB TAB

INSERT
INSERT

4. A PIN, PAPER CLIP, OR VENDOR

3. ALIGN THE ADHESIVE TAB TO FILL/VENT (V97393) SUPPLIED GUIDE
HOLES ON THE INSERT. TOOL CAN BE USED TO AID ALIGNMENT.
(REFER TO TABLE 6001)

INJECT POTTING
INJECTION TAB COMPOUND
VENT VENT TAB

POTTING POTTING
CAVITY CAVITY
TAB

INSERT

5. INSTALL THE INSERT, PUSH 6. INJECT THE POTTING COMPOUND THROUGH

THE TAB ON PANEL. MAKE THE HOLE IN INSERT UNTIL COMPOUND
SURE THE PROPER SEATING. EXTRUDES THROUGH THE OPPOSITE VENT.

PLUG

7. REMOVE THE TAB AND TRIM PLUGS

FLUSH WITH THE PANEL.

Insert Installation with Potting Compound

Figure 6001/GRAPHIC 50-11-05-300-010-A01

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TASK 50-11-05-300-803-A01
4. Fill and Relocate the Insert Holes

NOTE: Refer to Table 6001 for the recommended materials. If you would like assistance regarding the
applicable materials you can contact Safran Cabin Inc.

A. Remove the insert.

NOTE: The insert, when potted into a sandwich structure, holds the composite or other components
in position. Before the insert installation, the core is relieved below the skin and around the
hole perimeter of the insert. This does not let the adhesive plug to pull out of the composite.

(1) ALTERNATIVE 1:

(a) To remove the metal inserts, apply heat to them with a soldering iron. Put the end of the
soldering iron into the insert sleeve (threaded or through hole).

NOTE: The heat increases the temperature of the potting compound and the insert. As a
result, the L-318 potting compound cracks around the insert. Five (5) minutes
are necessary for this process to occur. The glass or carbon skins must show
no cracks or fractures.

(2) ALTERNATIVE 2:

(a) Put a bolt into the insert and, with a pneumatic wrench, apply a torque of 80 - 100 lbf-in (9
- 11.2 N-m). The standard inserts are made to get about 70 lbf-in (7.9 N-m) of torque.
When you increase the torque, the insert will turn and will permit removal of the insert
together with some of the defective adhesive.

(b) Let the insert turn freely for a minute or more to build heat and friction. The heat will crack
the epoxy and permit its removal. Do not cause damage to the skins. If you cannot
remove the insert easily, refer to Alternative 1.

B. After the insert removal, clean the panel hole to remove all dirt, dust, or other unwanted material.
If necessary, remove an additional amount of core at ~0.05 in (0.127 cm) below the surface with a
router. Let the skin stay intact. This will cause a blockage of the “plug” mechanically. If necessary,
clean the area with Isopropyl Alcohol, acetone, or other approved solvent.

C. Apply a 0.002 in (0.00508 cm) thick mask of flashbreaker mylar, glass, polyester, or other masking
tape around the insert hole.

D. Fill the hole with an applicable potting compound. Use a spatula or an equivalent edge tool to remove
the unwanted compound from the surface. Move the edge tool at an angle along the flashbreaker
tape to remove the unwanted adhesive. Do this until the remaining compound is 0.002 in (0.00508
cm) maximum above the skin surface.

CAUTION: BE CAREFUL WHEN YOU REMOVE THE MASKING TAPE TO PREVENT DAMAGE,
SCRATCH, OR CUT TO THE PANEL SURFACE.

E. Remove the masking tape. Apply the edge tool along the skin surface. Let the compound cure for
a sufficient time.

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F. After the cure of the compound, make the lifted edges smooth with a 180-220 grit sandpaper, if
necessary. To paint the composite, refer to paragraph 10.

G. Identify the new location and drill the composite to the correct diameter and depth.

H. Remove the core below the composite skin at ~0.05 in (0.127 cm) in the new location.

NOTE: There can be an overlap between the old and the new locations. If this occurs, release the
skin where it was not removed before. See Figure 6002.

CORE PLUG EXTENDS PAST SKIN

REMOVE CORE PAST SKIN AS REQUIRED

Fill and Relocate the Insert holes

Figure 6002/GRAPHIC 50-11-05-300-002-A01

TASK 50-11-05-300-804-A01
5. Replace Adhesive-Backed Rubstrip or Placard

NOTE: Refer to Table 6001 for the recommended materials. If you would like assistance regarding the
applicable materials you can contact Safran Cabin Inc.

A. Use a flat-blade screwdriver or an equivalent tool to remove the damaged rubstrip or placard from
the panel.

B. Clean the panel with ethyl alcohol to remove the adhesive and other contamination.

C. Remove the contact sheet from the back of the replacement rubstrip or placard.

D. Install the rubstrip or placard in the same location on the panel. Push the rubstrip or placard from the
center out to remove the air bubbles.

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TASK 50-11-05-300-805-A01
6. Repair Corrosion and Restore Metal

NOTE: Refer to Table 6001 for the recommended materials. If you would like assistance regarding the
applicable materials you can contact Safran Cabin Inc.

CAUTION: ALL DISSIMILAR METALS ARE ISOLATED WITH SEALS TO PREVENT GALVANIC
CORROSION. IF A REPAIR OR REPLACEMENT IS NECESSARY, THE MAINTENANCE
MECHANICS MUST REMOVE AND REPLACE ALL SEALS AND INSULATING BARRIERS.
REFER TO THE DISASSEMBLY AND ASSEMBLY SECTIONS IN THE APPLICABLE CMM,
TO DISASSEMBLE AND ASSEMBLE ALL PARTS. NO DEVIATIONS ARE PERMITTED.
ALL DEVIATIONS FROM THE REPAIR INSTRUCTIONS IN THIS DOCUMENT WILL VOID
THE WARRANTY GIVEN BY SAFRAN CABIN INC.

NOTE: For removal and installation of the parts/items intended for corrosion repair, refer to the
Disassembly, Assembly, and IPL sections in the applicable CMM. This Repair section applies
only to these subsequent material specifications:

(A) Aluminum stock, 0.375 in (0.9525 cm) thick, 7075-T73, Hard Anodized per MIL-A-8625 Ty
III (Floor).

(B) Sheet Stock Aluminum, 0.02 - 0.1 in (0.0508 - 0.254 cm) thick, Chem Filmed per MIL-C-5541,
or Anodized per MIL-A-8625 Ty II or III.

(C) Fittings Aluminum Stock 7075-T731, Chem-Filmed per MIL-C-5541, Class 1A Primer per
CDSPS007 or MIL-P-23377, and Topcoat per CDSPS007.

NOTE: You will keep the structural integrity of the part if you obey the repair requirements correctly and
carefully. The Flammability and other Certification will not be affected if you obey the limits and
the recommended materials in this document. If you want to use alternative materials which
have the same performance and requirement, if you would like assistance you can contact
Safran Cabin Inc.

NOTE: If light dust of Aluminum Oxide is the only corrosion present, obey the instructions that are given
in paragraph 6.A. (Size Limits for Repairs). Obey the Corrosion Inhibition (Surface Protection)
and Painting instructions (Primer Application Instructions) given in Paragraphs 6.E. and 6.G.

WARNING: DO NOT TOUCH THE CLEANED SURFACES. BE SURE TO WEAR GLOVES AND AVOID
VAPOR DURING CLEANING AND REPAIR.

A. Size Limits for Repairs

(1) Aluminum Fittings (Non-critical)

(a) You can repair damage up to 20% of non-critical fittings. Repair the damage which is more
than 20% of the fitting or includes two attachment points in a sequence. Replace the fitting.

NOTE: Refer to the Cleaning section in the applicable CMM for cleaning instructions
before repair. For Corrosion Repair Instructions, refer to paragraph 6.C. Apply
Aluminum-Filled Epoxy on the contour of the surface.

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(2) Aluminum Fittings (Critical).

(a) You can repair damage from 5% to 10% on upper floor fitting installation holes.

(b) Do not repair damage on lower floor fitting installation holes because these positions
carry most of the load.

(c) You can repair damage up to 10% on all the surfaces of the floor fittings. Do not repair
damage which is more than 5% of the fitting or includes two attachment points in a
sequence. Replace the fitting.

NOTE: Refer to the Cleaning section in the applicable CMM for cleaning instructions
before repair. For Corrosion Repair Instructions, refer to paragraph 6.C. Use
Aluminum-Filled Epoxy to fair out the surface to the contour.

(3) Stab-in Extrusions (Non-critical)

NOTE: It is not necessary to remove all signs of the epoxy adhesive on the extrusion or the
panel to make the repair. Use a scribe or an equivalent tool to examine the epoxy
filler. Remove all loose pieces.

NOTE: Refer to the Cleaning section in the applicable CMM for cleaning instructions before
repair. For Corrosion Repair Instructions, refer to paragraph 6.C. You can bond small
section of stab-in extrusion in the remaining gaps. It is permitted to fill the area with
Aluminum-Filled Epoxy.

(a) Extrusions that have through holes or clearance holes, where fittings are attached to
plates or metal fittings in the panel, are non-critical extrusions. If these extrusions are
non-cosmetic, you can repair them up to 30% of the length and up to ½ the thickness of
the original part. The mechanics must examine the extrusion carefully to make sure that
the extrusion is chemically protected/repaired to prevent more corrosion.

(4) Stab-in Extrusions (Critical)

NOTE: It is not necessary to remove all sign of the epoxy adhesive on the extrusion or the
panel to make the repair. Use a scribe or an equivalent tool to examine the epoxy
filler and remove all loose pieces.

NOTE: Refer to the Cleaning section in the applicable CMM for cleaning instructions before
repair. For Corrosion Repair Instructions, refer to paragraph 6.C. You can bond small
section of stab-in extrusion in the remaining gaps. It is permitted to fill the area with
Aluminum-Filled Epoxy.

(a) Extrusions, which are attachment points or where fittings are attached directly to, are
critical components. If these extrusions are damaged, get access to and identify them.
The attachment points can be critical to the related forward or downward Certification
Loading of the unit (if it holds a door or other component in position). You can repair or
replace these extrusions. If you would like assistance regarding the damages you can
contact Safran Cabin Inc, for analysis.

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B. Cleaning Requirements for Corrosion Removal

NOTE: Refer to the Cleaning section in the applicable CMM for cleaning of the metal parts.

C. Corrosion Repair Instructions

NOTE: Make sure that the damaged parts agree with the size limits for repair that are given in
paragraph 6.A.

(1) For Pit or Crevice Corrosion

(a) Use a grinding wheel or router bit to make the surface smooth and remove the pit type
corrosion. Use a vacuum to remove the particles and unwanted materials.

(b) Fill the service pits and corrosion with Devcon Aluminum-Filled Putty or Henkel Loctite
EA 9394.

(c) Make the surface smooth.

(d) If the anodized coating is removed in metal areas adjacent to the repair, use Alodine
Solution to make the surface resistant to corrosion again. For Surface Protection, refer
to paragraph 6.E.

(2) Exfoliated or Inter-Granular Corrosion

NOTE: To know the true extent of the damage and repair, remove all inter-granular corrosion.

(a) To make sure that all metal in bad condition and corrosion products are removed, do an
inspection on the component with a 5 or 10X loop.

(b) Use rubber-base wheels soaked with aluminum oxide to grind and to blend out or to make
the edges of the damaged areas smooth.

(c) Chemically inhibit the exposed surfaces and repair the chemical surface films or paints in
the same manner as other metallic surfaces.

NOTE: Cut away or abrade the exfoliated metal to clean the surface. This is not to
permit the embrittled layers to spread damage through the mounting. Use an
aluminum-filled epoxy that agrees with the minimum requirements of MM-A-132
Type 1.

D. Replacement of Aluminum Sections

(1) Example of replacement:

(a) Cut away a section of a non-critical stab-in extrusion.

(b) Bond in position one stab-in section or a solid piece of aluminum. The function of some
of these extrusions are to increase the compression loading that the panel or unit can
support.

(c) Remove a section of extrusion and replace it with a solid aluminum piece of the same
width and length.

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(d) Use Epoxy adhesives to bond the solid aluminum piece to make sure that the compression
loads are tolerated.

E. Surface Protection

(1) Chemical Surface Protection/Repair Anodized or Chem-Filmed Surfaces.

NOTE: Apply Alodine 600/1200S with a brush to the panel surfaces. Use Alodine 600 or
Alodine 1200 to seal the aluminum. You must paint the surfaces with Alodine solution.
Use Alodine 600 for parts that will stay in as “treated” condition. Use Alodine 1200S for
parts which must be painted. Refer to Henkel Corp. (V1N6B3) or supplier for Alodine
mixing Instructions and verification of material.

(a) Make sure that the Alodine covers all surfaces without protection. Let the parts stay
in Alodine for the sufficient time for them to soak fully. If it is necessary to apply the
protection with a brush, apply a thin uniform. The protection is satisfactory after 5 minutes.

(b) Flush the surfaces with clean, cold water. If possible, use distilled water. To prevent
contamination to the main body of the water, you must continuously overflow the water.

NOTE: Put the new or removed metal components into Alodine 600/1200S. For this
procedure, do steps (c) and (d):

(c) Make sure that the Alodine covers all surfaces without protection. Put the components
into the solution for 1 to 5 minutes. Let the parts stay in Alodine for the sufficient time for
them to soak fully.

(d) Flush the surfaces with clean and cold water. If possible, use distilled water. To prevent
contamination to the main body of the water, you must continuously overflow the water.
Collect the flowing water as practical. The water and treatment solution contain acids,
chromium compounds, and complex fluorides. To discard these materials, refer to
paragraph 6.F.

(2) Additional Corrosion Protection

NOTE: Safran Cabin Inc. normally does extensive tests to make sure that the materials used
do not significantly increase burn risks in the cabin. The related materials are those
included in this section and used as primers and topcoats on metal surfaces.

(a) Use Primers per MIL-P-23377 or organic primers to make the corrosion protection better.
These materials, when applied to metallic surfaces, do not significantly increase the
Flammability risk. Safran Cabin Inc. recommends you use these materials in areas that
are not cosmetic or viewable when you assemble the component. These materials
significantly make the corrosion inhibition better. For Primer Application Instructions,
refer to paragraph 6.G.

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F. Waste Disposal

NOTE: You must also obey the Applicable Local Regulations. Use the information below only as a
general guide.

NOTE: You can use alternative primers for metal protection. Primers must not contain chromate for
Class Divider Components. Refer to Table 6001 for Primers and Topcoats that agree with
USDA and FDA requirements for Food storage components.

(1) Disposal information for Alodine 600 and Alodine Toner 22 is given on MSDS Sheet for products.
Treat and neutralize the unwanted material before you discard it to the sewer (examine the
Local Regulations and Waste treatment Bulletin WT1004 from Parker-Amchem). Apply a
primer on the surface for full protection. Primers, shown in Table 6001, are corrosion-resistant
materials. For Primer Application Instructions, refer to paragraph 6.G.

G. Primer Application Instructions

GENERAL PRIMER INSTRUCTIONS:

NOTE: Refer to Table 6001 for the recommended materials. If you would like assistance
regarding the applicable materials you can contact Safran Cabin Inc.

(1) FR (Fluid Resistant) epoxy primers and FR epoxy topcoats are two-part catalyzing materials
purchased as a kit. When you mix them, only use the catalyst indicated for use with the
applicable base component.

(a) Mix the base material correctly before you add the catalyst.

(b) Slowly add catalyst while you mix the base component.

NOTE: Before you use the catalyzed primers, let a minimum of 15 minutes for their
chemical reaction. For catalyzed topcoats, let a minimum of 45 minutes. When
kept in a closed container at ambient temperature, catalyzed materials have an
useable pot life of 4 hours. You must mix the catalyzed materials all the time.

(c) When you use a spray gun, first put the material through a filter. Do this to prevent
clogging and contamination of the applied coatings.

(2) Mixing and Thinning Ratios

(a) Mixing

1 For the correct mixture ratios, make sure to mix the full contents of each part of the kit.
To use the full contents of the kits, purchase applicable kits for specific applications
and job requirements. To mix less than a full kit, add accordingly (by volume or weight
the necessary proportion of each component) to a mixture container.

(b) Thinning

1 FR (Fluid Resistant) primers and FR topcoats are prepared to use them when
catalyzed. If the thinning of the topcoat is necessary, change the viscosity to vary
from 18 to 21.5 seconds. Use a #2 Zahn cup with thinner for optimum application.
Refer to Table 6001 for list of topcoats and primers.

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(3) Requirements

NOTE: The chemical surface treatment must agree with the requirements specified on the
applicable Finish Specification.

(a) Dry Film Thickness

1 FR Primer

NOTE: The optimum thickness for FR Primer dry-film is 0.001 - 0.0013 in (0.00254 -
0.0033 cm). The permitted primer thickness on edges, ends, and recesses
can vary from 0.0006 - 0.002 in (0.001524 - 0.00508 cm), if the fit or function
of the part is not damaged.

2 FR Topcoat

NOTE: The optimum thickness for FR Topcoat dry-film is between 0.0012 - 0.0017
in (0.00305 - 0.004318 cm).

(b) Coating Appearance

1 When a primer and topcoat are specified, the system must be uniform, correct color,
full hiding, and with no defects (cratering, pinholes, blisters, unwanted materials,
scuffs, scratches, dry over-spray, runs, or sags). Small paint runs are permitted on
hidden items and items to which it is not easy to apply a coat, but make sure that
the fit and clearance are not changed.

2 Adhesion Test: After 16 hours, you can apply a tape test to the coating system. Use
3M #250 applied to the surface with 5 - 6 lb (2.27 - 2.72 kg) of pressure. Abruptly
pull the tape and examine for removal. If removal of paint occurs, paint again as
necessary.

(4) Primer Application Instructions

(a) To clean the equipment, refer to the instructions in the Cleaning section of the affected
CMM.

(b) Use a pressure spray or siphon cup gun or equivalent (Table 6001) to apply a full-covering
wet cross-coat. Full coverage is indicated by the color of primer and contrast with the
aluminum.

NOTE: On surfaces, which have a primer, apply one light and uniform coat of FR Primer
before you apply the topcoat.

NOTE: For 502 Pressure Spray gun with #FX tip and needle #765 air cap (or equivalent),
control the equipment to supply 6 - 9 psi (41.37 - 62.05 kPa) at the feed tank and
35 - 45 psi (241.32 - 310.26 kPa) at the gun. For 502 Siphon Cup gun with #FX
tip and needle #765 air cap (or equivalent), control the air pressure to supply 35 -
45 psi (241.32 - 310.26 kPa) at the gun.

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(c) Primer Dry Time:

Dry Time
Dry the primer in the air to permit you to touch it. 30 minutes
Dry the primer in the air to permit you to stack it.
Dry the primer in the air to permit you to remove grease with 16 hours
vapor.
Dry the primer in the air to make it resistant to water (Do not 48 hours
put it into water).
Dry the Plumbing Lines in the air to permit you to do a Pressure 2 hours minimum
Test (Do not put them into water).

Make the primer cure faster to permit you to do a Pressure Test Dry in the air for a minimum of 5 minutes
or remove grease with vapor. and then bake at approximately 200°F
(93°C) for a minimum of 15 minutes.
Dry the primer in the air to permit you to topcoat it. 1 hour minimum to 3 hours maximum
(see Note).
Make the primer cure faster to permit you to topcoat it. Dry in the air for a minimum of 5
minutes and then bake at approximate
time/temperature.
Make the primer cure faster. Dry in the air for a minimum of 5
minutes and then bake AT A MAXIMUM
TEMPERATURE OF 225°F (107°C).

NOTE: The optimum time to dry the primer in the air to topcoat is 1 to 3 hours. You
can extend the dry time to a maximum of 24 hours, if you do not remove
the parts/surfaces from the clean environment of a paint shop and you use
contamination-free methods to handle them.

(d) Topcoat:

1 Use a spray gun or apply a full wet cross-coat. The time to dry in the air is 16 hours
minimum. Dry the topcoat in the air for a minimum of 10 minutes. Then bake it at a
maximum temperature of 225°F (107°C).

H. Install the Fasteners Wet to Decrease the Corrosion Rate (Refer to Table 6001 for the recommended
materials. If you would like assistance regarding the applicable materials you can contact Safran
Cabin Inc.).

NOTE: You must install the fasteners wet to decrease the corrosion rate. To use Corrosion Inhibiting
Compounds (CIC) or catalyzed primers, refer to the instructions given in this Repair section.

(1) Refer to the Cleaning section in the applicable CMM for surface preparation (cleaning).

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(2) CIC Methods of Application

(a) Method A – Dip

1 Put the component into the CIC momentarily with one continuous movement for full
coverage of the chosen area.

2 Let the unwanted compound to drain freely from the surface.

3 Use an absorbent cloth or brush to remove the drips and sags that do not flow or
fall from bottom edges.

(b) Method B – Brush

1 Use a clean touch-up brush to apply the compound with a smooth, continuous
movement. When you soak the brush again with the compound, apply the brush
in overlap movements.

2 Apply the brush again to those regions where it is not easy for the compound to make
a continuous layer. This includes notched details, unfilleted inside corners, crevices,
and undercut edges (between laminated or stack shims).

(c) Method C – Spray

NOTE: Refer to manufacturer’s instructions for equipment (where applicable).

1 The spray technique is equivalent to other sprayable materials. You will get a full
and best coverage with a smooth, continuous sweep, slightly overlapping at the
ends of each pass.

2 Apply the spray gun again to the regions where compound shows dry or light in
coverage, and in specially not easy areas where blow-back often occurs. This
includes notched details, unfilleted inside corners, crevices, etc.

(3) Installation of Fasteners and Application of Torque

(a) The “wet” (with Corrosion-Inhibiting Compound) installation of fasteners must occur before
the CIC “working time” is expired. For the assembly time, refer to Table 6001.

(b) Complete the torque application in a minimum of 60 minutes (20 minutes or less for
materials with work-lives shorter than one hour) or in an approved assembly time. Tighten
all bolt and nut installations to maximum values, unless specified differently.

NOTE: Use the dry bolt torque, unless the bolt is self-lubricated as shown in the
applicable part specification (wet CIC is not a lubricant).

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(c) When necessary, apply torque again to the nut/bolt combination with the maximum torque
value. If you would like assistance you can contact Safran Cabin Inc. Complete the
reapplication of torque before the assembly time expires. The ambient temperature and
humidity can change the assembly time. Refer to Materials and Process for specific
application of CIC. Do not use the power-torque control tools to apply the torque again.

NOTE: It is not necessary to remove the CIC from threaded assemblies, if you apply all
the torque during the assembly time.

(4) General requirements for “wet” assembly with CIC.

(a) Use a spray gun, a brush, or put the threaded components into the CIC momentarily
where applicable. If you would like assistance you can contact Safran Cabin Inc.

NOTE: It is better to apply the CIC with a brush on part details, such as: small diameter
holes and / or radii and fillets.

(b) To assemble all treated surfaces, refer to the preparation, application, and installation
procedures in this document.

(c) Touch-Up:

1 If the coating shows to be deficient, touch up the component again with a localized
treatment before assembly.

2 Keep the touch-up to a minimum with a sufficient coverage to make sure for the
CIC layer continuity.

NOTE: You can apply the materials shown in Table 6003. If you would like assistance
regarding the applicable materials you can contact Safran Cabin Inc.

Properties of Corrosion-Inhibition Compound (CIC) Materials

Table 6003/TABLE 50-11-05-940-009-A01

Dry Layer Handling Assembly

Material Material Type Design Type
Thickness Time (Hrs) Time (Min)
CIC, Tack-free,
0.013 in (0.033 cm)
NYCOTE 7-11 Thin Film, Dry Layer 1 < 60
(one dip coat)
Abr. Resistant
CIC, Tack-free,
water 0.008 in (0.02032
DINITROL AV 8 Dry Layer < 1 < 60
displacing, cm) (nominal)
medium term.
CIC, Tack-free,
0.015 - 0.025 in
DINITROL AV water
Dry Layer (0.0381 - 0.0635 ~1 < 60
15 displacing,
cm)
long term.

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Properties of Corrosion-Inhibition Compound (CIC) Materials
Table 6003/TABLE 50-11-05-940-009-A01 (continued)

Dry Layer Handling Assembly

Material Material Type Design Type
Thickness Time (Hrs) Time (Min)
CIC, Soft,
DINITROL AV general
Tacky Layer 0.025 in (0.0635 cm) ½ - 1 < 60
25 purpose,
long term.
CIC, Tack-free,
DINITROL AV water 0.03 in (0.0762 cm)
Dry Layer 3 60-90
30 displacing, (nominal)
long term.
CIC, Tack-free,
water
SOCOPAC 65H Dry Layer 0.015 in (0.0381 cm) ~1 < 60
displacing,
long term.
CIC, Soft,
~0.02 in
self healing,
(0.0508 cm)
COR-BAN 22 water Tacky Long ~1 < 60
0.04 in (0.102
displacing,
cm) - wet
long term.
CIC, Soft,
~0.02 in
self healing,
(0.0508 cm)
COR-BAN 33 water Tacky Moderate ~1 < 60
0.04 in (0.102
displacing,
cm) - wet
medium term.
CIC, Tack-free, ~0.02 in
water (0.0508 cm)
COR-BAN 35 Dry Layer < 1 < 60
displacing, 0.04 in (0.102
long term. cm) - wet
CIC, Tack-free, ~0.01 in
COR-BAN water (0.0254 cm)
Dry Layer < 1 < 60
D-5023NS displacing, 0.025 in (0.0635
short term. cm) - wet
CIC, Tack-free, ~0.03 in
COR-BAN water (0.0762 cm)
Dry Layer < 12 > 60
D-5029NS displacing, 0.076 in (0.193
medium term. cm) - wet

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TASK 50-11-05-300-807-A01
7. Repair Fiberglass Composite Panel

NOTE: Refer to Table 6001 for the recommended materials. If you would like assistance regarding the
applicable materials you can contact Safran Cabin Inc.

WARNING: DIRECT CONTACT WITH ISOPROPYL ALCOHOL CAN CAUSE IRRITATION IN EYES,
NOSE, THROAT, AND SKIN. EXTENDED PERIODS OF CONTACT CAN CAUSE
HEADACHES, DIZZINESS, AND NAUSEA. WEAR GLOVES, APRON, AND GOGGLES.
USE THIS PRODUCT IN AN AREA WITH GOOD AIRFLOW. DO NOT BREATHE THE
FUMES. DO NOT TAKE INTERNALLY. IF YOU DO NOT OBEY THIS WARNING, INJURY
TO OR DEATH OF PERSONS CAN OCCUR.

FILLER COMPOUNDS ARE POISONOUS AND FLAMMABLE. WEAR PROTECTIVE

APPAREL TO PREVENT EYES AND SKIN CONTACT. DO NOT BREATHE THE FUMES.
KEEP THESE PRODUCTS AWAY FROM HEAT AND OPEN FLAME. USE THEM
IN AN AREA WITH GOOD AIRFLOW. DO NOT TAKE INTERNALLY. FLUSH THE
CONTAMINATION FROM YOUR EYES WITH WATER.

A. Classifications of Damage on Honeycomb Panels:

NOTE: If you would like assistance you can contact Safran Cabin Inc. to make sure which class
is applicable to the Safran Cabin Inc. unit.

(1) Class 1: Dents, surface scratches, scars, reinforcement delamination, or resin erosion. No
damage to the glass or carbon fibers. Local compression of the honeycomb core on dents. The
friction and vibration of two facings cause the Resin Erosion. One sign that shows the resin
erosion is the quantity of resin “dust” on the surfaces. Scratches are cosmetic defects in the
resin surface that do not cause damage to the underlying reinforcement. Refer to paragraph
7.B and see photos Class 1-1 and Class 1-2 in Figure 6003.

(2) Class 2: Small Punctures or Glass Fracture. Puncture in one side of the glass facing. Refer to
paragraph 7.C and see photos Class 2-1 and Class 2-2 in Figure 6003.

(3) Class 3: Holes or damage that extend fully through the sandwich panel. These include the two
facings and the core that are less than 16 in2 (103.2256 cm2). Refer to paragraph 7.D.

(4) Class 4: Extensive Damage, greater than 16 in2 (103.2256 cm2). The replacement of the panel
section or parts is necessary. DO NOT REPAIR THIS KIND OF DAMAGE.

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PHOTO CLASS 1−1 DENT PHOTO CLASS 1−2 DENT

CLASS 2−1 FRACTURE OF GLASS FACING (ONE SIDE ONLY)

Damage in Honeycomb Panels

(Sheet 1 of 2)
Figure 6003/GRAPHIC 50-11-05-300-004-A01

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Damage in Honeycomb Panels

(Sheet 2 of 2)
Figure 6003/GRAPHIC 50-11-05-300-004-A01

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B. Criteria and Repair Procedures for Class 1:

(1) Imperfection: Surface Depressions; Dents, Scratches, Shallow Scars, Surface Abrasion, and
Resin Erosion.

(a) Permitted Limits:

1 Decorative surface: Not permitted.

2 Non-Decorative Surface: The imperfection is permitted if it does not go into the

material reinforcement.

(b) Correctable Limits:

1 Decorative surface: The imperfection must not go into the material fibers and the
correction must not increase the panel weight by more than 2%.

2 Non-Decorative Surface: On imperfections that go into the material fibers, you cannot
repair them by this procedure.

CAUTION: PANELS WITH MORE THAN THE MAXIMUM PERMITTED COMPRESSION

STRESS (FOR A SPECIAL COMPONENT, OR SHARP CRASH, OR
EQUIVALENT TRAUMA), TYPICALLY CAUSE CORE DAMAGE. THE
SUBSEQUENT PROCEDURE INCREASES THE COMPRESSION STRESS OF
A LOCAL AREA SIGNIFICANTLY BECAUSE OF THE WEIGHT INCREASE AND
FLAMMABILITY PROBLEMS. THE REPAIR MUST NOT BE MORE THAN 16 IN2
(103.2256 CM2) OF THE PANEL AREA.

(c) Repair Procedure for Dents, Scratches, and Resin Erosion:

NOTE: The 16 in2 (103.2256 cm2) area for repair is the limit for an individual repair. The
limit quantity of repairs per galley panel should be 3 and each individual repair
should not extend in any length more than 4 in (10.16 cm) and if more than one
repair is done it should be at least 12 in (30.48 cm) from any adjacent repair.
If it is found that more repairs are required you should seek approval from local
authorities.

1 Make the surface smooth with a 120-240 grit sandpaper.

2 Use MEK or Isopropyl Alcohol and a clean, dry shop wipe. Make the cloth moist with
the solvent and rub it against the damaged area. After you use the moist cloth, apply
a clean, dry shop wipe. Do not let the solvent dry on the part surfaces.

NOTE: A part will be clean if there is no indication of dirt, oil, or unwanted materials
after you pass a clean, dry shop wipe on it.

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3 To mix Akemi #4 or Akemi #7, remove a 2 in (5.08 cm) diameter plug of filler and
place it on the mixing card. Squeeze out a 1 in (2.54 cm) long ribbon of Part B on
the mixing card. To mix the materials, fold Part B into Part A. The mixture must be
homogeneous after you mix the materials. The material is exothermic, do not mix it
for more than 1 minute.

NOTE: Furane (Huntsman) Araldite-252 epoxy paste, Akemi, and Adtech

MicroFillers have equivalent mixture instructions. These products are two
part materials. Part A is a light gray polyester resin. Part B is a small tube of
catalyst.

4 Immediately apply the filler on the void/dent/scratch area. Overfill slightly the
damaged area with the filler to permit its shrinkage.

5 Minimum cure time at 72°F (22°C) is 15 to 20 minutes, increase cure time if compound
is spread thicker. After compound is cured, sand the surface.

6 If necessary, make the surface smooth with a 120-240 grit sandpaper.

NOTE: Non-cosmetic surfaces which only filling material is necessary: Fill the
damaged area with the epoxy or polyester type materials shown here or use
one part adhesives and sealers (RTV’s). Apply these materials only to seal
the panel from water absorption and for non-cosmetic repair.

CAUTION: DO NOT TRY TO INCREASE THE SPEED OF THE MATERIAL CURE WITH THE
AID OF A LARGE QUANTITY OF CATALYST. MANY FILLERS AND ADHESIVES
WILL CURE FASTER WHEN YOU ADD MORE CATALYST, BUT THIS WILL
EMBRITTLE THE EPOXY RESINS.

(d) Repair Procedure for Erosion

NOTE: Vibration or fretting of two surfaces causes the erosion of the facing area.
To correct the erosion areas, identify and repair them. A usual procedure to
repair the erosion is to use an adhesive bridge between two components. This
will prevent fretting of the surfaces. The adhesive operates as a liquid shim
between the two parts and prevent clearance between them, but it increases
the flammable materials. If this occurs, you must send a report to the Design
Engineering and Flammability Certification for analysis before its implementation.
If you increase the number of fasteners, you can also decrease the erosion
or fretting, but adds substantial weight. These two procedures are out of the
original design scope, and the Design Engineering and Flammability must make
an analysis of them. Regardless, you must identify the source of the erosion
or the problem will continue.

1 Clean the surface with Isopropyl Alcohol or other approved solvent to remove the
contamination. Do not let the solvent dry on the panel. After you use the solvent,
apply a clean, dry shop wipe to remove all contamination.

2 Apply Polyester or Mylar masking tape, if available, to the areas adjacent to the
repair. This will prevent these surfaces from contamination by the repair procedure.
It will also decrease the clean-up time.

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3 To remove other dirt or contamination, use a sanding pad with 320 grit or finer to
make the surface lightly smooth. 3M Scotch-Brite (very fine) is also permitted.

4 Use a Filled Epoxy adhesive such as Cytec Industries Inc. (Solvay Group) L-301 with
milled glass or Cab-O-Sil Fumed Silica on a limited basis in field repairs. These
Epoxy fillers exhibit higher smoke characteristics than Polyesters as well as higher
OSU Heat Release. Use Epoxy Fillers in field repairs only. Apply them to a limit of
no more than 100 in2 (645.16 cm2) to each part. Remove the unwanted adhesive as
shown in the subsequent step.

5 Use an edge tool such as a spatula or razor blade to remove the unwanted adhesive.
Move the tool along the mylar tape. This will remove all unwanted filler higher than
0.002 in (0.00508 cm) thick (approximately the thickness of the tape).

6 It is frequently necessary to increase the speed of cure of a repair to permit you to put
the component back into service on time. If necessary, make the filled area hot with a
heat gun at 140°F - 160°F (60°C - 71°C) to decrease the set time.

7 After the cure of the filler, remove the masking tape.

8 Lightly sand and fair out the edges of the filler and its surrounding panel surface.

9 Refinish the repair if necessary. To paint the panel, refer to paragraph 10.

CAUTION: DO NOT TRY TO INCREASE THE SPEED OF THE MATERIAL CURE WITH THE
AID OF A LARGE QUANTITY OF CATALYST. MANY FILLERS AND ADHESIVES
WILL CURE FASTER WHEN YOU ADD MORE CATALYST, BUT THIS WILL
EMBRITTLE THE EPOXY RESINS.

(e) Repair Procedure for Shallow Scars, Scratches, and Surface Abrasion:

1 Use Isopropyl Alcohol or other approved solvent to remove the contamination. Do

not let the solvent dry on the panel. After you use the solvent, apply a clean, dry
shop wipe to remove all contamination.

2 Apply Polyester or Mylar masking tape, if available, to the areas adjacent to the
repair. This will prevent these surfaces from contamination by the repair procedure.
It will also decrease the clean-up time.

3 To remove other dirt or contamination, use a sanding pad with 320 grit or finer to
make the surface lightly smooth. 3M Scotch-Brite (very fine) is also permitted.

4 Use Polyester Fillers such as Akemi #7 or Adtech MicroFiller #15-3 to fill small
aberrations. Polyester Fillers do not contribute significantly to OSU Heat Release.

NOTE: You can use Epoxy Fillers and Adhesives such as 3M DP110 or DP190 or
DP420 on a limited basis in field repairs. These Epoxy fillers exhibit higher
smoke characteristics than Polyesters as well as higher OSU Heat Release.
Use Epoxy Fillers in Field Repairs only. Apply them to a limit of no more
than 16 in2 (103.2256 cm2) to each part. Remove the unwanted adhesive
as shown in the subsequent step.

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5 To remove the unwanted adhesive, use an edge tool such as a spatula or razor blade.
Move the tool along the mylar tape. This will remove all unwanted filler higher than
0.002 in (0.00508 cm) thick (approximately the thickness of the tape).

6 It is frequently necessary to increase the speed of cure of a repair to permit you to put
the component back into service on time. If necessary, make the filled area hot with
a heat gun (at a temperature of 120°F (49°C) for Akemi or Adtech MicroFiller or at
140°F - 160°F (60°C - 71°C) for epoxy) to decrease the set time.

NOTE: You can add Polyester systems like Adtech MicroFiller #15-3 or Akemi #4
or #7 catalyst at various ratios. Add a 2 in (5.08 cm) wide length from the
catalyst tube to a “golf ball size” portion of part A. Refer to the instructions
printed on the can. The actual ratio is 100 Parts of A to 2 parts of B.

7 After the cure of the filler, remove the masking tape.

8 Lightly sand and fair out the edges of the filler and its surrounding panel surface.

9 Refinish the repair if necessary. To paint the panel, refer to paragraph 10.

(2) Imperfection: Delamination of Face Ply on Honeycomb Panels

(a) Permitted Limits:

1 Decorative surface: Not permitted.

2 Non-Decorative Surface: Not permitted.

(b) Correctable Limits:

1 Decorative or Non-Decorative Surface: Corner delamination less than 2 in (5.08 cm).

Edge delamination of 3 in (7.62 cm) or less in length and 1 in (2.54 cm) in width.

(c) Repair Procedures with a Structural Laminating-Resin:

1 To repair local delamination, use a structural adhesive L-301 A/B or laminating resin
to bond the panel surface to the honeycomb.

2 Apply a masking tape to the area around the delamination.

3 At a minimum, drill two holes into the delaminated area. These holes must be at
the opposite side of the delaminated area. Use the Table 6001 for the selection of
the materials. Obey the instructions for that specific type of material or equivalent
material requirements.

4 Mix the adhesive and fill the void from the bottom. You must fill the local cells with
adhesive. Fill the hole with sufficient adhesive to bond the panel surface to the core.

5 While you fill the delamination, move the applicator around to make sure that the
surface ply is wet-out.

6 Use a clean, shop wipe moist with Isopropyl alcohol or MEK or Acetone to remove
the unwanted adhesive from the surface.

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7 If possible, put a flat plate on the delamination. Apply a Mylar or flashbreaker tape to
the surface of the plate to hold it.

8 Attach the plate in position with clamps and use sufficient pressure to push the ply
down on the composite surface. Hold it until the adhesive cures.

9 Remove the plate. Sand the remaining adhesive from the composite surface.

(d) Repair Procedure with a Laminating Resin:

1 Use one of these laminating resins: Epocast 50A with 976 (100:15) or Epocast 50A
with 9339 (100:15) or Shell 828 with Epikure 3233 (100:10):

– EPON 828 Resin with Mfg. Catalyst (Epikure DETA 3223 or Equivalent) or (Epikure
TETA 3234 or Equivalent)

– Epocast 50A1 with 9816 Catalyst or Epocast 50A1 with 946 Catalyst

– Loctite (Dexter Hysol) ® EA 956 A/B

2 Mix sufficient resin to make the necessary repair. Weigh the material in the specified
ratio and mix them fully.

3 Use an acid brush or nylon brush to apply the resin to the delamination and to the
core. Make sure that the ply is wet-out on the mating surface.

4 Use a teflon or nylon squeegee or a latex gloved finger to push the ply into position.

5 Remove the unwanted resin with a dry, shop wipe or rag.

6 Let the resin cure for 6 hours. To increase the speed of the cure, dry the resin in
the air until it is tack-free. Then increase the temperature to 120°F (49°C) with an
infrared lamp or oven for 5-30 minutes. Increase the temperature to approximately
150°F (66°C) for 2 hours.

NOTE: When you use a two-step cure, this prevents resin from bubbling or frothing.

(e) Repair Procedure with Adhesive Potting Compound:

1 Use 2-part adhesives. These adhesives offer higher strength, but also increase the
weight. Use one of these adhesives: L-301 or L-318 or equivalent.

2 For L-301 Type 4.11, mix (100:50) sufficient adhesive to apply to the damaged
area. Use a brush or spatula to add sufficient adhesive to the related parts. Use
clamps to attach the parts together for good contact if necessary. Let 2-3 hours for
green-strength cure. Then Increase the temperature to 150°F (66°C) for 2 hours
for high strength cure.

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C. Criteria and Repair Procedures for Class 2:

(1) Imperfection: Punctures, Core to skin Separation, and Damaged Honeycomb Core

(a) Permitted Limits:

1 Decorative surface: Not permitted.

2 Non-Decorative Surface: Not permitted.

(b) Correctable Limits:

1 Decorative Surface: For Punctures, correct 0.1875 in (0.4762 cm) or less in diameter.
Correct no more than 1% of the total panel area. The correction must not increase
the panel weight by more than 2%. For Core to Skin Separation, you can correct up
to 10% of panel edge. For Damaged Honeycomb Core, the repair is not permitted.

2 Non-Decorative Surface: For Punctures, correct 0.1875 in (0.4762 cm) or less in

diameter. The correction must not increase the panel weight by more than 2%.
For Core to Skin Separation, see Decorative Surface procedure. For Damaged
Honeycomb Core, no limit, but the correction must not increase the panel weight
by more than 2%.

(2) Repair Procedures:

NOTE: The 16 in2 (103.2256 cm2) area for repair is the limit for an individual repair. The limit
quantity of repairs per galley panel should be 3 and each individual repair should not
extend in any length more than 4 in (10.16 cm) and if more than one repair is done it
should be at least 12 in (30.48 cm) from any adjacent repair. If it is found that more
repairs are required you should seek approval from local authorities.

NOTE: The subsequent procedures apply for damage that extend through Facing Material,
with collateral damage to the core. When you repair non-structural decorative panels,
refer to these procedures, if the damage agrees with the flammability requirements.

NOTE: Advantages: It is not necessary to remove the damaged core. The local compression
is significantly higher because of the solid filler. The local peel strength is dramatically
improved because of the strength of the adhesive.

NOTE: Disadvantages: Weight Increase. More “fuel for fire” increases OSU potential. The
repair is limited in size because of the weight and flammability problems. The damage
cannot be greater than 16 in2 (103.2256 cm2).

CAUTION: PANELS WITH MORE THAN THE MAXIMUM PERMITTED

COMPRESSION-STRESS (FOR A SPECIAL COMPONENT, OR SHARP
CRASH, OR EQUIVALENT TRAUMA), TYPICALLY CAUSE CORE DAMAGE.
THE SUBSEQUENT PROCEDURE INCREASES THE COMPRESSION STRESS
OF A LOCAL AREA SIGNIFICANTLY BECAUSE OF THE WEIGHT INCREASE
AND FLAMMABILITY PROBLEMS. THE REPAIR MUST NOT BE MORE THAN
16 IN2 (103.2256 CM2) OF THE PANEL AREA.

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CAUTION: DO NOT TRY TO INCREASE THE SPEED OF THE MATERIAL CURE WITH
A LARGE QUANTITY OF CATALYST. MANY FILLERS AND ADHESIVES
WILL CURE FASTER WHEN YOU ADD MORE CATALYST, BUT THIS WILL
EMBRITTLE THE EPOXY RESINS.

SANDING OPERATIONS CAUSE SMALL GRANULAR PARTICLES INTO

BREATHING SPACE. GLASS AND CARBON PARTICLES, WHEN BREATHED,
CAN CAUSE CUMULATIVE DAMAGE TO LUNGS AND RESPIRATORY
SYSTEMS. THE GLASS AND PHENOLIC PARTICLES ARE A SOURCE OF
DERMATITIS. WEAR AN APPLICABLE BREATHING PROTECTION SUCH
AS DUST FILTER MASK. USE NECESSARY PRECAUTIONS DURING ALL
OPERATIONS.

(a) Potting Compound or Solid Plug Repair

1 Clean the surface with Isopropyl Alcohol or other approved solvent to remove the
contamination. Do not let the solvent dry on the panel. After you use the solvent,
apply a clean, dry shop wipe to remove all contamination.

2 Apply Polyester or Mylar masking tape, if available, to the areas adjacent to the
repair. This will prevent these surfaces from contamination by the repair procedure.
It will also decrease the clean-up time.

3 To remove other dirt or contamination, use a sanding pad with 320 grit or finer to
make the surface lightly smooth. 3M Scotch-Brite (very fine) is also permitted.

4 You can use Potting Compounds such as L-318 from Cytec Industries Inc. (Solvay
Group) or Epibond 1559-1 A/B from Huntsman to fill small aberrations.

5 To enhance the strength, undercut the core below the upper panel surface and fill it
totally. This will increase the overall strength. See Figure 6004. Make sure that the
undercut is 0.125 in (0.3175 cm) of the cell width.

6 To remove the unwanted adhesive, use an edge tool such as a spatula or razor blade.
Move the tool along the Mylar tape to remove the unwanted filler higher than 0.002 in
(0.00508 cm) thick (approximately the thickness of the tape).

7 Do not use heat to make the cure faster.

8 After the cure of the filler, remove the masking tape.

9 Lightly sand and fair out the edges of the filler and its surrounding panel surface.

10 Refinish the repair if necessary. To paint the panel, refer to paragraph 101.

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(b) Scarf Repair Procedure (Figure 6005)

NOTE: Advantages: It is necessary to remove and replace the damaged core, but this
prevents the weight increase. The local compression is the same as the parent
panel. The local core-peel strength is slightly better because of the strength of
the adhesive. The replacement of the facing increases the total durability.

NOTE: Disadvantages: Higher skill is necessary to remove and replace the core. Time
for the repair is longer. Wet lay-up or adhesive lay-up is messy.

1 Clean the surface with Isopropyl Alcohol or other approved solvent to remove the
contamination. Do not let the solvent dry on the panel. After you use the solvent,
apply a clean, dry shop wipe to remove all contamination.

2 Apply Polyester or Mylar masking tape, if available, to the areas adjacent to the
repair. This will prevent these surfaces from contamination by the repair procedure.
It will also decrease the clean-up time.

3 Trim the damaged area out to an oval or round shape. Rectangular or Square shapes
with rounded corners is permitted.

4 Grind the panel surface at an angle or taper shape. The width of the scarf must be
at a minimum of 100 times the facing thickness (example: 2 ply of 7781 is 0.02 in
(0.0508 cm) thick, the taper must be 2 in (5.08 cm) wide).

5 Use a vacuum or compressed air to remove all loose unwanted material and particles
from the work area.

6 Cut a section of core equal to the size of the repair area.

7 Put the core into the panel to make it flush with the opposite facing.

8 Use Potting Compound to bond the core in position.

9 Replace the Upper Facing with the Wet lay-up.

10 To fair out the surface, refer to paragraph 9.

11 After the cure of the filler, remove the masking tape.

12 Lightly sand to make the edges of the filler and its surrounding panel surface smooth.

13 Refinish the repair if necessary.

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DISTANCE FOR UNDERCUT

0.125 IN (0,3175 CM) MINIMUM (ONE CELL WIDE)
JAGGED EDGE FROM CORE UNDERCUT

Potting Compound or Solid Repair

Figure 6004/GRAPHIC 50-11-05-300-005-A01

Scarf Repair Procedure

Figure 6005/GRAPHIC 50-11-05-300-006-A01

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D. Criteria and Repair Procedure for Class 3:

(1) Imperfection: Damaged Honeycomb Core

(a) Permitted Limits:

1 Decorative surface: Not permitted.

2 Non-Decorative Surface: Not permitted.

(b) Correctable Limits:

1 Decorative surface: Not permitted.

2 Non-Decorative Surface: No limit, but the correction must not increase the panel
weight by more than 2%.

(2) Repair Procedure:

NOTE: For damage that extends fully through the sandwich panel, you can repair it by two
procedures: Scarf-joint procedure which is equivalent to the Class-2 Procedure and
Step-Joint Class-3 Procedure.

CAUTION: SANDING OPERATIONS CAUSE SMALL GRANULAR PARTICLES INTO

BREATHING SPACE. GLASS AND CARBON PARTICLES, WHEN BREATHED,
CAN CAUSE CUMULATIVE DAMAGE TO LUNGS AND RESPIRATORY
SYSTEMS. GLASS AND PHENOLIC PARTICLES ARE A SOURCE OF
DERMATITIS. WEAR AN APPLICABLE BREATHING PROTECTION SUCH AS
A DUST FILTER MASK. USE NECESSARY PRECAUTIONS DURING ALL
OPERATIONS.

(a) Tapered Scarf-Joint Procedure (Figure 6006)

NOTE: Advantages: It is necessary to remove and replace the damaged core, but this
prevents the weight increase. The local compression is the same as the parent
panel. The local core-peel strength is slightly better because of the strength of
the adhesive. The replacement of the facing increases the total durability. For
solid laminates, follow the lay-up procedure.

NOTE: Disadvantages: Higher skill is necessary to remove and replace the core. Time
for the repair is longer. Wet lay-up or adhesive lay-up is messy.

1 Clean the two surfaces with Isopropyl Alcohol or other approved solvent to remove
the contamination. Do not let the solvent dry on the panel. After you use the solvent,
apply a clean, dry shop wipe to remove all contamination.

2 Apply Polyester or Mylar masking Tape, if available, to the areas adjacent to the
repair. This will prevent these surfaces from contamination by the repair procedure.
It will also decrease the clean-up time.

3 Trim the damaged area out to an oval or round shape. Rectangular or Square shapes
with rounded corners is permitted.

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4 Grind the panel surface at an angle or taper shape on one or on the two sides as
practical. The width of the scarf joint must be at a minimum of 100 times the facing
thickness (example: 2 ply of 7781 is 0.02 in (0.0508 cm) thick, the taper must be 2
in (5.08 cm) wide).

5 Use a vacuum or compressed air to remove all loose unwanted material and particles
from the work area.

6 Cut a section of core equal to the size of the repair area. Put a temporary shim or
block on one side of the panel to hold the core and first facing repair. Make a shim
that is flush against the panel. The shim must have a step on the inside because of
the missing skin plies on that side. Cover the shim with teflon tape or equivalent
release material. Use teflon tape to attach the shim to the panel.

7 Replace the upper facing with the wet lay-up. Let the repair cure.

8 Remove the shim from the second facing. Examine the core and make sure that
it is correctly bonded in position by the wet lay-up. Add more potting compound,
if necessary.

9 To fair out the decorative surfaces, refer to paragraph 9.

10 After the cure of the filler, remove the masking tape.

11 Lightly scarf to make the edges of the filler and its surrounding panel surface smooth.

12 Refinish the repair if necessary.

(b) Step-Joint Procedure:

NOTE: Advantages: It is necessary to remove and replace the damaged core, but this
prevents the weight increase. The local compression is the same as the parent
panel. The local core-peel strength is slightly better because of the strength of
the adhesive. The replacement of the facing increases the total durability.

NOTE: Disadvantages: Higher skill is necessary to remove and replace the core. Time
for the repair is longer, as set time for repair. Wet lay-up or adhesive lay-up
is messy.

1 Clean the two surfaces with Isopropyl Alcohol or other approved solvent to remove
the contamination. Do not let the solvent dry on the panel. After you use the solvent,
apply a clean, dry shop wipe to remove all contamination.

2 Find the thickness of each facing and the plies used (P = plies per facing).

3 Multiply (P-1) x 1.5. Use a divider, compass, or rule to make a mark on the panel
away from the damage by the result. Be sure to use this minimum distance. Use the
same dimensions to make the pattern (oval or rectangular with rounded corners).

4 Apply Polyester or Mylar masking Tape, if available, to the areas adjacent to the
repair. This will prevent these surfaces from contamination by the repair procedure.
It will also decrease the clean-up time.

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5 Use a sharp knife or razor to cut the outer ply of the scribe line. Carefully remove
the trimmed ply section.

6 Do the procedure again for three (3) or more plies. Measure 1.5 in (3.81 cm) from this
step and trim the ply that you laid before. The number of steps is equal to the number
of plies minus 1 (3 Plies = 2 steps etc.).

7 For a 2-ply panel, cut a section of core equal to the size of the repair area. The core
must install snugly in position.

8 Put a temporary shim or block on one side of the panel to hold the core and first
facing repair. Make a shim that is flush with the panel. The shim must have a step on
the inside to align with the missing skin plies on that side. Cover the shim with teflon
tape or equivalent release material. Use Teflon tape to attach the shim to the panel.

9 Bond the core in position with wet lay-up resin or adhesive.

10 Replace the upper facing with the Wet lay-up. The dimension of each skin ply must
align correctly into each step. Each skin ply must touch the composite material or
keep a very small clearance. Do not increase the skin ply thickness too much. The
last ply on the top of the repair must extend 0.5 in (1.27 cm) far from the ply below
it. Let the repair cure.

11 Remove the shim from the second facing. Examine the core and make sure that
it is correctly bonded in position by the wet lay-up. Add more potting compound,
if necessary.

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DAMAGE

REMOVE DAMAGE
AND TAPER PANEL

100

ADD NEW PLIES

TAPERED PANEL

Taper Scarf Repair

Figure 6006/GRAPHIC 50-11-05-300-007-A01

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TASK 50-11-05-300-808-A01
8. Fill Edge Holes in Honeycomb Panels

NOTE: Refer to Table 6001 for the recommended materials. If you would like assistance regarding the
applicable materials you can contact Safran Cabin Inc.

NOTE: Use this procedure to fill the holes that you can see in the edges of each panel after the final
assembly.

WARNING: THIS PROCEDURE APPLIES TO HAZARDOUS MATERIALS. FOLLOW THE SHOP

SAFETY PRACTICES CAREFULLY TO PREVENT INJURY.

CAUTION: BE CAREFUL WHEN YOU USE BATCHES THAT ARE OVER THAN 500 TOTAL WEIGHT.
WHEN YOU MIX TOO MUCH OF LARGE BATCHES, THE BATCHES CAN BECOME
EXOTHERMIC (VERY HOT). YOU MUST USE THE STANDARD BATCH MIX SIZES.

A. Remove all unwanted material and particles from the hole with a vacuum or dry compressed air. It is
important to remove all unwanted material and loosened cell walls. Do this to make sure that the
sealant will contact the core material.

B. Use clean, lint-free cloths and MEK solvent to remove all oily dirt and unwanted materials. Let the
solvent dry from the honeycomb panel at least 15 minutes at room temperature.

C. Mix the two-part FR-8136W sealant in the mixture ratio of 100 parts by weight of Part A to 50 parts by
weight of Part B. Mix no more than you can use during the pot life of the compound (45 minutes at
75°F (24°C)). Mix the two components fully but do not let too much air into the mixture.

NOTE: Always follow the instructions given by the manufacturer. It is possible that the mixture ratio
can change after the publication of this manual.

D. Fill the hole in the panel with sealant.

E. Let the sealant cure for 12 hours at 70°F - 90°F (21°C - 32°C), or 3 hours at 120°F - 130°F (49°C
- 54.4°C).

F. Use a file or sand the sealant to make it smooth.

TASK 50-11-05-300-809-A01
9. Fill and Fair out Procedures for Panel

NOTE: Refer to Table 6001 for the recommended materials. If you would like assistance regarding the
applicable materials you can contact Safran Cabin Inc.

A. Surface Preparation

(1) Use clean cloths soaked with Isopropyl Alcohol, MEK, or other permitted solvent to remove the
loose dust or dirt from the panel. Remove all grease, release agent, or other contamination type
from the surface. Do this before you sand the panel surface. This step prevents contamination
into the surface caused by the pressure and abrasion of the sanding operation.

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(2) Be sure that the panel surface is clean and free of dirt or grime. For this, rub the panel surface
with a clean, dry shop wipe. The panel is clean if there is no indication of unwanted materials on
the shop wipe.

CAUTION: DO NOT SAND THE PART AGGRESSIVELY OR TOO MUCH. SCUFF THE SURFACE
RESIN ONLY. DO NOT MAKE THE REINFORCEMENT MATERIAL (GLASS, KEVLAR,
OR GRAPHITE) ROUGH.

(3) Lightly sand the surface with a 100-400 grit sandpaper to break the surface gloss and to remove
release agents or other contamination. Sand all the surface with equal movements.

(4) Do Steps (1) and (2) again until you see no dirt on a new shop wipe. The panel is now prepared
for fairing and filling.

B. Fill and Fair out Procedure

(1) Necessary Materials:

(a) Type 1 Compounds

1 Akemi No. 4

The application of Akemi 4 to fill and fair has no limitation in terms of surface area being
covered providing it is applied as a pore filler which requires that the amount of filler
applied per square foot does not exceed 0.009 lb (4 g). A general rule of the thumb would
be after the filler is applied and sanded the panel shall be visible except for a few dots of
white. If more filler is required refer to the Scratch and dent repair paragraph 10.B.1.C and
use the limitations specified in that repair.

2 Akemi No. 4 is a two component system. Part A is a can of gray putty like paste. Part
B is a small tube of hardener the material is white in color and approximately the
same consistency as toothpaste. These mixing instructions are for small quantities of
material. Should larger batches be called for, scale-up the mix accordingly.

A 2-½ in diameter slug of Akemi No. 4 should be placed on a clean mixing tray,
container, or a cardboard palette (with release paper). Place a 1 in (2.54 cm) length
of Part B straight from the tube onto the palette. Thoroughly fold the hardener into
the “Bondo”. A large flat spatula or putty knife will expedite the mixing process. Use
the blade to “swipe a path” through the putty and lift that section and fold into the
remaining filler on the palette, continue the process until all the Bondo is a uniform
color and consistency.

The filler can be thinned with Acetone. Use a mixture of 2 oz (59.15 ml) of acetone
with the above combination of material. More or less acetone can be added,
depending on the desired consistency. Thinning is desired to fill surface porosity. The
thinned mixture will “level” in the pores, thus reducing the time sanding the part. Dry
the component in an oven for 30 minutes at 120°F (49°C) if the Akemi is cut with
acetone prior to additional work.

(b) Type 2 Compounds Field Repair Fillers:

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1 The DP110 is a two-part epoxy adhesive. Use it only on field and non-structural
repairs of lofted geometry less than 2 in2 (12.9032 cm2) of the part total area. The
DP110 and DP190 come in a two part tube. A baffled mixing-chamber tip is necessary.

2 Epibond 1568 A/B is a self-extinguishing adhesive/filler and you can use it for
localized field repair. Use it only on field and non-structural repairs of lofted geometry
less than 2 in2 (12.9032 cm2) of the part total area. The material comes in Accumix
cartridges with the two components in side by side cylinders. A dispenser “gun” is
used with a baffled tube to mix the materials.

(2) Application of Fairing Compound:

(a) Apply a masking tape to the areas of the panel, as applicable.

(b) Apply the fairing compound to the structure with a spatula. Spread it as thin as possible
along the surface. Use a plastic spreader, a putty knife, or an equivalent tool to apply the
Filler. For thin, uniform and level application, hold the spreader at 90° to the panel surface
or at a slight angle to it. Too much compound application only increases the period of
time necessary to sand the part.

(c) Before sanding, let the fairing compound set in a sufficient time (15 to 20 minutes
minimum). Increase the cure time if compound is spread thicker.

(d) Examine the fairing compound visually to be sure of its correct cure. After this, apply light
pressure with a fingernail on the surface. The cure of the filler will be satisfactory when
you cannot make a mark on it with your nail.

(3) Sand and Contour the Filler:

CAUTION: REMOVE ONLY GRAY/WHITE FILLER. DO NOT GRIND INTO THE

REINFORCEMENT LAYERS OF THE PANEL.

(a) After you apply the filler and let it dry thoroughly, remove the unwanted material with a
200-400 grit sandpaper. Sand the filler with light equal movements, by hand or jitterbug
sander.

NOTE: You can repair the loft or radius on a part with filler compound, but do not apply
the compound too thickly. Only repair the corner or radius if you can see the fabric
in the corner. A part that is correctly laid-up or pressed will always have some
fabric in the corners, but the resin fill can not be sufficient. Do inspections on the
part during all the processing. Only fill or sweep a part that was examined before.

TASK 50-11-05-300-810-A01
10. Paint and Prime the Composite Panels

A. Filler Application

(1) Use a Digital Scale to Mix the Filler

(a) Materials:

1 Mankiewicz #343-55 Filler 15 parts

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2 Mankiewicz #345-15 Hardener 1 Part

3 5-15% Water as a dilution (5% is best to prevent “running” of the paint)

NOTE: For HSH (VB4946) and WLS (V0YY71) Paints, if you would like assistance
you can contact Safran Cabin Inc.

(2) Requirements for Filler Spraying Applicator:

(a) Materials:

1 SATA JET NR95 Gravity Spray Gun

2 Gravity feed cap gun with a 1.5 size head

3 Gun pressure at 50.75 psi (349.92 kPa)

4 Hose outlet pressure at 95 psi (655.03 kPa)

(b) Procedure:

1 First clean the panels with (Greider Co.) G99-S23 white tack cloth to remove all
dust particles.

2 Apply the filler with a spray gun in a criss-cross pattern, approximately 12 in (30.48
cm) away from the panel.

NOTE: Criss-Cross pattern means one pass along the length of panel and one pass
along the width. See Figure 6007.

3 Let the panel dry for 24 hours or until hard. To increase the speed of the cure, dry
the panel in an oven at 130°F (54.4°C).

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Criss-Cross Pattern
Figure 6007/GRAPHIC 50-11-05-300-008-A01

B. Top (Fog) Coat Application

(1) Panel Preparation

(a) Do an inspection on the filler painted panels for “runs” or dust particles. Then sand lightly
as necessary to remove dust particles. Examine the edges for holes or porosity. Fill them
with filler paint materials for small porosity, or with Akemi filler “Bondo” for larger holes.

(2) Top (Fog) Coat Mixing

(a) Materials:

1 Mankiewicz #346-65 Topcoat 6 Parts

2 Mankiewicz #345-19 Hardener 1 Part

3 Water as a dilution

4 A ± 0.0045 lb (2 g) of topcoat or hardener is permitted

NOTE: After you mix the paint, the paint solution has approximately four (4) hours of
workable time under normal environmental conditions.

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(3) Top (Fog) Coat Application

(a) Applicator requirements are as follows:

1 Gravity feed cap gun with a 1.5 size head

2 Gun pressure at 50.75 psi (349.92 kPa)

3 Hose outlet pressure at 95 psi (655.03 kPa)

(b) Apply top (fog) coat in one criss-cross pattern as shown in Figure 6008. Then let it dry for
approximately 20 to 30 minutes or until glossy finish of the painted panel becomes dull.

NOTE: To increase the speed of the drying time, apply ventilation to panels to release
the water particles.

C. Texture Coat Application

(1) Texture Coat Mixing

(a) Materials:

1 Mankiewicz #346-65 Topcoat 6 Parts

2 Mankiewicz #345-19 Hardener 1 Part

3 Water as a dilution

(b) Mix the Texture Coat by weight with a Digital Scale as follows:

1 A ± 0.0045 lb (2 g) of topcoat or hardener is permitted

NOTE: After you mix the paint, the paint solution has approximately four (4) hours of
workable time under normal environmental conditions.

(c) Applicator requirements are as follows:

1 Gravity feed cap gun with a 1.5 size head

2 Gun pressure at 2 psi (13.79 kPa) with H.V.L.P. gun (Non-H.V.L.P. at 20 psi (137.9
kPa))

3 Hose outlet pressure at 95 psi (655.03 kPa)

(2) Application

(a) Apply one criss-cross pattern and one criss coat or 1-1/2 coats to get the texture pattern
as shown in Figure 6008.

(b) Turn down the gun pressure.

(c) Apply a texture coat test on a sample piece for texture effect.

(d) Let dry for 24 hours or until hard. To increase the speed of the drying time, use an oven.

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1- ½+ Criss-Cross Pattern
Figure 6008/GRAPHIC 50-11-05-300-009-A01

D. Damage Repair

(1) For all types of damage, sand down the panel to filler coat. For damages with pits or holes, fill
with Akemi “bondo” and sand the panel to make it smooth.

(2) For Top (Fog) Coat Application and Texture Coat Application, refer to paragraphs 10.B. and
10.C.

(3) To blend newly painted surface with surrounding area, let the paint dry. Rub it with glass cleaner
to remove slightly the sandy surface finish.

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ASSEMBLY

TASK 50-11-05-99F-810-A01
1. General

A. This section contains special instructions and notes needed to prevent damage to components and
possible injury during assembly of the Sidewall Panel Assembly.

NOTE: Assembly sequence can be changed.

B. IPL Figure Item numbers include all configurations (alpha variants) unless otherwise noted.

C. Refer to REPAIR section to install all bonded components, adhesive-backed placards, and potted
inserts. Install the attaching parts given in the IPL to attach all other components.

TASK 50-11-05-400-801-A01
2. Assembly Procedures

CAUTION: THE MONUMENT HAS DECORATIVE SURFACES THAT ARE EASILY DAMAGED.
COVER THE SURFACES AND BE CAREFUL WITH UNIT TO PREVENT DAMAGE.

SUBTASK 50-11-05-440-001-A01
A. Shroud Assembly (IPL Figure 1)

(1) Install the shroud (25, -25A, 25B, -25C, 25D, -25E, 25F, -25G, 25H, -25J, -25K, -25L, 25M,
or -25N).

(2) Refer to REPAIR section to replace the bonded foam seal (22 or -22A).

(3) Refer to REPAIR section to replace the bonded foam seal (20).

(4) Refer to REPAIR section to replace the bonded foam seal (15, -15A, 15B, -15E, -15F, 15G,
or -15H).

(5) Refer to REPAIR section to replace the bonded foam seal (10, -10A, 10B, -10C, 10D, or -10E).

(6) Refer to REPAIR section to replace the bonded foam seal (5, -5A, 5B, or 5C).

SUBTASK 50-11-05-440-002-A01
B. Shroud Assembly (IPL Figure 1A)

(1) Install the shroud (35 or -35A).

(2) Assemble the shroud doubler assembly (10) as follows:

(a) Install the shroud doubler (30).

(b) Install the nutplates (20) with rivets (25).

(3) Install the shroud doubler assembly (10) with rivets (15).

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(4) Install the clip-on nut (5 or -5A).

SUBTASK 50-11-05-440-003-A01
C. Sloping Sidewall Liner Assembly (IPL Figure 1B)

(1) Install the sloping sidewall liner (35, -35A, -35B, -35C, -35D, -35E, -35F, -35G, -35H, -35J, -35K,
-35L, -35M, -35N, -35P, -35Q, -35R, -35S, -35T, -35U, -35V, -35W, -35X, -35Y, or -35Z).

(2) Refer to REPAIR section to replace the bonded placard (30, -30A, -30B, or -30C).

(3) Refer to REPAIR section to replace the bonded placard (25, -25A, -25B, -25C, -25D, -25E,
-25F, -25G, -25H, -25J, -25K, -25L, -25M, -25N, -25P, -25Q, -25R, -25S, -25T, -25U, -25V,
-25W, -25X, -26, -26A, -26B, -26C, -26C, -26D, -26E, -26F, -26G, -26H, -26J, -26K, -26L, -26M,
-26N, -26P, -26Q, or -26R).

(4) Refer to REPAIR section to replace the bonded placard (20B, -20C, -20D, -20E, or -20F).

(5) Refer to REPAIR section to replace the bonded transfer tape (-17 or -17A).

(6) Refer to REPAIR section to replace the bonded doubler (15, -15A, -15B, -15C, -15D, -15E, -15F,
-15G, -15H, -15J, -15K, -15L, -15M, -15N, -15P, -15Q, -15R, or -15S).

(7) Refer to REPAIR section to replace the bonded reinforcement strip (-12).

(8) Refer to REPAIR section to replace the bonded reinforcement strip (10, -10A, or -10B).

(9) Install the clip-on nuts (-5).

SUBTASK 50-11-05-440-004-A01
D. Bulk Sloping Sidewall Panel Assembly (IPL Figure 1C)

(1) Assemble and install the sidewall panel assembly (60, -60B, or -60C) as follows:

(a) Install the sidewall panel (-65, -65B, or -65C).

(2) Refer to REPAIR section to replace the bonded glass cloth tape (-57).

(3) Refer to REPAIR section to replace the bonded placard (55).

(4) Refer to REPAIR section to replace the bonded placard (50).

(5) Refer to REPAIR section to replace the bonded placard (45).

(6) Refer to REPAIR section to replace the bonded foam filler (40).

(7) Refer to REPAIR section to replace the bonded sidewall liner strip (30, -30A, or -30B). Install the
sidewall liner strip (30, -30A, or -30B) with screw (35 or -35A).

(8) Install the net fitting closeout (20) with screws (25).

(9) Install the net fitting closeout (10 or -10A) with screws (15 or -15A).

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(10) Install the clip-on nuts (5 or -5A).

SUBTASK 50-11-05-440-005-A01
E. Bulk Sloper Bracket Assembly (IPL Figure 1D)

(1) Install the bulk sloper bracket (15, -15A, -15B, -15C, -15D, or -15E).

(2) Install the nutplates (5 or -5A) with rivets (10 or -10A).

SUBTASK 50-11-05-440-006-A01
F. Bulk Endwall Assembly (IPL Figure 1E) - Deleted Figure

SUBTASK 50-11-05-440-007-A01
G. Vertical Sidewall Panel Assembly (IPL Figure 1F)

(1) Assemble the decompression blow subassembly (-80) as follows:

(a) Refer to REPAIR section to replace the bonded placard (-85 or -85A).

(b) Install the blow in panel (-90).

(2) Refer to REPAIR section to replace the bonded placard (75 or -75A).

(3) Refer to REPAIR section to replace the bonded placard (70 or -70A).

(4) Refer to REPAIR section to replace the bonded placard (65 or -65A).

(5) Refer to REPAIR section to replace the bonded placard (60 or -60A).

(6) Install the grill (55).

(7) Refer to REPAIR section to replace the bonded vertical sidewall liner (50).

(8) Install the blow in panel (45).

(9) Refer to REPAIR section to replace the bonded transfer tape (-44 or -44A).

(10) Refer to REPAIR section to replace the bonded glass cloth tape (-43A).

(11) Refer to REPAIR section to replace the bonded silicone foam tape (-42A).

(12) Refer to REPAIR section to replace the bonded cover strip (40).

(13) Refer to REPAIR section to replace the bonded cover strip (35).

(14) Refer to REPAIR section to replace the bonded cover strip (30).

(15) Refer to REPAIR section to replace the bonded spacer (-25A).

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(16) Refer to REPAIR section to replace the bonded sidewall extrusion (5). Install the sidewall
extrusion (5) with nuts (10A), washers (15), and screws (20).

SUBTASK 50-11-05-440-008-A01
H. Vertical Sidewall Panel Assembly (IPL Figure 1G)

(1) Refer to REPAIR section to replace the bonded placard (90B or -90C).

(2) Refer to REPAIR section to replace the bonded placard (85C).

(3) Refer to REPAIR section to replace the bonded placard (80E or -80F).

(4) Refer to REPAIR section to replace the bonded placard (75E or -75F).

(5) Refer to REPAIR section to replace the bonded transfer tape (-73 or -73A).

(6) Install the liner (70F).

(7) Refer to REPAIR section to replace the bonded insulation panel (30A).

(8) Install the sidewall extrusion (5E) with nuts (10E), washers (15), and screws (20).

(9) Refer to REPAIR section to replace the bonded silicone foam tape (-3).

SUBTASK 50-11-05-440-009-A01
I. Vertical Sidewall Panel Assembly (IPL Figure 1H)

(1) Install the vertical sidewall liner (125, -125A, -125B, or -125C).

(2) Refer to REPAIR section to replace the bonded transfer tape (-122 or -122A).

(3) Refer to REPAIR section to replace the bonded glass cloth tape (-120A).

(4) Refer to REPAIR section to replace the bonded placard (-115 or -115A).

(5) Refer to REPAIR section to replace the bonded placard (-110).

(6) Refer to REPAIR section to replace the bonded placard (-105, -105A, -105B, or -105C).

(7) Refer to REPAIR section to replace the bonded placard (100 or -100A).

(8) Refer to REPAIR section to replace the bonded placard (95, -95A, -95B, or -95C).

(9) Refer to REPAIR section to replace the bonded placard (90 or -90A).

(10) Refer to REPAIR section to replace the bonded placard (85, -85A, -85B, -85C, -85D, -85E,
-85F, or -85G).

(11) Refer to REPAIR section to replace the bonded silicone foam tape (-80A).

(12) Refer to REPAIR section to replace the bonded doubler strip (75, -75A, -75B, or -75C).

(13) Refer to REPAIR section to replace the bonded doubler strip (70, -70A, -70B, or -70C).

(14) Refer to REPAIR section to replace the bonded doubler strip (65, -65A, -65B, or -65C).

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(15) Install the retainers (-60, -60A, 60B, -60C, or -60D).

(16) Assemble and install the quarter turn fastener assemblies (45 or -45A) as follows:

(a) Install the stud (-55).

(b) Install the sleeve (-50).

(17) Refer to REPAIR section to replace the bonded hook fastener (40).

(18) Install the cargo access panel lanyard (25) with rivet (30) and nylon washers (35).

(19) Refer to REPAIR section to replace the bonded water dam liner (-22).

(20) Refer to REPAIR section to replace the bonded sidewall extrusion (5). Install the sidewall
extrusion (5) with nuts (10), washers (15), and screws (20).

(21) Refer to REPAIR section to replace the bonded silicone foam tape (-3).

SUBTASK 50-11-05-440-010-A01
J. Vertical Sidewall Panel Assembly (IPL Figure 1J)

(1) Install the access panel liner (165, -165A, or -165B).

(2) Refer to REPAIR section to replace the bonded vertical sidewall liner (160).

(3) Refer to REPAIR section to replace the bonded tape (-155A).

(4) Refer to REPAIR section to replace the bonded placard (-150).

(5) Refer to REPAIR section to replace the bonded placard (-145, -145A, -145B, or -145C).

(6) Refer to REPAIR section to replace the bonded placard (140).

(7) Refer to REPAIR section to replace the bonded placard (135).

(8) Refer to REPAIR section to replace the bonded placard (130).

(9) Refer to REPAIR section to replace the bonded placard (125 or -125A).

(10) Refer to REPAIR section to replace the bonded placard (120).

(11) Refer to REPAIR section to replace the bonded placard (115, -115A, -115B, -115C, -115D,
or -115E).

(12) Refer to REPAIR section to replace the bonded placard (110, -110A, -110B, or -110C).

(13) Refer to REPAIR section to replace the bonded placard (105, -105A, -105B, -105C, -105D,
or -105E).

(14) Refer to REPAIR section to replace the bonded silicone foam tape (-100A).

(15) Refer to REPAIR section to replace the bonded doubler strip (-95).

(16) Refer to REPAIR section to replace the bonded doubler strip (-90 or -90A).

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(17) Refer to REPAIR section to replace the bonded doubler strip (85, -85A, or -85B).

(18) Refer to REPAIR section to replace the bonded doubler strip (80 or -80A).

(19) Refer to REPAIR section to replace the bonded doubler strip (75).

(20) Refer to REPAIR section to replace the bonded doubler strip (70, -70A, or -70B).

(21) Refer to REPAIR section to replace the bonded tape (-68 or -68A).

(22) Install the retainers (-65, -65A, -65B, 65C, -65D, or -65E).

(23) Assemble and install the quarter turn fastener assemblies (50, -50A, or -50B) as follows:

(a) Install the stud (-60).

(b) Install the turn sleeve (-55).

(24) Refer to REPAIR section to replace the bonded sidewall extrusion (30, -30A, or -30B). Install
the sidewall extrusion (30, -30A, or -30B) with nuts (35 or -35A), washers (40 or -40A), and
screws (45 or -45A).

(25) Refer to REPAIR section to replace the bonded silicone foam tape (-28).

(26) Refer to REPAIR section to replace the bonded hook fasteners (25 or -25A).

(27) Install the cargo access panel lanyard (10) with rivets (15 or -15A) and washers (20 or -20A).

(28) Install the cargo access panel lanyards (5 or -5A).

SUBTASK 50-11-05-440-011-A01
K. Vertical Sidewall Panel Assembly (IPL Figure 1K)

(1) Assemble the decompression blow subassembly (-90) as follows:

(a) Refer to REPAIR section to replace the bonded placard (-95 or -95A).

(b) Refer to REPAIR section to replace the bonded placard (-100).

(c) Refer to REPAIR section to replace the bonded placard (-105).

(d) Install the blow in panel (-110).

(2) Refer to REPAIR section to replace the bonded placard (85, -85A, or -85B).

(3) Refer to REPAIR section to replace the bonded placard (80, -80A, or -80B).

(4) Refer to REPAIR section to replace the bonded placard (75, -75A, or -75B).

(5) Refer to REPAIR section to replace the bonded placard (70 or -70A).

(6) Refer to REPAIR section to replace the bonded placard (65, -65A, -65B, or -65C).

(7) Refer to REPAIR section to replace the bonded placard (60, -60A, -60B, or -60C).

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(8) Refer to REPAIR section to replace the bonded vertical sidewall liner (55 or -55A).

(9) Install the grill (50 or -50A).

(10) Refer to REPAIR section to replace the bonded vertical sidewall liner (45 or -45A).

(11) Remove the blow in panel (40, -40A, -40B, or -40D).

(12) Refer to REPAIR section to replace the bonded glass cloth tape (-38A).

(13) Refer to REPAIR section to replace the bonded silicone foam tape (-37A).

(14) Refer to REPAIR section to replace the bonded cover strip (35 or -35A).

(15) Refer to REPAIR section to replace the bonded cover strip (30).

(16) Refer to REPAIR section to replace the bonded cover strip (25).

(17) Refer to REPAIR section to replace the bonded transfer tape (-22 or -22A).

(18) Refer to REPAIR section to replace the bonded sidewall extrusion (5 or -5A). Install the sidewall
extrusion (5 or -5A) with nuts (10A), washers (15), and screws (20).

SUBTASK 50-11-05-440-012-A01
L. Vertical Sidewall Panel Assembly (IPL Figure 1L)

(1) Assemble the decompression blow subassembly (-110) as follows:

(a) Refer to REPAIR section to replace the bonded placard (-115 or -115A).

(b) Refer to REPAIR section to replace the bonded placard (-120).

(c) Install the blow in panel (-125).

(2) Assemble the decompression blow subassembly (-95) as follows:

(a) Refer to REPAIR section to replace the bonded placard (-100 or -100A).

(b) Install the blow in panel (-105).

(3) Refer to REPAIR section to replace the bonded placard (90 or -90A).

(4) Refer to REPAIR section to replace the bonded placard (85).

(5) Refer to REPAIR section to replace the bonded placard (80 or -80A).

(6) Refer to REPAIR section to replace the bonded placard (75 or -75A).

(7) Refer to REPAIR section to replace the bonded vertical sidewall liner (70).

(8) Install the blow out panel (65).

(9) Install the blow in panel (60).

(10) Install the blow in panel (55).

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(11) Refer to REPAIR section to replace the bonded glass cloth tape (-53A).

(12) Refer to REPAIR section to replace the bonded silicone foam tape (-52A).

(13) Refer to REPAIR section to replace the bonded transfer tape (-51 or -51A).

(14) Refer to REPAIR section to replace the bonded cover strip (50).

(15) Refer to REPAIR section to replace the bonded cover strip (45).

(16) Refer to REPAIR section to replace the bonded cover strip (40).

(17) Refer to REPAIR section to replace the bonded cover strip (35).

(18) Refer to REPAIR section to replace the bonded cover strip (30).

(19) Refer to REPAIR section to replace the bonded cover strip (25).

(20) Refer to REPAIR section to replace the bonded sidewall extrusion (5). Install the sidewall
extrusion (5) with nuts (10A), washers (15), and screws (20).

SUBTASK 50-11-05-440-013-A01
M. Vertical Sidewall Panel Assembly (IPL Figure 1M)

(1) Refer to REPAIR section to replace the bonded placard (-50 or -50A).

(2) Refer to REPAIR section to replace the bonded placard (45 or -45A).

(3) Refer to REPAIR section to replace the bonded placard (40 or -40A).

(4) Refer to REPAIR section to replace the bonded placard (35, -35A, -35B, or -35C).

(5) Install the vertical sidewall liner (30 or -30A).

(6) Refer to REPAIR section to replace the bonded transfer tape (-27 or -27A).

(7) Refer to REPAIR section to replace the bonded doubler strip (25 or -25A).

(8) Refer to REPAIR section to replace the bonded sidewall extrusion (5 or -5A). Install the sidewall
extrusion (5) with nuts (10A), washers (15), and screws (20).

(9) Refer to REPAIR section to replace the bonded silicone foam tape (-3).

SUBTASK 50-11-05-440-014-A01
N. Vertical Sidewall Panel Assembly (IPL Figure 1N)

(1) Assemble the decompression blow subassembly (-155) as follows:

(a) Refer to REPAIR section to replace the bonded placard (-160).

(b) Refer to REPAIR section to replace the bonded placard (-165 or -165A).

(c) Refer to REPAIR section to replace the bonded placard (-170 or -170A).

(d) Install the blow in panel (-175).

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(2) Install the access panel liner (150).

(3) Install the blow in panel (145).

(4) Install the decompression grill (140).

(5) Refer to REPAIR section to replace the bonded transfer tape (-137A).

(6) Refer to REPAIR section to replace the bonded glass cloth tape (-135A).

(7) Refer to REPAIR section to replace the bonded placard (130).

(8) Refer to REPAIR section to replace the bonded placard (125).

(9) Refer to REPAIR section to replace the bonded placard (120 or -120A).

(10) Refer to REPAIR section to replace the bonded placard (115 or -115A).

(11) Refer to REPAIR section to replace the bonded placard (110 or -110A).

(12) Refer to REPAIR section to replace the bonded placard (105 or -105A).

(13) Refer to REPAIR section to replace the bonded placard (100 or -100A).

(14) Refer to REPAIR section to replace the bonded silicone foam tape (-95A).

(15) Refer to REPAIR section to replace the bonded cover strip (90).

(16) Refer to REPAIR section to replace the bonded cover strip (85).

(17) Refer to REPAIR section to replace the bonded cover strip (80).

(18) Refer to REPAIR section to replace the bonded doubler strip (75).

(19) Refer to REPAIR section to replace the bonded doubler strip (70).

(20) Refer to REPAIR section to replace the bonded doubler strip (65).

(21) Install the retainers (-60 or 60A).

(22) Assemble and install the quarter turn fastener assemblies (45) as follows:

(a) Install the stud (-55).

(b) Install the sleeve (-50).

(23) Refer to REPAIR section to replace the bonded sidewall extrusion (25). Install the sidewall
extrusion (25) with nuts (30), washers (35), and screws (40).

(24) Refer to REPAIR section to replace the bonded hook fasteners (20).

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(25) Install the cargo access panel lanyards (5) with rivets (10) and nylon washers (15).

SUBTASK 50-11-05-440-015-A01
O. Vertical Sidewall Panel Assembly (IPL Figure 1P)

(1) Install the vertical sidewall liner (140).

(2) Install the vertical sidewall liner (135).

(3) Install the vertical sidewall liner (130).

(4) Install the vertical sidewall liner (125).

(5) Install the outboard decompression vent panel (120).

(6) Refer to REPAIR section to replace the bonded glass cloth tape (-115A).

(7) Refer to REPAIR section to replace the bonded placard (110).

(8) Refer to REPAIR section to replace the bonded placard (105 or -105A).

(9) Refer to REPAIR section to replace the bonded placard (100 or -100A).

(10) Refer to REPAIR section to replace the bonded placard (95).

(11) Refer to REPAIR section to replace the bonded placard (90).

(12) Refer to REPAIR section to replace the bonded placard (85 or -85A).

(13) Refer to REPAIR section to replace the bonded silicone foam tape (-80A).

(14) Refer to REPAIR section to replace the bonded doubler strip (75).

(15) Refer to REPAIR section to replace the bonded doubler strip (70).

(16) Refer to REPAIR section to replace the bonded doubler strip (65).

(17) Refer to REPAIR section to replace the bonded transfer tape (-63 or -63A).

(18) Install the retainers (-60 or 60A).

(19) Assemble and install the quarter turn fastener assemblies(45) as follows:

(a) Install the stud (-55).

(b) Install the sleeve (-50).

(20) Refer to REPAIR section to replace the bonded sidewall extrusion (25) .Install the sidewall
extrusion (25) with nuts (30), washers (35), and screws (40).

(21) Refer to REPAIR section to replace the bonded silicone foam tape (-22).

(22) Refer to REPAIR section to replace the bonded hook fastener (20).

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(23) Install the cargo access panel lanyard (5) with rivet (10) and nylon washers (15).

SUBTASK 50-11-05-440-016-A01
P. Vertical Sidewall Panel Assembly (IPL Figure 1Q)

(1) Refer to REPAIR section to replace the bonded transfer tape (-100A or -100B).

(2) Refer to REPAIR section to replace the bonded glass cloth tape (-95A).

(3) Refer to REPAIR section to replace the bonded silicone foam tape (-90A).

(4) Refer to REPAIR section to replace the bonded placard (85).

(5) Refer to REPAIR section to replace the bonded placard (80 or -80A).

(6) Refer to REPAIR section to replace the bonded placard (75 or -75A).

(7) Install the panel grill (70).

(8) Refer to REPAIR section to replace the bonded decompression panel assembly (55). Assemble
the decompression panel assembly (55) as follows:

(a) Refer to REPAIR section to replace the bonded transfer tape (-67 or -67A)

(b) Install the outboard decompression vent panel (65).

(c) Refer to REPAIR section to replace the bonded insulation panel (60).

(9) Refer to REPAIR section to replace the bonded decompression panel assembly (40 or -40A).
Assemble the decompression panel assembly (40 or -40A) as follows:

(a) Refer to REPAIR section to replace the bonded transfer tape (-53 or -53A).

(b) Install the inboard decompression vent panel (50 or -50A).

(c) Refer to REPAIR section to replace the bonded insulation panel (-48).

(d) Refer to REPAIR section to replace the bonded insulation panel (-47 or -47A).

(e) Refer to REPAIR section to replace the bonded insulation panel (-46 or -46A).

(f) Refer to REPAIR section to replace the bonded insulation panel (45).

(10) Refer to REPAIR section to replace the bonded cover strip (35).

(11) Refer to REPAIR section to replace the bonded doubler strip (30).

(12) Refer to REPAIR section to replace the bonded cover strip (25).

(13) Refer to REPAIR section to replace the bonded water dam liner (22).

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(14) Refer to REPAIR section to replace the bonded sidewall extrusion (5). Install the sidewall
extrusion (5) with nuts (10), washers (15), and screws (20).

SUBTASK 50-11-05-440-017-A01
Q. Vertical Sidewall Panel Assembly (IPL Figure 1R)

(1) Refer to REPAIR section to replace the bonded placard (50).

(2) Refer to REPAIR section to replace the bonded placard (45).

(3) Refer to REPAIR section to replace the bonded placard (40 or -40A).

(4) Refer to REPAIR section to replace the bonded transfer tape (-37 or -37A).

(5) Refer to REPAIR section to replace the bonded vertical sidewall liner (35).

(6) Refer to REPAIR section to replace the bonded vertical sidewall liner (30).

(7) Install the outboard decompression vent panel (25).

(8) Refer to REPAIR section to replace the bonded sidewall extrusion (5). Install the sidewall
extrusion (5) with nuts (10A), washers (15), and screws (20).

(9) Refer to REPAIR section to replace the bonded silicone foam tape (-3).

SUBTASK 50-11-05-440-018-A01
R. Vertical Sidewall Panel Assembly (IPL Figure 1S)

(1) Refer to REPAIR section to replace the bonded silicone foam tape (-55A).

(2) Refer to REPAIR section to replace the bonded placard (-50).

(3) Refer to REPAIR section to replace the bonded placard (45, -45A, -45B, -45C, -45D, -45D,
or -45E).

(4) Refer to REPAIR section to replace the bonded placard (40, -40A, -40B, -40C, -40E, -40F,
or -40G).

(5) Remove the vertical sidewall liner (35, -35A, -35B, or -35C).

(6) Refer to REPAIR section to replace the bonded transfer tape (-33, -33A, or -33B).

(7) Refer to REPAIR section to replace the bonded doubler strip (30, -30A, or -30B).

(8) Refer to REPAIR section to replace the bonded water dam liner (25).

(9) Install the sidewall extrusion (5 or -5A) with nuts (10 or -10A), washers (15 or -15A), and screws
(20 or -20A). Refer to REPAIR section to replace the bonded sidewall extrusion (5 or -5A).

SUBTASK 50-11-05-440-019-A01
S. Vertical Sidewall Vent Liner Assembly (IPL Figure 1T)

(1) Install the vertical sidewall liner panel (10, -10A, -10B, -10C, or -10D).

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(2) Refer to REPAIR section to replace the bonded placard (5, -5A, -5B, -5C, -5D, -5E, -5F, -5G,
-5H, -5J, -5K, -5L, -5M, or -5N).

SUBTASK 50-11-05-440-020-A01
T. Vertical Sidewall Panel Assembly (IPL Figure 1U)

(1) Assemble the decompression blow subassembly (-175) as follows:

(a) Refer to REPAIR section to replace the bonded placard (-180).

(b) Refer to REPAIR section to replace the bonded placard (-185 or -185A).

(c) Refer to REPAIR section to replace the bonded placard (-190 or -190A).

(d) Install the blow in panel (-195).

(2) Install the blow in panel (170 or -170A).

(3) Install the vertical decompression grill (165 or -165A).

(4) Refer to REPAIR section to replace the bonded vertical sidewall liner (160 or -160A).

(5) Refer to REPAIR section to replace the bonded vertical sidewall liner (155 or -155A).

(6) Refer to REPAIR section to replace the bonded glass cloth tape (-150A).

(7) Refer to REPAIR section to replace the bonded placard (-145).

(8) Refer to REPAIR section to replace the bonded placard (-140).

(9) Refer to REPAIR section to replace the bonded placard (135).

(10) Refer to REPAIR section to replace the bonded placard (130 or -130A).

(11) Refer to REPAIR section to replace the bonded placard (125 or -125A).

(12) Refer to REPAIR section to replace the bonded placard (120 or -120A).

(13) Refer to REPAIR section to replace the bonded placard (115 or -115A).

(14) Refer to REPAIR section to replace the bonded placard (110 or -110A).

(15) Refer to REPAIR section to replace the bonded placard (105).

(16) Refer to REPAIR section to replace the bonded placard (100, -100A, or -100B).

(17) Refer to REPAIR section to replace the bonded placard (95, -95A, -95B, or -95C).

(18) Refer to REPAIR section to replace the bonded transfer tape (-92 or -92A).

(19) Refer to REPAIR section to replace the bonded silicone foam tape (-90A).

(20) Refer to REPAIR section to replace the bonded cover strip (85 or -85A).

(21) Refer to REPAIR section to replace the bonded cover strip (80 or -80A).

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(22) Refer to REPAIR section to replace the bonded cover strip (75 or -75A).

(23) Refer to REPAIR section to replace the bonded doubler strip (70 or -70A).

(24) Refer to REPAIR section to replace the bonded doubler strip (65, -65A, or -65B).

(25) Install the retainers (-60, -60A, or 60B).

(26) Assemble and install the quarter turn fastener assemblies(45 or -45A) as follows:

(a) Install the stud (-55).

(b) Install the sleeve (-50).

(27) Refer to REPAIR section to replace the bonded sidewall extrusion (25). Install the sidewall
extrusion (25) with nuts (30), washers (35), and screws (40).

(28) Refer to REPAIR section to replace the bonded silicone foam tape (-23).

(29) Refer to REPAIR section to replace the bonded hook fastener (20).

(30) Install the cargo access panel lanyard (5) with rivet (10) and nylon washers (15A).

SUBTASK 50-11-05-440-021-A01
U. Vertical Sidewall Panel Assembly (IPL Figure 1V)

(1) Install the access panel liner (135).

(2) Refer to REPAIR section to replace the bonded vertical sidewall liner (130).

(3) Refer to REPAIR section to replace the bonded vertical sidewall liner (125).

(4) Install the blow out panel (120).

(5) Refer to REPAIR section to replace the bonded transfer tape (-117 or -117A).

(6) Refer to REPAIR section to replace the bonded glass cloth tape (-115A).

(7) Refer to REPAIR section to replace the bonded placard (110).

(8) Refer to REPAIR section to replace the bonded placard (105).

(9) Refer to REPAIR section to replace the bonded placard (100).

(10) Refer to REPAIR section to replace the bonded placard (95).

(11) Refer to REPAIR section to replace the bonded placard (90 or -90A).

(12) Refer to REPAIR section to replace the bonded placard (85 or -85A).

(13) Refer to REPAIR section to replace the bonded silicone foam tape (-80A).

(14) Refer to REPAIR section to replace the bonded doubler strip (75).

(15) Refer to REPAIR section to replace the bonded doubler strip (70).

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(16) Install the retainers (-65 or 65A).

(17) Assemble and install the quarter turn fastener assemblies (50) as follows:

(a) Install the stud (-60).

(b) Install the sleeve (-55).

(18) Refer to REPAIR section to replace the bonded spacer (45).

(19) Refer to REPAIR section to replace the bonded sidewall extrusion (25). Install the sidewall
extrusion (25) with nuts (30), washers (35), and screws (40).

(20) Refer to REPAIR section to replace the bonded silicone foam tape (-22).

(21) Refer to REPAIR section to replace the bonded hook fastener (20).

(22) Install the cargo access panel lanyard (5) with rivet (10) and nylon washers (15).

SUBTASK 50-11-05-440-022-A01
V. Vertical Sidewall Panel Assembly (IPL Figure 1W)

(1) Assemble the decompression blow subassembly (-165) as follows:

(a) Refer to REPAIR section to replace the bonded placard (-170).

(b) Install the blow in panel (-175).

(2) Remove the access panel liner (160).

(3) Remove the inboard decompression vent panel (155).

(4) Remove the decompression grill (150).

(5) Refer to REPAIR section to replace the bonded transfer tape (-147 or -147A).

(6) Refer to REPAIR section to replace the bonded glass cloth tape (-145A).

(7) Refer to REPAIR section to replace the bonded placard (120 or -120A).

(8) Refer to REPAIR section to replace the bonded placard (115).

(9) Refer to REPAIR section to replace the bonded placard (110).

(10) Refer to REPAIR section to replace the bonded placard (105 or -105A).

(11) Refer to REPAIR section to replace the bonded placard (100 or -100B).

(12) Refer to REPAIR section to replace the bonded silicone foam tape (-95A).

(13) Refer to REPAIR section to replace the bonded cover strip (90).

(14) Refer to REPAIR section to replace the bonded cover strip (85).

(15) Refer to REPAIR section to replace the bonded cover strip (80).

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(16) Refer to REPAIR section to replace the bonded doubler strip (75).

(17) Refer to REPAIR section to replace the bonded doubler strip (70).

(18) Refer to REPAIR section to replace the bonded doubler strip (65).

(19) Install the retainers (-60 or 60B).

(20) Assemble and install the quarter turn fastener assemblies (45) as follows:

(a) Install the stud (-55).

(b) Install the sleeve (-50).

(21) Refer to REPAIR section to replace the bonded sidewall extrusion (25). Install the sidewall
extrusion (25) with nuts (30), washers (35), and screws (40).

(22) Refer to REPAIR section to replace the bonded silicone foam tape (-22).

(23) Refer to REPAIR section to replace the bonded hook fastener (20).

(24) Install the cargo access panel lanyard (5) with rivet (10) and nylon washers (15).

SUBTASK 50-11-05-440-023-A01
W. Vertical Sidewall Panel Assembly (IPL Figure 1X)

(1) Assemble the decompression blow subassembly (-170) as follows:

(a) Refer to REPAIR section to replace the bonded placard (-175 or -175A).

(b) Refer to REPAIR section to replace the bonded placard (-180).

(c) Install the blow in panel (-185).

(2) Install the vertical sidewall liner (165).

(3) Install the inboard decompression vent panel (160).

(4) Install the vertical sidewall liner (155).

(5) Install the decompression grill (150).

(6) Refer to REPAIR section to replace the bonded transfer tape (-147 or -147A).

(7) Refer to REPAIR section to replace the bonded glass cloth tape (-145A).

(8) Refer to REPAIR section to replace the bonded placards (140).

(9) Refer to REPAIR section to replace the bonded placards (135).

(10) Refer to REPAIR section to replace the bonded placards (130 or -130A).

(11) Refer to REPAIR section to replace the bonded placards (125).

(12) Refer to REPAIR section to replace the bonded placards (120 or -120A).

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(13) Refer to REPAIR section to replace the bonded placard (115).

(14) Refer to REPAIR section to replace the bonded placards (110).

(15) Refer to REPAIR section to replace the bonded placard (105).

(16) Refer to REPAIR section to replace the bonded placard (100).

(17) Refer to REPAIR section to replace the bonded silicone foam tape (-95A).

(18) Refer to REPAIR section to replace the bonded cover strip (90).

(19) Refer to REPAIR section to replace the bonded cover strip (85).

(20) Refer to REPAIR section to replace the bonded cover strip (80).

(21) Refer to REPAIR section to replace the bonded doubler strip (75).

(22) Refer to REPAIR section to replace the bonded doubler strip (70).

(23) Refer to REPAIR section to replace the bonded doubler strip (65).

(24) Install the retainers (-60 or 60A).

(25) Assemble and install the quarter turn fastener assemblies (45) as follows:

(a) Install the stud (-55).

(b) Install the sleeve (-50).

(26) Refer to REPAIR section to replace the bonded sidewall extrusion (25). Install the sidewall
extrusion (25) with nuts (30), washers (35), and screws (40).

(27) Refer to REPAIR section to replace the bonded silicone foam tape (-22).

(28) Refer to REPAIR section to replace the bonded hook fastener (20).

(29) Install the cargo access panel lanyards (5) with rivets (10) and nylon washers (15A).

SUBTASK 50-11-05-440-024-A01
X. Vertical Sidewall Panel Assembly (IPL Figure 1Y)

(1) Install the vertical sidewall liner (75, -75A, or -75B).

(2) Refer to REPAIR section to replace the bonded transfer tape (-70A).

(3) Refer to REPAIR section to replace the bonded placard (65, -65A, or -65B).

(4) Refer to REPAIR section to replace the bonded placard (60).

(5) Refer to REPAIR section to replace the bonded placard (55).

(6) Refer to REPAIR section to replace the bonded placard (50, -50A, or -50B).

(7) Refer to REPAIR section to replace the bonded silicone foam tape (-45).

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(8) Refer to REPAIR section to replace the bonded doubler strip (40, -40A, or -40B).

(9) Refer to REPAIR section to replace the bonded doubler strip (35 or -35A).

(10) Refer to REPAIR section to replace the bonded doubler strip (30 or -30A).

(11) Refer to REPAIR section to replace the bonded doubler strip (25 or -25A).

(12) Install the retainers (-20, -20A, -20B, or 20C).

(13) Assemble and install the quarter turn fastener assemblies (5, -5A, or -5B) as follows:

(a) Install the stud (-15).

(b) Install the sleeve (-10).

SUBTASK 50-11-05-440-025-A01
Y. Vertical Sidewall Panel Assembly (IPL Figure 1Z)

(1) Install the vertical sidewall liner (65 or -65A).

(2) Refer to REPAIR section to replace the bonded transfer tape (-60A).

(3) Refer to REPAIR section to replace the bonded placard (55).

(4) Refer to REPAIR section to replace the bonded placard (50 or -50A).

(5) Refer to REPAIR section to replace the bonded silicone foam tape (-45).

(6) Refer to REPAIR section to replace the bonded doubler strip (40 or -40A).

(7) Refer to REPAIR section to replace the bonded doubler strip (35 or -35A).

(8) Refer to REPAIR section to replace the bonded doubler strip (30 or -30A).

(9) Refer to REPAIR section to replace the bonded doubler strip (25 or -25A).

(10) Install the retainers (-20, -20A, or 20B).

(11) Assemble and install the quarter turn fastener assemblies (5 or -5A) as follows:

(a) Install the stud (-15).

(b) Install the sleeve (-10).

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SPECIAL TOOLS, FIXTURES, EQUIPMENT, AND CONSUMABLES

TASK 50-11-05-940-801-A01
1. General

The recommended special tools, fixtures, and test equipment for the Sidewall Panel Assembly are given in
Table 9001. The recommended consumables for the Sidewall Panel Assembly are given in Table 9002.

NOTE: Equivalent items can be used.

Special Tools, Fixtures, and Equipment

Table 9001/TABLE 50-11-05-940-005-A01

Part or Specification
Nomenclature Source (CAGE)* Use
Number
Protective eyewear or N/A Commercially Available Cleaning.
safety goggles
Plastic Blade Scraper or N/A Commercially Available Cleaning.
Spatula
Vacuum Model# VK811SIWD / Cleva North America Cleaning / Repair.
125 CFM (or equivalent) (V70A87)
Sealant Gun, Pneumatic Model 250 PRC - Desoto Repair.
International Inc. (PPG
Aerospace) (V5HCF1)
Putty Knife N/A Commercially Available Repair.
Razor Blade N/A Commercially Available Repair.
Pliers or Router N/A Commercially Available Repair.
Heat Gun HL1920E or similar TE Connectivity Corp. Repair.
(V06090)
Pneumatic Wrench N/A Commercially Available Repair.
Soldering Iron N/A Commercially Available Repair.
Pressure Spray Gun #FX tip and needle #765 DeVilbiss Co. (ITW Inc.) Repair.
(JGA-502 Gun) air cap (or equivalent) (V0GAZ6)
Siphon Cup Gun #FX tip and needle #765 DeVilbiss Co. (ITW Inc.) Repair.
(JGA-502 Cup) air cap (or equivalent) (V0GAZ6)
* Refer to the IPL, paragraph 6, for the address.

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Consumables
Table 9002/TABLE 50-11-05-94A-002-A01

Part or Specification
Nomenclature Source (CAGE)* Use
Number
Apron N/A Commercially Available Cleaning.
Cotton Cloths (lint-free) (clean N/A Commercially Available Cleaning.
and dry)
Rubber Gloves or Latex N/A Commercially Available Cleaning.
Soft-bristled brush NSN 0038 Industries For The Blind Cleaning.
and Visually Impaired
Inc. (V9U362)
Solvent, cleaning Adhesive Acetone Commercially Available Cleaning.
removal CAS No. 67-64-1
MEK (Methyl Ethyl Commercially Available
Ketone)
CAS No. 78-93-3
(Fed. MIL Spec.
TT-M-261)
(metal parts only)
BRULIN 815MX Brulin Holding Co. Inc.
(V94058)
CALLA 301-A LEMON Andpak Ema Inc.
(V68491)
General overall surface Mild household detergent Commercially Available Cleaning.
cleaning (including decor)
(Mild Detergents)
BRULIN 815MX Brulin Holding Co. Inc.
(V94058)
CALLA 301-A LEMON Andpak Ema Inc.
(V68491)
Metal cleaning Solvent, Federal Optional Cleaning.
Specification P-D-680,
Type III
MEK (Methyl Ethyl Commercially Available
Ketone)
CAS No. 78-93-3
(Fed. MIL Spec.
TT-M-261)
(metal parts only)
BRULIN 815MX Brulin Holding Co. Inc.
(V94058)
* Refer to the IPL, paragraph 6, for the address.

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Consumables
Table 9002/TABLE 50-11-05-94A-002-A01 (continued)

Part or Specification
Nomenclature Source (CAGE)* Use
Number
Metal cleaning CALLA 301-A LEMON Andpak Ema Inc. Cleaning.
(V68491)
Sodium Bicarbonate Commercially Available
NaHCO3
CAS No. 144-55-8
Metal Preservation, Corrosion VCI-416 Cleaner Cortec Corp. (V44695) Cleaning.
Inhibitors/Cleaners Corrosion Inhibitor
Corwipe 300 Cortec Corp. (V44695)
Sponges (clean and dry) Non-Scratch Scrub 3M Company (V04963) Cleaning.
Sponge (Scotch-Brite)
Spray bottles N/A Commercially Available Cleaning.
Solvents - outside surfaces Isopropyl Alcohol Commercially Available Cleaning.
CAS No. 67-63-0
Acetone Commercially Available
CAS No. 67-64-1
Polyester tapes, used for Flashbreaker™ Polyester Airtech International Repair.
multipurpose lay-up at 400°F Pressure-Sensitive Inc. (Airtech Advanced
(202°C). Silicone or rubber Adhesive and Release Materials Group)
based Tape (V53912)
Polyester tapes, used for Flashbreaker™ Airtech International Repair.
multipurpose lay-up Pressure-Sensitive Inc. (Airtech Advanced
Adhesive Masking and Materials Group)
Release Tape (V53912)
Conformal Coating, Brush Military Spec Commercially Available Repair.
Application MIL-I-46058, Class C or Chase Corp. (V99109)
or Humiseal 1A33
Abrasive-Cloth, Federal Specification Commercially Available Repair.
Aluminum-Oxide, P-C-451
Medium-Grit
Cloth, Milled Glass Fibers MIL-C-9084, Hammer Commercially Available Repair.
Milled 0.03125 in (0.0793
cm) length or less.
Scotch-Brite Pad Aircraft Cleaning Pad 3M Company (V04963) Repair.
Ultra Fine Hand Pad 3M Company (V04963)
7448
* Refer to the IPL, paragraph 6, for the address.

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Consumables
Table 9002/TABLE 50-11-05-94A-002-A01 (continued)

Part or Specification
Nomenclature Source (CAGE)* Use
Number
Sandpaper 100-400 grit Commercially Available Repair.
120-240 grit
180-220 grit
200-400 grit
Sanding Pad 320 grit Commercially Available Repair.
Adhesives: Repair.
Decor Bonding adhesive Scotch-Weld™ #30 3M Company (V04963)
(Formerly Fast-Bond™
#30)
Scotch-Weld™ #30 NF 3M Company (V04963)
(Formerly Fast-Bond™
#30-NF)
Edge Wrap Aerobond 1801 Aerocell Corp. (V1SX35)
Aquabind Alternative Materials
Tech Inc. (Akzo Nobel
Coatings) (V0ZXD0)
Sealant/Adhesive (stainless DEVCON Aluminum ITW Polymers Adhesives
steel) Filled Epoxy NA (V0RZG3)
Per MMM-A-132 Type I
or equivalent
Henkel Loctite EA 9394 Henkel Corp. (V1N6B3)
Adhesive or equivalent
Adhesives Epibond 1210-A (Resin) Huntsman Advanced Repair.
9615-B (Hardener) Materials GmbH
Epibond 1559-1 A/B (V1532N)
Epocast 1618 D/B
Epocast 1628 A/B
L-301 A/B Cytec Industries
Inc. (Solvay Group)
(V0V7G8)
Versilok 506 Accelerator Lord Corp. (Chemical
#4 Products Div.) (V30676)
Scotch-Weld™ #5 3M Company (V04963)
(Formerly Scotch-Grip
#5)
* Refer to the IPL, paragraph 6, for the address.

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Consumables
Table 9002/TABLE 50-11-05-94A-002-A01 (continued)

Part or Specification
Nomenclature Source (CAGE)* Use
Number
Adhesives DP420 3M Company (V04963) Repair.
DP190
EC-3524
Fill and Fair Compounds, Akemi #7 Standard Filler AXSON North America Repair.
Polyester Based Inc. (Sika Advanced
Resins) (V3VPY6)
Akemi #4 Faster Version AXSON North America
Inc. (Sika Advanced
Resins) (V3VPY6)
Micro-Ultra Filler #15-3 Adtech Plastic Systems
Corp. Inc. (V09AU0)
Fire Retardant Reducer Adtech Plastic Systems
#15-3 Corp. Inc. (V09AU0)
Fill and Fair Compounds, Araldite 252, 2-part Paste Huntsman Advanced Repair.
Epoxy Based Adhesive Filler Materials GmbH
(V1532N)
DP110 3M Company (V04963)
Edge Fill L-306 Cytec Industries Repair.
Inc. (Solvay Group)
(V0V7G8)
Magnolia Plastics Magnolia Advanced
128-135 A/B Materials Inc. (V22121)
Potting Compound L-318 Kit Form Cytec Industries Repair.
Inc. (Solvay Group)
(V0V7G8)
Epibond 1559-1 A/B Huntsman Advanced
Epibond 420 or Redux Materials GmbH
420 (V1532N)
Epocast 1618 D/B
Epocast 89670-A/B
1631-A/B
1632-A/B
Magnobond 92-1 A/B Magnolia Advanced
Materials Inc. (V22121)
DP420 3M Company (V04963)
Polystrate #14270 - 5 min ITW Polymers Adhesives
epoxy NA (V0RZG3)
* Refer to the IPL, paragraph 6, for the address.

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Consumables
Table 9002/TABLE 50-11-05-94A-002-A01 (continued)

Part or Specification
Nomenclature Source (CAGE)* Use
Number
Potting Compound EY-3009 A/B or EY-3010 H.B. Fuller North America Repair.
A/B (V26348)
7160 A/B
7176
Aerobond 1507-A/B or Aerocell Corp. (V1SX35)
1508-A/B
Aerofill 1504-A/B
DAPCO 3040-A/B Cytec Industries
Inc.(Solvay Group)
(V0V7G8)
Potting Adhesive, Epoxy L-318 Cytec Industries Repair.
Based Inc.(Solvay Group)
(V0V7G8)
Structural Adhesive, Epoxy L-301 A/B Cytec Industries Repair.
Based Inc.(Solvay Group)
(V0V7G8)
Core Sealer-Edge Seal, L-306 FRHT (Alternate: Cytec Industries Repair.
Epoxy Based Araldite 252 A-B, 2-part Inc.(Solvay Group)
paste or Epocast 1628 (V0V7G8)
A-B from Huntsman)
DAPCO 3008 A/B Cytec Industries
DAPCO 3303 Inc.(Solvay Group)
(V0V7G8)
Magnolia 85-3 A/B Magnolia Advanced
Materials Inc. (V22121)
Laminating Resin Epoxy Epon 828 Resin Epikure Resolution Performance Repair.
3223 DETA Catalyst Products LLC (Hexion
Inc.) (V3FBZ6)
Epocast 50A1 (100 Parts Huntsman Advanced
by weight) Materials GmbH
(V1532N)
9816 Catalyst (15 Parts Huntsman Advanced
by weight) or 946 Catalyst Materials GmbH
(15 Parts by weight) (V1532N)
Hysol ® EA 956 A/B Henkel Corp. (V1N6B3)
* Refer to the IPL, paragraph 6, for the address.

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Consumables
Table 9002/TABLE 50-11-05-94A-002-A01 (continued)

Part or Specification
Nomenclature Source (CAGE)* Use
Number
Sealant, Silicone (white) RTV102 Momentive Performance Repair.
Dow Corning 7130 Materials Inc. (General
GE 160 Electric Co.) (V01139)
GE 5242
Sealant/Adhesive PR 1775/1776 Class A or Courtaulds Aerospace Repair.
B (PPG Aerospace)
(V05027)
P/S 890 Class A or B Sealants and Coatings
Technologies Inc.
(V45DF3)
Metal Surface Protection: VCI-416 Cleaner Cortec Corp. (V44695) Repair.
Metal Preservation, Corrosion Corrosion Inhibitor
Inhibitors/Cleaners
Corwipe 300 Cortec Corp. (V44695)
Organic Coating for Aluminum VCI-386 Topcoat and VCI Products are FDA Repair.
Surfaces VCI-393 / VCI-395 Primer and USDA approved
Alodine 600/1200 Henkel Corp. (V1N6B3)
Organic Coating for Aluminum White 44-W-7 Primer Deft Inc. (PPG
Surfaces A/B* Aerospace) (V33461)
Light Gray 44-W-18 Deft Inc. (PPG
Primer A/B* Aerospace) (V33461)
White 44-W-7 and Deft Inc. (PPG
44-W-18 Aerospace) (V33461)
NOTE: DO NOT HAVE
CHROMATE
Organic Epoxy Mastic M45/M46 Reduce with Benjamin Moore and Co. Repair.
Coating - Topcoat M95 Ltd. (V09585)
M62-01 Epoxy Gloss Certified for Food
Coating Processing and FDA
Approved for Food
Service
Fluid Resistant Primers: KOROPON Courtaulds Aerospace Repair.
515-700 PAINT (PPG Aerospace)
910-704 CATALYST (V05027)
463-12-8 PAINT Dexter Corp. Polymer
CA-116 CATALYST System (V1JB33)
* Refer to the IPL, paragraph 6, for the address.

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Consumables
Table 9002/TABLE 50-11-05-94A-002-A01 (continued)

Part or Specification
Nomenclature Source (CAGE)* Use
Number
Fluid Resistant Primers: 10-P4-7 PAINT Courtaulds Aerospace Repair.
EC-131 CATALYST (PPG Aerospace)
(V05027)
515X391 PAINT Courtaulds Aerospace
910c780 CATALYST (PPG Aerospace)
010x326 THINNER (V05027)
MIL-P-23377 primer Ty C&C VenturesLLC
II ClC MIL-T-81772B (Randolph Products
REDUCER (Green Co.) (V77672)
Primer)
MIL-P-23377 primer Ty C&C VenturesLLC
II ClC MIL-T-81772B (Randolph Products
REDUCER (Yellow Co.) (V77672)
Primer)
Topcoats: #442-3 (GLOSS COLOR) Bostik Inc. (Arkema) Repair.
#X-304 CATALYST (V5W425)
#453-3 (FLAT COLOR) Bostik Inc. (Arkema)
#CA-118 CATALYST (V5W425)
#980- (GLOSS COLOR) WLS Coatings Inc.
#982- (SEMI-GLOSS) (V0YY71)
Sher Will Enamel F63 Sherwin-Williams Co.
or H99 V66V29 catalyst. (V1JRP1)
R7KB29 or R7K84 or
R99KY29 (REDUCER)
(03Y091) Topcoat Deft Inc. (PPG
(03Y091) Catalyst Aerospace) (V33461)
MIL-T-81772 Type I
Reducer
MIL-PRF-85285C, Type I Deft Inc. (PPG
Polyurethane Aerospace) (V33461)
#343-55 (Filler) Mankiewicz Gebr. & Co.
#345-15 (Hardener) (VD2603)
#346-65 (Topcoat)
#345-19 (Hardener)
Acceptable CIC Materials: NYCOTE 7-11 Nycote Laboratories Repair.
Corp. (V05803) or
Chemetall Chemical
Products Inc. (V02CA7)
* Refer to the IPL, paragraph 6, for the address.

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Consumables
Table 9002/TABLE 50-11-05-94A-002-A01 (continued)

Part or Specification
Nomenclature Source (CAGE)* Use
Number
Acceptable CIC Materials: DINITROL / ARDROX AV Chemetall Oakite Inc. Repair.
Series Compounds (V0L040)
DINITROL AV 8
DINITROL AV 15
DINITROL AV 25
DINITROL AV 30
SOCOPAC 65H Socomore (VF6892)
Solvents: Isopropyl Alcohol Commercially Available Repair.
CAS No. 67-63-0
Acetone Commercially Available
CAS No. 67-64-1
MEK (Methyl Ethyl Commercially Available
Ketone)
CAS No. 78-93-3
(Fed. MIL Spec.
TT-M-261)
Ethyl Alcohol (Ethanol) Commercially Available
CAS No. 64-17-5
Thinner Humiseal #33 Chase Corp. (V99109) Repair.
* Refer to the IPL, paragraph 6, for the address.

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ILLUSTRATED PARTS LIST (IPL)

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TASK 50-11-05-99F-010-A01
1. General

This section describes and illustrates all component assemblies, subassemblies, and parts required
for maintenance of the Sidewall Panel assembly.

TASK 50-11-05-99F-025-A01
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).

B. How to Identify a Part

(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.

(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.

TASK 50-11-05-960-001-A01
3. Equipment Designator Index

The Equipment Designator Index is an aid to find the parts in the Detailed 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.

TASK 50-11-05-970-001-A01
4. Numerical Index

The Numerical Index is an aid to find parts in the Detailed 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.

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TASK 50-11-05-99F-026-A01
5. Explanation of Detailed Parts List Entries

The Detailed 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.

A. FIG. ITEM Column

(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.

B. PART NUMBER Column

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

The indenture is included in the NOMECLATURE column and shows how parts are related. A typical
relation is as follows:

End Item or Major Assembly

. Detailed Parts for End Item or Major Assembly
.. Subassemblies
ATTACHING PARTS
.. Attaching Parts for Subassemblies
---*---
... Detail Part for Subassemblies
ATTACHING PARTS
... Attaching Parts for Detail Parts
---*---

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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 Safran Cabin Inc.), 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.

(2) Assemblies, subassemblies, and detail parts subjected to modification, deletion, addition,
or replacement by an issued service bulletin are annotated to indicate both the pre- and
post-service bulletin configurations. The term (PRE SB XXXX) in the NOMENCLATURE
column identifies the original configuration, and the term (ADDED POST SB XXXX) identifies
assemblies and parts after the modification has been completed.

(3) The terms defined below are used when applicable to indicate the interchangeability of parts.

Term Abbreviation Definition

Alternate ALT The listed part is alternate to and
interchangeable with other parts
within the same item number
variant group or other item
numbers if designated.
(Two Way Interchangeable)
Optional OPT The part is fully interchangeable in
form, fit, and function with other
item numbers shown.
(Two Way Interchangeable)
Incorporated By Mistake INC BY MISTAKE The related part was added by
mistake to the IPL, so it is deleted
accordingly.
Superseded By SUPSD BY The part is superseded by and
is one way interchangeable with
the item number identified in the
notation.
(One Way Interchangeable)
Supersedes SUPSDS The part supersedes and is not
interchangeable with the item
number designated in the notation.
(One Way Interchangeable)
Replaced By RPLD BY The part is replaced by and is
interchangeable with the item
number designated in the notation.
(Two Way Interchangeable)
Replaces RPLS The part replaces and is
interchangeable with the item
number designated in the notation.
(Two Way Interchangeable)

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E. EFFECT CODE Column

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.

F. UNITS PER ASSY Column

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.

TASK 50-11-05-980-001-A01
6. Manufacturer's Names and Addresses

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
supplied by Safran Cabin Inc.

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MANUFACTURER’S NAMES AND ADDRESSES

CODE NAME ADDRESS

V04963 3M COMPANY 3M CENTER

SAINT PAUL
MN 55144-1000
PHONE 866-556-5712

V09AU0 ADTECH PLASTIC SYSTEMS CORP. 815 W SHEPHERD ST

INC. CHARLOTTE
MI 48813
PHONE 800-255-9934

V1SX35 AEROCELL CORP. 12806 STATE AVE

MARYSVILLE
WA 98271
PHONE 360-653-2600

V53912 AIRTECH INTERNATIONAL INC. 5700 SKYLAB RD

(AIRTECH ADVANCED MATERIALS HUNTINGTON BEACH
GROUP) CA 92647-2055
PHONE 714-899-8100

V0ZXD0 ALTERNATIVE MATERIALS TECH INC. 311 OTTERSON DR SUITE 60

(AKZO NOBEL COATINGS) CHICO
CA 95928
PHONE 530-894-3585

V68491 ANDPAK EMA INC. 400 JARVIS DR

MORGAN HILL
CA 95037
PHONE 408-782-2500

V3VPY6 AXSON NORTH AMERICA INC. (SIKA 1611 HULTS DR

ADVANCED RESINS) EATON RAPIDS
MI 48827-9500
PHONE 517-663-8191

Page 10007
50-11-05 Oct 09/23
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CODE NAME ADDRESS

V09585 BENJAMIN MOORE AND CO. LTD. 15 LLOYD AVE

TORONTO
CANADA M6N 1G9
PHONE 416-766-1173

V5W425 BOSTIK INC. (ARKEMA) 211 BOSTON ST

MIDDLETON
MA 01949-2128
PHONE 978-777-0100

V94058 BRULIN HOLDING CO. INC. 2920 DR A J BROWN AVE

INDIANAPOLIS
IN 46205-4066
PHONE 800-776-7149

V77672 CC VENTURES LLC (RANDOLPH 33 HAYNES CIRCLE

PRODUCTS CO.) CHICOPEE
MA 01020-3712
PHONE 413-592-4191

V99109 CHASE CORP. 128 1ST ST

PITTSBURGH
PA 15238-3223
PHONE 781-332-0765

V02CA7 CHEMETALL CHEMICAL PRODUCTS 50 VALLEY RD

INC. BERKELEY HEIGHTS
NJ 07922
PHONE 908-665-9466

V0L040 CHEMETALL OAKITE INC. 675 CENTRAL AVE

NEW PROVIDENCE
NJ 07974-1560
PHONE 800-526-4473

50-11-05 Page 10008

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CODE NAME ADDRESS

V70A87 CLEVA NORTH AMERICA 601 REGENT PARK CT

GREENVILLE
SC 29607
PHONE 866-384-8432

V44695 CORTEC CORP. 4119 WHITE BEAR PKWY

SAINT PAUL
MN 55110-7634
PHONE 800-426-7832

V05027 COURTAULDS AEROSPACE (PPG 410 JERSEY AVE

AEROSPACE) GLOUCESTER CITY
NJ 08030-2350
PHONE 856-742-9321

V0V7G8 CYTEC INDUSTRIES INC. (SOLVAY 5 GARRET MOUNTAIN PLZ

GROUP) WEST PATERSON
NJ 07424-3317
PHONE 973-357-3100

V33461 DEFT INC. (PPG AEROSPACE) 17451 VON KARMAN AVE

IRVINE
CA 92614-6205
PHONE 949-476-6723

V0GAZ6 DEVILBISS CO. (ITW INC.) 12878 E FLORENCE

SANTA FE SPRINGS
CA 90670
PHONE 562-463-9559

V1JB33 DEXTER CORP. POLYMER SYSTEM 1 DEXTER DR

SEABROOK
NH 03874
PHONE 603-474-5541

50-11-05 Page 10009

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 COMPONENT MAINTENANCE MANUAL
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CODE NAME ADDRESS

V26348 H.B. FULLER NORTH AMERICA 1200 WILLOW LAKE BLVD

VADNAIS HEIGHTS
MN 55110-5146
PHONE 651-236-5912

V1N6B3 HENKEL CORP. 32100 STEPHENSON HWY

MADISON HEIGHTS
MI 48071-5514
PHONE 248-577-2126

VB4946 HSH AEROSPACE FINISHES NV RESEARCH PARK ZONE 1 DE HAAK 3

ZELLIK
BELGIUM 1731
PHONE +32-2-4811065

V1532N HUNTSMAN ADVANCED MATERIALS WIPPLINGERSTRASSE 24

GMBH WIEN
AUSTRIA 1010
PHONE +49-431-8014320

V9U362 INDUSTRIES FOR THE BLIND AND 445 S CURTIS RD

VISUALLY IMPAIRED INC. WEST ALLIS
WI 53214-1016
PHONE 414-778-3055

V0RZG3 ITW POLYMERS ADHESIVES NA 30 ENDICOTT ST

DANVERS
MA 01923-3712
PHONE 978-646-5853

V30676 LORD CORP. (CHEMICAL PRODUCTS 2455 ROBISON RD W

DIV.) ERIE
PA 16509-4675
PHONE 814-217-6994

50-11-05 Page 10010

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CODE NAME ADDRESS

V22121 MAGNOLIA ADVANCED MATERIALS 4360 NORTHEAST EXPY

INC. ATLANTA
GA 30340-3401
PHONE 770-451-2777

VD2603 MANKIEWICZ GEBR. AND CO. GEORG-WILHELM-ST 189

HAMBURG
GERMANY 21107
PHONE +49-40-751030

V3A054 MCMASTER-CARR SUPPLY CO. 9630 NORWALK BLVD

SANTA FE SPRINGS
CA 90670-2932
PHONE 330-342-6135

V01139 MOMENTIVE PERFORMANCE 260 HUDSON RIVER RD

MATERIALS INC. (GENERAL WATERFORD
ELECTRIC CO.) NY 12188-1910
PHONE 518-233-3241

V05803 NYCOTE LABORATORIES CORP. 12750 RAYMER ST STE 3

NORTH HOLLYWOOD
CA 91605-4228
PHONE 818-764-9498

V5HCF1 PRC - DESOTO INTERNATIONAL INC. 12780 SAN FERNANDO RD

(PPG AEROSPACE) SYLMAR
CA 91342-3728
PHONE 818-741-1556

V3FBZ6 RESOLUTION PERFORMANCE 1600 SMITH ST 24TH FL

PRODUCTS LLC (HEXION INC.) HOUSTON
TX 77002-7496
PHONE 832-366-2385

50-11-05 Page 10011

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CODE NAME ADDRESS

V56135 SAFRAN CABIN INC. 5701 BOLSA AVE

HUNTINGTON BEACH
CA 92647-2063
PHONE 714-934-2287

V12624 SAINT-GOBAIN PERFORMANCE 1 SEALANTS PARK

PLASTICS CORP. GRANVILLE
NY 12832-1652
PHONE 518-642-2200

V45DF3 SEALANTS AND COATINGS 106 INDUSTRIAL WAY

TECHNOLOGIES INC. CHARLESTOWN
IN 47111
PHONE 812-256-3378

V86928 SEASTROM MFG. CO. INC. 456 SEASTROM ST

TWIN FALLS
ID 83301-8526
PHONE 208-737-4300

V1JRP1 SHERWIN-WILLIAMS CO. 2640 MAIN ST

SAN DIEGO
CA 92113-3613
PHONE 216-515-4825

VF6892 SOCOMORE 3707 PAUL DUPLEIX AVE

VANNES
FRANCE 56000
PHONE +33-2-97437690

V06090 TE CONNECTIVITY CORP. 501 OAKSIDE AVE SIDE

REDWOOD CITY
CA 94063-3800
PHONE 800-806-0480

50-11-05 Page 10012

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CODE NAME ADDRESS

V81205 THE BOEING CO. 7755 E MARGINAL WAY S

SEATTLE
WA 98108-4002
PHONE 480-891-1045

V0YY71 WLS COATINGS INC. 13413 S BROADWAY

LOS ANGELES
CA 90061
PHONE 310-538-2155

50-11-05 Page 10013

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50-11-05 Page 10014

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ALPHA/NUMERIC INDEX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

BAC27TCA0001 1B 20B 2
20C 1

BAC27TCA1 1B 20 D
20A D

BAC27TCH0370 2Q 145 D
2S 40 D
2T 185 D
2U 185 D

BAC27TCH0371 1V 90 1
2Q 95 D

BAC27TCH0429 1C 45 1
3C 50 D

BAC27WCH101 2C 225 D
3G 185 D

BAC27WCH102 1N 100 1
2H 120 D

BAC27WCH105 1N 105 1
2H 100 D

BAC27WCH106 2K 110 D

BAC27WCH117 1J 105 1
2D 165 D

BAC27WCH118 1K 80 1
1N 110 1
110B D
165 1
2E 135 D
2F 105 D

BAC27WCH122 2C 130 D
3G 100 D

BAC27WCH197 1J 105A 1

50-11-05 Page 10015

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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

BAC27WCH201 1G 80E 1
2 70 D
3 40 D
3A 45 D

BAC27WCH202 1G 80C D

BAC27WCH209 1G 90A D
1J 105B 1
1M 50 1
2N 100 D
2P 45 D

BAC27WCH210 1F 65 1
65B D
85 1
1H 105 1
2C 210 D
2Q 120 D

BAC27WCH211 1U 115 1
2C 120 D
3G 115 D

BAC27WCH212 1K 65 1
1N 115 1
115B D
170 1
2E 130 D
2F 70 D

BAC27WCH213 1J 145 1
1K 65A 1
65D D
95 1
2G 35 D
2H 90 D

BAC27WCH214 1J 145A 1
1L 115 1
80 1
80B D
2J 65 D
2K 215 D

BAC27WCH215 2N 65 D
2P 35 D

50-11-05 Page 10016

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

BAC27WCH216 2Q 85 D

BAC27WCH219 1F 70 1
1G 80A D
1S 45B 1
2C 145 D
2R 125 D

BAC27WCH220 2P 40 D

BAC27WCH221 1U 125 1
2C 160 D
3G 205 D

BAC27WCH222 2N 95 D

BAC27WCH224 1K 85 1
2G 45 D

BAC27WCH225 1L 100 1
90 1
90B D
2J 155 D

BAC27WCH226 2M 135 D

BAC27WCH227 2L 85 D

BAC27WCH228 1U 100 1
100C D
190 1
2C 235 D
3G 170 D

BAC27WCH235 2N 105 D

BAC27WCH238 2P 55 D

BAC27WCH240 1F 75 1
2C 150 D

BAC27WCH242 2Z 105 D

BAC27WCH243 1J 110 1
2D 145 D

BAC27WCH245 1K 75 1
2G 50 D

50-11-05 Page 10017

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

BAC27WCH246 2J 160 D

BAC27WCH249 1P 105 1
2S 165 D

BAC27WCH250 2Y 105 D

BAC27WCH251 3 45 D

BAC27WCH256 3A 50 D

BAC27WCH258 2T 160 D
2U 160 D

BAC27WCH264 2Y 95 D

BAC27WCH265 2T 70 D
2U 70 D

BAC27WCH267 2V 45 D

BAC27WCH269 1W 100A D
3F 125 D

50-11-05 Page 10018

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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

BAC27WCH269-152 1B 25N 1
25P 1
25Q 1
25T 1
25U 1
25W 1
1H 85C 1
1R 40 1
1S 40 1
1X 130 1
130B D
175 1
2 65A D
2T 165 D
190 D
75 D
2U 165 D
190 D
75 D
2V 50 D
75 D
2X 60 D
3A 140 D
200 D
55 D
3B 105 D
125 D

BAC27WCH270 1G 75D D
2A 180 D
2S 125 D
150 D
170 D
45 D
2W 130 D
50 D
70 D
3D 80 D
3E 145 D

50-11-05 Page 10019

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

BAC27WCH270-151 1G 75E 1
1P 85 1
1Q 46 1
75 1
75B D
1S 40A 1
1U 95A 1
1W 100 1
2Y 110 D
190 D
45 D
2Z 85 D

BAC27WCH276 1G 75A D
75B D
2F 115 D
80 D
2H 105 D
130 D
2K 115 D
235 D
2M 155 D
2P 60 D
2Q 100 D
125 D
150 D
2R 105 D
130 D

BAC27WCH276-122 1B 25E 1
25F 1
25G 1
25H 1
25R 1
25S 1
1H 85A 1
1J 115A 1
115B 1
1M 35 1
1N 120 1
1S 40B 1
1T 5B 1
5C 1
5D 1
1V 85 1
2 65 D

50-11-05 Page 10020

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

BAC27WCH277 1G 75 D
2C 115 D
115A D
155 D
155A D
220 D
220A D
2D 150 D
180 D
2E 115 D
145 D
2G 60 D
2J 140 D
165 D
85 D
2L 120 D
70 D
95 D
2N 80 D
3G 165 D
200 D
95 D

BAC27WCH277-121 1B 25 1
25A 1
25B 1
25C 1
25D 1
1F 60 1
1H 85 1
85B 1
1J 115 1
1K 60 1
60A 1
1L 75 1
1M 35A 1
1T 5 1
5A 1
1U 95 1

BAC27WCH282 1G 75C D

BAC27WCH282-162 1Y 50 1
1Z 50 1

BAC27WCH328 2R 100 D

50-11-05 Page 10021

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

BAC27WCH344 2E 140 D

BAC27WCH351 1P 100 1
1X 120 1
2S 115 D
2T 140 D
2U 140 D

BAC27WCH352 1H 105A 1
1S 45A 1
2V 35 D

BAC27WCH353 1G 90B 1
1W 125 D
3 135 D
3A 130 D
3F 130 D

BAC27WCH355 1W 105 1

BAC27WCH357 2S 140 D
2T 145 D
2U 145 D

BAC27WCH363 1G 80D D
1W 130 D
2Z 160 D
3A 185 D
3D 95 D
3F 115 D

BAC27WCH366 1G 90 D
2Y 175 D
3D 65 D

BAC27WCH369 1Q 47 1
80 1
80B D
2 55A D
3 100 D
3A 40 D

BAC27WCH371 2V 70 D

BAC27WCH375 2W 115 D
2X 35 D

50-11-05 Page 10022

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 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

BAC27WCH382 2X 45 D

BAC27WCH385 2W 40 D

BAC27WCH391 2W 45 D

BAC27WCH479 3 110 D

BAC27WCH496 2C 110 D

BAC27WCH510 2F 110 D

BAC27WCH715 1U 130 1
130B D
185 1
2A 225 D
2C 230 D
2Z 75 D
3E 130 D
3G 175 D

BAC27WEC163 1H 100 1
1W 120 1
2C 105 D

BAC27WEC165 1U 110 1
2A 175 D
2C 105A D
3E 140 D
3G 110 D

BACI12AG3UCM3 1E 125 D
245 D

BACI12AH5U1255 1E 240 D
240A D

BACN10JB3CM 1A 20 2
1D 5 5
5A 7

50-11-05 Page 10023

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

BACN10YR3CD 1F 10 D
1G 10 D
10A D
10B D
10C D
10D D
1K 10 D
1L 10 D
1M 10 D
1R 10 D

BACN10YR3CM 1E 10 D
1F 10A 8
1G 10E 4
1H 10 4
1J 35 9
35A 10
1K 10A 10
1L 10A 9
1M 10A 5
1N 30 10
1P 30 10
1Q 10 7
1R 10A 6
1S 10 3
10A 4
1U 30 9
1V 30 8
1W 30 6
30A D
1X 30 10
2 10 D
30 D
2A 10 D
3D 10 D
3E 10 D
3F 10 D

BACN11AL1CM 1A 5 2
5A 3
1B 5 4
1C 5 3
5A 4
2B 5 D
2C 10 D
5 D

50-11-05 Page 10024

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

2D 10 D
5 D
2E 10 D
5 D
2F 25 D
5 D
2G 10 D
5 D
2H 10 D
5 D
2J 10 D
5 D
2K 10 D
5 D
2L 10 D
5 D
2M 10 D
5 D
2N 10 D
5 D
2P 10 D
5 D
2Q 10 D
5 D
2R 10 D
5 D
2S 10 D
5 D
2T 20 D
5 D
2U 20 D
5 D
2V 20 D
5 D
2W 10 D
5 D
2X 10 D
5 D
2Y 20 D
5 D
2Z 20 D
5 D
3 20 D
5 D
3A 20 D
5 D

50-11-05 Page 10025

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

3B 10 D
5 D
3C 15 D
3G 10 D
25 D

BACP18BE4N0437U 1E 85 D

BACP18BE4N0750U 1E 25 D

BACR12AG5C 1E 205 D
205A D

BACS12ER3K6 1E 190 D
200 D

BACS12FA3K4 1C 15 4
15A 6
25 4
35 1
35A 2
1E 160 D
55 D
65 D
3C 25 D
35 D
45 D

BACS12FA3K5 1E 120 D
170 D
180 D
80 D

BACS12FA3K8 1F 20 8
1G 20 4
20A D
20B D
20C D
20D D
1H 20 4
1J 45 9
45A 10
1K 20 10
1L 20 9
1M 20 5
1N 40 10
1P 40 10

50-11-05 Page 10026

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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

1Q 20 7
1R 20 6
1S 20 3
20A 4
1U 40 9
1V 40 8
1W 40 6
40A D
1X 40 10
2 20 D
40 D
2A 20 D
2C 15 D
2D 15 D
2E 15 D
2F 10 D
2G 15 D
2H 15 D
2J 15 D
2K 15 D
2L 15 D
2M 15 D
2N 15 D
2P 15 D
2Q 15 D
2R 15 D
2S 15 D
2T 10 D
2U 10 D
2V 10 D
2W 15 D
2X 15 D
2Y 10 D
2Z 10 D
3 10 D
3A 10 D
3B 15 D
3D 20 D
3E 20 D
3F 20 D
3G 15 D

BACS12FA3K9 1E 15 D

BACS21AP6620RPS 1E 210 D
210A D

50-11-05 Page 10027

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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

BACW10P304L 2C 20 D
2D 20 D
2E 20 D
2F 15 D
2G 20 D
2H 20 D
2J 20 D
2K 20 D
2L 20 D
2M 20 D
2N 20 D
2P 20 D
2Q 20 D
2R 20 D
2S 20 D
2T 15 D
2U 15 D
2V 15 D
2W 20 D
2X 20 D
2Y 15 D
2Z 15 D
3 15 D
3A 15 D
3B 20 D
3G 20 D

BMS1-68 1E 225 D
2 80 D

BMS8-283 1E 230 D

BMS8-371 1 20 AR

C411026-010 1E 45 D

C411026-019 1E 90 D

C411026-021 1E 95 D

C411026-027 1E 50 D

C411026-028 1E 60 D

C411026-510 1E 5 D

C411026-511 1E 75 D

50-11-05 Page 10028

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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C411051-059 1 25 1

C411051-060 1 25A 1

C411051-061 1 25B 1

C411051-062 1 25C 1

C411051-063 1 25D 1

C411051-065 1 25E 1

C411051-071 1A 35 1

C411051-073 1A 35A 1

C411051-075 1A 30 1

C411051-085 1 15B 1

C411051-087 1 15D D

C411051-088 1 15C D

C411051-159 1 1 RF

C411051-160 1 1A RF

C411051-161 1 1B RF

C411051-162 1 1C RF

C411051-163 1 1D RF

C411051-165 1 1E RF

C411051-171 1A 1 RF

C411051-173 1A 1A RF

C411051-501 1A 10 1

C411051-67 1B 10B 1

C411051-87 1 15H 1

C411051-88 1 15G 1

C411051-89 1 10 1

50-11-05 Page 10029

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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C411051-90 1 10A 1

C411051-91 1 15 1

C411051-92 1 15A 1

C411051-93 1 5 1

C411051-94 1 5A 1

C411151-001 1B 35 1

C411151-003 1B 35A 1

C411151-005 1B 35B 1

C411151-007 1B 35C 1

C411151-009 1B 35D 1

C411151-013 1B 35F 1

C411151-015 1B 35G 1

C411151-017 1B 35H 1

C411151-031 1B 35L 1

C411151-033 1B 35M 1

C411151-043 1B 35R 1

C411151-045 1B 35S 1

C411151-051 1B 10 1
10A 2
2B 10 D

C411151-059 1C 65 1

C411151-073 1C 40 1

C411151-077 1C 10 1
3C 20 D

C411151-079 1C 20 1
3C 30 D

50-11-05 Page 10030

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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C411151-081 1C 40A D
3C 5 D

C411151-101 1B 1 RF

C411151-103 1B 1A RF

C411151-105 1B 1B RF

C411151-107 1B 1C RF

C411151-109 1B 1D RF

C411151-113 1B 1F RF

C411151-115 1B 1G RF

C411151-117 1B 1H RF

C411151-129 1B 1K RF

C411151-131 1B 1L RF

C411151-133 1B 1M RF

C411151-135 1B 1N RF

C411151-139 1B 1Q RF

C411151-143 1B 1R RF

C411151-145 1B 1S RF

C411151-147 1B 1T RF

C411151-149 1B 1U RF

C411151-153 1B 1V RF

C411151-155 1B 1W RF

C411151-159 1C 1 RF

C411151-173 1C 1A D

C411151-175 2B 1 D

C411151-177 3C 1 D

C411151-179 1B 1X RF

50-11-05 Page 10031

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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C411151-183 1B 1Y RF

C411151-29 1B 35K 1

C411151-35 1B 35N 1

C411151-39 1B 35Q 1

C411151-47 1B 35T 1

C411151-49 1B 35U 1

C411151-53 1B 35V 1

C411151-55 1B 35W 1

C411151-559 1C 60 1

C411151-573 1C 60A D

C411151-575 1C 3 D

C411151-577 3C 70 D

C411151-579 3C 10 D

C411151-73 1C 65A D

C411151-75 2B 25 D

C411151-79 1B 35X 1

C411151-83 1B 35Y 1

C411152-001 1B 15 1

C411152-003 1B 15A 1

C411152-005 1B 15B 1

C411152-007 1B 15C 1

C411152-009 1B 15D 1

C411152-011 1B 15E 1

C411152-013 1B 15F 1

C411152-015 1B 15G 1

50-11-05 Page 10032

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C411152-017 1B 15H 1

C411152-061 1D 15 1

C411152-063 1D 15A 1

C411152-065 1D 15B 1

C411152-067 1D 15C 1

C411152-069 1D 15D 1

C411152-071 1D 15E 1

C411152-075 1C 30 1
3C 40 D

C411152-161 1D 1 RF

C411152-163 1D 1A RF

C411152-165 1D 1B RF

C411152-167 1D 1C RF

C411152-169 1D 1D RF

C411152-171 1D 1E RF

C411152-23 1B 15J 1

C411152-25 1B 15K 1

C411152-27 1B 15L 1

C411152-29 1B 15M 1

C411152-31 1B 15N 1

C411152-33 1B 15P 1

C411152-35 1B 15Q 1

C411152-37 1B 15R 1
2B 15 D

C411152-39 1B 15S 1

C411162-11 1B 35E 1

50-11-05 Page 10033

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C411162-111 1B 1E RF

C411162-127 1B 1J RF

C411162-137 1B 1P RF

C411162-27 1B 35J 1

C411162-37 1B 35P 1

C411301-005 1E 35 D

C411302-007 1E 40 D

C412301-027 1E 250A D

C412301-029 1E 250 D

C412301-035 1E 165 D

C412301-037 1E 175 D

C412301-041 1E 185 D

C412301-043 1E 195 D

C412301-045 1E 140 D

C412301-047 1E 100 D

C412301-049 1E 250B D

C412301-051 1E 250C D

C412301-109 1E 1 D

C412301-111 1E 1A D

C412301-115 1E 1B D

C412301-117 1E 1C D

C412301-509 1E 235 D

C412301-511 1E 235A D

C412301-515 1E 70 D

C412301-517 1E 235B D

50-11-05 Page 10034

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C412301-519 1E 235C D

C412404-007 1Y 75 1

C412404-009 1Z 65 1

C412404-011 1G 70G D

C412404-17 1S 35C 1

C412405-045 1G 30 D

C412405-057 1Q 45 1

C412405-059 1Q 60 1

C412405-061 1G 30A 1

C412406-003 1G 5B D
1H 5 1
1S 5A 1
2 25 D

C412406-005 1G 5D D
1J 30 1
1U 25 1
2A 5 D
3D 5 D
3E 5 D

C412406-011 1K 5 1

C412406-012 1N 25 1

C412406-013 1K 5A 1

C412406-014 1J 30A 1

C412406-015 1J 30B 1
1L 5 1

C412406-019 1G 5A D
1S 5 1

C412406-021 1G 5C D
2 5 D

C412406-025 1R 5 1
1W 25 1

50-11-05 Page 10035

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C412406-027 1G 5E 1
2 25A D

C412406-029 1Q 5 1

C412406-030 1W 25A D
3F 5 D

C412406-041 1P 25 1

C412406-042 1X 25 1

C412406-043 1F 5 1

C412406-044 1V 25 1

C412406-045 1G 5 D
1M 5A 1

C412406-046 1M 5 1

C412407-036 1W 70A D
3F 45 D

C412407-038 1W 75A D
3F 55 D

C412407-040 1H 70C 1

C412407-042 1X 65 1

C412407-044 1X 75 1

C412407-055 1M 25 1

C412407-076 1W 85A D
3F 70 D

C412407-096 1F 40 1

C412409-101 1F 1 RF

C412409-111 1K 1 RF

C412409-113 1K 1A RF

C412409-115 1L 1 RF

50-11-05 Page 10036

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C412409-117 1G 1 D
1M 1A RF

C412409-118 1M 1 RF

C412409-121 1G 1A D
1S 1C RF

C412409-123 1G 1B D

C412409-137 1G 1C D

C412409-139 1Q 1 RF

C412409-143 1R 1 RF

C412409-147 1S 1 RF

C412409-149 2 1B D

C412409-159 1S 1B RF

C412409-161 1G 1D RF

C412409-167 1G 1E D

C412409-173 1S 1D RF

C412410-001 1F 55 1

C412410-003 1H 125 1

C412410-004 1H 125A 1

C412410-005 1U 155 1

C412410-007 1U 160 1
2A 110 D
3E 150 D

C412410-009 1J 160 1

C412410-011 1J 165 1

C412410-013 1H 125B 1

C412410-015 1K 45 1

C412410-017 1K 45A 1

50-11-05 Page 10037

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C412410-019 1L 70 1

C412410-021 1G 70 D
1M 30A 1

C412410-022 1M 30 1

C412410-023 1V 125 1

C412410-025 1V 135 1

C412410-027 1V 130 1

C412410-029 1G 70A D
1S 35B 1

C412410-031 1G 70B D
2 85 D

C412410-033 1N 140 1

C412410-035 1N 150 1

C412410-037 1J 165A 1

C412410-039 1J 165B 1

C412410-041 1P 135 1

C412410-043 1P 130 1

C412410-045 1P 125 1

C412410-047 1W 160 1

C412410-049 1W 150 1

C412410-051 1U 160A 1
2A 200 D
3E 155 D

C412410-053 1U 165A 1
2A 260 D
3E 175 D

C412410-055 1G 70C D
3D 120 D

C412410-057 1Q 70 1

50-11-05 Page 10038

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C412410-059 1X 155 1

C412410-061 1X 165 1

C412410-063 1X 150 1

C412410-065 1R 30 1

C412410-067 1H 125C 1

C412410-069 1S 35 1

C412410-071 2 85A D

C412410-073 1W 160A D
3F 145 D

C412410-075 1W 150A D
3F 150 D

C412410-079 1T 1E RF

C412410-081 1T 1F RF

C412410-083 1K 55 1

C412410-085 1T 1G RF

C412410-087 1K 55A 1

C412410-089 1T 1H RF

C412410-095 1G 70D D
3D 110 D

C412410-097 1G 70E D
3D 115 D

C412410-099 1G 70F 1

C412411-003 1V 120 1

C412411-005 1L 65 1

C412411-007 1F 45 1

C412411-009 1K 40 1
40D 1

50-11-05 Page 10039

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C412411-011 1K 40A 1

C412411-013 1L 55 1

C412411-015 1L 60 1

C412411-019 1N 145 1

C412411-023 1Q 65 1

C412411-025 1Q 50 1

C412411-027 1W 155 1

C412411-029 1P 120 1

C412411-035 1W 155A D

C412411-037 1R 25 1

C412411-039 1X 160 1

C412411-043 1G 60 D

C412411-045 1G 65 D

C412411-047 1U 170A 1
2A 265 D

C412411-051 1U 170 1

C412411-503 1Q 40 1

C412411-505 1Q 55 1

C412413-001 1U 70 1
2A 75 D
3E 90 D

C412413-002 1J 70 1

C412413-004 1H 65B 1

C412413-005 1V 70 1

C412413-006 1J 70B 1

C412413-007 1J 85B 1

50-11-05 Page 10040

Oct 09/23
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C412413-008 1J 70A 1

C412413-009 1N 65 1

C412413-010 1J 85A 1

C412413-011 1N 70 1

C412413-013 1H 65 1

C412413-014 1H 65A 1

C412413-015 1J 75 1

C412413-016 1J 80 1

C412413-017 1H 75B 1

C412413-018 1H 70B 1

C412413-019 1J 80A 1
90A 1

C412413-020 1J 90 1
1N 75 1

C412413-021 1J 95 1

C412413-022 1H 70A 1

C412413-023 1H 75A 1
1U 65 2
2A 70 D
3E 85 D

C412413-024 1V 75 2

C412413-025 1U 75 1

C412413-026 1U 80 1

C412413-027 1U 70A 1
2A 170 D
3E 105 D

C412413-028 1U 65B 1
2A 160 D
3E 95 D

50-11-05 Page 10041

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C412413-029 1U 65A 1
2A 165 D
3E 100 D

C412413-030 1W 65 1

C412413-031 1W 70 1

C412413-032 1W 75 1

C412413-033 1P 65 1

C412413-034 1P 70 1

C412413-035 1P 75 1

C412413-037 1W 65A D
3F 50 D

C412413-041 1H 65C 1

C412413-043 1X 70 1

C412413-045 1U 75A 1
2A 205 D
3E 160 D

C412413-046 1U 80A 1
2A 210 D
3E 165 D

C412413-048 1N 80 1

C412413-049 1H 75C 1

C412413-055 1G 25 D
1M 25A 1

50-11-05 Page 10042

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C412413-056 1H 25 1
1J 5 1
5A 2
1N 5 2
1P 5 1
1U 5 1
1W 5 1
1X 5 2
2A 120 D
30 D
3E 25 D
45 D
3F 95 D

C412413-057 1J 10 1
1V 5 1

50-11-05 Page 10043

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C412413-058 1H 40 1
1J 25 2
25A 3
1N 20 2
1P 20 1
1U 20 1
1V 20 1
1W 20 1
1X 20 2
2A 135 D
45 D
2C 70 D
2D 70 D
90 D
2E 70 D
2H 70 D
2K 165 D
185 D
70 D
2M 70 D
90 D
2Q 70 D
2R 70 D
2S 100 D
2T 135 D
2U 135 D
2Y 170 D
3A 125 D
3B 90 D
3E 40 D
60 D
3F 110 D
3G 90 D

C412413-059 1F 30 1

C412413-060 1F 35 1

C412413-061 1K 25 1
1L 30 1

C412413-062 1K 30 1
1L 25 1

C412413-063 1K 35 1

C412413-064 1K 35A 1

50-11-05 Page 10044

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C412413-065 1L 35 1

C412413-066 1Q 25 1

C412413-067 1Q 30 1

C412413-068 1Q 35 1

C412413-071 1N 85 1

C412413-072 1N 90 1

C412413-073 1L 40 1

C412413-074 1L 45 1

C412413-075 1L 50 1

C412413-077 1W 80A D
3F 60 D

C412413-078 1X 80 1

C412413-079 1X 85 1

C412413-081 1G 35 D
1S 30A 1

C412413-082 1G 40 D
3D 25 D
40 D

C412413-083 1G 25A D
2 50 D

C412413-084 1G 45 D
3D 30 D
45 D

C412413-085 1S 30 1

C412413-086 1G 50 D
3D 50 D

C412413-087 2 50A D

C412413-088 1G 55 D
3D 35 D

50-11-05 Page 10045

Oct 09/23
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C412413-089 1U 85 1

C412413-090 1U 85A 1
2A 215 D
3E 170 D

C412413-094 1W 80 1
1X 90 1

C412413-095 1W 90A D
3F 65 D

C412413-096 1W 85 1

C412413-097 1W 90 1

C412413-098 1H 75 1

C412413-099 1H 70 1

C412414-001 1F 50 1

C412414-003 1J 85 1

C412414-005 1U 165 1

C412414-007 1U 155A 1

C412414-015 1K 50 1

C412414-017 1K 50A 1

C412414-020 1Y 35 1

C412414-021 1Y 40 1

C412414-022 1Y 25 1

C412414-023 1Y 30 1

C412414-024 1Z 25 1

C412414-025 1Z 30 1

C412414-026 1Z 35 1

C412414-027 1Z 40 1

C412414-041 1P 140 1

50-11-05 Page 10046

Oct 09/23
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C412414-049 1S 35A 1

C412414-065 1R 35 1

C412414-70 1S 30B 1

C412416-103 1H 1 RF

C412416-104 1H 1A RF

C412416-105 1U 1 RF

C412416-107 1J 1 RF

C412416-109 1H 1B RF

C412416-119 1V 1 RF

C412416-125 1N 1 RF

C412416-127 1J 1A RF

C412416-129 1J 1B RF

C412416-131 1P 1 RF

C412416-133 1W 1 RF

C412416-135 1U 1A RF

C412416-141 1X 1 RF

C412416-145 1H 1C RF

C412416-151 1W 1A D

C412416-163 1Y 1 RF

C412416-165 1Z 1 RF

C412416-167 2A 1 D

C412417-123 2 1 D

C412417-139 1Q 1A RF

C412417-145 1H 1D RF

C412417-147 1S 1A RF

50-11-05 Page 10047

Oct 09/23
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C412417-149 2 1A D

C412418-101 1F 1A RF

C412418-103 1U 1B RF

C412418-105 1K 1B RF

C412418-107 1K 1C RF

C412418-109 1L 1A RF

C412418-111 1N 1A RF

C412418-113 1W 1B RF

C412418-115 3E 1 D

C412418-117 3D 1 D

C412418-119 1Q 1B RF

C412418-121 1X 1A RF

C412418-123 3F 1 D

C412419-11 1K 110 1
40C D

C412419-13 1L 105 1
55A D

C412419-15 1L 125 1
60A D

C412419-19 1N 145A D
175 1

C412419-25 1Q 50A 1

C412419-27 1W 155B D
175 1

C412419-35 3F 140 D

C412419-39 1X 160A D
185 1

C412419-43 3D 105 D

50-11-05 Page 10048

Oct 09/23
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C412419-45 3D 100 D

C412419-47 3E 195 D

C412419-503 1Q 40A 1

C412419-507 1F 80 1

C412419-51 1U 170B D
195 1

C412419-511 1K 90 1

C412419-513 1L 95 1

C412419-515 1L 110 1

C412419-519 1N 155 1

C412419-527 1W 165 1

C412419-539 1X 170 1

C412419-551 1U 175 1

C412419-7 1F 45A D
90 1

C412419-9 1K 40B 1

C412901-003 1H 60 30
60A 31
60D 30
1J 65 26
65A 22
65B 41
1N 60 36
1P 60 30
1U 60 31
60A 32
1V 65 24
1W 60 29
60A D
1X 60 35
1Y 20 31
1Z 20 29
2A 155 D
65 D

50-11-05 Page 10049

Oct 09/23
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C412901-5 1H 60B 30
60C 31
1J 65C 26
65D 22
65E 41
1N 60A 36
1P 60A 30
1U 60B 31
1V 65A 24
1W 60B 29
1X 60A 35
1Y 20A 32
20B 33
20C 31
1Z 20A 30
20B 29
2C 50 D
50A D
2D 50 D
2E 50 D
2H 50 D
2K 145 D
50 D
2M 50 D
2Q 50 D
2R 50 D
2S 80 D
2T 105 D
2U 105 D
2Y 140 D
3A 90 D
3B 55 D
3E 80 D
3F 40 D
3G 50 D

C414051-1 1 25F 1

C414051-101 1 1F RF

C414051-102 1 1G RF

C414051-2 1 25G 1

C414052-1 1 22 1

C414052-2 1 22A 1

50-11-05 Page 10050

Oct 09/23
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C414151-123 1C 1B RF

C414151-23 1C 65B 1

C414151-523 1C 60B 1

C414153-1 1C 30A 1

C414153-3 1C 10A 1

C414401-143 1Y 1C RF

C414408-101 1T 1J RF

C414408-105 1T 1K RF

C414408-107 1T 1L RF

C414408-109 1T 1M RF

C419051-1 1 25H 1

C419051-101 1 1H RF

C419051-102 1 1J RF

C419051-103 1 1K RF

C419051-104 1 1L RF

C419051-105 1 1M RF

C419051-106 1 1N RF

C419051-2 1 25J 1

C419051-3 1 25K 1

C419051-4 1 25L 1

C419051-5 1 25M 1

C419051-6 1 25N 1

C419052-1 1 10B 1

C419052-11 1 5B 1

C419052-15 1 5C 1

50-11-05 Page 10051

Oct 09/23
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C419052-2 1 10C 1

C419052-3 1 15E 1

C419052-4 1 15F 1

C419052-5 1 10D 1

C419052-6 1 10E 1

C419151-143 1C 1C RF

C419151-155 1B 1Z RF

C419151-43 1C 65C 1

C419151-543 1C 60C 1

C419151-55 1B 35Z 1

C419153-1 1B 12 1

C419153-3 1C 30B 1

C419401-101 2C 1 D

C419401-103 2C 1A D

C419401-105 2D 1 D

C419401-107 2E 1 D

C419401-109 2G 1 D

C419401-111 2J 1 D

C419401-113 2L 1 D

C419401-115 2N 1 D

C419401-117 2Q 1 D

C419401-119 2R 1 D

C419401-121 2F 1 D

C419401-123 2H 1 D

C419401-125 2K 1 D

50-11-05 Page 10052

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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C419401-127 2M 1 D

C419401-129 2P 1 D

C419401-131 2S 1 D

C419401-135 2W 1 D

C419401-137 2Y 1 D

C419401-139 2Z 1 D

C419401-141 3 1 D

C419401-143 2T 1 D
2U 1 D

C419401-145 2V 1 D

C419401-147 2X 1 D

C419401-149 3B 1 D

C419401-151 3A 1 D

C419401-153 1Y 1A RF

C419401-155 1G 1F D

C419401-157 1Z 1A RF

C419401-159 1Y 1B RF

C419401-171 1Y 1D RF

C419402-1 2C 25 D

C419402-10 2H 25 D

C419402-11 2J 25 D

C419402-12 2K 25 D

C419402-13 2L 25 D

C419402-14 2M 25 D

C419402-15 2N 25 D

C419402-16 2P 25 D

50-11-05 Page 10053

Oct 09/23
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C419402-17 2Q 25 D

C419402-19 2R 25 D

C419402-21 2F 30 D

C419402-23 2S 25 D

C419402-24 2T 25 D
2U 25 D

C419402-26 2V 25 D

C419402-27 2W 25 D

C419402-29 3 30 D

C419402-3 2D 25 D
2Z 25 D

C419402-31 2X 25 D

C419402-33 3B 30 D

C419402-35 3A 30 D

C419402-41 2C 25A D
2Y 25 D
3G 5 D

C419402-7 2E 25 D

C419402-9 2G 25 D

C419403-1 2C 165 D

C419403-11 2J 170 D

C419403-13 2L 125 D

C419403-15 2N 115 D

C419403-17 2Q 155 D

C419403-19 2R 135 D

C419403-21 2F 120 D

C419403-23 2H 135 D

50-11-05 Page 10054

Oct 09/23
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C419403-25 2P 65 D

C419403-27 2S 50 D

C419403-29 2S 175 D

C419403-3 2C 165A D
3G 210 D

C419403-33 2W 55 D

C419403-35 2W 75 D

C419403-37 2Y 50 D

C419403-39 2Z 115 D

C419403-41 3 70 D

C419403-43 2T 195 D
2U 195 D

C419403-45 2V 55 D

C419403-47 2X 65 D

C419403-49 3B 135 D

C419403-5 2D 185 D

C419403-501 2C 140 D

C419403-503 2C 140A D
3G 195 D

C419403-505 2D 160 D

C419403-507 2E 125 D

C419403-509 2G 30 D

C419403-51 3A 65 D

C419403-511 2J 150 D

C419403-513 2L 105 D

C419403-515 2N 90 D

50-11-05 Page 10055

Oct 09/23
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C419403-517 2Q 135 D

C419403-519 2R 115 D

C419403-521 2F 90 D

C419403-523 2H 115 D

C419403-525 2P 30 D

C419403-527 2S 30 D

C419403-529 2S 160 D

C419403-53 1G 70H D

C419403-533 2W 30 D

C419403-535 2W 60 D

C419403-537 2Y 30 D

C419403-539 2Z 95 D

C419403-541 3 35 D

C419403-543 2T 175 D
2U 175 D

C419403-545 2V 30 D

C419403-547 2X 30 D

C419403-549 3B 115 D

C419403-551 3A 35 D

C419403-7 2E 150 D

C419403-9 2G 65 D

C419404-1 2C 135 D

C419404-11 2R 110 D

C419404-13 2H 110 D

C419404-15 2K 120 D

C419404-17 2K 240 D

50-11-05 Page 10056

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C419404-19 2M 160 D

C419404-21 2S 130 D

C419404-29 2T 170 D
2U 170 D

C419404-3 2C 135A D
2Y 195 D
3G 120 D

C419404-31 3B 110 D

C419404-33 3A 145 D

C419404-35 1Y 75A 1

C419404-37 1Z 65A 1

C419404-39 1Y 75B 1

C419404-5 2D 155 D

C419404-501 2C 30 D

C419404-503 2C 30A D
3G 30 D

C419404-505 2D 30 D

C419404-507 2E 30 D

C419404-509 2Q 30 D

C419404-511 2R 30 D

C419404-513 2H 30 D

C419404-515 2K 30 D

C419404-517 2K 125 D

C419404-519 2M 30 D

C419404-521 2S 60 D

C419404-527 2Y 120 D

50-11-05 Page 10057

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C419404-529 2T 85 D
2U 85 D

C419404-531 3B 35 D

C419404-533 3A 70 D

C419404-7 2E 120 D

C419404-9 2Q 105 D

C419405-1 2C 200 D

C419405-11 2N 55 D
2W 105 D

C419405-13 2Q 130 D

C419405-15 2F 60 D

C419405-17 2V 80 D

C419405-19 2S 155 D

C419405-27 2Z 150 D

C419405-3 2C 200A D
2Y 85 D
2Z 60 D
3G 155 D

C419405-31 3 165 D

C419405-37 3A 175 D

C419405-5 2J 125 D

C419405-501 2C 175 D

C419405-503 2C 175A D
2Y 60 D
2Z 35 D
3G 130 D

C419405-505 2J 100 D

C419405-507 2J 35 D
2T 35 D
2U 35 D

50-11-05 Page 10058

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C419405-509 2L 40 D

C419405-511 2N 35 D
2W 85 D

C419405-513 2Q 115 D

C419405-515 2F 40 D

C419405-517 2V 65 D

C419405-519 2S 135 D

C419405-527 2Z 125 D

C419405-531 3 130 D

C419405-537 3A 155 D

C419405-7 2J 55 D
2T 55 D
2U 55 D

C419405-9 2L 75 D

C419406-1 2C 240 D

C419406-11 2N 85 D
2W 135 D

C419406-13 2Q 110 D

C419406-15 2F 85 D

C419406-17 2L 35 D
2V 60 D

C419406-19 2S 55 D

C419406-27 2Z 175 D

C419406-29 3 90 D

C419406-3 2C 240A D
2Y 115 D
2Z 90 D

C419406-31 3 125 D

50-11-05 Page 10059

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C419406-37 3A 205 D

C419406-5 2J 145 D

C419406-501 2C 205 D

C419406-503 2C 205A D

C419406-505 2J 130 D

C419406-507 2J 60 D

C419406-509 2L 80 D

C419406-511 2N 60 D

C419406-515 2F 65 D

C419406-521 2W 110 D

C419406-523 2Y 90 D

C419406-525 2Z 65 D

C419406-527 2Z 155 D

C419406-529 3 80 D

C419406-531 3 95 D

C419406-533 2T 60 D
2U 60 D

C419406-537 3A 180 D

C419406-7 2J 90 D
2T 80 D
2U 80 D

C419406-9 2L 100 D

C419407-1 2C 185 D

C419407-10 2R 85 D

50-11-05 Page 10060

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C419407-11 2C 85A D
90 D
2D 105 D
2E 85 D
2R 75 D
2Y 145 D
3G 55 D

C419407-13 2C 185A D
2Y 70 D
2Z 135 D
45 D
3G 135 D

C419407-14 2C 190A D
2Y 75 D
2Z 140 D
50 D
3G 140 D

C419407-15 2C 195A D
2N 50 D
2W 100 D
2Y 80 D
2Z 55 D
3G 145 D

C419407-17 2C 95A D
2D 110 D
2M 110 D
2Y 150 D
3G 60 D

C419407-19 2D 115 D

C419407-21 2D 125 D

C419407-23 2E 95 D

50-11-05 Page 10061

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C419407-25 2F 50 D
2J 115 D
45 D
2K 90 D
2M 130 D
2N 45 D
2T 40 D
2U 40 D
2W 95 D

C419407-26 2F 45 D
2J 110 D
40 D
2N 40 D
2T 45 D
2U 45 D
2W 90 D

C419407-27 2J 120 D

C419407-29 2J 50 D
2T 50 D
2U 50 D

C419407-3 2C 195 D

C419407-31 2L 55 D

C419407-32 2L 50 D

C419407-33 2L 60 D

C419407-35 2D 120 D
2M 120 D
2Q 80 D

C419407-37 2Q 75 D

C419407-39 2R 120 D

C419407-40 2F 95 D

C419407-41 2F 55 D

50-11-05 Page 10062

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C419407-43 2E 90 D
2H 75 D
2K 190 D
85 D
2M 105 D
2S 105 D
2T 110 D
2U 110 D
3B 60 D

C419407-45 2H 80 D

C419407-47 2K 95 D

C419407-49 2K 205 D

C419407-5 2C 190 D

C419407-51 2K 200 D
2M 115 D

C419407-53 2K 195 D

C419407-55 2M 125 D

C419407-57 2S 110 D

C419407-61 2Z 145 D

C419407-63 3 150 D

C419407-65 3 160 D

C419407-67 3 155 D

C419407-69 2T 115 D
2U 115 D

C419407-7 2C 85 D
2R 80 D

C419407-71 3B 70 D

C419407-73 3B 65 D

C419407-75 3B 130 D

C419407-77 3A 60 D

50-11-05 Page 10063

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C419407-79 3A 95 D

C419407-81 3A 105 D

C419407-83 3A 100 D

C419407-85 3A 165 D

C419407-87 3A 170 D

C419407-89 3A 160 D

C419407-9 2C 95 D

C419407-91 1Y 40A 1

C419407-93 1Y 30A 1

C419407-95 1Y 25A 1

C419407-97 1Y 35A 1

C419407-99 1Z 30A 1

C419408-1 1T 10 1

C419408-101 1T 1 RF

C419408-103 1T 1A RF

C419408-105 1T 1B RF

C419408-107 1T 1C RF

C419408-109 1T 1D RF

C419408-11 1Y 40B 1

C419408-3 1T 10A 1

C419408-5 1T 10B 1

C419408-7 1T 10C 1

C419408-9 1T 10D 1

C419409-1 1Z 25A 1

C419409-3 1Z 35A 1

50-11-05 Page 10064

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C419409-5 1Z 40A 1

C419409-501 2C 170 D

C419409-503 2C 170A D

C419409-505 2J 95 D

C419409-507 2J 30 D

C419409-509 2L 30 D

C419409-511 2N 30 D

C419409-515 2F 35 D

C419409-521 2W 80 D

C419409-523 2Y 55 D

C419409-525 2Z 30 D

C419409-527 2Z 120 D

C419409-531 3 75 D

C419409-533 2T 30 D
2U 30 D

C419409-537 3A 150 D

C419409-7 2K 210 D

C419410-101 2C 1B D

C419410-103 3G 1 D

C419410-111 2J 1A D

C419410-113 2L 1A D

C419410-115 2N 1A D

C419410-121 2F 1A D

C419410-135 2W 1A D

C419410-137 2Y 1A D

C419410-139 2Z 1A D

50-11-05 Page 10065

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C419410-141 3 1A D

C419410-143 2T 1A D
2U 1A D

C419410-151 3A 1A D

C419412-1 3 60 D

C419412-3 3 85 D

C419412-5 3 120 D

C419413-1 2C 55 D
2D 75 D
2E 55 D
2H 55 D
2K 170 D
55 D
2M 75 D
2R 55 D
2S 85 D
2T 120 D
2U 120 D
2Y 155 D
3A 110 D
3B 75 D
3G 75 D

C419413-3 2D 55 D
2K 150 D
2M 55 D
2Q 55 D

C419414-3 3 25 D

C419414-5 3B 25 D

C419414-501 2F 20 D

C419414-7 3A 25 D

C419415-501 2C 170B D

C419415-503 3G 125 D

C419415-505 2J 95A D

50-11-05 Page 10066

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C419415-507 2J 30A D

C419415-509 2L 30A D

C419415-511 2N 30A D

C419415-515 2F 35A D

C419415-521 2W 80A D

C419415-523 2Y 55A D

C419415-525 2Z 30A D

C419415-527 2Z 120A D

C419415-531 3 75A D

C419415-533 2T 30A D
2U 30A D

C419415-537 3A 150A D

C419416-1 2C 240B D

C419416-11 2N 85A D
2W 135A D

C419416-15 2F 85A D

C419416-27 2Z 175A D

C419416-3 2Y 115A D
2Z 90A D
3G 190 D

C419416-31 3 125A D

C419416-37 3A 205A D

C419416-5 2J 145A D

C419416-501 2C 205B D

C419416-503 3G 160 D

C419416-505 2J 130A D

C419416-507 2J 60A D

50-11-05 Page 10067

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

C419416-509 2L 80A D

C419416-511 2N 60A D

C419416-515 2F 65A D

C419416-521 2W 110A D

C419416-523 2Y 90A D

C419416-525 2Z 65A D

C419416-527 2Z 155A D

C419416-531 3 95A D

C419416-533 2T 60A D
2U 60A D

C419416-537 3A 180A D

C419416-7 2J 90A D
2T 80A D
2U 80A D

C419416-9 2L 100A D

C512416-535 2A 115 D

C512416-567 2A 25 D

CDM200-03 1Q 100 D
2A 105 D

50-11-05 Page 10068

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

CDM200-05 1E 135 D
1F 43 D
1H 120 D
1J 155 D
1K 38 D
1L 53 D
1N 135 D
1P 115 D
1Q 95 D
1U 150 D
1V 115 D
1W 145 D
1X 145 D
1Y 70 D
1Z 60 D
2A 100 D
190 D
250 D
2C 180 D
80X D
2D 100 D
2E 80 D
2J 105 D
2K 80 D
2L 45 D
2M 100 D
2Y 65 D
2Z 130 D
40 D
3 145 D
55 D
3C 65 D
3D 60 D
3E 185 D
3F 80 D
3G 150 D
70 D

CDPL1361-1 1J 105C 1

CDPL1361-2 1K 80B 1
1N 110A 1
165A 1

CDPL1361-3 1J 105D 1

50-11-05 Page 10069

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

CDPL1361-4 1G 80F 1

CDPL1362-1 1J 110C 1

CDPL1362-2 1K 75B 1

CDPL1362-4 1P 105A 1

CDPL1362-9 1N 105A 1

CDPL1364-1 1F 65A 1
85A 1
1H 105B 1

CDPL1364-2 1U 115A 1

CDPL1364-3 1K 65B 1
1N 115A 1
170A 1

CDPL1364-4 1J 145B 1
1K 65C 1
95A 1

CDPL1364-5 1J 145C 1
1L 115A 1
80A 1

CDPL1364-7 1P 100A 1
1X 120A 1

CDPL1364-8 1H 105C 1
1S 45D 1

CDPL1364-9 1G 90C 1

CDPL1365-10 1U 110A 1

CDPL1365-2 1F 70A 1
1S 45C 1
45E 1

CDPL1365-4 1U 125A 1

CDPL1365-6 1Q 47A 1
80A 1

50-11-05 Page 10070

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

CDPL1365-8 1B 20D 1
20E 2
20F 1

CDPL1365-9 1H 100A 1
1W 120A 1

CDPL1366-1 1N 100A 1

CDPL1366-2 1K 85B 1

CDPL1366-3 1L 100A 1
90A 1

CDPL1366-6 1W 105A 1

CDPL1366-9 1J 105E 1
1M 50A 1

CDPL1367-3 1F 75A 1

CDPL1367-6 1U 100B 1
190A 1

CDPL1367-7 1V 90A 1

CDPL1379-1 1B 26 1

CDPL1379-10 1H 85F 1

CDPL1379-11 1K 60B 1

CDPL1379-12 1K 60C 1

CDPL1379-13 1T 5H 1
5J 1

CDPL1379-14 1L 75A 1

CDPL1379-15 1M 35C 1

CDPL1379-2 1F 60A 1

CDPL1379-22 1T 5K 1

CDPL1379-27 1T 5E 1

CDPL1379-3 1B 26A 1

50-11-05 Page 10071

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

CDPL1379-4 1H 85D 1

CDPL1379-5 1B 26B 1

CDPL1379-6 1U 95B 1

CDPL1379-7 1B 26C 1

CDPL1379-8 1J 115C 1

CDPL1379-9 1B 26D 1

CDPL1380-1 1P 85A 1

CDPL1380-2 1W 100B 1

CDPL1380-3 1S 40F 1

CDPL1380-4 1U 95C 1

CDPL1380-6 1G 75F 1

CDPL1380-7 1Q 46A 1
75A 1

CDPL1381-1 1B 26E 1

CDPL1381-10 1B 26G 1

CDPL1381-12 1B 26H 1

CDPL1381-14 1N 120A 1

CDPL1381-15 1J 115D 1

CDPL1381-16 1J 115E 1

CDPL1381-17 1M 35B 1

CDPL1381-18 1T 5M 1

CDPL1381-2 1V 85A 1

CDPL1381-20 1T 5F 1
5N 1

CDPL1381-24 1T 5G 1

CDPL1381-3 1T 5L 1

50-11-05 Page 10072

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

CDPL1381-4 1B 26M 1

CDPL1381-5 1H 85E 1

CDPL1381-6 1B 26N 1

CDPL1381-7 1S 40C 1
40G 1

CDPL1381-8 1B 26F 1

CDPL1382-1 1B 26J 1

CDPL1382-11 1B 26R 1

CDPL1382-2 1X 130A 1
175A 1

CDPL1382-3 1B 26K 1

CDPL1382-4 1R 40A 1

CDPL1382-5 1B 26P 1

CDPL1382-6 1H 85G 1

CDPL1382-7 1B 26Q 1

CDPL1382-8 1S 40E 1

CDPL1382-9 1B 26L 1

CDPL1383-3 1Y 50A 1
50B 1

CDPL1383-5 1Z 50A 1

CDPL1385-3 1U 130A 1
185A 1

CDPL767-1 1G 80 D
1M 45A 1

CDPL767-11 1H 95 1

CDPL767-13 1U 105 1

CDPL767-15 1K 70 1

50-11-05 Page 10073

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

CDPL767-17 1H 95B 1
2E 110 D

CDPL767-21 1L 120 1
85 1
85A D
2L 110 D

CDPL767-23 1G 85 D
1M 40A 1
2L 65 D

CDPL767-25 1J 120 1
1K 85A 1
2D 175 D
2L 115 D

CDPL767-27 1J 125 1

CDPL767-29 1K 75A 1

CDPL767-3 1U 120 1
120B D
180 1

CDPL767-31 1K 100 1
70A 1
70B D

CDPL767-33 1K 105 1
80A 1
80C D
2J 70 D

CDPL767-35 1B 30 1

CDPL767-37 1B 30A 1

CDPL767-39 1U 135 1
2C 125 D
2Y 40 D
3D 70 D
3G 105 D

CDPL767-41 1J 130 1
2D 140 D

50-11-05 Page 10074

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

CDPL767-43 1J 135 1
2D 135 D

CDPL767-45 1H 115 1
2E 105 D

CDPL767-47 1J 140 1
1U 140 1
2A 90 D
3E 120 D

CDPL767-5 2E 100 D

CDPL767-55 2D 130 D

CDPL767-57 2N 75 D

CDPL767-59 2J 80 D

CDPL767-61 2G 40 D
2H 85 D

CDPL767-63 2G 55 D

CDPL767-65 2D 170 D
2Y 185 D

CDPL767-67 2N 110 D

CDPL767-69 1Y 65B 1

CDPL767-7 1H 90 1
2C 100 D
2R 90 D

CDPL768-10 1H 90A 1

CDPL768-12 1H 95A 1

CDPL768-14 1G 85A D
2 60 D

CDPL768-18 1J 110B 1

50-11-05 Page 10075

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

CDPL768-2 1P 95 1
1V 95 1
1X 100 1
2Q 140 D
2S 35 D
2T 180 D
2U 180 D

CDPL768-22 1V 100 1

CDPL768-24 1J 125A 1
2K 100 D

CDPL768-26 1M 45 1

CDPL768-30 1J 110A 1

CDPL768-32 1B 30B 1

CDPL768-34 1B 30C 1
1C 50 1
3C 55 D

CDPL768-36 1M 40 1
2M 150 D

CDPL768-38 1V 105 1
2Q 90 D

CDPL768-4 1N 125 1
125A D
160 1

CDPL768-40 1H 110 1
115A 1
2R 95 D
3B 95 D

CDPL768-42 1J 150 1
1N 130 1
2H 95 D
2K 105 D
220 D
2M 140 D

CDPL768-46 2H 125 D

CDPL768-48 2K 225 D

50-11-05 Page 10076

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

CDPL768-50 2K 230 D

CDPL768-52 2M 145 D

CDPL768-54 2P 50 D

CDPL768-8 1G 80B D
2 55 D
2F 100 D

CDPL776-1 1Q 48 1
85 1
85A D

CDPL776-11 1B 25M 1
25X 1

CDPL776-15 1U 100A 1
2A 230 D
3E 135 D

CDPL776-17 1G 85C 1

CDPL776-19 1U 120A 1
2A 220 D
3E 125 D

CDPL776-21 1S 50 1

CDPL776-23 1W 115 1
115A D
170 1

CDPL776-25 1U 145 1
2A 80 D
3E 110 D

CDPL776-27 1G 100 D
3D 90 D

CDPL776-29 1G 95 D
2W 65 D
3D 75 D

CDPL776-3 1R 45 1
1W 110 1
2V 40 D

50-11-05 Page 10077

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

CDPL776-31 1G 105 D
2Z 100 D
3D 85 D

CDPL776-33 1P 110 1
2S 120 D

CDPL776-35 1B 25V 1
2B 20 D

CDPL776-37 2S 145 D

CDPL776-39 2W 35 D
2X 40 D

CDPL776-41 2W 125 D

CDPL776-43 2Y 35 D

CDPL776-45 2Z 80 D

CDPL776-47 2Z 110 D

CDPL776-49 2Z 170 D

CDPL776-5 1B 25J 1

CDPL776-51 3 50 D

CDPL776-53 3 140 D

CDPL776-55 3 115 D

CDPL776-7 1B 25K 1

CDPL776-9 1B 25L 1

CDPL777-12 1W 135 D
3F 120 D

CDPL777-16 1H 95C 1

CDPL777-18 2 60A D

CDPL777-2 1X 110 2

CDPL777-20 1X 105 1

CDPL777-22 1S 45 1

50-11-05 Page 10078

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

CDPL777-24 1P 90 1
1V 110 1
1X 115 1

CDPL777-26 1X 135 1
2T 155 D
2U 155 D

CDPL777-28 1X 140 1
2T 150 D
2U 150 D

CDPL777-30 1W 140 D
3A 135 D
3F 135 D

CDPL777-31 2X 55 D

CDPL777-33 2X 50 D

CDPL777-35 3B 100 D

CDPL777-37 3B 120 D

CDPL777-39 3A 195 D

CDPL777-4 1X 125 1
125B D
180 1

CDPL777-6 1R 50 1

CDPL785-1 1E 150 D

CDPL785-2 1E 150A D

CDPL785-3 1E 145 D

CDPL785-5 1E 155 D

CDPL788-11 1Y 65 1

CDPL788-13 1Y 65A 1

CDPL788-2 1C 55 1
3C 60 D

CDPL788-3 1G 85B D

50-11-05 Page 10079

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

CDPL788-5 1Y 55 1

CDPL788-7 1Y 60 1

CDPL788-9 1Z 55 1

CDPL789-1 2A 85 D
2Y 180 D
3E 115 D

CDSP1239-1 1H 50 1
1J 55 1
1N 50 1
1P 50 1
1U 50 1
1V 55 1
1W 50 1
1X 50 1
1Y 10 1
1Z 10 1
2A 145 D
55 D
2C 40 D
2D 40 D
2E 40 D
2H 40 D
2K 135 D
40 D
2M 40 D
2Q 40 D
2R 40 D
2S 70 D
2T 95 D
2U 95 D
2Y 130 D
3A 80 D
3B 45 D
3E 70 D
3F 30 D
3G 40 D

50-11-05 Page 10080

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 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

CDSP1239-3 1H 55 1
1J 60 1
1N 55 1
1P 55 1
1U 55 1
1V 60 1
1W 55 1
1X 55 1
1Y 15 1
1Z 15 1
2A 150 D
60 D
2C 45 D
2D 45 D
2E 45 D
2H 45 D
2K 140 D
45 D
2M 45 D
2Q 45 D
2R 45 D
2S 75 D
2T 100 D
2U 100 D
2Y 135 D
3A 85 D
3B 50 D
3E 75 D
3F 35 D
3G 45 D

50-11-05 Page 10081

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

CDSP1239-501 1H 45 30
45A 31
1J 50 26
50A 22
50B 41
1N 45 36
1P 45 30
1U 45 31
45A 32
1V 50 24
1W 45 29
45A D
1X 45 35
1Y 5 31
5A 32
5B 33
1Z 5 29
5A 30
2A 140 D
50 D
2C 35 D
35A D
2D 35 D
2E 35 D
2H 35 D
2K 130 D
35 D
2M 35 D
2Q 35 D
2R 35 D
2S 65 D
2T 90 D
2U 90 D
2Y 125 D
3A 75 D
3B 40 D
3E 65 D
3F 25 D
3G 35 D

CDSP5906C3-1250 1E 130 D

MS15795-844 1E 115 D

50-11-05 Page 10082

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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

MS16535-134 1H 30 1
1J 15 2
15A 3
1N 10 2
1P 10 1
1U 10 1
1V 10 1
1W 10 1
1X 10 2
2A 125 D
235 D
35 D
2C 60 D
2D 60 D
80 D
2E 60 D
2H 60 D
2K 155 D
175 D
60 D
2M 60 D
80 D
2Q 60 D
2R 60 D
2S 90 D
2T 125 D
2U 125 D
2Y 160 D
3A 115 D
3B 80 D
3E 30 D
50 D
3F 100 D
3G 80 D

NAS1149C0416R 1E 30 D

NAS1149CN516R 1E 110 D

NAS1198-3-4 1A 15 4

NAS1199-3-3 1A 25 4
1D 10 10
10A 14

NAS1398C3-3 1E 105 D

50-11-05 Page 10083

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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

NAS1515H3 1E 20 D
1F 15 8
1G 15 4
15A D
15B D
15C D
15D D
1H 15 4
1J 40 9
40A 10
1K 15 10
1L 15 9
1M 15 5
1N 35 10
1P 35 10
1Q 15 7
1R 15 6
1S 15 3
15A 4
1U 35 9
1V 35 8
1W 35 6
35A D
1X 35 10
2 15 D
35 D
2A 15 D
3D 15 D
3E 15 D
3F 15 D

50-11-05 Page 10084

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

SNS512AF 1F 42 D
1H 80 D
1J 100 D
1K 37 D
1L 52 D
1N 95 D
1P 80 D
1Q 90 D
1S 55 D
1U 90 D
1V 80 D
1W 95 D
1X 95 D
2 75 D
2A 185 D
245 D
95 D
3D 55 D
3E 180 D
3F 75 D
3G 65 D

SNS512AF0625200 1F 42A AR
1G 3 AR
1H 3 AR
1J 28 AR
1K 37A AR
1L 52A AR
1M 3 AR
1N 95A AR
1P 22 AR
1Q 90A AR
1R 3 AR
1S 55A AR
1U 23 AR
1V 22 AR
1W 22 AR
1X 22 AR

50-11-05 Page 10085

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

SNS512AF125250 1H 80A AR
1J 100A AR
1P 80A AR
1U 90A AR
1V 80A AR
1W 95A AR
1X 95A AR
2C 75X D
2D 95 D
2E 75 D
2K 75 D
2M 95 D

SNS512AF250500 1Y 45 AR
1Z 45 AR

10155610 1N 15 4
1U 15A 2
1W 15 2
1X 15A 4

14-18-150-24 1E 215 D
215A D

398FR 1C 57 AR
1F 43A AR
1H 120A AR
1J 155A AR
1K 38A AR
1L 53A AR
1N 135A AR
1P 115A AR
1Q 95A AR
1U 150A AR
1V 115A AR
1W 145A AR
1X 145A AR
1Y 70A AR
1Z 60A AR

5010-10-15 1H 35 2
1J 20 4
20A 6
1P 15 2
1V 15 2

50-11-05 Page 10086

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

5610-10-015 1U 15 D
1X 15 D
2A 130 D
240 D
40 D

5610-10-15 2C 65 D
2D 65 D
85 D
2E 65 D
2H 65 D
2K 160 D
180 D
65 D
2M 65 D
85 D
2Q 65 D
2R 65 D
2S 95 D
2T 130 D
2U 130 D
2Y 165 D
3A 120 D
3B 85 D
3E 35 D
55 D
3F 105 D
3G 85 D

85-46-101-41 1E 220 D
220A D

852Z0440-2 2 45 D

852Z0440-4 1S 25 1

852Z0440-5 1H 22 1

852Z0440-7 2 45A D

852Z0440-9 1Q 22 1

50-11-05 Page 10087

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

852Z8400-17 2C 215 D
2F 75 D
2J 135 D
75 D
2L 90 D
2N 70 D
2T 65 D
2U 65 D
2W 120 D
2Y 100 D
2Z 165 D
70 D
3 105 D
3A 190 D
3G 180 D

926 1B 17 AR
1F 44 AR
1G 73 AR
1H 122 AR
1J 68 AR
1K 22 AR
1L 51 AR
1M 27 AR
1N 137 AR
1P 63 AR
1Q 100A AR
53 AR
67 AR
1R 37 AR
1S 33 AR
1U 92 AR
1V 117 AR
1W 147 AR
1X 147 AR
2A 195 D
255 D
3E 190 D
3F 85 D

94639A137 1F 25 1

94639A567 1F 25A 1
1V 45 1

9485 3F 90 D

50-11-05 Page 10088

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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PART NUMBER AIRLINE FIGURE ITEM TOTAL

STOCK NUMBER NUMBER REQ'D
NUMBER

9485PC 1B 17A AR
1F 44A AR
1G 73A AR
1H 122A AR
1J 68A AR
1K 22A AR
1L 51A AR
1M 27A AR
1N 137A AR
1P 63A AR
1Q 100B AR
53A AR
67A AR
1R 37A AR
1S 33A AR
33B AR
1U 92A AR
1V 117A AR
1W 147A AR
1X 147A AR
3 65 D

50-11-05 Page 10089

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COMPONENT MAINTENANCE MANUAL
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DETAILED PARTS LIST

50-11-05 Page 10091

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

A F
B C D E

20

10

15

25

C411051−159
C411051−160
5011050101

Shroud Assembly
(Sheet 1 of 6)
Figure 1/GRAPHIC 50-11-05-99B-001-A01

50-11-05 Page 10092

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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20

15B

20

25B

C411051−161
C411051−162

B
5011050102

Shroud Assembly
(Sheet 2 of 6)
Figure 1/GRAPHIC 50-11-05-99B-001-A01

50-11-05 Page 10093

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

15G

20 25D

C411051−163
C411051−165
C419051−103
C419051−104

C
5011050103

Shroud Assembly
(Sheet 3 of 6)
Figure 1/GRAPHIC 50-11-05-99B-001-A01

50-11-05 Page 10094

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

20

22

20

25F

C414051−101
C414051−102

D
5011050104

Shroud Assembly
(Sheet 4 of 6)
Figure 1/GRAPHIC 50-11-05-99B-001-A01

50-11-05 Page 10095

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

10B
20

5B

25H

C419051−101
C419051−102

E
5011050105

Shroud Assembly
(Sheet 5 of 6)
Figure 1/GRAPHIC 50-11-05-99B-001-A01

50-11-05 Page 10096

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

10D
20

25M

5C

C419051−105
C419051−106

F
5011050106

Shroud Assembly
(Sheet 6 of 6)
Figure 1/GRAPHIC 50-11-05-99B-001-A01

50-11-05 Page 10097

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50-11-05 Page 10098

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 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1 – 1 C411051-159 SHROUD ASSY A RF

– 1A C411051-160 SHROUD ASSY B RF

– 1B C411051-161 SHROUD ASSY C RF

– 1C C411051-162 SHROUD ASSY D RF

– 1D C411051-163 SHROUD ASSY E RF

– 1E C411051-165 SHROUD ASSY F RF

– 1F C414051-101 SHROUD ASSY, SEC 43 G RF

– 1G C414051-102 SHROUD ASSY, SEC 43 H RF

– 1H C419051-101 SHROUD ASSY J RF

– 1J C419051-102 SHROUD ASSY K RF

– 1K C419051-103 SHROUD ASSY L RF

– 1L C419051-104 SHROUD ASSY M RF

– 1M C419051-105 SHROUD ASSY N RF

– 1N C419051-106 SHROUD ASSY P RF

5 C411051-93 . SEAL, FOAM A 1

(BONDED)

– 5A C411051-94 . SEAL, FOAM B 1

(BONDED)

5B C419052-11 . SEAL, FOAM J,K 1

(BONDED)

5C C419052-15 . SEAL, FOAM N,P 1

(BONDED)

10 C411051-89 . SEAL, FOAM A 1

(BONDED)

– 10A C411051-90 . SEAL, FOAM B 1

(BONDED)

10B C419052-1 . SEAL, FOAM J 1

(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10099

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1 – 10C C419052-2 . SEAL, FOAM K 1

(BONDED)

10D C419052-5 . SEAL, FOAM N 1

(BONDED)

– 10E C419052-6 . SEAL, FOAM P 1

(BONDED)

15 C411051-91 . SEAL, FOAM A 1

(BONDED)

– 15A C411051-92 . SEAL, FOAM B 1

(BONDED)

15B C411051-085 . SEAL, FOAM C,D 1

(BONDED)

– 15C C411051-088 . DELETED E D

(INCORRECT PN)

– 15D C411051-087 . DELETED F D

(INCORRECT PN)

– 15E C419052-3 . SEAL, FOAM L 1

(BONDED)

– 15F C419052-4 . SEAL, FOAM M 1

(BONDED)

15G C411051-88 . SEAL, FOAM E 1

(BONDED)
(CORRECT PN)

– 15H C411051-87 . SEAL, FOAM F 1

(BONDED)
(CORRECT PN)

20 BMS8-371 . SEAL, FOAM A-J,L-M AR

(V81205)
(BONDED)

22 C414052-1 . SEAL, FOAM G 1

(BONDED)

– 22A C414052-2 . SEAL, FOAM H 1

(BONDED)

25 C411051-059 . SHROUD A 1

– 25A C411051-060 . SHROUD B 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10100

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1 25B C411051-061 . SHROUD C 1

– 25C C411051-062 . SHROUD D 1

25D C411051-063 . SHROUD E 1

– 25E C411051-065 . SHROUD F 1

25F C414051-1 . SHROUD G 1

– 25G C414051-2 . SHROUD H 1

25H C419051-1 . SHROUD J 1

– 25J C419051-2 . SHROUD K 1

– 25K C419051-3 . SHROUD L 1

– 25L C419051-4 . SHROUD M 1

25M C419051-5 . SHROUD N 1

– 25N C419051-6 . SHROUD P 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10101

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

C B

35
50110501A01

Shroud Assembly
(Sheet 1 of 2)
Figure 1A/GRAPHIC 50-11-05-99B-002-A01

50-11-05 Page 10102

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

B
TYPICAL

D
10

25

20
15

30
C

D
50110501A02

Shroud Assembly
(Sheet 2 of 2)
Figure 1A/GRAPHIC 50-11-05-99B-002-A01

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 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1A – 1 C411051-171 SHROUD ASSY A RF

– 1A C411051-173 SHROUD ASSY B RF

5 BACN11AL1CM . NUT, CLIP-ON A 2

– 5A BACN11AL1CM . NUT, CLIP-ON B 3

10 C411051-501 . DOUBLER ASSY, SHROUD A 1

ATTACHING PARTS

15 NAS1198-3-4 . RIVET A 4

***

20 BACN10JB3CM . . NUTPLATE A 2

ATTACHING PARTS

25 NAS1199-3-3 . . RIVET A 4

***

30 C411051-075 . . DOUBLER, SHROUD A 1

35 C411051-071 . SHROUD A 1

– 35A C411051-073 . SHROUD B 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10105

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

30

25
20B

35

20B

10

15
50110501B01

Sloping Sidewall Liner Assembly

Figure 1B/GRAPHIC 50-11-05-99B-003-A01

50-11-05 Page 10106

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1B – 1 C411151-101 SIDEWALL LINER ASSY, SLOPING A RF

– 1A C411151-103 SIDEWALL LINER ASSY, SLOPING B RF

– 1B C411151-105 SIDEWALL LINER ASSY, SLOPING C RF

– 1C C411151-107 SIDEWALL LINER ASSY, SLOPING D RF

– 1D C411151-109 SIDEWALL LINER ASSY, SLOPING E RF

– 1E C411162-111 SIDEWALL LINER ASSY, SLOPING F RF

– 1F C411151-113 SIDEWALL LINER ASSY, SLOPING G RF

– 1G C411151-115 SIDEWALL LINER ASSY, SLOPING H RF

– 1H C411151-117 SIDEWALL LINER ASSY, SLOPING J RF

– 1J C411162-127 SIDEWALL LINER ASSY, SLOPING K RF

– 1K C411151-129 SIDEWALL LINER ASSY, SLOPING L RF

– 1L C411151-131 SIDEWALL LINER ASSY, SLOPING M RF

– 1M C411151-133 SIDEWALL LINER ASSY, SLOPING N RF

– 1N C411151-135 SIDEWALL LINER ASSY, SLOPING P RF

– 1P C411162-137 SIDEWALL LINER ASSY, SLOPING Q RF

– 1Q C411151-139 SIDEWALL LINER ASSY, SLOPING R RF

– 1R C411151-143 SIDEWALL LINER ASSY, SLOPING S RF

– 1S C411151-145 SIDEWALL LINER ASSY, SLOPING T RF

– 1T C411151-147 SIDEWALL LINER ASSY, SLOPING U RF

– 1U C411151-149 SIDEWALL LINER ASSY, SLOPING V RF

– 1V C411151-153 SIDEWALL LINER ASSY, SLOPING W RF

(SUPSD BY PN C411151-175, SEE
CMM 50-11-07 FOR DET)

– 1W C411151-155 SIDEWALL LINER ASSY, SLOPING X RF

– 1X C411151-179 SIDEWALL LINER ASSY, SEC 41 Y RF

SLOPING

– 1Y C411151-183 SIDEWALL LINER ASSY, SEC 41 Z RF

SLOPING
– ITEM NOT ILLUSTRATED

50-11-05 Page 10107

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 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1B – 1Z C419151-155 SIDEWALL LINER ASSY, SEC 46/47 AA RF

SLOPING

– 5 BACN11AL1CM . NUT, CLIP-ON B-E,G-J, 4

L-N,Q-S,
U,W-Y,AA

10 C411151-051 . STRIP, REINFORCEMENT A,E,F,J, 1

(BONDED) K,P,S-AA

– 10A C411151-051 . STRIP, REINFORCEMENT B-D,G, 2

(BONDED) H,L-N,
Q,R

– 10B C411051-67 . STRIP, REINFORCEMENT X 1

(BONDED)

– 12 C419153-1 . STRIP, REINFORCEMENT AA 1

(BONDED)

15 C411152-001 . DOUBLER A 1
(BONDED)

– 15A C411152-003 . DOUBLER B 1

(BONDED)

– 15B C411152-005 . DOUBLER C 1

(BONDED)

– 15C C411152-007 . DOUBLER D 1

(BONDED)

– 15D C411152-009 . DOUBLER E 1

(BONDED)

– 15E C411152-011 . DOUBLER F 1

(BONDED)

– 15F C411152-013 . DOUBLER G 1

(BONDED)

– 15G C411152-015 . DOUBLER H 1

(BONDED)

– 15H C411152-017 . DOUBLER J 1

(BONDED)

– 15J C411152-23 . DOUBLER K 1

(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10108

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1B – 15K C411152-25 . DOUBLER L 1

(BONDED)

– 15L C411152-27 . DOUBLER M 1

(BONDED)

– 15M C411152-29 . DOUBLER N,AA 1

(BONDED)

– 15N C411152-31 . DOUBLER P 1

(BONDED)

– 15P C411152-33 . DOUBLER Q 1

(BONDED)

– 15Q C411152-35 . DOUBLER R 1

(BONDED)

– 15R C411152-37 . DOUBLER W 1

(BONDED)

– 15S C411152-39 . DOUBLER X 1

(BONDED)

– 17 926 . TAPE, TRANSFER A-R,W,X, AR

(V04963) AA
(BONDED)

– 17A 9485PC . TAPE, TRANSFER A-R,W,X, AR

(V04963) AA
(BONDED)
(OPT TO ITEM -17)

– 20 BAC27TCA1 . DELETED A,C,E,G, D

(INCORRECT PN) J,K,M,P

– 20A BAC27TCA1 . DELETED B,D,F, D

(INCORRECT PN) H,L,N,
Q-V

20B BAC27TCA0001 . PLACARD, "NO STEP" A,C,E,G, 2

(BONDED) J,K,M,P

– 20C BAC27TCA0001 . PLACARD, "NO STEP" B,D,F, 1

(BONDED) H,L,N,
Q-V,Y,Z

– 20D CDPL1365-8 . PLACARD, "NO STEP" AA 1

(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10109

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1B – 20E CDPL1365-8 . PLACARD, "NO STEP" A,C,E,G, 2

(ALT TO ITEM 20B) J,K,M,P
(BONDED)

– 20F CDPL1365-8 . PLACARD, "NO STEP" B,D,F, 1

(ALT TO ITEM -20C) H,L,N,
(BONDED) Q-V,Y,Z

25 BAC27WCH277-121 . PLACARD, "121ABW" A 1

(BONDED)
(TRUE PN BAC27WCH277-121ABW)

– 25A BAC27WCH277-121 . PLACARD, "121BBW" B 1

(BONDED)
(TRUE PN BAC27WCH277-121BBW)

– 25B BAC27WCH277-121 . PLACARD, "121CBW" C 1

(BONDED)
(TRUE PN BAC27WCH277-121CBW)

– 25C BAC27WCH277-121 . PLACARD, "121DBW" D 1

(BONDED)
(TRUE PN BAC27WCH277-121DBW)

– 25D BAC27WCH277-121 . PLACARD, "121EBW" E 1

(BONDED)
(TRUE PN BAC27WCH277-121EBW)

– 25E BAC27WCH276-122 . PLACARD, "122ABW" F 1

(BONDED)
(TRUE PN BAC27WCH276-122ABW)

– 25F BAC27WCH276-122 . PLACARD, "122DBW" G 1

(BONDED)
(TRUE PN BAC27WCH276-122DBW)

– 25G BAC27WCH276-122 . PLACARD, "122EBW" H 1

(BONDED)
(TRUE PN BAC27WCH276-122EBW)

– 25H BAC27WCH276-122 . PLACARD, "122FBW" J 1

(BONDED)
(TRUE PN BAC27WCH276-122FBW)

– 25J CDPL776-5 . PLACARD, "151ABW" K 1

(BONDED)

– 25K CDPL776-7 . PLACARD, "151BBW" L 1

(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10110

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 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1B – 25L CDPL776-9 . PLACARD, "151CBW" M 1

(BONDED)

– 25M CDPL776-11 . PLACARD, "151DBW" N 1

(BONDED)

– 25N BAC27WCH269-152 . PLACARD, "152ABW" P 1

(BONDED)
(TRUE PN BAC27WCH269-152ABW)

– 25P BAC27WCH269-152 . PLACARD, "152BBW" Q 1

(BONDED)
(TRUE PN BAC27WCH269-152BBW)

– 25Q BAC27WCH269-152 . PLACARD, "152EBW" R 1

(BONDED)
(TRUE PN BAC27WCH269-152EBW)

– 25R BAC27WCH276-122 . PLACARD, "122BBW" S,Y 1

(BONDED)
(TRUE PN BAC27WCH276-122BBW)

– 25S BAC27WCH276-122 . PLACARD, "122CBW" T,Z 1

(BONDED)
(TRUE PN BAC27WCH276-122CBW)

– 25T BAC27WCH269-152 . PLACARD, "152CBW" U 1

(BONDED)
(TRUE PN BAC27WCH269-152CBW)

– 25U BAC27WCH269-152 . PLACARD, "152DBW" V 1

(BONDED)
(TRUE PN BAC27WCH269-152DBW)

– 25V CDPL776-35 . PLACARD, "151 EBW" W 1

(BONDED)

– 25W BAC27WCH269-152 . PLACARD, "152FBW" X 1

(BONDED)
(TRUE PN BAC27WCH269-152FBW)

– 25X CDPL776-11 . PLACARD, "151DBW" AA 1

(BONDED)

– 26 CDPL1379-1 . PLACARD, 121ABW A 1

(ALT TO ITEM 25)
(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10111

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 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1B – 26A CDPL1379-3 . PLACARD, "121BBW" B 1

(ALT TO ITEM -25A)
(BONDED)

– 26B CDPL1379-5 . PLACARD, "121CBW" C 1

(ALT TO ITEM -25B)
(BONDED)

– 26C CDPL1379-7 . PLACARD, "121DBW" D 1

(ALT TO ITEM -25C)
(BONDED)

– 26D CDPL1379-9 . PLACARD, "121EBW" E 1

(ALT TO ITEM -25D)
(BONDED)

– 26E CDPL1381-1 . PLACARD, "122ABW" F 1

(ALT TO ITEM -25E)
(BONDED)

– 26F CDPL1381-8 . PLACARD, "122DBW" G 1

(ALT TO ITEM -25F)
(BONDED)

– 26G CDPL1381-10 . PLACARD, "122EBW" H 1

(ALT TO ITEM -25G)
(BONDED)

– 26H CDPL1381-12 . PLACARD, "122FBW" J 1

(ALT TO ITEM -25H)
(BONDED)

– 26J CDPL1382-1 . PLACARD, "152ABW" P 1

(ALT TO ITEM -25N)
(BONDED)

– 26K CDPL1382-3 . PLACARD, "152BBW" Q 1

(ALT TO ITEM -25P)
(BONDED)

– 26L CDPL1382-9 . PLACARD, "152EBW" R 1

(ALT TO ITEM -25Q)
(BONDED)

– 26M CDPL1381-4 . PLACARD, "122BBW" S,Y 1

(ALT TO ITEM -25R)
(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10112

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 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1B – 26N CDPL1381-6 . PLACARD, "122CBW" T,Z 1

(ALT TO ITEM -25S)
(BONDED)

– 26P CDPL1382-5 . PLACARD, "152CBW" U 1

(ALT TO ITEM -25T)
(BONDED)

– 26Q CDPL1382-7 . PLACARD, "152DBW" V 1

(ALT TO ITEM -25U)
(BONDED)

– 26R CDPL1382-11 . PLACARD, "152FBW" X 1

(ALT TO ITEM -25W)
(BONDED)

30 CDPL767-35 . PLACARD, "THE CARGO…" A,K 1

(BONDED)

– 30A CDPL767-37 . PLACARD, "THE CARGO…" E 1

(ALT TO ITEM -25T)
(BONDED)

– 30B CDPL768-32 . PLACARD, "THE CARGO…" F 1

(ALT TO ITEM -25U)
(BONDED)

– 30C CDPL768-34 . PLACARD, "THE CARGO…" J 1

(BONDED)

35 C411151-001 . SIDEWALL LINER, SLOPING A 1

– 35A C411151-003 . SIDEWALL LINER, SLOPING B 1

– 35B C411151-005 . SIDEWALL LINER, SLOPING C 1

– 35C C411151-007 . SIDEWALL LINER, SLOPING D 1

– 35D C411151-009 . SIDEWALL LINER, SLOPING E 1

– 35E C411162-11 . SIDEWALL LINER, SLOPING F 1

– 35F C411151-013 . SIDEWALL LINER, SLOPING G 1

– 35G C411151-015 . SIDEWALL LINER, SLOPING H 1

– 35H C411151-017 . SIDEWALL LINER, SLOPING J 1

– 35J C411162-27 . SIDEWALL LINER, SLOPING K 1

– 35K C411151-29 . SIDEWALL LINER, SLOPING L 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10113

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1B – 35L C411151-031 . SIDEWALL LINER, SLOPING M 1

– 35M C411151-033 . SIDEWALL LINER, SLOPING N 1

– 35N C411151-35 . SIDEWALL LINER, SLOPING P 1

– 35P C411162-37 . SIDEWALL LINER, SLOPING Q 1

– 35Q C411151-39 . SIDEWALL LINER, SLOPING R 1

– 35R C411151-043 . SIDEWALL LINER, SLOPING S 1

– 35S C411151-045 . SIDEWALL LINER, SLOPING T 1

– 35T C411151-47 . SIDEWALL LINER, SLOPING U 1

– 35U C411151-49 . SIDEWALL LINER, SLOPING V 1

– 35V C411151-53 . SIDEWALL LINER, SLOPING W 1

– 35W C411151-55 . SIDEWALL LINER, SLOPING X 1

– 35X C411151-79 . SIDEWALL LINER, SLOPING Y 1

– 35Y C411151-83 . SIDEWALL LINER, SLOPING Z 1

– 35Z C419151-55 . SIDEWALL LINER, SLOPING AA 1

– ITEM NOT ILLUSTRATED

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 COMPONENT MAINTENANCE MANUAL
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55
50

45
50110501C01

Bulk Sloping Sidewall Panel Assembly

(Sheet 1 of 2)
Figure 1C/GRAPHIC 50-11-05-99B-004-A01

50-11-05 Page 10116

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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30 35

25
20

15

10
60

40

50110501C02

B
ROTATED 180°

Bulk Sloping Sidewall Panel Assembly

(Sheet 2 of 2)
Figure 1C/GRAPHIC 50-11-05-99B-004-A01

50-11-05 Page 10117

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50-11-05 Page 10118

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 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1C – 1 C411151-159 PANEL ASSY, BULK SLOPING A RF

SIDEWALL

– 1A C411151-173 DELETED B D

– 1B C414151-123 PANEL ASSY, SEC 47 BULK SLOPING C RF

SIDEWALL

– 1C C419151-143 PANEL ASSY, SEC 47 BULK SLOPING D RF

SIDEWALL

– 3 C411151-575 . DELETED B D

5 BACN11AL1CM . NUT, CLIP-ON A 3

– 5A BACN11AL1CM . NUT, CLIP-ON C,D 4

10 C411151-077 . CLOSEOUT, NET FITTING A,D 1

– 10A C414153-3 . CLOSEOUT, NET FITTING C 1

ATTACHING PARTS

15 BACS12FA3K4 . SCREW A,B,D 4

– 15A BACS12FA3K4 . SCREW C 6

***

20 C411151-079 . CLOSEOUT, NET FITTING 1

ATTACHING PARTS

25 BACS12FA3K4 . SCREW 4

***

30 C411152-075 . LINER STRIP, SIDEWALL A 1

(BONDED)

– 30A C414153-1 . LINER STRIP, SIDEWALL C 1

(BONDED)

– 30B C419153-3 . LINER STRIP, SIDEWALL D 1

(BONDED)

ATTACHING PARTS

35 BACS12FA3K4 . SCREW A-C 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10119

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1C – 35A BACS12FA3K4 . SCREW D 2

***

40 C411151-073 . FILLER, FOAM A 1

(BONDED)

– 40A C411151-081 . DELETED B D

45 BAC27TCH0429 . PLACARD, "FITTINGS USED…" 1

(BONDED)

50 CDPL768-34 . PLACARD, "THE CARGO…" 1

(BONDED)

55 CDPL788-2 . PLACARD, "162ABW" 1

(BONDED)

– 57 398FR . TAPE, GLASS CLOTH AR

(V04963)
(BONDED)
(1")

60 C411151-559 . PANEL ASSY A 1

– 60A C411151-573 . DELETED B D

– 60B C414151-523 . PANEL ASSY C 1

– 60C C419151-543 . PANEL ASSY D 1

– 65 C411151-059 . . PANEL A 1

– 65A C411151-73 . . DELETED B D

– 65B C414151-23 . . PANEL C 1

– 65C C419151-43 . . PANEL D 1

– ITEM NOT ILLUSTRATED

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50-11-05 Page 10121

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 COMPONENT MAINTENANCE MANUAL
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10

15

50110501D01

Bulk Sloper Bracket Assembly

Figure 1D/GRAPHIC 50-11-05-99B-005-A01

50-11-05 Page 10122

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1D – 1 C411152-161 BRACKET ASSY, BULK SLOPER A RF

– 1A C411152-163 BRACKET ASSY, BULK SLOPER B RF

– 1B C411152-165 BRACKET ASSY, BULK SLOPER C RF

– 1C C411152-167 BRACKET ASSY, BULK SLOPER D RF

– 1D C411152-169 BRACKET ASSY, BULK SLOPER E RF

– 1E C411152-171 BRACKET ASSY, BULK SLOPER F RF

5 BACN10JB3CM . NUTPLATE A,D 5

– 5A BACN10JB3CM . NUTPLATE B,C,E,F 7

ATTACHING PARTS

10 NAS1199-3-3 . RIVET A,D 10

– 10A NAS1199-3-3 . RIVET B,C,E,F 14

***

15 C411152-061 . BRACKET, BULK SLOPER A 1

– 15A C411152-063 . BRACKET, BULK SLOPER B 1

– 15B C411152-065 . BRACKET, BULK SLOPER C 1

– 15C C411152-067 . BRACKET, BULK SLOPER D 1

– 15D C411152-069 . BRACKET, BULK SLOPER E 1

– 15E C411152-071 . BRACKET, BULK SLOPER F 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10123

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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D
TE
LE
DE

Bulk Endwall Assembly

Figure 1E/GRAPHIC 50-11-05-99B-006-A01

50-11-05 Page 10124

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1E – 1 C412301-109 DELETED A D

– 1A C412301-111 DELETED B D

– 1B C412301-115 DELETED C D

– 1C C412301-117 DELETED D D

– 5 C411026-510 . DELETED D

ATTACHING PARTS

– 10 BACN10YR3CM . DELETED D

– 15 BACS12FA3K9 . DELETED D

– 20 NAS1515H3 . DELETED D

***

– 25 BACP18BE4N0750U . . DELETED D

– 30 NAS1149C0416R . . DELETED D

– 35 C411301-005 . . DELETED D

– 40 C411302-007 . . DELETED D

– 45 C411026-010 . . DELETED D

– 50 C411026-027 . DELETED D

ATTACHING PARTS

– 55 BACS12FA3K4 . DELETED D

***

– 60 C411026-028 . DELETED D

ATTACHING PARTS

– 65 BACS12FA3K4 . DELETED D

***

– 70 C412301-515 . DELETED D

– 75 C411026-511 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10125

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1E ATTACHING PARTS

– 80 BACS12FA3K5 . . DELETED D

***

– 85 BACP18BE4N0437U . . . DELETED D

– 90 C411026-019 . . . DELETED D

– 95 C411026-021 . . . DELETED D

– 100 C412301-047 . . DELETED D

ATTACHING PARTS

– 105 NAS1398C3-3 . . DELETED D

– 110 NAS1149CN516R . . DELETED D

– 115 MS15795-844 . . DELETED D

– 120 BACS12FA3K5 . . DELETED D

***

– 125 BACI12AG3UCM3 . . DELETED D

– 130 CDSP5906C3-1250 . . DELETED D

– 135 CDM200-05 . . DELETED D

– 140 C412301-045 . . DELETED D

– 145 CDPL785-3 . DELETED D

– 150 CDPL785-1 . DELETED A,C D

– 150A CDPL785-2 . DELETED B,D D

– 155 CDPL785-5 . DELETED B-D D

– 160 BACS12FA3K4 . DELETED D

– 165 C412301-035 . DELETED D

ATTACHING PARTS

– 170 BACS12FA3K5 . DELETED D

***
– 175 C412301-037 . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10126

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1E ATTACHING PARTS

– 180 BACS12FA3K5 . DELETED D

***

– 185 C412301-041 . DELETED D

ATTACHING PARTS

– 190 BACS12ER3K6 . DELETED D

***

– 195 C412301-043 . DELETED D

ATTACHING PARTS

– 200 BACS12ER3K6 . DELETED D

***
– 205 BACR12AG5C . DELETED C D

– 205A BACR12AG5C . DELETED D D

– 210 BACS21AP6620RPS . DELETED C D

– 210A BACS21AP6620RPS . DELETED D D

– 215 14-18-150-24 . DELETED C D

– 215A 14-18-150-24 . DELETED D D

– 220 85-46-101-41 . DELETED C D

– 220A 85-46-101-41 . DELETED D D

– 225 BMS1-68 . DELETED D

– 230 BMS8-283 . DELETED C,D D

– 235 C412301-509 . DELETED A D

– 235A C412301-511 . DELETED B D

– 235B C412301-517 . DELETED C D

– 235C C412301-519 . DELETED D D

– 240 BACI12AH5U1255 . . DELETED C D

– 240A BACI12AH5U1255 . . DELETED D D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10127

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1E – 245 BACI12AG3UCM3 . . DELETED C D

– 250 C412301-029 . . DELETED A D

– 250A C412301-027 . . DELETED B D

– 250B C412301-049 . . DELETED C D

– 250C C412301-051 . . DELETED D D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10128

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 COMPONENT MAINTENANCE MANUAL
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25
A

55
15

10A
70

50

75
20

65 60

30

40
45

35
A
50110501F01

Vertical Sidewall Panel Assembly

Figure 1F/GRAPHIC 50-11-05-99B-007-A01

50-11-05 Page 10130

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1F – 1 C412409-101 PANEL ASSY, VERTICAL SIDEWALL A RF

– 1A C412418-101 PANEL ASSY, SEC 41 VERTICAL B RF

SIDEWALL

5 C412406-043 . EXTRUSION, SIDEWALL 1

(BONDED)

ATTACHING PARTS

– 10 BACN10YR3CD . DELETED A D
(INCORRECT PN)

10A BACN10YR3CM . NUT 8

15 NAS1515H3 . WASHER 8

20 BACS12FA3K8 . SCREW 8

***

25 94639A137 . SPACER A 1
(V3A054)
SUPSD BY ITEM -25A

– 25A 94639A567 . SPACER 1

(V3A054)
(BONDED)
SUPSDS ITEM 25

30 C412413-059 . STRIP, COVER 1

(BONDED)

35 C412413-060 . STRIP, COVER 1

(BONDED)

40 C412407-096 . STRIP, COVER 1

(BONDED)

– 42 SNS512AF . DELETED D
(INCORRECT PN)

– 42A SNS512AF0625200 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

– 43 CDM200-05 . DELETED D
(INCORRECT PN)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10131

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1F – 43A 398FR . TAPE, GLASS CLOTH AR

(V04963)
(BONDED)
(1")
(0.5")

– 44 926 . TAPE, TRANSFER AR

(V04963)
(BONDED)

– 44A 9485PC . TAPE, TRANSFER AR

(V04963)
(BONDED)
(OPT TO ITEM -44)

45 C412411-007 . BLOW IN PANEL A 1

– 45A C412419-7 . DELETED B D

50 C412414-001 . LINER, VERTICAL SIDEWALL 1

(BONDED)

55 C412410-001 . GRILL 1

60 BAC27WCH277-121 . PLACARD, "121AW" 1

(BONDED)
(TRUE PN BAC27WCH277-121AW)

– 60A CDPL1379-2 . PLACARD, "121AW" 1

(ALT TO ITEM 60)
(BONDED)

65 BAC27WCH210 . PLACARD, "PALLET 11" A 1

(BONDED)

– 65A CDPL1364-1 . PLACARD, "PALLET 11" A 1

(ALT TO ITEM 65)
(BONDED)

– 65B BAC27WCH210 . DELETED B D

70 BAC27WCH219 . PLACARD, "P11" 1

(BONDED)

– 70A CDPL1365-2 . PLACARD, "P11" 1

(ALT TO ITEM 70)
(BONDED)

75 BAC27WCH240 . PLACARD, "11L|" 1

(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10132

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1F – 75A CDPL1367-3 . PLACARD, "11L|" 1

(ALT TO ITEM 75)
(BONDED)

– 80 C412419-507 . DECOMPRESSION BLOW, SUBASSY B 1

– 85 BAC27WCH210 . . PLACARD, "PALLET 11" B 1

(BONDED)

– 85A CDPL1364-1 . . PLACARD, "PALLET 11" B 1

(ALT TO ITEM -85)
(BONDED)

– 90 C412419-7 . . BLOW IN PANEL B 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10133

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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30A
10E
15
5E

20

90B
80E

70F

85C
75E

A
50110501G01

Vertical Sidewall Panel Assembly

Figure 1G/GRAPHIC 50-11-05-99B-008-A01

50-11-05 Page 10134

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1G – 1 C412409-117 DELETED A D

– 1A C412409-121 DELETED B D

– 1B C412409-123 DELETED C D

– 1C C412409-137 DELETED D D

– 1D C412409-161 PANEL ASSY, VERTICAL SIDEWALL E RF

– 1E C412409-167 DELETED F D

– 1F C419401-155 DELETED G D

– 3 SNS512AF0625200 . TAPE, SILICONE FOAM E AR

(V12624)
(BONDED)

– 5 C412406-045 . DELETED A D

– 5A C412406-019 . DELETED B D

– 5B C412406-003 . DELETED C D

– 5C C412406-021 . DELETED C D

– 5D C412406-005 . DELETED D D

5E C412406-027 . EXTRUSION, SIDEWALL E 1

(BONDED)

ATTACHING PARTS

– 10 BACN10YR3CD . DELETED E D
(INCORRECT PN)

– 10A BACN10YR3CD . DELETED A D

– 10B BACN10YR3CD . DELETED B D

– 10C BACN10YR3CD . DELETED C D

– 10D BACN10YR3CD . DELETED D D

10E BACN10YR3CM . NUT E 4

15 NAS1515H3 . WASHER E 4

– 15A NAS1515H3 . DELETED A D

– 15B NAS1515H3 . DELETED B D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10135

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1G – 15C NAS1515H3 . DELETED C D

– 15D NAS1515H3 . DELETED D D

20 BACS12FA3K8 . SCREW E 4

– 20A BACS12FA3K8 . DELETED A D

– 20B BACS12FA3K8 . DELETED B D

– 20C BACS12FA3K8 . DELETED C D

– 20D BACS12FA3K8 . DELETED D D

***
– 25 C412413-055 . DELETED A D

– 25A C412413-083 . DELETED C D

– 30 C412405-045 . DELETED
E D
(INCORRECT PN)

30A C412405-061 . PANEL, INSULATION

E 1
(BONDED)

– 35 C412413-081 . DELETED B D

– 40 C412413-082 . DELETED D D

– 45 C412413-084 . DELETED D D

– 50 C412413-086 . DELETED D D

– 55 C412413-088 . DELETED D D

– 60 C412411-043 . DELETED D D

– 65 C412411-045 . DELETED C D

– 70 C412410-021 . DELETED A D

– 70A C412410-029 . DELETED B D

– 70B C412410-031 . DELETED C D

– 70C C412410-055 . DELETED D D

– 70D C412410-095 . DELETED D D

– 70E C412410-097 . DELETED D D

70F C412410-099 . LINER E 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10136

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1G – 70G C412404-011 . DELETED F D

– 70H C419403-53 . DELETED G D

– 73 926 . TAPE, TRANSFER E AR

(V04963)
(BONDED)
(0.75")

– 73A 9485PC . TAPE, TRANSFER E AR

(V04963)
(BONDED)
(OPT TO ITEM -73)
(1")

– 75 BAC27WCH277 . DELETED A D

– 75A BAC27WCH276 . DELETED B D

– 75B BAC27WCH276 . DELETED C D

– 75C BAC27WCH282 . DELETED F,G D

– 75D BAC27WCH270 . DELETED D D

75E BAC27WCH270-151 . PLACARD, "151FW" E 1

(BONDED)
(TRUE PN BAC27WCH270-151FW)

– 75F CDPL1380-6 . PLACARD, "151FW" E 1

(ALT TO ITEM 75E)
(BONDED)

– 80 CDPL767-1 . DELETED A D

– 80A BAC27WCH219 . DELETED B D

– 80B CDPL768-8 . DELETED C D

– 80C BAC27WCH202 . DELETED F,G D

– 80D BAC27WCH363 . DELETED D D

80E BAC27WCH201 . PLACARD, "STA 1600" E 1

(BONDED)

– 80F CDPL1361-4 . PLACARD, "STA 1600" E 1

(ALT TO ITEM 80E)
(BONDED)

– 85 CDPL767-23 . DELETED A D
– ITEM NOT ILLUSTRATED

50-11-05 Page 10137

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1G – 85A CDPL768-14 . DELETED C D

– 85B CDPL788-3 . DELETED F,G D

85C CDPL776-17 . PLACARD, "43L|42L" E 1

(BONDED)

– 90 BAC27WCH366 . DELETED D D

– 90A BAC27WCH209 . DELETED A D

90B BAC27WCH353 . PLACARD, "PALLET 42" E 1

(BONDED)

– 90C CDPL1364-9 . PLACARD, "PALLET 42" E 1

(ALT TO ITEM 90B)
(BONDED)

– 95 CDPL776-29 . DELETED D D

– 100 CDPL776-27 . DELETED D D

– 105 CDPL776-31 . DELETED D D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10138

Oct 09/23
COMPONENT MAINTENANCE MANUAL
C41XXXX

This page intentionally left blank.

50-11-05 Page 10139

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

15
20
10

100

70

75

90
65

25
40
35
125

95

85

60B
35
30
45
50110501H01

Vertical Sidewall Panel Assembly

Figure 1H/GRAPHIC 50-11-05-99B-009-A01

50-11-05 Page 10140

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1H – 1 C412416-103 PANEL ASSY, SEC 41 VERTICAL A RF

SIDEWALL

– 1A C412416-104 PANEL ASSY, SEC 41 VERTICAL B RF

SIDEWALL

– 1B C412416-109 PANEL ASSY, SEC 41 VERTICAL C RF

SIDEWALL

– 1C C412416-145 PANEL ASSY, VERTICAL SIDEWALL D RF

SUPSD BY ITEM -1D

– 1D C412417-145 PANEL ASSY, SEC 46 VERTICAL E RF

SIDEWALL
SUPSDS ITEM -1C

– 3 SNS512AF0625200 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

5 C412406-003 . EXTRUSION, SIDEWALL 1

(BONDED)

ATTACHING PARTS

10 BACN10YR3CM . NUT 4

15 NAS1515H3 . WASHER 4

20 BACS12FA3K8 . SCREW 4

***

– 22 852Z0440-5 . LINER, WATER DAM E 1

(V81205)
(BONDED)

25 C412413-056 . LANYARD, CARGO ACCESS PANEL 1

ATTACHING PARTS

30 MS16535-134 . RIVET 1

35 5010-10-15 . WASHER, NYLON 2

(V86928)

***

40 C412413-058 . HOOK FASTENER 1

(BONDED)
– ITEM NOT ILLUSTRATED

50-11-05 Page 10141

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1H 45 CDSP1239-501 . QUARTER TURN FASTENER ASSY A,C-E 30

– 45A CDSP1239-501 . QUARTER TURN FASTENER ASSY B 31

– 50 CDSP1239-1 . . SLEEVE 1

– 55 CDSP1239-3 . . STUD 1

– 60 C412901-003 . RETAINER A,C,E 30

(OPT TO ITEM 60B)

– 60A C412901-003 . RETAINER B 31

(OPT TO ITEM -60C)

60B C412901-5 . RETAINER A,C,E 30

– 60C C412901-5 . RETAINER B 31

– 60D C412901-003 . RETAINER D 30

65 C412413-013 . STRIP, DOUBLER A 1

(BONDED)

– 65A C412413-014 . STRIP, DOUBLER B 1

(BONDED)

– 65B C412413-004 . STRIP, DOUBLER C 1

(BONDED)

– 65C C412413-041 . STRIP, DOUBLER D-E 1

(BONDED)

70 C412413-099 . STRIP, DOUBLER A 1

(BONDED)

– 70A C412413-022 . STRIP, DOUBLER B 1

(BONDED)

– 70B C412413-018 . STRIP, DOUBLER C 1

(BONDED)
– 70C C412407-040 . STRIP, DOUBLER D-E 1
(BONDED)

75 C412413-098 . STRIP, DOUBLER A 1

(BONDED)

– 75A C412413-023 . STRIP, DOUBLER B 1

(BONDED)
– 75B C412413-017 . STRIP, DOUBLER
C 1
(BONDED)
– ITEM NOT ILLUSTRATED

50-11-05 Page 10142

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1H – 75C C412413-049 . STRIP, DOUBLER D-E 1

(BONDED)

– 80 SNS512AF . DELETED D
(INCORRECT PN)

– 80A SNS512AF125250 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

85 BAC27WCH277-121 . PLACARD, "121BW" A 1

(BONDED)
(TRUE PN BAC27WCH277-121BW)

– 85A BAC27WCH276-122 . PLACARD, "122BW" B 1

(BONDED)
(TRUE PN BAC27WCH276-122BW)

– 85B BAC27WCH277-121 . PLACARD, "121EW" C 1

(BONDED)
(TRUE PN BAC27WCH277-121EW)

– 85C BAC27WCH269-152 . PLACARD, "152CW" D,E 1

(BONDED)
(TRUE PN BAC27WCH269-152CW)

– 85D CDPL1379-4 . PLACARD, "121BW" A 1

(ALT TO ITEM 85)
(BONDED)

– 85E CDPL1381-5 . PLACARD, "122BW" B 1

(ALT TO ITEM -85A)
(BONDED)

– 85F CDPL1379-10 . PLACARD, "121EW" C 1

(ALT TO ITEM -85B)
(BONDED)

– 85G CDPL1382-6 . PLACARD, "152CW" D,E 1

(ALT TO ITEM -85C)
(BONDED)

90 CDPL767-7 . PLACARD, "|STA 400" A 1

(BONDED)

– 90A CDPL768-10 . PLACARD, "|STA 400" B 1

(BONDED)

95 CDPL767-11 . PLACARD, "12L|11L" A 1

(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10143

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1H – 95A CDPL768-12 . PLACARD, "11R|12R" B 1

(BONDED)

– 95B CDPL767-17 . PLACARD, "14L" C 1

(BONDED)

– 95C CDPL777-16 . PLACARD, "33R" D,E 1

(BONDED)

100 BAC27WEC163 . PLACARD, "E/E COOLING SUPPLY A 1

FAN"
(BONDED)

– 100A CDPL1365-9 . PLACARD, "E/E COOLING SUPPLY A 1

FAN"
(ALT TO ITEM 100)
(BONDED)

– 105 BAC27WCH210 . PLACARD, "PALLET 11" B 1

(BONDED)

– 105A BAC27WCH352 . PLACARD, "PALLET 32" D,E 1

(BONDED)

– 105B CDPL1364-1 . PLACARD, "PALLET 11" B 1

(ALT TO ITEM -105)
(BONDED)

– 105C CDPL1364-8 . PLACARD, "PALLET 32" D,E 1

(ALT TO ITEM -105A)
(BONDED)

– 110 CDPL768-40 . PLACARD, "LARGE CARGO DOOR..." B 1

(BONDED)

– 115 CDPL767-45 . PLACARD, "HUMIDIFIER INTERFACE C 1

UNIT (OPTIONAL)"
(BONDED)

– 115A CDPL768-40 . PLACARD, "LARGE CARGO DOOR..." D,E 1

(BONDED)

– 120 CDM200-05 . DELETED D

(INCORRECT PN)

– 120A 398FR . TAPE, GLASS CLOTH AR

(V04963)
(BONDED)
(1")

– ITEM NOT ILLUSTRATED

50-11-05 Page 10144

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1H – 122 926 . TAPE, TRANSFER AR

(V04963)
(BONDED)
(0.75")

– 122A 9485PC . TAPE, TRANSFER AR

(V04963)
(BONDED)
(1")
(OPT TO ITEM -122)

125 C412410-003 . LINER, VERTICAL SIDEWALL A 1

– 125A C412410-004 . LINER, VERTICAL SIDEWALL B 1

– 125B C412410-013 . LINER, VERTICAL SIDEWALL C 1

– 125C C412410-067 . LINER, VERTICAL SIDEWALL D-E 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10145

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

30 105
65C 160

35
40
75

165 50

125 140
85 130
80 25

115

45 135
70 120

10
20 15
20 110
25

15
20
20 5

A
50110501J01

Vertical Sidewall Panel Assembly

Figure 1J/GRAPHIC 50-11-05-99B-010-A01

50-11-05 Page 10146

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1J – 1 C412416-107 PANEL ASSY, SEC 41 VERTICAL A RF

SIDEWALL

– 1A C412416-127 PANEL ASSY, SEC 43 VERTICAL B RF

SIDEWALL

– 1B C412416-129 PANEL ASSY, SEC 43 VERTICAL C RF

SIDEWALL

5 C412413-056 . LANYARD, CARGO ACCESS PANEL A 1

– 5A C412413-056 . LANYARD, CARGO ACCESS PANEL B,C 2

10 C412413-057 . LANYARD, CARGO ACCESS PANEL 1

ATTACHING PARTS

15 MS16535-134 . RIVET A 2

– 15A MS16535-134 . RIVET B,C 3

20 5010-10-15 . WASHER, NYLON A 4

(V86928)

– 20A 5010-10-15 . WASHER, NYLON B,C 6

(V86928)

***

25 C412413-058 . HOOK FASTENER A 2

(BONDED)

– 25A C412413-058 . HOOK FASTENER B,C 3

(BONDED)

– 28 SNS512AF0625200 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

30 C412406-005 . EXTRUSION, SIDEWALL A 1

(BONDED)

– 30A C412406-014 . EXTRUSION, SIDEWALL B 1

(BONDED)

– 30B C412406-015 . EXTRUSION, SIDEWALL C 1

(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10147

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1J ATTACHING PARTS

35 BACN10YR3CM . NUT A,C 9

– 35A BACN10YR3CM . NUT B 10

40 NAS1515H3 . WASHER A,C 9

– 40A NAS1515H3 . WASHER B 10

45 BACS12FA3K8 . SCREW A,C 9

– 45A BACS12FA3K8 . SCREW B 10

***

50 CDSP1239-501 . QUARTER TURN FASTENER ASSY A 26

– 50A CDSP1239-501 . QUARTER TURN FASTENER ASSY B 22

– 50B CDSP1239-501 . QUARTER TURN FASTENER ASSY C 41

– 55 CDSP1239-1 . . SLEEVE 1

– 60 CDSP1239-3 . . STUD 1

– 65 C412901-003 . RETAINER A 26
(OPT TO ITEM 65C)

– 65A C412901-003 . RETAINER B 22

(OPT TO ITEM -65D)

– 65B C412901-003 . RETAINER C 41

(OPT TO ITEM -65E)

65C C412901-5 . RETAINER A 26

– 65D C412901-5 . RETAINER B 22

– 65E C412901-5 . RETAINER C 41

– 68 926 . TAPE, TRANSFER AR

(V04963)
(BONDED)
(0.75")

– 68A 9485PC . TAPE, TRANSFER AR

(V04963)
(BONDED)
(1")
(OPT TO ITEM -68)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10148

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1J 70 C412413-002 . STRIP, DOUBLER A 1

(BONDED)

– 70A C412413-008 . STRIP, DOUBLER B 1

(BONDED)

– 70B C412413-006 . STRIP, DOUBLER C 1

(BONDED)

75 C412413-015 . STRIP, DOUBLER A 1

(BONDED)

80 C412413-016 . STRIP, DOUBLER A 1

(BONDED)

– 80A C412413-019 . STRIP, DOUBLER B,C 1

(BONDED)

85 C412414-003 . STRIP, DOUBLER A 1

(BONDED)

– 85A C412413-010 . STRIP, DOUBLER B 1

(BONDED)

– 85B C412413-007 . STRIP, DOUBLER C 1

(BONDED)

– 90 C412413-020 . STRIP, DOUBLER C 1

(BONDED)

– 90A C412413-019 . STRIP, DOUBLER B 1

(BONDED)

– 95 C412413-021 . STRIP, DOUBLER C 1

(BONDED)

– 100 SNS512AF . DELETED D

(INCORRECT PN)

– 100A SNS512AF125250 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

105 BAC27WCH117 . PLACARD, "STA|500" A 1

(BONDED)

– 105A BAC27WCH197 . PLACARD, "STA|700" B 1

(BONDED)

– 105B BAC27WCH209 . PLACARD, "STA|800" C 1

(BONDED)
– ITEM NOT ILLUSTRATED

50-11-05 Page 10149

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1J – 105C CDPL1361-1 . PLACARD, "STA|500" A 1

(ALT TO ITEM 105)
(BONDED)

– 105D CDPL1361-3 . PLACARD, "STA|700" B 1

(ALT TO ITEM -105A)
(BONDED)

– 105E CDPL1366-9 . PLACARD, "STA|800" C 1

(ALT TO ITEM -105B)
(BONDED)

110 BAC27WCH243 . PLACARD, "L14|L13" A 1

(BONDED)

– 110A CDPL768-30 . PLACARD, "22R|23R" B 1

(BONDED)

– 110B CDPL768-18 . PLACARD, "23R|24R" C 1

(BONDED)

– 110C CDPL1362-1 . PLACARD, "L14|L13" A 1

(ALT TO ITEM 110)
(BONDED)

115 BAC27WCH277-121 . PLACARD, "121DW" A 1

(BONDED)
(TRUE PN BAC27WCH277-121DW)

– 115A BAC27WCH276-122 . PLACARD, "121HW" B 1

(BONDED)
(TRUE PN BAC27WCH276-122HW)

– 115B BAC27WCH276-122 . PLACARD, "122JW" C 1

(BONDED)
(TRUE PN BAC27WCH276-122JW)

– 115C CDPL1379-8 . PLACARD, "121DW" A 1

(ALT TO ITEM 115)
(BONDED)
– 115D CDPL1381-15 . PLACARD, "121HW" B 1
(ALT TO ITEM -115A)
(BONDED)

– 115E CDPL1381-16 . PLACARD, "122JW" C 1

(ALT TO ITEM -115B)
(BONDED)
120 CDPL767-25 . PLACARD, "TEMP SENSOR..."
A 1
(BONDED)
– ITEM NOT ILLUSTRATED

50-11-05 Page 10150

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1J 125 CDPL767-27 . PLACARD, "P13|P12" A 1

(BONDED)

– 125A CDPL768-24 . PLACARD, "P21|P22" C 1

(BONDED)

130 CDPL767-41 . PLACARD, "POSITIVE PRESSURE..." A 1

(BONDED)

135 CDPL767-43 . PLACARD, "FLIGHT DECK..." A 1

(BONDED)

140 CDPL767-47 . PLACARD, "CARGO LOADING" A 1

(BONDED)

– 145 BAC27WCH213 . PLACARD, "PALLET 21" B 1

(BONDED)

– 145A BAC27WCH214 . PLACARD, "PALLET 22" C 1

(BONDED)

– 145B CDPL1364-4 . PLACARD, "PALLET 21" B 1

(ALT TO ITEM -145)
(BONDED)

– 145C CDPL1364-5 . PLACARD, "PALLET 22" C 1

(ALT TO ITEM -145A)
(BONDED)

– 150 CDPL768-42 . PLACARD, "FIRE..." B,C 1

(BONDED)

– 155 CDM200-05 . DELETED D

(INCORRECT PN)

– 155A 398FR . TAPE, GLASS CLOTH AR

(V04963)
(BONDED)
(1")
(0.5")

160 C412410-009 . LINER, VERTICAL SIDEWALL A 1

(BONDED)

165 C412410-011 . LINER, ACCESS PANEL A 1

– 165A C412410-037 . LINER, ACCESS PANEL B 1

– 165B C412410-039 . LINER, ACCESS PANEL C 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10151

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

65

5
80
10A 15

70

60

20
85

45
50
75 40
25
55

35

30

A
50110501K01

Vertical Sidewall Panel Assembly

Figure 1K/GRAPHIC 50-11-05-99B-011-A01

50-11-05 Page 10152

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1K – 1 C412409-111 PANEL ASSY, VERTICAL SIDEWALL A RF

– 1A C412409-113 PANEL ASSY, VERTICAL SIDEWALL B RF

– 1B C412418-105 PANEL ASSY, SEC 43 VERTICAL C RF

SIDEWALL

– 1C C412418-107 PANEL ASSY, SEC 43 VERTICAL D RF

SIDEWALL

5 C412406-011 . EXTRUSION, SIDEWALL A,C 1

(BONDED)

– 5A C412406-013 . EXTRUSION, SIDEWALL B,D 1

(BONDED)

ATTACHING PARTS

– 10 BACN10YR3CD . DELETED A,B D

(INCORRECT PN)

10A BACN10YR3CM . NUT 10

15 NAS1515H3 . WASHER 10

20 BACS12FA3K8 . SCREW 10

***

– 22 926 . TAPE, TRANSFER AR

(V04963)
(BONDED)
(0.75")

– 22A 9485PC . TAPE, TRANSFER AR

(V04963)
(BONDED)
(1")
(OPT TO ITEM -22)

25 C412413-061 . STRIP, COVER 1

(BONDED)

30 C412413-062 . STRIP, COVER 1

(BONDED)

35 C412413-063 . STRIP, COVER A,C 1

(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10153

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1K – 35A C412413-064 . STRIP, COVER B,D 1

(BONDED)

– 37 SNS512AF . DELETED D
(INCORRECT PN)

– 37A SNS512AF0625200 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

– 38 CDM200-05 . DELETED D
(INCORRECT PN)

– 38A 398FR . TAPE, GLASS CLOTH AR

(V04963)
(BONDED)
(1")
(0.5")

40 C412411-009 . BLOW IN PANEL A 1

– 40A C412411-011 . BLOW IN PANEL B 1

– 40B C412419-9 . BLOW IN PANEL C 1

– 40C C412419-11 . DELETED D D

– 40D C412411-009 . BLOW IN PANEL C 1

(OPT TO ITEM -40B)

45 C412410-015 . LINER, VERTICAL SIDEWALL A,C 1

(BONDED)

– 45A C412410-017 . LINER, VERTICAL SIDEWALL B,D 1

(BONDED)

50 C412414-015 . GRILL A,C 1

– 50A C412414-017 . GRILL B,D 1

55 C412410-083 . LINER, VERTICAL SIDEWALL A,C 1

(BONDED)

– 55A C412410-087 . LINER, VERTICAL SIDEWALL B,D 1

(BONDED)

60 BAC27WCH277-121 . PLACARD, "121FW" A,C 1

(BONDED)
(TRUE PN BAC27WCH277-121FW)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10154

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1K – 60A BAC27WCH277-121 . PLACARD, "121GW" B,D 1

(BONDED)
(TRUE PN BAC27WCH277-121GW)

– 60B CDPL1379-11 . PLACARD, "121FW" A,C 1

(ALT TO ITEM 60)
(BONDED)

– 60C CDPL1379-12 . PLACARD, "121GW" B,D 1

(ALT TO ITEM -60A)
(BONDED)

65 BAC27WCH212 . PLACARD, "PALLET 13" A,C 1

(BONDED)

– 65A BAC27WCH213 . PLACARD, "PALLET 21" B 1

(BONDED)

– 65B CDPL1364-3 . PLACARD, "PALLET 13" A,C 1

(ALT TO ITEM 65)
(BONDED)

– 65C CDPL1364-4 . PLACARD, "PALLET 21" B 1

(ALT TO ITEM -65A)
(BONDED)

– 65D BAC27WCH213 . DELETED D D

70 CDPL767-15 . PLACARD, "21L" A,C 1

(BONDED)

– 70A CDPL767-31 . PLACARD, "22L" B 1

(BONDED)
– 70B CDPL767-31 . DELETED D D

75 BAC27WCH245 . PLACARD, "22L|21L" A,C 1

(BONDED)

– 75A CDPL767-29 . PLACARD, "23L" B,D 1

(BONDED)

– 75B CDPL1362-2 . PLACARD, "22L|21L" A,C 1

(ALT TO ITEM 75)
(BONDED)

80 BAC27WCH118 . PLACARD, "STA|600" A,C 1

(BONDED)

– 80A CDPL767-33 . PLACARD, "|STA 700" B 1

(BONDED)
– ITEM NOT ILLUSTRATED

50-11-05 Page 10155

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1K – 80B CDPL1361-2 . PLACARD, "STA|600" A,C 1

(ALT TO ITEM 80)
(BONDED)

– 80C CDPL767-33 . DELETED D D

85 BAC27WCH224 . PLACARD, "P21|P13" A,C 1

(BONDED)

– 85A CDPL767-25 . PLACARD, "TEMP SENSOR..." B,D 1

(BONDED)

– 85B CDPL1366-2 . PLACARD, "P21|P13" A,C 1

(ALT TO ITEM 85)
(BONDED)

– 90 C412419-511 . DECOMPRESSION BLOW, SUBASSY D 1

– 95 BAC27WCH213 . . PLACARD, "PALLET 21" D 1

(BONDED)

– 95A CDPL1364-4 . . PLACARD, "PALLET 21" D 1

(ALT TO ITEM -95)
(BONDED)

– 100 CDPL767-31 . . PLACARD, "22L" D 1

(BONDED)

– 105 CDPL767-33 . . PLACARD, "|STA 700" D 1

(BONDED)

– 110 C412419-11 . . BLOW IN PANEL D 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10156

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 COMPONENT MAINTENANCE MANUAL
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10A
15

20
45

65 90
55

75

80

50

70

85 30

40

60
25
35
50110501L01

A
Vertical Sidewall Panel Assembly
Figure 1L/GRAPHIC 50-11-05-99B-012-A01

50-11-05 Page 10158

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1L – 1 C412409-115 PANEL ASSY, VERTICAL SIDEWALL A RF

– 1A C412418-109 PANEL ASSY, SEC 43 VERTICAL B RF

SIDEWALL

5 C412406-015 . EXTRUSION, SIDEWALL 1

(BONDED)

ATTACHING PARTS

– 10 BACN10YR3CD . DELETED D
(INCORRECT PN)

10A BACN10YR3CM . NUT 9

15 NAS1515H3 . WASHER 9

20 BACS12FA3K8 . SCREW 9

***

25 C412413-062 . STRIP, COVER 1

(BONDED)

30 C412413-061 . STRIP, COVER 1

(BONDED)

35 C412413-065 . STRIP, COVER 1

(BONDED)

40 C412413-073 . STRIP, COVER 1

(BONDED)

45 C412413-074 . STRIP, COVER 1

(BONDED)

50 C412413-075 . STRIP, COVER 1

(BONDED)

– 51 926 . TAPE, TRANSFER AR

(V04963)
(BONDED)
(0.75")

– 51A 9485PC . TAPE, TRANSFER AR

(V04963)
(BONDED)
(1")
(OPT TO ITEM -51)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10159

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1L – 52 SNS512AF . DELETED D
(INCORRECT PN)

– 52A SNS512AF0625200 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

– 53 CDM200-05 . DELETED D
(INCORRECT PN)

– 53A 398FR . TAPE, GLASS CLOTH AR

(V04963)
(BONDED)
(0.5")
(1")

55 C412411-013 . BLOW IN PANEL A 1

– 55A C412419-13 . DELETED B D

60 C412411-015 . BLOW IN PANEL A 1

– 60A C412419-15 . DELETED B D

65 C412411-005 . BLOW OUT PANEL 1

70 C412410-019 . LINER, VERTICAL SIDEWALL 1

(BONDED)

75 BAC27WCH277-121 . PLACARD, "121HW" 1

(BONDED)
(TRUE PN BAC27WCH277-121HW)

– 75A CDPL1379-14 . PLACARD, "121HW" 1

(ALT TO ITEM 75)
(BONDED)

80 BAC27WCH214 . PLACARD, "PALLET 22" A 1

(BONDED)

– 80A CDPL1364-5 . PLACARD, "PALLET 22" A 1

(ALT TO ITEM 80)
(BONDED)

– 80B BAC27WCH214 . DELETED B D

85 CDPL767-21 . PLACARD, "24L|" A 1

(BONDED)

– 85A CDPL767-21 . DELETED B D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10160

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1L 90 BAC27WCH225 . PLACARD, "P22|P21" A 1

(BONDED)

– 90A CDPL1366-3 . PLACARD, "P22|P21" A 1

(ALT TO ITEM 90)
(BONDED)

– 90B BAC27WCH225 . DELETED B D

– 95 C412419-513 . DECOMPRESSION BLOW, SUBASSY B 1

– 100 BAC27WCH225 . . PLACARD, "P22|P21" B 1

(BONDED)

– 100A CDPL1366-3 . . PLACARD, "P22|P21" B 1

(ALT TO ITEM -100)
(BONDED)

– 105 C412419-13 . . BLOW IN PANEL B 1

– 110 C412419-515 . DECOMPRESSION BLOW, SUBASSY B 1

– 115 BAC27WCH214 . . PLACARD, "PALLET 22" B 1

(BONDED)

– 115A CDPL1364-5 . . PLACARD, "PALLET 22" B 1

(ALT TO ITEM -115)
(BONDED)

– 120 CDPL767-21 . . PLACARD, "24L|" B 1

(BONDED)

– 125 C412419-15 . . BLOW IN PANEL B 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10161

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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45

A
5

25

15

10A

20

40

35

30

50110501M01

Vertical Sidewall Panel Assembly

Figure 1M/GRAPHIC 50-11-05-99B-013-A01

50-11-05 Page 10162

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1M – 1 C412409-118 PANEL ASSY, VERTICAL SIDEWALL A RF

– 1A C412409-117 PANEL ASSY, VERTICAL SIDEWALL B RF

– 3 SNS512AF0625200 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

5 C412406-046 . EXTRUSION, SIDEWALL A 1

(BONDED)

– 5A C412406-045 . EXTRUSION, SIDEWALL B 1

(BONDED)

ATTACHING PARTS

– 10 BACN10YR3CD . DELETED D
(INCORRECT PN)

10A BACN10YR3CM . NUT 5

15 NAS1515H3 . WASHER 5

20 BACS12FA3K8 . SCREW 5

***

25 C412407-055 . STRIP, DOUBLER A 1

(BONDED)

– 25A C412413-055 . STRIP, DOUBLER B 1

(BONDED)

– 27 926 . TAPE, TRANSFER AR

(V04963)
(BONDED)

– 27A 9485PC . TAPE, TRANSFER AR

(V04963)
(BONDED)
(OPT TO ITEM -27)

30 C412410-022 . LINER, VERTICAL SIDEWALL A 1

– 30A C412410-021 . LINER, VERTICAL SIDEWALL B 1

35 BAC27WCH276-122 . PLACARD, "122KW" A 1

(BONDED)
(TRUE PN BAC27WCH276-122KW)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10163

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1M – 35A BAC27WCH277-121 . PLACARD, "121JW" B 1

(BONDED)
(TRUE PN BAC27WCH277-121JW)

– 35B CDPL1381-17 . PLACARD, "122KW" A 1

(ALT TO ITEM 35)
(BONDED)

– 35C CDPL1379-15 . PLACARD, "121JW" B 1

(ALT TO ITEM -35A)
(BONDED)

40 CDPL768-36 . PLACARD, "24R |" A 1

(BONDED)

– 40A CDPL767-23 . PLACARD, "24L |" B 1

(BONDED)

45 CDPL768-26 . PLACARD, "P22 |" A 1

(BONDED)

– 45A CDPL767-1 . PLACARD, "P22 |" B 1

(BONDED)

– 50 BAC27WCH209 . PLACARD, "STA 800 |" B 1

(BONDED)

– 50A CDPL1366-9 . PLACARD, "STA 800 |" B 1

(ALT TO ITEM -50)
(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10164

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 COMPONENT MAINTENANCE MANUAL
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60A

65

C
45
B
A
150 100

140
B

130
145
70

105

120

115

110

125
80

75

90

85
50110501N01

A
Vertical Sidewall Panel Assembly
(Sheet 1 of 2)
Figure 1N/GRAPHIC 50-11-05-99B-014-A01

50-11-05 Page 10166

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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20

15

15

10

B
TYPICAL

35
30

40

25

C
50110501N02

Vertical Sidewall Panel Assembly

(Sheet 2 of 2)
Figure 1N/GRAPHIC 50-11-05-99B-014-A01

50-11-05 Page 10167

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 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1N – 1 C412416-125 PANEL ASSY, SEC 43 VERTICAL A RF

SIDEWALL

– 1A C412418-111 PANEL ASSY, SEC 43 VERTICAL B RF

SIDEWALL

5 C412413-056 . LANYARD, CARGO ACCESS PANEL 2

ATTACHING PARTS

10 MS16535-134 . RIVET 2

15 10155610 . WASHER, NYLON 4

(V86928)
(TRUE PN 10/15/5610)

***

20 C412413-058 . HOOK FASTENER 2

(BONDED)

25 C412406-012 . EXTRUSION, SIDEWALL 1

(BONDED)

ATTACHING PARTS

30 BACN10YR3CM . NUT 10

35 NAS1515H3 . WASHER 10

40 BACS12FA3K8 . SCREW 10

***

45 CDSP1239-501 . QUARTER TURN FASTENER ASSY 36

– 50 CDSP1239-1 . . SLEEVE 1

– 55 CDSP1239-3 . . STUD 1

– 60 C412901-003 . RETAINER 36
(OPT TO ITEM 60A)

60A C412901-5 . RETAINER 36

65 C412413-009 . STRIP, DOUBLER 1

(BONDED)

70 C412413-011 . STRIP, DOUBLER 1

(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10169

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1N 75 C412413-020 . STRIP, DOUBLER 1

(BONDED)

80 C412413-048 . STRIP, COVER 1

(BONDED)

85 C412413-071 . STRIP, COVER 1

(BONDED)

90 C412413-072 . STRIP, COVER 1

(BONDED)

– 95 SNS512AF . DELETED D
(INCORRECT PN)

– 95A SNS512AF0625200 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

100 BAC27WCH102 . PLACARD, "P13|P21" 1

(BONDED)

– 100A CDPL1366-1 . PLACARD, "P13|P21" 1

(ALT TO ITEM 100)
(BONDED)

105 BAC27WCH105 . PLACARD, "21R|22R" 1

(BONDED)

– 105A CDPL1362-9 . PLACARD, "21R|22R" 1

(ALT TO ITEM 105)
(BONDED)

110 BAC27WCH118 . PLACARD, "STA|600" A 1

(BONDED)

– 110A CDPL1361-2 . PLACARD, "STA|600" A 1

(ALT TO ITEM 110)
(BONDED)

– 110B BAC27WCH118 . DELETED B D

115 BAC27WCH212 . PLACARD, "PALLET 13" A 1

(BONDED)

– 115A CDPL1364-3 . PLACARD, "PALLET 13" A 1

(ALT TO ITEM 115)
(BONDED)

– 115B BAC27WCH212 . DELETED B D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10170

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1N 120 BAC27WCH276-122 . PLACARD, "122GW" 1

(BONDED)
(TRUE PN BAC27WCH276-122GW)

– 120A CDPL1381-14 . PLACARD, "122GW" 1

(ALT TO ITEM 120)
(BONDED)

125 CDPL768-4 . PLACARD, "|21R" A 1

(BONDED)

– 125A CDPL768-4 . DELETED B D

130 CDPL768-42 . PLACARD, "FIRE..." 1

(BONDED)

– 135 CDM200-05 . DELETED D

(INCORRECT PN)

– 135A 398FR . TAPE, GLASS CLOTH AR

(V04963)
(BONDED)
(1")
(0.5")

– 137 926 . TAPE, TRANSFER AR

(V04963)
(BONDED)
(1")

– 137A 9485PC . TAPE, TRANSFER AR

(V04963)
(BONDED)
(0.75")
(OPT TO ITEM -137)

140 C412410-033 . GRILL, DECOMPRESSION 1

145 C412411-019 . BLOW IN PANEL A 1

– 145A C412419-19 . DELETED B D

150 C412410-035 . LINER, ACCESS PANEL 1

– 155 C412419-519 . DECOMPRESSION BLOW, SUBASSY B 1

– 160 CDPL768-4 . . PLACARD, "|21R" B 1

(BONDED)

– 165 BAC27WCH118 . . PLACARD, "STA|600" B 1

(BONDED)
– ITEM NOT ILLUSTRATED

50-11-05 Page 10171

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1N – 165A CDPL1361-2 . . PLACARD, "STA|600" B 1

(ALT TO ITEM -165)
(BONDED)

– 170 BAC27WCH212 . . PLACARD, "PALLET 13" B 1

(BONDED)

– 170A CDPL1364-3 . . PLACARD, "PALLET 13" B 1

(ALT TO ITEM -170)
(BONDED)

– 175 C412419-19 . . BLOW IN PANEL B 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10172

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 COMPONENT MAINTENANCE MANUAL
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A
120

95

135
140
C

75 90

85

100
65

110

105

60A
125
45

70
130
50110501P01

Vertical Sidewall Panel Assembly

(Sheet 1 of 2)
Figure 1P/GRAPHIC 50-11-05-99B-015-A01

50-11-05 Page 10174

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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20

15

5
15

10

25

30
35

40
50110501P02

Vertical Sidewall Panel Assembly

(Sheet 2 of 2)
Figure 1P/GRAPHIC 50-11-05-99B-015-A01

50-11-05 Page 10175

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COMPONENT MAINTENANCE MANUAL
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Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1P – 1 C412416-131 PANEL ASSY, SEC 46 VERTICAL RF

SIDEWALL

5 C412413-056 . LANYARD, CARGO ACCESS PANEL 1

ATTACHING PARTS

10 MS16535-134 . RIVET 1

15 5010-10-15 . WASHER, NYLON 2

(V86928)

***

20 C412413-058 . HOOK FASTENER 1

(BONDED)

– 22 SNS512AF0625200 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

25 C412406-041 . EXTRUSION, SIDEWALL 1

(BONDED)

ATTACHING PARTS

30 BACN10YR3CM . NUT 10

35 NAS1515H3 . WASHER 10

40 BACS12FA3K8 . SCREW 10

***

45 CDSP1239-501 . QUARTER TURN FASTENER ASSY 30

– 50 CDSP1239-1 . . SLEEVE 1

– 55 CDSP1239-3 . . STUD 1

– 60 C412901-003 . RETAINER 30
(OPT TO ITEM 60A)

60A C412901-5 . RETAINER 30

– 63 926 . TAPE, TRANSFER AR

(V04963)
(BONDED)
(0.75")

– ITEM NOT ILLUSTRATED

50-11-05 Page 10177

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1P – 63A 9485PC . TAPE, TRANSFER AR

(V04963)
(BONDED)
(1")
(OPT TO ITEM -63)

65 C412413-033 . STRIP, DOUBLER 1

(BONDED)

70 C412413-034 . STRIP, DOUBLER 1

(BONDED)

75 C412413-035 . STRIP, DOUBLER 1

(BONDED)

– 80 SNS512AF . DELETED D
(INCORRECT PN)

– 80A SNS512AF125250 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

85 BAC27WCH270-151 . PLACARD, "151AW" 1

(BONDED)
(TRUE PN BAC27WCH270-151AW)

– 85A CDPL1380-1 . PLACARD, "151AW" 1

(ALT TO ITEM 85)
(BONDED)

90 CDPL777-24 . PLACARD, "|" 1

(BONDED)

95 CDPL768-2 . PLACARD, "|" 1

(BONDED)

100 BAC27WCH351 . PLACARD, "PALLET 31" 1

(BONDED)

– 100A CDPL1364-7 . PLACARD, "PALLET 31" 1

(ALT TO ITEM 100)
(BONDED)

105 BAC27WCH249 . PLACARD, "32L | 31L" 1

(BONDED)

– 105A CDPL1362-4 . PLACARD, "32L | 31L" 1

(ALT TO ITEM 105)
(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10178

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1P 110 CDPL776-33 . PLACARD, "P813 PANEL" 1

(BONDED)

– 115 CDM200-05 . DELETED D

– 115A 398FR . TAPE, GLASS CLOTH AR

(V04963)
(BONDED)
(0.5")
(1")

120 C412411-029 . VENT PANEL, OUTBD 1

DECOMPRESSION

125 C412410-045 . LINER, VERTICAL SIDEWALL 1

130 C412410-043 . LINER, VERTICAL SIDEWALL 1

135 C412410-041 . LINER, VERTICAL SIDEWALL 1

140 C412414-041 . LINER, VERTICAL SIDEWALL 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10179

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

55

80
70

C 85
40
75

25

35
30
50110501Q01

Vertical Sidewall Panel Assembly

(Sheet 1 of 2)
Figure 1Q/GRAPHIC 50-11-05-99B-016-A01

50-11-05 Page 10180

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

22

10 15 5 20

B
60
45

65

50
50110501Q02

D
C

Vertical Sidewall Panel Assembly

(Sheet 2 of 2)
Figure 1Q/GRAPHIC 50-11-05-99B-016-A01

50-11-05 Page 10181

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Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1Q – 1 C412409-139 PANEL ASSY, SEC 46 VERTICAL A RF

SIDEWALL
SUPSD BY ITEM -1A

– 1A C412417-139 PANEL ASSY, VERTICAL SIDEWALL B RF

SUPSDS ITEM -1

– 1B C412418-119 PANEL ASSY, SEC 47 VERTICAL C RF

SIDEWALL

5 C412406-029 . EXTRUSION, SIDEWALL 1

(BONDED)

ATTACHING PARTS

10 BACN10YR3CM . NUT 7

15 NAS1515H3 . WASHER 7

20 BACS12FA3K8 . SCREW 7

***

22 852Z0440-9 . LINER, WATER DAM B,C 1

(V81205)
(BONDED)

25 C412413-066 . STRIP, COVER 1

(BONDED)

30 C412413-067 . STRIP, DOUBLER 1

(BONDED)

35 C412413-068 . STRIP, COVER 1

(BONDED)

40 C412411-503 . PANEL ASSY, DECOMPRESSION A,B 1

(BONDED)

– 40A C412419-503 . PANEL ASSY, DECOMPRESSION C 1

(BONDED)

45 C412405-057 . . PANEL, INSULATION 1

(BONDED)

– 46 BAC27WCH270-151 . . PLACARD, "151GW" C 1

(BONDED)
(TRUE PN BAC27WCH270-151GW)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10183

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1Q – 46A CDPL1380-7 . . PLACARD, "151GW" C 1

(ALT TO ITEM -46)
(BONDED)

– 47 BAC27WCH369 . . PLACARD, "|P42" C 1

(BONDED)

– 47A CDPL1365-6 . . PLACARD, "|P42" C 1

(ALT TO ITEM -47)
(BONDED)

– 48 CDPL776-1 . . PLACARD, "|43L" C 1

(BONDED)

50 C412411-025 . . VENT PANEL, INBD A,B 1

DECOMPRESSION

– 50A C412419-25 . . VENT PANEL, INBD C 1

DECOMPRESSION

– 53 926 . . TAPE, TRANSFER AR

(V04963)
(BONDED)

– 53A 9485PC . . TAPE, TRANSFER AR

(V04963)
(BONDED)
(OPT TO ITEM -53)

55 C412411-505 . PANEL ASSY, DECOMPRESSION 1

(BONDED)

60 C412405-059 . . PANEL, INSULATION 1

(BONDED)

65 C412411-023 . . VENT PANEL, OUTBD 1

DECOMPRESSION

– 67 926 . . TAPE, TRANSFER AR

(V04963)
(BONDED)

– 67A 9485PC . . TAPE, TRANSFER AR

(V04963)
(BONDED)
(OPT TO ITEM -67)

70 C412410-057 . GRILL, PANEL 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10184

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1Q 75 BAC27WCH270-151 . PLACARD, "151GW" A,B 1

(BONDED)
(TRUE PN BAC27WCH270-151GW)

– 75A CDPL1380-7 . PLACARD, "151GW" A,B 1

(ALT TO ITEM 75)
(BONDED)

– 75B BAC27WCH270-151 . DELETED C D

80 BAC27WCH369 . PLACARD, "|P42" A,B 1

(BONDED)

– 80A CDPL1365-6 . PLACARD, "|P42" A,B 1

(ALT TO ITEM 80)
(BONDED)

– 80B BAC27WCH369 . DELETED C D

85 CDPL776-1 . PLACARD, "|43L" A,B 1

(BONDED)

– 85A CDPL776-1 . DELETED C D

– 90 SNS512AF . DELETED D
(INCORRECT PN)

– 90A SNS512AF0625200 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

– 95 CDM200-05 . DELETED D
(INCORRECT PN)

– 95A 398FR . TAPE, GLASS CLOTH AR

(V04963)
(BONDED)
(0.5")
(1")

– 100 CDM200-03 . DELETED D

(INCORRECT PN)

– 100A 926 . TAPE, TRANSFER AR

(V04963)
(BONDED)
(0.75")

– ITEM NOT ILLUSTRATED

50-11-05 Page 10185

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1Q – 100B 9485PC . TAPE, TRANSFER AR

(V04963)
(BONDED)
(1")
(OPT TO ITEM -100A)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10186

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50-11-05 Page 10187

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 COMPONENT MAINTENANCE MANUAL
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A 5

15
20
35

10A

45

50

25

40

30
50110501R01

Vertical Sidewall Panel Assembly

Figure 1R/GRAPHIC 50-11-05-99B-017-A01

50-11-05 Page 10188

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1R – 1 C412409-143 PANEL ASSY, VERTICAL SIDEWALL RF

– 3 SNS512AF0625200 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

5 C412406-025 . EXTRUSION, SIDEWALL 1

(BONDED)

ATTACHING PARTS

– 10 BACN10YR3CD . DELETED D
(INCORRECT PN)

10A BACN10YR3CM . NUT 6

15 NAS1515H3 . WASHER 6

20 BACS12FA3K8 . SCREW 6

***

25 C412411-037 . VENT PANEL, OUTBD 1

DECOMPRESSION

30 C412410-065 . LINER, VERTICAL SIDEWALL 1

(BONDED)

35 C412414-065 . LINER, VERTICAL SIDEWALL 1

(BONDED)

– 37 926 . TAPE, TRANSFER AR

(V04963)
(BONDED)
(0.75")

– 37A 9485PC . TAPE, TRANSFER AR

(V04963)
(BONDED)
(1")
(OPT TO ITEM -37)

40 BAC27WCH269-152 . PLACARD, "152BW" 1

(BONDED)
(TRUE PN BAC27WCH269-152BW)

– 40A CDPL1382-4 . PLACARD, "152BW" 1

(ALT TO ITEM 40)
(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10189

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1R 45 CDPL776-3 . PLACARD, "STA 1400" 1

(BONDED)

50 CDPL777-6 . PLACARD, "32R" 1

(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10190

Oct 09/23
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50-11-05 Page 10191

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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A 25
10 5
15

45

20

35

30

A 40
50110501S01

Vertical Sidewall Panel Assembly

Figure 1S/GRAPHIC 50-11-05-99B-018-A01

50-11-05 Page 10192

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1S – 1 C412409-147 PANEL ASSY, VERTICAL SIDEWALL A RF

SUPSD BY ITEM -1A

– 1A C412417-147 PANEL ASSY, VERTICAL SIDEWALL B RF

SUPSDS ITEM -1

– 1B C412409-159 PANEL ASSY, VERTICAL SIDEWALL C RF

– 1C C412409-121 PANEL ASSY, VERTICAL SIDEWALL D RF

– 1D C412409-173 PANEL ASSY, SEC 41 VERTICAL E RF

SIDEWALL

5 C412406-019 . EXTRUSION, SIDEWALL A,B,D,E 1

(BONDED)

– 5A C412406-003 . EXTRUSION, SIDEWALL C 1

(BONDED)

ATTACHING PARTS

10 BACN10YR3CM . NUT A,B,D,E 3

– 10A BACN10YR3CM . NUT C 4

15 NAS1515H3 . WASHER A,B,D,E 3

– 15A NAS1515H3 . WASHER C 4

20 BACS12FA3K8 . SCREW A,B,D,E 3

– 20A BACS12FA3K8 . SCREW C 4

***

25 852Z0440-4 . LINER, WATER DAM B 1

(V81205)
(BONDED)

30 C412413-085 . STRIP, DOUBLER A,B 1

(BONDED)

– 30A C412413-081 . STRIP, DOUBLER D 1

(BONDED)

– 30B C412414-70 . STRIP, DOUBLER E 1

(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10193

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1S – 33 926 . TAPE, TRANSFER A-D AR

(V04963)
(BONDED)
(0.75")

– 33A 9485PC . TAPE, TRANSFER A-D AR

(V04963)
(BONDED)
(1")
(OPT TO ITEM -33)

– 33B 9485PC . TAPE, TRANSFER E AR

(V04963)
(BONDED)
(1")

35 C412410-069 . LINER, VERTICAL SIDEWALL A,B 1

– 35A C412414-049 . LINER, VERTICAL SIDEWALL C 1

– 35B C412410-029 . LINER, VERTICAL SIDEWALL D 1

– 35C C412404-17 . LINER, VERTICAL SIDEWALL E 1

40 BAC27WCH269-152 . PLACARD, "152DW" A,B 1

(BONDED)
(TRUE PN BAC27WCH269-152DW)

– 40A BAC27WCH270-151 . PLACARD, "151CW" C 1

(BONDED)
(TRUE PN BAC27WCH270-151CW)

– 40B BAC27WCH276-122 . PLACARD, "122CW" D 1

(BONDED)
(TRUE PN BAC27WCH276-122CW)

– 40C CDPL1381-7 . PLACARD, "122CW" E 1

(BONDED)

– 40E CDPL1382-8 . PLACARD, "152DW" A,B 1

(ALT TO ITEM 40)
(BONDED)

– 40F CDPL1380-3 . PLACARD, "151CW" C 1

(ALT TO ITEM -40A)
(BONDED)

– 40G CDPL1381-7 . PLACARD, "122CW" D 1

(ALT TO ITEM -40B)
(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10194

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1S 45 CDPL777-22 . PLACARD, "P32" A,B 1

(BONDED)

– 45A BAC27WCH352 . PLACARD, "PALLET 32" C 1

(BONDED)

– 45B BAC27WCH219 . PLACARD, "P11 I " D 1

(BONDED)

– 45C CDPL1365-2 . PLACARD, "P11 I " E 1

(BONDED)

– 45D CDPL1364-8 . PLACARD, "PALLET 32" C 1

(ALT TO ITEM -45A)
(BONDED)

– 45E CDPL1365-2 . PLACARD, "P11 I " D 1

(ALT TO ITEM -45B)
(BONDED)

– 50 CDPL776-21 . PLACARD, "33L" C 1

(BONDED)

– 55 SNS512AF . DELETED D
(INCORRECT PN)

– 55A SNS512AF0625200 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10195

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

10
50110501T01

Vertical Sidewall Vent Liner Assembly

Figure 1T/GRAPHIC 50-11-05-99B-019-A01

50-11-05 Page 10196

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1T – 1 C419408-101 VENT LINER, SEC 41 CARGO VSW A RF

– 1A C419408-103 VENT LINER, SEC 43 CARGO VSW B RF

– 1B C419408-105 VENT LINER, SEC 41 CARGO VSW C RF

– 1C C419408-107 VENT LINER, SEC 43 CARGO VSW D RF

– 1D C419408-109 VENT LINER, SEC 43 CARGO VSW E RF

– 1E C412410-079 VENT LINER, VERTICAL SIDEWALL F RF

– 1F C412410-081 VENT LINER, VERTICAL SIDEWALL G RF

– 1G C412410-085 VENT LINER, VERTICAL SIDEWALL H RF

– 1H C412410-089 VENT LINER, VERTICAL SIDEWALL J RF

– 1J C414408-101 VENT LINER, VERTICAL SIDEWALL K RF

– 1K C414408-105 VENT LINER, VERTICAL SIDEWALL L RF

– 1L C414408-107 VENT LINER, VERTICAL SIDEWALL M RF

– 1M C414408-109 VENT LINER, VERTICAL SIDEWALL N RF

5 BAC27WCH277-121 . PLACARD, "121HAW" A 1

(BONDED)
(TRUE PN BAC27WCH277-121HAW)

– 5A BAC27WCH277-121 . PLACARD, "121RAW" B 1

(BONDED)
(TRUE PN BAC27WCH277-121RAW)

– 5B BAC27WCH276-122 . PLACARD, "122BAW" C 1

(BONDED)
(TRUE PN BAC27WCH276-122BAW)

– 5C BAC27WCH276-122 . PLACARD, "122LAW" D 1

(BONDED)
(TRUE PN BAC27WCH276-122LAW)

– 5D BAC27WCH276-122 . PLACARD, "122MAW" E 1

(BONDED)
(TRUE PN BAC27WCH276-122MAW)

– 5E CDPL1379-27 . PLACARD, "121TAW" K 1

(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10197

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1T – 5F CDPL1381-20 . PLACARD, "122MAW" L 1

(BONDED)

– 5G CDPL1381-24 . PLACARD, "122NAW" M 1

(BONDED)

– 5H CDPL1379-13 . PLACARD, "121HAW" N 1

(BONDED)

– 5J CDPL1379-13 . PLACARD, "121HAW" A 1

(ALT TO ITEM 5)
(BONDED)

– 5K CDPL1379-22 . PLACARD, "121RAW" B 1

(ALT TO ITEM -5A)
(BONDED)

– 5L CDPL1381-3 . PLACARD, "122BAW" C 1

(ALT TO ITEM -5B)
(BONDED)

– 5M CDPL1381-18 . PLACARD, "122LAW" D 1

(ALT TO ITEM -5C)
(BONDED)

– 5N CDPL1381-20 . PLACARD, "122MAW" E 1

(ALT TO ITEM -5D)
(BONDED)

10 C419408-1 . PANEL, VERTICAL SIDEWALL LINER A,N 1

– 10A C419408-3 . PANEL, VERTICAL SIDEWALL LINER B,K 1

– 10B C419408-5 . PANEL, VERTICAL SIDEWALL LINER C 1

– 10C C419408-7 . PANEL, VERTICAL SIDEWALL LINER D,L 1

– 10D C419408-9 . PANEL, VERTICAL SIDEWALL LINER E,M 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10198

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 COMPONENT MAINTENANCE MANUAL
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30

A
35

25

165

155
40

65 125
80
120

130

65
105
115 110 100 95

75
20

5
15A 135
170
70

85
60B 15A 10
50110501U01

160
45
A

Vertical Sidewall Panel Assembly

Figure 1U/GRAPHIC 50-11-05-99B-020-A01

50-11-05 Page 10200

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1U – 1 C412416-105 PANEL ASSY, SEC 41 VERTICAL A RF

SIDEWALL

– 1A C412416-135 PANEL ASSY, VERTICAL SIDEWALL B RF

(SEE CMM 50-11-07 FOR DET)
SUPSD BY PN C412416-167

– 1B C412418-103 PANEL ASSY, VERTICAL SIDEWALL C RF

5 C412413-056 . LANYARD, CARGO ACCESS PANEL 1

ATTACHING PARTS

10 MS16535-134 . RIVET 1

– 15 5610-10-015 . DELETED D
(INCORRECT PN)

15A 10155610 . WASHER, NYLON 2

***

20 C412413-058 . HOOK FASTENER 1

(BONDED)

– 23 SNS512AF0625200 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

25 C412406-005 . EXTRUSION, SIDEWALL 1

(BONDED)

ATTACHING PARTS

30 BACN10YR3CM . NUT 9

35 NAS1515H3 . WASHER 9

40 BACS12FA3K8 . SCREW 9

***

45 CDSP1239-501 . QUARTER TURN FASTENER ASSY A,C 31

– 45A CDSP1239-501 . QUARTER TURN FASTENER ASSY B 32

– 50 CDSP1239-1 . . SLEEVE 1

– 55 CDSP1239-3 . . STUD 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10201

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1U – 60 C412901-003 . RETAINER A 31
(OPT TO ITEM 60B)

– 60A C412901-003 . RETAINER B 32

60B C412901-5 . RETAINER A,C 31

65 C412413-023 . STRIP, DOUBLER A,C 2

(BONDED)

– 65A C412413-029 . STRIP, DOUBLER B 1

(BONDED)

– 65B C412413-028 . STRIP, DOUBLER B 1

(BONDED)

70 C412413-001 . STRIP, DOUBLER A,C 1

(BONDED)

– 70A C412413-027 . STRIP, DOUBLER B 1

(BONDED)

75 C412413-025 . STRIP, COVER A,C 1

(BONDED)

– 75A C412413-045 . STRIP, COVER B 1

(BONDED)

80 C412413-026 . STRIP, COVER A,C 1

(BONDED)

– 80A C412413-046 . STRIP, COVER B 1

(BONDED)

85 C412413-089 . STRIP, COVER A,C 1

(BONDED)

– 85A C412413-090 . STRIP, COVER B 1

(BONDED)

– 90 SNS512AF . DELETED D
(INCORRECT PN)

– 90A SNS512AF125250 . TAPE, SILICONE FOAM A-C AR

(V12624)
(BONDED)
– 92 926 . TAPE, TRANSFER AR
(V04963)
(BONDED)
(0.75")
– ITEM NOT ILLUSTRATED

50-11-05 Page 10202

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1U – 92A 9485PC . TAPE, TRANSFER AR

(V04963)
(BONDED)
(1")
(OPT TO ITEM -87)

95 BAC27WCH277-121 . PLACARD, "121CW" A,C 1

(BONDED)
(TRUE PN BAC27WCH277-121CW)

– 95A BAC27WCH270-151 . PLACARD, "151DW" B 1

(BONDED)
(TRUE PN BAC27WCH270-151DW)

– 95B CDPL1379-6 . PLACARD, "121CW" A,C 1

(ALT TO ITEM 95)
(BONDED)

– 95C CDPL1380-4 . PLACARD, "151DW" B 1

(ALT TO ITEM -95A)
(BONDED)

100 BAC27WCH228 . PLACARD, "|12L" A 1

(BONDED)

– 100A CDPL776-15 . PLACARD, "41L|33L" B 1

(BONDED)

– 100B CDPL1367-6 . PLACARD, "|12L" A 1

(ALT TO ITEM 100)
(BONDED)

– 100C BAC27WCH228 . DELETED C D

105 CDPL767-13 . PLACARD, "13L" A,C 1

(BONDED)

110 BAC27WEC165 . PLACARD, "E/E COOLING AIR 1

FILTER"
(BONDED)

– 110A CDPL1365-10 . PLACARD, "E/E COOLING AIR 1

FILTER"
(ALT TO ITEM 110)
(BONDED)

115 BAC27WCH211 . PLACARD, "PALLET 12" A,C 1

(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10203

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1U – 115A CDPL1364-2 . PLACARD, "PALLET 12" A,C 1

(ALT TO ITEM 115)
(BONDED)

120 CDPL767-3 . PLACARD, "P12" A 1

(BONDED)

– 120A CDPL776-19 . PLACARD, "P41|P32" B 1

(BONDED)

– 120B CDPL767-3 . DELETED C D

125 BAC27WCH221 . PLACARD, "|P11" A,C 1

(BONDED)

– 125A CDPL1365-4 . PLACARD, "|P11" A,C 1

(ALT TO ITEM 125)
(BONDED)

130 BAC27WCH715 . PLACARD, "CAUTION..." A 1

(BONDED)

– 130A CDPL1385-3 . PLACARD, "CAUTION..." A 1

(ALT TO ITEM 130)
(BONDED)

– 130B BAC27WCH715 . DELETED C D

135 CDPL767-39 . PLACARD, "CAUTION..." A,C 1

(BONDED)

– 140 CDPL767-47 . PLACARD, "CARGO LOADING" B 1

(BONDED)

– 145 CDPL776-25 . PLACARD, "STA 1500|" B 1

(BONDED)

– 150 CDM200-05 . DELETED D

(INCORRECT PN)

– 150A 398FR . TAPE, GLASS CLOTH AR

(V04963)
(BONDED)
(0.5")
(1")
155 C412410-005 . LINER, VERTICAL SIDEWALL A,C 1
(BONDED)

– 155A C412414-007 . LINER, VERTICAL SIDEWALL B 1

(BONDED)
– ITEM NOT ILLUSTRATED

50-11-05 Page 10204

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1U 160 C412410-007 . LINER, VERTICAL SIDEWALL A,C 1

(BONDED)

– 160A C412410-051 . LINER, VERTICAL SIDEWALL B 1

(BONDED)

165 C412414-005 . GRILL, DECOMPRESSION A,C 1

– 165A C412410-053 . GRILL, DECOMPRESSION B 1

170 C412411-051 . BLOW IN PANEL A 1

– 170A C412411-047 . BLOW IN PANEL B 1

– 170B C412419-51 . DELETED C D

– 175 C412419-551 . DECOMPRESSION BLOW, SUBASSY C 1

– 180 CDPL767-3 . . PLACARD, "P12" C 1

(BONDED)

– 185 BAC27WCH715 . . PLACARD, "CAUTION..." C 1

(BONDED)

– 185A CDPL1385-3 . . PLACARD, "CAUTION..." C 1

(ALT TO ITEM -185)
(BONDED)

– 190 BAC27WCH228 . . PLACARD, "|12L" C 1

(BONDED)

– 190A CDPL1367-6 . . PLACARD, "|12L" C 1

(ALT TO ITEM -190)
(BONDED)

– 195 C412419-51 . . BLOW IN PANEL C 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10205

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

A 30 35

25

40
120
75

45

75 135

130

105

100

5 20
90
15 85
70 95

110
15 10
65A 50
125
50110501V01

A
Vertical Sidewall Panel Assembly
Figure 1V/GRAPHIC 50-11-05-99B-021-A01

50-11-05 Page 10206

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1V – 1 C412416-119 PANEL ASSY, SEC 41 VERTICAL RF

SIDEWALL

5 C412413-057 . LANYARD, CARGO ACCESS PANEL 1

ATTACHING PARTS

10 MS16535-134 . RIVET 1

15 5010-10-15 . WASHER, NYLON 2

(V86928)

***

20 C412413-058 . HOOK FASTENER 1

(BONDED)

– 22 SNS512AF0625200 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

25 C412406-044 . EXTRUSION, SIDEWALL 1

(BONDED)

ATTACHING PARTS

30 BACN10YR3CM . NUT 8

35 NAS1515H3 . WASHER 8

40 BACS12FA3K8 . SCREW 8

***

45 94639A567 . SPACER 1
(V3A054)
(BONDED)

50 CDSP1239-501 . QUARTER TURN FASTENER ASSY 24

– 55 CDSP1239-1 . . SLEEVE 1

– 60 CDSP1239-3 . . STUD 1

– 65 C412901-003 . RETAINER 24
(OPT TO ITEM 65A)

65A C412901-5 . RETAINER 24

– ITEM NOT ILLUSTRATED

50-11-05 Page 10207

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1V 70 C412413-005 . STRIP, DOUBLER 1

(BONDED)

75 C412413-024 . STRIP, DOUBLER 2

(BONDED)

– 80 SNS512AF . DELETED D
(INCORRECT PN)

– 80A SNS512AF125250 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

85 BAC27WCH276-122 . PLACARD, "122AW" 1

(BONDED)
(TRUE PN BAC27WCH276-122AW)

– 85A CDPL1381-2 . PLACARD, "122AW" 1

(ALT TO ITEM 85)
(BONDED)

90 BAC27TCH0371 . PLACARD, "11R" 1

(BONDED)

– 90A CDPL1367-7 . PLACARD, "11R" 1

(ALT TO ITEM 90)
(BONDED)

95 CDPL768-2 . PLACARD, "|" 1

(BONDED)

100 CDPL768-22 . PLACARD, "P11" 1

(BONDED)

105 CDPL768-38 . PLACARD, "FWD E/E COOLING..." 1

(BONDED)

110 CDPL777-24 . PLACARD, "|" 1

(BONDED)

– 115 CDM200-05 . DELETED D

(INCORRECT PN)

– 115A 398FR . TAPE, GLASS CLOTH AR

(V04963)
(BONDED)
(0.5")
(1")

– ITEM NOT ILLUSTRATED

50-11-05 Page 10208

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX
FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1V – 117 926 . TAPE, TRANSFER AR

(V04963)
(BONDED)
(0.75")

– 117A 9485PC . TAPE, TRANSFER AR

(V04963)
(BONDED)
(1")
(OPT TO ITEM -117)

120 C412411-003 . BLOW OUT PANEL 1

125 C412410-023 . LINER, VERTICAL SIDEWALL 1

(BONDED)

130 C412410-027 . LINER, VERTICAL SIDEWALL 1

(BONDED)

135 C412410-025 . LINER, ACCESS PANEL 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10209

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

25

30
35

75
70 105
90

65
5
20
120
15
40

150 115 110

60B

45

100

10
160 15

155

80 85
50110501W01

Vertical Sidewall Panel Assembly

Figure 1W/GRAPHIC 50-11-05-99B-022-A01

50-11-05 Page 10210

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1W – 1 C412416-133 PANEL ASSY, SEC 46 VERTICAL A RF

SIDEWALL

– 1A C412416-151 DELETED B D

– 1B C412418-113 PANEL ASSY, SEC 46 VERTICAL C RF

SIDEWALL

5 C412413-056 . LANYARD, CARGO ACCESS PANEL 1

ATTACHING PARTS

10 MS16535-134 . RIVET 1

15 10155610 . WASHER, NYLON 2

(V86928)
(TRUE PN 10/15/5610)

***

20 C412413-058 . HOOK FASTENER 1

(BONDED)

– 22 SNS512AF0625200 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

25 C412406-025 . EXTRUSION, SIDEWALL A,C 1

(BONDED)

– 25A C412406-030 . DELETED B D

ATTACHING PARTS

30 BACN10YR3CM . NUT A,C 6

– 30A BACN10YR3CM . DELETED B D

35 NAS1515H3 . WASHER A,C 6

– 35A NAS1515H3 . DELETED B D

40 BACS12FA3K8 . SCREW A,C 6

– 40A BACS12FA3K8 . DELETED B D

***

45 CDSP1239-501 . QUARTER TURN FASTENER ASSY A,C 29

– ITEM NOT ILLUSTRATED

50-11-05 Page 10211

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1W – 45A CDSP1239-501 . DELETED B D

– 50 CDSP1239-1 . . SLEEVE 1

– 55 CDSP1239-3 . . STUD 1

– 60 C412901-003 . RETAINER A,C 29

(OPT TO ITEM 60B)

– 60A C412901-003 . DELETED B D

60B C412901-5 . RETAINER A,C 29

65 C412413-030 . STRIP, DOUBLER A,C 1

(BONDED)

– 65A C412413-037 . DELETED B D

70 C412413-031 . STRIP, DOUBLER A,C 1

(BONDED)

– 70A C412407-036 . DELETED B D

75 C412413-032 . STRIP, DOUBLER A,C 1

(BONDED)

– 75A C412407-038 . DELETED B D

80 C412413-094 . STRIP, COVER A,C 1

(BONDED)

– 80A C412413-077 . DELETED B D

85 C412413-096 . STRIP, COVER A,C 1

(BONDED)

– 85A C412407-076 . DELETED B D

90 C412413-097 . STRIP, COVER A,C 1

(BONDED)

– 90A C412413-095 . DELETED B D

– 95 SNS512AF . DELETED D
(INCORRECT PN)

– 95A SNS512AF125250 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10212

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1W 100 BAC27WCH270-151 . PLACARD, "151BW" A,C 1

(BONDED)
(TRUE PN BAC27WCH270-151BW)

– 100A BAC27WCH269 . DELETED B D

– 100B CDPL1380-2 . PLACARD, "151BW" A,C 1

(ALT TO ITEM 100)
(BONDED)

105 BAC27WCH355 . PLACARD, "P32|P31" A,C 1

(BONDED)

– 105A CDPL1366-6 . PLACARD, "P32|P31" A,C 1

(ALT TO ITEM 105)
(BONDED)

110 CDPL776-3 . PLACARD, "|STA 1400" A,C 1

(BONDED)

115 CDPL776-23 . PLACARD, "|32L" A 1

(BONDED)

– 115A CDPL776-23 . DELETED C D

120 BAC27WEC163 . PLACARD, "E/E COOLING SUPPLY A,C 1

FAN"
(BONDED)

– 120A CDPL1365-9 . PLACARD, "E/E COOLING SUPPLY A,C 1

FAN"
(ALT TO ITEM 120)
(BONDED)

– 125 BAC27WCH353 . DELETED B D

– 130 BAC27WCH363 . DELETED B D

– 135 CDPL777-12 . DELETED B D

– 140 CDPL777-30 . DELETED B D

– 145 CDM200-05 . DELETED D

(INCORRECT PN)

– 145A 398FR . TAPE, GLASS CLOTH AR

(V04963)
(BONDED)
(0.5")
(1")

– ITEM NOT ILLUSTRATED

50-11-05 Page 10213

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1W – 147 926 . TAPE, TRANSFER AR

(V04963)
(BONDED)
(1")

– 147A 9485PC . TAPE, TRANSFER AR

(V04963)
(BONDED)
(1")
(OPT TO ITEM -147)

150 C412410-049 . GRILL, DECOMPRESSION A,C 1

– 150A C412410-075 . DELETED B D

155 C412411-027 . VENT PANEL, INBD A 1

DECOMPRESSION

– 155A C412411-035 . DELETED B D

– 155B C412419-27 . DELETED C D

160 C412410-047 . LINER, ACCESS PANEL A,C 1

(BONDED)

– 160A C412410-073 . DELETED B D

– 165 C412419-527 . DECOMPRESSION BLOW, SUBASSY C 1

– 170 CDPL776-23 . . PLACARD, "|32L" C 1

(BONDED)

– 175 C412419-27 . . VENT PANEL, INBD C 1

DECOMPRESSION
(BONDED)

– ITEM NOT ILLUSTRATED

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30 35 25

150
65
90 40

125
85
75
70 120
160
105
135
100 130

5 20 140

110
110 80
15A

115

165
60A

15A
155
10
45
A
50110501X01

Vertical Sidewall Panel Assembly

Figure 1X/GRAPHIC 50-11-05-99B-023-A01

50-11-05 Page 10216

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1X – 1 C412416-141 PANEL ASSY, SEC 46 VERTICAL A RF

SIDEWALL

– 1A C412418-121 PANEL ASSY, SEC 46 VERTICAL B RF

SIDEWALL

5 C412413-056 . LANYARD, CARGO ACCESS PANEL 2

ATTACHING PARTS

10 MS16535-134 . RIVET 2

– 15 5610-10-015 . DELETED D
(INCORRECT PN)

15A 10155610 . WASHER, NYLON 4

(V86928)
(TRUE PN 10/15/5610)

***

20 C412413-058 . HOOK FASTENER 2

(BONDED)

– 22 SNS512AF0625200 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

25 C412406-042 . EXTRUSION, SIDEWALL 1

(BONDED)

ATTACHING PARTS

30 BACN10YR3CM . NUT 10

35 NAS1515H3 . WASHER 10

40 BACS12FA3K8 . SCREW 10

***

45 CDSP1239-501 . QUARTER TURN FASTENER ASSY 35

– 50 CDSP1239-1 . . SLEEVE 1

– 55 CDSP1239-3 . . STUD 1

– 60 C412901-003 . RETAINER 35
(OPT TO ITEM 60A)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10217

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1X 60A C412901-5 . RETAINER 35

65 C412407-042 . STRIP, DOUBLER 1

(BONDED)

70 C412413-043 . STRIP, DOUBLER 1

(BONDED)

75 C412407-044 . STRIP, DOUBLER 1

(BONDED)

80 C412413-078 . STRIP, COVER 1

(BONDED)

85 C412413-079 . STRIP, COVER 1

(BONDED)

90 C412413-094 . STRIP, COVER 1

(BONDED)

– 95 SNS512AF . DELETED D
(INCORRECT PN)

– 95A SNS512AF125250 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

100 CDPL768-2 . PLACARD, "|" 1

(BONDED)

105 CDPL777-20 . PLACARD, "P31" 1

(BONDED)

110 CDPL777-2 . PLACARD, "31R" 2

(BONDED)

115 CDPL777-24 . PLACARD, "|" 1

(BONDED)

120 BAC27WCH351 . PLACARD, "PALLET 31" 1

(BONDED)

– 120A CDPL1364-7 . PLACARD, "PALLET 31" 1

(ALT TO ITEM 120)
(BONDED)

125 CDPL777-4 . PLACARD, "|32R" A 1

(BONDED)

– 125B CDPL777-4 . DELETED B D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10218

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 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1X 130 BAC27WCH269-152 . PLACARD, "152AW" A 1

(BONDED)
(TRUE PN BAC27WCH269-152AW)

– 130A CDPL1382-2 . PLACARD, "152AW" A 1

(ALT TO ITEM 130)
(BONDED)

– 130B BAC27WCH269-152 . DELETED B D

135 CDPL777-26 . PLACARD, "AFT E/E COOLING..." 1

(BONDED)

140 CDPL777-28 . PLACARD, "P814 PANEL" 1

(BONDED)

– 145 CDM200-05 . DELETED D

(INCORRECT PN)

– 145A 398FR . TAPE, GLASS CLOTH AR

(V04963)
(BONDED)
(0.5")
(1")

– 147 926 . TAPE, TRANSFER AR

(V04963)
(BONDED)
(0.75")

– 147A 9485PC . TAPE, TRANSFER AR

(V04963)
(BONDED)
(1")
(OPT TO ITEM -147)

150 C412410-063 . GRILL, DECOMPRESSION 1

155 C412410-059 . LINER, VERTICAL SIDEWALL 1

160 C412411-039 . VENT PANEL, INBD A 1

DECOMPRESSION

– 160A C412419-39 . DELETED B D

165 C412410-061 . LINER, VERTICAL SIDEWALL 1

– 170 C412419-539 . DECOMPRESSION BLOW, SUBASSY B 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10219

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1X – 175 BAC27WCH269-152 . . PLACARD, "152AW" B 1

(BONDED)
(TRUE PN BAC27WCH269-152AW)

– 175A CDPL1382-2 . . PLACARD, "152AW" B 1

(ALT TO ITEM -175)
(BONDED)

– 180 CDPL777-4 . . PLACARD, "|32R" B 1

(BONDED)

– 185 C412419-39 . . VENT PANEL, INBD B 1

DECOMPRESSION

– ITEM NOT ILLUSTRATED

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40
A

75

35

65

30

25

60
50
55

20C
50110501Y01

Vertical Sidewall Panel Assembly

Figure 1Y/GRAPHIC 50-11-05-99B-024-A01

50-11-05 Page 10222

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1Y – 1 C412416-163 PANEL ASSY, SEC 47 VERTICAL A RF

SIDEWALL

– 1A C419401-153 PANEL ASSY, SEC 47 VERTICAL B RF

SIDEWALL

– 1B C419401-159 PANEL ASSY, SEC 47 VERTICAL C RF

SIDEWALL

– 1C C414401-143 PANEL ASSY, SEC 47 VERTICAL D RF

SIDEWALL

– 1D C419401-171 PANEL ASSY, SEC 47 VERTICAL E RF

SIDEWALL

5 CDSP1239-501 . QUARTER TURN FASTENER ASSY A 31

– 5A CDSP1239-501 . QUARTER TURN FASTENER ASSY B 32

– 5B CDSP1239-501 . QUARTER TURN FASTENER ASSY C-E 33

– 10 CDSP1239-1 . . SLEEVE 1

– 15 CDSP1239-3 . . STUD 1

– 20 C412901-003 . RETAINER A 31
(OPT TO ITEM 20C)

– 20A C412901-5 . RETAINER B 32

– 20B C412901-5 . RETAINER C-E 33

20C C412901-5 . RETAINER A 31

25 C412414-022 . STRIP, DOUBLER A 1

(BONDED)

– 25A C419407-95 . STRIP, DOUBLER B-E 1

(BONDED)

30 C412414-023 . STRIP, DOUBLER A 1

(BONDED)

– 30A C419407-93 . STRIP, DOUBLER B-E 1

(BONDED)

35 C412414-020 . STRIP, DOUBLER A 1

(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10223

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1Y – 35A C419407-97 . STRIP, DOUBLER B-E 1

(BONDED)

40 C412414-021 . STRIP, DOUBLER A 1

(BONDED)

– 40A C419407-91 . STRIP, DOUBLER B 1

(BONDED)

– 40B C419408-11 . STRIP, DOUBLER C-E 1

(BONDED)

– 45 SNS512AF250500 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

50 BAC27WCH282-162 . PLACARD, "162AW" A-C 1

(BONDED)
(TRUE PN BAC27WCH282-162AW)

– 50A CDPL1383-3 . PLACARD, "162AW" D,E 1

(BONDED)

– 50B CDPL1383-3 . PLACARD, "162AW" A-C 1

(ALT TO ITEM 50)
(BONDED)

55 CDPL788-5 . PLACARD, "BULK CARGO..." 1

(BONDED)

60 CDPL788-7 . PLACARD, "LAV/ GALLEY..." 1

(BONDED)

65 CDPL788-11 . PLACARD, "CARGO LOADING" A,E 1

(BONDED)

– 65A CDPL788-13 . PLACARD, "CARGO LOADING" B,C 1

(BONDED)

– 65B CDPL767-69 . PLACARD, "CARGO LOADING" D 1

(BONDED)

– 70 CDM200-05 . DELETED A D
(INCORRECT PN)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10224

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1Y – 70A 398FR . TAPE, GLASS CLOTH AR

(V04963)
(BONDED)
(0.5")
(1")
(2")

75 C412404-007 . LINER, VERTICAL SIDEWALL A 1

– 75A C419404-35 . LINER, VERTICAL SIDEWALL B 1

– 75B C419404-39 . LINER, VERTICAL SIDEWALL C-E 1

– ITEM NOT ILLUSTRATED

50-11-05 Page 10225

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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30

40

25

65

35
55

50

20B

5
50110501Z01

Vertical Sidewall Panel Assembly

Figure 1Z/GRAPHIC 50-11-05-99B-025-A01

50-11-05 Page 10226

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

1Z – 1 C412416-165 PANEL ASSY, SEC 47 VERTICAL A RF

SIDEWALL

– 1A C419401-157 PANEL ASSY, SEC 47 VERTICAL B RF

SIDEWALL

5 CDSP1239-501 . QUARTER TURN FASTENER ASSY A 29

– 5A CDSP1239-501 . QUARTER TURN FASTENER ASSY B 30

– 10 CDSP1239-1 . . SLEEVE 1

– 15 CDSP1239-3 . . STUD 1

– 20 C412901-003 . RETAINER A 29
(OPT TO ITEM 20B)

– 20A C412901-5 . RETAINER B 30

20B C412901-5 . RETAINER A 29

25 C412414-024 . STRIP, DOUBLER A 1

(BONDED)

– 25A C419409-1 . STRIP, DOUBLER B 1

(BONDED)

30 C412414-025 . STRIP, DOUBLER A 1

(BONDED)

– 30A C419407-99 . STRIP, DOUBLER B 1

(BONDED)

35 C412414-026 . STRIP, DOUBLER A 1

(BONDED)

– 35A C419409-3 . STRIP, DOUBLER B 1

(BONDED)

40 C412414-027 . STRIP, DOUBLER A 1

(BONDED)

– 40A C419409-5 . STRIP, DOUBLER B 1

(BONDED)

– 45 SNS512AF250500 . TAPE, SILICONE FOAM AR

(V12624)
(BONDED)

– ITEM NOT ILLUSTRATED

50-11-05 Page 10227

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

1Z 50 BAC27WCH282-162 . PLACARD, "162CW" 1

(BONDED)
(TRUE PN BAC27WCH282-162CW)

– 50A CDPL1383-5 . PLACARD, "162CW" 1

(ALT TO ITEM 50)
(BONDED)

55 CDPL788-9 . PLACARD, "LAV/ GALLEY VENT 1

FANS"
(BONDED)

– 60 CDM200-05 . DELETED A D
(INCORRECT PN)

– 60A 398FR . TAPE, GLASS CLOTH AR

(V04963)
(BONDED)
(0.5")
(1")

65 C412404-009 . LINER, VERTICAL SIDEWALL A 1

– 65A C419404-37 . LINER, VERTICAL SIDEWALL B 1

– ITEM NOT ILLUSTRATED

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D
TE
LE
DE

Vertical Sidewall Panel Assembly

Figure 2/GRAPHIC 50-11-05-99B-026-A01

50-11-05 Page 10230

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
C41XXXX

FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2 – 1 C412417-123 DELETED A D

– 1A C412417-149 DELETED B D

– 1B C412409-149 DELETED C D

– 5 C412406-021 . DELETED D

ATTACHING PARTS

– 10 BACN10YR3CM . DELETED D

– 15 NAS1515H3 . DELETED D

– 20 BACS12FA3K8 . DELETED D

***

– 25 C412406-003 . DELETED A D

– 25A C412406-027 . DELETED B,C D

ATTACHING PARTS

– 30 BACN10YR3CM . DELETED D

– 35 NAS1515H3 . DELETED D

– 40 BACS12FA3K8 . DELETED D

***

– 45 852Z0440-2 . DELETED A D

– 45A 852Z0440-7 . DELETED B D

– 50 C412413-083 . DELETED A D

– 50A C412413-087 . DELETED B,C D

– 55 CDPL768-8 . DELETED A D

– 55A BAC27WCH369 . DELETED B,C D

– 60 CDPL768-14 . DELETED A D

– 60A CDPL777-18 . DELETED B,C D

– 65 BAC27WCH276-122 . DELETED A D

– 65A BAC27WCH269-152 . DELETED B,C D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10231

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2 – 70 BAC27WCH201 . DELETED B,C D

– 75 SNS512AF . DELETED D

– 80 BMS1-68 . DELETED A D

– 85 C412410-031 . DELETED A D

– 85A C412410-071 . DELETED B,C D

– ITEM NOT ILLUSTRATED

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D
TE
LE
DE

Vertical Sidewall Panel Assembly

Figure 2A/GRAPHIC 50-11-05-99B-027-A01

50-11-05 Page 10234

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2A – 1 C412416-167 DELETED D

– 5 C412406-005 . DELETED D

ATTACHING PARTS

– 10 BACN10YR3CM . DELETED D

– 15 NAS1515H3 . DELETED D

– 20 BACS12FA3K8 . DELETED D

***

– 25 C512416-567 . DELETED D

– 30 C412413-056 . . DELETED D

ATTACHING PARTS

– 35 MS16535-134 . . DELETED D

– 40 5610-10-015 . . DELETED D

***

– 45 C412413-058 . . DELETED D

– 50 CDSP1239-501 . . DELETED D

– 55 CDSP1239-1 . . . DELETED D

– 60 CDSP1239-3 . . . DELETED D

– 65 C412901-003 . . DELETED D

– 70 C412413-023 . . DELETED D

– 75 C412413-001 . . DELETED D

– 80 CDPL776-25 . . DELETED D

– 85 CDPL789-1 . . DELETED D

– 90 CDPL767-47 . . DELETED D

– 95 SNS512AF . . DELETED D

– 100 CDM200-05 . . DELETED D

– 105 CDM200-03 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10235

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2A – 110 C412410-007 . . DELETED D

– 115 C512416-535 . DELETED D

– 120 C412413-056 . . DELETED D

ATTACHING PARTS

– 125 MS16535-134 . . DELETED D

– 130 5610-10-015 . . DELETED D

***

– 135 C412413-058 . . DELETED D

– 140 CDSP1239-501 . . DELETED D

– 145 CDSP1239-1 . . . DELETED D

– 150 CDSP1239-3 . . . DELETED D

– 155 C412901-003 . . DELETED D

– 160 C412413-028 . . DELETED D

– 165 C412413-029 . . DELETED D

– 170 C412413-027 . . DELETED D

– 175 BAC27WEC165 . . DELETED D

– 180 BAC27WCH270 . . DELETED D

– 185 SNS512AF . . DELETED D

– 190 CDM200-05 . . DELETED D

– 195 926 . . DELETED D

– 200 C412410-051 . . DELETED D

– 205 C412413-045 . DELETED D

– 210 C412413-046 . DELETED D

– 215 C412413-090 . DELETED D

– 220 CDPL776-19 . DELETED D

– 225 BAC27WCH715 . DELETED D

– 230 CDPL776-15 . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10236

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2A – 235 MS16535-134 . DELETED D

– 240 5610-10-015 . DELETED D

– 245 SNS512AF . DELETED D

– 250 CDM200-05 . DELETED D

– 255 926 . DELETED D

– 260 C412410-053 . DELETED D

– 265 C412411-047 . DELETED D

– ITEM NOT ILLUSTRATED

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Sloping Sidewall Liner Assembly

Figure 2B/GRAPHIC 50-11-05-99B-028-A01

50-11-05 Page 10238

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2B – 1 C411151-175 DELETED D

– 5 BACN11AL1CM . DELETED D

– 10 C411151-051 . DELETED D

– 15 C411152-37 . DELETED D

– 20 CDPL776-35 . DELETED D

– 25 C411151-75 . DELETED D

– ITEM NOT ILLUSTRATED

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Section 41 Vertical Sidewall Assembly

Figure 2C/GRAPHIC 50-11-05-99B-029-A01

50-11-05 Page 10240

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2C – 1 C419401-101 DELETED A D

– 1A C419401-103 DELETED B D

– 1B C419410-101 DELETED C D

– 5 BACN11AL1CM . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 C419402-1 . DELETED A,C D

– 25A C419402-41 . DELETED B D

– 30 C419404-501 . DELETED A,C D

– 30A C419404-503 . DELETED B D

– 35 CDSP1239-501 . . DELETED A,C D

– 35A CDSP1239-501 . . DELETED B D

– 40 CDSP1239-1 . . . DELETED D

– 45 CDSP1239-3 . . . DELETED D

– 50 C412901-5 . . DELETED A,C D

– 50A C412901-5 . . DELETED B D

– 55 C419413-1 . . DELETED D

ATTACHING PARTS

– 60 MS16535-134 . . DELETED D

– 65 5610-10-15 . . DELETED D

***

– 70 C412413-058 . . DELETED D

– 75X SNS512AF125250 . . DELETED D

– ITEM NOT ILLUSTRATED

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2C – 80X CDM200-05 . . DELETED D

– 85 C419407-7 . . DELETED A,C D

– 85A C419407-11 . . DELETED B D

– 90 C419407-11 . . DELETED D

– 95 C419407-9 . . DELETED A,C D

– 95A C419407-17 . . DELETED B D

– 100 CDPL767-7 . . DELETED A,C D

– 105 BAC27WEC163 . . DELETED A,C D

– 105A BAC27WEC165 . . DELETED B D

– 110 BAC27WCH496 . . DELETED A,C D

– 115 BAC27WCH277 . . DELETED A,C D

– 115A BAC27WCH277 . . DELETED B D

– 120 BAC27WCH211 . . DELETED B D

– 125 CDPL767-39 . . DELETED B D

– 130 BAC27WCH122 . . DELETED B D

– 135 C419404-1 . . DELETED A,C D

– 135A C419404-3 . . DELETED B D

– 140 C419403-501 . DELETED A,C D

– 140A C419403-503 . DELETED B D

– 145 BAC27WCH219 . . DELETED A,C D

– 150 BAC27WCH240 . . DELETED A,C D

– 155 BAC27WCH277 . . DELETED A,C D

– 155A BAC27WCH277 . . DELETED B D

– 160 BAC27WCH221 . . DELETED B D

– 165 C419403-1 . . DELETED A,C D

– 165A C419403-3 . . DELETED B D

– 170 C419409-501 . DELETED A D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10242

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2C – 170A C419409-503 . DELETED B D

– 170B C419415-501 . DELETED C D

– 175 C419405-501 . . DELETED A,C D

– 175A C419405-503 . . DELETED B D

– 180 CDM200-05 . . . DELETED D

– 185 C419407-1 . . . DELETED A,C D

– 185A C419407-13 . . . DELETED B D

– 190 C419407-5 . . . DELETED A,C D

– 190A C419407-14 . . . DELETED B D

– 195 C419407-3 . . . DELETED A,C D

– 195A C419407-15 . . . DELETED B D

– 200 C419405-1 . . . DELETED A,C D

– 200A C419405-3 . . . DELETED B D

– 205 C419406-501 . . DELETED A D

– 205A C419406-503 . . DELETED B D

– 205B C419416-501 . . DELETED C D

– 210 BAC27WCH210 . . . DELETED A,C D

– 215 852Z8400-17 . . . DELETED D

– 220 BAC27WCH277 . . . DELETED A,C D

– 220A BAC27WCH277 . . . DELETED B D

– 225 BAC27WCH101 . . . DELETED B D

– 230 BAC27WCH715 . . . DELETED B D

– 235 BAC27WCH228 . . . DELETED B D

– 240 C419406-1 . . . DELETED A D

– 240A C419406-3 . . . DELETED B D

– 240B C419416-1 . . . DELETED C D

– ITEM NOT ILLUSTRATED

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Section 41 Vertical Sidewall Assembly

Figure 2D/GRAPHIC 50-11-05-99B-030-A01

50-11-05 Page 10244

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2D – 1 C419401-105 DELETED D

– 5 BACN11AL1CM . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 C419402-3 . DELETED D

– 30 C419404-505 . DELETED D

– 35 CDSP1239-501 . . DELETED D

– 40 CDSP1239-1 . . . DELETED D

– 45 CDSP1239-3 . . . DELETED D

– 50 C412901-5 . . DELETED D

– 55 C419413-3 . . DELETED D

ATTACHING PARTS

– 60 MS16535-134 . . DELETED D

– 65 5610-10-15 . . DELETED D

***

– 70 C412413-058 . . DELETED D

– 75 C419413-1 . . DELETED D

ATTACHING PARTS

– 80 MS16535-134 . . DELETED D

– 85 5610-10-15 . . DELETED D

***

– 90 C412413-058 . . DELETED D

– 95 SNS512AF125250 . . DELETED D
– ITEM NOT ILLUSTRATED

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2D – 100 CDM200-05 . . DELETED D

– 105 C419407-11 . . DELETED D

– 110 C419407-17 . . DELETED D

– 115 C419407-19 . . DELETED D

– 120 C419407-35 . . DELETED D

– 125 C419407-21 . . DELETED D

– 130 CDPL767-55 . . DELETED D

– 135 CDPL767-43 . . DELETED D

– 140 CDPL767-41 . . DELETED D

– 145 BAC27WCH243 . . DELETED D

– 150 BAC27WCH277 . . DELETED D

– 155 C419404-5 . . DELETED D

– 160 C419403-505 . DELETED D

– 165 BAC27WCH117 . . DELETED D

– 170 CDPL767-65 . . DELETED D

– 175 CDPL767-25 . . DELETED D

– 180 BAC27WCH277 . . DELETED D

– 185 C419403-5 . . DELETED D

– ITEM NOT ILLUSTRATED

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Section 41 Vertical Sidewall Assembly

Figure 2E/GRAPHIC 50-11-05-99B-031-A01

50-11-05 Page 10248

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2E – 1 C419401-107 DELETED D

– 5 BACN11AL1CM . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 C419402-7 . DELETED D

– 30 C419404-507 . DELETED D

– 35 CDSP1239-501 . . DELETED D

– 40 CDSP1239-1 . . . DELETED D

– 45 CDSP1239-3 . . . DELETED D

– 50 C412901-5 . . DELETED D

– 55 C419413-1 . . DELETED D

ATTACHING PARTS

– 60 MS16535-134 . . DELETED D

– 65 5610-10-15 . . DELETED D

***

– 70 C412413-058 . . DELETED D

– 75 SNS512AF125250 . . DELETED D

– 80 CDM200-05 . . DELETED D

– 85 C419407-11 . . DELETED D

– 90 C419407-43 . . DELETED D

– 95 C419407-23 . . DELETED D

– 100 CDPL767-5 . . DELETED D

– 105 CDPL767-45 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10249

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2E – 110 CDPL767-17 . . DELETED D

– 115 BAC27WCH277 . . DELETED D

– 120 C419404-7 . . DELETED D

– 125 C419403-507 . DELETED D

– 130 BAC27WCH212 . . DELETED D

– 135 BAC27WCH118 . . DELETED D

– 140 BAC27WCH344 . . DELETED D

– 145 BAC27WCH277 . . DELETED D

– 150 C419403-7 . . DELETED D

– ITEM NOT ILLUSTRATED

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Section 41 Vertical Sidewall Assembly

Figure 2F/GRAPHIC 50-11-05-99B-032-A01

50-11-05 Page 10252

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2F – 1 C419401-121 DELETED A D

– 1A C419410-121 DELETED B D

– 5 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 10 BACS12FA3K8 . DELETED D

– 15 BACW10P304L . DELETED D

***

– 20 C419414-501 . DELETED D

– 25 BACN11AL1CM . DELETED D

– 30 C419402-21 . DELETED D

– 35 C419409-515 . DELETED A D

– 35A C419415-515 . DELETED B D

– 40 C419405-515 . . DELETED D

– 45 C419407-26 . . . DELETED D

– 50 C419407-25 . . . DELETED D

– 55 C419407-41 . . . DELETED D

– 60 C419405-15 . . . DELETED D

– 65 C419406-515 . . DELETED A D

– 65A C419416-515 . . DELETED B D

– 70 BAC27WCH212 . . . DELETED D

– 75 852Z8400-17 . . . DELETED D

– 80 BAC27WCH276 . . . DELETED D

– 85 C419406-15 . . . DELETED A D

– 85A C419416-15 . . . DELETED B D

– 90 C419403-521 . DELETED D

– 95 C419407-40 . . DELETED D
– ITEM NOT ILLUSTRATED

50-11-05 Page 10253

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2F – 100 CDPL768-8 . . DELETED D

– 105 BAC27WCH118 . . DELETED D

– 110 BAC27WCH510 . . DELETED D

– 115 BAC27WCH276 . . DELETED D

– 120 C419403-21 . . DELETED D

– ITEM NOT ILLUSTRATED

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Section 43 Vertical Sidewall Assembly

Figure 2G/GRAPHIC 50-11-05-99B-033-A01

50-11-05 Page 10256

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2G – 1 C419401-109 DELETED D

– 5 BACN11AL1CM . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 C419402-9 . DELETED D

– 30 C419403-509 . DELETED D

– 35 BAC27WCH213 . . DELETED D

– 40 CDPL767-61 . . DELETED D

– 45 BAC27WCH224 . . DELETED D

– 50 BAC27WCH245 . . DELETED D

– 55 CDPL767-63 . . DELETED D

– 60 BAC27WCH277 . . DELETED D

– 65 C419403-9 . . DELETED D

– ITEM NOT ILLUSTRATED

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Section 43 Vertical Sidewall Assembly

Figure 2H/GRAPHIC 50-11-05-99B-034-A01

50-11-05 Page 10258

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2H – 1 C419401-123 DELETED D

– 5 BACN11AL1CM . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 C419402-10 . DELETED D

– 30 C419404-513 . DELETED D

– 35 CDSP1239-501 . . DELETED D

– 40 CDSP1239-1 . . . DELETED D

– 45 CDSP1239-3 . . . DELETED D

– 50 C412901-5 . . DELETED D

– 55 C419413-1 . . DELETED D

ATTACHING PARTS

– 60 MS16535-134 . . DELETED D

– 65 5610-10-15 . . DELETED D

***

– 70 C412413-058 . . DELETED D

– 75 C419407-43 . . DELETED D

– 80 C419407-45 . . DELETED D

– 85 CDPL767-61 . . DELETED D

– 90 BAC27WCH213 . . DELETED D

– 95 CDPL768-42 . . DELETED D

– 100 BAC27WCH105 . . DELETED D

– 105 BAC27WCH276 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10259

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2H – 110 C419404-13 . . DELETED D

– 115 C419403-523 . DELETED D

– 120 BAC27WCH102 . . DELETED D

– 125 CDPL768-46 . . DELETED D

– 130 BAC27WCH276 . . DELETED D

– 135 C419403-23 . . DELETED D

– ITEM NOT ILLUSTRATED

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Section 43 Vertical Sidewall Assembly

Figure 2J/GRAPHIC 50-11-05-99B-035-A01

50-11-05 Page 10262

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2J – 1 C419401-111 DELETED A D

– 1A C419410-111 DELETED B D

– 5 BACN11AL1CM . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 C419402-11 . DELETED D

– 30 C419409-507 . DELETED A D

– 30A C419415-507 . DELETED B D

– 35 C419405-507 . . DELETED D

– 40 C419407-26 . . . DELETED D

– 45 C419407-25 . . . DELETED D

– 50 C419407-29 . . . DELETED D

– 55 C419405-7 . . . DELETED D

– 60 C419406-507 . . DELETED A D

– 60A C419416-507 . . DELETED B D

– 65 BAC27WCH214 . . . DELETED D

– 70 CDPL767-33 . . . DELETED D

– 75 852Z8400-17 . . . DELETED D

– 80 CDPL767-59 . . . DELETED D

– 85 BAC27WCH277 . . . DELETED D

– 90 C419406-7 . . . DELETED A D

– 90A C419416-7 . . . DELETED B D

– 95 C419409-505 . DELETED A D
– ITEM NOT ILLUSTRATED

50-11-05 Page 10263

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2J – 95A C419415-505 . DELETED B D

– 100 C419405-505 . . DELETED D

– 105 CDM200-05 . . . DELETED D

– 110 C419407-26 . . . DELETED D

– 115 C419407-25 . . . DELETED D

– 120 C419407-27 . . . DELETED D

– 125 C419405-5 . . . DELETED D

– 130 C419406-505 . . DELETED A D

– 130A C419416-505 . . DELETED B D

– 135 852Z8400-17 . . . DELETED D

– 140 BAC27WCH277 . . . DELETED D

– 145 C419406-5 . . . DELETED A D

– 145A C419416-5 . . . DELETED B D

– 150 C419403-511 . DELETED D

– 155 BAC27WCH225 . . DELETED D

– 160 BAC27WCH246 . . DELETED D

– 165 BAC27WCH277 . . DELETED D

– 170 C419403-11 . . DELETED D

– ITEM NOT ILLUSTRATED

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Section 43 Vertical Sidewall Assembly

Figure 2K/GRAPHIC 50-11-05-99B-036-A01

50-11-05 Page 10266

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2K – 1 C419401-125 DELETED D

– 5 BACN11AL1CM . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 C419402-12 . DELETED D

– 30 C419404-515 . DELETED D

– 35 CDSP1239-501 . . DELETED D

– 40 CDSP1239-1 . . . DELETED D

– 45 CDSP1239-3 . . . DELETED D

– 50 C412901-5 . . DELETED D

– 55 C419413-1 . . DELETED D

ATTACHING PARTS

– 60 MS16535-134 . . DELETED D

– 65 5610-10-15 . . DELETED D

***

– 70 C412413-058 . . DELETED D

– 75 SNS512AF125250 . . DELETED D

– 80 CDM200-05 . . DELETED D

– 85 C419407-43 . . DELETED D

– 90 C419407-25 . . DELETED D

– 95 C419407-47 . . DELETED D

– 100 CDPL768-24 . . DELETED D

– 105 CDPL768-42 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10267

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2K – 110 BAC27WCH106 . . DELETED D

– 115 BAC27WCH276 . . DELETED D

– 120 C419404-15 . . DELETED D

– 125 C419404-517 . DELETED D

– 130 CDSP1239-501 . . DELETED D

– 135 CDSP1239-1 . . . DELETED D

– 140 CDSP1239-3 . . . DELETED D

– 145 C412901-5 . . DELETED D

– 150 C419413-3 . . DELETED D

ATTACHING PARTS

– 155 MS16535-134 . . DELETED D

– 160 5610-10-15 . . DELETED D

***

– 165 C412413-058 . . DELETED D

– 170 C419413-1 . . DELETED D

ATTACHING PARTS

– 175 MS16535-134 . . DELETED D

– 180 5610-10-15 . . DELETED D

***
– 185 C412413-058 . . DELETED D

– 190 C419407-43 . . DELETED D

– 195 C419407-53 . . DELETED D

– 200 C419407-51 . . DELETED D

– 205 C419407-49 . . DELETED D

– 210 C419409-7 . . DELETED D

– 215 BAC27WCH214 . . DELETED D

– 220 CDPL768-42 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10268

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2K – 225 CDPL768-48 . . DELETED D

– 230 CDPL768-50 . . DELETED D

– 235 BAC27WCH276 . . DELETED D

– 240 C419404-17 . . DELETED D

– ITEM NOT ILLUSTRATED

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Section 43 Vertical Sidewall Assembly

Figure 2L/GRAPHIC 50-11-05-99B-037-A01

50-11-05 Page 10270

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2L – 1 C419401-113 DELETED A D

– 1A C419410-113 DELETED B D

– 5 BACN11AL1CM . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 C419402-13 . DELETED D

– 30 C419409-509 . DELETED A D

– 30A C419415-509 . DELETED B D

– 35 C419406-17 . . DELETED D

– 40 C419405-509 . . DELETED D

– 45 CDM200-05 . . . DELETED D

– 50 C419407-32 . . . DELETED D

– 55 C419407-31 . . . DELETED D

– 60 C419407-33 . . . DELETED D

– 65 CDPL767-23 . . . DELETED D

– 70 BAC27WCH277 . . . DELETED D

– 75 C419405-9 . . . DELETED D

– 80 C419406-509 . . DELETED A D

– 80A C419416-509 . . DELETED B D

– 85 BAC27WCH227 . . . DELETED D

– 90 852Z8400-17 . . . DELETED D

– 95 BAC27WCH277 . . . DELETED D

– 100 C419406-9 . . . DELETED A D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10271

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2L – 100A C419416-9 . . . DELETED B D

– 105 C419403-513 . DELETED D

– 110 CDPL767-21 . . DELETED D

– 115 CDPL767-25 . . DELETED D

– 120 BAC27WCH277 . . DELETED D

– 125 C419403-13 . . DELETED D

– ITEM NOT ILLUSTRATED

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Figure 2M/GRAPHIC 50-11-05-99B-038-A01

50-11-05 Page 10274

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2M – 1 C419401-127 DELETED D

– 5 BACN11AL1CM . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 C419402-14 . DELETED D

– 30 C419404-519 . DELETED D

– 35 CDSP1239-501 . . DELETED D

– 40 CDSP1239-1 . . . DELETED D

– 45 CDSP1239-3 . . . DELETED D

– 50 C412901-5 . . DELETED D

– 55 C419413-3 . . DELETED D

ATTACHING PARTS

– 60 MS16535-134 . . DELETED D

– 65 5610-10-15 . . DELETED D

***

– 70 C412413-058 . . DELETED D

– 75 C419413-1 . . DELETED D

ATTACHING PARTS

– 80 MS16535-134 . . DELETED D

– 85 5610-10-15 . . DELETED D

***

– 90 C412413-058 . . DELETED D

– 95 SNS512AF125250 . . DELETED D
– ITEM NOT ILLUSTRATED

50-11-05 Page 10275

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2M – 100 CDM200-05 . . DELETED D

– 105 C419407-43 . . DELETED D

– 110 C419407-17 . . DELETED D

– 115 C419407-51 . . DELETED D

– 120 C419407-35 . . DELETED D

– 125 C419407-55 . . DELETED D

– 130 C419407-25 . . DELETED D

– 135 BAC27WCH226 . . DELETED D

– 140 CDPL768-42 . . DELETED D

– 145 CDPL768-52 . . DELETED D

– 150 CDPL768-36 . . DELETED D

– 155 BAC27WCH276 . . DELETED D

– 160 C419404-19 . . DELETED D

– ITEM NOT ILLUSTRATED

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Figure 2N/GRAPHIC 50-11-05-99B-039-A01

50-11-05 Page 10278

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2N – 1 C419401-115 DELETED A D

– 1A C419410-115 DELETED B D

– 5 BACN11AL1CM . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 C419402-15 . DELETED D

– 30 C419409-511 . DELETED A D

– 30A C419415-511 . DELETED B D

– 35 C419405-511 . . DELETED D

– 40 C419407-26 . . . DELETED D

– 45 C419407-25 . . . DELETED D

– 50 C419407-15 . . . DELETED D

– 55 C419405-11 . . . DELETED D

– 60 C419406-511 . . DELETED A D

– 60A C419416-511 . . DELETED B D

– 65 BAC27WCH215 . . . DELETED D

– 70 852Z8400-17 . . . DELETED D

– 75 CDPL767-57 . . . DELETED D

– 80 BAC27WCH277 . . . DELETED D

– 85 C419406-11 . . . DELETED A D

– 85A C419416-11 . . . DELETED B D

– 90 C419403-515 . DELETED D

– 95 BAC27WCH222 . . DELETED D
– ITEM NOT ILLUSTRATED

50-11-05 Page 10279

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2N – 100 BAC27WCH209 . . DELETED D

– 105 BAC27WCH235 . . DELETED D

– 110 CDPL767-67 . . DELETED D

– 115 C419403-15 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10280

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Figure 2P/GRAPHIC 50-11-05-99B-040-A01

50-11-05 Page 10282

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2P – 1 C419401-129 DELETED D

– 5 BACN11AL1CM . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 C419402-16 . DELETED D

– 30 C419403-525 . DELETED D

– 35 BAC27WCH215 . . DELETED D

– 40 BAC27WCH220 . . DELETED D

– 45 BAC27WCH209 . . DELETED D

– 50 CDPL768-54 . . DELETED D

– 55 BAC27WCH238 . . DELETED D

– 60 BAC27WCH276 . . DELETED D

– 65 C419403-25 . . DELETED D

– ITEM NOT ILLUSTRATED

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Section 41 Vertical Sidewall Assembly

Figure 2Q/GRAPHIC 50-11-05-99B-041-A01

50-11-05 Page 10284

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2Q – 1 C419401-117 DELETED D

– 5 BACN11AL1CM . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 C419402-17 . DELETED D

– 30 C419404-509 . DELETED D

– 35 CDSP1239-501 . . DELETED D

– 40 CDSP1239-1 . . . DELETED D

– 45 CDSP1239-3 . . . DELETED D

– 50 C412901-5 . . DELETED D

– 55 C419413-3 . . DELETED D

ATTACHING PARTS

– 60 MS16535-134 . . DELETED D

– 65 5610-10-15 . . DELETED D

***

– 70 C412413-058 . . DELETED D

– 75 C419407-37 . . DELETED D

– 80 C419407-35 . . DELETED D

– 85 BAC27WCH216 . . DELETED D

– 90 CDPL768-38 . . DELETED D

– 95 BAC27TCH0371 . . DELETED D

– 100 BAC27WCH276 . . DELETED D

– 105 C419404-9 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10285

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2Q – 110 C419406-13 . DELETED D

– 115 C419405-513 . DELETED D

– 120 BAC27WCH210 . . DELETED D

– 125 BAC27WCH276 . . DELETED D

– 130 C419405-13 . . DELETED D

– 135 C419403-517 . DELETED D

– 140 CDPL768-2 . . DELETED D

– 145 BAC27TCH0370 . . DELETED D

– 150 BAC27WCH276 . . DELETED D

– 155 C419403-17 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10286

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Section 41 Vertical Sidewall Assembly

Figure 2R/GRAPHIC 50-11-05-99B-042-A01

50-11-05 Page 10288

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2R – 1 C419401-119 DELETED D

– 5 BACN11AL1CM . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 C419402-19 . DELETED D

– 30 C419404-511 . DELETED D

– 35 CDSP1239-501 . . DELETED D

– 40 CDSP1239-1 . . . DELETED D

– 45 CDSP1239-3 . . . DELETED D

– 50 C412901-5 . . DELETED D

– 55 C419413-1 . . DELETED D

ATTACHING PARTS

– 60 MS16535-134 . . DELETED D

– 65 5610-10-15 . . DELETED D

***

– 70 C412413-058 . . DELETED D

– 75 C419407-11 . . DELETED D

– 80 C419407-7 . . DELETED D

– 85 C419407-10 . . DELETED D

– 90 CDPL767-7 . . DELETED D

– 95 CDPL768-40 . . DELETED D

– 100 BAC27WCH328 . . DELETED D

– 105 BAC27WCH276 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10289

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2R – 110 C419404-11 . . DELETED D

– 115 C419403-519 . DELETED D

– 120 C419407-39 . . DELETED D

– 125 BAC27WCH219 . . DELETED D

– 130 BAC27WCH276 . . DELETED D

– 135 C419403-19 . . DELETED D

– ITEM NOT ILLUSTRATED

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Section 46 Vertical Sidewall Assembly

Figure 2S/GRAPHIC 50-11-05-99B-043-A01

50-11-05 Page 10292

Oct 09/23
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2S – 1 C419401-131 DELETED D

– 5 BACN11AL1CM . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 C419402-23 . DELETED D

– 30 C419403-527 . DELETED D

– 35 CDPL768-2 . . DELETED D

– 40 BAC27TCH0370 . . DELETED D

– 45 BAC27WCH270 . . DELETED D

– 50 C419403-27 . . DELETED D

– 55 C419406-19 . DELETED D

– 60 C419404-521 . DELETED D

– 65 CDSP1239-501 . . DELETED D

– 70 CDSP1239-1 . . . DELETED D

– 75 CDSP1239-3 . . . DELETED D

– 80 C412901-5 . . DELETED D

– 85 C419413-1 . . DELETED D

ATTACHING PARTS

– 90 MS16535-134 . . DELETED D

– 95 5610-10-15 . . DELETED D

***

– 100 C412413-058 . . DELETED D

– 105 C419407-43 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10293

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2S – 110 C419407-57 . . DELETED D

– 115 BAC27WCH351 . . DELETED D

– 120 CDPL776-33 . . DELETED D

– 125 BAC27WCH270 . . DELETED D

– 130 C419404-21 . . DELETED D

– 135 C419405-519 . DELETED D

– 140 BAC27WCH357 . . DELETED D

– 145 CDPL776-37 . . DELETED D

– 150 BAC27WCH270 . . DELETED D

– 155 C419405-19 . . DELETED D

– 160 C419403-529 . DELETED D

– 165 BAC27WCH249 . . DELETED D

– 170 BAC27WCH270 . . DELETED D

– 175 C419403-29 . . DELETED D

– ITEM NOT ILLUSTRATED

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Vertical Sidewall Panel Assembly

Figure 2T/GRAPHIC 50-11-05-99B-044-A01

50-11-05 Page 10296

Oct 09/23
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2T – 1 C419401-143 DELETED A D

– 1A C419410-143 DELETED B D

– 5 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 10 BACS12FA3K8 . DELETED D

– 15 BACW10P304L . DELETED D

***

– 20 BACN11AL1CM . DELETED D

– 25 C419402-24 . DELETED D

– 30 C419409-533 . DELETED A D

– 30A C419415-533 . DELETED B D

– 35 C419405-507 . . DELETED D

– 40 C419407-25 . . . DELETED D

– 45 C419407-26 . . . DELETED D

– 50 C419407-29 . . . DELETED D

– 55 C419405-7 . . . DELETED D

– 60 C419406-533 . . DELETED A D

– 60A C419416-533 . . DELETED B D

– 65 852Z8400-17 . . . DELETED D

– 70 BAC27WCH265 . . . DELETED D

– 75 BAC27WCH269-152 . . . DELETED D

– 80 C419406-7 . . . DELETED A D

– 80A C419416-7 . . . DELETED B D

– 85 C419404-529 . DELETED D

– 90 CDSP1239-501 . . DELETED D

– 95 CDSP1239-1 . . . DELETED D
– ITEM NOT ILLUSTRATED

50-11-05 Page 10297

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2T – 100 CDSP1239-3 . . . DELETED D

– 105 C412901-5 . . DELETED D

– 110 C419407-43 . . DELETED D

– 115 C419407-69 . . DELETED D

– 120 C419413-1 . . DELETED D

ATTACHING PARTS

– 125 MS16535-134 . . DELETED D

– 130 5610-10-15 . . DELETED D

***

– 135 C412413-058 . . DELETED D

– 140 BAC27WCH351 . . DELETED D

– 145 BAC27WCH357 . . DELETED D

– 150 CDPL777-28 . . DELETED D

– 155 CDPL777-26 . . DELETED D

– 160 BAC27WCH258 . . DELETED D

– 165 BAC27WCH269-152 . . DELETED D

– 170 C419404-29 . . DELETED D

– 175 C419403-543 . DELETED D

– 180 CDPL768-2 . . DELETED D

– 185 BAC27TCH0370 . . DELETED D

– 190 BAC27WCH269-152 . . DELETED D

– 195 C419403-43 . . DELETED D

– ITEM NOT ILLUSTRATED

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Section 46 Vertical Sidewall Assembly

Figure 2U/GRAPHIC 50-11-05-99B-045-A01

50-11-05 Page 10300

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2U – 1 C419401-143 DELETED A D

– 1A C419410-143 DELETED B D

– 5 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 10 BACS12FA3K8 . DELETED D

– 15 BACW10P304L . DELETED D

***

– 20 BACN11AL1CM . DELETED D

– 25 C419402-24 . DELETED D

– 30 C419409-533 . DELETED A D

– 30A C419415-533 . DELETED B D

– 35 C419405-507 . . DELETED D

– 40 C419407-25 . . . DELETED D

– 45 C419407-26 . . . DELETED D

– 50 C419407-29 . . . DELETED D

– 55 C419405-7 . . . DELETED D

– 60 C419406-533 . . DELETED A D

– 60A C419416-533 . . DELETED B D

– 65 852Z8400-17 . . . DELETED D

– 70 BAC27WCH265 . . . DELETED D

– 75 BAC27WCH269-152 . . . DELETED D

– 80 C419406-7 . . . DELETED A D

– 80A C419416-7 . . . DELETED B D

– 85 C419404-529 . DELETED D

– 90 CDSP1239-501 . . DELETED D

– 95 CDSP1239-1 . . . DELETED D
– ITEM NOT ILLUSTRATED

50-11-05 Page 10301

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2U – 100 CDSP1239-3 . . . DELETED D

– 105 C412901-5 . . DELETED D

– 110 C419407-43 . . DELETED D

– 115 C419407-69 . . DELETED D

– 120 C419413-1 . . DELETED D

ATTACHING PARTS

– 125 MS16535-134 . . DELETED D

– 130 5610-10-15 . . DELETED D

***

– 135 C412413-058 . . DELETED D

– 140 BAC27WCH351 . . DELETED D

– 145 BAC27WCH357 . . DELETED D

– 150 CDPL777-28 . . DELETED D

– 155 CDPL777-26 . . DELETED D

– 160 BAC27WCH258 . . DELETED D

– 165 BAC27WCH269-152 . . DELETED D

– 170 C419404-29 . . DELETED D

– 175 C419403-543 . DELETED D

– 180 CDPL768-2 . . DELETED D

– 185 BAC27TCH0370 . . DELETED D

– 190 BAC27WCH269-152 . . DELETED D

– 195 C419403-43 . . DELETED D

– ITEM NOT ILLUSTRATED

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Vertical Sidewall Panel Assembly

Figure 2V/GRAPHIC 50-11-05-99B-046-A01

50-11-05 Page 10304

Oct 09/23
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2V – 1 C419401-145 DELETED D

– 5 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 10 BACS12FA3K8 . DELETED D

– 15 BACW10P304L . DELETED D

***

– 20 BACN11AL1CM . DELETED D

– 25 C419402-26 . DELETED D

– 30 C419403-545 . DELETED D

– 35 BAC27WCH352 . . DELETED D

– 40 CDPL776-3 . . DELETED D

– 45 BAC27WCH267 . . DELETED D

– 50 BAC27WCH269-152 . . DELETED D

– 55 C419403-45 . . DELETED D

– 60 C419406-17 . DELETED D

– 65 C419405-517 . DELETED D

– 70 BAC27WCH371 . . DELETED D

– 75 BAC27WCH269-152 . . DELETED D

– 80 C419405-17 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10305

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Section 46 Vertical Sidewall Assembly

Figure 2W/GRAPHIC 50-11-05-99B-047-A01

50-11-05 Page 10306

Oct 09/23
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2W – 1 C419401-135 DELETED A D

– 1A C419410-135 DELETED B D

– 5 BACN11AL1CM . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 C419402-27 . DELETED D

– 30 C419403-533 . DELETED D

– 35 CDPL776-39 . . DELETED D

– 40 BAC27WCH385 . . DELETED D

– 45 BAC27WCH391 . . DELETED D

– 50 BAC27WCH270 . . DELETED D

– 55 C419403-33 . . DELETED D

– 60 C419403-535 . DELETED D

– 65 CDPL776-29 . . DELETED D

– 70 BAC27WCH270 . . DELETED D

– 75 C419403-35 . . DELETED D

– 80 C419409-521 . DELETED A D

– 80A C419415-521 . DELETED B D

– 85 C419405-511 . . DELETED D

– 90 C419407-26 . . . DELETED D

– 95 C419407-25 . . . DELETED D

– 100 C419407-15 . . . DELETED D

– 105 C419405-11 . . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10307

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2W – 110 C419406-521 . . DELETED A D

– 110A C419416-521 . . DELETED B D

– 115 BAC27WCH375 . . . DELETED D

– 120 852Z8400-17 . . . DELETED D

– 125 CDPL776-41 . . . DELETED D

– 130 BAC27WCH270 . . . DELETED D

– 135 C419406-11 . . . DELETED A D

– 135A C419416-11 . . . DELETED B D

– ITEM NOT ILLUSTRATED

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Vertical Sidewall Panel Assembly

Figure 2X/GRAPHIC 50-11-05-99B-048-A01

50-11-05 Page 10310

Oct 09/23
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2X – 1 C419401-147 DELETED D

– 5 BACN11AL1CM . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 C419402-31 . DELETED D

– 30 C419403-547 . DELETED D

– 35 BAC27WCH375 . . DELETED D

– 40 CDPL776-39 . . DELETED D

– 45 BAC27WCH382 . . DELETED D

– 50 CDPL777-33 . . DELETED D

– 55 CDPL777-31 . . DELETED D

– 60 BAC27WCH269-152 . . DELETED D

– 65 C419403-47 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10311

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Figure 2Y/GRAPHIC 50-11-05-99B-049-A01

50-11-05 Page 10312

Oct 09/23
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2Y – 1 C419401-137 DELETED A D

– 1A C419410-137 DELETED B D

– 5 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 10 BACS12FA3K8 . DELETED D

– 15 BACW10P304L . DELETED D

***

– 20 BACN11AL1CM . DELETED D

– 25 C419402-41 . DELETED D

– 30 C419403-537 . DELETED D

– 35 CDPL776-43 . . DELETED D

– 40 CDPL767-39 . . DELETED D

– 45 BAC27WCH270-151 . . DELETED D

– 50 C419403-37 . . DELETED D

– 55 C419409-523 . DELETED A D

– 55A C419415-523 . DELETED B D

– 60 C419405-503 . . DELETED D

– 65 CDM200-05 . . . DELETED D

– 70 C419407-13 . . . DELETED D

– 75 C419407-14 . . . DELETED D

– 80 C419407-15 . . . DELETED D

– 85 C419405-3 . . . DELETED D

– 90 C419406-523 . . DELETED A D

– 90A C419416-523 . . DELETED B D

– 95 BAC27WCH264 . . . DELETED D

– 100 852Z8400-17 . . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10313

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2Y – 105 BAC27WCH250 . . . DELETED D

– 110 BAC27WCH270-151 . . . DELETED D

– 115 C419406-3 . . . DELETED A D

– 115A C419416-3 . . . DELETED B D

– 120 C419404-527 . DELETED D

– 125 CDSP1239-501 . . DELETED D

– 130 CDSP1239-1 . . . DELETED D

– 135 CDSP1239-3 . . . DELETED D

– 140 C412901-5 . . DELETED D

– 145 C419407-11 . . DELETED D

– 150 C419407-17 . . DELETED D

– 155 C419413-1 . . DELETED D

ATTACHING PARTS

– 160 MS16535-134 . . DELETED D

– 165 5610-10-15 . . DELETED D

***

– 170 C412413-058 . . DELETED D

– 175 BAC27WCH366 . . DELETED D

– 180 CDPL789-1 . . DELETED D

– 185 CDPL767-65 . . DELETED D

– 190 BAC27WCH270-151 . . DELETED D

– 195 C419404-3 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10314

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Figure 2Z/GRAPHIC 50-11-05-99B-050-A01

50-11-05 Page 10316

Oct 09/23
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

2Z – 1 C419401-139 DELETED A D

– 1A C419410-139 DELETED B D

– 5 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 10 BACS12FA3K8 . DELETED D

– 15 BACW10P304L . DELETED D

***

– 20 BACN11AL1CM . DELETED D

– 25 C419402-3 . DELETED D

– 30 C419409-525 . DELETED A D

– 30A C419415-525 . DELETED B D

– 35 C419405-503 . . DELETED D

– 40 CDM200-05 . . . DELETED D

– 45 C419407-13 . . . DELETED D

– 50 C419407-14 . . . DELETED D

– 55 C419407-15 . . . DELETED D

– 60 C419405-3 . . . DELETED D

– 65 C419406-525 . . DELETED A D

– 65A C419416-525 . . DELETED B D

– 70 852Z8400-17 . . . DELETED D

– 75 BAC27WCH715 . . . DELETED D

– 80 CDPL776-45 . . . DELETED D

– 85 BAC27WCH270-151 . . . DELETED D

– 90 C419406-3 . . . DELETED A D

– 90A C419416-3 . . . DELETED B D

– 95 C419403-539 . DELETED D
– ITEM NOT ILLUSTRATED

50-11-05 Page 10317

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

2Z – 100 CDPL776-31 . . DELETED D

– 105 BAC27WCH242 . . DELETED D

– 110 CDPL776-47 . . DELETED D

– 115 C419403-39 . . DELETED D

– 120 C419409-527 . DELETED A D

– 120A C419415-527 . DELETED B D

– 125 C419405-527 . . DELETED D

– 130 CDM200-05 . . . DELETED D

– 135 C419407-13 . . . DELETED D

– 140 C419407-14 . . . DELETED D

– 145 C419407-61 . . . DELETED D

– 150 C419405-27 . . . DELETED D

– 155 C419406-527 . . DELETED A D

– 155A C419416-527 . . DELETED B D

– 160 BAC27WCH363 . . . DELETED D

– 165 852Z8400-17 . . . DELETED D

– 170 CDPL776-49 . . . DELETED D

– 175 C419406-27 . . . DELETED A D

– 175A C419416-27 . . . DELETED B D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10318

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Figure 3/GRAPHIC 50-11-05-99B-051-A01

50-11-05 Page 10320

Oct 09/23
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

3 – 1 C419401-141 DELETED A D

– 1A C419410-141 DELETED B D

– 5 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 10 BACS12FA3K8 . DELETED D

– 15 BACW10P304L . DELETED D

***

– 20 BACN11AL1CM . DELETED D

– 25 C419414-3 . DELETED D

– 30 C419402-29 . DELETED D

– 35 C419403-541 . DELETED D

– 40 BAC27WCH201 . . DELETED D

– 45 BAC27WCH251 . . DELETED D

– 50 CDPL776-51 . . DELETED D

– 55 CDM200-05 . . DELETED D

– 60 C419412-1 . . DELETED D

– 65 9485PC . . DELETED D
(V04963)

– 70 C419403-41 . . DELETED D

– 75 C419409-531 . DELETED A D

– 75A C419415-531 . DELETED B D

– 80 C419406-529 . . DELETED D

– 85 C419412-3 . . . DELETED D

– 90 C419406-29 . . . DELETED D

– 95 C419406-531 . . DELETED A D

– 95A C419416-531 . . DELETED B D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10321

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

3 – 100 BAC27WCH369 . . . DELETED D

– 105 852Z8400-17 . . . DELETED D

– 110 BAC27WCH479 . . . DELETED D

– 115 CDPL776-55 . . . DELETED D

– 120 C419412-5 . . . DELETED D

– 125 C419406-31 . . . DELETED A D

– 125A C419416-31 . . . DELETED B D

– 130 C419405-531 . . DELETED D

– 135 BAC27WCH353 . . . DELETED D

– 140 CDPL776-53 . . . DELETED D

– 145 CDM200-05 . . . DELETED D

– 150 C419407-63 . . . DELETED D

– 155 C419407-67 . . . DELETED D

– 160 C419407-65 . . . DELETED D

– 165 C419405-31 . . . DELETED D

– ITEM NOT ILLUSTRATED

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Figure 3A/GRAPHIC 50-11-05-99B-052-A01

50-11-05 Page 10324

Oct 09/23
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

3A – 1 C419401-151 DELETED A D

– 1A C419410-151 DELETED B D

– 5 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 10 BACS12FA3K8 . DELETED D

– 15 BACW10P304L . DELETED D

***

– 20 BACN11AL1CM . DELETED D

– 25 C419414-7 . DELETED D

– 30 C419402-35 . DELETED D

– 35 C419403-551 . DELETED D

– 40 BAC27WCH369 . . DELETED D

– 45 BAC27WCH201 . . DELETED D

– 50 BAC27WCH256 . . DELETED D

– 55 BAC27WCH269-152 . . DELETED D

– 60 C419407-77 . . DELETED D

– 65 C419403-51 . . DELETED D

– 70 C419404-533 . DELETED D

– 75 CDSP1239-501 . . DELETED D

– 80 CDSP1239-1 . . . DELETED D

– 85 CDSP1239-3 . . . DELETED D

– 90 C412901-5 . . DELETED D

– 95 C419407-79 . . DELETED D

– 100 C419407-83 . . DELETED D

– 105 C419407-81 . . DELETED D

– 110 C419413-1 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10325

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

3A ATTACHING PARTS

– 115 MS16535-134 . . DELETED D

– 120 5610-10-15 . . DELETED D

***

– 125 C412413-058 . . DELETED D

– 130 BAC27WCH353 . . DELETED D

– 135 CDPL777-30 . . DELETED D

– 140 BAC27WCH269-152 . . DELETED D

– 145 C419404-33 . . DELETED D

– 150 C419409-537 . DELETED A D

– 150A C419415-537 . DELETED B D

– 155 C419405-537 . . DELETED D

– 160 C419407-89 . . . DELETED D

– 165 C419407-85 . . . DELETED D

– 170 C419407-87 . . . DELETED D

– 175 C419405-37 . . . DELETED D

– 180 C419406-537 . . DELETED A D

– 180A C419416-537 . . DELETED B D

– 185 BAC27WCH363 . . . DELETED D

– 190 852Z8400-17 . . . DELETED D

– 195 CDPL777-39 . . . DELETED D

– 200 BAC27WCH269-152 . . . DELETED D

– 205 C419406-37 . . . DELETED A D

– 205A C419416-37 . . . DELETED B D

– ITEM NOT ILLUSTRATED

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Figure 3B/GRAPHIC 50-11-05-99B-053-A01

50-11-05 Page 10328

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

3B – 1 C419401-149 DELETED D

– 5 BACN11AL1CM . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 C419414-5 . DELETED D

– 30 C419402-33 . DELETED D

– 35 C419404-531 . DELETED D

– 40 CDSP1239-501 . . DELETED D

– 45 CDSP1239-1 . . . DELETED D

– 50 CDSP1239-3 . . . DELETED D

– 55 C412901-5 . . DELETED D

– 60 C419407-43 . . DELETED D

– 65 C419407-73 . . DELETED D

– 70 C419407-71 . . DELETED D

– 75 C419413-1 . . DELETED D

ATTACHING PARTS

– 80 MS16535-134 . . DELETED D

– 85 5610-10-15 . . DELETED D

***

– 90 C412413-058 . . DELETED D

– 95 CDPL768-40 . . DELETED D

– 100 CDPL777-35 . . DELETED D

– 105 BAC27WCH269-152 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10329

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 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

3B – 110 C419404-31 . . DELETED D

– 115 C419403-549 . DELETED D

– 120 CDPL777-37 . . DELETED D

– 125 BAC27WCH269-152 . . DELETED D

– 130 C419407-75 . . DELETED D

– 135 C419403-49 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10330

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Figure 3C/GRAPHIC 50-11-05-99B-054-A01

50-11-05 Page 10332

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

3C – 1 C411151-177 DELETED D

– 5 C411151-081 . DELETED D

– 10 C411151-579 . DELETED D

– 15 BACN11AL1CM . . DELETED D

– 20 C411151-077 . . DELETED D

ATTACHING PARTS

– 25 BACS12FA3K4 . . DELETED D

***

– 30 C411151-079 . . DELETED D

ATTACHING PARTS

– 35 BACS12FA3K4 . . DELETED D

***

– 40 C411152-075 . . DELETED D

ATTACHING PARTS

– 45 BACS12FA3K4 . . DELETED D

***

– 50 BAC27TCH0429 . . DELETED D

– 55 CDPL768-34 . . DELETED D

– 60 CDPL788-2 . . DELETED D

– 65 CDM200-05 . . DELETED D

– 70 C411151-577 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10333

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Figure 3D/GRAPHIC 50-11-05-99B-055-A01

50-11-05 Page 10334

Oct 09/23
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

3D – 1 C412418-117 DELETED D

– 5 C412406-005 . DELETED D

ATTACHING PARTS

– 10 BACN10YR3CM . DELETED D

– 15 NAS1515H3 . DELETED D

– 20 BACS12FA3K8 . DELETED D

***

– 25 C412413-082 . DELETED D

– 30 C412413-084 . DELETED D

– 35 C412413-088 . DELETED D

– 40 C412413-082 . DELETED D

– 45 C412413-084 . DELETED D

– 50 C412413-086 . DELETED D

– 55 SNS512AF . DELETED D

– 60 CDM200-05 . DELETED D

– 65 BAC27WCH366 . DELETED D

– 70 CDPL767-39 . DELETED D

– 75 CDPL776-29 . DELETED D

– 80 BAC27WCH270 . DELETED D

– 85 CDPL776-31 . DELETED D

– 90 CDPL776-27 . DELETED D

– 95 BAC27WCH363 . DELETED D

– 100 C412419-45 . DELETED D

– 105 C412419-43 . DELETED D

– 110 C412410-095 . DELETED D

– 115 C412410-097 . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10335

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

3D – 120 C412410-055 . DELETED D

– ITEM NOT ILLUSTRATED

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Figure 3E/GRAPHIC 50-11-05-99B-056-A01

50-11-05 Page 10338

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

3E – 1 C412418-115 DELETED D

– 5 C412406-005 . DELETED D

ATTACHING PARTS

– 10 BACN10YR3CM . DELETED D

– 15 NAS1515H3 . DELETED D

– 20 BACS12FA3K8 . DELETED D

***

– 25 C412413-056 . DELETED D

ATTACHING PARTS

– 30 MS16535-134 . DELETED D

– 35 5610-10-15 . DELETED D

***

– 40 C412413-058 . DELETED D

– 45 C412413-056 . DELETED D

ATTACHING PARTS

– 50 MS16535-134 . DELETED D

– 55 5610-10-15 . DELETED D

***

– 60 C412413-058 . DELETED D

– 65 CDSP1239-501 . DELETED D

– 70 CDSP1239-1 . . DELETED D

– 75 CDSP1239-3 . . DELETED D

– 80 C412901-5 . DELETED D

– 85 C412413-023 . DELETED D

– 90 C412413-001 . DELETED D

– 95 C412413-028 . DELETED D
– ITEM NOT ILLUSTRATED

50-11-05 Page 10339

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

3E – 100 C412413-029 . DELETED D

– 105 C412413-027 . DELETED D

– 110 CDPL776-25 . DELETED D

– 115 CDPL789-1 . DELETED D

– 120 CDPL767-47 . DELETED D

– 125 CDPL776-19 . DELETED D

– 130 BAC27WCH715 . DELETED D

– 135 CDPL776-15 . DELETED D

– 140 BAC27WEC165 . DELETED D

– 145 BAC27WCH270 . DELETED D

– 150 C412410-007 . DELETED D

– 155 C412410-051 . DELETED D

– 160 C412413-045 . DELETED D

– 165 C412413-046 . DELETED D

– 170 C412413-090 . DELETED D

– 175 C412410-053 . DELETED D

– 180 SNS512AF . DELETED D

– 185 CDM200-05 . DELETED D

– 190 926 . DELETED D

– 195 C412419-47 . DELETED D

– ITEM NOT ILLUSTRATED

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Figure 3F/GRAPHIC 50-11-05-99B-057-A01

50-11-05 Page 10342

Oct 09/23
 COMPONENT MAINTENANCE MANUAL
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

3F – 1 C412418-123 DELETED D

– 5 C412406-030 . DELETED D

ATTACHING PARTS

– 10 BACN10YR3CM . DELETED D

– 15 NAS1515H3 . DELETED D

– 20 BACS12FA3K8 . DELETED D

***

– 25 CDSP1239-501 . DELETED D

– 30 CDSP1239-1 . . DELETED D

– 35 CDSP1239-3 . . DELETED D

– 40 C412901-5 . DELETED D

– 45 C412407-036 . DELETED D

– 50 C412413-037 . DELETED D

– 55 C412407-038 . DELETED D

– 60 C412413-077 . DELETED D

– 65 C412413-095 . DELETED D

– 70 C412407-076 . DELETED D

– 75 SNS512AF . DELETED D

– 80 CDM200-05 . DELETED D

– 85 926 . DELETED D

– 90 9485 . DELETED D

– 95 C412413-056 . DELETED D

ATTACHING PARTS

– 100 MS16535-134 . DELETED D

– 105 5610-10-15 . DELETED D

***
– ITEM NOT ILLUSTRATED

50-11-05 Page 10343

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

3F – 110 C412413-058 . DELETED D

– 115 BAC27WCH363 . DELETED D

– 120 CDPL777-12 . DELETED D

– 125 BAC27WCH269 . DELETED D

– 130 BAC27WCH353 . DELETED D

– 135 CDPL777-30 . DELETED D

– 140 C412419-35 . DELETED D

– 145 C412410-073 . DELETED D

– 150 C412410-075 . DELETED D

– ITEM NOT ILLUSTRATED

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Figure 3G/GRAPHIC 50-11-05-99B-058-A01

50-11-05 Page 10346

Oct 09/23
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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS

STOCK 1234567 CODE PER
NUMBER ASSY

3G – 1 C419410-103 DELETED D

– 5 C419402-41 . DELETED D

– 10 BACN11AL1CM . DELETED D

ATTACHING PARTS

– 15 BACS12FA3K8 . DELETED D

– 20 BACW10P304L . DELETED D

***

– 25 BACN11AL1CM . DELETED D

– 30 C419404-503 . DELETED D

– 35 CDSP1239-501 . . DELETED D

– 40 CDSP1239-1 . . . DELETED D

– 45 CDSP1239-3 . . . DELETED D

– 50 C412901-5 . . DELETED D

– 55 C419407-11 . . DELETED D

– 60 C419407-17 . . DELETED D

– 65 SNS512AF . . DELETED D

– 70 CDM200-05 . . DELETED D

– 75 C419413-1 . . DELETED D

ATTACHING PARTS

– 80 MS16535-134 . . DELETED D

– 85 5610-10-15 . . DELETED D

***

– 90 C412413-058 . . DELETED D

– 95 BAC27WCH277 . . DELETED D

– 100 BAC27WCH122 . . DELETED D

– 105 CDPL767-39 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10347

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FIG. ITEM PART NUMBER AIRLINE NOMENCLATURE EFFECT UNITS
STOCK 1234567 CODE PER
NUMBER ASSY

3G – 110 BAC27WEC165 . . DELETED D

– 115 BAC27WCH211 . . DELETED D

– 120 C419404-3 . . DELETED D

– 125 C419415-503 . DELETED D

– 130 C419405-503 . . DELETED D

– 135 C419407-13 . . . DELETED D

– 140 C419407-14 . . . DELETED D

– 145 C419407-15 . . . DELETED D

– 150 CDM200-05 . . . DELETED D

– 155 C419405-3 . . . DELETED D

– 160 C419416-503 . . DELETED D

– 165 BAC27WCH277 . . . DELETED D

– 170 BAC27WCH228 . . . DELETED D

– 175 BAC27WCH715 . . . DELETED D

– 180 852Z8400-17 . . . DELETED D

– 185 BAC27WCH101 . . . DELETED D

– 190 C419416-3 . . . DELETED D

– 195 C419403-503 . DELETED D

– 200 BAC27WCH277 . . DELETED D

– 205 BAC27WCH221 . . DELETED D

– 210 C419403-3 . . DELETED D

– ITEM NOT ILLUSTRATED

50-11-05 Page 10348

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 COMPONENT MAINTENANCE MANUAL
C41XXXX
STORAGE (INCLUDING TRANSPORTATION)

TASK 50-11-05-550-801-A01
1. Storage Instructions

A. Reason for Job

Self Explanation

B. Job Setup Information

NOTE: You can use equivalent alternatives for the materials given except where indicated. Refer to
9001 for the specifications and where to get the items given.

(1) Tools, Fixtures, and Equipment

Not Applicable

C. Job Setup

Not Applicable

D. Procedure

(1) Preservation

NOTE: The sidewall panel assembly is essentially corrosion resistant and therefore no special
preservation is required.

(2) Packing

(a) Put the sidewall panels in an approved container that will:

– keep them dry

– prevent damage if moved to a different location

(b) Use ESD protection materials.

(3) Storage

(a) Keep the sidewall panels in a storage area that is cool and dry until necessary for use.

(b) Identify the assembly by part number and date of overhaul on a tag or in a convenient
location on the assembly wrapper.

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COMPONENT MAINTENANCE MANUAL
C41XXXX

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