COMPONENT MAINTENANCE

MANUAL

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

MiQ™ 1367870 SERIES
PASSENGER SEATS FOR
VIRGIN AUSTRALIA AIRLINES B737-8 AIRCRAFT

Component Maintenance Manual

(with Illustrated Parts List)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

25-20-83-4667

Gutierrez

COLLINS AEROSPACE PROPRIETARY

NEITHER POSSESSION NOR RECEIPT OF THIS DOCUMENT FROM ANY SOURCE CONSTITUTES
PERMISSION TO USE. USE, COPYING, AND FURTHER DISCLOSURE FOR ANY PURPOSE WITHOUT
EXPRESS WRITTEN PERMISSION FROM COLLINS AEROSPACE MAY RESULT IN CRIMINAL AND/OR
CIVIL LIABILITY.

U.S. Export Classification: EAR 9E991

COLLINS AEROSPACE PROPRIETARY
Subject to the restriction on the cover page.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

U.S. Export Classification: EAR 9E991

COLLINS AEROSPACE PROPRIETARY
Subject to the restriction on the cover page.
THIS PAGE IS INTENTIONALLY LEFT BLANK.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Gutierrez
 MiQ™ 1367870 SERIES
PASSENGER SEATS FOR
VIRGIN AUSTRALIA AIRLINES B737-8 AIRCRAFT

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Component Maintenance Manual
(With Illustrated Parts List)

This manual includes coverage of the following equipment:

1367870-005MS08 1367870-101MS08
1367870-008MS08 1367870-104MS08
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

B/E Aerospace, Inc., a part of Collins Aerospace

Winston-Salem, North Carolina 27105, USA
CAGE Code: V92802

25-20-83-4667
© 2023 Collins Aerospace U.S. Export Classification: EAR 9E991 T-1
COLLINS AEROSPACE PROPRIETARY Initial Issue: Oct 20, 2023
523-0834997 Subject to the restriction on the cover page. Revision 0: Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

We try to supply publications that are free of errors, but some can occur. If a problem is found with this
publication, you can send the necessary data to Collins Aerospace. When you report a specified problem,
give short instructions. Include the publication number, the paragraph or figure number, and the page
number.

To send data to Collins Aerospace about this publication:

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Address: Collins Aerospace
B/E Aerospace, Seating Products Group
190 Oak Plaza Blvd.
Winston-Salem, North Carolina 27105, USA
(336) 767-2000
Email: publications@collins.com

To get access to more technical publications on your account, please visit:

Website: https://www.collinsaerospace.com/Technical-Publications
Email: publications@collins.com

To access the latest technical publications, please visit:

Website: https://www.collinsaerospace.com/Technical-Publications

For technical support, please contact Collins Aerospace Service and Support:
Website: https://www.collinsaerospace.com/what-we-do/service-and-support/support/interiors
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

PUBLICATION COPYRIGHT NOTICE

© 2023 Collins Aerospace

SOFTWARE COPYRIGHT NOTICE

© 2023 Collins Aerospace
All software resident in the equipment covered by this publication is protected by copyright.

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY T-2
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

ALERT
THIS COMPONENT MAINTENANCE MANUAL IDENTIFIES REPLACEMENT PARTS AND
REPAIR PROCEDURES SPECIFICALLY ENGINEERED FOR SEATING PRODUCT
MANUFACTURED BY B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE. B/E PARTS ARE
MANUFACTURED UNDER STRINGENT QUALITY CONTROL PROCESSES. USING
NON-B/E PARTS MAY JEOPARDIZE YOUR WARRANTY AND RESULT IN DEGRADED SEAT
PERFORMANCE. MODIFICATIONS TO B/E SEATING PRODUCTS WHICH HAVE NOT BEEN
APPROVED BY B/E ENGINEERING MAY INVALIDATE THE TSO. ALL MODIFICATIONS

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

SHOULD BE COORDINATED IN ADVANCE TO AVOID THIS POSSIBILITY.

PLEASE REFER TO NO. 25-20-83-4667 or 523-0834997 IN ALL CORRESPONDENCE TO

B/E AEROSPACE REGARDING THIS COMPONENT MAINTENANCE MANUAL AND ILLUSTRATED
PARTS LIST.

TECHNICAL AND WARRANTY SUPPORT

Winston-Salem Interiors CMM Customer Portal: https://www.collinsaerospace.com/Technical-Publications
3D PDF requests by E-mail: ws_techpubs3d@collins.com
Technical and/or warranty support inquiries:
https://www.collinsaerospace.com/what-we-do/service-and-support/support/interiors

This document contains proprietary information of B/E Aerospace, Inc., a part of Collins Aerospace and is
disclosed to the original recipient in strict confidence. Except for rights expressly granted by B/E Aerospace,
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Inc. in writing, the document may not, in whole or in part, be duplicated, reproduced, disclosed or used for
any unauthorized purpose or by any unauthorized person without prior direct written authorization from
B/E Aerospace, Inc. Any document updates, changes or modifications for the original recipient do not
transfer to subsequent owners of these seating products.

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY T-3
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY T-4
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

LIST OF EFFECTIVE PAGES

SECTION PAGE DATE SECTION PAGE DATE

TITLE PAGE DESCRIPTION AND OPERATION

T-1 Oct 20, 2023 1 Oct 20, 2023
T-2 Oct 20, 2023 2 Oct 20, 2023
T-3 Oct 20, 2023 3 Oct 20, 2023

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

T-4 Oct 20, 2023 4 Oct 20, 2023
LIST OF EFFECTIVE PAGES
5 Oct 20, 2023
6 Oct 20, 2023
LEP-1 Oct 20, 2023 7 Oct 20, 2023
LEP-2 Oct 20, 2023 8 Oct 20, 2023
LEP-3 Oct 20, 2023 9 Oct 20, 2023
LEP-4 Oct 20, 2023 10 Oct 20, 2023
LEP-5 Oct 20, 2023 11 Oct 20, 2023
LEP-6 Oct 20, 2023 12 Oct 20, 2023
RECORD OF REVISIONS 13 Oct 20, 2023
RR-1 Oct 20, 2023 14 Oct 20, 2023
RR-2 Oct 20, 2023 15 Oct 20, 2023
16 Oct 20, 2023
RECORD OF TEMPORARY REVISIONS 17 Oct 20, 2023
RTR-1 Oct 20, 2023 18 Oct 20, 2023
RTR-2 Oct 20, 2023 19 Oct 20, 2023
20 Oct 20, 2023
SERVICE BULLETIN LIST 21 Oct 20, 2023
SB-1 Oct 20, 2023 22 Oct 20, 2023
SB-2 Oct 20, 2023 23 Oct 20, 2023
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

24 Oct 20, 2023

TABLE OF CONTENTS
25 Oct 20, 2023
TOC-1 Oct 20, 2023 26 Oct 20, 2023
TOC-2 Oct 20, 2023 27 Oct 20, 2023
TOC-3 Oct 20, 2023 28 Oct 20, 2023
TOC-4 Oct 20, 2023 29 Oct 20, 2023
INTRODUCTION 30 Oct 20, 2023
31 Oct 20, 2023
INTRO-1 Oct 20, 2023 32 Oct 20, 2023
INTRO-2 Oct 20, 2023 33 Oct 20, 2023
INTRO-3 Oct 20, 2023 34 Oct 20, 2023
INTRO-4 Oct 20, 2023 35 Oct 20, 2023
INTRO-5 Oct 20, 2023 36 Oct 20, 2023 Gutierrez
INTRO-6 Oct 20, 2023 37 Oct 20, 2023
INTRO-7 Oct 20, 2023 38 Oct 20, 2023
INTRO-8 Oct 20, 2023 39 Oct 20, 2023
INTRO-9 Oct 20, 2023 40 Oct 20, 2023
INTRO-10 Oct 20, 2023 41 Oct 20, 2023
INTRO-11 Oct 20, 2023 42 Oct 20, 2023
INTRO-12 Oct 20, 2023 43 Oct 20, 2023
44 Oct 20, 2023

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY LEP-1
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

SECTION PAGE DATE SECTION PAGE DATE

DESCRIPTION AND OPERATION (CONTINUED) DISASSEMBLY (CONTINUED)
45 Oct 20, 2023 3008 Oct 20, 2023
46 Oct 20, 2023 3009 Oct 20, 2023
47 Oct 20, 2023 3010 Oct 20, 2023
48 Oct 20, 2023 3011 Oct 20, 2023
49 Oct 20, 2023 3012 Oct 20, 2023

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

50 Oct 20, 2023 3013 Oct 20, 2023
51 Oct 20, 2023 3014 Oct 20, 2023
52 Oct 20, 2023 3015 Oct 20, 2023
3016 Oct 20, 2023
TESTING AND FAULT ISOLATION
3017 Oct 20, 2023
1001 Oct 20, 2023 3018 Oct 20, 2023
1002 Oct 20, 2023 3019 Oct 20, 2023
1003 Oct 20, 2023 3020 Oct 20, 2023
1004 Oct 20, 2023 3021 Oct 20, 2023
1005 Oct 20, 2023 3022 Oct 20, 2023
1006 Oct 20, 2023 3023 Oct 20, 2023
1007 Oct 20, 2023 3024 Oct 20, 2023
1008 Oct 20, 2023
CLEANING
SCHEMATIC AND WIRING DIAGRAMS 4001 Oct 20, 2023
4002 Oct 20, 2023
2001 Oct 20, 2023 4003 Oct 20, 2023
2002 Oct 20, 2023 4004 Oct 20, 2023
2003 Oct 20, 2023 4005 Oct 20, 2023
2004 Oct 20, 2023 4006 Oct 20, 2023
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

2005 Oct 20, 2023 4007 Oct 20, 2023

2006 Oct 20, 2023 4008 Oct 20, 2023
2007 Oct 20, 2023 4009 Oct 20, 2023
2008 Oct 20, 2023 4010 Oct 20, 2023
2009 Oct 20, 2023 4011 Oct 20, 2023
2010 Oct 20, 2023 4012 Oct 20, 2023
2011 Oct 20, 2023 4013 Oct 20, 2023
2012 Oct 20, 2023 4014 Oct 20, 2023
2013 Oct 20, 2023
2014 Oct 20, 2023 INSPECTION/CHECK
2015 Oct 20, 2023 5001 Oct 20, 2023
2016 Oct 20, 2023 5002 Oct 20, 2023
5003 Oct 20, 2023 Gutierrez
DISASSEMBLY
5004 Oct 20, 2023
3001 Oct 20, 2023 5005 Oct 20, 2023
3002 Oct 20, 2023 5006 Oct 20, 2023
3003 Oct 20, 2023
3004 Oct 20, 2023 REPAIR
3005 Oct 20, 2023 6001 Oct 20, 2023
3006 Oct 20, 2023 6002 Oct 20, 2023
3007 Oct 20, 2023 6003 Oct 20, 2023

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY LEP-2
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

SECTION PAGE DATE SECTION PAGE DATE

REPAIR (CONTINUED) ASSEMBLY (CONTINUED)
6004 Oct 20, 2023 7028 Oct 20, 2023
6005 Oct 20, 2023 7029 Oct 20, 2023
6006 Oct 20, 2023 7030 Oct 20, 2023
6007 Oct 20, 2023
FITS AND CLEARANCES
6008 Oct 20, 2023

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

6009 Oct 20, 2023 8001 Oct 20, 2023
6010 Oct 20, 2023 8002 Oct 20, 2023
6011 Oct 20, 2023
SPECIAL TOOLS, FIXTURES, AND EQUIPMENT
6012 Oct 20, 2023
6013 Oct 20, 2023 9001 Oct 20, 2023
6014 Oct 20, 2023 9002 Oct 20, 2023
6015 Oct 20, 2023 9003 Oct 20, 2023
6016 Oct 20, 2023 9004 Oct 20, 2023
6017 Oct 20, 2023 9005 Oct 20, 2023
6018 Oct 20, 2023 9006 Oct 20, 2023
6019 Oct 20, 2023 9007 Oct 20, 2023
6020 Oct 20, 2023 9008 Oct 20, 2023
9009 Oct 20, 2023
ASSEMBLY 9010 Oct 20, 2023
7001 Oct 20, 2023
ILLUSTRATED PARTS LIST
7002 Oct 20, 2023
7003 Oct 20, 2023 10001 Oct 20, 2023
7004 Oct 20, 2023 10002 Oct 20, 2023
7005 Oct 20, 2023 10003 Oct 20, 2023
7006 Oct 20, 2023 10004 Oct 20, 2023
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

7007 Oct 20, 2023 10005 Oct 20, 2023

7008 Oct 20, 2023 10006 Oct 20, 2023
7009 Oct 20, 2023 10007 Oct 20, 2023
7010 Oct 20, 2023 10008 Oct 20, 2023
7011 Oct 20, 2023 10009 Oct 20, 2023
7012 Oct 20, 2023 10010 Oct 20, 2023
7013 Oct 20, 2023 10011 Oct 20, 2023
7014 Oct 20, 2023 10012 Oct 20, 2023
7015 Oct 20, 2023 10013 Oct 20, 2023
7016 Oct 20, 2023 10014 Oct 20, 2023
7017 Oct 20, 2023 10015 Oct 20, 2023
7018 Oct 20, 2023 10016 Oct 20, 2023
7019 Oct 20, 2023 10017 Oct 20, 2023 Gutierrez
7020 Oct 20, 2023 10018 Oct 20, 2023
7021 Oct 20, 2023 10019 Oct 20, 2023
7022 Oct 20, 2023 10020 Oct 20, 2023
7023 Oct 20, 2023 10021 Oct 20, 2023
7024 Oct 20, 2023 10022 Oct 20, 2023
7025 Oct 20, 2023 10023 Oct 20, 2023
7026 Oct 20, 2023 10024 Oct 20, 2023
7027 Oct 20, 2023 10025 Oct 20, 2023

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY LEP-3
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

SECTION PAGE DATE SECTION PAGE DATE

ILLUSTRATED PARTS LIST (CONTINUED) ILLUSTRATED PARTS LIST (CONTINUED)
10026 Oct 20, 2023 10072 Oct 20, 2023
10027 Oct 20, 2023 10073 Oct 20, 2023
10028 Oct 20, 2023 10074 Oct 20, 2023
10029 Oct 20, 2023 10075 Oct 20, 2023
10030 Oct 20, 2023 10076 Oct 20, 2023

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

10031 Oct 20, 2023 10077 Oct 20, 2023
10032 Oct 20, 2023 10078 Oct 20, 2023
10033 Oct 20, 2023 10079 Oct 20, 2023
10034 Oct 20, 2023 10080 Oct 20, 2023
10035 Oct 20, 2023 10081 Oct 20, 2023
10036 Oct 20, 2023 10082 Oct 20, 2023
10037 Oct 20, 2023 10083 Oct 20, 2023
10038 Oct 20, 2023 10084 Oct 20, 2023
10039 Oct 20, 2023 10085 Oct 20, 2023
10040 Oct 20, 2023 10086 Oct 20, 2023
10041 Oct 20, 2023 10087 Oct 20, 2023
10042 Oct 20, 2023 10088 Oct 20, 2023
10043 Oct 20, 2023 10089 Oct 20, 2023
10044 Oct 20, 2023 10090 Oct 20, 2023
10045 Oct 20, 2023 10091 Oct 20, 2023
10046 Oct 20, 2023 10092 Oct 20, 2023
10047 Oct 20, 2023 10093 Oct 20, 2023
10048 Oct 20, 2023 10094 Oct 20, 2023
10049 Oct 20, 2023 10095 Oct 20, 2023
10050 Oct 20, 2023 10096 Oct 20, 2023
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

10051 Oct 20, 2023 10097 Oct 20, 2023

10052 Oct 20, 2023 10098 Oct 20, 2023
10053 Oct 20, 2023 10099 Oct 20, 2023
10054 Oct 20, 2023 10100 Oct 20, 2023
10055 Oct 20, 2023 10101 Oct 20, 2023
10056 Oct 20, 2023 10102 Oct 20, 2023
10057 Oct 20, 2023 10103 Oct 20, 2023
10058 Oct 20, 2023 10104 Oct 20, 2023
10059 Oct 20, 2023 10105 Oct 20, 2023
10060 Oct 20, 2023 10106 Oct 20, 2023
10061 Oct 20, 2023 10107 Oct 20, 2023
10062 Oct 20, 2023 10108 Oct 20, 2023
10063 Oct 20, 2023 10109 Oct 20, 2023 Gutierrez
10064 Oct 20, 2023 10110 Oct 20, 2023
10065 Oct 20, 2023 10111 Oct 20, 2023
10066 Oct 20, 2023 10112 Oct 20, 2023
10067 Oct 20, 2023 10113 Oct 20, 2023
10068 Oct 20, 2023 10114 Oct 20, 2023
10069 Oct 20, 2023 10115 Oct 20, 2023
10070 Oct 20, 2023 10116 Oct 20, 2023
10071 Oct 20, 2023 10117 Oct 20, 2023

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY LEP-4
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

SECTION PAGE DATE SECTION PAGE DATE

ILLUSTRATED PARTS LIST (CONTINUED) ILLUSTRATED PARTS LIST (CONTINUED)
10118 Oct 20, 2023 10164 Oct 20, 2023
10119 Oct 20, 2023 10165 Oct 20, 2023
10120 Oct 20, 2023 10166 Oct 20, 2023
10121 Oct 20, 2023 10167 Oct 20, 2023
10122 Oct 20, 2023 10168 Oct 20, 2023

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

10123 Oct 20, 2023 10169 Oct 20, 2023
10124 Oct 20, 2023 10170 Oct 20, 2023
10125 Oct 20, 2023 10171 Oct 20, 2023
10126 Oct 20, 2023 10172 Oct 20, 2023
10127 Oct 20, 2023 10173 Oct 20, 2023
10128 Oct 20, 2023 10174 Oct 20, 2023
10129 Oct 20, 2023 10175 Oct 20, 2023
10130 Oct 20, 2023 10176 Oct 20, 2023
10131 Oct 20, 2023 10177 Oct 20, 2023
10132 Oct 20, 2023 10178 Oct 20, 2023
10133 Oct 20, 2023 10179 Oct 20, 2023
10134 Oct 20, 2023 10180 Oct 20, 2023
10135 Oct 20, 2023 10181 Oct 20, 2023
10136 Oct 20, 2023 10182 Oct 20, 2023
10137 Oct 20, 2023 10183 Oct 20, 2023
10138 Oct 20, 2023 10184 Oct 20, 2023
10139 Oct 20, 2023 10185 Oct 20, 2023
10140 Oct 20, 2023 10186 Oct 20, 2023
10141 Oct 20, 2023 10187 Oct 20, 2023
10142 Oct 20, 2023 10188 Oct 20, 2023
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

10143 Oct 20, 2023 10189 Oct 20, 2023

10144 Oct 20, 2023 10190 Oct 20, 2023
10145 Oct 20, 2023 10191 Oct 20, 2023
10146 Oct 20, 2023 10192 Oct 20, 2023
10147 Oct 20, 2023 10193 Oct 20, 2023
10148 Oct 20, 2023 10194 Oct 20, 2023
10149 Oct 20, 2023 10195 Oct 20, 2023
10150 Oct 20, 2023 10196 Oct 20, 2023
10151 Oct 20, 2023 10197 Oct 20, 2023
10152 Oct 20, 2023 10198 Oct 20, 2023
10153 Oct 20, 2023 10199 Oct 20, 2023
10154 Oct 20, 2023 10200 Oct 20, 2023
10155 Oct 20, 2023 10201 Oct 20, 2023 Gutierrez
10156 Oct 20, 2023 10202 Oct 20, 2023
10157 Oct 20, 2023 10203 Oct 20, 2023
10158 Oct 20, 2023 10204 Oct 20, 2023
10159 Oct 20, 2023 10205 Oct 20, 2023
10160 Oct 20, 2023 10206 Oct 20, 2023
10161 Oct 20, 2023 10207 Oct 20, 2023
10162 Oct 20, 2023 10208 Oct 20, 2023
10163 Oct 20, 2023 10209 Oct 20, 2023

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY LEP-5
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

SECTION PAGE DATE SECTION PAGE DATE

ILLUSTRATED PARTS LIST (CONTINUED) ILLUSTRATED PARTS LIST (CONTINUED)
10210 Oct 20, 2023 10256 Oct 20, 2023
10211 Oct 20, 2023 10257 Oct 20, 2023
10212 Oct 20, 2023 10258 Oct 20, 2023
10213 Oct 20, 2023 10259 Oct 20, 2023
10214 Oct 20, 2023 10260 Oct 20, 2023

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

10215 Oct 20, 2023 10261 Oct 20, 2023
10216 Oct 20, 2023 10262 Oct 20, 2023
10217 Oct 20, 2023 10263 Oct 20, 2023
10218 Oct 20, 2023 10264 Oct 20, 2023
10219 Oct 20, 2023 10265 Oct 20, 2023
10220 Oct 20, 2023 10266 Oct 20, 2023
10221 Oct 20, 2023
10222 Oct 20, 2023 USING 3D ELECTRICAL DRAWINGS
10223 Oct 20, 2023 17001 Oct 20, 2023
10224 Oct 20, 2023 17002 Oct 20, 2023
10225 Oct 20, 2023 17003 Oct 20, 2023
10226 Oct 20, 2023 17004 Oct 20, 2023
10227 Oct 20, 2023 17005 Oct 20, 2023
10228 Oct 20, 2023 17006 Oct 20, 2023
10229 Oct 20, 2023 17007 Oct 20, 2023
10230 Oct 20, 2023 17008 Oct 20, 2023
10231 Oct 20, 2023
10232 Oct 20, 2023
10233 Oct 20, 2023
10234 Oct 20, 2023
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

10235 Oct 20, 2023

10236 Oct 20, 2023
10237 Oct 20, 2023
10238 Oct 20, 2023
10239 Oct 20, 2023
10240 Oct 20, 2023
10241 Oct 20, 2023
10242 Oct 20, 2023
10243 Oct 20, 2023
10244 Oct 20, 2023
10245 Oct 20, 2023
10246 Oct 20, 2023
10247 Oct 20, 2023 Gutierrez
10248 Oct 20, 2023
10249 Oct 20, 2023
10250 Oct 20, 2023
10251 Oct 20, 2023
10252 Oct 20, 2023
10253 Oct 20, 2023
10254 Oct 20, 2023
10255 Oct 20, 2023

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY LEP-6
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RECORD OF REVISIONS

REV REV
NO. ISSUE DATE DATE INSERTED BY NO. ISSUE DATE DATE INSERTED BY
00 Oct 20, 2023

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY RR-1
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY RR-2
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RECORD OF TEMPORARY REVISIONS

TEMPORARY REV NO. PAGE NUMBER ISSUE DATE INSERT DATE BY DATE REMOVED BY

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY RTR-1
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY RTR-2
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

SERVICE BULLETIN LIST

Service Bulletins (SBs) are B/E Aerospace engineering documents that authorize customers
to modify B/E seating products. B/E Aerospace files all SBs with the Federal Aviation
Administration (FAA).

All SBs that direct mandatory implementation will be incorporated into the Component
Maintenance Manual (CMM). Optional SBs are implemented at the discretion of the customer.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

B/E Aerospace will incorporate only those optional SBs that the customer informs us have been
implemented. Incorporation can occur in three ways:

A. Scheduled CMM Revision - B/E Aerospace incorporates part number changes, SBs and other
customer-requested changes into the next scheduled CMM revision.

B. Quick Revision - Part number changes that occur between scheduled full CMM revisions are
addressed by Quick Revisions. These Quick Revisions are minimal in nature and are
designed to facilitate procurement of correct parts.

C. Attachments - SBs, as well as Service Letters (SLs) may be added to this CMM as
attachments, and if so will be listed as such in the Table of Contents.

NOTE: The CMM user can verify at any time whether the SB(s) or SL(s) included as
attachments or listed below are the current revision release by going to the public
B/E Aerospace, Inc., a part of Collins Aerospace CMM Index online at:
https://portal.rockwellcollins.com/web/publications-and-training. The link for
the “Interiors Seating Technical Publications Index” can be accessed under the
“Registration Tutorials” heading.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

DATE
SB NUMBER REV TITLE DATE INCORPORATED
25-GENXMIQ-05 A MiQ™ / All Customers / All Aircraft Aug 24, 2020 Oct 20, 2023
Types / Installation of Armrest FOD
Seal

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY SB-1
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY SB-2
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

TABLE OF CONTENTS

SECTION PAGE
LIST OF EFFECTIVE PAGES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEP-1
RECORD OF REVISIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RR-1
RECORD OF TEMPORARY REVISIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RTR-1
SERVICE BULLETIN LIST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SB-1
INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INTRO-1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

DESCRIPTION AND OPERATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
TESTING AND FAULT ISOLATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1001
SCHEMATIC AND WIRING DIAGRAMS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2001
DISASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3001
CLEANING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4001
INSPECTION/CHECK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5001
REPAIR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6001
ASSEMBLY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7001
FITS AND CLEARANCES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8001
SPECIAL TOOLS, FIXTURES, AND EQUIPMENT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9001
ILLUSTRATED PARTS LIST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10001
IPL Figure 01: Seat Assembly - Double . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10034
IPL Figure 02: Cable Routing. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10044
IPL Figure 03: Installation - Legrest . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10050
IPL Figure 04: Legrest Assembly. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10056
IPL Figure 05: Paddle Assembly - Legrest . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10064
IPL Figure 06: Frame Link Assembly. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10070
IPL Figure 07: Link Assembly - Legrest . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10076
IPL Figure 08: Installation - Seatpan Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . 10080
IPL Figure 09: Installation - Seatpan Support . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10082
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

IPL Figure 10: Seatpan Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10084

IPL Figure 11: Headrest Frame Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10086
IPL Figure 12: Installation - Video Bezel and Upper Literature Pocket Assembly . 10088
IPL Figure 13: Installation - Coat Hook . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10090
IPL Figure 14: Installation - Lower Literature Assembly and Back Trim . . . . . . . . . 10092
IPL Figure 15: Installation - Back Assembly. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10096
IPL Figure 16: Back Assembly - Riveted . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10102
IPL Figure 17: Quadrant Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10112
IPL Figure 18: Installation - Electrical . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10116
IPL Figure 19: Installation - Lower Console . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10126
IPL Figure 20: Installation - Center Console . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10132
IPL Figure 21: Center Console Assembly - Non-Video . . . . . . . . . . . . . . . . . . . . . . 10134
IPL Figure 22: Cocktail Table Assembly. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10146 Gutierrez
IPL Figure 23: Button Assembly - Seat Control . . . . . . . . . . . . . . . . . . . . . . . . . . . 10148
IPL Figure 24: Pocket Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10152
IPL Figure 25: Trim Assembly - Front . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10158
IPL Figure 26: Console Structure Assembly - Non-Video . . . . . . . . . . . . . . . . . . . . 10160
IPL Figure 27: Installation - Foodtray Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . 10166
IPL Figure 28: Foodtray Assembly. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10168
IPL Figure 29: Installation - Endbay . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10178
IPL Figure 30: Endbay Assembly - IUL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10180

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY TOC-1
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

IPL Figure 31: Button Assembly - Endbay Arm . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10194

IPL Figure 32: Endbay Bracket Assembly - INBD . . . . . . . . . . . . . . . . . . . . . . . . . 10196
IPL Figure 33: Bowtie Assembly - Endbay Arm . . . . . . . . . . . . . . . . . . . . . . . . . . . 10200
IPL Figure 34: Endbay Arm Assembly - INBD . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10206
IPL Figure 35: Frame Assembly - Endbay Arm . . . . . . . . . . . . . . . . . . . . . . . . . . . 10210
IPL Figure 36: Wall Endbay Assembly - Special . . . . . . . . . . . . . . . . . . . . . . . . . . . 10216
IPL Figure 37: Endbay Wall Arm Assembly - Special . . . . . . . . . . . . . . . . . . . . . . . 10224
IPL Figure 38: Table Latch Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10228

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

IPL Figure 39: Frame Assembly - Endbay Arm - Outer . . . . . . . . . . . . . . . . . . . . . . 10230
IPL Figure 40: Installation - Shroud . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10236
IPL Figure 41: Installation - Electrical Raceway. . . . . . . . . . . . . . . . . . . . . . . . . . . . 10242
IPL Figure 42: Installation - Baggage Bar . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10248
IPL Figure 43: Frame Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10250
IPL Figure 44: Spreader Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10254
IPL Figure 45: Leg Assembly. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10260
IPL Figure 46: Vendor Refurbishment Parts [REF No. WK0044]. . . . . . . . . . . . . . . 10264
USING 3D ELECTRICAL DRAWINGS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .17001

ATTACHMENTS :
NOTE: Collins Aerospace controlled documents and/or drawings and vendor calibration
documents provided as attachments to this CMM were the revision release
available at the time of the release of this CMM. The CMM user is advised to
check with Collins Aerospace and/or the vendor for the latest revision of the
document or drawing listed below.

NOTE: Vendor controlled document(s) and/or drawing(s) referenced in this CMM, and not
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

shown in the attachment list below, must be verified and obtained through the
applicable vendor. The CMM user is advised to check with the vendor to obtain the
latest revision of the document(s) and/or drawing(s). Vendor contact information is
listed in the INTRODUCTION page block of this CMM.

NOTE: In order to view the attachments, click on the “paper clip” in the tool bar to the far
left of the document in Adobe Acrobat®.
01: B/E Aerospace Service Letter (SL) SL-16-051, Revision (Rev) A - Adjust MiQ™
Foodtray and HCEB Deployment / Generic / All
02: B/E Aerospace SL-20-065, Rev B - All B/E Aerospace Interior Products /
Discoloration of Cabin Interior Products Due to Application of Cleaning
Products and Disinfectants Gutierrez
03: B/E Aerospace SL-21-015, Rev A - Generic / MiQ™ Replacement of Endbay
Shroud Clips

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY TOC-2
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

3D PDF ELECTRICAL INSTALLATIONS:

NOTE: 3D PDF Electrical Installation drawings associated with this CMM are available
upon request. All 3D PDF electrical installations are listed below. Requests for
3D PDFs should be sent to the following: ws_techpubs3d@collins.com
NOTE: DO NOT use part numbers contained in the 3D PDF to order parts. Always use the
part numbers contained in the ILLUSTRATED PARTS LIST for parts ordering.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

01: 1097112-701 - Revision B - Electrical 3D PDF
02: 1097112-703 - Revision A - Electrical 3D PDF
03: 1097112-705 - Revision B - Electrical 3D PDF
04: 1097112-707 - Revision A - Electrical 3D PDF
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY TOC-3
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY TOC-4
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

INTRODUCTION

1. Purpose and Scope of This Manual

This Component Maintenance Manual (CMM) contains descriptive information, maintenance

procedures and an Illustrated Parts List (IPL) for Virgin Australia Airlines B737-8 Aircraft,
equipped with MiQ™ 1367870 Series passenger seats manufactured by B/E Aerospace, Seating
Products Group, 190 Oak Plaza Blvd., Winston-Salem, North Carolina 27105.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

The CMM user can verify at any time whether the CMM in hand is the current revision issued
to it by going to the Winston-Salem Interiors CMM Customer Portal. You do not have to be a
registered user to complete a search for publications. The “Publication Type” for all
Winston-Salem Interiors should be set to “CMMPL” (Component Maintenance Manual with Parts
List) for the search criteria. The Winston-Salem Interiors CMM Customer Portal is located at:
https://www.collinsaerospace.com/Technical-Publications

2. Product Support Services

TECHNICAL AND WARRANTY SUPPORT

Winston-Salem Interiors CMM Customer Portal: https://www.collinsaerospace.com/Technical-Publications
3D PDF requests by E-mail: ws_techpubs3d@collins.com
Technical and/or warranty support inquiries:
https://www.collinsaerospace.com/what-we-do/service-and-support/support/interiors

3. Verification
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

The following sections in this Component Maintenance Manual (CMM) are approved. The
applicable tasks of Testing and Fault Isolation using verification by simulation were completed
through the Technical Publications Department via approved and released engineering
documentation.

SECTION PAGE BLOCK DATE

Testing and Fault Isolation 1001-1999 Oct 20, 2023
Disassembly 3001-3999 Oct 20, 2023
Assembly 7001-7999 Oct 20, 2023
Gutierrez
4. Maintenance Concept

A. This CMM supports seat maintenance activities that may be reasonably done by first-tier
maintenance personnel. This includes routine servicing and maintenance needed to maintain
the B/E Aerospace seating system in a satisfactory operating condition throughout its life
cycle. Areas addressed in this CMM include:

(1) Required inspections and checks designed to ensure safety and operational readiness.

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY INTRO-1
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

(2) Fault isolation procedures for identifying components that may need adjustment or
replacement.

(3) Step-by-step disassembly and assembly instructions enabling technicians to remove

and replace line-replaceable assemblies.

(4) Commonly recurring adjustment and repair procedures.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(5) Required tools and equipment.

(6) Tolerances and torque values.

(7) Detailed illustrations of the major assemblies and installations, with listings of all
procurable items replaceable within the scope of the maintenance instructions.

(8) Information regarding the incorporation of Service Bulletins/Letters.

B. This CMM does not support the repair of riveted, welded, or bonded assemblies. Repair of
these types of assemblies can lead to a loss of structural integrity. Since these assemblies
have very low incidences of failure under normal operating conditions, they are treated as the
lowest replaceable assemblies in the maintenance concept for this seat.

5. Arrangement of This CMM

This CMM is arranged in the following sections to facilitate the presentation of maintenance
instructions.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

SECTION PAGE BLOCK

Description and Operation 1-999
Testing and Fault Isolation 1001-1999
Schematic and Wiring Diagrams 2001-2999
Disassembly 3001-3999
Cleaning 4001-4999
Inspection/Check 5001-5999
Repair 6001-6999
Assembly 7001-7999 Gutierrez

Fits and Clearances 8001-8999

Special Tools, Fixtures, and Equipment 9001-9999
Illustrated Parts List 10001-10999
Using 3D Electrical Drawings 17001-17999

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY INTRO-2
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 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

6. WARNINGS, CAUTIONS, and NOTES

Throughout this CMM there are points where special attention or clarification is needed.
There are three categories: WARNING, CAUTION, and NOTE. The purpose of each and how
they appear in the CMM are as follows:

WARNING: THE USE OF A WARNING STATEMENT INDICATES POTENTIALLY

DANGEROUS MATERIALS, METHODS, OR PROCEDURES. SPECIAL CARE
MUST BE TAKEN TO PREVENT BODILY INJURY.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

CAUTION: THE CAUTION STATEMENT INDICATES A METHOD OR PROCEDURE THAT
MUST BE FOLLOWED PRECISELY IN ORDER TO AVOID DAMAGE TO PARTS
OR EQUIPMENT.

NOTE: The NOTE statement clarifies data or procedures to prevent misunderstandings and
difficulty performing instructions.

7. List of Abbreviations

The following abbreviations may be used in this CMM:

ABBREVIATION EXPANSION
AAIR® AmSafe® Aviation Inflatable Restraint
A/C Aircraft
AC Alternating Current
ACO Arm Cap Open
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

ACOU AC Outlet
ALT Alternate
A/R Armrest
AR As Required
ASSY Assembly
ATA Air Transportation Association of America
AUH Active USB Hub
AUX Auxiliary
B/C Business Class Gutierrez
BK Back
BKDN Breakdown
BL Butt Line
BMDH Back-Mounted Device Holder
BMFT Back-Mounted Foodtray

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY INTRO-3
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

ABBREVIATION EXPANSION
BMV Back-Mounted Video
B/O Breakover
BTM Bottom
CAS Cabin Attendant Seat
CCR Credit Card Reader

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

CCW Counterclockwise
CFE Customer-Furnished Equipment
CFR Code of Federal Regulations
CFU Cabin Fiber Unit
CMM Component Maintenance Manual
CMMPL Component Maintenance Manual with Parts List
CRES Corrosion Resistant Steel
CRP Cushion Reference Point
CRPH Cushion Reference Point Height
CSK Countersunk
CTR Center
CTS Cushion to Stud
CW Clockwise
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

DBL Double
DC Direct Current
DCPS DC Power Supply
DECLAM Decorative Laminate
DET Detailed
DET BKDN Detailed Breakdown
DISC Disconnect
DOC Document
DOM Digital Overhead Monitor Gutierrez
DOT Department of Transportation
DPCU Digital Passenger Control Unit
DSEBI Digital Seat Electronics Box Interface
EAR Export Administration Regulation
EASA European Aviation Safety Agency

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY INTRO-4
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

ABBREVIATION EXPANSION
E/B Endbay
ECB Electronics Control Box
ECCN Export Control Classification Number
ECU Electronics Control Unit
EEPL Emergency Escape Path Light

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

EEPMS Emergency Escape Path Marking System
EFF Effectivity
EMA Electronic Module Assembly
EMI Electro-Magnetic Interference
ENVIR Environmental
EPL Emergency Path Light
ESDS Electrostatic Discharge Sensitive
eSIB Electronic Seat Interface Box
ETSO European Technical Standard Order
EWIS Electrical Wiring Interconnecting Systems
FAA Federal Aviation Administration
FAR Federal Aviation Regulation
FB Fireblocking
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

FBL Fireblocking Layer

F/C First Class
FH Firehard
FIG Figure
FLDG Folding
FNOB Forward Narrow O/B
FOA Front of Armrest
F/R Front Row
F/T Foodtray Gutierrez
FT-LB Foot-Pounds
FTL Flight Time Limitations
FWD Forward
GA General Arrangement
GND Ground (Electrical)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY INTRO-5
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

ABBREVIATION EXPANSION
HCEB Handicapped Endbay
HD Head
HEX Hexagonal
HGT Height
HIC Head Injury Criteria

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

HMAR Hatch-Mounted Armrest
HPS High Power Seatbox
IAFT In-Arm Foodtray
IAT In-Arm Table
IAV In-Arm Video
I/B Inboard
ICA Instructions for Continued Airworthiness
ICM Interface Control Module
ID Identification
IDENT Identity
IFE In-Flight Entertainment
IIL Installation Instructions and Limitations
INBD Inboard
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

INT’L International
IN-LB Inch-Pounds
IN-LBF Inch-Pounds Force
INSTL Installation
IPL Illustrated Parts List
ISM In-Seat Monitor
ISPC In-Seat Power Control
ISPS In-Seat Power Supply
ISPSU In-Seat Power Supply Unit Gutierrez
ITU Integrated Tablet Unit
IUL In-Use Light
JAR Joint Aviation Requirement
JPB Junction Power Box
KDB Keypad Driving Interface Box

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY INTRO-6
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

ABBREVIATION EXPANSION
KDU Keypad Driving Interface Unit
LCD Liquid Crystal Display
LED Light Emitting Diode
LH Left Hand
LIT Literature

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

LK Lock
LKG Locking
LRD Leg Rest Deployed
LRG Large
LRU Line-Replaceable Unit
LSR Load Spreading Rivet
LT Light
LWR Lower
MAX Maximum
MC Mechanical Lock
MCC Mechanical Control Cable
MCE Main Cabin Extra
MCSU Mechanical Crash Sensor Unit
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

MECH Mechanical
MEK Methyl Ethyl Ketone
MIBK Methyl Isobutyl Ketone
MOR Manual Override
MSDS Material Safety Data Sheet
MSN Manufacturer Serial Number
MUX Multiplexer
N/A Not Applicable
NC Not Connected Gutierrez
NHA Next Higher Assembly
NOB Narrow O/B
N-m Newton-Meter
NOC Narrow O/B and Center
NP Non-Procurable

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY INTRO-7
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 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

ABBREVIATION EXPANSION
NRW Narrow
O/B Outboard
OEM Original Equipment Manufacturer
OHCR Overhead Crew Rest
OU Outlet Unit

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

OUTBD Outboard
OWE Overwing Exit
PAX Passenger
PCM Passenger Control Module
PCP Passenger Computer Power
PCU Passenger Control Unit
PDM Power Distribution Module
PED Portable Electronic Device
PES Passenger Entertainment System
P/N Part Number
PMU Passenger Media Unit
PNP Plug-N-Play
PPUI PC Power Use Indicator
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

PRM Provision for Reduced Mobility

PROX Proximity
PSI Pounds per Square Inch
PSM Power Supply Module
PVT Pivot
PWR Power
QAM Quadrature Amplitude Modulation
QR Code Quick Read Code
QTY Quantity Gutierrez
QUAD Quadruple
QUINT Quintuple
REC Recline
RED Reduced
REF Refer To / Reference

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

ABBREVIATION EXPANSION
RF Radio Frequency
RF Reference Only
RFID Radio Frequency Identification
RH Right Hand
RJU Remote Jack Unit

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

RPO Remote Power Outlet
RR Rear
RTN Return
S2S Seat-to-Seat
SACS Seat Actuation Control System
SAO Seating Aftermarket Operations
SB Service Bulletin
SBUH Seat Back Upright Height
SCF Scarf
SCG Seat Center of Gravity
SCGH Seat Center of Gravity Height
SCM Seat Control Module
SDB Seat Data Box
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

SDU Seat Disconnect Unit

SDU Super-High Display Unit
SEB Seat Electronics Box
SEU Seat Electronic Unit
SGL Single
SIB Seat Interface Box
SJB Seat Junction Box
SL Service Letter
SLFLKG Self-Locking Gutierrez
SMAS Structure Mounted Airbag System
SMU Seat Massage Unit
SPB Seat Power Box
SPM Seat Power Module
SPIM Smart Passenger Interface Module

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY INTRO-9
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 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

ABBREVIATION EXPANSION
SPU Seat Power Unit
SRP Seat Reference Point
SSB Settop Seat Box
STA Stationary
STD Standard

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

STS Stud-to-Stud
SUPSD Superseded
SUPSDS Supersedes
SVDU Super Visual Display Unit
SW Side Wall
T/C Tourist Class
T/N Tool Number
T2 Type 2
TAC Track to Aisle Cushion
TAR Track to Armrest Strip
TBD To Be Determined
TOA Track to Outboard Arm
TPL Triple
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

TPMU Touch Passenger Media Unit

TR Temporary Revision
TSO Technical Standard Order
TSOA Technical Standard Order Authorization
TSPCU Touch Screen Passenger Control Unit
TSW Total Seat Width
TTL REQ Total Required
U/O Used On
UEB Underseat Electronic Box Gutierrez
ULP Upper Literature Pocket
UPR Upper
USB Universal Serial Bus
USC Under Seat Clearance
USVS Under Seat Video System

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY INTRO-10
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 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

ABBREVIATION EXPANSION
VDB Video Distribution Box
VDU Video Display Unit
VGS Variable Geometry Seat
VSEB Video Seat Electronics Box
W/ With

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

W/O Without
WCU Wireless Control Unit
WELS Wireless Emergency Light System

8. Vendor Controlled Document / Drawing Contact Information

The table below contains information specific to vendor document(s) and/or drawing(s) that are
referenced in this CMM and not included as an attachment. The CMM user is advised to check
with the vendor to obtain the latest revision of the document(s) and/or drawing(s).

NOTE: This table is applicable to vendor controlled documents and/or drawings only and has no
direct relation to vendor parts not manufactured by Collins Aerospace.

AMSAFE®, INC.
1043 N. 47th Avenue Telephone: +1 602 850 2850
Phoenix, AZ 85043-1817
FAX: +1 602 850 2812
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

United States
Website: https://www.amsafe.com/
E-mail: customerservice@amsafe.com
CAGE Code: 35FB9

ASTRONICS ADVANCED ELECTRONIC SYSTEMS CORP.

12950 Willows Road NE Telephone: +1 425 881 1700
Kirkland, WA 98034
FAX: N/A
United States
Website: https://www.astronics.com/ Gutierrez
E-mail: AESsupport@astronics.com
CAGE Code: 3E2Y8

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY INTRO-11
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 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

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THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY INTRO-12
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 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

DESCRIPTION AND OPERATION

1. Configuration

The MiQ™ passenger seats for Virgin Australia Airlines B737-8 Aircraft have been manufactured
in 4 versions. The seat versions are listed in Table 1. The aircraft configuration is from Envelope
Drawing 1367862 and is shown in Figure 1.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Table 1
Virgin Australia Airlines B737-8 - 8 PAX Configuration (Envelope Drawing 1367862)
MiQ™ Passenger Seat Models

MAX SEAT
SEAT SEAT VIEW ON
IDENT SEAT PART WEIGHT SEAT DWG
# NUMBER SEAT DESCRIPTION (LBS) QTY 1116000
101 1367870-101MS08 Seat Assembly - LH Double, F/R, 195 1 A, AD, L
Legrest, Passenger Computer
Power, Dual Emergency Escape
Path Light
104 1367870-104MS08 Seat Assembly - RH Double, F/R, 195 1 A, AD, L
Legrest, Passenger Computer Power
5 1367870-005MS08 Seat Assembly - LH Double, Last 180 1 E, AD, L
Row, Legrest, Passenger Computer
Power, Dual Emergency Escape
Path Light
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

8 1367870-008MS08 Seat Assembly - RH Double, Last 180 1 E, AD, L

Row, Legrest, Passenger Computer
Power

NOTE: Maximum seat weights (Units: LBS) include all components, except any equipment the
seat installer / operator may add to the seat, such as emergency equipment or literature
pocket contents.

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 1
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 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Virgin Australia Airlines B737-8 - 8 PAX Configuration (Envelope Drawing 1367862)

Figure 1

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 2
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 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

2. Seat Dimensions

Figure 2 shows the seat dimensions from Envelope Drawing 1367862. Figure 3 shows the basic
seat dimensions and installation information from Basic Dimension Drawing 1116000. Some of
the views in Figure 3 will not apply to the seats in this Component Maintenance Manual (CMM).
Refer to the last column in the configuration table for the views from Basic Dimension Drawing
1116000 that apply to your seats. Flag notes on the front views of the seats show the seat belt
buckle and tip locations (B = Buckle, T = Tip). Refer to Table 2 for frame assembly dimensions. All
dimensions are in inches unless noted otherwise.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

NOTE: If there is a variation in the same dimension shown on both the Envelope Drawing and
the Basic Dimension Drawing, the Envelope Drawing dimension takes priority.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 3
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 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Seat Dimensions (Envelope Drawing 1367862)

Figure 2 (Sheet 1 of 15)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 4
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 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Seat Dimensions (Envelope Drawing 1367862)

Figure 2 (Sheet 2 of 15)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 5
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 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Seat Dimensions (Envelope Drawing 1367862)

Figure 2 (Sheet 3 of 15)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 6
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 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Seat Dimensions (Envelope Drawing 1367862)

Figure 2 (Sheet 4 of 15)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 7
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 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Seat Dimensions (Envelope Drawing 1367862)

Figure 2 (Sheet 5 of 15)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 8
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Seat Dimensions (Envelope Drawing 1367862)

Figure 2 (Sheet 6 of 15)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 9
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Seat Dimensions (Envelope Drawing 1367862)

Figure 2 (Sheet 7 of 15)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Seat Dimensions (Envelope Drawing 1367862)

Figure 2 (Sheet 8 of 15)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 11
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COMPONENT MAINTENANCE MANUAL
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Seat Dimensions (Envelope Drawing 1367862)

Figure 2 (Sheet 9 of 15)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 12
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Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Seat Dimensions (Envelope Drawing 1367862)

Figure 2 (Sheet 10 of 15)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 13
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COMPONENT MAINTENANCE MANUAL
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Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Seat Dimensions (Envelope Drawing 1367862)

Figure 2 (Sheet 11 of 15)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 14
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Seat Dimensions (Envelope Drawing 1367862)

Figure 2 (Sheet 12 of 15)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 15
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Seat Dimensions (Envelope Drawing 1367862)

Figure 2 (Sheet 13 of 15)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 16
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COMPONENT MAINTENANCE MANUAL
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Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Seat Dimensions (Envelope Drawing 1367862)

Figure 2 (Sheet 14 of 15)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 17
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MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Seat Dimensions (Envelope Drawing 1367862)

Figure 2 (Sheet 15 of 15)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 18
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 1 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 19
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COMPONENT MAINTENANCE MANUAL
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 2 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 20
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
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COMPONENT MAINTENANCE MANUAL
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 3 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 21
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 4 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 22
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MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 5 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 23
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 6 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 24
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 7 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 25
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 8 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 26
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 9 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 27
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 10 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 28
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 11 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 12 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 13 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 14 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 15 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 16 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 17 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 18 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 19 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 20 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 21 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 22 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Basic Seat Dimensions (Basic Dimension Drawing 1116000)

Figure 3 (Sheet 23 of 23)

U.S. Export Classification: EAR 9E991 25-20-83-4667

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Table 2
Frame Assembly Dimensions - Part Number 1021505 (Refer to IPL Figure 43)

SEAT
DASH NO. DIM A DIM B DIM C DIM D DIM E WIDTH
-057, -058 12.475 11.475 20.750 22.295 18.575 56.920

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

"D" "D"

"B" "C" "E"

"A"
LH FRAME ASSEMBLY LOOKING
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

TOWARDS AFT OF PLANE

"D" "D"

Gutierrez

"E" "C" "B"

RH FRAME ASSEMBLY LOOKING "A"

TOWARDS AFT OF PLANE

U.S. Export Classification: EAR 9E991 25-20-83-4667

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3. Description

A. General

The seats described in this CMM are forward facing and are of the types stated in Table 1.
Figure 4 shows the main assemblies found on the double seat assemblies.

For the operator, the seat has been designed on a modular basis to allow for ease of
maintenance. The seat is comprised of the following major modules:

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Frame Assembly

Seatpan Assemblies

Legrest Assemblies

Back Assemblies

Headrest Assemblies

Endbay Assemblies

CTR Console Assembly

All of these modules (excluding the frame assembly) can be easily removed from the seat on
the aircraft with a minimum of tools. The module can then be quickly replaced by a substitute
module and any maintenance work can be carried out away from the aircraft.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

The environmental operating conditions for the seats in this CMM are as follows:

Temperature -15 to 55 ºC (5 to 131 ºF)

Relative Humidity (MAX) 95% for 6 hours

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COVER ASSEMBLY - HEADREST

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

CUSHION ASSEMBLY - HEADREST

CENTER CONSOLE
ASSEMBLY - NON-VIDEO
COVER ASSEMBLY - BACK
CUSHION - BACKREST
BUTTON
ASSEMBLY - SEAT CONTROLS

BACK ASSEMBLY

FOODTRAY ASSEMBLY
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

WALL ENDBAY
ASSEMBLY

IN-USE LAP BELT ASSEMBLY

LIGHT COCKTAIL TABLE ASSEMBLY
PULL STRAP - LIFE VEST
COVER ASSEMBLY - BOTTOM
CUSHION ASSEMBLY - BOTTOM
COVER ASSEMBLY - FOOT PADDLE
CUSHION ASSEMBLY - LEGREST Gutierrez
ENDBAY ASSEMBLY - IUL
BUTTON ASSEMBLY - ENDBAY ARM

MiQ™ Seat Assembly - Double

Figure 4

U.S. Export Classification: EAR 9E991 25-20-83-4667

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B. Standard Features

The MiQ™ seats have the following standard features:

Machined aluminum primary structure

Fabric bottom diaphragm suspension system

Life vest box under center console

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Quick release anti-rattle track fitting

Articulating legrest support

Forward baggage bar

C. Endbay Assembly (With In-arm Foodtray Assembly)

CAUTION: DO NOT PUT OBJECTS COLDER THAN 10 DEGREES CELSIUS

(50 DEGREES FAHRENHEIT) OR HOTTER THAN 71 DEGREES CELSIUS
(160 DEGREES FAHRENHEIT) ON THE FOODTRAY ASSEMBLY. THIS WILL
HELP PREVENT DAMAGE TO THE FOODTRAY. TEMPERATURES COLDER
THAN 10 DEGREES CELSIUS (50 DEGREES FAHRENHEIT) OR HOTTER
THAN 71 DEGREES CELSIUS (160 DEGREES FAHRENHEIT) CAN CAUSE
THE FOODTRAY TO WARP AND POSSIBLY COME APART.

The endbay assembly features a leather wrapped, spring-loaded armcap (sculptured for
additional hip room), a robust machined aluminum aisle rubstrip and integral flight attendant
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

step. Open the armcap to access the In-arm foodtray assembly, counter balanced and
self-presenting. Pulling on the foodtray latch to release, the foodtray assembly is bi-fold with
laminate inserts and a cup holder recess. It is self supporting and can slide forward up to
5 inches.

The aisle endbay assembly also has a ‘Drop Down’ feature for handicap access and is DOT
compliant. Pull on the control lever at the front of the endbay and lower the endbay assembly.
The Power Port In-use light is located at the rear of the side rubstrip assembly.

D. Center Console

The center console is the central divider in the double seats. It features hinged leather
wrapped armcaps and a fixed cocktail table with laminate insert. Push at the front of the Gutierrez
cocktail table to present the forward snack tray. There is a recess under each armcap for
amenities stowage. The RJUs and PC Power ports are located at the rear of the amenities
stowage area. The seat control levers (Recline, Legrest and Foot Paddle) are side mounted
on the center console.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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E. Back Assembly

The back assembly features adjustable recline. At the rear of the back assembly are housed
the upper literature pocket assembly, deluxe lower literature pocket and side mounted coat
hook.

F. Headrest Assembly

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

The headrest assembly provides the passenger with increased comfort. The headrest is
adjustable vertically to allow for variation in passenger height. Also the side supports
(headrest ears) can be rotated to provide side support for the passenger’s head.

G. Seatpan Assembly

The seatpan assembly supports the passenger with a fabric-based bottom support. It also
includes an articulating feature for increased comfort.

H. Legrest Assembly

The legrest assembly can be rotated to any angle within the range. It can also be extended
and retracted to suit the passenger. The foot paddle can be used in either the open position
to support the passenger’s feet or in the closed position to give increased leg support.

J. Seat Belt Tip / Buckle Location

(1) Seat belt’s tip / buckle locations for the seats are as follow (from outboard to inboard):
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(a) Outboard location: Tip / Buckle

(b) Inboard location: Buckle / Tip

K. Nameplate - TSO Tag with QR (Quick Read)

The Nameplate - TSO Tag (P/N 1002933-029), located on the seat frame, contains a QR
Code that can be read by an appropriate hand-held scanner, pointed at the TSO Tag. The QR
Code contains the birth record of the seat, including it’s model number, serial number, and
date and place of manufacture. This information can then be read or downloaded from the
scanner.

The Nameplate - TSO Tag is located on the aisle side of the front beam, facing FWD. Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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L. RFID (Radio Frequency Identification) Tag

The seats are equipped with an RFID Tag, located on the seat back. The RFID can be
activated from a short distance from the seat by an appropriate hand-held RFID scanner.
No contact with the seat or uncovering any parts is necessary. The activated RFID Tag
transmits the birth record of the seat to the scanner, including it’s model number, serial
number, and date and place of manufacture. This information can then be read or downloaded
from the scanner

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

The RFID Tags are located on the aisle PAX of the LH and RH seats. See Figure 5 for location
of the RFID Tag on the seat back.

The RFID Tag contains the following information (as a minimum):

Seat Part Number (Integrated Part Number, if IFE installed)

Serial Number

Date of Manufacture

CAGE Code or (Manufacturer Code)

NOTE: Refer to REPAIR (Page Block 6000) for RFID tag replacement instructions.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

RFID TAG
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

TYPICAL FOR MiQ™ LH AISLE BACKS

(CUSHIONS REMOVED, RH OPPOSITE)

RFID Tag Location on Seat Back

Figure 5

U.S. Export Classification: EAR 9E991 25-20-83-4667

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M. Easy Access to the Seat Electrical Boxes (Refer to Figure 6)

The seatpan assembly has a support feature (Refer to IPL Figure 9) to allow easy access to
the seat power boxes. To access the seat power box, follow the steps below:

(1) Remove the bottom / legrest covers and cushion assemblies.

(2) Pull on the legrest control and rotate the legrest assembly to the fully extended
(deployed) position.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(3) Disconnect the seatpan straps at the inboard / outboard side of the seatpan assembly
and unwrap from the rollers.

NOTE: Reconnect the seatpan straps when they have been disconnected to service
the other components on the seat.

(4) Lift up the seatpan assembly and position the seatpan support on the roller to support
the seatpan assembly.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

SEATPAN
STRAP

SUPPORT
STAND

Gutierrez

Easy Access to Seat Electrical Boxes

Figure 6

U.S. Export Classification: EAR 9E991 25-20-83-4667

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N. Removal and Installation of the ISPS (Refer to Figure 7)

NOTE: To remove the ISPS, the spring latches connecting the harnesses must be
disengaged before releasing the screws.

NOTE: Depending upon individual seat configuration, front row or standard, it may be
easier to gain access to the spring latches from the top (underneath the seatpan)
or from the bottom (the rear of the seat).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

To remove the ISPS, follow the steps below:

(1) Remove the ISPS shroud assembly (REF IPL FIG 40, Item 5) by removing the tiedown
straps (REF IPL FIG 40, Item 10).

(2) Disengage all the spring latches holding the harness connectors and disconnect all
harnesses from the ISPS.

NOTE: The dust caps are not fixed to the seat assembly once removed from the
SEB / SPM. Bag and tag the caps by part number and record their location on
the SEB / SPM for re-installation.

(3) Turn the four captive screws (2 front, 2 rear) on the ISPS counterclockwise to release.

(4) Carefully remove the ISPS from the mounting plate.

(5) Repeat steps (1) thru (4) in reverse order to re-install the ISPS.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

UNCLIP SPRING LATCHES

TO REMOVE DUST CAPS
(BAG AND STOW CAPS) Gutierrez

UNCLIP SPRING LATCHES

CAPTIVE SCREWS TO REMOVE HARNESSES

Removal/Installation of ISPS
Figure 7

U.S. Export Classification: EAR 9E991 25-20-83-4667

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4. Seat Assembly Operation

A. Back Recline

To move any back assembly from the upright to the recline position, activate the recline
control lever and apply pressure against the backrest. When the control lever is released the
backrest is restrained from any further movement.

To re-erect the backrest, activate the recline control lever, release pressure from the backrest

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

and it will return automatically to the normal upright position.

The recline unit incorporates an override device which will allow the backrest to be moved
from a recline position to any angle up to and including the normal upright position by the
application of a nominal load at the backrest top.

B. Headrest Operation

The headrest may be adjusted manually by sliding the headrest up or down as required.
A friction device ensures that the headrest remains in the chosen position.

The headrest ears can be adjusted manually by rotating the ears to the required position.
Again, friction ensures that the ears remain in the chosen position.

C. Legrest Deployment

Activating the legrest rotation control lever allows the legrest to rotate upwards. It can be
stopped at any position within the range by releasing the lever.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Once the legrest has been rotated to the most comfortable position, the passenger can then
activate the footrest extension control lever which extends the legrest and presents the
footrest to the passenger. The passenger can then choose to keep the footrest closed or open
as required.

D. Foodtray Deployment

Open the endbay armcap and pull on the foodtray latch to release the foodtray and allow it to
present itself. Pull the foodtray upwards to its maximum position. The table can now be swung
into its deployed position ready for use. Close the armcap.

In the deployed position, the foodtray table can slide forward and aft to allow for passenger
comfort. The table is bi-fold, and can be used with either one or two leaves opened, as Gutierrez
required.

E. Attachment of the Seat Assembly

The seat assembly is attached to the aircraft seat tracks by securing the legs, fore and aft,
with studs and track fittings.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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F. Life Vest Box Assembly (Refer to Figure 8)

The life vest box assembly, with integrated metal latch and provision for a pull strap, is located
under the center console and accessed from the front by the pull strap.

The preflight briefing must inform the passengers of the life vest container location and
request that the passenger take a moment and locate the container with the pull strap by the
passenger's feet.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

G. Installation - Life Vest (Refer to Figure 8)

The life vest container assembly is located under the center console and the life vests are
accessed from the front by the pull strap.

When installing the life vests, follow the steps below:

(1) Open the life vest door.

(2) Insert the life vests into the side by side compartments. The life vests are EAM World
Wide P/N P01074-201W.

(3) Close the life vest door assembly and ensure the latch is fully engaged.

(4) Install the life vest tamper evident seals.

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

LIFE VEST STRAP

Gutierrez

PLACE LIFE VEST

IN EACH
COMPARTMENT

Installation - Life Vest

Figure 8

U.S. Export Classification: EAR 9E991 25-20-83-4667

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TESTING AND FAULT ISOLATION

1. Proper Assembly

Proper assembly of the passenger seat will preclude the necessity for elaborate testing
procedures. Complete disassembly of the seat is not usually required. Disassembly should
proceed only so far as to correct malfunctions or replace damaged and worn parts. After
assembly, check all seat functions to ensure that each performs smoothly with no excessive

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

binding or other evidence of faulty assembly.

2. Seat Back Recline Mechanism

Seat backs recline through the operation of a recline control lever with pressure applied in an aft
direction on the back. When the recline control lever is pulled with no pressure exerted on the
back, the seat should return to its full upright position. If the seat back fails to operate in the above
fashion, refer to REPAIR (Page Block 6000) for corrective action. Refer to the envelope drawings
in this CMM for recline operation.

On mechanical locks, check clutch engagement in the recline hydraulic lock by placing the seat
back in the upright position and applying pressure in an aft direction. If the seat back reclines
slightly and a click is audible, refer to REPAIR (Page Block 6000).

3. Breakover

Seat backs have limited breakover by the use of a shoulder screw.

4. Seat Attachment To Aircraft

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

The seat assemblies should lock securely to the floor track at the lock mechanisms and studs at
the bottom of the leg assemblies.

5. Troubleshooting Procedures

Table 1001 consists of three columns:

A. FAULT - Defines the problem.

B. PROBABLE CAUSE AND FAULT ISOLATION - Defines the most likely cause of the problem.

C. CORRECTIVE ACTION - Provides the corrective action to be taken in the order that would
most likely correct the problem. Gutierrez

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Table 1001
Troubleshooting Procedures

PROBABLE CAUSE AND

FAULT FAULT ISOLATION CORRECTIVE ACTION
ENDBAY ARM TOO Front / rear bolts loose Tighten front and rear bolts and torque to
LOOSE / TOO MUCH proper value per torque tables in FITS AND

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

PLAY CLEARANCES (Page Block 8000).

ENDBAY WILL NOT Check for loose / missing Re-torque / reinstall hardware.
STAY UP IN LOCKED hardware (IPL FIG 34,
POSITION Items 10, 15, 25, 30, 40,
45, 55, 60, 70, 75, 85, 90,
100, 105, 115, 120)

AISLE ENDBAY DOES 1. Debris obstructing a. Check for debris impeding movement.
NOT DROP DOWN movement
b. If problem persists, go to step 2.

2. Control cable out of slot a. Inspect button assembly to see if

in button assembly the control cable has slipped out of the
slot in button lever assembly.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

b. Reinstall cable into slot.

c. If problem persists, go to step 3.

3. Control cable out of slot a. Inspect pivot assembly at bottom of

in pivot assembly endbay to see if the control cable has
slipped out of the slot in the pivot
assembly.

b. Reinstall cable into slot.

c. If problem persists, go to step 4.

Gutierrez

4. Control cable broken a. Replace control cable.

b. Test endbay drop down for proper

operation.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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Table 1001 (Continued)

Troubleshooting Procedures

PROBABLE CAUSE AND

FAULT FAULT ISOLATION CORRECTIVE ACTION
IN-ARM FOODTRAY 1. Control cable out of slot a. Inspect table latch to see if the control
DOES NOT PRESENT in table latch cable has slipped out of the slot in table
ON RELEASE latch.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

b. Reinstall cable into slot.

c. If problem persists, go to step 2.

2. Control cable out of slot a. Inspect table release at bottom of endbay

in table release to see if the control cable has slipped out
of the slot in the table release.

b. Reinstall cable into slot.

c. If problem persists, go to step 3.

3. Control cable broken a. Replace control cable.

b. Test table release for proper operation.

4. Cord reel damaged or Replace in-arm foodtray cord reel.

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

broken

IN-ARM FOODTRAY Loose hardware at this Re-torque / reinstall hardware.

WILL NOT LOCK IN location
STOWED POSITION

IN-ARM FOODTRAY Foodtray damper is worn a. Inspect for damaged parts.

WILL NOT ROTATE or damaged
b. Replace damaged components.

Gutierrez
IN-ARM FOODTRAY 1. Slide rails dirty or Clean slide rails, then apply only clear
WILL NOT SLIDE corroded paraffin wax to allow for easy and smooth
FREELY sliding action.

2. IGUS carriages are worn Replace any IGUS carriages.

or damaged

U.S. Export Classification: EAR 9E991 25-20-83-4667

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Table 1001 (Continued)

Troubleshooting Procedures

PROBABLE CAUSE AND

FAULT FAULT ISOLATION CORRECTIVE ACTION
FOODTRAY INNER Foodtray leaf hinge(s) Replace foodtray leaf hinge(s).
AND OUTER LEAF broken
ASSEMBLIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

BROKEN AT HINGE

SEAT BACK WILL 1. Recline control cable a. Inspect recline hydraulic lock actuator to
NOT RECLINE loose from actuator end see if the control cable has slipped out of
of the hydraulic lock the actuator slot, or if the actuator has
slipped off the hydraulic lock.

b. Reinstall cable to actuator slot or actuator

to hydraulic lock.

c. If problem persists, go to step 2.

2. Recline control cable a. Quarter-turn the (2) screws attaching

out of cable lever slot in seat control assembly to console
seat control assembly assembly.

b. Replace control cable into cable lever slot

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

and test for proper operation.

c. If problem persists, go to step 3.

3. Recline control cable a. Replace control cable.

broken
b. Adjust cable tension.

c. Test recline control lever for proper

recline operation.

d. If problem persists, go to step 4.

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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Table 1001 (Continued)

Troubleshooting Procedures

PROBABLE CAUSE AND

FAULT FAULT ISOLATION CORRECTIVE ACTION
SEAT BACK WILL 4. Hydraulic lock a. Replace recline control hydraulic lock.
NOT RECLINE damaged / inoperative
(CONT’D) b. Reattach control cable at actuator and

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control cable lever ends of seat assembly.
Route cable harness according to cable
routing guidelines.

c. Test recline control for proper operation.

d. Adjust as necessary to ensure cable

remains in slots (both ends) and that
hydraulic lock is adjusted for proper
tension.

NOTE: The most common recline problems are due to improperly

adjusting the hydraulic lock cable for proper tension during
installation. If tension is not accurately adjusted, the cable
simply slips out of the actuator end of the cable assembly
and in some cases, the control button end of the cable
assembly. Ensuring proper adjustment during maintenance
activity will ensure fewer problems of this nature.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

NOTE: Refer to REPAIR (Page Block 6000) for more detailed

instructions on removal and installation of seat control
components.

HEADREST TENSION Headrest worn Replace the headrest assembly.

TOO LOOSE

Gutierrez

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Table 1001 (Continued)

Troubleshooting Procedures

PROBABLE CAUSE AND

FAULT FAULT ISOLATION CORRECTIVE ACTION
SEAT LEGREST 1. Legrest control cable a. Inspect gas lock lever assembly to see
INOPERATIVE assembly not installed to whether control cable has slipped out
actuator slot in gas lock of actuator slot.

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lever assembly
b. Reinstall cable assembly and test seat
legrest control lever for proper operation.

c. If problem persists, go to step 2.

2. Legrest control cable a. Quarter-turn the (2) screws attaching

not installed to cable seat control assembly to console
lever slot in seat control assembly.
assembly
b. Replace control cable into cable lever slot
and test for proper operation.

c. If problem persists, go to step 3.

3. Legrest control cable a. Replace control cable.

broken
b. Adjust cable tension.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

c. Test legrest control lever for proper

operation.

d. If problem persists, go to step 4.

4. Gas lock damaged / a. Replace gas lock.

inoperative
b. Install control cable at lever assembly and
control lever ends of seat assembly.

c. Test legrest control for proper operation.

Gutierrez
d. Adjust cable tension as necessary

NOTE: Refer to REPAIR (Page Block 6000) for more detailed

instructions on removal and installation of seat control
components.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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Table 1001 (Continued)

Troubleshooting Procedures

PROBABLE CAUSE AND

FAULT FAULT ISOLATION CORRECTIVE ACTION
SEAT FOOT PADDLE 1. Foot paddle control a. Inspect release head on gas lock to
INOPERATIVE cable loose from slot in see whether control cable has slipped out
release head end of gas of release head slot.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

lock
b. Reinstall control cable and test seat
foot paddle control lever for proper
operation.

c. If problem persists, go to step 2.

2. Foot paddle control a. Quarter-turn the (2) screws attaching seat

cable not installed to control assembly to console assembly.
cable lever slot in seat
control assembly b. Replace control cable into cable lever slot
and test for proper operation.

c. If problem persists, go to step 3.

3. Foot paddle control a. Replace control cable.

cable broken
b. Adjust cable tension.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

c. Test foot paddle control lever for proper

operation.

d. If problem persists, go to step 4.

4. Gas lock a. Replace gas lock.

damaged / inoperative
b. Install control cable at release head and
control cable lever ends of seat assembly.

c. Test foot paddle control for proper

operation. Gutierrez

d. Adjust cable tension as necessary.

NOTE: Refer to REPAIR (Page Block 6000) for more detailed

instructions on removal and installation of seat control
components.

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Table 1001 (Continued)

Troubleshooting Procedures

PROBABLE CAUSE AND

FAULT FAULT ISOLATION CORRECTIVE ACTION
SEAT LEGREST Cylinder end of legrest a. Inspect valve release assembly for
CABLE TENSION NOT control cable is misaligned correct orientation of legrest control cable.
CONSISTENT with groove on the valve

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(LEGREST DOESN'T release assembly b. Rotate to align control cable into the
STOW CORRECTLY) groove on the valve release assembly.
NOTE: Refer to REPAIR (Page Block 6000) for more detailed
instructions on removal and installation of seat control
components.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

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SCHEMATIC AND WIRING DIAGRAMS

1. Introduction

This section contains cable routing and grounding standards and procedures. When applicable,
system cable block diagram(s) are included.

USING 3D ELECTRICAL DRAWINGS (Page Block 17000) provides instructions on using the 3D

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

PDF Electrical Installations referenced in this CMM. The 3D PDF provides models showing all
electrical component installations and cable routing information. Use the IPL only to identify part
numbers for part ordering (IPL Figure 18).

3D PDF electrical installation drawings are available to the customer upon request. Requests
should be sent to the following E-mail address: ws_techpubs3d@collins.com

Panasonic Avionics Block Diagram CA7/VOZ 737-8 of the IFE system contains more specific
details. Contact Panasonic Avionics for the latest released version of this document (Refer to
INTRODUCTION page block of this CMM for vendor contact information).

2. General

NOTE: Refer to the customer-furnished equipment maintenance documentation for appropriate

troubleshooting and maintenance of customer-furnished electronics and electrical
equipment used within these B/E Aerospace seating products.

A. Cable Routing

This section contains installation, maintenance and service procedures for properly routing
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

and securing electrical cables on aircraft seating equipment. These general practices apply to
all series of aircraft passenger seats manufactured by B/E Aerospace. Refer to aircraft
manufacturer’s specifications for OEM requirements.

(1) Routing Principles

(a) Cables shall be as accessible as possible to allow for ease of maintenance and
inspection since most repairs are carried out on the aircraft.

(b) Route cables to avoid possible damage from passenger contact, underseat carry
on storage and shifting, spills, and/or mechanical movement of seat components.
Refer to Figure 2001.
Gutierrez

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STRUCTURE

RECLINE MECHANISM

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UNACCEPTABLE ACCEPTABLE

CABLE SEAT FRONT BEAM

Figure 2001
(c) When seat parts can rotate between each other, route the cables parallel to the
rotation axis. Refer to Figure 2002.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

ACCEPTABLE

UNACCEPTABLE Gutierrez

Figure 2002
(d) Route cables to minimize the need for protective methods and materials like wrap
or sleeves.

(e) Route cables exiting a connector in a straight line for at least 0.25 inches before
making a bend. Refer to Figure 2003.

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(f) Route cables with enough slack to prevent mechanical strain on wires, terminals,
connections, junctions and supports. Refer to Figure 2003.

CONNECTOR

0.25" MINIMUM
STRAIN POINTS
SMOOTH TRANSITION

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

SPACER

CABLE TIE
WRONG RIGHT SEAT BEAM

Figure 2003
(g) When cables cross or are in proximity to seat moving parts, route them on either
side of those moving parts.

(h) Locate the breakout of individual cables adjacent to cable support or clamping
points. This minimizes the amplitude of vibration transmitted to the breakout wires
from the main harnesses.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(j) Provide service loops to allow for adjustment, service or removal of connectors or
components with minimal disassembly. Refer to Figure 2004.

SERVICE LOOP
(TYPICAL)

Gutierrez

SEB

Figure 2004

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(2) Clearances

(a) Install cables with enough clearance to prevent chafing against the sharp edges of
structure, equipment, etc. (1/8'' minimum clearance unless secondary protection is
provided).

(b) When not specifically controlled, the slack portion of the cable bundles may
contact smooth flat surfaces and smooth radii of 1/8'' or larger of either metal or

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

plastic.

(c) Route power wiring for motorized equipment, in-seat power, or reading lights
separately from IFE and communication wiring. Sensitive signal or communication
wiring should have at least a one-inch separation from electrical wiring. When a
one-inch separation is not possible, enclose the power wiring in a metallic shield
grounded to seat structure to minimize EMI. Refer to Figure 2005.

CABLES

CABLE TIE
WITH SPACERS

1''

SEAT BEAM
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Figure 2005
(3) Bend Radius

(a) For coaxial cable, use a minimum bend radius of ten times the cable diameter. In
restricted places, the bend radius for coaxial cable may be a minimum of six times
the cable diameter. Too severe a bend in coaxial cable can damage the cable and
cause loss of signal. For standard wire cable, the bend radius will be a minimum of
three times the cable diameter, but six times the cable diameter is preferred.

(b) The bend radius of a cable bundle will not be less than six times the diameter of
the largest cable in the bundle.
Gutierrez
(c) Clamping or the pressure of cable rubbing against structure causes bend
sensitivity and reduced cable life. Increase bend radius to maximize cable life.

NOTE: If the cable jacket or sheathing becomes crimped, the bend radius is too
small.

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(4) Cable Slack

(a) Distribute slack evenly throughout the length of the cable bundle.

(b) In applicable areas, ensure there is enough cable slack to allow the following
operations:

1 Replacement of terminations and/or connectors

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

2 Movement of hinged or sliding joints

3 Removal and replacement of face mounted equipment

4 Coupling and uncoupling of connectors

5 Movement of equipment to perform adjustment, servicing or removal.

(c) Provide drip loops so that liquids will not drip on or into electrical equipment. Do not
use drip loops unless cable routing will permit liquids to run down the wiring into
the connector. Drip loops are not required on wires or connectors that terminate in
a potted connector. Take care to prevent the drip loop from chafing on adjacent
structure or equipment. If chafing can occur, that section of wire or cable must be
sleeved or tape wrapped. Do not use drip loops to take up excess wire length.
Refer to Figure 2006.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

DRIP LOOP

Figure 2006
(5) Cable Ties
Gutierrez
(a) Untangle cables as much as practical before tying them into groups. Lay cable
groups parallel when practical before tying them into bundles.

(b) In underseat baggage stow areas, place cable out of reach of passenger and
install ties as necessary to ensure no slack in this area.

(c) The use of nylon straps (Cable Ties, Panduit, etc.) attached directly to smooth
structure is acceptable.

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(d) Cut off cable ties square and flush with the cable tie head to prevent injury. Refer to
Figure 2007.

WRONG RIGHT

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TRIMMED CABLE TIES

Figure 2007
(e) Where a cable or cables break out of a cable bundle, each group shall be tied
together and/or secured at a maximum distance of 1 inch from the break out point.
Refer to Figure 2008.

CABLE TIES

1''
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

6" TO 8" 1" 1"

Figure 2008
(f) Do not use cable ties in areas where the head of the cable tie can press against
and abrade adjacent wires, or where the clamping pressure results in deformation
of a coaxial cable. Refer to Figure 2009.

Gutierrez

WRONG

CABLE TIE HEAD

Figure 2009

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(g) When cable ties intrude into the foam of the seat (e.g., seat back), turn the head of
the cable tie to one side to minimize risk of damage to the seat cushion.

(6) Spacing Ties for Bundle Support

(a) Space ties on cable bundles a minimum of 6” and a maximum of 8” apart.

(b) Ties may be placed as required to provide adequate support at bends, breakout
and locations where cables are adjacent to moving parts.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(7) Clamping

(a) Cable bundles should never be attached directly to the structure. Instead, use
stand-offs and spacers. Refer to Figure 2010.

CABLE TIE

SPACER
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

CABLE TIE SEAT REAR BEAM

Figure 2010
(b) Select the smallest clamp size that

1 Holds the wiring securely.

2 Allows no abrasive movement.

Gutierrez
3 Neither crushes nor pinches the wire.

(c) Use standard clamps. Clamping and installation should be done in a way that
facilitates the removal and replacement of cable assemblies.

(d) Tie and support wire or cable bundles to prevent mechanical strain on individual
wires or terminations.

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(e) When the diameter of the cable is smaller than what the clamp can securely hold,
use nylon tape to wrap the cable before clamping.

(f) Do not use hook and loop fasteners to secure cable bundles.

(8) Connectors

(a) Minimize the handling of connectors and cabling at all times to reduce the

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

possibility of connector damage.

(b) Minimize the bending of wire conductors. Cables containing any wire with
damaged insulation should be replaced.

(c) Wiring should be periodically inspected for signs of unacceptable damage such as
cuts, breaks, cracked or burnt insulation or excessive kinks.

(d) Periodically inspect connectors for signs of contamination with metal particles,
water, dirt, grease, oil, carbon or adhesive.

(e) Periodically inspect connectors for bent or corroded contacts. Do not straighten
bent connector contacts. Do not reject tarnished silver, gold or rhodium plating on
contacts.

(f) Use standard snug fitting dust caps to protect the uncoupled end of connectors
from mechanical damage and contamination. Install the dust covers on all
connectors to prevent damage.

(g) When performing service requiring disconnecting connectors, protect connectors

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

from contamination by metal particles, water, dirt, grease and oil. Use polyethylene
bags.

(h) Route cables to minimize mechanical strain on connectors and cabling.

(j) Protect cables against breakage at connections by providing enough slack and
using mechanical clamping as needed to relieve strain.

(k) Install connectors to prevent their usage as steps, hand holds, or footrest, and to
prevent mechanical strain on attached cables.

(l) Securely attach each connector on the seat structure using one of the following
methods: Gutierrez

1 Plastic straps (Cable Ties, Panduit, etc.)

2 Clamps

3 Structure provision (Raceway, Bracket, etc.).

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(m) Mount connectors horizontally to allow for drainage and to prevent the trapping of
liquid or condensation.

(9) Drip Loops for Cables into Video Boxes

(a) To prevent liquids from entering junction boxes, connectors, or other enclosed
items, provide a drip loop in the cable just before it enters the item or equipment.

(b) Locate drip loops so that liquid will not enter the electrical equipment. Refer to

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Figure 2006.

(10) Handling of Electrostatic Discharge (EDS)-Sensitive Parts and Assemblies

(a) Protect parts and assemblies from damage and contamination during all
transportation and storage periods. They must be capable of meeting the
requirements of the drawing and specification to which they were manufactured.
Damage may consist of bends, dents, deformations, loose or missing fasteners,
broken or kinked wires, and EDS damage. Contamination may consist of foreign
material such as dirt, dust, chips, filings, loose material, solder particles, grease, oil
paint and moisture.

(b) Use suitable cushioning and wrapping materials for equipment protection.

NOTE: Cushioning and wrapping materials may vary, depending on the

environment in which they are to be used.

3. Grounding of Seats and Seat Equipment

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

This section contains installation, maintenance and service procedures for properly grounding
seats and seat electrical/electronic components.

Seat tracks on modern transport aircraft are not designed to carry ground. All electrical seat and
seat-related components should be grounded via the aircraft’s electrical system. Proper
grounding and bonding techniques used on the metal portions of the seat group are essential to
ensure adequate grounding.

NOTE: B/E Aerospace seating products are manufactured to conform to the aircraft
manufacturer’s electrical grounding specifications that are/were current at the time of
manufacture. Specifications continue to change, and not all products currently in service
conform to present specifications. For information on upgrading seat electric/electronic
equipment grounding to current manufacturing specifications, contact B/E Aerospace’s Gutierrez
Seating Aftermarket Operations (SAO) for options and quotes. Although properly
maintained seating products continue to meet certification, evolving OEM specifications
may result in the application of different grounding specifications during a prolonged
schedule of manufacture and delivery.

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A. Grounding to A/C Electrical System

(1) Main static ground for the seat is the grounding connection through the seat-to-seat
cable. This main static ground may be either a contact in the seat-to-seat connector or a
#10 stud connected to a ground cable from the seat-to-seat cable. Refer to Figure 2011
for an example.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

7 - SPARE 2 - AC RETURN

1 - SINGLE-PHASE 115VAC

6 - STATIC GROUND 3 - STATIC GROUND

5 - NOT USED 4 - NOT USED

115VAC
400Hz
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Figure 2011

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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(2) Static ground connection to the ECU from ground stud(s) on the seat structure may be
accomplished through a ground strap that is a component of the seat-to-seat wiring
harness or via ground fittings on the ECU enclosure itself. Refer to Figure 2012 for an
example.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

TWO REDUNDANT
JXX JXX JXX GROUND FITTINGS

0 0 0 0

0 0 0 0

ECU

3 6 3 6
J1 J2

SEAT-TO - SEAT-TO-
SEAT CABLE SEAT CABLE
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

BONDED TO SEAT PRIMARY GROUND

Figure 2012
Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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(3) Ground stud(s) on the seat’s metallic frame provide for ground strap terminal
connections. Refer to Figure 2013.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

ISPS (PC POWER)
SEAT
STRUCTURE

OUTPUT
1
3-PHASE 4
POWER 5 READING
3
LIGHT
3

6 SECONDARY
BONDING STUD
(OPTIONAL)
AIRCRAFT STATIC
GROUND AT SIDEWALL
FLOORBOX
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

DISCONNECT INPUT MOTOR

3-PHASE 1
POWER 4
5

X 3

X 6

3 CONTROLLER

PRIMARY
BONDING
STUD (#10)
Gutierrez

AIRCRAFT SEAT

Figure 2013

U.S. Export Classification: EAR 9E991 25-20-83-4667

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B. Ground Studs, Types Utilized

(1) Direct Ground Stud - A ground stud installation where necessary terminal(s) is/are
installed simultaneously with the ground stud. The ground stud must be removed to
remove the terminal(s). Refer to Figures 2014 and 2015.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

SELF-LOCKING NUT

PRESSURE WASHER
TERMINAL

CLEANED SURFACE
CORROSION PROTECTIVE WASHER

METAL STRUCTURE
CORROSION PROTECTIVE WASHER

FASTENER

Figure 2014
Direct Ground Stud with Single Terminal
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

SELF-LOCKING NUT

PRESSURE WASHER
TERMINAL

CLEANED SURFACE
CORROSION PROTECTIVE WASHER
METAL STRUCTURE Gutierrez
CORROSION PROTECTIVE WASHER

FASTENER

Figure 2015
Direct Ground Stud with Multiple Terminals

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(2) Pre-installed Ground Stud - A ground stud installation that allows terminals (installed by
separate process) to be installed and/or removed without removing the ground stud.

(3) Standard Ground Stud - A ground stud comprised of standard fasteners, washers and
nuts. Refer to Figures 2016 and 2017.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

SELF-LOCKING NUT

PRESSURE WASHER
TERMINAL

METAL STRUCTURE
PRE-INSTALLED GROUND STUD

PRESSURE WASHER CORROSION PROTECTIVE WASHER

Figure 2016
Standard Ground Stud with Single Terminal
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

SELF-LOCKING NUT

PRESSURE WASHER
TERMINAL

METAL STRUCTURE
PRE-INSTALLED GROUND STUD Gutierrez

CORROSION PROTECTIVE WASHER

PRESSURE WASHER

Figure 2017
Standard Ground Terminal with Multiple Terminals

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C. Grounding Procedures

(1) Each seat must be provided with a #10 ground stud to ground equipment and structure
not otherwise attached to main static ground.

(2) If a ground stud needs to be installed or reinstalled, refer to OEM specifications on

surface preparation, materials and testing.

(3) When more than one terminal is installed on one ground stud, put the largest terminal

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

next to the corrosion protective washer and stack the other terminals in order of
decreasing size. Fan the terminals around the stud whenever possible. Refer to
Figure 2018.

(4) A maximum of six terminals may be installed on a single ground stud, whether primary
or secondary bonding stud.

(5) For restricted spaces, a ground strap terminal may be bent 90 degrees one time only.
Ensure that enough clearance exists between the terminal shank and the ground stud to
allow installation and removal without further bending. Repeated bending of a terminal
may cause it to break.

(6) Corrosion protective and pressure (locking) washers must be used on ground studs.
Refer to Figures 2014 through 2017.

(7) When more than two ground terminals are installed on a ground stud, corrosion
protective flat washers must be installed on each side of each terminal. Refer to
Figure 2018.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

HEX NUT

FLAT WASHERS EACH BASE MATERIAL

SIDE OF TERMINAL NOT SHOWN

HEX NUT
Gutierrez

Figure 2018
(8) Terminals can be turned over to assist installations.

(9) Nuts on ground studs must be properly torqued. Refer to Tables 2001 and 2002 and
aircraft OEM specifications.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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Table 2001
Self-Locking Electrical Nut Torque Values
STUD SIZE TIN COATED COPPER TERMINAL ON ALUMINUM
MINIMUM MAXIMUM
10-32 28 IN-LB 35 IN-LB
1/4-28 65 IN-LB 70 IN-LB

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5/16-24 135 IN-LB 145 IN-LB

Table 2002
Plain Electrical Nut Torque Values
NUT SIZE MINIMUM MAXIMUM
10-32 35 IN-LB 40 IN-LB
1/4-28 85 IN-LB 105 IN-LB
5/16-24 150 IN-LB 180 IN-LB

(10) If a ground terminal is removed from a ground stud with more than one terminal, the
other terminals must be resecured with the ground stud to the seat using proper
procedures. This will apply when a component of the seat may be removed for repair or
replacement at a later date.

(11) Whenever a ground terminal is removed and reinstalled or replaced, or whenever a

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

ground stud is installed or replaced, use an ohmmeter to verify that resistance to ground
is within an acceptable range. (Figure 2019 illustrates a method for testing for resistance
to ground with an ohmmeter.) Refer to aircraft OEM specs for details of stud sizes and
maximum resistance.

OHMMETER

METAL
STRUCTURE
Gutierrez

APPROX 0.25"

Figure 2019

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DISASSEMBLY

1. General

WARNING: BEFORE SERVICING SEATS HAVING POWER COMPONENTS, DISCONNECT

POWER TO THE SEAT TO AVOID ELECTRICAL SHOCK.

CAUTION: DO NOT REMOVE RIVETED ASSEMBLIES OR SUBASSEMBLIES UNLESS

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

DAMAGE MAKES IT NECESSARY TO REPLACE A PROCURABLE PART.
(REFER TO ILLUSTRATED PARTS LIST FOR A LIST OF PROCURABLE PARTS)
IF YOU REMOVE AND INSTALL RIVETS AGAIN AND AGAIN, YOU WILL
DAMAGE ADJACENT SURFACES AND MAKE THE RIVET HOLES LARGER.

CAUTION: DO NOT DISASSEMBLE RIVETED, CEMENTED, OR BONDED

SUBASSEMBLIES. IF THE ASSEMBLY IS DAMAGED AT THESE POINTS, YOU
MUST REPLACE THE ENTIRE ASSEMBLY.

NOTE: Unless there is a plan to replace hardware removed in disassembly, safely store all
removed hardware for replacement at assembly. Use plastic bags and markers as
necessary to record the assemblies and seat part numbers for which the hardware is to
be used.

NOTE: Cable ties (nylon straps) used to secure parts and assemblies can be cut and removed
to allow performance of service and maintenance, and at completion must be replaced
by the equivalent device in the same manner per specifications.

A. This section gives complete disassembly instructions for the full seat assembly. If you must
repair or replace a part or subassembly, disassemble only as much as necessary to repair or
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

replace the damaged part or subassembly.

B. Read all instructions and look at the related illustrations before starting disassembly.

C. Identify all parts with a label as you remove them.

D. Make sure that all wiring harness electrical connections are unplugged to enable parts and
harnesses to be removed.

E. TESTING AND FAULT ISOLATION (Page Block 1000) contains procedures you can use to
make an analysis of the operation and condition of subassemblies. It contains a table that
identifies possible malfunctions and gives procedures to correct the malfunctions.
Gutierrez
F. SCHEMATIC AND WIRING DIAGRAMS (Page Block 2000) contains procedures, notes,
warnings and cautions for the electrical system.

G. INSPECTION/CHECK (Page Block 5000) contains procedures you can use to inspect parts
and subassemblies. Inspections will help you make a decision to set adjustments, clean
subassemblies and repair or replace damaged parts.

H. REPAIR (Page Block 6000) contains procedures you can use to make small repairs.

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2. Removal of the Seat Assembly from the Aircraft

Lifting points for seats for installation and transportation to be from both outermost seat belts
(doubles). An appropriate torso shaped lifting device shall be properly positioned in the seat and
strapped in with seat belts prior to lifting seat. Seats should be lifted by the torso lifting devices
only.

CAUTION: DO NOT SLIDE THE SEAT ASSEMBLY ACROSS ABRASIVE SURFACES; THIS

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

WILL CAUSE TOO MUCH WEAR ON THE TRACK STUDS AND FITTINGS.

Seat assemblies are attached to the aircraft seat tracks with a stud and anti-rattle nut located at
the bottom of the forward leg and a track fitting assembly located at the bottom of the rear leg.
See Figures 3001 for examples.

LEG
(FRONT)

SCREW

LEG
(REAR)

ANTI-RATTLE
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

NUT

STUD
REAR TRACK
FITTING

Figure 3001
(1) Use a 9/16" open end wrench to loosen the anti-rattle nut at the front of the leg.

(2) Use a 3/16" HEX head wrench to loosen the lock screw on top of the rear track fitting.
This will loosen the plunger that attaches the studs to the aircraft seat tracks.

(3) Push the seat assembly either forward or aft one-half inch and lift it off the aircraft seat
tracks. Gutierrez

NOTE: Track savers are recommended to protect the track fittings when the seat is
removed from the aircraft. They can be ordered from B/E Aerospace.

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3. Disassembly Procedures

A. Removal of the Covers, Cushions, and Lap Belts

(Refer to IPL FIG 1)
(1) Remove the lap belt assembly (5).

NOTE: Pull off the entire cushion / cover assembly from the seat before removing the

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

cover from the cushion.

(2) Remove the bottom legrest covers (10) from the seatpan assembly by disengaging the
hook-and-pile fastenings.

(3) Remove the bottom cushion assemblies (15) from the seatpan diaphragm by
disengaging the hook-and-pile fastenings.

(4) Remove the foot paddle covers (20) from the foot paddle assembly by disengaging the
hook-and-pile fastenings.

(5) Remove the legrest foot cushion assemblies (25) from the legrest assembly by
disengaging the hook-and-pile fastenings..

(6) Remove the headrest cover assemblies (30) and headrest cushion assemblies (35)
from the headrest assembly by disengaging the hook-and-pile fastenings.

(7) Remove the back cover assemblies (40) and backrest cushions (45) from the back
assembly by disengaging the hook-and-pile fastenings.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(8) Remove the literature pocket cover assemblies (-50) from the back assemblies by
disengaging the hook-and-pile fastenings.

B. Removal of the Control Cables

(Refer to IPL FIG 2)
(1) To provide easier access to the control cables:

(a) Remove the bottom cushion assembly.

(b) Pull on the legrest control lever and raise the legrest assembly.

(c) Unsnap the seatpan straps (REF IPL FIG 9, Items 25, 30) and unwrap from around Gutierrez
the seatpan rollers.

(d) Lift up the seatpan assembly, unclip the seatpan support stand (REF IPL FIG 9,
Item 5) and position the seatpan support stand (REF IPL FIG 9, Item 5) on the
seatpan roller to support the seatpan assembly.

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B. Removal of the Control Cables (Continued)

(Refer to IPL FIG 2)
(2) Disconnect the control cables (5, 10, 15) from the recline, legrest, and food paddle gas
springs.

(3) Unroute the control cables (5, 10, 15) from the console assembly (REF) by removing
the tiedown straps (20, 25, 40), ring connectors (30), push mounts (35), and cable
spacers (45) as required. Remove the 3M™ foam tape (50).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

NOTE: To access the tiedown straps (20, 25, 40), remove the cocktail table
assembly (REF IPL FIG 21, Item 45) by removing the hinged screw
covers (REF IPL FIG 21, Item 60) and screws (REF IPL FIG 21, Items 50, 55).

(4) Remove the seat control button assemblies (REF IPL FIG 21, Items 160, 165) by turning
the retainer a quarter-turn and lifting clear.

(5) Disconnect the control cables (5, 10, 15) from the seat control buttons.

C. Removal of the Legrest

(Refer to IPL FIG 3)
(1) Remove the legrest shroud (5) by removing the snap rivets (10).

(2) Disconnect the control cables (REF IPL FIG 2, Items 10, 15) from the lockable gas
spring (15) and extension lock assembly (REF IPL FIG 4, Item 25).

(3) Remove the lockable gas spring (15) from the seatpan front tube assembly (REF) by
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

removing the bolt (20) and nut (25).

(4) Remove the rod end assembly (45).

(5) To disassemble the rod end assembly (45), remove the bearing (-50) from the rod
end (-55).

(6) Remove the valve release (60) from the lockable gas spring (15) by removing the
retaining ring (30).

(7) Remove the lockable gas spring (15) from the legrest assembly (115) by removing the
washers (35) and nuts (40).

(8) To disassemble the valve release (60): Gutierrez

(a) Remove the top jaw (65) by removing the bolt (70).

(b) Remove the helical spring (75) from the bottom jaw (90).

(c) Remove the cable ferrule (80) from the bottom jaw (90) by removing the
retaining ring (85).

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C. Removal of the Legrest (Continued)

(Refer to IPL FIG 3)
(9) Remove the fixed shrouds (95, 105) by removing the snap rivets (100, 110).

(10) Remove the legrest assembly (115) from the seatpan assembly (REF) by removing the
bolts (120), bushings (125), spacers (130), nuts (135), screws (140), bushings (145),
spacers (150), nuts (155), bushings (160), washers (165), and nuts (170).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

D. Disassembly of the Legrest Assembly
(Refer to IPL FIG 4)
(1) Remove the legrest shroud (5) by removing the screws (10) and snap rivets (15).

(2) If necessary, remove the 3M™ loop tape (20).

(3) Remove the extension lock assembly (25) by removing the bolt (30), pivot pin (35),
spacer (40), and retaining ring (45).

(4) To disassemble the extension lock assembly (25):

(a) Remove the valve release (55) from the gas spring (50).

(b) To disassemble the valve release (55):

1 Remove the lever arm (60) by removing the bolt (65).

2 Remove the spring (70) from the valve release head (85).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

3 Remove the cable ferrule (75) from the valve release head (85) by removing
the retaining ring (80).

(5) Remove the paddle assembly (90) by removing the screws (95, 105) and washer (100).

(6) Remove the pivot support (110) by removing the screws (115).

(7) Remove the 3M™ hook tape (120) and 3M™ loop tape (125) from the frame link
assembly (135) by removing the rivets (-130).

E. Disassembly of the Paddle Assembly - Legrest Gutierrez

(Refer to IPL FIG 5)
(1) Remove the link arm assembly (5) from the legrest extension pan (170) by removing the
screw (10), bushings (15, 20), spacer (25), and washer (30).

(2) To disassemble the link arm assembly (5), remove the flanged bearing (35) from the
extension link arm (40).

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E. Disassembly of the Paddle Assembly - Legrest (Continued)

(Refer to IPL FIG 5)
(3) Remove the foot pan assembly (45) from the legrest extension pan (170) by removing
the screws (50).

(4) To disassemble the foot pan assembly (45):

(a) Remove the torque hinge mount assemblies (55, 80) from the foot paddle (165) by

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

removing the screws (60, 85).

(b) To disassemble the torque hinge mount assemblies (55, 80), remove the torque
hinge mounts (65, 90) and reeltorq insert (70, -95) from the pivot hinges (75, 100).

(c) Remove the paddle hinge mount assemblies (105, 135) from the torque hinge
mount assemblies (55, 80) by removing the bolts (-110, 140), washers (-115, 145),
and bushings (-120, 150).

(d) To disassemble the paddle hinge mount assemblies (105, 135), remove the
bearings (125, -155) from the paddle hinge mounts (130, -160).

F. Disassembly of the Frame Link Assembly

(Refer to IPL FIG 6)
(1) Remove the legrest pan assembly (5) by removing the screws (10).

(2) Remove the edging grommet (15), from legrest pan assembly (5).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(3) Remove the rotation pivot brackets (20, 40) by removing the screws (25, 45),
washers (30, 50), and nuts (35, 55).

(4) Remove the flanged bearings (60) and I-bolt (65).

(5) Remove the pivot extension bracket (70) by removing the screws (75).

(6) Remove the legrest lower cross bar (80) by removing the bolts (85) and nuts (90).

(7) Remove the extension bumpers (95) by removing the screws (100).

(8) Remove the IGUS drylin rails (105) from the link assemblies (120, 125) by removing the
screws (110).
Gutierrez
(9) Remove the custom coils (115).

G. Disassembly of the Link Assembly - Legrest

(Refer to IPL FIG 7)
(1) Remove the link shroud (5) by removing the snap rivets (10).

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G. Disassembly of the Link Assembly - Legrest (Continued)

(Refer to IPL FIG 7)
(2) Remove the link shroud (15) by removing the screws (20).

(3) Remove the link assembly (25) from the link assembly (95) by removing the
spacer (30) and retaining ring (35).

(4) To disassemble the link assembly (25), remove the bearings (40, 45) from the

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

legrest link (50).

(5) Remove the link assembly (55) and link shroud (90) from the link assemblies (95, 140)
by removing the spacers (60), washer (65), and retaining rings (70).

(6) To disassemble the link assembly (55), remove the bearings (75, 80) from the legrest
link (85).

(7) Remove the link assembly (95) from the legrest main body support (180) by removing
the bolt (100), washer (105), bushing (110), spacer (115), and nut (120).

(8) To disassemble the link assembly (95), remove the bearings (125) and pivot pins (130)
from the legrest link (135).

(9) Remove the link assembly (140) from the legrest main body support (180) by removing
the bolt (145), washer (150), bushing (155), and nut (160).

(10) To disassemble the link assembly (140), remove the bearings (165) and pivot pin (170)
from the legrest link (175).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

H. Removal of the Seatpan Assembly

(Refer to IPL FIG 8)
(1) Remove the seatpan assembly (5) from the riveted back assembly (REF) by removing
the bolt (10), washers (15, 30), bushing (20), collar (25), and nut (35).

J. Removal of the Seatpan Support

(Refer to IPL FIG 9)
(1) Remove the seatpan support stand (5) from the seatpan assembly (REF) by removing
the retaining ring (10) and flange bearing (15).
Gutierrez
(2) Remove the wire clip (20) from the seatpan assembly (REF).

(3) Remove the seatpan straps (25, 30) from the seatpan assembly (REF) by removing the
rivets (35) and washers (40).

NOTE: Reconnect the seatpan straps (25, 30) when they have been disconnected to
service other components on the seat.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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J. Removal of the Seatpan Support (Continued)

(Refer to IPL FIG 9)
(4) Remove the snap studs (45) from the seatpan assembly (REF) by removing the
rivets (50).

K. Disassembly of the Seatpan Assembly

(Refer to IPL FIG 10)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(1) Disconnect the bottom diaphragm (20) from the rail assemblies (25, 30) by disengaging
the hook-and-pile fastening.

NOTE: Use the tool listed in SPECIAL TOOLS, FIXTURES, AND EQUIPMENT
(Page Block 9000) and follow the instructions in reverse to remove the bottom
diaphragm (20) and crystal flex tube (15) from the rail assemblies (25, 30).

(2) Remove the front tube assembly (5) from the rail assemblies (25, 30) by removing the
bolts (10).

(3) Remove the crystal flex tube (15) from the bottom diaphragm (20).

L. Removal of the Headrest Frame Assembly

(Refer to IPL FIG 11)
(1) Remove the headrest assembly (5) from the back (REF) by releasing the captive
screws, pivoting the headrest assembly (5) forwards and pulling downwards to remove
from the slots in the back.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(2) Remove the receptacles (10) from the back (REF).

M. Removal of the Video Bezel / Upper Literature Pocket Assembly

(Refer to IPL FIG 12)
(1) Remove the upper literature pocket bonded assembly (5) from the back assembly (REF)
by removing the screws (10) and washers (15).

N. Removal of the Coat Hook

(Refer to IPL FIG 13)
Gutierrez
(1) Remove the bushing (-25) by removing the rivet (-30).

(2) Remove the coat hook pin (5) from the back frame (REF) by removing the spring (10),
washer (15), and retaining ring (20).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

P. Removal of the Lower Literature Assembly and Back Trim

(Refer to IPL FIG 14)
(1) Remove the lower literature assembly (5) from the back assembly (REF) by removing
the screws (10) and loop clamps (15).

(2) Remove the lower literature pocket handle (20) and lower literature pocket spring (25).

(3) Remove the lower literature pocket assembly (30) by removing the screws (35).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(4) Remove the back trim (40) from the back assembly (REF) by removing the screws (45)
and washers (50).

Q. Removal of the Back Assembly

(Refer to IPL FIG 15)
(1) Detach the seatpan assembly (REF IPL FIG 8, Item 5) from the back frame
assembly (5). Refer to Paragraph K.

(2) Disconnect the control cable (REF IPL FIG 2, Item 5) from the hydraulic lock (90).

(3) Remove the hydraulic lock (90) from the spreader assembly (REF) by removing the
nuts (110) and washers (115).

(4) Remove the hydraulic lock (90) from the back frame assembly (5) by removing the
bolt (95), washer (100), and nut (105).

(5) Detach the back frame assembly (5) from the spreader assembly (REF) at the
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

hydraulic lock side by removing the screw (45), shackle fitting (50), bushing (55),
washers (60, 65), nut (70), and vinyl cap (75). Loosen the screw (85) and remove
the screw (80).

(6) Detach the back frame assembly (5) from the spreader assembly (REF) at the
non-hydraulic lock side by removing the screws (10, 40), shackle fitting (15),
bushing (20), washers (25, 30), and nut (35).

(7) Carefully lift the back frame assembly (5) away from the spreader assemblies.

R. Disassembly of the Back Assembly

(Refer to IPL FIG 16) Gutierrez
(1) Remove the lower literature sub-brackets (5, 10) from the back frame assembly (125B)
by removing the screws (15).

(2) Remove the lower literature pocket brackets (20, 25) from the back frame
assembly (125B) by removing the screws (30).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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R. Disassembly of the Back Assembly (Continued)

(Refer to IPL FIG 16)
(3) Remove the literature spring (35) by removing the screws (40), loop clamps (45), and
nuts (50).

(4) Remove the literature spring supports (55) by removing the screws (60) and
washers (65).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(5) To disassemble the back frame assembly (125, 125B):

(a) Remove the back diaphragm (130, 130A) from the back frame
w/ quadrants (140, 140B).

NOTE: Use the tool listed in SPECIAL TOOLS, FIXTURES, AND EQUIPMENT
(Page Block 9000) and follow the instructions in reverse to remove the
back diaphragm (130, 130A).

(b) If necessary, remove the 3M™ hook tapes (135) from the back frame
w/ quadrants (140, 140B).

(c) To disassemble the back frame w/ quadrants (140, 140B), remove the quadrant
assemblies (145, 145B, 150, 150B) from the back frame (170) by removing the
pins (155), bushings (160), and retaining rings (165).

(6) Remove the comfort pads (70, 75) from the back frame assembly (125, 125B) by
removing the screws (80).

(7) Remove the upper literature pocket bracket assembly (85) by removing the
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

screws (90), washers (95), and rivets (-100, -105).

(8) Remove the video bezel mounts (110, 115) by removing the rivets (120).

S. Disassembly of the Quadrant Assembly

(Refer to IPL FIG 17)
(1) Remove the HIC links (5) from the quadrants (30, 30B) by removing the plain
bushings (10, 10A) and dowel pin (15).

(2) Remove the bushings (20, 25) from the quadrants (30, 30B).
Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
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T. Removal of the Electrical Components

[Refer to IPL FIG 18, SCHEMATIC AND WIRING DIAGRAMS (Page Block 2000) and 3D PDF
electrical drawings for more electrical details.]
NOTE: IPL FIG 18 contains a complete listing of components for parts ordering.
SCHEMATIC AND WIRING DIAGRAMS (Page Block 2000) contains detailed
guidance for removing electrical components and harnesses. Refer to 3D PDF
electrical drawings referenced in this CMM for specific electrical information related

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

to the product addressed in this CMM. USING 3D ELECTRICAL DRAWINGS
(Page Block 17000) contains guidance for 3D interface. 3D PDF electrical
installation drawings are available to the customer upon request. Requests should
be sent to the following E-mail address: ws_techpubs3d@collins.com

NOTE: For specific instructions on removal of the ISPS, refer to DESCRIPTION AND
OPERATION Section, Paragraph 3.N.

U. Removal and Disassembly of the Lower Console

(Refer to IPL FIG 19)
(1) Remove the rear panel assembly (5) from the frame assembly (REF IPL FIG 1,
Item -230) by removing the screws (10, 20), hinged screw covers (25), and snap
rivets (15).

(2) To disassemble the rear panel assembly (5):

(a) Remove the lower SPM panels (30, 35) by removing the screws (40).

(b) Remove the reinforcement bracket assembly (45) and lower trim bezels (65, 70)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

from the lower SPM panel shroud (75) by removing the screws (50).

(c) To disassemble the reinforcement bracket assembly (45), remove the clip nuts (55)
from the reinforcement bracket (60).

V. Removal of the Center Console and Console Plug

(Refer to IPL FIG 20)
(1) Disconnect the control cables (REF IPL FIG 2, Item 5). Refer to Paragraph B.

(2) Remove the rear trim bezel (REF IPL FIG 21, Item 105) by removing the screws (REF
IPL FIG 21, Item 110). Remove the rear trim assembly (REF IPL FIG 21, Item 115) by Gutierrez
removing the screws (REF IPL FIG 21, Item 120) and sliding upwards.

(3) Disconnect the IFE power cables and cut tiedown straps, as required.

(4) Remove the center console assembly (5) from the frame assembly (REF) by removing
the bolts (10) and dome plugs (15).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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V. Removal of the Center Console and Console Plug (Continued)

(Refer to IPL FIG 20)
(5) Lift the center console assembly (5) clear off the seat assembly.

W. Disassembly of the Center Console Assembly

(Refer to IPL FIG 21)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(1) Remove the armcap assemblies (5) by removing the screws (10).

(2) To disassemble the armcap assemblies (5):

(a) Remove the armcap closeout (15) from the overmold armcap assembly (40) by
removing the snap rivets (20).

(b) Remove the armcap trim (25) from the overmold armcap assembly (40) by
removing the bolts (30).

(c) Remove the bumpers (35).

(3) Remove the fixed cocktail table assembly (45) by removing the screws (50, 55) and
hinged covers (60).

NOTE: Deploy the sliding cocktail table assembly (80) to access the screws (50)
located at the front of the fixed cocktail table assembly (45).

(4) To disassemble the fixed cocktail table assembly (45), remove the body (65) from the
fixed cocktail table assembly (75) by removing the screws (70).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(5) Remove the cocktail table assembly (80) by removing the screws (85).

(6) Remove the bumper bar bracket (90) by removing the screws (95). Remove the
bumper grommet (100).

(7) Remove the rear trim bezel (105) by removing the screws (110).

(8) Remove the rear trim assembly (115) from the console structure assembly (300) by
removing the screws (120) and sliding upwards.

(9) To disassemble the rear trim assembly (115), remove the support bracket (125) and the
rear trim bezels (135, 145) from the rear panel (155) by removing the
screws (130, -140, 150). Gutierrez

(10) Remove the button assemblies (160, 165) by turning the retainers a quarter-turn and
lifting clear.

(11) Remove the side shrouds (170, 185) by removing the snap rivets (175, 180, -190, -195).

(12) Remove the articulating hinge assemblies (200) by removing the screws (205).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

W. Disassembly of the Center Console Assembly (Continued)

(Refer to IPL FIG 21)
(13) Remove the pocket assembly (210) by removing the bolts (215) and snap rivets (220).

(14) Remove the life vest box door assembly (225) by removing the screws (230).

(15) To disassemble the life vest box door assembly (225):

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(a) Remove the latch assembly (235) by removing the captive screws (REF).

(b) To disassemble the latch assembly (235), remove the life vest pull strap (240) from
the dual pawl assembly (-245).

(16) Remove the front bottom bezel assembly (250) by removing the screws (255).

(17) To disassemble the front bottom bezel assembly (250), remove the front bottom trim
bezels (-260, -265) by removing the screws (270).

(18) Remove the front trim assembly (275) by removing the screws (280, 285).

(19) Remove the center console foam (-290) and 3M™ adhesive transfer tape (295) from the
console structure assembly (300).

X. Disassembly of the Cocktail Table Assembly

(Refer to IPL FIG 22)
(1) Remove the carriage and rail (5) from the cocktail table assembly (45) by removing the
screws (10).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(2) Remove the magnetic ring (15) by removing the screw (20).

(3) Remove the striker (25) from the cocktail table assembly (45) by removing the rivets (30)
and vinyl caps (35).

(4) Remove the snap rivet (40) from the cocktail table assembly (45).

Y. Disassembly of the Seat Control Button Assembly

(Refer to IPL FIG 23)
(1) Remove the control buttons (5, 10, 15) from the seat control housing (60) by removing Gutierrez
the retaining ring (25) and seat control pin (20).

(2) Remove the helical springs (30) from the control buttons (5, 10, 15).

(3) Remove the retainer assemblies (35) from the seat control housing (60) by removing the
screws (40).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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Y. Disassembly of the Seat Control Button Assembly (Continued)

(Refer to IPL FIG 23)
(4) To disassemble the retainer assemblies (35), remove the retaining clip (45) from the
RJU and RJM bezel (55) by removing the screw (50).

Z. Disassembly of the Pocket Assembly

(Refer to IPL FIG 24)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(1) Remove the side pocket panels (5, 15) by removing the snap rivets (10, -20).

(2) Remove the pocket shroud panel (25) by removing the snap rivets (30).

(3) Remove the lower pocket panels (35, 45) by removing the snap rivets (40, -50).

(4) Remove the FWD pocket panels (55, 65) from the aft pocket panel (75) by removing the
snap rivets (60, -70).

AA. Disassembly of the Front Trim Assembly

(Refer to IPL FIG 25)
(1) Remove the life vest top shroud panel (5) by removing the screws (10) and clip
nuts (15).

(2) Remove the front trim assembly (20) by removing the screws (25).

(3) To disassemble the front trim assembly (20), remove the latch striker (-30) by removing
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

the retaining ring (-35).

(4) Remove the bottle bucket (40), front trim bezel (45), and trim bezel (50) from the life vest
top shroud panel (5).

AB. Disassembly of the Console Structure Assembly - Non-Video

(Refer to IPL FIG 26)
(1) Remove the life vest box assembly (5) by removing the screws (10).

(2) Remove the cocktail table (15) by removing the screws (20).

(3) Separate the life vest bracket assemblies (25, 45) by removing the screws (30, 50). Gutierrez

(4) To disassemble the life vest bracket assemblies (25, 45), remove the clip nuts (35, 55)
from the life vest bracket attachments (40, 60).

(5) Separate the console side panels (65, 80) by removing the screws (70, 75, 85, 90).

(6) Remove the center brace (95) by removing the bolts (100).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
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AB. Disassembly of the Console Structure Assembly - Non-Video (Continued)

(Refer to IPL FIG 26)
(7) Remove the hinge support (105) from the bracket assembly (120) by removing the
bolts (115) and screw (110).

(8) To disassemble the bracket assembly (120), remove the clip nut (-125) from the trim
bracket PC power (-130).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

AC. Removal of the Foodtray
(Refer to IPL FIG 27)
(1) Deploy the foodtray assembly (5).

(2) Remove the foodtray assembly (5) from the endbay assembly (REF IPL FIG 29,
Items 5, -10) by removing the screws (10) and lifting clear.

AD. Disassembly of the Foodtray Assembly

(Refer to IPL FIG 28)
(1) Remove the foodtray leaf assembly (5) from the foodtray main leaf (170) by removing
the hinges (10) and hinge pins (15).

(2) Remove the latch bracket (20) by removing the screws (25).

(3) Remove the socket drive shoulder post (30) and nut (35).

(4) Remove the foodtray forward stop (40) by removing the screws (45).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(5) Remove the foodtray dampener assembly (50) by removing the bolts (55).

(6) To disassemble the foodtray dampener assembly (50), remove the bearing (-60) from
the dampener housing (65).

(7) Remove the rotary damper (70) from the closeout assembly (75).

(8) To disassemble the closeout assembly (75), remove the bearing (-80) from the foodtray
closeout (-85).

(9) Remove the door cover shroud (90) by removing the snap rivets (95).
Gutierrez
(10) Remove the foodtray assembly arm linkage (100) by removing the screws (105).

(11) To disassemble the foodtray assembly arm linkage (100):

(a) Remove the tray table strut (110) and pivot link (120) from the foodtray
paddle (140) by removing the dowel pins (115, 125).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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MiQ™ 1367870 SERIES

AD. Disassembly of the Foodtray Assembly (Continued)

(Refer to IPL FIG 28)
(b) Remove the bumper tray table (130) from the foodtray paddle (145) by removing
the screws (135).

(c) Remove the bearings (140) from the foodtray paddle (145).

(12) Remove the rails (150) from the foodtray main leaf (170) by removing the screws (155).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(13) Remove the IGUS carriages (160, 165) from the foodtray main leaf (170).

AE. Removal of the Endbay

(Refer to IPL FIG 29)
(1) Remove the endbay assemblies (5, -10) by removing the bolts (15).

(2) Carefully lift the endbay assemblies (5, -10) away from the frame assembly (REF).

AF. Disassembly of the IUL Endbay Assembly

(Refer to IPL FIG 30)
(1) Remove the rear access EPL (5) and front access EPL (10) by removing the
screws (15).

(2) Install the armcap assemblies (20, 20A) by installing the screws (25).

(3) To disassemble the armcap assemblies (20, 20A), remove the armcap
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

closeouts (30, 30A) from the armcap subassemblies (45, 45A) by removing the snap
rivets (35) and 3M™ adhesive transfer tape (-40).

(4) Remove the bonded shroud assemblies (50, 50A) by removing the snap rivets (55).

(5) Remove the bonded shroud assemblies (60, 60A) by removing the screws (65).

(6) Remove the rubstrip assemblies (70, 70A) by removing the screws (75).

(7) To disassemble the rubstrip assemblies (70, 70A), remove the endbay front
rubstrips (80, 80A) from the endbay forward rubstrips (90, 90A) by removing the
screws (85).
Gutierrez
(8) Remove the endbay aft rubstrips (95, 95A) by removing the screws (100).

(9) Remove the endbay arm button assemblies (105, 105A) by removing the
screws (110, 110A, 120) and vinyl cap (-115) and disconnecting from the control
cable (REF IPL FIG 32, Item 5).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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AF. Disassembly of the IUL Endbay Assembly (Continued)

(Refer to IPL FIG 30)
(10) Remove the endbay shroud assemblies (125, 125A) from the INBD endbay bracket
assemblies (165, 165A) by removing the snap rivets (130, 130A) and screws (135).

(11) Remove the PAX side endbay shrouds (140, 140A) and endbay foams (145, 145A) from
the INBD endbay bracket assemblies (165, 165A) by removing the snap
rivets (150, 150A).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(12) If necessary, remove the 3M™ adhesive transfer tape (155) and 3M™ double sided
tape (160) from the bonded shroud assemblies (50, 50A, 60, 60A).

AG. Disassembly of the Endbay Arm Button Assembly

(Refer to IPL FIG 31)
(1) Remove the endbay arm button (5) from the button housing (35) by removing the button
pin (10), retaining rings (15), and spring (20).

(2) Remove the pulley (25) from the button housing (35) by removing the screw (30).

AH. Disassembly of the Endbay Bracket Assembly - INBD

(Refer to IPL FIG 32)
(1) Remove the handicap latch (5) by removing the screw (10).

(2) Remove the endbay control cable (15) and cable ferrule (20) from the endbay side
bracket (35) by removing the retaining rings (25) and tiedown straps (-30).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(3) To disassemble the endbay arm bowtie assembly (40), refer to Paragraph AJ.

AJ. Disassembly of the Bowtie Assembly - Endbay Arm

(Refer to IPL FIG 33)
WARNING: USE EXTREME CAUTION WHEN CONNECTING OR DISCONNECTING THE
SCREW (10) OR INJURY CAN RESULT. THIS SCREW (10) ATTACHES THE
CABLE OF THE SPRING REEL AND IS UNDER HIGH TENSION!

(1) Remove the INBD endbay arm assembly (5) from the bowtie endbay assembly (45) by
removing the screw (10), spacer (15), and sliding apart.
Gutierrez
(2) Remove the reel (20) from the bowtie endbay assembly (45) by removing the screw (25)
and washer (30).

(3) Remove the reel adjuster (35) by removing the screw (40).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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AJ. Disassembly of the Bowtie Assembly - Endbay Arm (Continued)

(Refer to IPL FIG 33)
(4) To disassemble the bowtie endbay assembly (45):

(a) Remove the pivot assembly (50) from the bowtie endbay assembly (115) by
removing the screws (55), latch caps (60), and spring (65).

(b) To disassemble the pivot assembly (50):

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

1 Remove the handicap latches (70, 80) from the endbay arm pivot (95) by
removing the screws (75, 85).

2 Remove the bearings (90) from the endbay arm pivot (95).

(c) Remove the rollon rails (100, 105) from the bowtie endbay assembly (115) by
removing the screws (110).

(d) To disassemble the bowtie endbay assembly (115):

1 Remove the stew step strut (120) by removing the screws (125).

2 Remove the adjuster restrain bracket (130) by removing the screws (135).

3 Remove the cord guide (140) by removing the rivets (145).

AK. Disassembly of the Endbay Arm Assembly - INBD

(Refer to IPL FIG 34)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(1) Remove the sliders (5, 35, 65, 95) from the carriage arm mount plates (20, 50, 80, 110)
by removing the screws (10, 40, 70, 100) and washers (15, 45, 75, 105).

(2) Remove the carriage arm mount plates (20, 50, 80, 110) by removing the
bolts (25, 55, 85, 115) and washers (30, 60, 90, 120).

(3) Remove the armcap hinge assemblies (125) and hinge cover (155) from the endbay arm
frame assembly (160) by removing the screws (130).

(4) To disassemble the armcap hinge assemblies (125), remove the machined
hinge (135) from the hinge base (150) by removing the pin (140) and spring (145).

Gutierrez
AL. Disassembly of the Frame Assembly - Endbay Arm
(Refer to IPL FIG 35)
(1) Remove the table latch assembly (5) by removing the screws (10) and disconnecting
from the foodtray latch cable (REF IPL FIG 39, Item 5). Remove the retaining ring (15).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

AL. Disassembly of the Frame Assembly - Endbay Arm (Continued)

(Refer to IPL FIG 35)
(2) Remove the cord reel access door assembly (20) from the inner endbay arm frame
assembly (55) by removing the screws (25).

(3) Remove the mechanical reel (50) from the cord reel access door assembly (20) by
removing the screw (30) and reel adjuster (45).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(4) Remove the inner endbay arm frame assembly (55) from the outer endbay arm frame
assembly (110) by removing the screws (60).

(5) To disassemble the inner endbay arm frame assembly (55):

(a) Remove the endbay arm handhold (65) by removing the screws (70).

(b) Remove the stop block assembly (75) from the endbay arm frame assembly (95)
by removing the screws (80).

(c) Remove the grommet bumpers (85) from the stop block (90).

WARNING: USE EXTREME CAUTION WHEN CONNECTING OR DISCONNECTING THE

BOLT (100) OR INJURY CAN RESULT. THIS BOLT (100) ATTACHES THE
CABLE OF THE SPRING REEL AND IS UNDER HIGH TENSION!

(6) Remove the foodtray latch cable (REF IPL FIG 39, Item 5) from the mechanical reel (50)
(Cord Reel) from the outer endbay arm frame assembly (110) by removing the
bolt (100).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(7) Remove the grommet bumper (105) from the inner endbay arm frame assembly (55).

AM. Disassembly of the Wall Endbay Assembly - Special

(Refer to IPL FIG 36)
(1) Remove the armcap assembly (5) by removing the screws (10).

(2) To disassemble the armcap assembly (5), remove the armcap closeout (15) from the
armcap subassembly (30) by removing the snap rivets (20) and the 3M™ adhesive
transfer tape (-25).

(3) Remove the wall PAX side shroud (35) by removing the snap rivets (40).
Gutierrez
(4) Remove the wall PAX aft shroud (45) by removing the snap rivets (50).

(5) Remove the bonded shroud assembly (55) and wall side shroud (65) from the endbay
wall assembly (80) by removing the snap rivets (60, 70).

(6) If necessary, remove the 3M™ adhesive transfer tape (-75).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

AM. Disassembly of the Wall Endbay Assembly - Special (Continued)

(Refer to IPL FIG 36)
(7) To disassemble the endbay wall assembly (80):

(a) Remove the hinge assemblies (85) from the endbay wall arm assembly (135) by
removing the screws (90).

(b) To disassemble the hinge assembly (85), remove the machined hinge (95) from

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

the hinge base (110) by removing the hinge pin (100) and hinge spring (105).

(c) Remove the hinge cover (115) by removing the screw (120).

(d) Remove the baggage bar (125) by removing the screw (130).

AN. Disassembly of the Endbay Wall Arm Assembly - Special

(Refer to IPL FIG 37)
(1) Remove the table latch assembly (5) by removing the screws (10) and disconnecting
from the foodtray latch cable (REF IPL FIG 39, Item 5) by removing retaining ring (15).

(2) Remove the cord reel access door assembly (20) from the endbay special wall
assembly (55) by removing the screws (25).

(3) Remove the mechanical reel (50) from the cord reel access door assembly (20) by
removing the screw (30) and reel adjuster (45).

(4) Remove the endbay special wall assembly (55) from the outer endbay special wall arm
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

assembly (75) by removing the screws (60).

WARNING: USE EXTREME CAUTION WHEN CONNECTING OR DISCONNECTING THE

BOLT (65) OR INJURY CAN RESULT. THIS BOLT (65) ATTACHES THE
CABLE OF THE SPRING REEL AND IS UNDER HIGH TENSION!

(5) Remove the foodtray latch cable (REF IPL FIG 39, Item 5) from mechanical reel (50)
(cord reel) from the outer endbay special wall arm assembly (75) by removing the
bolt (65).

(6) Remove the grommet bumper (70) from the endbay special wall assembly (55).

AP. Disassembly of the Table Latch Assembly Gutierrez

(Refer to IPL FIG 38)
(1) Remove the table release latch (5) from the table latch housing (35) by removing the
dowel pin (10).

(2) Remove the spring (15).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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AP. Disassembly of the Table Latch Assembly (Continued)

(Refer to IPL FIG 38)
(3) Remove the cable adapter (20) from the table latch housing (35) by removing the
screw (25) and nut (30).

AQ. Disassembly of the Endbay Arm Frame Assembly - Outer

(Refer to IPL FIG 39)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(1) Remove the latch cables (5, 5A) by removing the tiedown straps (10) and retaining
ring (15).

(2) Remove the pulley (20) by removing the bolt (25).

(3) Remove the release latch (30) from the endbay arm frame assembly (100) by removing
the screw (35), spring (40), bushing (45), and nut (50).

(4) Remove the table mount assembly (55) by removing the screws (60).

(5) To disassemble the table mount assembly (55), remove the grommet bumper (65) from
the table mount block (70).

(6) Remove the rails (75, 75A) from the endbay arm frame assembly (100) by removing the
screws (80).

(7) Remove the support hinge (85) from the endbay arm frame assembly (100B) by
removing the screws (90, 95).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

AR. Removal of the Shroud

(Refer to IPL FIG 40)
(1) Remove the mount plates/shroud assembly (5) by cutting the straps (10) and 3M™
double sided tapes (-15).

(2) If necessary, remove the edging grommet (20) from the mount plates/shroud
assembly (5).

(3) To disassemble the mount plates/shroud assembly (5) remove the ISPS shroud (25)
from the door assembly (30).

(4) To disassemble the door assembly (30), remove the IFE shroud face plate (35), turn the Gutierrez
studs (40) a quarter-turn in counterclockwise direction and lift clear.

(5) To disassemble the disconnect shroud assembly (65), remove the disconnect
shroud (70) turn the studs (75) a quarter-turn in counterclockwise direction to disengage
them from the receptacles (110) and lift clear.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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AR. Removal of the Shroud (Continued)

(Refer to IPL FIG 40)
(6) Remove the disconnect bracket assembly (85) and disconnect leg isolator (90) by
removing the bolts (95), spacers (100), and nuts (105).

(7) If necessary, remove the edging grommet (115) from the disconnect bracket
assembly (85).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(8) If required, remove the 3M™ double sided tapes (-120) from the disconnect leg
isolator (90).

AS. Removal of the Electrical Raceway

(Refer to IPL FIG 41)
(1) Remove the spreader cover (5) by cutting the tiedown straps (10).

(2) Remove the pancake raceway (15, 30, 45) from the beams (REF) by cutting the tiedown
straps (20, 35, 50) and removing the 3M™ double sided tapes (-25, 40, -55).

(3) Remove the leg isolator shroud IFE (60) by cutting the tiedown straps (65).

(4) Remove the leg IFE shroud console (70) and cable protection shroud (75) by removing
the 3M™ double sided tapes (80).

AT. Removal of the Baggage Bar

(Refer to IPL FIG 42)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(1) Remove the standard baggage bar tube (5) by removing the screw (10), washer (15),
and set screw (20).

(2) Remove the canted baggage bar tube (25) by removing the screw (30), washer (35),
and set screw (40).

(3) If necessary, remove the baggage bar doubler (-45).

(4) Remove the baggage bar plugs (50) from the standard baggage bar tube (5) and canted
baggage bar tube (25).

AU. Disassembly of the Frame Assembly Gutierrez

(Refer to IPL FIG 43)
(1) Remove the non-lock spreader assemblies (5, 10) by removing the bolts (15) and
nuts (20), and sliding the non-lock spreader assemblies (5, 10) off the beams (55).

(2) Remove the leg assemblies (25) from the beams (55). Refer to Paragraph AW for
removal instructions.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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AU. Disassembly of the Frame Assembly (Continued)

(Refer to IPL FIG 43)
(3) Remove the lock spreader assemblies (30, 35) by removing the bolts (40, 45) and
nuts (50), and sliding the lock spreader assemblies (30, 35) of the beams (55).

AV. Disassembly of the Spreader Assembly

(Refer to IPL FIG 44)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(1) Remove the articulation roller (5) from the roller machined shaft (40, 40A) by removing
the screw (10) and washer (15).

(2) Remove the recline lock eyebolt (20) from the spreader assembly (30B) by removing the
retaining ring (25).

(3) To disassemble the spreader assemblies (30, 30B), remove the flanged bushing (35)
and machined shaft roller (40, 40A) from the spreader (45, 45B).

AW. Disassembly of the Leg Assembly

(Refer to IPL FIG 45)
(1) Remove the leg assembly (REF) from the beams (REF IPL FIG 43, Item 55) by
loosening the bolts (5, 15) and nuts (10, 20).

(2) Remove the stud (25) and anti-rattle nuts (30) from the machined leg (70).

(3) Remove the track fitting (35) from the machined leg (70) by removing the
bolt (40), spacers (45), and nut (50).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(4) Remove the doublers (55) from the machined leg (70) by removing the bolt (60) and
nut (65).

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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CLEANING

1. General

NOTE: There are multiple cleaning agents and materials listed in this page block. Determine the
applicable cleaning process for the material that applies to each specific seat assembly.
All applicable WARNINGS, CAUTIONS, and NOTES should be thoroughly reviewed
before initiating any type of cleaning process.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

External surfaces and upholstery should be periodically checked and cleaned. Table 4001 lists
recommended disinfectants used on the seat/furniture assembly. Table 4002 lists cleaning agents
and materials used on the seat/furniture assembly.

Since each cleaning agent has specific features and limitations, carefully follow the instructions
given on any product container to ensure best results. The normal cleaning method for seat
covers is to remove them from the seat and commercially dry clean with perchlorethane.

NOTE: Before dry cleaning, mate the hook attachment with the opposing piece of pile.

To comply with Electrical Wiring Interconnecting Systems (EWIS) maintenance procedure it is

essential to keep all wiring bundles and electrical components free of dust, dirt and contamination
to prevent any electrical malfunction due to arcing, short circuit, etc.

2. Disinfectants

CAUTION: THE FAA EMPHASIZES THAT OWNERS AND OPERATORS SHOULD FOLLOW,
AND NOT EXCEED, THE DISINFECTANT MANUFACTURER’S INSTRUCTIONS
FOR APPLICATION OF DISINFECTANTS IDENTIFIED AS APPROPRIATE FOR
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

THE AIRCRAFT BY THE AIRCRAFT MANUFACTURER. IMPROPER

APPLICATION OF DISINFECTANTS (EXCESSIVE TEMPERATURE, DWELL TIME,
ETC.) MAY RESULT IN DAMAGE TO SEATING/FURNITURE MATERIALS,
INCLUDING, BUT NOT LIMITED TO, STAINING, EMBRITTLEMENT, INCREASED
FLAMMABILITY AND ELECTRICAL SHORT CIRCUIT. REFER TO FAA SPECIAL
AIRWORTHINESS INFORMATION BULLETIN NM-20-17.

NOTE: FAA Aviation Safety Special Airworthiness Information Bulletins can be found online at:
https://www.faa.gov/aircraft/safety/alerts/saib/

Table 4001
Recommended Disinfectants Gutierrez

AGENT USAGE
Alcohol - Ethyl Approximately 70% Concentration
Alcohol - Isopropyl Approximately 70% Concentration
Disinfectants - Neutral PH Level 6.0 - 8.0
Caustic and Ammonia Free

U.S. Export Classification: EAR 9E991 25-20-83-4667

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3. List of Cleaning Materials and Usage

WARNING: ISOLATE POWER BEFORE CLEANING ANY ELECTRICAL COMPONENTS OR

WIRING.

WARNING: SOLVENT CLEANING AGENTS MUST BE USED IN A WELL VENTILATED

AREA. AVOID PROLONGED SOLVENT CONTACT WITH SKIN AND AVOID
BREATHING VAPORS. OBSERVE APPROPRIATE FIRE REGULATIONS.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

WARNING: READ AND FOLLOW ALL LABEL DIRECTIONS FOR THE CLEANING
MATERIALS IN USE. SOME PRODUCTS CAN BE HAZARDOUS TO HEALTH
UNLESS SPECIAL PRECAUTIONS ARE FOLLOWED.

WARNING: TO MAINTAIN THE FLAMMABILITY CHARACTERISTICS OF THE CUSHIONS

AND COVERS OVER THE PRODUCT LIFE CYCLE, THE CLEANING AND
MAINTENANCE INSTRUCTIONS OF THIS CMM, AS LISTED IN THIS PAGE
BLOCK MUST BE FOLLOWED. IMPLEMENTATION OF THIS CLEANING AND
MAINTENANCE PROCESS IS THE RESPONSIBILITY OF THE AIRLINE.

CAUTION: DO NOT USE THE FOLLOWING TYPES OF CLEANING AGENTS: CITRUS

CLEANERS, TRICHLORETHYLENE, TRICLENE, METHYL ETHYL KETONE
(MEK), METHYL ISO BUTYL KETONE (MIBK), LYES, ALKALINE CLEANERS,
TOLUOL, BENZOL, ACETONE AND CARBON TETRACHLORIDE.

CAUTION: READ AND FOLLOW ALL LABEL DIRECTIONS FOR THE CLEANING
MATERIALS IN USE. SOME PRODUCTS MAY CAUSE DAMAGE TO FABRICS
OR FINISHES WHEN USED INCORRECTLY.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

CAUTION: ALWAYS TEST A CLEANING AGENT ON A SMALL, INCONSPICUOUS AREA TO

BE SURE IT WILL NOT STAIN OR DAMAGE THE FABRIC OR FINISH.

CAUTION: DO NOT USE ISOPROPYL ALCOHOL ON ANY SURFACE THAT CONTAINS

PRINTED LETTERING/GRAPHICS OR DEGRADATION CAN RESULT.

CAUTION: USING A MELAMINE FOAM PAD TO CLEAN THE SEAT/FURNITURE ASSEMBLY

WILL, OVERTIME, DAMAGE DECORATIVE LAMINATE, PLASTIC COMPONENTS,
COATINGS AND FINISHES. THEY SHOULD NOT BE USED UNLESS NEEDED.

NOTE: Follow the instructions on the product label for the appropriate application and dilution
requirements. Hot water enhances the cleaning power of most cleaning compounds. Gutierrez

NOTE: Service Letter SL-20-065 is attached to this CMM to provide information to airline
customers to help prevent discoloration and/or degradation of plastics in cabin interior
products due to the application of cleaning products and disinfectants.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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Table 4002
Cleaning Agents and Materials
USAGE CLEANING AGENT
Composite Mild soap and water
Neutral cleaner (Caustic & Ammonia Free) with PH level of 6.0 - 8.0
Ethyl or Isopropyl Alcohol (Approximately 70% Concentration)
Fabric-Backed Vinyl Mild soap and water

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Leather (Generic) Commercial saddle soap
Metal: Dirt, Grime, Mild soap and water
Grease and Oil Neutral cleaner (Caustic & Ammonia Free) with PH level of 6.0 - 8.0
Ethyl or Isopropyl Alcohol (Approximately 70% Concentration)

(Agents may be applied using a melamine foam pad.)

Painted Surface Soapy water (recommended)

(Agents may be applied using a melamine foam pad.)

PCU Isopropyl alcohol (Approximately 70% Concentration), mild
detergent, aliphatic naphtha
Perrone™ (EnduraLite®) Mild soap and water with a clean cloth or horsehair brush
Plastic: Dirt and Grime Mild soap and water
Neutral cleaner (Caustic & Ammonia Free) with PH level of 6.0 - 8.0
Ethyl or Isopropyl Alcohol (Approximately 70% Concentration)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(Agents may be applied using a melamine foam pad.)

Tape Adhesive Residue Isopropyl alcohol (Approximately 70% Concentration)
Ultraleather™, Cortina Recommended mild (non-detergent) soap and water but always
Leather, Muirhead® follow manufacturer’s cleaning instructions.
Leather
Upholstery Isopropyl alcohol (Approximately 70% Concentration), grain alcohol
(ethanol), wood alcohol (methanol), naphtha, white kerosene,
petroleum, ether, heptane, freon TF, mild soap and water, upholstery
shampoo
NOTE: Equivalent substitutes may be used for cleaning agents listed above.
Gutierrez
4. Cushion Cleaning

The dress covers protect the cushion from most dirt and staining. If the cushion is thought to have
been significantly stained by any organic or inorganic substances, the cushion should be replaced
due to possible deterioration of the fire blocking properties of the cushion. For light stains on the
cushions, dabbing with a soft cloth or sponge and warm water is permissible. The cushions must
not be exposed to any chemical cleaning agents. Never rub or scrub a cushion with any material
or device.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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5. Electrical Component and Wiring Cleaning

A. Clean all wiring bundles and/or electrical components with a vacuum cleaner or light brush.

B. For more persistent contamination use a clean, dry lint-free cloth.

6. Fabric-Backed Vinyl Cleaning

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Clean fabric-backed vinyl with a mild soap and water solution and wipe clean and dry. Do not use
solvent-type of cleaners on vinyl.

7. Leather (Generic) Cleaning

CAUTION: DO NOT USE DETERGENTS, CITRUS CLEANERS, OR SOLVENTS FOR

CLEANING LEATHER. FOR SPECIALTY CFE LEATHER (E.G., CORTINA,
MUIRHEAD®), DO NOT USE SADDLE SOAP AND FOLLOW THE
MANUFACTURER’S CLEANING INSTRUCTIONS.

Clean leather covers with commercial saddle soap.

8. Metal Parts Cleaning

A. Dirt, Grime, Grease and Oil

Moisten a clean, dry cloth or melamine foam pad with the desired agent shown in Table 4002
and thoroughly wipe metal parts. Repeat as required to remove stubborn accumulations of
dirt, grime, grease and oil. Dry with a fresh, clean, and dry cloth.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

9. Muirhead® Leather Cleaning

A. Clean with a damp cloth soaked with a mild soap (not detergent) and water solution. Apply the
damp cloth to the surface of the leather in a light circular motion, turning the cloth regularly.
Avoid aggressive rubbing action. Remove the residue with a damp cloth rinsed in clean warm
water.

B. Allow to dry and lightly polish using a clean, dry soft cloth.

C. Avoid ‘feeding’ the leather with care kits, saddle soaps, and waxes.

10. Painted Surface Cleaning

Gutierrez

Clean painted surfaces with non-abrasive soaps. Agents may be applied using a melamine foam
pad.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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11. PCU Cleaning

WARNING: PERFORM DE-ACTIVATION PROCEDURES AS DETAILED IN THE

DISASSEMBLY CHAPTER OF THE APPROPRIATE AIRCRAFT MANUAL.

WARNING: ALIPHATIC NAPHTHA IS FLAMMABLE. USE NAPHTHA ONLY IN A WELL

VENTILATED AREA AWAY FROM FLAMES OR ELEVATED TEMPERATURES.

WARNING: USE STANDARD SAFETY PRECAUTIONS FOR HANDLING FLAMMABLE

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

MATERIALS.

A. Lightly brush all accessible electrical parts, connections, and wiring with a soft-bristle,
non-metallic brush.

B. Use dry, filtered air at moderate pressure (25 psi maximum) to blow away loosened dust and
dirt.

C. Clean all accessible areas with a clean, lint-free cloth or soft bristle brush moistened in
aliphatic naphtha.

D. Allow parts to thoroughly air dry before returning to service.

12. Perrone™ (EnduraLite®) Cleaning

A. General Light Duty Cleaning

(1) Use a mild soap and water solution for cleaning EnduraLite® in conjunction with a clean
cloth or horsehair brush.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(2) Instructions:

(a) Spray or soak the mild soap and water solution into a cloth or the bristles of a
horsehair brush.

(b) Apply brush to the EnduraLite® surface and agitate in a random circular motion.

(c) Wipe off soil and excess chemical with a clean, soft cloth.

B. Heavy Duty Cleaning

Gutierrez
(1) Use Perrone’s Deep Cleaner (#DC-305, #DC-328, #DC-332, #DC-355) for leather in
conjunction with a horsehair brush to effectively remove heavy body oils and soils.

(2) Instructions:

(a) Spray Perrone’s Deep Cleaner into the bristles of a horsehair brush.

(b) Apply brush to the EnduraLite® surface and agitate in a random circular motion.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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(c) Wipe off soil and excess chemical with a clean, soft cloth.

(d) For extremely heavily soiled areas, repeat steps (a) through (c).

C. Ink & Stains

(1) Use Perrone’s Ink & Stain Remover as needed to remove stubborn stains that cannot be
removed by following general cleaning instructions. For best results, go after stains as

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

soon as possible.

(2) Instructions:

(a) Use a cotton swab or tip of clean cloth to locally apply Perrone’s Ink & Stain
Remover to the stain area.

(b) The cleaning agent will immediately start to break up the stain from EnduraLite®
surface.

(c) Wipe affected area by constantly turning clean, dry part of cotton swab or cloth as
to not re-deposit stain.

D. Leather Touch-Up Pen System from Perrone™ Aerospace

(1) Step 1 - Ink Treatment (Remover) Pen P/N ITR-101:

(a) Use Ink Treatment to remove dried, ink stained leather. Shake well before use.
Gently apply felt top of pen to stained area until ink is no longer visible. Follow up
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

with Step 2 - Leather Touch Up.

NOTE: Some discoloration and/or gloss change of the leather may occur during
this process.

(2) Step 2 - Leather Touch-Up Pen

(a) Part Number LTP-XXXX (4 digit number is specific to a customer leather color part
number. Contact Perrone™ Customer Service for this part number.)

(b) First, use STEP 1 - Ink Treatment on affected area of dried ink stain as directed on
label. Next, use STEP 2 - Leather Touch-Up to effectively refinish and protect the
affected area. Shake well before use. Gently apply the felt tip of pen to the area,
Gutierrez
ensure that the leather touch-up from pen is saturating the felt tip. This is done by
lightly depressing the felt tip into the black dispenser cap.

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(c) Allow finish from pen used to touch-up area to dry and cure for a minimum of 1
hour before passenger interaction if in contact area. If the area is in a non-contact
area of the leather, then wait until area is dry to the touch before releasing to
service. You may use a hair dryer to hasten the drying process. Do not clean area
within 24 hours of performing touch-up.

NOTE: The Leather Touch-Up Pen System is to be used as a supplement to a

comprehensive leather cleaning, maintenance and repair program from
Perrone™ Aerospace. The system does not constitute a complete

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

leather repair process. Rather, it is a short term solution for our valued
customers until the part can be sent off to a qualified leather FAA/EASA
Repair Station. Failure to follow along with manufacturer’s
recommendations for all of these areas can result in premature wear or
failure of the durability and aesthetics of your leather.

E. Gum Removal

(1) Use Perrone’s Deep Cleaner for leather (#DC-305, #DC-328, #DC-332, #DC-355) to
effectively remove gum from EnduraLite®.

(2) Allow product to soften gum to allow mechanical removal. For best results, go after gum
areas as soon as possible following the instructions below.

(3) Instructions:

(a) Spray Perrone’s Deep Cleaner directly onto the gum area.

(b) Allow product to stand on the gum area for 3-5 minutes.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(c) Using a wood craft stick or similar, mechanically remove the softened gum.

(d) If any gum residue remains, use Perrone’s Deep Cleaner in conjunction with a
horsehair bristle brush. Follow general cleaning instructions.

F. Frequency of Cleaning

(1) It is recommended that EnduraLite® be cleaned every 30 days in a commercial seating

application.

(2) For stubborn stains, clean as needed.

Gutierrez
(3) It is recommended to go after stains as quickly as they happen.

G. Recommended Amount of Cleaning Product Per Passenger Place

(1) Use approximately 1 oz. per (economy) passenger place of cleaning solution for the light
duty cleaning of EnduraLite®.

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(2) Use approximately 1 oz. per (economy) passenger place of Perrone’s Deep Cleaner
(#DC-305, #DC-328, #DC-332, #DC-355) for the heavy-duty cleaning of EnduraLite®.

(3) Use Perrone’s Ink & Stain Remover as needed for ink, stains and heavy soiling.

H. EnduraLite® Gluing or Laminating

(1) Perrone™ Aerospace recommends the use of water based adhesives and glues when

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

working with EnduraLite®.

(2) It is not recommended to use solvent based glues or adhesives on EnduraLite® due to
the volatile nature of these products.

(3) For specific applications regarding gluing or laminating, please contact Perrone™
Aerospace.

PERRONE™ AEROSPACE
182 A Riverside Drive Telephone: +1 518 853 4300
Fultonville, NY 12072
FAX: +1 518 853 4533
United States
Website: https://www.perroneaero.com/
E-mail: sales@perroneaero.com
CAGE Code: 49U11
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

13. Plastic Cleaning

CAUTION: CITRUS CLEANERS AND CLEANING AGENTS CONTAINING CHLORINATED

HYDROCARBONS WILL MAR PLASTIC AND CAUSE DAMAGING CHANGES TO
ITS CHEMICAL COMPOSITION. THE USE OF ANY SUCH CLEANING AGENTS
WILL REDUCE THE SERVICE LIFE OF PLASTIC PARTS AND VOID WARRANTY
CLAIMS.

A. Use extreme care when cleaning any plastic surface. Never use abrasive soaps and bleach.
Instead, clean all plastic surfaces with the specified agent shown in Table 4002.

B. Mix the specified agent to the suggested concentration, depending on the strength needed for
Gutierrez
cleaning. Apply the solution directly to the plastic and rub with a clean, lint-free cloth or
melamine foam pad to loosen dirt and debris. Wipe with a fresh, clean, lint-free cloth or rinse
with water and dry with a turkish towel.

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14. Seat Belt Cleaning

CAUTION: B/E AEROSPACE DOES NOT RECOMMEND DRY CLEANING OF THE SEAT
BELT ASSEMBLIES OR WEBBING. DRY CLEANING WILL CAUSE THE
WEBBING TO LOSE SOME OF ITS ABRASION-RESISTANT COATING AND
DECREASE THE SEAT BELT SERVICE LIFE.

A. Metal components and hardware on seat belts can be cleaned with a lint-free cloth moistened
with isopropyl alcohol (Approximately 70% Concentration), with the webbing covered to

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

prevent contact with the isopropyl alcohol.

B. Webbing can be hand washed using a soft brush and mild soap (e.g., liquid dish washing
soap or household laundry detergent), with the metal parts covered to protect them from
contact with the soap.

C. The assemblies must be dried in an area with good air flow and away from sources of heat or
sunlight.

15. Tape/Adhesive Residue Cleaning

CAUTION: DO NOT USE SOLVENTS OTHER THAN ISOPROPYL ALCOHOL OR GRAIN

ALCOHOL (ETHANOL) AS A CLEANER FOR ADHESIVE RESIDUE. SOLVENTS
WILL WEAKEN THE BONDED SURFACES.

Use a soft cloth wet with small amounts of isopropyl alcohol (Approximately 70% Concentration)
to remove adhesive residue (i.e., double-sided tape residue). Once the area is clean and free
from adhesive residue, use a soft, dry, lint-free cloth to completely dry the area.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

16. Ultraleather™ Cleaning

CAUTION: DO NOT USE HEAVY DETERGENTS, CITRUS CLEANERS, OR SOLVENTS FOR

CLEANING ULTRALEATHER™. DO NOT MACHINE WASH THIS MATERIAL.

A. Spot clean with mild soap and water. Air dry or quick dry with warm setting of a hair dryer.
Disinfect with a 5:1 bleach solution. Dry cleanable by conventional methods using commercial
dry cleaning solvents.

B. Use a mild detergent to remove stains from coffee, tea, red wine, liquor, soft drinks, milk,
ketchup, steak sauce, soy sauce, mayonnaise, butter, salad dressing, chocolate, cosmetic
foundation, lipstick, face cream, suntan oil/lotion, shoe polish and urine.
Gutierrez
C. Use a mild cleaning fluid on stains like machine oil and on more stubborn stains when mild
detergent is not enough.

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17. Upholstery Cleaning (For Spots and Small Areas)

Both wool and synthetic fabric seat covers require periodic dry cleaning. See Section 18 in this
page block for detailed cleaning recommendations.

A. Vacuum upholstery thoroughly or brush with a medium stiff bristle upholstery or clothes brush.
Do not pound or beat upholstered covers, as this does not effectively clean the upholstery and
can hasten the wear.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

NOTE: Vigorous rubbing may be required to obtain uniform stain removal and to avoid a
spotty or blotchy appearance after drying.

B. Remove dry or water-borne soil with upholstery shampoo. Dilute the upholstery shampoo as
directed on its container and apply to a small area (approximately one square foot) with a
small, clean brush. Liberal application will assist in loosening deeply imbedded dirt.

C. Oily grease spots are best removed with solvent-type cleaning agents or with
solvent-impregnated powder. Test the material to be cleaned by first applying the cleaning
agent to a small inconspicuous area of the material. Use cleaning agents sparingly, without
saturating fabric, to avoid spotting and damage. Apply the cleaning agent with a soft, clean
cloth and avoid spreading stains by working from the outer edges of the stain toward the
center.

D. After using upholstery shampoo, solvent-type cleaning agents, or solvent-impregnated

powder, roll a clean turkish towel or other absorbent cloth into a cylindrical shape and wipe off
the cleaned area. Rotate the rolled cloth frequently to present a clean section to the fabric
surface.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

18. Wool and Synthetic Fabric Cleaning

B/E Aerospace provides the following information as a guideline for the care and maintenance of
fabric covers. Repeated cleaning of the covers can reduce the flammability retardant
characteristics of the dress cover assembly and, in turn, affect the flammability characteristics of
the cushion-cover system. Some cleaning processes may reduce the flammability protection
more than others. Please follow the fabric manufacturer’s instructions for dress cover fabric
cleaning. The flammability requirements for the dress cover assembly and all other components
of the cushion-cover system are defined by 14CFR25.853 (a) and (c).

A. Flame-Resistant Synthetic Upholstery Fabrics

NOTE: As a rule, synthetic fabrics do not require pretreatment because of the inherent Gutierrez
non-staining characteristics of the fibers.

(1) Laundry machines

Use a laundry machine with a load capacity of approximately 40 pounds. Machines with
larger loading capacities tend to accelerate abrasion of the fabric.

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(2) Detergents

Use only non-ionic detergents.

(3) Fabric preparation for laundering

(a) Cover hook tape with pile tape to avoid fabric damage during laundering.

(b) Turn covers inside out before laundering.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(4) Laundering procedure

NOTE: Load the laundry machine to approximately 33% of rated capacity. Loading
machines higher than 33% may impair cleaning efficiency and accelerate
abrasion of the fabric. Underloading may impair flame retardant properties
because of detergent absorption.

Follow the guidelines in Table 4003 for laundry machine settings:

Table 4003
Laundry Machine Settings
CYCLE TEMPERATURE ADD CYCLE TIME
First Wash 85° F 1 ounce all-in-one 10-15 minutes
non-ionic detergent
Intermediate Rinse 85° F 5-10 minutes
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Second Wash 85°-105° F 0.4 ounce all-in-one 10-15 minutes

non-ionic detergent
Final Rinse 85° F
Drying 131° F maximum Variable; remove promptly when dry to
avoid wrinkling.

Gutierrez

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B. Flame-Resistant Wool and Wool-blend Upholstery Fabrics

(1) Sort fabrics by stain characteristics and pretreat stains as described in Table 4004:

Table 4004
Stain and Pretreatment Methods
TYPE EXAMPLES PRETREATMENT METHOD

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Water soluble Tea, coffee, a. Moisten the stain with water.
red wine, fruit,
urine b. Work the spotting reagent into the stain with a spatula or
tamping brush.

c. Blow steam through the spot.

d. Follow steam with forced air and simultaneous vacuuming.

Protein-type Milk, chocolate, a. Moisten the stain with water.
water soluble blood
b. Work the spotting reagent into the stain with a spatula or
tamping brush.

c. Blow steam through the spot.

d. Follow steam with forced air and simultaneous vacuuming.

Water In-soluble Ink, lipstick, a. Work the spotting reagent into the stain (dry fabric) with a
nail polish, spatula or tamping brush.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

shoe polish
b. Dry clean the fabric before the reagent dries.
Unknown stains CAUTION: USING AN ANIONIC OR ALKALINE REAGENT
CAN IMPAIR THE FLAME-RETARDANT
CHARACTERISTICS OF THE FABRIC AND
ADVERSELY AFFECT CERTIFICATION.

a. Use a commercial, non-ionic stain removal kit that includes

procedures for removing unknown stains.

b. Test the cleaner on a small area for colorfastness before

proceeding.
Gutierrez
(2) Laundry machines:

(a) Use a dry cleaning machine with a load capacity of 20-65 pounds. Machines with
larger loading capacities tend to accelerate fabric abrasion.

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(b) Load machines to about 70% of rated capacity. Loading machines higher than
70% may impair cleaning efficiency and accelerate fabric abrasion. Underloading
may result in impairment of flame retardant properties because of detergent
absorption or excessive shrinkage.

(c) Use a non-ionic dry cleaning detergent.

(d) Although the dry cleaning process is designed to be waterless, Lantal Textiles, a
manufacturer, states that the addition of some water is necessary to reduce the

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

long-term buildup of perspiration salts and sebum, which will cause a reduction in
flame retardancy.

(e) The temperature of the dry cleaning solvent should be 65°-70° F. Maintain this
temperature throughout the dry cleaning process. Higher temperatures can cause
undue shrinkage.

(3) Preparing fabric for dry cleaning:

(a) Cover hook tape with pile tape to avoid fabric damage during dry cleaning.

(b) Turn covers inside out.

(4) Dip-wash / filter-rinse dry cleaning procedures are shown in Table 4005:

Table 4005
Dry Cleaning Procedures
STAGE PROCEDURE
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Dip wash a. Wet the fabric with solvent containing 3-5 grams per liter of detergent.

b. Add water mixed with detergent (see the detergent or manufacturer’s

recommendation) to the cage with a hopper or automatic metering pump.

c. Circulate solvent without filtering for 7-10 minutes.

d. Pump out the solvent and centrifuge the fabric.

Filter rinse a. Add distilled solvent and circulate continuously from the cage to the button trap
to the pump to the filter to the cage for 3-5 minutes.

b. Centrifuge for 2 minutes then dry. Gutierrez

(5) Drying temperature:

Tumble dry flame-retardant wool and wool blend fabrics with a maximum outlet air
temperature of 120° F.

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THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

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INSPECTION/CHECK

1. General

A. Seat assembly attaching hardware requires visual and operational inspection periodically, or
following any incident that may result in the loosening of the attaching hardware. The
frequency of visual and operational inspection of the seat assembly hardware is the
responsibility and at the discretion of the airline.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

B. Visually inspect all new and existing parts before installation or reinstallation on the seat
assembly using a strong light and a 5x to 7x magnifying glass. When inspecting for damage or
corrosion, an inspection mirror must be used to determine the condition of all exposed
surfaces.

C. The following applies to Cover and Cushion Assemblies:

WARNING: TO MAINTAIN THE COVER AND CUSHION ASSEMBLY FLAMMABILITY

PERFORMANCE PER THE REQUIREMENTS IN 14CFR25.853 (a) AND (c)
OVER THE PRODUCT LIFE CYCLE, THE CLEANING (PAGE BLOCK 4000),
INSPECTION/CHECK (PAGE BLOCK 5000) AND REPAIR (PAGE BLOCK
6000) SECTIONS OF THIS CMM MUST BE FOLLOWED.

WARNING: TO MAINTAIN THE FLOTATION CHARACTERISTICS OF THE CUSHION

AND COVERS FOR TSO C72 OVER THE PRODUCT LIFE CYCLE, THE
CLEANING (PAGE BLOCK 4000), INSPECTION/CHECK (PAGE BLOCK
5000) AND REPAIR (PAGE BLOCK 6000) SECTIONS OF THIS CMM MUST
BE FOLLOWED.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

WARNING: IMPLEMENTATION OF THE ABOVE OUTLINED INSPECTION / CHECK

PROCESSES, AND ANY CORRESPONDING CUSHION AND COVER
MAINTENANCE ACTIONS, ARE THE RESPONSIBILITY OF THE AIRLINE.

2. Seat Assembly Serviceability Inspection

Perform the following checks listed in Table 5001 after any significant repair work or disassembly
of the seat assembly. If specific components are not present on your seats, skip those particular
checks. Replace any part that fails to meet the requirements of the check with a serviceable part.
If a defective part is repairable, note the defect and assign that part for repair.

Table 5001
Detailed Inspection Gutierrez

DETAILED INSPECTION (ACCEPT/REJECT EACH ITEM LISTED)

Check for required tags on the seat assembly. If modifications have been made to
the seat per service documentation, check that proper tags and/or entries have been
applied.
Check that all parts are clean and free of cracks, corrosion, deterioration and
obvious signs of damage.

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Table 5001 (Continued)

Detailed Inspection
DETAILED INSPECTION (ACCEPT/REJECT EACH ITEM LISTED)
Check seat belts and seat belt shackles for serviceability, proper installation, and
tightness of attaching hardware. See Paragraph 3 for detailed inspection
procedures.
Check for proper installation and function of the legrest and foot paddle.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Check back assemblies and installations:
Check for proper seat back recline function.
Check for proper installation and function of the hydraulic lock.
Check for missing parts, broken parts and parts not securely attached or
fastened.
Check hardware and metal parts for orientation, tightness, and burrs.
Check the literature pocket.
Check the coat hook.
Check Legrest assemblies and installations:
Check for proper installation and function of the legrest and foot paddle.
Check for proper deployment and stowage of the legrest assembly.
Check for proper installation and function of the gas locks.
Check for smooth rotation of the foot paddle.
Check for missing parts, broken parts and parts not securely attached or
fastened.
Check hardware and metal parts for orientation, tightness, and burrs.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Check legrest assembly for serviceable appearance.

Endbay:
Check ‘drop down’ operation for proper function.
Check hardware and metal parts for proper direction, tightness, and sharp
edges/burrs.
Check paint and finishes for chipping and worn spots. Note the condition of
bonding on parts and assemblies.

Gutierrez

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Table 5001 (Continued)

Detailed Inspection
DETAILED INSPECTION (ACCEPT/REJECT EACH ITEM LISTED)
Check foodtray assemblies:
Check that the foodtray release latch properly presents the table.
Check that the foodtray table deploys and stows properly.
Check the foodtray table top shrouds for nicks, cracks, stains, or burrs.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

NOTE: Burrs, nicks and scratches are defined as material raised above
the normal surface which, if not removed, would prevent
complete and proper mating of parts and sealing surfaces.
Where nicks and scratches allow bare metal to show through
a protective finish, note the defect and assign the part for repair.
Dents or other damage must not impair finish or functional
operation of any part.
Check foodtray table surfaces for serviceable appearance.
Console:
Check video and handsets for function and installation.
Check USB, RJU and PC power outlets for function and installation.
Check mechanical control levers for proper function.
Check cable routings.
Check hardware and metal parts for proper direction, tightness, and sharp
edges/burrs.
Check paint and finishes for chipping and worn spots. Note the condition of
bonding on parts and assemblies.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Bottom Diaphragm:
Check for proper installation.
Check for proper tension. The diaphragm should not have sags or appear
loose.
Check for tears or other damage to the fabric.
Check for part identification.
Baggage Bar:
Check baggage bar for serviceable appearance.
Ensure that baggage bar plugs are installed.
Check all baggage bar hardware for tightness, burrs, and sharp edges.
Gutierrez
Wiring Harnesses, Cables and Electrical Components:
Inspect for chafing and splitting.
Check for loose connections.
Check for cleanliness (No dirt, dust or contamination).

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Table 5001 (Continued)

Detailed Inspection
DETAILED INSPECTION (ACCEPT/REJECT EACH ITEM LISTED)
Electrical Boxes:
Check all SEB hardware and metal surfaces for sharp edges.
Check for proper cable routing.
Check the connectors for proper installation.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Dress Covers:
Check dress covers for cleanliness and serviceability.
Check dress cover labels for number of cleanings.

NOTE: Refer to CLEANING (Page Block 4000) for information on

flammability retardancy as affected by dry cleaning.
Check all dress covers for proper fit and alignment.
Check the rear track fittings and front track studs on legs for secure attachment to
the aircraft floor tracks. Also, check for wear or deformation of these parts.
Check life vest and life vest box assembly for serviceability.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

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3. Seat Belt Detailed Inspection and Limitations

A. Seat belts require visual and operational inspection periodically or when an incident may
indicate potential damage. B/E Aerospace recommends that the seat belt be inspected during
every light check. Inspections should at minimum coincide with the Continued Airworthiness
inspection of the aircraft or at intervals of no greater than one year.

WARNING: THE SEAT BELT MUST BE REPLACED AFTER ANY HIGH LOAD STRESS/
CRASH/IMPACT EVENT THAT COULD CAUSE A LOSS OF STRUCTURAL

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

INTEGRITY OR INABILITY TO PERFORM TO DESIGN.

B. Frayed webbing consists of broken filaments on either the longitudinal (warp) or filler
(transverse) yarns. Broken filaments that make identification of any individual yarn unclean
(from a viewing distance of about eight inches) is excessive fraying. Refer to Figure 5001.

STITCH
PATTERN EDGE OF
LOCATION WEBBING
(EXAMPLE)

FILLER
YARN

WARP YARN
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Figure 5001

C. Seat Belt Checks:

(1) Check that the seat belt webbing is clean and free of dirt, corrosive materials or any
inappropriate substances. For cleaning instructions, refer to instructions in
CLEANING (Page Block 4000).

(2) Check that all seat belt attaching parts are properly secured.

(3) Buckle and unbuckle the seat belt to verify proper operation. Replace the belt if the Gutierrez
operation failed.

(4) Pull the free end of the webbing to check that the belt adjusts smoothly. Replace the belt
if the operation failed.

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(5) Check the seat belt webbing for wear, tears and/or frayed or damaged stitching or
threads or fusing of the web material (Refer to Figure 5001).

WARNING: THE SEAT BELT MUST BE REPLACED WHEN THE WEBBING SHOWS
SIGNS OF EXTENSIVE WEAR, FRAYING, DAMAGED STITCHES OR
THREADS, OR WHEN THE FRAYING IS SUFFICIENT TO CAUSE IMPROPER
OPERATION OF ANY COMPONENT OF THE SEAT BELT. IMMEDIATELY
REPLACE ANY SEAT BELT THAT IS CUT OR WORN ON THE EDGE OF THE

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

WEBBING MATERIAL (REFER TO FIGURE 5001).

(6) Minimal amounts of wear or fraying of the seat belt webbing will allow the webbing to
retain required strength and does not require immediate replacement of the seat belt.
Minimal amounts of fraying can be described as follows, subject to the seat belt
manufacturers specifications:

(a) The fraying is less than 10% of the width of the webbing (but not at either edge)
and less than eight inches in length.

(b) There are less than fifteen broken yarns anywhere other than the edge.

(c) There are less than fifteen torn stitches in a stitch pattern.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

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REPAIR

1. Introduction

This page block contains the repair procedures that can be applied to damaged component parts
of the seat unit to restore them to a serviceable condition.

CAUTION: EXTREME CARE SHOULD BE TAKEN TO PROTECT WIRING AND ELECTRICAL

COMPONENTS DURING ANY REPAIR PROCEDURES. WIRING AND

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

ELECTRICAL COMPONENTS ADJACENT TO REPAIR OPERATIONS SHOULD
BE CAREFULLY DISPLACED OR COVERED. CLEAN ALL WIRING AND
ELECTRICAL COMPONENTS DURING AND AFTER COMPLETION OF REPAIR
WORK.

2. Special Tools, Fixtures, and Equipment

NOTE: Refer to SPECIAL TOOLS, FIXTURES, AND EQUIPMENT (Page Block 9000) for
detailed information.
Table 6001
Suggested Tools and Equipment
NAME SPEC / PART NO. QTY
Brush, Wire 1
Cleaner & Degreaser Loctite®-ODC-Free AR

Cloth, Abrasive Coarse-Grade 1

Cloth, Lint Free AR
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

File, Thread 1
Filler, Catalyzed Polyester Resin AR
Grain Alcohol (Ethanol) N/A AR
Installation Tool, Pop Rivet 1
Isopropyl Alcohol Federal Specification TT-I-735 AR
Naphtha Solvent VARSOL™ or equivalent AR
Needle, Sewing 1
Scissors 1 PR
Sealant AR Gutierrez

Spatula 1

Thread, KEVLAR® AR
(A Registered Trademark of DuPont)
Wool, Steel AR
NOTE: Equivalent substitutes may be used for listed items.

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3. Procedures

Table 6002
Procedure Contents

PARAGRAPH PROCEDURE
A Light Alloy and Steel Components

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Negligible Surface Damage
B Thermoformed Plastic Panels
C Screw Threads
D Removal of Negligible Surface Corrosion
E Upholstery - Fabric
F Seat Belt Repair
G Replacing the Recline Hydraulic Lock and Adjusting Back Upright and
Recline Settings
H Replacing the Legrest Gas Lock
J Replacing the Foot Paddle Gas Lock
K Replacing Mechanical Control Cables and Control Buttons
L Mechanical Control Cable (MCC) Adjustment
M Adjusting Foodtray and HCEB Deployment
N Seat Back Replacement (Equipped with RFID Tag)
P RFID Tag Only Replacement
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

A. Negligible Surface Damage (Light Alloy and Steel Components)

(1) Blend out negligible surface damage using an abrasive cloth.

NOTE: Negligible surface damage is considered to be abrasions and scratches that do

not compromise structural integrity by being confined only to the surface.

(2) Buff the endbay rubstrip (REF) with 180 grit media to remove minor scratches and
abrasions. Examples of 180 grit media are as follow:

(a) Medium grit nonwoven buffing wheel Gutierrez

(b) Medium grit belt sander

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(c) Medium grit dishwashing scouring pad

NOTE: Brush visible surfaces and connecting radius edges with the existing
grain direction (REF Figure 6001) to buff out markings on an endbay
rubstrip (REF).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

ENDBAY RUBSTRIP (REF)

Figure 6001
Brushed Metal Rubstrip Buffing
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(3) If applicable, restore the surface treatment in accordance with local regulations.

B. Negligible Surface Damage (Thermoformed Plastic Panels)

(1) Clean plastic surface with isopropyl alcohol, grain alcohol (ethanol), or an aliphatic
solvent such as mineral spirits or heptane.

CAUTION: LONG-TERM USAGE OF SUCH SOLVENTS CAN DEGRADE THE

PLASTIC.

(2) Fill any surface irregularities with catalyzed polyester resin filler.

NOTE: Catalyze only the amount of filler needed immediately because the material will Gutierrez
begin to harden within five minutes. An automotive body repair surfacing putty
may be used as a filler.

(3) Level filler with a spatula before it hardens. Stipple the filler with a stiff bristle brush
before it hardens to restore surface texture.

(4) After the filler fully hardens (10 to 15 minutes), rub the area lightly with an abrasive cloth
to blend the repair into adjacent areas.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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C. Screw Threads

(1) Slightly rough or burred screw threads may be cleaned up using a thread file, or small
three corner file, on external threads, and a plug tap of correct size for internal threads.

(2) Components having slightly stripped threads may be cleaned up by using a plug tap of
the correct size for internal threads, but threads which cannot be suitably cleaned up to
ensure secure fastening require component replacement with an approved spare.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

D. Removal of Negligible Surface Corrosion

NOTE: Negligible corrosion is generally that which has scarred or eaten away the surface
protective coat and begun to etch the metal. Refer to FAA Advisory Circular 43-4B,
Corrosion Control for Aircraft.

(1) Light alloy components

(a) Remove corrosion from light alloys using an abrasive cloth.

(b) If applicable, restore the surface treatment in accordance with local regulations.

(2) Steel components

(a) Remove corrosion from steel using a coarse grade wire brush, steel wool, or
abrasive cloth.

E. Upholstery - Fabric
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

WARNING: NEVER USE NYLON OR COTTON THREAD FOR REPAIRS. THE CUSHION
ASSEMBLIES USED ON THE MODELS IDENTIFIED IN THIS MANUAL HAVE
BEEN CERTIFIED TO CONFORM TO FAR 25.853 (c). CHANGING EITHER
THE DRESS COVER OR FIRE BLOCKER MATERIALS MAY CAUSE
CUSHIONS TO FAIL THE REQUIREMENTS OF FAR 25.853 (c) AND WILL
EFFECTIVELY VOID THE CUSHION CERTIFICATION.

(1) Discard excessively worn or damaged seat dress covers.

(2) Repair flotation straps and any small cuts and tears using KEVLAR® thread.

F. Seat Belt Repair

Gutierrez
(1) An abrasive cloth can be used to remove minor scratches and nicks on aluminum parts.

(2) Crocus cloth can be used to remove minor scratches and nicks on steel parts.

(3) After any repair, the seat belt must be cleaned. Refer to CLEANING (Page Block 4000).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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G. Replacing the Recline Hydraulic Lock and Adjusting Back Upright and Recline Settings
(Refer to Figure 6002 and Table 6003)

BACK ASSEMBLY (REF)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

SPREADER ASSEMBLY
(REF)

EYEBOLT
(REF) 105

90 100
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

95
110

115

(REF) 110

Figure 6002
Back Recline Hydraulic Lock Procedures

Table 6003
Recline Control Hydraulic Lock Components
ITEM DESCRIPTION ITEM DESCRIPTION Gutierrez

REF Control Cable Assembly 105 Jam Nut

90 Hydraulic Lock 110 Jam Nut
95 Bolt - HEX HD 115 Washer - Nord-Lock
100 Washer - Plastic
NOTE: For specific part information, see IPL FIG 15.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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(1) To remove the hydraulic lock:

(a) Place the seat in the fully upright position to remove tension from the
hydraulic lock (90).

(b) Disconnect the clip on the control cable assembly (REF) from the threaded end of
the hydraulic lock (90).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(c) Remove the bolt (95), plastic washer (100), and jam nut (105) securing the
hydraulic lock (90) to the back assembly (REF). Retain for reuse.

(d) Remove the jam nut (105) and nord-lock washer (115) from the threaded end of
hydraulic lock (90). Retain for reuse.

(e) Remove the hydraulic lock (90) from the eyebolt (REF).

(f) Remove the other nord-lock washer (115) and jam nut (110) from the hydraulic
lock (90). Retain for reuse.

(2) To install the hydraulic lock:

(a) Install the jam nut (110) and nord-lock washer (115) to the hydraulic lock (90).

(b) Install the hydraulic lock (90) to the back assembly and secure with the bolt (95),
plastic washer (100), and jam nut (105).

(c) Install the hydraulic lock (90) onto the eyebolt (REF) and secure with the nord-lock
washer (115) and jam nut (110).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(d) Install the control cable assembly (REF) on the threaded end of the recline
lock (90) and connect the clip.

(e) Test operation by activating the recline button to determine if seat back reclines
smoothly to full recline dimension.

(3) To adjust back upright setting:

(a) Loosen jam nuts (110) used to secure hydraulic lock (90) to the eyebolt (REF).

(b) Position the seat back to desired setting

(Refer to DESCRIPTION AND OPERATION Section for seat recline dimensions). Gutierrez

NOTE: A plum bob (or plummet) can be used to obtain the vertical reference
point from the seat back and a tape measure for the horizontal.

(c) Tighten jam nuts (110).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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(d) Test operation by putting seat back in full upright position and measuring upright
dimension.

NOTE: In the case of recline mechanism failure, disconnect the control cable
assembly (REF) from the hydraulic lock (90) and use the instructions
above to reset the back in the full upright position.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

ADJUSTER RETAINING RING
SLEEVE

Figure 6003
Hydraulic Lock Assembly

(4) To adjust seat back recline setting:

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(a) Place the seat in the fully reclined position.

(b) Remove the retaining ring from the adjuster sleeve on the hydraulic lock (REF).

(c) Rotate the adjuster sleeve to obtain the desired recline setting (Refer to
DESCRIPTION AND OPERATION Section for seat dimensions). Rotate the
adjuster sleeve clockwise to lessen the recline setting, counterclockwise to
increase the recline setting.

(d) Slide the castellated adjuster sleeve into the tab to lock the adjustment into place
and install the retaining ring.

(e) Test operation by putting seat back in full recline position and measuring recline. Gutierrez

NOTE: In the case of recline mechanism failure, disconnect the control cable
assembly (REF) from the hydraulic lock (95) and use the instructions
above to reset the back in the full upright position.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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H. Replacing the Legrest Gas Lock

(Refer to Figure 6004 and Table 6004)

25
20

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

15

45

15 (REF)

40
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

35

35

40
60
30

Figure 6004
Gas Lock Procedures

Table 6004
Gutierrez
Legrest Gas Lock Components
ITEM DESCRIPTION ITEM DESCRIPTION
15 Gas Spring - Lockable 35 Washer - Lock, External Tooth
20 Bolt - HEX HD 40 Nut - Jam
25 Nut - HEX 45 Rod End Assembly - Press
30 Ring - Retaining 60 Valve Release
NOTE: For specific part information, see IPL FIG 3.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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(1) To remove the legrest gas lock:

(a) Remove the valve release (60) from the lockable gas spring (15) by removing the
retaining ring (30).

(b) Remove the bolt (20) and HEX nut (25) securing the lockable gas spring (15) to the
seatpan. Retain the parts for reuse.

(c) Remove the bottom jam nuts (40) and lock washers (35) securing the lockable gas

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

spring (15) to the legrest assembly. Retain nut and washer for reuse.

(d) Remove the rod end assembly (45) from the lockable gas spring (15). Retain for
reuse.

(2) To install the legrest gas lock:

(a) Install the rod end assembly (45) to the lockable gas spring (15).

(b) Install the upper jam nuts (40) and lock washers (35) to the threaded end of the
lockable gas spring (15).

(c) Install the threaded end of the lockable gas spring (15) to legrest assembly, as
shown. Secure with lower lock washers (35) and jam nuts (40).

(d) Install the lockable gas spring (15) to the seatpan with bolt (20) and HEX nut (25).

(e) Install the valve release (60) (with control cable attached) to the lockable gas
spring (15) and secure with the retaining ring (30).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(f) Test operation.

(g) Adjust the valve release (60), as required.

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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J. Replacing the Foot Paddle Gas Lock

(Refer to Figure 6005 and Table 6005)

(REF)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

30

25

35 40

45
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Figure 6005
Foot Paddle Gas Lock Procedure

Table 6005
Foot Paddle Gas Lock Components
ITEM DESCRIPTION ITEM DESCRIPTION
REF Control Cable 35 Pin - Pivot
25 Extension Lock Assembly - Legrest 40 Spacer - Nylon
30 Bolt - HEX HD 45 Ring - Retaining
NOTE: For specific part information, see IPL FIG 4. Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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(1) To remove the foot paddle gas lock:

(a) Disconnect the control cable (REF) from the extension lock assembly (25).

(b) Remove the bolt (30), pivot pin (35), nylon spacer (40), and retaining ring (45)
securing the extension lock assembly (25) to the legrest assembly. Retain the parts
for reuse.

(c) Disassemble the extension lock assembly (25) and replace parts as required.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(2) To install the foot paddle gas lock:

(a) Assemble the extension lock assembly (25).

(b) Install the extension lock assembly (25) to the legrest assembly by installing the
bolt (30), pivot pin (35), nylon spacer (40), and retaining ring (45).

(c) Connect the control cable (REF) to the extension lock assembly (25).

(d) Test operation.

(e) Adjust the extension lock assembly (IPL FIG 4, Item 25), as required. Refer to
DESCRIPTION AND OPERATION Section for dimensions and limits.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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K. Replacing Mechanical Control Cables and Control Buttons

(Refer to Figure 6006 and Table 6006)

NOTE: The procedures to follow have been validated by Collins Aerospace. Any deviation
to the steps as specified could result in unexpected movements of seat control
components contrary to their stated functions, and/or could cause them to not
function properly at all.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

15

30 10

60 5

30
25

30
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

20

(REF IPL FIG 2 - ITEM 15)

(REF IPL FIG 2 - ITEM 10)

(REF IPL FIG 2 - ITEM 5)

Figure 6006
Control Cable Procedures

Table 6006
Control Cable Components
Gutierrez
ITEM DESCRIPTION ITEM DESCRIPTION
REF Control Cable 20 Pin - Seat Control
5 Control Button - Recline 25 Ring - Retaining
10 Control Button - Footrest 30 Spring - Helical, Compression
15 Control Button - Foot Paddle 60 Housing - Seat Control
NOTE: For specific part information, see IPL FIG 23.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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(1) To remove the control cables:

(a) Remove the control button assembly from the console assembly by turning the
locking screws a quarter-turn.

(b) Retain all parts removed during this procedure for reuse.

(c) Identify and tag all the control cables to be removed.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(d) Relieve tension on the control cables (REF IPL FIG 2, Items 5, 10, 15) by returning
component to the normal position.

(e) Remove the control cable from the lock (refer to Paragraphs G, H, and J) and
unroute to the control housing (60).

(f) Disconnect the control cables (REF IPL FIG 2, Items 5, 10, 15) from the control
buttons (5, 10, 15).

(2) To install the control cables:

CAUTION: ATTACH CONTROL CABLE(S) IN THE CORRECT POSITION. CONTROL

CABLES HAVE SPECIFIC LENGTHS, DEPENDING ON FUNCTION.
INCORRECT INSTALLATION WILL PREVENT PROPER OPERATION
AND MAY CAUSE DAMAGE TO SEAT MECHANISMS.

(a) Make sure that affected component is in the normal position.

(b) Route the cable properly through the seat and console and secure with hardware.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Refer to illustrations in IPL Figure 2 for views of cable routing.

(c) Install the control cables (REF IPL FIG 2, Items 5, 10, 15) to the control
buttons (5, 10, 15).

(d) Install the control cable to the hydraulic/gas lock (refer to Paragraphs G, H, and J).

(e) Adjust tension and test for proper operation.

(3) To remove the control buttons:

(a) Remove the control button assembly from the console assembly by turning the
locking screws a quarter-turn. Gutierrez

(b) Retain all parts removed during this procedure for reuse.

(c) Identify and tag all the control cables to be removed.

(d) Relieve tension on the control cables (REF IPL FIG 2, Items 5, 10, 15) by returning
component to the normal position.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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(e) Disconnect the control cables (REF IPL FIG 2, Items 5, 10, 15) from the control
buttons (5, 10, 15).

(f) Remove the control buttons (5, 10, 15) from the control housing (60) by removing
the retaining ring (25), seat control pin (20) and springs (30).

(4) To install the control buttons:

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(a) Install the control buttons (5, 10, 15) onto the control housing (60) by installing the
springs (30), seat control pin (20), and retaining ring (25).

(b) Install the control cables (REF IPL FIG 2, Items 5, 10, 15) to the control
buttons (5, 10, 15) - see Paragraph 2 above.

(c) Test for proper operation.

L. Mechanical Control Cable (MCC) Adjustment

NOTE: The procedures to follow have been validated by Collins Aerospace. Any deviation
to the steps as specified could result in unexpected movements of seat control
components contrary to their stated functions, and/or could cause them to not
function properly at all.

NOTE: The MCC cannot be routed with bends with a radius of one inch (1”) or less. Bend
radius of two to three inches (2” to 3”) is recommended for best operation. Service
loops cannot be used as they will change the trim length of the center cable.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Figure 6007
MCC Bend Radius and Service Loops

U.S. Export Classification: EAR 9E991 25-20-83-4667

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NOTE: If the MCC becomes kinked to the point where there is a crease of the sheathing or
cable jacket, it is no longer serviceable and must be replaced.

INPUT ASSEMBLY
(APPEARANCE VARIES BY
OUTPUT ASSEMBLY MODEL NUMBER)
(APPEARANCE VARIES BY

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

MODEL NUMBER)

CABLE/CONDUIT ASSEMBLY
(LENGTH VARIES BY PART NUMBER)

Figure 6008
MCC Assembly
NOTE: Lubrication of the MCC is unnecessary and not recommended as the MCC has a
self-lubricating liner.

HYDRAULIC LOCK
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

OUTPUT ASSEMBLY OUTPUT SHAFT

RELEASE
PIN

PADDLE

THREADED FERRULE
Gutierrez
JAM NUT
CONTROL
CABLE
HEX ADJUSTER
RETAINER

Figure 6009
Recline Mechanical Control Cable

U.S. Export Classification: EAR 9E991 25-20-83-4667

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(1) Adjusting the Mechanical Controls

(a) Recline Control Cable Adjustment: (Refer to Figure 6009)

1 Connect cable to hydraulic lock output assembly.

2 Set the back to the fully reclined position.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

3 Turn the jam nut counterclockwise away from the HEX adjuster.

4 Turn the HEX adjuster until console has a “firm” button and no initial play is
detected.

.005
GAP
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

RAISED
PROTRUSION CONTROL
ROD TIP

Figure 6010
Adjustment Gap Dimension

CAUTION: IF TOO MUCH FORCE IS APPLIED TO THE LEVER, THE CAST

BALL CAN BE PULLED OFF THE CABLE.
Gutierrez
5 Turn the HEX adjuster as necessary for the paddle to just contact the
hydraulic lock release pin. Back the HEX adjuster off 1/4 to 1/2 turn to create
a small gap.

NOTE: The correct adjustment will leave a gap of approximately 0.005 in.
(0.13 mm) between the raised protrusion of the paddle and the tip of
the control rod. Refer to Figure 6010.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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CAUTION: DO NOT TORQUE THE JAM NUT MORE THAN THE MAXIMUM
TORQUE. TOO MUCH TORQUE ON THE JAM NUT DAMAGES THE
THREADED FERRULE, WHICH IS MADE OF CAST METAL.

6 While holding the HEX adjuster with one wrench, use another wrench to
tighten the jam nut against the HEX adjuster. Torque the jam nut
to 8 IN-LB (0.9 N-m).

7 Actuate the hydraulic lock and bring the seat to the full upright position.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Ensure that the gap between the raised protrusion and the tip of the control
rod is slightly larger than at recline.

NOTE: The button has more “play” than at recline.

(b) Legrest Cable Adjustment:

(Refer to Figure 6011)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Figure 6011
Control Cable Adjustment - Legrest
1 Connect cable to gas lock valve release assembly.

2 Turn the center conduit jam nut counterclockwise away from the HEX
adjuster.

3 Turn the HEX adjuster until console has a “firm” button and no initial play is
detected.
Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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CAUTION: IF TOO MUCH FORCE IS APPLIED TO THE LEVER, THE CAST

BALL CAN BE PULLED OFF THE CABLE.

4 Turn the HEX adjuster as necessary for the paddle to just contact the
hydraulic lock release pin. Back the HEX adjuster off 1/4 to 1/2 turn to create
a small gap. Refer to Figure 6011.

NOTE: The correct adjustment will leave a gap of approximately 0.005 in.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(0.13 mm) between the raised protrusion of the paddle and the tip of
the control rod. Refer to Figure 6010.

CAUTION: DO NOT TORQUE THE JAM NUT MORE THAN THE MAXIMUM
TORQUE. TOO MUCH TORQUE ON THE JAM NUT DAMAGES THE
THREADED FERRULE, WHICH IS MADE OF CAST METAL.

5 While holding the HEX adjuster with one wrench, use another wrench to
tighten the jam nut against the HEX adjuster. Torque the jam nut
to 8 IN-LB (0.9 N-m).

6 Ensure that the gap between the raised protrusion and the tip of the control
rod is slightly larger than at extension.

(c) Foot Paddle Cable Adjustment:

(Refer to Figure 6012)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Figure 6012 Gutierrez

Control Cable Adjustment - Foot Paddle
1 Connect cable to gas lock valve release assembly.

2 Turn the center conduit jam nut counterclockwise away from the HEX
adjuster.

3 Turn the HEX adjuster until console has a “firm” button and no initial play is
detected.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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CAUTION: IF TOO MUCH FORCE IS APPLIED TO THE LEVER, THE CAST

BALL CAN BE PULLED OFF THE CABLE.

4 Turn the HEX adjuster as necessary for the paddle to just contact the
hydraulic lock release pin. Back the HEX adjuster off 1/4 to 1/2 turn to create
a small gap. Refer to Figure 6012.

NOTE: The correct adjustment will leave a gap of approximately 0.005 in.
(0.13 mm) between the raised protrusion of the paddle and the tip of

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

the control rod. Refer to Figure 6010.

CAUTION: DO NOT TORQUE THE JAM NUT MORE THAN THE MAXIMUM
TORQUE. TOO MUCH TORQUE ON THE JAM NUT DAMAGES THE
THREADED FERRULE, WHICH IS MADE OF CAST METAL.

5 While holding the HEX adjuster with one wrench, use another wrench to
tighten the jam nut against the HEX adjuster. Torque the jam nut
to 8 IN-LB (0.9 N-m).

6 Ensure that the gap between the raised protrusion and the tip of the control
rod is slightly larger than at extension.

M. Adjusting Foodtray and HCEB Deployment

(1) To adjust the tension of the foodtray deployment and HCEB cord reels, refer to
SL-16-051 “Adjust MiQ™ Foodtray and HCEB Deployment / Generic / All” added as an
attachment to this CMM.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

N. Seat Back Replacement (Equipped With RFID Tag)

NOTE: Refer to DESCRIPTION AND OPERATION Section, for additional RFID Tag
details.

(1) Scan old RFID tag and store the Birth/ID information.

(2) Remove and replace back assembly. Refer to DISASSEMBLY (Page Block 3000) and
ASSEMBLY (Page Block 7000) for details.

(3) Clean RFID tag mounting surface using isopropyl alcohol (or equivalent) and wipe dry
with a lint free cloth.
Gutierrez
(4) Install 3M™ 425 Aluminum Foil tape onto the back substrate. Install pressure sensitive
RFID tag onto the aluminum tape. Locate approximately as shown in the DESCRIPTION
AND OPERATION Section of this CMM.

(5) Write the old tag Birth / ID information onto the new tag.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

P. RFID Tag Only Replacement

NOTE: Refer to DESCRIPTION AND OPERATION Section, for additional RFID Tag
details.

(1) Scan old RFID tag and store the Birth/ID information.

(2) Remove old tag and metal tape.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(3) Clean off any excess adhesive using isopropyl alcohol (or equivalent) and wipe dry
with a lint free cloth.

(4) Install 3M™ 425 Aluminum Foil tape onto the back substrate. Install pressure sensitive
RFID tag onto the aluminum tape. Locate approximately as shown in the DESCRIPTION
AND OPERATION Section of this CMM.

(5) Write the old tag Birth / ID information onto the new tag.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
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ASSEMBLY

1. General

A. Seat assembly attaching hardware requires visual and operational inspection periodically, or
following any incident that may result in the loosening of the attaching hardware. The
frequency of visual and operational inspection of the seat assembly hardware is the
responsibility and at the discretion of the airline.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

WARNING: BE SURE TO TIGHTEN ALL SCREWS, BOLTS AND NUTS TO THE
CORRECT TORQUE VALUE. IF YOU DO NOT USE THE CORRECT TORQUE
VALUE, THE SEAT OR PARTS OF THE SEAT COULD BECOME LOOSE.
THIS COULD CAUSE DAMAGE OR INJURY. IF THE TORQUE VALUE IS
NOT SHOWN, USE THE TORQUE VALUES GIVEN IN TABLE 8001 IN THE
FITS AND CLEARANCES (PAGE BLOCK 8000). WHEN YOU TIGHTEN A
NUT AND BOLT THAT ARE USED TOGETHER, MEASURE THE TORQUE
VALUE ON THE NUT. IF YOU CANNOT GET ACCESS TO THE NUT OR A
NUT IS NOT USED, MEASURE THE TORQUE ON THE BOLT.

NOTE: Cable ties (nylon straps) used to secure parts and assemblies can be cut and
removed to allow performance of service and maintenance, and at completion
must be replaced by the equivalent device in the same manner per specifications.

NOTE: SCHEMATIC AND WIRING DIAGRAMS (Page Block 2000) contains detailed
guidance for installing electrical components and harnesses. IPL Figure 18
contains a complete listing of those components for parts ordering.

B. When assembling the seat, always replace attaching parts (cotter pins, screws, washers,
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

nuts, grommets, cable holders, etc.) with new parts. Replacing these low-cost items helps
decrease maintenance that will be necessary if these items fail. Before assembly, inspect all
parts for wear and/or damage that could cause failure of the seat assembly or any of its
component assemblies.

C. Loctite® products or equivalent are required for seat assembly.

D. Unless instructions for individual pieces of hardware specify otherwise, use the following
guidelines per manufacturer‘s instructions:

For threaded hardware used on plastic components (for example; injection molded w/ inserts,
machined threads in plastics, etc.) apply Loctite®-454 cyanoacrylate based adhesive to ALL Gutierrez
hardware that is installed without a threadlocking element (for example, lock patch, locking
helicoil insert, etc.). Apply one drop (.05 mL) per square inch of engaged threads. Excessive
application may result in an inseparable assembly.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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CAUTION: PLASTIC COMPONENTS MAY DEGRADE AND FAIL WITH CONTACT FROM
ANAEROBIC BASED THREAD LOCKING ADHESIVES (FOR EXAMPLE,
LOCTITE®-222, -242, -243, -262, -263). AVOID EXCESSIVE APPLICATION
THAT MAY CAUSE SPILLAGE ON PLASTICS, OR USE A CYANOACRYLATE
BASED THREAD LOCKER (FOR EXAMPLE, LOCTITE®-454) THAT IS SAFE
FOR PLASTICS. STICK FORM LOCTITE® (FOR EXAMPLE, LOCTITE®-2X8)
CAN ALSO BE USED TO AVOID SPILLAGE ON PLASTIC PARTS.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(1) For hardware with thread size 8 and higher, apply Loctite®-243 adhesive to ALL
non-locking hardware and ALL hardware used in joints with no locking element.

(2) For hardware with thread size less than 8, apply Loctite®-222 adhesive and
Loctite®-7649 activator to all non-locking hardware and all hardware used in joints
with no locking element.

2. Installation of Seat Assembly on Aircraft

CAUTION: AVOID HANDLING / MANEUVERING / LIFTING SEAT ASSEMBLIES BY THE

SEAT BACKS. DAMAGE MAY OCCUR TO THE SEAT BACK ASSEMBLY SAFETY
BREAK OVER MECHANISM IF EXCESS PRESSURE IS APPLIED IN THE
FORWARD BREAK OVER DIRECTION. THIS WILL RESULT IN A FORWARD
COLLAPSE OF THE SEAT BACK ASSEMBLY, ITS INABILITY TO STAY
UPRIGHT, AND REQUIRE REPLACEMENT OF THE SEAT BACK ASSEMBLY
FRAME QUADRANTS.

Lifting points for seats for installation and transportation to be from both outermost seat belts
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(doubles). An appropriate torso shaped lifting device shall be properly positioned in the seat and
strapped in with seat belts prior to lifting seat. Seats should be lifted by the torso lifting devices
only.

A. Clean floor tracks, studs, and track fittings when seats are moved. This will prevent unwanted
wear on fastener assemblies.

B. To attach the seat assemblies to the aircraft, put the track studs and track fittings at the
bottom of the leg assemblies into matching notches in the floor track.

C. Slide the seat assembly forward or aft approximately one-half inch until the locking
mechanism on the track fitting can be pressed into an access hole.

CAUTION: USING TOO MUCH FORCE TO TIGHTEN THE ANTI-RATTLE DEVICE COULD Gutierrez
DAMAGE IT.

D. To lock the front track fitting into position, raise the front of the leg to ensure the top of the stud
is bearing against the underside of the track lips. Use a 9/16" open end wrench to tighten the
anti-rattle nut until it is flush with the top of the seat track plus 1/4 turn.

E. To lock the track fitting into position, use a 3/16" HEX head wrench to tighten the lock screw to
60 ±10 IN-LB. The lock screw should be flush with the track fitting body when engaged.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

3. Assembly Procedures

A. Assembly of the Leg

(Refer to IPL FIG 45)
(1) Attach the doublers (55) to the machined leg (70) by installing the bolt (60) and
nut (65).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

NOTE: Torque the bolt (60) and nut (65) to 96 ±24 IN-LB.

(2) Attach the track fitting (35) to the machined leg (70) with the bolt (40),
spacers (45), and nut (50).

NOTE: Torque the bolt (40) and nut (50) to 110 ±24 IN-LB.

(3) Attach the stud (25) and anti-rattle nuts (30) to machined leg (70).

NOTE: Apply Loctite®-270 to the internal threads on the leading edge of machined
leg (70). Loctite® cures fully in 24 hours. Loctite®-263 can be used as an
alternate.

NOTE: Torque the stud (25) to 180 ±10 IN-LB.

(4) Attach the leg assembly (REF) to the beams (REF IPL FIG 43, Item 55) by tightening the
bolts (5, 15) and nuts (10, 20).

NOTE: Torque the bolt (5) to 84-120 IN-LB.

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

NOTE: Torque the bolt (15) to 240-300 IN-LB.

B. Assembly of the Spreader

(Refer to IPL FIG 44)
(1) To assemble the spreader assemblies (30, 30B), install the flanged bushing (35) and
machined shaft roller (40, 40A) to the spreader (45, 45B).

(2) Attach the recline lock eyebolt (20) to the spreader assembly (30B) by installing the
retaining ring (25).

(3) Attach the articulation roller (5) to the roller machined shaft (40, 40A) by installing the
screw (10) and washer (15). Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
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C. Assembly of the Frame

(Refer to IPL FIG 43)
(1) Install the lock spreader assemblies (30, 35) by installing the bolts (40, 45) and
nuts (50), and sliding the lock spreader assemblies (30, 35) of the beams (55).

NOTE: Torque the bolts (40, 45) to 75 ±5 IN-LB.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(2) Install the leg assemblies (25) onto the beams (55). Refer to Paragraph A for installation
instructions.

(3) Slide the non-lock spreader assemblies (5, 10) onto the beams (55) and install the
bolts (15) and nuts (20).

NOTE: Torque the bolts (15) to 75 ±5 IN-LB.

D. Installation of the Baggage Bar

(Refer to IPL FIG 42)
(1) Install the baggage bar plugs (50) onto the standard baggage bar tube (5) and canted
baggage bar tube (25).

(2) If removed, install the baggage bar doubler (-45).

(3) Install the canted baggage bar tube (25) by installing the screw (30), washer (35), and
set screw (40).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(4) Install the standard baggage bar tube (5) by installing the screw (10), washer (15), and
set screw (20).

E. Installation of the Electrical Raceway

(Refer to IPL FIG 41)
(1) Attach the leg IFE shroud console (70) and cable protection shroud (75) by attach with
3M™ double sided tape (80).

(2) Attach the leg isolator shroud IFE (60) with the tiedown straps (65).

(3) Attach the pancake raceway (15, 30, 45) to the beams (REF) with the tiedown
straps (20, 35, 50) and attach the 3M™ double sided tapes (-25, 40, -55). Gutierrez

(4) Attach the spreader cover (5) with the tiedown straps (10).

F. Installation of the Shroud

(Refer to IPL FIG 40)
(1) If removed, attach the 3M™ double sided tapes (-120) to the disconnect leg isolator (90).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
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F. Installation of the Shroud (Continued)

(Refer to IPL FIG 40)
(2) If removed, attach the edging grommet (115) onto the disconnect bracket assembly (85).

NOTE: Attach the edging grommet (115) with Loctite®-454.

(3) Install the disconnect bracket assembly (85) and disconnect leg isolator (90) by installing
the bolts (95), spacers (100), and nuts (105).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(4) To assemble the disconnect shroud assembly (65), install the disconnect shroud (70)
turn the studs (75) a quarter-turn in clockwise direction to engage them into the
receptacles (110).

(5) To assemble the door assembly (30), install the IFE shroud face plate (35), turn the
studs (40) a quarter-turn in clockwise direction.

(6) To assemble the mount plates/shroud assembly (5) install the ISPS shroud (25) to the
door assembly (30).

(7) If removed, attach the edging grommet (20) onto the mount plates/shroud assembly (5).

NOTE: Attach the edging grommet (20) with Loctite®-454.

(8) Install the mount plates/shroud assembly (5) with the straps (10) and 3M™ double sided
tapes (-15).

G. Assembly of the Endbay Arm Frame - Outer

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(Refer to IPL FIG 39)

(1) Install the support hinge (85) onto the endbay arm frame assembly (100B) by installing
the screws (90, 95).

(2) Install the rail (75, 75A) onto the endbay arm frame assembly (100) by installing the
screws (80).

(3) To assemble the table mount assembly (55), install the grommet bumper (65) onto the
table mount block (70).

(4) Install the table mount assembly (55) by installing the screws (60).
Gutierrez
NOTE: Apply Loctite®-243 to threads of the screws (60).

(5) Install the release latch (30) onto the endbay arm frame assembly (100) by installing the
screw (35), spring (40), bushing (45), and nut (50).

(6) Install the pulley (20) by installing the bolt (25).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

G. Assembly of the Endbay Arm Frame - Outer (Continued)

(Refer to IPL FIG 39)
(7) Install the latch cables (5, 5A) by installing the tiedown straps (10) and retaining
ring (15).

H. Assembly of the Table Latch

(Refer to IPL FIG 38)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(1) Install the cable adapter (20) onto the table latch housing (35) by installing the
screw (25) and nut (30).

NOTE: Torque the screw (25) to 15 ±4 IN-LB.

(2) Install the spring (15).

(3) Install the table release latch (5) onto the table latch housing (35) by installing the dowel
pin (10).

J. Assembly of the Endbay Wall Arm - Special

(Refer to IPL FIG 37)
(1) Install the grommet bumper (70) onto the endbay special wall assembly (55).

WARNING: USE EXTREME CAUTION WHEN CONNECTING OR DISCONNECTING THE

BOLT (65) OR INJURY CAN RESULT. THIS BOLT (65) ATTACHES THE
CABLE OF THE SPRING REEL AND IS UNDER HIGH TENSION!
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(2) With a tray table installed, attach the foodtray latch cable (REF IPL FIG 39, Item 5) to the
mechanical reel (50) (cord reel) to the outer endbay special wall arm assembly (75) by
installing the bolt (65).

(3) Put the foodtray latch cable (REF IPL FIG 39, Item 5) through the pulley (REF IPL
FIG 39, Item 20) in outer endbay special wall arm assembly (75) and wind reel to
remove slack.

(4) Attach the mechanical reel (50) to cord reel access door assembly (20) by installing the
screw (30) and reel adjuster (45).

NOTE: Refer to SL-16-051, added as an attachment to this CMM for reel adjustment.
Gutierrez
(5) Attach the cord reel access door assembly (20) to the endbay special wall assembly (55)
by installing the screws (25).

(6) Attach the endbay special wall assembly (55) to the outer endbay special wall arm
assembly (75) by installing the screws (60).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

J. Assembly of the Endbay Wall Arm - Special (Continued)

(Refer to IPL FIG 37)
(7) Connect the foodtray latch cable (REF IPL FIG 39, Item 5) to table latch assembly (5)
by installing the retaining ring (15).

(8) Install the table latch assembly (5) by installing the screws (10).

(9) Loosen the screw (30) and clock reel using reel adjuster (45) until tray deploys at 5.5

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

inches ±1 inch above the top surface of the assembly. Secure reel retention wheel with
screw (30). The allowable deployment range after inspection and at the customer is 5.25
inches ±1.75 inches.

K. Assembly of the Wall Endbay - Special

(Refer to IPL FIG 36)
(1) To assemble the endbay wall assembly (80):

(a) Install the baggage bar (125) by installing the screw (130).

(b) Install the hinge cover (115) by installing the screw (120).

(c) To assemble the hinge assembly (85), install the machined hinge (95) onto the
hinge base (110) by installing the hinge pin (100) and hinge spring (105).

NOTE: Assemble hinge pin (100) into clearance hole of hinge base (110), thru
machined hinge (95) and hinge spring (105), and press fit into the far
side of hinge base (110) flush at the end.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(d) Install the hinge assemblies (85) onto the endbay wall arm assembly (135) by
installing the screws (90).

(2) If removed, attach the 3M™ adhesive transfer tape (-75).

(3) Install the bonded shroud assembly (55) and wall side shroud (65) onto the endbay wall
assembly (80) by installing the snap rivets (60, 70).

NOTE: Attach the edge of the endbay wall assembly (80) with the structural adhesive
Loctite®-3412.

NOTE: Refer to SL-21-015 added as an attachment to this CMM for replacement of

endbay shroud clips. Gutierrez

(4) Install the wall PAX aft shroud (45) by installing the snap rivets (50).

(5) Install the wall PAX side shroud (35) by installing the snap rivets (40).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

K. Assembly of the Wall Endbay - Special (Continued)

(Refer to IPL FIG 36)
(6) To assemble the armcap assembly (5), install the armcap closeout (15) onto the armcap
subassembly (30) by installing the snap rivets (20) and the 3M™ adhesive transfer
tape (-25).

(7) Install the armcap assembly (5) by installing the screws (10).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

L. Assembly of the Frame - Endbay Arm
(Refer to IPL FIG 35)
(1) Attach the grommet bumper (105) to the inner endbay arm frame assembly (55).

WARNING: USE EXTREME CAUTION WHEN CONNECTING OR DISCONNECTING THE

BOLT (100) OR INJURY CAN RESULT. THIS BOLT (100) ATTACHES THE
CABLE OF THE SPRING REEL AND IS UNDER HIGH TENSION!

(2) With a tray table installed, attach the foodtray latch cable (REF IPL FIG 39, Item 5) to
mechanical reel (50) (Cord Reel) to outer endbay arm frame assembly (110) by installing
the bolt (100).

(3) Put the foodtray latch cable (REF IPL FIG 39, Item 5) through the pulley (REF IPL
FIG 39, Item 20) in outer endbay arm frame assembly (110) and wind reel to remove
slack.

(4) Attach the mechanical reel (50) to cord reel access door assembly (20) by installing the
screw (30) and reel adjuster (45).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

NOTE: Refer to SL-16-051 added as an attachment to this CMM for reel adjustment.

(5) Attach the cord reel access door assembly (20) to the inner endbay arm frame
assembly (55) by installing the screws (25).

(6) To assemble the inner endbay arm frame (55):

(a) Install the grommet bumpers (85) onto the stop block (90).

(b) Install the stop block assembly (75) onto the endbay arm frame assembly (95) by
installing the screws (80).

(c) Install the endbay arm handhold (65) by installing the screws (70). Gutierrez

(7) Install the inner endbay arm frame assembly (55) onto the outer endbay arm frame
assembly (110) by installing the screws (60).

(8) Connect the foodtray latch cable (REF IPL FIG 39, Item 5) to table latch assembly (5) by
installing the retaining ring (15).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

L. Assembly of the Frame - Endbay Arm (Continued)

(Refer to IPL FIG 35)
(9) Install the table latch assembly (5) by installing the screws (10).

(10) Loosen the screw (30) and clock reel using reel adjuster (45) until tray deploys at
5.5 ±1 inch above the top surface of the assembly. Secure reel retention wheel with the
screw (30). The allowable deployment range after inspection and at the customer is
5.25 ±1.75 inches.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

M. Assembly of the Endbay Arm - INBD
(Refer to IPL FIG 34)
(1) To assemble the armcap hinge assemblies (125), install the machined hinge (135) onto
the hinge base (150) by installing the pin (140) and spring (145).

NOTE: Assemble the pin (140) into clearance hole of the hinge base (150), thru the
machined hinge (135), pin (140), and spring (145), and press fit into the far
side of the hinge base (150) flush at the end.

(2) Install the armcap hinge assemblies (125) and hinge cover (155) onto the endbay arm
frame assembly (160) by installing the screws (130).

(3) Install the carriage arm mount plates (20, 50, 80, 110) by installing the
bolts (25, 55, 85, 115) and washers (30, 60, 90, 120).

NOTE: Torque the bolts (25, 55, 85, 115) to 60 ±5 IN-LB.

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(4) Install the sliders (5, 35, 65, 95) to the carriage arm mount plates (20, 50, 80, 110)
by installing the screws (10, 40, 70, 100) and washers (15, 45, 75, 105).

NOTE: Torque the screws (10, 40, 70, 100) to 45 ±5 IN-LB.

N. Assembly of the Bowtie Assembly - Endbay Arm

(Refer to IPL FIG 33)
(1) To assemble the bowtie endbay assembly (45):

(a) To assemble the bowtie endbay assembly (115):

1 Install the cord guide (140) by installing the rivets (145). Gutierrez

2 Install the adjuster restrain bracket (130) by installing the screws (135).

3 Install the stew step strut (120) by installing the screws (125).

(b) Install the rollon rails (100, 105) to the bowtie endbay assembly (115) by installing
the screws (110).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

N. Assembly of the Bowtie Assembly - Endbay Arm (Continued)

(Refer to IPL FIG 33)
(c) To assemble the pivot assembly (50):

1 Install the bearings (90) to the endbay arm pivot (95).

2 Install the handicap latches (70, 80) to the endbay arm pivot (95) by installing
the screws (75, 85).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

NOTE: Torque the screws (75, 85) to 26 ±2 IN-LB.

(d) Install the pivot assembly (50) to the bowtie endbay assembly (115) by installing
the screws (55), latch caps (60), and spring (65).

(2) Attach the reel adjuster (35) by installing the screw (40).

(3) Install the reel (20) to the bowtie endbay assembly (45) by installing the screw (25) and
washer (30).

NOTE: Refer to SL-16-051, added as an attachment to this CMM for reel adjustment.

WARNING: USE EXTREME CAUTION WHEN CONNECTING OR DISCONNECTING THE

SCREW (10) OR INJURY CAN RESULT. THIS SCREW (10) ATTACHES THE
CABLE OF THE SPRING REEL AND IS UNDER HIGH TENSION!

(4) Slide the INBD endbay arm assembly (5) onto the bowtie endbay assembly (45) and
attach the spring reel cable with the screw (10) and spacer (15).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

P. Assembly of the Endbay Bracket - INBD

(Refer to IPL FIG 32)
(1) To assemble the endbay arm bowtie assembly (40), refer to Paragraph N.

(2) Route and install the endbay control cable (15) and cable ferrule (20) to the endbay side
bracket (35) with the retaining rings (25) and tiedown straps (-30).

(3) Install the handicap latch (5) by installing the screw (10).

NOTE: Handicap latch (5) to be installed after control cable (15).

Gutierrez
Q. Assembly of the Endbay Arm Button
(Refer to IPL FIG 31)
(1) Install the pulley (25) onto the button housing (35) by installing the screw (30).

(2) Install the endbay arm button (5) onto the button housing (35) by installing the button
pin (10), retaining rings (15), and spring (20).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

R. Assembly of the IUL Endbay

(Refer to IPL FIG 30)
(1) If removed, attach the 3M™ adhesive transfer tape (155) and 3M™ double sided
tape (160) onto the bonded shroud assemblies (50, 50A, 60, 60A).

(2) Install the PAX side endbay shrouds (140, 140A) and endbay foam (145, 145A) onto the
INBD endbay bracket assemblies (165, 165A) by installing the snap rivets (150, 150A).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(3) Install the endbay shroud assemblies (125, 125A) onto the INBD endbay bracket
assemblies (165, 165A) by installing the snap rivets (130, 130A) and screws (135).

(4) Install the endbay arm button assemblies (105, 105A) by installing the
screws (110, 110A, 120) and vinyl cap (-115) and connecting the control cable (REF IPL
FIG 32, Item 5).

(5) Install the endbay aft rubstrips (95, 95A) by installing the screws (100).

(6) To assemble the rubstrip assemblies (70, 70A), attach the endbay front
rubstrips (80, 80A) to the endbay forward rubstrips (90, 90A) by installing the
screws (85).

(7) Install the rubstrip assemblies (70, 70A) by installing the screws (75).

(8) Install the bonded shroud assemblies (60, 60A) by installing the screws (65).

NOTE: Refer to SL-21-015 added as an attachment to this CMM for replacement of

endbay shroud clips.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(9) Install the bonded shroud assemblies (50, 50A) by installing the snap rivets (55).

NOTE: Refer to SL-21-015 added as an attachment to this CMM for replacement of

endbay shroud clips.

(10) To assemble the armcap assemblies (20, 20A), attach the armcap closeouts (30, 30A)
to the armcap subassemblies (45, 45A) by installing the snap rivets (35) and 3M™
adhesive transfer tape (-40).

NOTE: Attach 3M™ adhesive transfer tape (-40) on the armcap

subassemblies (45, 45A), before installing the armcap closeouts (30, 30A).

(11) Install the armcap assemblies (20, 20A) by installing the screws (25). Gutierrez

(12) Install the rear access EPL (5) and front access EPL (10) by installing the
screws (15).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
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S. Installation of the Endbay

(Refer to IPL FIG 29)
(1) Carefully align the endbay assemblies (5, -10) onto the frame assembly (REF).

(2) Attach the endbay assemblies (5, -10) by installing the bolts (15).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

T. Assembly of the Foodtray
(Refer to IPL FIG 28)
(1) Install the IGUS carriages (160, 165) to the foodtray main leaf (170).

(2) Install the rails (150) to the foodtray main leaf (170) by installing the screws (155).

(3) To assemble the foodtray assembly arm linkage (100):

(a) Attach the bearings (140) onto the foodtray paddle (145).

(b) Install the bumper tray table (130) onto the foodtray paddle (145) by installing the
screws (135).

(c) Install the tray table strut (110) and pivot link (120) onto the foodtray
paddle (140) by installing the dowel pins (115, 125).

NOTE: Refer to SL-18-017, for more details on Loctite® information.

(4) Install the foodtray assembly arm linkage (100) by installing the screws (105).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(5) Install the door cover shroud (90) by installing the snap rivets (95).

(6) To assemble the closeout assembly (75), install the bearing (-80) into the foodtray
closeout (-85).

(7) Install the rotary damper (70) to the closeout assembly (75).

(8) To assemble the foodtray dampener assembly (50), install the bearing (-60) into the
dampener housing (65).

(9) Install the foodtray dampener assembly (50) by installing the bolts (55).

(10) Install the foodtray forward stop (40) by installing the screws (45). Gutierrez

(11) Install the socket drive shoulder post (30) and nut (60).

(12) Install the latch bracket (20) by installing the screws (25).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
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T. Assembly of the Foodtray (Continued)

(Refer to IPL FIG 28)
(13) Attach the foodtray leaf assembly (5) to the foodtray main leaf (170) by installing the
hinge pins (15) and hinges (10).

NOTE: Cover the head of hinge pins (15) with silicone sealant P/N AD-RTVR-T.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

U. Installation of the Foodtray
(Refer to IPL FIG 27)
(1) Align the foodtray assembly (5) onto the endbay assembly (REF IPL FIG 29,
Items 5, -10).

(2) Attach the foodtray assembly (5) by installing the screws (10).

V. Assembly of the Console Structure - Non-Video

(Refer to IPL FIG 26)
(1) To assemble the bracket assembly (120), install the clip nut (-125) to the trim bracket PC
power (-130).

(2) Attach the hinge support (105) to the bracket assembly (120) by installing the
bolts (115) and screw (110).

(3) Install the center brace (95) by installing the bolts (100).

(4) Attach the console side panels (65, 80) by installing the screws (70, 75, 85, 90).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(5) To assemble the life vest bracket assemblies (25, 45), install the clip nuts (35, 55) to the
life vest bracket attachments (40, 60).

(6) Install the life vest bracket assemblies (25, 45) by installing the screws (30, 50).

(7) Install the cocktail table (15) by installing the screws (20).

(8) Install the life vest box assembly (5) by installing the screws (10).

W. Assembly of the Front Trim

(Refer to IPL FIG 25) Gutierrez
(1) Install the bottle bucket (40), front trim bezel (45), and trim bezel (50) to the life vest top
shroud panel (5).

(2) To assemble the front trim assembly (20), install the latch striker (-30) by installing the
retaining ring (-35).

(3) Install the front trim assembly (20) by installing the screws (25).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
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W. Assembly of the Front Trim (Continued)

(Refer to IPL FIG 25)
(4) Install the life vest top shroud panel (5) by installing the screws (10) and clip nuts (15).

X. Assembly of the Pocket

(Refer to IPL FIG 24)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(1) Attach the FWD pocket panels (55, 65) onto the aft pocket panel (75) with the
snap rivets (60, -70).

(2) Attach the lower pocket panels (35, 45) with the snap rivets (40, -50).

(3) Attach the pocket shroud panel (25) with the snap rivets (30).

(4) Attach the side pocket panels (5, 15) with the snap rivets (10, -20).

Y. Assembly of the Seat Control Button

(Refer to IPL FIG 23)
(1) To assemble the retainer assemblies (35), install the retaining clip (45) onto the RJU and
RJM bezel (55) by installing the screw (50).

(2) Attach the retainer assemblies (35) to the seat control housing (60) by installing the
screws (40).

(3) Install the helical springs (30) into the control buttons (5, 10, 15).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(4) Install the control buttons (5, 10, 15) onto the seat control housing (60) by installing the
seat control pin (20) and retaining ring (25).

Z. Assembly of the Cocktail Table

(Refer to IPL FIG 22)
(1) Install the snap rivet (40) onto the cocktail table assembly (45).

(2) Install the striker (25) onto the cocktail table assembly (45) by installing the rivets (30)
and vinyl caps (35).

NOTE: Attach vinyl caps (35) with Loctite®-454. Gutierrez

(3) Install the magnetic ring (15) by installing the screw (20).

(4) Install the carriage and rail (5) onto the cocktail table assembly (45) by installing the
screws (10).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

AA. Assembly of the Center Console

(Refer to IPL FIG 21)
(1) Install the center console foam (-290) and 3M™ adhesive transfer tape (295) onto the
console structure assembly (300).

(2) Install the front trim assembly (275) by installing the screws (280, 285).

(3) To assemble the front bottom bezel assembly (250), align the trim bezels (-260, -265)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

and install the screws (270).

(4) Install the front bottom bezel assembly (250) by installing the screws (255).

(5) To assemble the life vest box door assembly (225):

(a) To assemble the latch assembly (235), attach the life vest pull strap (240) to the
dual pawl assembly (-245) by wrapping pull strap around the slot and engaging
hook and loop securely.

(b) Attach the latch assembly (235) by installing the captive screws (REF).

(6) Install the life vest box door assembly (225) by installing the screws (230).

(7) Install the pocket assembly (210) by installing the bolts (215) and snap rivets (220).

(8) Install the articulating hinge assemblies (200) by installing the screws (205).

(9) Install the side shrouds (170, 185) by installing the snap rivets (175, 180, -190, -195).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(10) Install the button assemblies (160, 165) and turn the retainers a quarter-turn, ensuring
they are firmly engaged.

(11) To assemble the rear trim assembly (115), install the support bracket (125) and the rear
trim bezels (135, 145) onto the rear panel (155) by installing the screws (130, -140, 150).

(12) Align the rear trim assembly (115) on the console structure assembly (300) and install
the screws (120).

(13) Install the rear trim bezel (105) by installing the screws (110).

(14) Install the bumper bar bracket (90) by installing the screws (95). Install the bumper
grommet (100). Gutierrez

(15) Install the cocktail table assembly (80) by installing the screws (85).

(16) To assemble the fixed cocktail table assembly (45), install the body (65) to the fixed
cocktail table assembly (75) by installing the screws (70).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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AA. Assembly of the Center Console (Continued)

(Refer to IPL FIG 21)
(17) Install the fixed cocktail table assembly (45) by installing the screws (50, 55) and hinged
covers (60).

NOTE: Deploy the sliding cocktail table assembly (80) to install the screws (50)
located at the front of the fixed cocktail table assembly (45).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(18) To assemble the armcap assemblies (5):

(a) Install the bumpers (35).

NOTE: Attach the bumpers (35) with Loctite®-454.

(b) Install the armcap trim (25) onto the overmold armcap assembly (40) by installing
the bolts (30).

(c) Install the armcap closeout (15) onto the overmold armcap assembly (40) by
installing the snap rivets (20).

(19) Install the armcap assemblies (5) by installing the screws (10).

AB. Installation of the Center Console Assembly and Console Plug

(Refer to IPL FIG 20)
(1) Align the center console assembly (5) onto the spreader assemblies.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(2) Attach the center console assembly (5) to the frame assembly (REF) by installing the
bolts (10) and dome plugs (15).

(3) Attach the rear trim bezel (REF IPL FIG 21, Item 105) by installing the screws
(REF IPL FIG 21, Item 110). Attach the rear trim assembly (REF IPL FIG 21, Item 115)
by installing the screws (REF IPL FIG 21, Item 120).

(4) Connect the IFE power cables to the power outlets.

(5) Connect the control cables (REF IPL FIG 2, Item 5). Refer to Paragraph AV.

AC. Assembly and Installation of the Lower Console

Gutierrez
(Refer to IPL FIG 19)
(1) To assemble the rear panel assembly (5):

(a) To assemble the reinforcement bracket assembly (45), install the clip nuts (55)
onto the reinforcement bracket (60).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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AC. Assembly and Installation of the Lower Console (Continued)

(Refer to IPL FIG 19)
(b) Install the reinforcement bracket assembly (45) and lower trim bezels (65, 70) onto
the lower SPM panel shroud (75) by installing the screws (50).

(c) Install the lower SPM panels (30, 35) by installing the screws (40).

(2) Align the rear panel assembly (5) onto the frame assembly (REF IPL FIG 1,

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Item -230) and install the screws (10, 20), hinged screw covers (25), and snap
rivets (15).

AD. Installation of the Electrical Components

[Refer to IPL FIG 18, SCHEMATIC AND WIRING DIAGRAMS (Page Block 2000)
and 3D PDF electrical drawings for more electrical details.]
NOTE: IPL FIG 18 contains a complete listing of components for parts ordering.
SCHEMATIC AND WIRING DIAGRAMS (Page Block 2000) contains detailed
guidance for installing electrical components and harnesses. Refer to 3D PDF
electrical drawings referenced in this CMM for specific electrical information related
to the product addressed in this CMM. USING 3D ELECTRICAL DRAWINGS
(Page Block 17000) contains guidance for 3D interface. 3D PDF electrical
installation drawings are available to the customer upon request. Requests should
be sent to the following E-mail address: ws_techpubs3d@collins.com

NOTE: For specific instructions on installation of the ISPS, refer to DESCRIPTION AND
OPERATION Section, Paragraph 3.N.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

AE. Assembly of the Quadrant

(Refer to IPL FIG 17)
(1) Install the bushings (20, 25) into the quadrants (30, 30B).

(2) Install the HIC links (5) onto the quadrants (30, 30B) by installing the plain
bushings (10, 10A) and dowel pin (15).

AF. Assembly of the Back

(Refer to IPL FIG 16)
(1) Install the video bezel mounts (110, 115) by installing the rivets (120). Gutierrez

(2) Install the upper literature pocket bracket assembly (85) by installing the screws (90),
washers (95), and rivets (-100, -105).

(3) Install the comfort pads (70, 75) to the back frame assembly (125, 125B) by installing the
screws (80).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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COMPONENT MAINTENANCE MANUAL
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AF. Assembly of the Back (Continued)

(Refer to IPL FIG 16)
(4) To assemble the back frame assembly (125, 125B):

(a) To assemble the back frame w/ quadrants (140, 140B), install the quadrant
assemblies (145, 145B, 150, 150B) to the back frame (170) by installing the
pins (155), bushings (160), and retaining rings (165).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(b) If removed, attach the 3M™ hook tapes (135) to the back frame
w/ quadrants (140, 140B).

(c) Install the back diaphragm (130, 130A) to the back frame
w/ quadrants (140, 140B).

NOTE: Use the tool listed in SPECIAL TOOLS, FIXTURES, AND EQUIPMENT
(Page Block 9000) and follow the instructions to install the back
diaphragm (130, 130A).

(5) Install the literature spring supports (55) by installing the screws (60) and washers (65).

(6) Install the literature spring (35) by installing the screws (40), loop clamps (45), and
nuts (50).

(7) Install the lower literature pocket brackets (20, 25) to the back frame assembly (125B)
by installing the screws (30).

(8) Install the lower literature sub-brackets (5, 10) to the back frame assembly (125B) by
installing the screws (15).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

AG. Installation of the Back Assembly

(Refer to IPL FIG 15)
(1) Carefully align the back frame assembly (5) onto the spreader assemblies.

(2) Attach the back frame assembly (5) to the spreader assembly (REF) at the
non-hydraulic lock side by installing the screws (10, 40), shackle fitting (15),
bushing (20), washers (25, 30), and nut (35).

NOTE: Torque the screw (10) to 90 ±10 IN-LB.

NOTE: Torque the screw (40) to 100 ±10 IN-LB. Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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AG. Installation of the Back Assembly (Continued)

(Refer to IPL FIG 15)
(3) Attach the back frame assembly (5) to the spreader assembly (REF) at the hydraulic
lock side by installing the screw (45), shackle fitting (50), bushing (55), washers (60, 65),
nut (70), and vinyl cap (75), and screw (80).

NOTE: Torque the screw (45) to 90 ±10 IN-LB.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

NOTE: Torque the screw (80) to 100 ±10 IN-LB.

(4) Attach the screw (85).

NOTE: Set back upright position prior to installing. Tighten until free play is removed
between quadrant assembly and shoulder screw (40) and screws (80), then
add 1/4 turn.

(5) Attach the hydraulic lock (90) to the back frame assembly (5) by installing the bolt (95),
washer (100), and nut (105).

(6) Install the hydraulic lock (90) onto the spreader assembly (REF) by installing the
washers (115) and nuts (110).

NOTE: Turn the nuts (110) in order to close the cams on both washers (115), then
fully tighten to recline lock mount eyebolt.

(7) Connect the control cable (REF IPL 2, Item 5) to the hydraulic lock (90).

(8) Attach the seatpan assembly (REF IPL 8, Item 5) onto the back assembly (5). Refer to
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Paragraph AP.

AH. Installation of the Lower Literature Assembly and Back Trim

(Refer to IPL FIG 14)
(1) Attach the back trim (40) to the back assembly (REF) by installing the screws (45) and
washers (50).

(2) Attach the lower literature pocket assembly (30) by installing the screws (35).

(3) Attach the lower literature pocket handle (20) and lower literature pocket spring (25).

(4) Attach the lower literature assembly (5) onto the back assembly (REF) by installing the Gutierrez
screws (10) and loop clamps (15).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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AJ. Installation of the Coat Hook

(Refer to IPL FIG 13)
(1) Install the coat hook pin (5) on to the back frame (REF) by installing the spring (10),
washer (15), and retaining ring (20).

(2) Install the bushing (-25) by installing the rivet (-30).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

AK. Installation of the Video Bezel / Upper Literature Pocket Assembly
(Refer to IPL FIG 12)
(1) Install the upper literature pocket bonded assembly (5) onto the back assembly (REF) by
installing the screws (10) and washers (15).

AL. Installation of the Headrest Frame Assembly

(Refer to IPL FIG 11)
(1) Install the receptacles (10) on to the back (REF).

NOTE: Install the receptacles (10) before installing the headrest assembly (5).

(2) Align the headrest assembly (5) into the slots on back (REF) and engage the captive
screws on to the receptacles (10).

AM. Assembly of the Seatpan

(Refer to IPL FIG 10)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(1) Slide the crystal flex tube (15) and front tube assembly (5) through the flap of the bottom
diaphragm (20).

(2) Attach the front tube assembly (5) to the rail assemblies (25, 30) by installing the
bolts (10).

NOTE: Use the tool listed in SPECIAL TOOLS, FIXTURES, AND EQUIPMENT
(Page Block 9000) and follow the instructions to assemble the bottom
diaphragm (20) and crystal flex tube (15) onto the rail assemblies (25, 30).

(3) Wrap the bottom diaphragm (20) around the rail assemblies (25, 30) and engage the
hook-and-pile fastening.
Gutierrez

AN. Installation of the Seatpan Support

(Refer to IPL FIG 9)
(1) Install the snap studs (45) onto the seatpan assembly (REF) by installing the rivets (50).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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AN. Installation of the Seatpan Support (Continued)

(Refer to IPL FIG 9)
(2) Install the seatpan straps (25, 30) onto the seatpan assembly (REF) by installing the
rivets (35) and washers (40).

NOTE: Reconnect the seatpan straps (25, 30) when they have been disconnected to
service other components on the seat.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(3) Install the wire clip (20) onto the seatpan assembly (REF).

(4) Install the seatpan support stand (5) onto the seatpan assembly (REF) by installing the
retaining ring (10), flange bearing (15), and clip onto the wire clip (20).

AP. Installation of the Seatpan Assembly

(Refer to IPL FIG 8)
(1) Align the seatpan assembly (5) onto the riveted back assembly (REF) and install the
bolt (10), washers (15, 30), bushing (20), collar (25), and nut (35).

AQ. Assembly of the Link - Legrest

(Refer to IPL FIG 7)
(1) To assemble the link assembly (140), install the bearings (165) and pivot pin (170) into
the legrest link (175).

(2) Install the link assembly (140) onto the main body support (180) by installing the
bolt (145), washer (150), bushing (155), and nut (160).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(3) To assemble the link assembly (95), install the bearings (125) and pivot pins (130) into
the legrest link (135).

(4) Install the link assembly (95) onto the legrest main body support (180) by installing the
bolt (100), washer (105), bushing (110), spacer (115), and nut (120).

(5) To assemble the link assembly (55), install the bearings (75, 80) into the legrest
link (85).

(6) Install the link assembly (55) and link shroud (90) onto the link assemblies (95, 140) by
installing the spacers (60), washer (65), and retaining rings (70).
Gutierrez
(7) To assemble the link assembly (25), install the bearings (40, 45) into the legrest
link (50).

(8) Install the link assembly (25) onto the link assembly (95) by installing the spacer (30)
and retaining ring (35).

(9) Install the link shroud (15) by installing the screws (20).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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AQ. Assembly of the Link - Legrest (Continued)

(Refer to IPL FIG 7)
(10) Install the link shroud (5) by installing the snap rivets (10).

AR. Assembly of the Frame Link

(Refer to IPL FIG 6)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(1) Install the custom coils (115).

(2) Install the IGUS drylin rails (105) to the link assemblies (120, 125) by installing the
screws (110).

(3) Install the extension bumpers (95) by installing the screws (100).

(4) Install the legrest lower cross bar (80) by installing the bolts (85) and nuts (90).

(5) Install the pivot extension bracket (70) by installing the screws (75).

(6) Assemble the flanged bearings (60) and I-bolt (65).

(7) Install rotation pivot brackets (20, 40) and install the screws (25, 45), washers (30, 50),
and nuts (35, 55).

(8) Attach the edging grommet (15) onto the legrest pan assembly (5).

NOTE: Attach the edging grommet (15) with Loctite®-454.

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(9) Install the legrest pan assembly (5) by installing the screws (10).

AS. Assembly of the Paddle - Legrest

(Refer to IPL FIG 5)
(1) To assemble the foot pan assembly (45):

(a) To assemble the paddle hinge mount assemblies (105, 135), install the
bearings (125, -155) into the paddle hinge mounts (130, -160).

(b) Install the paddle hinge mount assemblies (105, 135) to the torque hinge mount
assemblies (55, 80) by installing the bolts (-110, 140), washers (-115, 145), and
bushings (-120, 150). Gutierrez

(c) To assemble the torque hinge mount assemblies (55, 80), install the torque hinge
mounts (65, 90) and reeltorq insert (70, -95) to the pivot hinges (75, 100).

(d) Install the torque hinge mount assemblies (55, 80) to the foot paddle (165) by
installing the screws (60, 85).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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AS. Assembly of the Paddle - Legrest (Continued)

(Refer to IPL FIG 5)
(2) Install the foot pan assembly (45) onto the legrest extension pan (170) by installing the
screws (50).

(3) To assemble the link arm assembly (5), install the flanged bearing (35) into the
extension link arm (40).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(4) Install the link arm assembly (5) onto the legrest extension pan (170) by installing the
screw (10), bushings (15, 20), spacer (25), and washer (30).

AT. Assembly of the Legrest

(Refer to IPL FIG 4)
(1) Install the 3M™ hook tape (120) and 3M™ loop tape (125) to the frame link
assembly (135) by installing the rivets (-130).

(2) Install the pivot support (110) by installing the screw (115).

NOTE: Torque the screw (115) to 15-18 IN-LB.

(3) Install the paddle assembly (90) by installing the screws (95, 105) and washer (100).

NOTE: Add the washer (100) and screw (95) thru slot, but do not tighten down.

NOTE: Torque screw (105) down securely into position.

(4) To assemble the extension lock assembly (25):

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(a) To assemble the valve release (55):

1 Attach the cable ferrule (75) to valve release head (85) by installing the
retaining ring (80).

2 Install the spring (70) onto the valve release head (85).

3 Attach the lever arm (60) by installing the bolt (65).

(b) Install the valve release (55) to the gas spring (50).

(5) Install the extension lock assembly (25) by installing the bolt (30), pivot pin (35), Gutierrez
spacer (40), and retaining ring (45).

(6) If removed, attach the 3M™ loop tape (20).

(7) Install the legrest shroud (5) by installing the screws (10) snap rivets (15).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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AU. Installation of the Legrest

(Refer to IPL FIG 3)
(1) Install the legrest assembly (115) onto the seatpan assembly (REF) by installing the
bolts (120), bushings (125), spacers (130), nuts (135), screws (140), bushings (145),
spacers (150), nuts (155), bushings (160), washers (165), and nuts (170).

(2) Install the fixed shrouds (95, 105) by installing the snap rivets (100, 110).

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(3) To assemble the valve release (60):

(a) Attach the cable ferrule (80) to the bottom jaw (90) with the retaining ring (85).

(b) Install the helical spring (75) onto the bottom jaw (90).

(c) Attach the top jaw (65) by installing the bolt (70).

(4) Attach the lockable gas spring (15) to the legrest assembly (115) with the washers (35)
and nuts (45).

(5) Attach the valve release (60) to the lockable gas spring (15) with the retaining ring (30).

(6) To assemble the rod end assembly (45), install the bearing (-50) into the rod end (-55).

(7) Install the rod end assembly (45).

(8) Install the lockable gas spring (15) and rod end assembly (45) to the seatpan front tube
assembly (REF) with the bolt (20) and nut (25).
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(9) Connect the control cables (REF IPL FIG 2, Items 10, 15) to the lockable gas spring (15)
and extension lock assembly (REF IPL FIG 4, Item 25).

(10) Install the legrest shroud (5) by installing the snap rivets (10).

AV. Installation of the Control Cables

(Refer to IPL FIG 2)
(1) Remove the seat control button assemblies (REF IPL FIG 21, Items 160, 165) by turning
the retainer a quarter-turn and lifting clear.

(2) Connect the control cables (5, 10, 15) to the seat control buttons. Gutierrez

(3) Re-install the seat control button assemblies (REF IPL FIG 21, Items 160, 165) and turn
the retainer a quarter-turn to re-engage.

(4) To provide easier access to route the control cables through the seat:

(a) Remove the bottom cushion assembly.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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AV. Installation of the Control Cables (Continued)

(Refer to IPL FIG 2)
(b) Pull on the legrest control lever and raise the legrest assembly.

(c) Unsnap the seatpan straps (REF IPL FIG 9, Items 25, 30) and unwrap onto around
the seatpan rollers.

(d) Lift up the seatpan assembly, unclip the seatpan support stand (REF IPL FIG 9,

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Item 5) and position the seatpan support stand (REF IPL FIG 9, Item 5) on the
seatpan roller to support the seatpan assembly.

(5) Route the control cables (5, 10, 15) through the console assembly (REF) and install the
tiedown straps (20, 25, 40), ring connectors (30), push mounts (35), cable spacers (45),
and 3M™ foam tape (50) as required.

NOTE: To access the tiedown straps (20, 25, 40), remove the cocktail table
assembly (REF IPL FIG 21, Item 45) by removing the hinged screw
covers (REF IPL FIG 21, Item 60) and screws (REF IPL FIG 21, Items 50, 55).

(6) Connect the control cables (5, 10, 15) to the recline, legrest, and foot paddle gas
springs.

AW. Installation of the Covers, Cushions, and Lap Belts

(Refer to IPL FIG 1)
(1) Install the literature pocket cover assemblies (-50) to the back assemblies by engaging
the hook-and-pile fastenings.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(2) Install the backrest cushions (45) and back cover assemblies (40) on to the back
assembly and engage the hook-and-pile fastenings.

(3) Install the headrest cushion assemblies (35) and headrest cover assemblies (30) on to
the headrest assembly and engage the hook-and-pile fastenings.

(4) Install the foot legrest cushion assemblies (25) on to the legrest assembly and engage
the hook-and-pile fastenings.

(5) Install the foot paddle covers (20) on to the foot paddle assembly and engage the
hook-and-pile fastenings.

(6) Install the bottom cushion assemblies (15) to the seatpan assembly by engaging the Gutierrez
hook-and-pile fastenings.

(7) Install the bottom legrest covers (10) on to the seatpan assemblies and engage the
hook-and-pile fastenings.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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AW. Installation of the Covers, Cushions, and Lap Belts (Continued)

(Refer to IPL FIG 1)
(8) Install the seat bottom cushion assemblies onto the seatpan diaphragm by doing the
following:

(a) Attach the back cover tail flap to the diaphragm using hook / loop surfaces.

(b) Make sure edge of cover tails aligns with marking on diaphragm as shown in

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Figure 7001.

Figure 7001
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(c) Locate hook/loop strips used for bottom cushion (marked "A" and "B") in
Figure 7002.

Gutierrez

Figure 7002

U.S. Export Classification: EAR 9E991 25-20-83-4667

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AW. Installation of the Covers, Cushions, and Lap Belts (Continued)

(Refer to IPL FIG 1)
(d) Position Cushion as far aft as possible to align A and B.

(e) Hold cushion up and away from bottom diaphragm and apply pressure in the aft
direction to ensure cushion is positioned as far aft as possible. Refer to
Figure 7003.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Figure 7003

(f) Lie cushion flat while maintaining pressure in the aft direction as shown in
Figure 7004.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Figure 7004

U.S. Export Classification: EAR 9E991 25-20-83-4667

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AW. Installation of the Covers, Cushions, and Lap Belts (Continued)

(Refer to IPL FIG 1)
(g) Apply even pressure across entire cushion in the downward direction to make sure
"A" and "B" are completely engaged as shown in Figure 7005.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Figure 7005

(h) Inspect cushion installation. There should be no gap between seat back and
bottom cushion as shown in Figure 7006.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Figure 7006

(9) Install the lap belt assemblies (5).

U.S. Export Classification: EAR 9E991 25-20-83-4667

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4. Dress Cover Assemblies Installation

A. Be careful when installing dress covers so they will look good. Apply the dress cover on the
foam smoothly. Work the cover with the palm of the hand so the cover is in position before it is
locked down. The fold of all cord seams must be on the top or the bottom, the front or the rear,
but not on the side of the foam.

CAUTION: IF USING AN AWL, DO NOT PUSH THE POINT OF THE AWL INTO THE FOAM
BECAUSE IT WILL DAMAGE THE CUSHION.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

B. The same fold should be put onto the top or the bottom, the front or the rear of the foam as the
cover is moved into place. parts of the rear fold can move out of position. To locate a fold that
is out of position, feel along the seam edges after the cover is installed. Adjust the fold with a
sharp pointed awl. Move the point of the awl 1/4 to 3/8 inch (6.35 to 9.63 mm) into the material
along the seam fold. Move the awl handle to catch the seam fold and move it into position.

C. When attaching the hook-and-pile tape, align the edges so the cover is smooth. The
hook-and-pile tape will not be seen when it is correctly attached.

5. Storage

A. General

(1) The seat assembly, spare seat assembly components, furniture assembly and/or spare
furniture assembly components should be stored either in its original packaging
(if available), in a suitable container, or should be properly wrapped. (For details,
see Paragraph C below.)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(2) If stacked storage must be used, avoid damage caused by excessive weight. (Refer to
DESCRIPTION AND OPERATION Section for seat and/or furniture assembly weights.)

(3) The packed / wrapped seat assembly, spare seat assembly components, furniture
assembly and/or spare furniture assembly components ideally should be stored in a
clean, dry, well-ventilated, temperature- and humidity-controlled environment.

(4) The seat assembly, spare seat assembly components, furniture assembly and/or spare
furniture assembly components storage should be maintained between 5°C (41°F)
minimum and 30°C (86°F) maximum.

(5) Relative humidity should not exceed 65%.

Gutierrez
(6) The packed / wrapped seat assembly, spare seat assembly components, furniture
assembly and/or spare furniture assembly components should not be stored in the
vicinity of corrosive fluids or gases, in direct sunlight, or near heat or ozone generating
surfaces.

(7) The packed / wrapped seat assembly, spare seat assembly components, furniture
assembly and/or spare furniture assembly components should be positioned so that
storage identification label (See Paragraph D below) can be easily checked.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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B. Preservation

(1) Before packing / wrapping for storage, the seat assembly, spare seat assembly
components, furniture assembly and/or spare furniture assembly components should be
preserved in accordance with Specification MIL-STD-2073-1D.

C. Packing / Wrapping

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(1) The seat assembly, spare seat assembly components, furniture assembly and/or spare
furniture assembly components should be stored either in its original packaging
(if available) or a suitable container, in accordance with Air Transport Association
Specification No. 300 (ATA 300).

(2) If a container is used, cushioning material and bracing must be provided to prevent
accidental damage. (Refer to DESCRIPTION AND OPERATION Section for seat and/or
furniture assembly dimensions.)

(3) If wrapped, the seat assembly, spare seat assembly components, furniture assembly
and/or spare furniture assembly components should be completely covered in
waterproof wrapping paper (Federal Specification UU-P-271, or equivalent), or plastic
cover. Use tape (Federal Specification JAN-P-127, or equivalent) to secure wrapping
plastic or plastic cover.

D. Storage Identification Label

(1) A storage identification label should be affixed to the seat assembly, spare seat
assembly components, furniture assembly and/or spare furniture assembly components
before packing / wrapping, but an identical identification label MUST be affixed to
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

outside of package / wrapping.

(2) Labels must contain all relevant data, including seat assembly, spare seat assembly
components, furniture assembly and/or spare furniture assembly components part
number, date of storage, and dates for condition checks during storage.

(3) If label is missing, the seat assembly, spare seat assembly components, furniture
assembly and/or spare furniture assembly components should not be approved for
storage until properly reidentified.

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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FITS AND CLEARANCES

1. General

Normal maintenance of the seat assemblies does not require fit and clearance information.

2. Torque Tables

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

A. Threaded Fastener Torque Ranges

When specific torque values are not shown on the applicable drawing, use the torque values
in Table 8001 as a guide for tightening nuts, studs, bolts, and screws. When tightening a nut
and bolt that are used together, measure the torque value on the nut. If the nut is inaccessible
or a nut is not used, measure the torque on the bolt.

(1) Standards and Specifications for Values

(a) Self-Locking Fasteners

A self-locking fastener supplies more resistance when it is turned on a thread.

Because of this, add the prevailing torque value to the standard torque value to get
the correct torque value for a self-locking fastener. This helps prevent unwanted
vibrations that can work the fastener loose (See Table 8001).

(b) Standard Fastener Values

Most standard fastener values are from the Standard Aircraft Handbook. Refer to it
for any fastener not listed in Table 8001.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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Table 8001
Common Assembly Torque Values (IN-LB)
EXCEPTIONS
PREVAILING (SELF-LOCKING)
TORQUE MIN-MAX
_____________________
STANDARD MAX(2)(3)(4) SELF-LOCKING
THREAD FASTENERS (REFERENCE FASTENERS DECORATIVE

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THREAD/IN TYPE MIN-MAX(1)(3) ONLY) MIN-MAX(4) PLASTIC(5)
4-40(3) Coarse 3-4 4 7-8 3-4

6-32(3) Coarse 5-6 8 13 - 14 6-7

8-32 Coarse 7-9 12 19 - 21 9 - 11
10-32 Fine 12 - 15 17 29 - 32 14 - 16
1/4-28 Fine 30 - 40 40 70 - 80 35 - 40
5/16-24 Fine 60 - 85 80 140 - 165 70 - 83
3/8-24 Fine 95 - 110 110 205 - 220 102 - 110
7/16-20 Fine 270 - 300 135 405 - 435 202 - 218
1/2-20 Fine 290 - 410 204 494 - 614 247 - 307

(1) Values taken from AC43.13-1B for shear type fasteners. Refer to this document for any
fasteners sizes not shown.
(2) Prevailing torque values taken from ASME B18.16.6, Prevailing Torque Locknuts (Inch
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Series). Refer to this standard for values not shown.

(3) Torque values provided by Collins Aerospace Seating for sizes 4-40 and 6-32.
(4) These values apply to bolts and nuts.
(5) Values derived as follows: Decorative Plastic: 50% of Self-Locking MIN-MAX.

3. Quarter-Turn and Other Fixed Fasteners

To properly secure items fastened by quarter-turn (1/4) and other fixed fasteners, align the holes
on the part being fastened, press and hold the part in place, turn fastener to engage.

Gutierrez

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SPECIAL TOOLS, FIXTURES, AND EQUIPMENT

1. Tools

A. Generally, only common hand tools are required to assemble and / or disassemble the seats.
Refer to Table 9001 for a list of suggested common hand tools.

However, special tools are required to install / remove the seatpan and back diaphragms, and

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

privacy divider assembly. Refer to Table 9002 for a list of special tools and Paragraph 4 for
operation instructions.

NOTE: Equivalent substitutes may be used for items listed in Table 9001.

Table 9001
Suggested Common Hand Tools
QUANTITY
TOOL REQUIRED
#1 Flat Screwdriver 1
#2 Flat Screwdriver 1
#2 Phillips Head Screwdriver 1
#3 Phillips Head Screwdriver 1
1/2" Opened, Closed Ended Wrench 2
1/2" Thin Wall Socket - 3/8" Drive 2
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

11/32" Opened, Closed Ended Wrench 2

3/4" Thin Wall Socket - 3/8" Drive 2
3/8" Thin Wall Socket - 3/8" Drive 2
4" Ratchet Extension - 3/8" Drive 1
6" Ratchet Extension - 3/8" Drive 1
7/16" Opened, Closed Ended Wrench 2
7/16" Thin Wall Socket - 3/8" Drive 2
8" Ratchet Extension - 3/8" Drive 1
9/16" Opened, Closed Ended Wrench 2 Gutierrez
9/16" Thin Wall Socket - 3/8" Drive 2
Ball Peen Hammer 1
Channel Lock 1
Cordless Drill 1
File Set 1

U.S. Export Classification: EAR 9E991 25-20-83-4667

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Table 9001 (Continued)

Suggested Common Hand Tools
QUANTITY
TOOL REQUIRED
HEX Wrench Set - Metric 1
HEX Wrench Set - Standard 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Needle Nose Pliers 1
Pliers 1
Ratchet - 3/8" Drive 1
Razor Knife 1
Reamer Set 1
Rubber Tipped Hammer 1
Scissors 1
Scratch Awl 1
Snap Ring 1
Tape Measure - 6' 1
Tie Wire Cutters 1
Torque Wrench (200 IN-LB MAX Capacity) 1
Wire Cutters 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Table 9002
Special Tools
PART
DESCRIPTION NUMBER
Back Diaphragm Installation Tool (Alternate) 800-B-063
Back Diaphragm Stretcher Tool 800-F-156
Seatpan Diaphragm Tool 800-F-189

NOTE: For seatpan and back diaphragm tool operation instructions, see Paragraph 4 below.
Gutierrez
2. Fixtures

There are no special fixture requirements.

3. Equipment

There are no special equipment requirements.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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4. Special Tools Operation Instructions

A. Seatpan Diaphragm Stretcher Tool (800-F-189)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(1) Ensure the ram is fully retracted by loosening the bleed screw. Then make sure the
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

bleed screw is tight.

Gutierrez

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Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(2) Slide the front and rear diaphragm tubes through the diaphragm and attach the front
tube to the side rails by installing screws. Align the seatpan assembly on the tool.

NOTE: Ensure the rear tube is located at the rear of the tool (below the side rails)
and the diaphragm is correctly orientated with label visible as shown above.

Gutierrez

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Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(3) With the tubes in position, pump the cylinder to stretch the diaphragm.

Gutierrez

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Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(4) Operate the pump handle to stretch the diaphragm further until the rear tube is located
behind the slots in the side rails.

(5) Push the side rails downward over the rear tube and ensure the slots are aligned with
the rear tube.

(6) Loosen the bleed tube slightly to allow the hydraulic ram to retract, ensure the rear tube
is aligned and moves into the slots of the side rails as it moves forwards and is fully
engaged.

Gutierrez

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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(7) Remove the seatpan from the fixture and turn upside down.

(8) Pull the side flaps around the side rails and engage the hook and pile fastenings at the
underside of the rails.

NOTE: The above operation can be used in reverse to remove the diaphragm.

Gutierrez

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B. Back Diaphragm Stretcher Tool (800-F-156)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(1) Install the back diaphragm onto the seat back and place the twin rods into all the loops of
the diaphragm. Align the top loops with the black lines on each rod, as shown.

(2) Slide the threaded block onto the LH rod until the pin on the threaded block slides into
one of the holes on the rod. Using 3/4” socket and cordless drill turn the threaded rod
slowly until the pin on the second threaded block slides into the parallel corresponding
hole on the RH rod - See below.

Gutierrez

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Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(3) When the pins are properly located in the holes continue to turn the threaded bar to
stretch the diaphragm.

Gutierrez

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 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(4) Once the twin rods are parallel, align the flaps and close the zippers.

WARNING: ENSURE SEAT BACK DIAPHRAGM ZIPPERS HAVE THEIR

METALSLIDERS / TANGS POSITIONS ON THE AFT SIDE OF THE
HORIZONTAL CROSS BEAM OR ELSE THEY WILL BE FELT AS A
SHARP POINT IN THE PASSENGER'S BACK AND COULD CAUSE
INJURY.

(5) To remove the tool, reverse the drill and retract the threaded bar until the threaded
blocks can be removed from the rods. Pull the twin rods out of the diaphragm loops.
Gutierrez
NOTE: The above operation can be used in reverse to remove the diaphragm.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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ILLUSTRATED PARTS LIST

1. Introduction

A. Purpose

This Illustrated Parts List (IPL) helps to find and identify procurable parts of the seats.
A procurable part is one that can be purchased as a replacement part.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

B. How to Use the IPL

Each IPL figure has an illustration that uses item numbers to identify parts of the seat that
can be replaced. Each illustration is followed by a parts list that shows all of the parts in item
number sequence. Each parts list has the following columns:

Table 10001
IPL Column Description
FIG. ITEM The number at the top of this column identifies the IPL Figure.
The other numbers are item numbers. An item number is given to
each part that can be replaced and is shown on the illustration.
A dash (-) before an item number shows that the part is not
shown on the illustration.
PART NUMBER Identifies installations, assemblies and parts by number.
If a part number is followed by (NP), that part is not procurable.
If a part number is followed by (REF), that part number is a
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

reference only because the actual ‘true’ part number does not
conform to ATA Spec 2000. The ‘true’ part number for ordering
purposes and replacement is found in the nomenclature column.
AIRLINE PART NO. Blank column for airline use.
NOMENCLATURE Identifies parts by name and is indented to show how parts
are related to the primary assembly. See the next page for more
details.
EFF CODE Identifies which parts are used on the primary assemblies.
The primary assemblies are shown at the start of the IPL figure.
An effectivity code letter is given to each primary assembly.
Each part used on a primary assembly is given the effectivity
code letter of that primary assembly. If a part is used on all of the Gutierrez
primary assemblies, it is not given an effectivity code.
The effectivity codes in each IPL figure apply only to that figure
and are not related to the effectivity codes in any other IPL figure.
UNITS/ASSY Identifies the quantity of each part used on the primary assembly.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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The Nomenclature column uses bullet indents (•) to show the relationship between parts, as in the
examples that follow:

Table 10002
Nomenclature Column Descriptions
Assembly or Installation This is the primary assembly/installation and is not indented.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

• Subassembly/Detail Part This is a subassembly or detail part of the primary assembly/
installation. It is indented with one bullet (•).
If parts with two bullets (• •) follow the subassembly, they are part
of the subassembly.
• • Sub-subassembly/Detail A sub-subassembly/detail part of the subassembly. It is indented
Part with two bullets (• •). If you can purchase the one indent
subassembly/part, this part will be included. If parts with three
bullets (• • •) follow the sub-subassembly, they are part of the
sub-subassembly.
• • • Detail Part Detail part for the sub-subassembly. It is indented with three
bullets (• • •). If you can purchase the two-indent part, this part will
be included.
ATTACHING PARTS Shows that the parts listed after it attach the part or parts before it.
Shows the end of an ATTACHING PARTS list. Also used at the
* * * end of individual IPL parts listing tables.
C. Unless instructions for individual pieces of hardware specify otherwise, use the following
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

guidelines per manufacturer's instructions:

For threaded hardware used on plastic components (for example; injection molded w/ inserts,
machined threads in plastics, etc.) apply Loctite®-454 cyanoacrylate based adhesive to ALL
hardware that is installed without a threadlocking element (for example, lock patch, locking
helicoil insert, etc.). Apply one drop (.05 mL) per square inch of engaged threads. Excessive
application may result in an inseparable assembly.

CAUTION: PLASTIC COMPONENTS MAY DEGRADE AND FAIL WITH CONTACT FROM
ANAEROBIC BASED THREAD LOCKING ADHESIVES (FOR EXAMPLE,
LOCTITE®-222, -242, -243, -262, -263). AVOID EXCESSIVE APPLICATION
THAT MAY CAUSE SPILLAGE ON PLASTICS, OR USE A CYANOACRYLATE
BASED THREAD LOCKER (FOR EXAMPLE, LOCTITE®-454) THAT IS SAFE Gutierrez
FOR PLASTICS. STICK FORM LOCTITE® (FOR EXAMPLE, LOCTITE®-2X8)
CAN ALSO BE USED TO AVOID SPILLAGE ON PLASTIC PARTS.

(1) For hardware with thread size 8 and higher, apply Loctite®-243 adhesive to ALL
non-locking hardware and ALL hardware used in joints with no locking element.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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(2) For hardware with thread size less than 8, apply Loctite®-222 adhesive and
Loctite®-7649 activator to all non-locking hardware and all hardware used in joints
with no locking element.

2. Vendor Codes

Vendor Code numbers are specified in the current issue of Federal Supply Code for
Manufacturers, Catalogue Handbooks H4-1, H4-3 and/or NATO codes, and are available

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

on the internet at: https://cage.dla.mil.

3. Trim and Finish Codes

All seat part numbers and some parts in the IPL include a Trim and Finish (T & F) code at the end
of the part number. Be sure to include the T & F codes when purchasing replacement parts.
Example: part number 1367870-005MS08 where MS08 is the part’s T & F code.

4. LPxxxxx Parts Versus MSxxxxx Parts

The “LP” in LPxxxxx part numbers indicates that the part (typically a fastener such as a bolt,
screw or nut) has “lockpatch” material applied to the threads to make the part self-locking. When
such a part is used, the lockpatch is compressed, creating a much stronger metal-to-metal contact
and positive resistance to vibration and loosening. YOU CAN REPLACE AN LPxxxxx PART WITH
AN EQUIVALENT MSxxxxx PART ONLY IF YOU USE A LOCKING MATERIAL (SUCH AS
LOCTITE®) ON THE THREADS OF THE MSxxxxx PART. For example, you may use part number
MS27039 in place of part number LP27039 only when you apply Loctite® to the threads before
installation.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

5. Product Support Services

TECHNICAL AND WARRANTY SUPPORT

Winston-Salem Interiors CMM Customer Portal: https://www.collinsaerospace.com/Technical-Publications
3D PDF requests by E-mail: ws_techpubs3d@collins.com
Technical and/or warranty support inquiries:
https://www.collinsaerospace.com/what-we-do/service-and-support/support/interiors

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

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MiQ™ 1367870 SERIES

6. Parts Replacement Data

Interchangeability relationship between parts is identified in the IPL NOMENCLATURE column.

A list of terms and associated abbreviations and definitions is given in Table 10003, Parts
Replacement Data.

Table 10003

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Parts Replacement Data
TERM ABBREVIATION DEFINITION
Part fully meets functional and structural
specifications, but may differ either in
overall external dimensions, connections,
Alternate ALT
installation, and/or mounting provisions,
and may require rework or modifications to
install in a specific application.
Part is replaced by and is interchangeable
(two-way) with item number listed in
Replaced By REPLD BY
nomenclature. Old parts may be used until
the supply is exhausted.
Part replaces and is interchangeable
(two-way) with item number listed in
Replaces REPLS
nomenclature. “Replaced By” parts may be
used until the supply is exhausted.
Part is replaced by and is not
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Superseded By SUPSD BY interchangeable (one-way) with item

number listed in nomenclature.
Part replaces and is not interchangeable
Supersedes SUPSDS (one-way) with item number listed in
nomenclature.
Identifies when a service bulletin (SB) has
an effect on a part. PRE SB shows the
PRE SB
condition of the part before the work in the
service bulletin is done.
Service Bulletins
Identifies when a service bulletin (SB) has
an effect on a part. POST SB shows the
POST SB
condition after the work in the service Gutierrez
bulletin is done.

U.S. Export Classification: EAR 9E991 25-20-83-4667

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7. Alpha/Numerical Index

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
ACD508ASM 13 -30 1
AC11427-00 39 5A 1
AC11429-00 39 5 1
AC97164-00 2 15 2

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

AC97166-00 2 10 2
AC97220-00 2 5 2
AD66ALS 16 120 2
AN3-5A 5 -110 1
AN3-5A 5 140 1
AN316-4R 15 105 1
AN316-6R 3 40 2
AN316-6R 15 110 2
AN4-11A 10 10 2
AN4-11A 3 120 2
AN4-14A 7 100 1
AN4-14A 7 145 1
AN5-5A 4 30 1
AN5-6A 3 20 1
AN565A1032H12 42 20 1
AN565A1032H12 42 40 1
AN970-3 42 15 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

AN970-3 42 35 1
AN970-4 44 15 1
APPPHC810108 21 60 2
APPPHC810108 19 25 2
AT327-14 18 -90 2
AT327-14 18 -90A 1
B1831AH030008L 21 85 4
CA7V0Z737-8 (NP) 1 -270 RF
CBSM5-10 34 10 2
CBSM5-10 34 40 2
CBSM5-10 34 70 2 Gutierrez
CBSM5-10 34 100 2
CBSTSE4-10 33 110 5
CR2 2 30 6
CR2 18 -110 2
CR2 18 -110A 3
CR4H 18 -115 3
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

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PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
CSCS 2 45 4
CSCS 18 -120 1
CSCS05-04 (REF) 9 50 1
CSW18-60-2RST (REF) 34 65 1
CSW18-60-2RST (REF) 34 95 1
CSW18-60-2RSU (REF) 34 5 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

CSW18-60-2RSU (REF) 34 35 1
D8-316-716-190 40 75 4
D8-326-101-200 40 80 4
D8-336-200-190 40 110 4
EIM030D04M 38 15 1
FTH3-01 (REF) 18 -215 1
FTH3-01 (REF) 18 -105 2
FTH3-01 (REF) 30 -180 3
FTH3-01 (REF) 30 -180A 6
FYNP1L183 (REF) 28 70 1
FYNP1R183 (REF) 28 -70A 1
GFI0405-04 (REF) 28 -80 1
GFI0405-05 (REF) 9 15 1
GSI0506-04 (REF) 3 -50 1
GSI1214-08 (REF) 28 -60 1
HV17500-10 15 90 1
IK0ML9C1R160H (REF) 22 5 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

JAH99-95 (REF) 21 200 2

JFI0506-04 (REF) 7 40 2
JFI0506-04 (REF) 7 75 4
JFI0506-06 (REF) 5 -155 1
JFI0506-06 (REF) 5 125 1
JFI0506-06 (REF) 6 60 2
JFI0608-04 (REF) 7 45 2
JFI0608-04 (REF) 7 80 2
JFI0608-04 (REF) 7 125 2
JFI0608-04 (REF) 7 165 2
JFI1012-08 (REF) 5 35 1 Gutierrez
LCM055D09M 13 10 1
LC016C13M 23 30 3
LC016C13M 3 75 1
LC016C13M 4 70 1
LC026EE10S 39 40 1
LE022B001M 33 65 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

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PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
LE037C00M 31 20 1
LWC50H25 9 20 1
MC37B0DY (REF) 21 65 1
MC37BLK1STRK (REF) 22 25 1
MFI0304-04 (REF) 28 140 4
ML1912 (REF) 33 20 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

MS16555-32 38 10 1
MS16555-43 28 115 4
MS16555-43 28 125 2
MS16555-54 17 15 1
MS16633-1012 31 15 2
MS16633-1012 23 25 1
MS16633-1018 13 20 1
MS16633-1018 25 -35 2
MS16633-2025 35 15 1
MS16633-2025 37 15 1
MS16633-2025 3 85 1
MS16633-2025 4 45 1
MS16633-2025 4 80 1
MS16633-2025 32 25 2
MS16633-2025 39 15 1
MS16633-2031 3 30 1
MS16633-2031 7 35 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

MS16633-2031 7 70 2
MS16633-4050 44 25 1
MS20253-2-103 34 140 1
MS20253-2-103 36 100 1
MS21042-08 6 35 1
MS21042-08 6 55 1
MS21042-08 38 30 1
MS21042-3 28 35 1
MS21042-3 39 50 1
MS21042-3 18 65 1
MS21042-3 18 85 1
Gutierrez
MS21042-3 43 20 2
MS21042-3 43 50 2
MS21042-4 3 155 2
MS21042-4 6 90 2
MS21042-4 15 35 1
MS21042-4 15 70 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

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PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
MS21042-6 45 20 1
MS21042L4 45 10 1
MS21043-3 16 50 2
MS21043-4 8 35 1
MS24693-25B 35 70 3
MS24693-25B 21 10 8

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

MS24693-25B 33 25 1
MS24693-46B 35 30 1
MS24693-46B 37 30 1
MS24693-48B 37 10 4
MS24693-49B 35 10 4
MS24693C2 (REF) 28 135 2
MS24693C24 (REF) 28 155 6
MS24693C25 (REF) 32 10 1
MS24693C3 (REF) 22 20 1
MS24693C47 (REF) 35 25 2
MS24693C47 (REF) 37 25 2
MS24693C49 (REF) 30 65 2
MS24693S276 (REF) 39 35 1
MS24693S48 (REF) 5 60 3
MS24693S48 (REF) 5 85 3
MS24694C4 (REF) 30 110 1
MS24694C48 (REF) 21 270 2
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

MS24694C5 (REF) 30 110A 1

MS24694C50 (REF) 21 205 2
MS25281F3 (REF) 14 15 4
MS25281F3 (REF) 16 45 2
MS27039-0804 7 20 2
MS27039-0806 14 35 4
MS27039-0806 4 10 2
MS27039-0806 5 50 8
MS27039-0806 6 10 6
MS27039-0806 16 15 2
MS27039-0807 16 90 4 Gutierrez
MS27039-0819 6 75 2
MS27039-0822 6 25 1
MS27039-0822 6 45 1
MS27039-1-06 4 115 1
MS27039-1-07 35 80 2
MS27039-1-08 5 10 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

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PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
MS27039-1-08 14 45 4
MS27039-1-10 4 95 1
MS27039-1-14 42 10 1
MS27039-1-14 42 30 1
MS27039-4-11 6 110 2
MS27039C0805 39 90 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

MS27039C0810 36 120 1
MS27980-7N 9 45 2
MS3367-4-0 32 -30 2
MS3367-4-9 2 20 10
MS3367-4-9 18 -220 AR
MS3367-4-9 18 -130 AR
MS3367-4-9 30 -185 11
MS3367-5-9 2 25 10
MS3367-5-9 18 -225 AR
MS3367-5-9 18 -135 AR
MS3367-5-9 30 -190 11
MS3367-5-9 39 10 4
MS3367-5-9 41 10 2
MS3367-5-9 41 65 2
MS3367-7-9 2 40 4
MS3367-7-9 18 -140 AR
MS3367-7-9 40 10 8
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

MS3367-7-9 41 20 4
MS3367-7-9 41 35 4
MS3367-7-9 41 50 2
MS35206-226 26 110 1
MS35335-35 3 35 2
MS35338-43P 18 50 1
MS35650-304 18 60 1
MS35650-304 18 80 1
MS51576-10 21 230 2
MS51576-2 31 30 1
MS51975-17P 15 40 1
Gutierrez
MS51975-17P 15 80 1
M225292-2R100 (REF) 40 115 AR
M225292-3R100 (REF) 6 15 1
M225292-5R100 (REF) 40 20 AR
M8372360-214A (REF) 18 -125 1
NAS1149A0316H 18 55 3
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

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PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
NAS1149A0316H 18 75 2
NAS1149CN416R 18 -100 8
NAS1149CN416R 18 -100A 4
NAS1149CN816R 16 95 4
NAS1149CN816R 16 65 2
NAS1149CN832B 12 15 2

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

NAS1149CN832R 6 30 2
NAS1149CN832R 6 50 2
NAS1149C0332R 5 -115 1
NAS1149C0332R 5 30 1
NAS1149C0332R 5 145 1
NAS1149C0332R 14 50 4
NAS1149C0416R 9 40 1
NAS1149C0432R 3 165 2
NAS1149C0432R 7 105 1
NAS1149C0432R 7 150 1
NAS1149C0432R 8 30 1
NAS1149C0432R 15 30 1
NAS1149C0432R 15 65 1
NAS1149C0532R 7 65 1
NAS1149D0332K 13 15 1
NAS1149G0332P 4 100 1
NAS1169-8L 33 30 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

NAS1297-3-2 35 100 1
NAS1297-3-2 37 65 1
NAS1351-3-14 27 10 2
NAS1351-3-6 21 255 4
NAS1351-3-6 21 280 4
NAS1351-3-6P 21 120 2
NAS1351-4-10 35 60 4
NAS1351-4-10 37 60 7
NAS1352-04-10 23 50 1
NAS1352-04-6 18 -95 8
NAS1352-04-6 18 -95A 4 Gutierrez
NAS1352-04-6P 21 70 4
NAS1352-06-4 22 10 3
NAS1352-06-6 28 25 4
NAS1352-06-6P 19 10 2
NAS1352-06-6P 33 75 1
NAS1352-06-6P 33 85 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

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PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
NAS1352-06-7 21 50 2
NAS1352-08-14 16 30 2
NAS1352-08-6P 33 125 2
NAS1352-08-8 16 60 2
NAS1352-08-8 26 20 4
NAS1352-08LB6 36 90 2

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

NAS1352-08LB6 34 130 2
NAS1352-08LB8P 30 85 2
NAS1352-08LB8P 30 100 2
NAS1352C06-6 33 40 1
NAS1515H4L 15 100 1
NAS1635-06-8 21 110 2
NAS1801-08-20 38 25 1
NAS1801-08-4 30 120 1
NAS1801-3-12 28 45 2
NAS1801-3-16 19 20 2
NAS1801-4-26 3 140 2
NAS1802-3-12P 18 45 1
NAS1802-3-14 16 40 2
NAS514P1032-8 26 70 2
NAS514P1032-8 26 85 2
NAS514P428-10B 30 25 2
NAS514P428-10B 36 10 2
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

NAS514P440-4 23 40 1
NAS514P832-5 39 95 5
NAS517-4-28 15 10 1
NAS517-4-38 15 45 1
NAS601-10P 33 55 4
NAS601-3P 30 135 2
NAS601-5B 21 95 2
NAS601-5P 19 40 2
NAS601-6B 6 100 1
NAS601-6P 19 50 4
NAS601-6P 21 -140 2
Gutierrez
NAS601-6P 21 130 2
NAS601-6P 21 150 2
NAS601-7B 36 130 3
NAS601-7P 21 285 2
NAS601-7P 25 10 2
NAS601-7P 26 10 4
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

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PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
NAS601-7P 26 30 2
NAS601-7P 26 50 2
NAS601-7P 26 75 4
NAS601-7P 26 90 4
NAS602-20P 33 10 1
NAS602-7B 25 25 6

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

NAS602-8B 12 10 2
NAS602-8B 30 15 2
NAS602-8P 16 80 2
NAS603-10P 4 105 8
NAS603-7B 21 55 2
NAS603-7B 15 85 2
NAS6204-9 15 95 1
NAS6603-1 21 215 2
NAS6603-1 28 55 2
NAS6603-1 21 30 3
NAS6603-1 26 100 2
NAS6603-1 26 115 2
NAS6603-1 34 25 2
NAS6603-1 34 55 2
NAS6603-1 34 85 2
NAS6603-1 34 115 2
NAS6603-32 43 15 2
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

NAS6603-32 43 40 1
NAS6603-34 43 45 1
NAS6604-1 20 10 4
NAS6604-11 29 15 4
NAS6604-14 6 85 2
NAS6604-18 40 95 3
NAS6604-19 45 60 1
NAS6604-25 8 10 1
NAS6604-4 39 25 1
NAS6604-9 45 5 1
NAS6606-18 45 40 1 Gutierrez
NAS6606-7 45 15 1
NAS75-3-013 5 -120 1
NAS75-3-013 5 150 1
NAS75-4-007 17 25 1
NAS75-4-008 3 160 2
NAS75-4-016 8 20 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10012
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
NAS75-4-024 3 125 2
NAS75-4-024 3 145 2
NAS75-4-100 7 110 1
NAS75-4-100 7 155 1
NAS75-4-104 17 10A 1
NAS75-4-105 17 10 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

NAS77-10-050 17 20 1
NAS77-3-019 5 15 1
NAS77-3-026 39 45 1
NAS77-6-024 44 35 1
NAS8302-4 28 105 8
NAS8302-8 14 10 4
NAS8602-6 3 70 1
NAS8602-6 4 65 1
NA0069A030006 (REF) 39 60 8
NA0069A030006 (REF) 39 80 7
NL38 (REF) 15 115 2
NL5 34 15 2
NL5 34 30 2
NL5 34 45 2
NL5 34 60 2
NL5 34 75 2
NL5 34 90 2
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

NL5 34 105 2
NL5 34 120 2
NPS24693S49 (REF) 33 135 2
NPS27039-4-06 44 10 1
NW12-0832-27 (REF) 28 160 2
NW12-0832-27Z (REF) 28 165 2
PUM049-30 (REF) 2 35 2
RA22CSN (REF) 22 15 1
RFI0607-04 (REF) 33 90 4
R4-99-421SLV (REF) 21 -245 1
SD32BS 4 -130 4
Gutierrez
SJ3518FR100B (REF) 4 20 AR
SJ3518FR200B (REF) 4 125 AR
SJ3519FR100B (REF) 4 120 AR
SJ3519FR100B (REF) 16 135 AR
SL210-06-1 25 15 4
SL210-06-1 26 -125 2
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10013
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
SL210-06-1 26 35 4
SL210-06-1 26 55 4
SL211-3-1 19 55 2
SP2063 31 25 1
SP25897C1430 32 -15A 1
SP25897C1630 32 15 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

SSDH43BS 33 145 4
SSD45BS 22 30 2
SSD52BS 16 -105 4
SSD66BS 9 35 1
UP4125 39 20 1
VC156-4 (REF) 22 35 2
VC161-3 (REF) 30 -115 1
VC240-3 (REF) 15 75 1
WJUM1032-10AL 6 115 4
WS10-250 (REF) 6 105 2
W0A7KK1033-1 (REF) 4 50 1
X0N0XK3-044-27 (REF) 3 15 1
0BF01-00523 16 -100 4
0601-034 21 35 2
1002933-029 (NP) 1 -245 1
1003114-201 45 55 2
1004710-007 42 50 4
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1012023-007 45 35 1
1012042-109 30 75 3
1012042-115 28 15 4
1016258-099 (NP) 1 -100 2
1016258-099 (NP) 13 -1 RF
1016258-109 13 5 1
1016258-111 13 -25 1
1017020-701 (NP) 18 -40 2
1017020-705 (NP) 18 -70 1
1017797-001 18 -175 1
1017797-003 18 -180 1 Gutierrez
1017797-005 18 -185 1
1020222-111 44 20 1
1021472-057MS02 28 5 1
1021472-058MS02 28 -5A 1
1021473-057MS02 28 170 1
1021473-058MS02 28 -170A 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10014
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
1021486-101 44 45 1
1021486-102 44 -45A 1
1021486-119 44 45B 1
1021486-120 44 -45C 1
1021487-015MS02 21 80 1
1021487-015MS02 22 -1 RF

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

1021487-017MS02 21 45 1
1021487-097MS02 21 75 1
1021487-099MS02 22 45 1
1021487-115 25 -30 1
1021487-205 26 40 1
1021487-206 26 60 1
1021505-057 1 -230 1
1021505-057 43 -1 RF
1021505-058 1 -230A 1
1021505-058 43 -1A RF
1021507-107 45 70 1
1021520-103 16 55 2
1021520-303ZXK 16 110 1
1021520-304ZXK 16 115 1
1021546-057 5 45 1
1021547-027FQ13 1 65 2
1021547-027FQ13 3 115 RF
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1021547-027FQ13 4 -1 RF
1021548-087 4 90 1
1021548-087 5 -1 RF
1021557-057 5 165 1
1021567-049 (NP) 1 -55 1
1021567-049 (NP) 2 -1 RF
1021569-003 1 -85 2
1021569-003 11 -1 RF
1021684-061 28 50 1
1021684-062 28 -50A 1
1021684-111 28 150 2
Gutierrez
1021684-117 28 65 1
1021684-118 28 -65A 1
1021684-137 28 40 1
1021684-139 28 -40A 1
1021684-140 28 -40B 1
1021684-141 28 -85 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10015
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
1021684-142 28 -85A 1
1021684-303FCJ 28 90 1
1021685-001 39 55 1
1021685-002 39 -55A 1
1021685-011 35 75 1
1021685-015 33 50 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

1021685-016 33 -50A 1
1021685-049 34 125 2
1021685-049 36 85 2
1021685-061 33 115 1
1021685-062 33 -115A 1
1021685-071 33 45 1
1021685-072 33 -45A 1
1021685-101 39 70 1
1021685-102 39 -70A 1
1021685-111 35 90 1
1021685-115 33 95 1
1021685-117 33 80 1
1021685-121 33 100 1
1021685-123 33 105 1
1021685-137 32 5 1
1021685-143 31 10 1
1021685-159 33 60 2
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1021685-160 33 -60A 2
1021685-169 38 35 1
1021685-173 38 20 1
1021685-193 33 120 1
1021685-194 33 -120A 1
1021685-195 34 135 1
1021685-195 36 95 1
1021685-261 34 145 1
1021685-261 36 105 1
1021685-263 34 50 1
1021685-267 34 110 1 Gutierrez
1021685-269 34 20 1
1021685-269 34 80 1
1021685-305ZYN 33 140 1
1021685-330FCJ 30 5 1
1021685-351FCJ 30 30 1
1021685-351FCJ 36 15 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10016
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
1021685-352FCJ 30 30A 1
1021685-352FCJ 36 -15A 1
1021685-398FCJ 30 10 1
1021685-403 30 145A 1
1021685-411 30 145 1
1021685-653 33 15 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

1021685-661 30 90 1
1021685-662 30 90A 1
1021685-663 30 80 1
1021685-664 30 80A 1
1021685-665 30 95 1
1021685-666 30 95A 1
1021685-677 38 5 1
1021685-678 38 -5A 1
1021685-758 32 -45 1
1021685-793 35 5 1
1021685-793 37 5 1
1021685-793 38 -1 RF
1021685-794 35 -5A 1
1021685-794 37 -5A 1
1021685-794 38 -1A RF
1021686-005 32 -45A 1
1021686-131 34 150 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1021686-131 36 110 1
1021687-109 36 125 1
1021694-147 5 170 1
1021695-107 6 80 1
1021697-107 5 40 1
1021698-307DSX 4 5 1
1021700-051 7 25 1
1021700-053 7 55 1
1021700-055 7 95 1
1021700-057 7 140 1
1021700-063FQ13 6 120 1
Gutierrez
1021700-063FQ13 7 -1 RF
1021700-064FQ13 6 125 1
1021700-064FQ13 7 -1A RF
1021700-065 5 105 1
1021700-066 5 135 1
1021700-067 5 55 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10017
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
1021700-068 5 80 1
1021700-071 4 25 1
1021700-075 3 45 1
1021700-101 7 50 1
1021700-103 7 85 1
1021700-105 7 135 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

1021700-107 7 175 1
1021700-109 7 180 1
1021700-110 7 -180A 1
1021700-111 5 130 1
1021700-112 5 -160 1
1021700-113 5 65 1
1021700-114 5 90 1
1021700-115 5 75 1
1021700-116 5 100 1
1021700-117 6 70 1
1021700-123 6 20 1
1021700-124 6 40 1
1021700-125 7 130 2
1021700-125 7 170 1
1021700-127 4 35 1
1021700-131 6 65 1
1021700-151 3 -55 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1021700-171 4 110 1
1021700-303ZZM 6 95 4
1021700-305ZYC 5 20 1
1021700-307DSX 7 -15A 1
1021700-308DSX 7 15 1
1021700-309DSX 7 -5A 1
1021700-310DSX 7 5 1
1021700-311DSX 7 -90A 1
1021700-312DSX 7 90 1
1021700-325ZWA 3 95 1
1021700-326ZWA 3 105 1 Gutierrez
1021700-327ZWA 3 5 1
1021980-019 43 25 2
1021980-019 45 -1 RF
1021981-051 43 -5A 1
1021981-051 43 10 1
1021981-051 44 -1 RF
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10018
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
1021981-052 43 5 1
1021981-052 43 -10A 1
1021981-052 44 -1A RF
1021981-063 43 -30A 1
1021981-063 43 35 1
1021981-063 44 -1B RF

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

1021981-064 43 30 1
1021981-064 43 -35A 1
1021981-064 44 -1C RF
1021981-301 44 5 1
1021984-007 1 -80 2
1021984-007 8 5 RF
1021984-007 10 -1 RF
1021985-107 10 15 1
1021986-057 10 20 1
1021989-057 10 5 1
1021990-053 10 25 1
1021990-054 10 30 1
1021990-061 9 25 1
1021990-063 9 30 1
1021990-109 9 5 1
1022492-081 16 150 1
1022492-081 17 -1 RF
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1022492-082 16 -150A 1
1022492-082 17 -1A RF
1022492-083 16 145 1
1022492-083 17 -1B RF
1022492-084 16 -145A 1
1022492-084 17 -1C RF
1022492-085 16 150B 1
1022492-085 17 -1D RF
1022492-086 16 -150C 1
1022492-086 17 -1E RF
1022492-087 16 145B 1
Gutierrez
1022492-087 17 -1F RF
1022492-088 16 -145C 1
1022492-088 17 -1G RF
1022492-107 15 20 1
1022492-109 15 55 1
1022492-119 16 155 2
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10019
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
1022492-121 16 160 2
1022492-125 15 15 1
1022492-125 15 50 1
1022492-131 17 30B 1
1022492-132 17 -30C 1
1022492-141 17 5 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

1022492-143 17 -5A 1
1022492-155 17 30 1
1022492-156 17 -30A 1
1022492-301ZYC 8 25 1
1022493-051 44 30 1
1022493-052 44 -30A 1
1022493-063 44 30B 1
1022493-064 44 -30C 1
1022493-151 44 40 1
1022493-153 44 40A 1
1023851-027MS02 21 160 1
1023851-027MS02 23 -1 RF
1023851-029MS02 21 165 1
1023851-029MS02 23 -1A RF
1023851-111 23 5 1
1023851-112 23 -5A 1
1023851-113 23 15 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1023851-114 23 -15A 1
1023851-115 23 10 1
1023851-116 23 -10A 1
1023851-323BWC 23 60 1
1023851-324BWC 23 -60A 1
1025664-317 16 170 1
1025665-047 16 140 1
1025665-048 16 -140A 1
1025665-057 16 140B 1
1025665-058 16 -140C 1
1027368-711 (NP) 1 -70 4 Gutierrez
1027368-711 (NP) 8 -1 RF
1027368-725 (NP) 1 -90 2
1027368-725 (NP) 12 -1 RF
1027368-733 (NP) 19 -1 RF
1027368-733 (NP) 1 -165 1
1027368-741 (NP) 1 -200 2
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10020
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
1027368-741 (NP) 29 -1 RF
1027368-745 (NP) 1 -75 2
1027368-745 (NP) 9 -1 RF
1027368-759 (NP) 1 -120 2
1027368-759 (NP) 14 -3 RF
1027368-765 (NP) 20 -1 RF

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

1027368-765 (NP) 1 -175 1
1027368-791 (NP) 27 -1 RF
1027368-791 (NP) 1 -185 2
1027369-703 (NP) 1 -130 2
1027369-703 (NP) 15 -1 RF
1027369-705 (NP) 1 -135 2
1027369-705 (NP) 15 -1A RF
1027369-707 (NP) 1 -140 2
1027369-707 (NP) 15 -2 RF
1027369-715 (NP) 1 -105 2
1027369-715 (NP) 14 -1 RF
1027371-753MS08 1 -180 1
1027371-753MS08 20 5 RF
1027371-753MS08 21 -1 RF
1027372-021 25 20 1
1027372-041 23 -35A 2
1027372-047MS02 21 275 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1027372-047MS02 25 -1 RF
1027372-051MS02 21 115 1
1027372-065 26 25 1
1027372-066 26 45 1
1027372-071MS08 21 5 2
1027372-073MS08 21 40 1
1027372-075 23 35 2
1027372-107 26 15 1
1027372-115 26 105 1
1027372-119 26 95 1
1027372-203 21 90 1
Gutierrez
1027372-221 23 45 1
1027372-227 21 125 1
1027372-231 19 60 1
1027372-307DSX 25 5 1
1027372-311FCJ 24 35 1
1027372-312FCJ 24 45 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10021
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
1027372-317FCJ 24 55 1
1027372-337ZWZ 23 55 1
1027372-347FCJ 24 65 1
1027372-359ZWZ 23 -55A 1
1027372-371FCJ 21 15 1
1027372-373FCJ 24 25 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

1027372-381DTF 25 40 1
1027372-393DV0 (REF) 41 75 1
1027372-401 21 -290 1
1027372-641 25 45 1
1027372-651 21 25 1
1027372-653 21 105 1
1027372-655 21 145 1
1027372-656 21 135 1
1027372-751MS02 21 210 1
1027372-751MS02 24 -1 RF
1027877-107 28 145 1
1027877-117 28 -145A 1
1027879-051 28 75 1
1027879-052 28 -75A 1
1027888-123 28 120 1
1027888-151 28 110 1
1027888-152 28 -110A 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1027888-303ZWZ 28 130 1
1027900-057MS02 1 -190A 1
1027900-057MS02 27 5 RF
1027900-057MS02 28 -1 RF
1027900-058MS02 1 190 1
1027900-058MS02 27 -5A RF
1027900-058MS02 28 -1A RF
1027900-067MS02 1 195 1
1027900-067MS02 27 -5B RF
1027900-067MS02 28 -1B RF
1027900-068MS02 1 -195A 1 Gutierrez
1027900-068MS02 27 -5C RF
1027900-068MS02 28 -1C RF
1027989-057 28 100 1
1027989-058 28 -100A 1
1027989-067 28 -100B 1
1027989-068 28 -100C 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10022
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
1028283-651 19 65 1
1028283-652 19 70 1
1028285-047 16 125 1
1028285-048 16 -125A 1
1028285-059 16 125B 1
1028285-060 16 -125C 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

1028296-007 1 -145A 1
1028296-007 1 150 1
1028296-007 15 5 RF
1028296-007 16 -1 RF
1028296-008 1 145 1
1028296-008 1 -150A 1
1028296-008 15 -5A RF
1028296-008 16 -1A RF
1029716-057 16 130 1
1029723-057 6 5 1
1029724-057FQ13 4 135 1
1029724-057FQ13 6 -1 RF
1029725-057 5 5 1
1029944-003 1 -250 1
1030130-301ZXK 36 115 1
1030130-303ZXK 34 155 1
1030486-119 39 30 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1031728-065 19 45 1
1031728-083MS02 1 -170 1
1031728-083MS02 19 5 RF
1031754-107 33 70 1
1031754-108 33 -70A 1
1031754-137 28 20 1
1031754-139 28 30 1
1032569-077FQ14 1 -95 2
1032569-077FQ14 12 5 RF
1035657-141 16 20 1
1035657-142 16 25 1
Gutierrez
1035657-201 16 5 1
1035657-202 16 10 1
1040065-017 1 -125 2
1040065-017 14 40 RF
1040627-309DTF 21 170 1
1040627-310DTF 21 185 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10023
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
1040966-317ZYN 41 15 2
1040966-355FCJ 24 5 1
1040966-356FCJ 24 15 1
1041035-331DV0 (REF) 41 30 2
1041736-007 1 45 2
1041737-007 1 15 2

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

1041738-007 1 35 2
1042484-107 16 35 1
1045427-337DV0 (REF) 41 5 2
1045594-077 1 25 2
1046962-303FCI 30 140 1
1047795-051 30 70 1
1047795-052 30 70A 1
1048430-001MS02 30 125 1
1048430-024MS02 30 125A 1
1048456-007 1 -110 2
1048456-007 14 5 RF
1048457-107 14 20 1
1048458-107 14 25 1
1049930-337 1 -240 2
1049930-339 1 -235A 1
1049930-341 1 -235 1
1049941-105 26 65 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1049941-106 26 80 1
1049965-301DTE 25 50 1
1050090-301DTE 19 75 1
1050092-301DTE 19 30 1
1050092-302DTE 19 35 1
1050222-151 35 40 1
1050222-151 37 40 1
1050222-152 35 -40A 1
1050222-152 37 -40A 1
1050222-305FCJ 36 65 1
1050222-306FCJ 36 -65A 1 Gutierrez
1050222-363FCJ 36 35 1
1050222-364FCJ 36 -35A 1
1050222-369FCJ 36 45 1
1050222-370FCJ 36 -45A 1
1050222-451 35 35 1
1050222-451 37 35 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10024
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
1050223-165 39 85 1
1050223-166 39 -85A 1
1050253-301DTE 21 155 1
1050914-359DV0 (REF) 41 60 1
1052040-007 26 120 1
1052089-055FQ13 21 300 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

1052089-055FQ13 26 -1 RF
1052184-105 23 20 1
1053686-087 16 85 1
1053775-201 26 -130 1
1053775-301FCJ 24 75 1
1054903-302FCI 30 140A 1
1054904-051 32 -50 1
1055300-053 21 235 1
1055304-001 21 240 1
1057208-101 45 25 1
1057208-103 45 30 2
1058817-105 35 45 1
1058817-105 37 45 1
1058817-107 33 35 1
1059281-057 30 105 1
1059281-057 31 -1 RF
1059281-062 30 105A 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1059281-062 31 -1A RF
1059281-103 3 80 1
1059281-103 4 75 1
1059281-105 32 20 1
1059281-161 31 5 1
1059281-162 31 -5A 1
1059281-165 31 35 1
1059281-172 31 -35A 1
1059731-101 33 130 1
1059800-005 4 55 1
1059800-007 3 60 1
Gutierrez
1059800-103 4 60 1
1059800-105 4 85 1
1059800-113 3 65 1
1059800-121 3 90 1
1060340-051MS08 30 20 1
1060340-051MS08 36 5 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10025
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
1060340-052MS08 30 20A 1
1060340-052MS08 36 -5A 1
1060340-053MS08 30 45 1
1060340-053MS08 36 30 1
1060340-054MS08 30 45A 1
1060340-054MS08 36 -30A 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

1060355-003 32 -40A 1
1060355-003 33 -1 RF
1060355-004 32 40 1
1060355-004 33 -1A RF
1060357-781 32 -35A 1
1060357-788 32 35 1
1060358-003 33 5 1
1060358-003 34 -1 RF
1060358-004 33 -5A 1
1060358-004 34 -1A RF
1060363-081 35 20 1
1060363-081 37 20 1
1060363-082 35 -20A 1
1060363-082 37 -20A 1
1060363-091MS02 36 55 1
1060363-092MS02 36 -55A 1
1060363-095MS02 30 50 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1060363-096MS02 30 50A 1
1060363-097MS02 30 60 1
1060363-098MS02 30 60A 1
1060363-119 35 65 1
1060363-120 35 -65A 1
1060364-001 35 110 1
1060364-001 39 -1 RF
1060364-002 35 -110A 1
1060364-002 39 -1A RF
1060364-005 37 75 1
1060364-005 39 -1B RF Gutierrez
1060364-006 37 -75A 1
1060364-006 39 -1C RF
1060365-001 35 55 1
1060365-002 35 -55A 1
1060368-001 36 80 1
1060368-002 36 -80A 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10026
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
1060369-009 34 160 1
1060369-009 35 -1 RF
1060369-010 34 -160A 1
1060369-010 35 -1A RF
1060369-013 36 135 1
1060369-013 37 -1 RF

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

1060369-014 36 -135A 1
1060369-014 37 -1A RF
1060372-051MS08 1 210 1
1060372-051MS08 29 5 RF
1060372-051MS08 36 -1 RF
1060372-052MS08 1 -210A 1
1060372-052MS08 29 -5A RF
1060372-052MS08 36 -1A RF
1060694-051 39 100 1
1060694-052 39 -100A 1
1060694-055 39 100B 1
1060694-056 39 -100C 1
1060695-051 35 95 1
1060695-052 35 -95A 1
1060695-055 37 55 1
1060695-056 37 -55A 1
1060733-014 30 165A 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1060733-014 32 -1 RF
1060733-781 30 165 1
1060733-781 32 -1A RF
1061299-209 15 25 1
1061299-209 15 60 1
1061798-061MS02 40 65 1
1061798-062MS02 40 -65A 1
1061798-069 40 85 1
1061798-070 40 -85A 1
1061798-307DV0 (REF) 40 70 1
1061798-308DV0 (REF) 40 -70A 1
Gutierrez
1061798-309DV0 (REF) 40 90 1
1061798-310DV0 (REF) 40 -90A 1
1061798-711MS02 (NP) 40 60 1
1061798-712MS02 (NP) 40 -60A 1
1061905-003 (NP) 42 -1 RF
1061905-003 (NP) 1 -225 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10027
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
1061905-004 (NP) 42 -1A RF
1061905-004 (NP) 1 -225A 1
1061964-319ZYN 41 45 1
1062416-135 42 25 1
1062416-136 42 -25A 1
1062416-137 42 5 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

1063309-011 21 250 1
1063309-039FQ13 26 5 1
1063309-111 21 -260 1
1063309-113 21 -265 1
1063550-001MS02 21 225 1
1063561-101 43 55 2
1064524-307DV0 (REF) 40 35 1
1064529-053MS02 40 30 1
1067131-057 16 130A 1
1071964-055MS02 40 5 1
1071964-057MS02 40 -5A 1
1071964-311DV0 (REF) 41 70 1
1071964-313DV0 (REF) 40 25 1
1071964-314DV0 (REF) 40 -25A 1
1076689-065MS08 1 -205A 1
1076689-065MS08 29 -10 RF
1076689-065MS08 30 -1 RF
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1076689-076MS08 1 205 1
1076689-076MS08 29 -10A RF
1076689-076MS08 30 -1A RF
1076691-041 (NP) 30 -170 1
1076691-058 (NP) 30 -170A 1
1081489-351ZXK 16 70 1
1081489-352ZXK 16 75 1
1089825-101 42 -45 1
1096327-057FQ14 1 -115 2
1096327-057FQ14 14 30 RF
1097108-701 (NP) 18 -5 1 Gutierrez
1097108-703 (NP) 18 -5A 1
1097108-705 (NP) 18 -5B 1
1097108-707 (NP) 18 -5C 1
1097109-701MS02 (NP) 40 -1 RF
1097109-701MS02 (NP) 1 -215 1
1097109-703MS02 (NP) 40 -1A RF
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10028
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
1097109-703MS02 (NP) 1 -215A 1
1097110-701MS02 (NP) 41 -1 RF
1097110-701MS02 (NP) 1 -220 1
1097110-703MS02 (NP) 41 -1A RF
1097110-703MS02 (NP) 1 -220A 1
1097111-705 (NP) 18 -190 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

1097112-701 (NP) 1 -160B RF
1097112-703 (NP) 1 -160C RF
1097112-705 (NP) 1 -160 RF
1097112-707 (NP) 1 -160A RF
1097452-701 (NP) 18 -1 RF
1097452-701 (NP) 1 -155B 1
1097452-703 (NP) 18 -1A RF
1097452-703 (NP) 1 -155C 1
1097452-705 (NP) 18 -1B RF
1097452-705 (NP) 1 -155 1
1097452-707 (NP) 18 -1C RF
1097452-707 (NP) 1 -155A 1
1116000 (NP) 1 -260 RF
11528 35 85 2
11528 35 105 1
11528 37 70 1
11528 39 65 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1170821-44 30 -175 1
1180645-773 (NP) 1 -60 2
1180645-773 (NP) 3 -1 RF
1191-46 18 -20 1
1191810-44 18 -25 1
1191811-44 18 -30 1
12-11017-11 11 10 2
12-6-1 46 5 2
12-99-1026 46 10 2
1294-2-2 18 -10 1
1295-2-118 18 -15 2
Gutierrez
1297168-107HDZ 1 30 2
1297168-117HEA 1 -40A 2
1297168-127HEA 1 40 2
1297168-137HEA 1 10 2
1297168-807HEA 1 -50 2
1297168-907HEA 1 20 2
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10029
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
1299854-101011 18 -35A 1
1299855-101011 18 -35 1
1327240-007 1 -145C 1
1327240-007 1 -150B 1
1327240-007 15 -5B RF
1327240-007 16 -1B RF

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

1327240-008 1 -145B 1
1327240-008 1 -150C 1
1327240-008 15 -5C RF
1327240-008 16 -1C RF
1367862 (NP) 1 -265 RF
1367870-005MS08 1 -1 RF
1367870-008MS08 1 -1A RF
1367870-101MS08 1 -1B RF
1367870-104MS08 1 -1C RF
1401445-025 18 -150A 1
1401445-033 18 -145 1
1401445-045 18 -150 1
2SRS9XMUU375 (REF) 39 75A 1
2SRS9XMUU400 (REF) 39 75 1
20-008 5 70 1
20-008 5 -95 1
2162-1-111-2396 1 5 2
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

2500210-003 11 5 1
2500210-051 46 -1 1
27SR0012 21 220 14
27SR0012 24 10 4
27SR0012 24 -20 4
27SR0012 24 30 4
27SR0012 24 40 4
27SR0012 24 -50 4
27SR0012 24 60 1
27SR0012 24 -70 1
27SR0012WHITE (REF) 22 40 1 Gutierrez
27SR0018 21 20 7
27SR0018 21 -195 2
27SR0018 21 180 2
27SR0018 30 35 14
27SR0018 36 20 14
27SR0018WHITE (REF) 21 175 8
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10030
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
27SR0018WHITE (REF) 21 -190 8
27SR0020 36 40 8
27SR102190 28 95 4
27SR1600315 3 10 4
27SR1600315 3 100 2
27SR1600315 3 110 2

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

27SR1600315 4 15 4
27SR1600315 7 10 2
27SR1600315 19 15 2
27SR1600315 36 50 6
27SR1600315 36 60 1
27SR1600315 36 70 4
27SR1600315 30 55 2
27SR2000370 30 130 10
27SR2000370 30 130A 9
27SR2000370 30 150 5
27SR2000370 30 150A 4
2700 20 15 2
3M425100ALUM 1 -255 AR
3M5958-1 18 -155 AR
3M5958-1 30 160 AR
3M5958-1 40 -15 AR
3M5958-1 40 -120 AR
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

3M5958-1 41 -25 AR
3M5958-1 41 40 AR
3M5958-1 41 -55 AR
3M5958-1 41 80 AR
3M5958-1 2 50 AR
3M9485PC050 (REF) 30 155 AR
3M9485PC050 (REF) 36 -25 AR
3M9485PC050 (REF) 36 -75 AR
3M9485PC050 (REF) 30 -40 AR
3M9485PC050 (REF) 21 295 AR
301344-1 35 50 1
Gutierrez
301344-1 37 50 1
409615 21 100 1
42NKE048 (REF) 7 120 1
42NKE048 (REF) 7 160 1
42NKE048 (REF) 40 105 3
42NKE048 (REF) 45 65 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10031
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

PART NUMBER AIRLINE PART NO. IPL FIG. ITEM TTL REQ
43-13-1-24 40 45 4
44960029 18 -195 2
44960101 30 -205 2
44960103 18 -200 1
47000283 28 10 2
52NKE064 (REF) 45 50 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

52NKTE048 (REF) 3 135 2
52NKTE048 (REF) 3 170 2
52NKTE054 (REF) 3 25 1
5304-25 9 10 1
5304-25 16 165 2
5672500572 18 -160 AR
5672500572 18 -210 AR
5672500572 30 -195 AR
5672500872 18 -165 AR
5672500872 18 -205 AR
5672500872 30 -200 AR
5672501372 18 -170 AR
5710-55-30 8 15 1
82-19-220-16 40 40 4
82-32-201-20 40 55 4
82-46-101-41 40 50 4
98038007 7 30 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

98038007 7 60 2
98038073 3 130 2
98038073 3 150 2
98038115 45 45 2
98038241 40 100 10
98038267 7 115 1
98038335 5 25 1
98038389 4 40 1

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10032
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10033
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

30
35

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

150

40
45
30
35

145

195

40
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

45

210

10
15
190 25
20
65
5
10 Gutierrez
15
25
20
205
65

Seat Assembly - Double

IPL Figure 1

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10034
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
1
-1 1367870-005MS08 Seat Assembly - LH Double, Last Row, A RF
Legrest, Passenger Computer Power,
Dual Emergency Escape Path Light
-1A 1367870-008MS08 Seat Assembly - RH Double, Last Row, B RF
Legrest, Passenger Computer Power

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

-1B 1367870-101MS08 Seat Assembly - LH Double, F/R, Legrest, C RF
Passenger Computer Power, Dual,
Emergency Escape Path Light
-1C 1367870-104MS08 Seat Assembly - RH Double, F/R, D RF
Legrest, Passenger Computer Power

5 2162-1-111-2396 • Lap Belt Assembly (AmSafe®) 2

(Refer to INTRODUCTION Page Block
of this CMM for Vendor Contact
Information)

10 1297168-137HEA • Cover Assembly - Bottom Legrest 2

15 1041737-007 • Cushion Assembly - Bottom 2

20 1297168-907HEA • Cover Assembly - Foot Paddle 2

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

25 1045594-077 • Cushion Assembly - Legrest Foot 2

30 1297168-107HDZ • Cover Assembly - Headrest 2

35 1041738-007 • Cushion Assembly - Headrest 2

40 1297168-127HEA • Cover Assembly - Back, Last Row AB 2

-40A 1297168-117HEA • Cover Assembly - Back CD 2
Gutierrez

45 1041736-007 • Cushion - Backrest 2

-50 1297168-807HEA • Cover Assembly - Literature Pocket CD 2

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10035
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
1
-55 1021567-049 (NP) • Cable Routing - STD, DBL 1
(See IPL FIG 2 for DET BKDN)

-60 1180645-773 (NP) • Installation - Legrest, 47 Degree 2

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Rotation
(See IPL FIG 3 for DET BKDN)
65 1021547-027FQ13 • Legrest Assembly 2
(See IPL FIG 4 for DET BKDN)

-70 1027368-711 (NP) • Installation - Seatpan Assembly 4

(See IPL FIG 8 for DET BKDN)
-75 1027368-745 (NP) • Installation - Seatpan Support, DBL 2
Strap
(See IPL FIG 9 for DET BKDN)
-80 1021984-007 • Seatpan Assembly 2
(See IPL FIG 10 for DET BKDN)

-85 1021569-003 • Headrest Frame Assembly 2

(See IPL FIG 11 for DET BKDN)

-90 1027368-725 (NP) • Installation - Video Bezel CD 2

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(See IPL FIG 12 for DET BKDN)

-95 1032569-077FQ14 • Upper Literature Pocket Assembly - CD 2
Bonded, No Coat Hook
(See IPL FIG 12 for DET BKDN)

-100 1016258-099 (NP) • Installation - Coat Hook 2

(See IPL FIG 13 for DET BKDN)

-105 1027369-715 (NP) • Installation - Lower Literature Assembly CD 2

(See IPL FIG 14 for DET BKDN)
-110 1048456-007 • Lower Literature Assembly CD 2 Gutierrez
(See IPL FIG 14 for DET BKDN)
-115 1096327-057FQ14 • Lower Literature Pocket Assembly CD 2
(See IPL FIG 14 for INSTL Details)

-120 1027368-759 (NP) • Installation - Back Trim CD 2

(See IPL FIG 14 for DET BKDN)
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10036
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
1
-125 1040065-017 • Back Trim - Riveted CD 2
(See IPL FIG 14 for INSTL Details)

-130 1027369-703 (NP) • Installation - Back Assembly, Non-Lock 2

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Side
(See IPL FIG 15 for DET BKDN)
-135 1027369-705 (NP) • Installation - Back Assembly, Lock Side 2
(See IPL FIG 15 for DET BKDN)
-140 1027369-707 (NP) • Installation - Back Assembly, Backlash 2
Screw
(See IPL FIG 15 for DET BKDN)
145 1028296-008 • Back Assembly - Riveted, W/ Bolster, A 1
Last Row (INBD)
(See IPL FIG 16 for DET BKDN)
-145A 1028296-007 • Back Assembly - Riveted, W/ Bolster, B 1
Last Row (INBD)
(See IPL FIG 16 for DET BKDN)
-145B 1327240-008 • Back Assembly - Riveted, W/ Bolster, C 1
HIC (INBD)
(See IPL FIG 16 for DET BKDN)
-145C 1327240-007 • Back Assembly - Riveted, W/ Bolster, D 1
HIC (INBD)
(See IPL FIG 16 for DET BKDN)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

150 1028296-007 • Back Assembly - Riveted, W/ Bolster, A 1

Last Row (OUTBD)
(See IPL FIG 16 for DET BKDN)
-150A 1028296-008 • Back Assembly - Riveted, W/ Bolster, B 1
Last Row (OUTBD)
(See IPL FIG 16 for DET BKDN)
-150B 1327240-007 • Back Assembly - Riveted, W/ Bolster, C 1
HIC (OUTBD)
(See IPL FIG 16 for DET BKDN)
-150C 1327240-008 • Back Assembly - Riveted, W/ Bolster, D 1
HIC (OUTBD)
(See IPL FIG 16 for DET BKDN)
Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10037
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
1
-155 1097452-705 (NP) • Installation - Electrical, LH Last Row, A 1
DBL
(See IPL FIG 18 for DET BKDN)

(See SCHEMATIC AND WIRING

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

DIAGRAMS [Page Block 2000])

(See USING 3D ELECTRICAL

DRAWINGS [Page Block 17000])
(3D PDF Electrical Installation Drawing
[Available Upon Request])
-155A 1097452-707 (NP) • Installation - Electrical, RH Last Row, B 1
DBL
(See IPL FIG 18 for DET BKDN)
(See SCHEMATIC AND WIRING
DIAGRAMS [Page Block 2000])

(See USING 3D ELECTRICAL

DRAWINGS [Page Block 17000])

(3D PDF Electrical Installation Drawing

[Available Upon Request])
-155B 1097452-701 (NP) • Installation - Electrical, LH F/R, DBL C 1
(See IPL FIG 18 for DET BKDN)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(See SCHEMATIC AND WIRING

DIAGRAMS [Page Block 2000])
(See USING 3D ELECTRICAL
DRAWINGS [Page Block 17000])
(3D PDF Electrical Installation Drawing
[Available Upon Request])
-155C 1097452-703 (NP) • Installation - Electrical, RH F/R, DBL D 1
(See IPL FIG 18 for DET BKDN)

(See SCHEMATIC AND WIRING

DIAGRAMS [Page Block 2000])
Gutierrez
(See USING 3D ELECTRICAL
DRAWINGS [Page Block 17000])

(3D PDF Electrical Installation Drawing

[Available Upon Request])

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10038
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
1
-160 1097112-705 (NP) • Installation - 3D Electrical, LH Last A RF
Row, DBL

(See USING 3D ELECTRICAL

DRAWINGS [Page Block 17000])

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(3D PDF Electrical Installation Drawing
[Available Upon Request])
-160A 1097112-707 (NP) • Installation - 3D Electrical, RH Last B RF
Row, DBL

(See USING 3D ELECTRICAL

DRAWINGS [Page Block 17000])

(3D PDF Electrical Installation Drawing

[Available Upon Request])
-160B 1097112-701 (NP) • Installation - 3D Electrical, LH F/R, DBL C RF

(See USING 3D ELECTRICAL

DRAWINGS [Page Block 17000])
(3D PDF Electrical Installation Drawing
[Available Upon Request])
-160C 1097112-703 (NP) • Installation - 3D Electrical, RH F/R, D RF
DBL
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(See USING 3D ELECTRICAL

DRAWINGS [Page Block 17000])

(3D PDF Electrical Installation Drawing

[Available Upon Request])

-165 1027368-733 (NP) • Installation - Lower Console 1

(See IPL FIG 19 for DET BKDN)
-170 1031728-083MS02 • Rear Panel Assembly - PC Power 1
(See IPL FIG 19 for DET BKDN)

-175 1027368-765 (NP) • Installation - Center Console, Black 1

Plug Gutierrez
(See IPL FIG 20 for DET BKDN)
-180 1027371-753MS08 • Console Assembly - Non-Video 1
(See IPL FIG 21 for DET BKDN)

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10039
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
1
-185 1027368-791 (NP) • Installation - Foodtray 2
(See IPL FIG 27 for DET BKDN)
190 1027900-058MS02 • Foodtray Assembly - Tablet (INBD) AC 1
(See IPL FIG 28 for DET BKDN)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

-190A 1027900-057MS02 • Foodtray Assembly - Tablet (INBD) BD 1
(See IPL FIG 28 for DET BKDN)
195 1027900-067MS02 • Foodtray Assembly - Special, LH AC 1
(OUTBD)
(See IPL FIG 28 for DET BKDN)
-195A 1027900-068MS02 • Foodtray Assembly - Special, RH BD 1
(OUTBD)
(See IPL FIG 28 for DET BKDN)

-200 1027368-741 (NP) • Installation - Endbay 2

(See IPL FIG 29 for DET BKDN)
205 1076689-076MS08 • Endbay Assembly - IUL (INBD) AC 1
(See IPL FIG 30 for DET BKDN)
-205A 1076689-065MS08 • Endbay Assembly - IUL (INBD) BD 1
(See IPL FIG 30 for DET BKDN)
210 1060372-051MS08 • Endbay Assembly - Wall, Special AC 1
(OUTBD)
(See IPL FIG 36 for DET BKDN)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

-210A 1060372-052MS08 • Endbay Assembly - Wall, Special BD 1

(OUTBD)
(See IPL FIG 36 for DET BKDN)

-215 1097109-701MS02 (NP) • Installation - Shroud, LH, DBL AC 1

(See IPL FIG 40 for DET BKDN)
-215A 1097109-703MS02 (NP) • Installation - Shroud, RH, DBL BD 1
(See IPL FIG 40 for DET BKDN)
-220 1097110-701MS02 (NP) • Installation - Raceway, LH AC 1
(See IPL FIG 41 for DET BKDN)
-220A 1097110-703MS02 (NP) • Installation - Raceway, RH BD 1
(See IPL FIG 41 for DET BKDN) Gutierrez

-225 1061905-003 (NP) • Installation - Baggage Bar AC 1

(See IPL FIG 42 for DET BKDN)
-225A 1061905-004 (NP) • Installation - Baggage Bar BD 1
(See IPL FIG 42 for DET BKDN)
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10040
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
1
-230 1021505-057 • Frame Assembly - DBL AC 1
(See IPL FIG 43 for DET BKDN)
-230A 1021505-058 • Frame Assembly - DBL BD 1
(See IPL FIG 43 for DET BKDN)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

-235 1049930-341 • Placard - Console Last Row AB 1
“Fasten Seat Belt While Seated
Life Jacket Under Your Seat”

(See DESCRIPTION AND

OPERATION Section for Location
Details)
-235A 1049930-339 • Placard - Console CD 1
“During Taxi, Takeoff & Landing,
No Stowage in Center Console,
Raise & Latch Aisle Armrest
Life Jacket Under Center Console
Fasten Seat Belt While Seated”

(See DESCRIPTION AND

OPERATION Section for Location
Details)
-240 1049930-337 • Placard - Safety W/ Divider CD 2
“Literature Only”
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(See DESCRIPTION AND

OPERATION Section for Location
Details)

-245 1002933-029 (NP) • Nameplate - TSO Tag, RFID, Boeing 1

-250 1029944-003 • • RFID - TEGO Flexible Tag - Large 1
-255 3M425100ALUM • • 3M™ Aluminum Tape 425, 1.0'' AR
(Order Separately)

-260 1116000 (NP) • Basic Dimension Drawing - Virgin RF

Australia Airlines B737-8 MiQ™ Gutierrez

-265 1367862 (NP) • Envelope Drawing - Virgin Australia RF

Airlines B737-8 MAX MiQ™

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10041
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
1
-270 CA7V0Z737-8 (NP) Astronics Block Diagram - Virgin Australia RF
Airlines B737-8 MiQ™
(True P/N is CA7/VOZ 737-8)
(Refer to Envelope Drawing 1367862)
(Refer to INTRODUCTION Page Block of

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

this CMM for Vendor Contact Information)
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10042
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10043
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

15

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

10

45
40
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

20
25 15
30

10

Gutierrez
15

10

Cable Routing
IPL Figure 2 (Sheet 1 of 4)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10044
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

25

20 30
45

40

35

15 (REF) 10 (REF)

20
25
30

20
45
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

40

50

20
25
30
10 (REF) 15 (REF)

Gutierrez

Cable Routing
IPL Figure 2 (Sheet 2 of 4)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10045
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

20
25
30 20
25
30

25

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

25
40 40
45 45
50 50
20
25
30
20 20
30 35
25 25
30 30
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez
15 (REF)
5 (REF)

10 (REF)

Cable Routing
IPL Figure 2 (Sheet 3 of 4)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10046
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 (REF)

10 (REF)

15 (REF)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Cable Routing
IPL Figure 2 (Sheet 4 of 4)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10047
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10048
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
2
-1 1021567-049 (NP) Cable Routing RF
(See IPL FIG 1 for NHA)

5 AC97220-00 • Cable - Recline 2

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(Order Separately)
10 AC97166-00 • Cable - Legrest 2
(Order Separately)
15 AC97164-00 • Cable - Foot Paddle 2
(Order Separately)
ATTACHING PARTS
20 MS3367-4-9 • Strap - Tiedown, Adjustable 10
(Order Separately)
25 MS3367-5-9 • Strap - Tiedown, Adjustable 10
(Order Separately)
30 CR2 • Connector Ring 6
(Order Separately)
35 PUM049-30 (REF) • Mount - Push, Umbrella 2
(Order Separately by True P/N
PUM-049-_30)
40 MS3367-7-9 • Strap - Tiedown, Adjustable 4
(Order Separately)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

45 CSCS • Cable Spacer - Cross 4

(Order Separately)
50 3M5958-1 • 3M™ Tape - Double Sided AR
(Order Separately)
* * *

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10049
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

15

40

35
115
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

35
Gutierrez
10 40
10
10
30 60

Installation - Legrest
IPL Figure 3 (Sheet 1 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10050
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

65

75

85

90
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

80

70

1059800-007
VALVE RELEASE
Gutierrez

Installation - Legrest
IPL Figure 3 (Sheet 2 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10051
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FRONT TUBE
110
ASSEMBLY - SEATPAN
(REF)
120

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

130
155
135
25
135
165 20 130

105 140
120

150
165
160 170 160
155

125
45 150 140

145 95
100
15 (REF)
125
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

145

Gutierrez
115 (REF)

Installation - Legrest
IPL Figure 3 (Sheet 3 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10052
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
3
-1 1180645-773 (NP) Installation - Legrest RF
(See IPL FIG 1 for NHA)

5 1021700-327ZWA • Shroud - Legrest 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(Order Separately)
ATTACHING PARTS
10 27SR1600315 • Rivet - Snap 4
(Order Separately)
* * *

15 X0N0XK3-044-27 (REF) • Gas Spring - Lockable 1

(Order Separately by True P/N
X0N0XK3-044-275--001/300N)
ATTACHING PARTS
20 AN5-6A • Bolt - HEX HD 1
(Order Separately)
25 52NKTE054 (REF) • Nut - HEX, Nylon Cap 1
(Order Separately by True P/N
52NKTE-054)
30 MS16633-2031 • Ring - Retaining, External 1
(Order Separately)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

35 MS35335-35 • Washer - Lock, External Tooth 2

(Order Separately)
40 AN316-6R • Nut - Jam 2
(Order Separately)
* * *

45 1021700-075 • Rod End Assembly - Press 1

(Order Separately)

-50 GSI0506-04 (REF) • • Bearing - Sleeve, IGUS 1

(True P/N is GSI-0506-04) Gutierrez

-55 1021700-151 • • Rod End - Cylinder 1

60 1059800-007 • Valve Release 1

(Order Separately)

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10053
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
3
65 1059800-113 • • Jaw - Top 1
ATTACHING PARTS
70 NAS8602-6 • • Bolt - CSK 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

* * *

75 LC016C13M • • Spring - Helical, Compression 1

80 1059281-103 • • Ferrule - Cable 1

ATTACHING PARTS
85 MS16633-2025 • • Ring - Retaining, External 1
* * *

90 1059800-121 • • Jaw - Bottom 1

95 1021700-325ZWA • Shroud - Fixed, LH 1

(Order Separately)
ATTACHING PARTS
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

100 27SR1600315 • Rivet - Snap 2

(Order Separately)
* * *

105 1021700-326ZWA • Shroud - Fixed, RH 1

(Order Separately)
ATTACHING PARTS
110 27SR1600315 • Rivet - Snap 2
(Order Separately)
* * * Gutierrez

115 1021547-027FQ13 Legrest Assembly RF

(See IPL FIG 1 for NHA)
(See IPL FIG 4 for DET BKDN)
ATTACHING PARTS

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10054
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
3
120 AN4-11A • Bolt - HEX HD 2
(Order Separately)
125 NAS75-4-024 • Bushing - Plain, Press Fit 2
(Order Separately)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

130 98038073 • Spacer - Nylon 2
(Order Separately)
135 52NKTE048 (REF) • Nut - HEX, Nylon Cap 2
(Order Separately by True P/N
52NKTE-048)
140 NAS1801-4-26 • Screw - HEX HD 2
(Order Separately)
145 NAS75-4-024 • Bushing - Plain, Press Fit 2
(Order Separately)
150 98038073 • Spacer - Nylon 2
(Order Separately)
155 MS21042-4 • Nut - LKG 2
(Order Separately)
160 NAS75-4-008 • Bushing - Plain, Press Fit 2
(Order Separately)
165 NAS1149C0432R • Washer - Flat 2
(Order Separately)
170 52NKTE048 (REF) • Nut - HEX, Nylon Cap 2
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(Order Separately by True P/N

52NKTE-048)
* * *

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10055
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

25

30

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

110 45
100 40
95 135

10 90
115 35
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

15

20

15
10

Gutierrez
20
15
15

Legrest Assembly
IPL Figure 4 (Sheet 1 of 5)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10056
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

55

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

50

1021700-071
EXTENSION LOCK ASSEMBLY - LEGREST

Gutierrez

Legrest Assembly
IPL Figure 4 (Sheet 2 of 5)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10057
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

60

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

80

85
70
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

65

1059800-005
VALVE RELEASE - C-CLIP

75
Gutierrez

Legrest Assembly
IPL Figure 4 (Sheet 3 of 5)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10058
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

135
(REF)

105

105
125

105
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

120
105

90 (REF)

125

Gutierrez

Legrest Assembly
IPL Figure 4 (Sheet 4 of 5)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10059
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

135 (REF)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

125

125

125 Gutierrez

Legrest Assembly
IPL Figure 4 (Sheet 5 of 5)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10060
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
4
-1 1021547-027FQ13 Legrest Assembly RF
(See IPL FIG 1 for NHA)

5 1021698-307DSX • Shroud - Legrest, Rear 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

ATTACHING PARTS
10 MS27039-0806 • Screw - Pan HD 2
15 27SR1600315 • Rivet - Snap 4
20 SJ3518FR100B (REF) • 3M™ Loop Tape - Adhesive 100 Black AR
(True P/N is SJ3518FR100BLACK)
* * *

25 1021700-071 • Extension Lock Assembly - Legrest 1

ATTACHING PARTS
30 AN5-5A • Bolt - HEX HD 1
35 1021700-127 • Pin - Pivot 1
40 98038389 • Spacer - Nylon 1
45 MS16633-2025 • Ring - Retaining 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

* * *

50 W0A7KK1033-1 (REF) • • Gas Spring - Lockable 1

(True P/N is
W0A7KK1-033-176--001/300N)
55 1059800-005 • • Valve Release - C-Clip 1

60 1059800-103 • • • Lever Arm - Valve Release 1

ATTACHING PARTS
65 NAS8602-6 • • • Bolt - CSK 1
Gutierrez
* * *

70 LC016C13M • • • Spring - Helical, Compression 1

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10061
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
4
75 1059281-103 • • • Ferrule - Cable 1
ATTACHING PARTS
80 MS16633-2025 • • • Ring - Retaining 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

* * *

85 1059800-105 • • • Head - Valve Release 1

90 1021548-087 • Paddle Assembly - Legrest 1

(See IPL FIG 5 for DET BKDN)
ATTACHING PARTS
95 MS27039-1-10 • Screw - Pan HD 1
(Add Washer and Screw thru Slot, But
do not Tighten Down)
(Torque Washer and Screw Down
Securely into Position)
100 NAS1149G0332P • Washer - Flat 1
(Add Washer and Screw thru Slot, But
do not Tighten Down)
(Torque Washer and Screw Down
Securely into Position)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

105 NAS603-10P • Screw - Pan HD 8

* * *

110 1021700-171 • Pivot Support - Block 1

ATTACHING PARTS
115 MS27039-1-06 • Screw - Pan HD 1
(Torqued to 15-18 IN-LB)
(Torque Side Screw Down Securely
into Position)
* * *
Gutierrez

120 SJ3519FR100B (REF) • 3M™ Hook Tape - Adhesive 100 Black AR

(True P/N is SJ3519FR100BLACK)
125 SJ3518FR200B (REF) • 3M™ Loop Tape - Adhesive 200 Black AR
(True P/N is SJ3518FR200BLACK)
ATTACHING PARTS
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10062
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
4
-130 SD32BS • Rivet - Blind, Pan 4
* * *

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

135 1029724-057FQ13 • Frame Link Assembly 1
(See IPL FIG 6 for DET BKDN)
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10063
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

170

5
40

10
15
20
25 45
30
35
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

50

50

Gutierrez

Paddle Assembly - Legrest

IPL Figure 5 (Sheet 1 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10064
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

165

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

90
135

105

150
85
80 145
100 140
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

55 105 (REF)
60

65

130
75
55 (REF)
70

125

Gutierrez

1021546-057
FOOT PAN ASSEMBLY

Paddle Assembly - Legrest

IPL Figure 5 (Sheet 2 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10065
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10066
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
5
-1 1021548-087 Paddle Assembly - Legrest RF
(See IPL FIG 4 for NHA)

5 1029725-057 • Link Arm Assembly 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

ATTACHING PARTS
10 MS27039-1-08 • Screw - Pan HD 1
15 NAS77-3-019 • Bushing - Flanged, Press Fit 1
20 1021700-305ZYC • Bushing - Cam Flange 1
25 98038335 • Spacer - Nylon 1
30 NAS1149C0332R • Washer - Flat 1
* * *

35 JFI1012-08 (REF) • • Bearing - Flange, IGUS 1

(True P/N is JFI-1012-08)

40 1021697-107 • • Extension Link Arm 1

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

45 1021546-057 • Foot Pan Assembly 1

ATTACHING PARTS
50 MS27039-0806 • Screw - Pan HD 8
* * *

55 1021700-067 • • Torque Hinge Mount Assembly - LH 1

ATTACHING PARTS
60 MS24693S48 (REF) • • Screw - CSK 3
(True P/N is MS24693-S48)
* * * Gutierrez

65 1021700-113 • • • Mount - Torque Hinge, LH 1

70 20-008 • • • Insert - Reeltorq 1
75 1021700-115 • • • Hinge - Pivot, LH 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10067
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
5
80 1021700-068 • • Torque Hinge Mount Assembly - RH 1
ATTACHING PARTS
85 MS24693S48 (REF) • • Screw - CSK 3
(True P/N is MS24693-S48)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

* * *

90 1021700-114 • • • Mount - Torque Hinge, RH 1

-95 20-008 • • • Insert - Reeltorq 1
100 1021700-116 • • • Hinge - Pivot, RH 1

105 1021700-065 • • Paddle Hinge Mount Assembly - LH 1

ATTACHING PARTS
-110 AN3-5A • • Bolt - HEX HD 1
-115 NAS1149C0332R • • Washer - Flat 1
-120 NAS75-3-013 • • Bushing - Plain Press Fit 1
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

125 JFI0506-06 (REF) • • • Bearing - Flange 1

(True P/N is JFI-0506-06)

130 1021700-111 • • • Mount - Paddle Hinge, LH 1

135 1021700-066 • • Paddle Hinge Mount Assembly - RH 1

ATTACHING PARTS
140 AN3-5A • • Bolt - HEX HD 1
145 NAS1149C0332R • • Washer - Flat 1
Gutierrez
150 NAS75-3-013 • • Bushing - Plain Press Fit 1
* * *

-155 JFI0506-06 (REF) • • • Bearing - Flange 1

(True P/N is JFI-0506-06)
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10068
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
5
-160 1021700-112 • • • Mount - Paddle Hinge, RH 1

165 1021557-057 • • Foot Paddle - Molded 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

170 1021694-147 • Legrest Extension Pan 1
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10069
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

125

120
15
5

10

10
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

10

15

10 Gutierrez

Frame Link Assembly

IPL Figure 6 (Sheet 1 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10070
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

125
(REF)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

120
(REF)

55

50

40
35

30 60
20 65 90
60
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

80
85

50

90
30 45

25
70
Gutierrez

85 75

Frame Link Assembly

IPL Figure 6 (Sheet 2 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10071
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

125 (REF)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

95

115 100

115
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

105 110

100

95
Gutierrez
110

Frame Link Assembly

IPL Figure 6 (Sheet 3 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10072
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
6
-1 1029724-057FQ13 Frame Link Assembly RF
(See IPL FIG 4 for NHA)

5 1029723-057 • Legrest Pan Assembly 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

ATTACHING PARTS
10 MS27039-0806 • Screw - Pan HD 6
* * *

15 M225292-3R100 (REF) • • Grommet - Edging 1

(True P/N is M22529/2-3R-100)
(Attach with Loctite®-454)

20 1021700-123 • Bracket - Rotation Pivot LH 1

ATTACHING PARTS
25 MS27039-0822 • Screw - Pan HD 1
30 NAS1149CN832R • Washer - Flat 2
35 MS21042-08 • Nut - LKG 1
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

40 1021700-124 • Bracket - Rotation Pivot RH 1

ATTACHING PARTS
45 MS27039-0822 • Screw - Pan HD 1
50 NAS1149CN832R • Washer - Flat 2
55 MS21042-08 • Nut - LKG 1
* * *

60 JFI0506-06 (REF) • Bearing - Flange, IGUS 2 Gutierrez

(True P/N is JFI-0506-06)
65 1021700-131 • I-Bolt - Gas Spring 1

70 1021700-117 • Bracket - Pivot Extension 1

ATTACHING PARTS
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10073
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
6
75 MS27039-0819 • Screw - Pan HD 2
* * *

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

80 1021695-107 • Cross Bar - Legrest Lower 1
ATTACHING PARTS
85 NAS6604-14 • Bolt - HEX HD 2
90 MS21042-4 • Nut - LKG 2
* * *

95 1021700-303ZZM • Bumper - Extension 4

ATTACHING PARTS
100 NAS601-6B • Screw - Pan HD 1
* * *

105 WS10-250 (REF) • IGUS Drylin Rail 2

(True P/N is WS-10-250)
ATTACHING PARTS
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

110 MS27039-4-11 • Screw - Pan HD 2

* * *

115 WJUM1032-10AL • Custom Coil 4

120 1021700-063FQ13 • Link Assembly - Legrest 1

(See IPL FIG 7 for DET BKDN)
125 1021700-064FQ13 • Link Assembly - Legrest 1
(See IPL FIG 7 for DET BKDN)
* * * Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10074
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10075
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

120 55
85 25
45 50
160
115 70
80 65
110
125 35

155
165 60
20
105
100

145

70 30
10 60
150 40
75
130 15
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

140
90
175
10 130 95
135 180
170

Gutierrez

Link Assembly - Legrest

IPL Figure 7

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10076
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
7
-1 1021700-063FQ13 Link Assembly - Legrest A RF
(See IPL FIG 6 for NHA)
-1A 1021700-064FQ13 Link Assembly - Legrest B RF
(See IPL FIG 6 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 1021700-310DSX • Shroud - Link C A 1
-5A 1021700-309DSX • Shroud - Link C B 1
ATTACHING PARTS
10 27SR1600315 • Rivet - Snap 2
* * *

15 1021700-308DSX • Shroud - Link A A 1

-15A 1021700-307DSX • Shroud - Link A B 1
ATTACHING PARTS
20 MS27039-0804 • Screw - Pan HD 2
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

25 1021700-051 • Link A Assembly - Press 1

ATTACHING PARTS
30 98038007 • Spacer - Nylon 1
35 MS16633-2031 • Ring - Retaining, External 1
* * *

40 JFI0506-04 (REF) • • Bearing - Flange, IGUS 2

(True P/N is JFI-0506-04)
45 JFI0608-04 (REF) • • Bearing - Flange, IGUS 2
(True P/N is JFI-0608-04)
Gutierrez

50 1021700-101 • • Link A - Legrest 1

55 1021700-053 • Link B Assembly - Press 1

ATTACHING PARTS
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10077
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
7
60 98038007 • Spacer - Nylon 2
65 NAS1149C0532R • Washer - Flat 1
70 MS16633-2031 • Ring - Retaining, External 2

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

* * *

75 JFI0506-04 (REF) • • Bearing - Flange, IGUS 4

(True P/N is JFI-0506-04)
80 JFI0608-04 (REF) • • Bearing - Flange, IGUS 2
(True P/N is JFI-0608-04)

85 1021700-103 • • Link B - Legrest 1

90 1021700-312DSX • Shroud - Link B A 1

-90A 1021700-311DSX • Shroud - Link B B 1

95 1021700-055 • Link C Assembly - Press 1

ATTACHING PARTS
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

100 AN4-14A • Bolt - HEX HD 1

105 NAS1149C0432R • Washer - Flat 1
110 NAS75-4-100 • Bushing - Plain, Press Fit 1
115 98038267 • Spacer - Nylon 1
120 42NKE048 (REF) • Nut - HEX, Nylon Cap 1
(True P/N is P/N 42NKE-048)
* * *

125 JFI0608-04 (REF) • • Bearing - Flange, IGUS 2

(True P/N is JFI-0608-04) Gutierrez
130 1021700-125 • • Pin - Pivot 2

135 1021700-105 • • Link C - Legrest 1

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10078
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
7
140 1021700-057 • Link D Assembly - Press 1
ATTACHING PARTS
145 AN4-14A • Bolt - HEX HD 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

150 NAS1149C0432R • Washer - Flat 1
155 NAS75-4-100 • Bushing - Plain, Press Fit 1
160 42NKE048 (REF) • Nut - HEX, Nylon Cap 1
(True P/N is P/N 42NKE-048)
* * *

165 JFI0608-04 (REF) • • Bearing - Flange, IGUS 2

(True P/N is JFI-0608-04)
170 1021700-125 • • Pin - Pivot 1

175 1021700-107 • • Link D - Legrest 1

180 1021700-109 • Support - Legrest Main Body A 1

-180A 1021700-110 • Support - Legrest Main Body B 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

* * *

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10079
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

BACK FRAME
ASSEMBLY (REF)
30 35

25
5

20
15

10
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Installation - Seatpan Assembly

IPL Figure 8

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10080
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
8
-1 1027368-711 (NP) Installation - Seatpan Assembly RF
(See IPL FIG 1 for NHA)

5 1021984-007 Seatpan Assembly RF

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(See IPL FIG 1 for NHA)
(See IPL FIG 10 for DET BKDN)
ATTACHING PARTS
10 NAS6604-25 • Bolt - HEX HD 1
(Order Separately)
15 5710-55-30 • Washer - Flat 1
(Order Separately)
20 NAS75-4-016 • Bushing - Plain, Press Fit 1
(Order Separately)
25 1022492-301ZYC • Collar - Seatpan Pivot 1
(Order Separately)
30 NAS1149C0432R • Washer - Flat 1
(Order Separately)
35 MS21043-4 • Nut - LKG 1
(Order Separately)
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10081
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

35
40 30

15
50
5
45 10
20
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

40
35

45
50

SEATPAN
ASSEMBLY
(REF)

25

Gutierrez

Installation - Seatpan Support

IPL Figure 9

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10082
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
9
-1 1027368-745 (NP) Installation - Seatpan Support, Double RF
Strap
(See IPL FIG 1 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 1021990-109 • Support Stand - Seatpan 1
(Order Separately)
ATTACHING PARTS
10 5304-25 • Ring - Retaining 1
(Order Separately)
15 GFI0405-05 (REF) • Bearing - Flange, IGUS 1
(Order Separately by True P/N
GFI-0405-05)
* * *

20 LWC50H25 • Clip - Wire, Latching 1

(Order Separately)

25 1021990-061 • Seatpan Strap 1

(Order Separately)
30 1021990-063 • Seatpan Strap 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(Order Separately)
ATTACHING PARTS
35 SSD66BS • Rivet - Dome, Pop 1
(Order Separately)
40 NAS1149C0416R • Washer - Flat 1
(Order Separately)
* * *

45 MS27980-7N • Stud - Snap 2

(Order Separately)
ATTACHING PARTS Gutierrez
50 CSCS05-04 (REF) • Rivet - Blind, CSK 1
(Order Separately by True P/N
CSCS-05-04)
* * *

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10083
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

15
30 20

10
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

25

10

Gutierrez

Seatpan Assembly
IPL Figure 10

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10084
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
10
-1 1021984-007 Seatpan Assembly RF
(See IPL FIG 1 for NHA)

5 1021989-057 • Front Tube Assembly - Seatpan 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

ATTACHING PARTS
10 AN4-11A • Bolt - HEX HD 2
* * *

15 1021985-107 • Tube - Crystal Flex 1

20 1021986-057 • Bottom Diaphragm 1

25 1021990-053 • Rail Assembly - Seatpan 1

30 1021990-054 • Rail Assembly - Seatpan 1
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10085
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

10
BACK ASSEMBLY (REF)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Headrest Frame Assembly

IPL Figure 11

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10086
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
11
-1 1021569-003 Headrest Frame Assembly RF
(See IPL FIG 1 for NHA)

5 2500210-003 • Headrest Assembly - Wide 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

[See IPL FIG 46 for Vendor
Refurbishment Parts
(REF No. WK0044)]
ATTACHING PARTS
10 12-11017-11 • Receptacle 2
(Install Item 10 Before Installing Item 5)
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10087
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

15

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

BACK ASSEMBLY - RIVETED 10
(REF)

15

10 5
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

BACK SHROUD ASSEMBLY

(REF)

Gutierrez

Installation - Video Bezel and Upper Literature Pocket Assembly

IPL Figure 12

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10088
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
12
-1 1027368-725 (NP) Installation - Video Bezel RF
(See IPL FIG 1 for NHA)

5 1032569-077FQ14 Upper Literature Pocket Assembly - RF

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Bonded, No Coat Hook
(See IPL FIG 1 for NHA)
ATTACHING PARTS
10 NAS602-8B • Screw - Pan HD 2
(Order Separately)
15 NAS1149CN832B • Washer - Flat 2
(Order Separately)
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10089
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

BACK
FRAME
(REF)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

20
15
10

5
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Installation - Coat Hook

IPL Figure 13

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10090
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
13
-1 1016258-099 (NP) Installation - Coat Hook RF
(See IPL FIG 1 for NHA)

5 1016258-109 • Pin - Coat Hook 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(Order Separately)
ATTACHING PARTS
10 LCM055D09M • Spring - Helical, Compression 1
(Order Separately)
15 NAS1149D0332K • Washer - Flat 1
(Order Separately)
20 MS16633-1018 • Ring - Retaining 1
(Order Separately)
* * *

-25 1016258-111 • Bushing - Riveted 1

(Order Separately)
ATTACHING PARTS
-30 ACD508ASM • Rivet - Blind, Pan 1
(Order Separately)
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10091
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

BACK ASSEMBLY
(REF)

30
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

20
15
15 25 5

15
35
15

10
Gutierrez

1027369-715
10 INSTALLATION - LOWER LITERATURE
35
ASSEMBLY

Installation - Lower Literature Assembly and Back Trim

IPL Figure 14 (Sheet 1 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10092
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

BACK ASSEMBLY - RIVETED

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

40

50
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

45

50 45 Gutierrez

1027368-759
INSTALLATION - BACK TRIM

Installation - Lower Literature Assembly and Back Trim

IPL Figure 14 (Sheet 2 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10093
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10094
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
14
-1 1027369-715 (NP) Installation - Lower Literature Assembly A RF
(See IPL FIG 1 for NHA)
-3 1027368-759 (NP) Installation - Back Trim B RF
(See IPL FIG 1 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 1048456-007 Lower Literature Assembly C RF
(See IPL FIG 1 for NHA)
ATTACHING PARTS
10 NAS8302-8 • Screw - Washer HD A 4
(Order Separately)
15 MS25281F3 (REF) • Clamp - Loop A 4
(Order Separately by True P/N
MS25281-F3)
* * *

20 1048457-107 • Handle - Lower Literature Pocket C 1

25 1048458-107 • Spring - Lower Literature Pocket C 1

30 1096327-057FQ14 Lower Literature Pocket Assembly RF

(See IPL FIG 1 for NHA)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

ATTACHING PARTS
35 MS27039-0806 • Screw - Pan HD A 4
(Order Separately)
* * *

40 1040065-017 Back Trim - Riveted RF

(See IPL FIG 1 for NHA)
ATTACHING PARTS
45 MS27039-1-08 • Screw - Pan HD B 4
(Order Separately)
Gutierrez
50 NAS1149C0332R • Washer - Flat B 4
(Order Separately)
* * *

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10095
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5

35
30

25
20
15
10

40
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

BEAM (REF)

1027369-703
Gutierrez
INSTALLATION - BACK ASSEMBLY
NON-LOCK SIDE

Installation - Back Assembly

IPL Figure 15 (Sheet 1 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10096
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 (REF)

BEAM (REF)
70
65 75

60
55
105
50
45
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

90
100
95
80

115
110

1027369-705
INSTALLATION - BACK ASSEMBLY
LOCK SIDE Gutierrez

Installation - Back Assembly

IPL Figure 15 (Sheet 2 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10097
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 (REF)

BEAM (REF)

85
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

85

1027369-707
INSTALLATION - BACK ASSEMBLY
BACKLASH SCREW

Gutierrez

Installation - Back Assembly

IPL Figure 15 (Sheet 3 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10098
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
15
-1 1027369-703 (NP) Installation - Back Assembly, A RF
Non-Lock Side
(See IPL FIG 1 for NHA)
-1A 1027369-705 (NP) Installation - Back Assembly, B RF
Lock Side

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(See IPL FIG 1 for NHA)

-2 1027369-707 (NP) Installation - Back Assembly, Backlash C RF

Screw
(See IPL FIG 1 for NHA)

5 1028296-007 Back Assembly - Riveted, W/ Bolster, RF

Last Row
(See IPL FIG 1 for NHA)
(See IPL FIG 16 for DET BKDN)
-5A 1028296-008 Back Assembly - Riveted, W/ Bolster, RF
Last Row
(See IPL FIG 1 for NHA)
(See IPL FIG 16 for DET BKDN)
-5B 1327240-007 Back Assembly - Riveted, W/ Bolster, HIC RF
(See IPL FIG 1 for NHA)
(See IPL FIG 16 for DET BKDN)
-5C 1327240-008 Back Assembly - Riveted, W/ Bolster, HIC RF
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(See IPL FIG 1 for NHA)

(See IPL FIG 16 for DET BKDN)
ATTACHING PARTS
10 NAS517-4-28 • Screw - CSK, Shear A 1
(Order Separately)
(Torque to 90 ±10 IN-LB)
15 1022492-125 • Shackle Fitting A 1
(Order Separately)
20 1022492-107 • Bushing - Mount, Back (Non-Lock) A 1
(Order Separately)
(Painted Line must be Horizontal)
25 1061299-209 • Washer - Flat A 1 Gutierrez
(Order Separately)
30 NAS1149C0432R • Washer - Flat A 1
(Order Separately)
35 MS21042-4 • Nut - LKG A 1
(Order Separately)

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10099
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
15
40 MS51975-17P • Screw - HEX HD, Shoulder A 1
(Order Separately)
(Torque to 100 ±10 IN-LB)
45 NAS517-4-38 • Screw - CSK, Shear B 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(Order Separately)
(Torque to 90 ±10 IN-LB)
50 1022492-125 • Shackle Fitting B 1
(Order Separately)
55 1022492-109 • Bushing - Mount, Back (Lock) B 1
(Order Separately)
(Painted Line must be Horizontal)
60 1061299-209 • Washer - Flat B 1
(Order Separately)
65 NAS1149C0432R • Washer - Flat B 1
(Order Separately)
70 MS21042-4 • Nut - LKG B 1
(Order Separately)
75 VC240-3 (REF) • Cap - Vinyl B 1
(Order Separately by True P/N
VC-240-3)
80 MS51975-17P • Screw - HEX HD, Shoulder B 1
(Order Separately)
(Torque to 100 ±10 IN-LB)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

* * *

85 NAS603-7B • Screw - Pan HD C 2

(Order Separately)
(Set Back Upright Position Prior to
Installing)
(Tighten Until Free Play is Removed
Between Quadrant Assembly and
Shoulder Screws, Items 40 and 80,
Then Add 1/4 turn)

90 HV17500-10 • Hydraulic Lock B 1 Gutierrez

(Order Separately)
ATTACHING PARTS
95 NAS6204-9 • Bolt - HEX HD B 1
(Order Separately)
100 NAS1515H4L • Washer - Plastic B 1
(Order Separately)
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10100
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
15
105 AN316-4R • Nut - Jam B 1
(Order Separately)
110 AN316-6R • Nut - Jam B 2
(Order Separately)
(Turn Both Nuts [Item 110] in Order to

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Close the Cams on Both Lock Washers
[Item 115] Then Fully Tighten to
Recline-Lock Mount Eyebolt)
115 NL38 (REF) • Washer - Nord-Lock B 2
(Order Separately by True P/N
NL3/8)
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10101
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

75

115

80 110

70
80
80

80
120

120

95
30
10
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

25 90
95 90

15 95
15 85
90
125B 30 5

95
20 90

1327240-007
BACK ASSEMBLY - RIVETED - W/ BOLSTER - HIC
Gutierrez

Back Assembly - Riveted

IPL Figure 16 (Sheet 1 of 4)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10102
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

125

80

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

80

75

80

80 35

70
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

40
55

50 45
60 65
55

60
65
50
45

40

Gutierrez
1028296-007
BACK ASSEMBLY - RIVETED - W/ BOLSTER - LAST ROW

Back Assembly - Riveted

IPL Figure 16 (Sheet 2 of 4)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10103
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

130

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

140
170
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

155

150 135
165
160

145
135
1028285-047 Gutierrez
FRAME ASSEMBLY - BACK

Back Assembly - Riveted

IPL Figure 16 (Sheet 3 of 4)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10104
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

130A

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

140B
170
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

155
165 150B
160 135

145B
135
1028285-059
Gutierrez
FRAME ASSEMBLY - BACK

Back Assembly - Riveted

IPL Figure 16 (Sheet 4 of 4)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10105
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10106
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
16
-1 1028296-007 Back Assembly - Riveted, W/ Bolster, A RF
Last Row
(See IPL FIG 1 for NHA)
-1A 1028296-008 Back Assembly - Riveted, W/ Bolster, B RF
Last Row

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(See IPL FIG 1 for NHA)
-1B 1327240-007 Back Assembly - Riveted, W/ Bolster, HIC C RF
(See IPL FIG 1 for NHA)
-1C 1327240-008 Back Assembly - Riveted, W/ Bolster, HIC D RF
(See IPL FIG 1 for NHA)

5 1035657-201 • Sub-Bracket - Lower Literature CD 1

10 1035657-202 • Sub-Bracket - Lower Literature CD 1
ATTACHING PARTS
15 MS27039-0806 • Screw - Pan HD CD 2
* * *

20 1035657-141 • Bracket - Lower Literature Pocket CD 1

25 1035657-142 • Bracket - Lower Literature Pocket CD 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

ATTACHING PARTS
30 NAS1352-08-14 • Screw - Socket HD, Cap CD 2
* * *

35 1042484-107 • Literature Spring AB 1

ATTACHING PARTS
40 NAS1802-3-14 • Screw - HEX AB 2
45 MS25281F3 (REF) • Clamp - Loop AB 2
(True P/N is MS25281-F3)
50 MS21043-3 • Nut - LKG AB 2 Gutierrez

* * *

55 1021520-103 • Literature Spring Support AB 2

ATTACHING PARTS
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10107
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
16
60 NAS1352-08-8 • Screw - Socket HD Cap AB 2
65 NAS1149CN816R • Washer - Flat AB 2
* * *

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

70 1081489-351ZXK • Comfort Pad 1
75 1081489-352ZXK • Comfort Pad 1
ATTACHING PARTS
80 NAS602-8P • Screw - Pan HD 2
* * *

85 1053686-087 • Upper Literature Pocket Bracket CD 1

Assembly
ATTACHING PARTS
90 MS27039-0807 • Screw - Pan HD CD 4
95 NAS1149CN816R • Washer - Flat CD 4
-100 0BF01-00523 • Rivet - Pan CD 4
-105 SSD52BS • Rivet - Dome, Pop CD 4
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

* * *

110 1021520-303ZXK • Mount - Video Bezel CD 1

115 1021520-304ZXK • Mount - Video Bezel CD 1
ATTACHING PARTS
120 AD66ALS • Rivet - Blind, Pan CD 2
* * *

125 1028285-047 • Frame Assembly - Back A 1 Gutierrez

-125A 1028285-048 • Frame Assembly - Back B 1

125B 1028285-059 • Frame Assembly - Back C 1
-125C 1028285-060 • Frame Assembly - Back D 1

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10108
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
16
130 1029716-057 • • Diaphragm - Back AB 1
130A 1067131-057 • • Diaphragm - Back CD 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

135 SJ3519FR100B (REF) • • 3M™ Hook Tape - Adhesive 100 AR
Black
(True P/N is SJ3519FR100BLACK)

140 1025665-047 • • Frame W/ Quadrants - Back A 1

-140A 1025665-048 • • Frame W/ Quadrants - Back B 1
140B 1025665-057 • • Frame W/ Quadrants - Back C 1
-140C 1025665-058 • • Frame W/ Quadrants - Back D 1

145 1022492-083 • • • Quadrant Assembly - Non-Lock A 1

(See IPL FIG 17 for DET BKDN)
-145A 1022492-084 • • • Quadrant Assembly - Non-Lock B 1
(See IPL FIG 17 for DET BKDN)
145B 1022492-087 • • • Quadrant Assembly - Non-Lock C 1
(See IPL FIG 17 for DET BKDN)
-145C 1022492-088 • • • Quadrant Assembly - Non-Lock D 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(See IPL FIG 17 for DET BKDN)

150 1022492-081 • • • Quadrant Assembly - Lock A 1

(See IPL FIG 17 for DET BKDN)
-150A 1022492-082 • • • Quadrant Assembly - Lock B 1
(See IPL FIG 17 for DET BKDN)
150B 1022492-085 • • • Quadrant Assembly - Lock C 1
(See IPL FIG 17 for DET BKDN)
-150C 1022492-086 • • • Quadrant Assembly - Lock D 1
(See IPL FIG 17 for DET BKDN)
ATTACHING PARTS
Gutierrez
155 1022492-119 • • • Back Pin - Quadrant 2
160 1022492-121 • • • Bushing 2
165 5304-25 • • • Ring - Retaining 2
* * *

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10109
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
16
170 1025664-317 • • • Back Frame 1
* * *

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10110
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10111
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

20

30
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

10

15
1022492-081
QUADRANT ASSEMBLY - LOCK

Gutierrez

25

Quadrant Assembly
IPL Figure 17 (Sheet 1 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10112
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5

10A

30B
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

20 1022492-083
15
QUADRANT ASSEMBLY - NON-LOCK

Gutierrez

Quadrant Assembly
IPL Figure 17 (Sheet 2 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10113
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10114
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
17
-1 1022492-081 Quadrant Assembly - Lock A RF
(See IPL FIG 16 for NHA)
-1A 1022492-082 Quadrant Assembly - Lock B RF
(See IPL FIG 16 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

-1B 1022492-083 Quadrant Assembly - Non-Lock C RF
(See IPL FIG 16 for NHA)
-1C 1022492-084 Quadrant Assembly - Non-Lock D RF
(See IPL FIG 16 for NHA)
-1D 1022492-085 Quadrant Assembly - Lock E RF
(See IPL FIG 16 for NHA)
-1E 1022492-086 Quadrant Assembly - Lock F RF
(See IPL FIG 16 for NHA)
-1F 1022492-087 Quadrant Assembly - Non-Lock G RF
(See IPL FIG 16 for NHA)
-1G 1022492-088 Quadrant Assembly - Non-Lock H RF
(See IPL FIG 16 for NHA)

5 1022492-141 • HIC Link A-D 1

-5A 1022492-143 • HIC Link E-H 1
ATTACHING PARTS
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

10 NAS75-4-105 • Bushing - Plain, Press Fit ABEF 1

10A NAS75-4-104 • Bushing - Plain, Press Fit CDGH 1
15 MS16555-54 • Pin - Dowel 1
* * *

20 NAS77-10-050 • Bushing - Flanged, Press Fit 1

25 NAS75-4-007 • Bushing - Plain, Press Fit ABEF 1

30 1022492-155 • Quadrant - Lock Side AE 1 Gutierrez

-30A 1022492-156 • Quadrant - Lock Side BF 1
30B 1022492-131 • Quadrant - Non-Lock Side CG 1
-30C 1022492-132 • Quadrant - Non-Lock Side DH 1
* * *
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10115
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

3D ELECTRICAL INSTALLATION DRAWINGS ASSOCIATED WITH THIS CMM
ARE AVAILABLE BY REQUEST. REQUESTS FOR 3D PDFs SHOULD BE SENT TO
THE FOLLOWING:
ws_techpubs3d@collins.com

REFER TO USING 3D ELECTRICAL DRAWINGS (PAGE BLOCK 17000)

FOR INFORMATION AND INSTRUCTIONS FOR USING 3D
ELECTRICAL DRAWINGS REFERENCED IN THIS CMM.

REFER TO PART NUMBER(S) CONTAINED IN THE ILLUSTRATED PARTS LIST

FOR PART(S) ORDERING - DO NOT USE THE 3D PDF FOR PART(S) ORDERING.

REFER TO SCHEMATIC AND WIRING DIAGRAMS (PAGE BLOCK 2000)

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

FOR CABLE ROUTING AND GROUNDING STANDARDS AND PROCEDURES.

REFER TO ASTRONICS BLOCK DIAGRAM CA7/VOZ 737-8 OF THE IFE SYSTEM FOR
MORE SPECIFIC DETAILS. CONTACT ASTRONICS FOR THE LATEST RELEASED
VERSION OF THIS DOCUMENT (REFER TO INTRODUCTION PAGE BLOCK OF THIS
CMM FOR VENDOR CONTACT INFORMATION).

Gutierrez

Installation - Electrical
IPL Figure 18 (Sheet 1 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10116
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

65
GROUND STRAP

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

REFERENCE

55
SEAT STRUCTURE
REFERENCE

60

55

55
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

50

45

1017020-701
Gutierrez
INSTALLATION - GROUND STUD

Installation - Electrical
IPL Figure 18 (Sheet 2 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10117
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

GROUND STRAP
REFERENCE

85

75

SEAT STRUCTURE
REFERENCE

80
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

75

1017020-705
INSTALLATION - GROUND STUD

Gutierrez

Installation - Electrical
IPL Figure 18 (Sheet 3 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10118
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
18
-1 1097452-701 (NP) Installation - Electrical, LH F/R, DBL A RF
(See IPL FIG 1 for NHA)

(See SCHEMATIC AND WIRING

DIAGRAMS [Page Block 2000])

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(See USING 3D ELECTRICAL
DRAWINGS [Page Block 17000])
(3D PDF 1097112-701 [Available Upon
Request])
-1A 1097452-703 (NP) Installation - Electrical, RH F/R, DBL B RF
(See IPL FIG 1 for NHA)

(See SCHEMATIC AND WIRING

DIAGRAMS [Page Block 2000])

(See USING 3D ELECTRICAL

DRAWINGS [Page Block 17000])
(3D PDF 1097112-703 [Available Upon
Request])
-1B 1097452-705 (NP) Installation - Electrical, LH Last Row, DBL C RF
(See IPL FIG 1 for NHA)

(See SCHEMATIC AND WIRING

DIAGRAMS [Page Block 2000])
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(See USING 3D ELECTRICAL

DRAWINGS [Page Block 17000])

(3D PDF 1097112-705 [Available Upon

Request])
-1C 1097452-707 (NP) Installation - Electrical, RH Last Row, DBL D RF
(See IPL FIG 1 for NHA)

(See SCHEMATIC AND WIRING

DIAGRAMS [Page Block 2000])

(See USING 3D ELECTRICAL

DRAWINGS [Page Block 17000])
Gutierrez
(3D PDF 1097112-707 [Available Upon
Request])

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10119
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
18
-5 1097108-701 (NP) • Installation - Electrical SIB / SPM LH A 1
DBL
(3D Bubble Number 901)
-5A 1097108-703 (NP) • Installation - Electrical SIB / SPM RH B 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

DBL
(3D Bubble Number 901)
-5B 1097108-705 (NP) • Installation - Electrical SIB / SPM LH C 1
DBL
(3D Bubble Number 901)
-5C 1097108-707 (NP) • Installation - Electrical SIB / SPM RH D 1
DBL
(3D Bubble Number 901)
-10 1294-2-2 • • AC Power In Use Light 1
(Order Separately)
(3D Bubble Number 302)
-15 1295-2-118 • • AC / USB Outlet Unit 2
(Order Separately)
(3D Bubble Number 303)
-20 1191-46 • • In - Seat Power Supply 1
(Order Separately)
(3D Bubble Number 301)

-25 1191810-44 • • Cable Assembly - ISPS to Flange AB 1

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

DISC
(Order Separately)
(3D Bubble Number 352)
-30 1191811-44 • • Cable Assembly - DISC to ISPS 1
(Order Separately)
(3D Bubble Number 353)
-35 1299855-101011 • • Cable Assembly - ISPS to OU / USB AC 1
(Order Separately)
(3D Bubble Number 354)
-35A 1299854-101011 • • Cable Assembly - ISPS to OU / USB BD 1
(Order Separately)
(3D Bubble Number 354)
Gutierrez

-40 1017020-701 (NP) • • Installation - Ground Stud 2

(3D Bubble Number 421)
45 NAS1802-3-12P • • • Screw - HEX HD 1
(Order Separately)
50 MS35338-43P • • • Washer - Lock Spring 1
(Order Separately)
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10120
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
18
55 NAS1149A0316H • • • Washer - Flat 3
(Order Separately)
60 MS35650-304 • • • Nut - Plain 1
(Order Separately)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

65 MS21042-3 • • • Nut - LKG 1
(Order Separately)

-70 1017020-705 (NP) • • Installation - Ground Stud 1

(3D Bubble Number 425)
75 NAS1149A0316H • • • Washer - Flat 2
(Order Separately)
80 MS35650-304 • • • Nut - Plain 1
(Order Separately)
85 MS21042-3 • • • Nut - LKG 1
(Order Separately)

-90 AT327-14 • • Nut - Plate, Connector AB 2

(Order Separately)
(3D Bubble Number 682)
-90A AT327-14 • • Nut - Plate, Connector CD 1
(Order Separately)
(3D Bubble Number 682)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

ATTACHING PARTS
-95 NAS1352-04-6 • • Screw - Socket HD, Cap AB 8
(Order Separately)
(3D Bubble Number 675)
-95A NAS1352-04-6 • • Screw - Socket HD, Cap CD 4
(Order Separately)
(3D Bubble Number 675)
-100 NAS1149CN416R • • Washer - Flat AB 8
(Order Separately)
(3D Bubble Number 683)
-100A NAS1149CN416R • • Washer - Flat CD 4
(Order Separately) Gutierrez
(3D Bubble Number 683)
* * *

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10121
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
18
-105 FTH3-01 (REF) • • Mount - Cable Tie, Push 2
(Order Separately by True P/N
FTH-3-01)
(3D Bubble Number 658)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

-110 CR2 • • Connector - Ring AC 2
(Order Separately)
(3D Bubble Number 623)
-110A CR2 • • Connector - Ring BD 3
(Order Separately)
(3D Bubble Number 623)
-115 CR4H • • Connector - Ring 3
(Order Separately)
(3D Bubble Number 624)
-120 CSCS • • Cable - Spacer, Cross 1
(Order Separately)
(3D Bubble Number 625)
-125 M8372360-214A (REF) • • Connector - Cover Electrical CD 1
(Order Separately by True P/N
M83723/60-214AN)
(3D Bubble Number 391)

-130 MS3367-4-9 • • Strap - Tiedown, Adjustable AR

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(Order Separately)
(3D Bubble Number 629)
-135 MS3367-5-9 • • Strap - Tiedown, Adjustable AR
(Order Separately)
(3D Bubble Number 631)
-140 MS3367-7-9 • • Strap - Tiedown, Adjustable AR
(Order Separately)
(3D Bubble Number 636)

-145 1401445-033 • • PMA - Ground Strap 1

(Order Separately)
(3D Bubble Number 401)
Gutierrez
-150 1401445-045 • • Ground Strap AC 1
(Order Separately)
(3D Bubble Number 402)
-150A 1401445-025 • • PMA - Ground Strap BD 1
(Order Separately)
(3D Bubble Number 402)

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10122
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
18
-155 3M5958-1 • • Foam Tape - DBL Sided AR
(Order Separately)
(3D Bubble Number 731)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

-160 5672500572 • • ROUNDIT® - 2000 MA AR
(Order Separately)
(3D Bubble Number 700)

-165 5672500872 • • ROUNDIT® - 2000 MA AR

(Order Separately)
(3D Bubble Number 701)
-170 5672501372 • • ROUNDIT® - 2000 MA AR
(Order Separately)
(3D Bubble Number 702)

-175 1017797-001 • • Placard - Ground 1

(Order Separately)
(3D Bubble Number 451)
-180 1017797-003 • • Placard - Ground 1
(Order Separately)
(3D Bubble Number 453)
-185 1017797-005 • • Placard - Ground 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(Order Separately)
(3D Bubble Number 455)

-190 1097111-705 (NP) • Installation - EEPL Lights AC 1

(3D Bubble Number 902)
-195 44960029 • • PMA - Aisle Light Clear AC 2
(Order Separately)
(3D Bubble Number 500)
-200 44960103 • • PMA - Aisle Light Harness AC 1
(Order Separately)
(3D Bubble Number 521)

Gutierrez
-205 5672500872 • • ROUNDIT® - 2000 MA AC AR
(Order Separately)
(3D Bubble Number 701)
-210 5672500572 • • ROUNDIT® - 2000 MA AC AR
(Order Separately)
(3D Bubble Number 700)
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10123
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
18
-215 FTH3-01 (REF) • • Mount - Cable Tie, Push AC 1
(Order Separately by True P/N
FTH-3-01)
(3D Bubble Number 658)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

-220 MS3367-4-9 • • Strap - Tiedown, Adjustable AC AR
(Order Separately)
(3D Bubble Number 629)
-225 MS3367-5-9 • • Strap - Tiedown, Adjustable AC AR
(Order Separately)
(3D Bubble Number 631)
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10124
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10125
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

SIDE PANEL - CONSOLE (REF)

15
10
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

15
10

5
25 Gutierrez

20

Installation - Lower Console

IPL Figure 19 (Sheet 1 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10126
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

40

35

30
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Installation - Lower Console

IPL Figure 19 (Sheet 2 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10127
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

70

40
75

30 (REF)

65
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

50
55

45
60
40 55
50

Gutierrez

Installation - Lower Console

IPL Figure 19 (Sheet 3 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10128
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
19
-1 1027368-733 (NP) Installation - Lower Console A RF
(See IPL FIG 1 for NHA)

5 1031728-083MS02 Rear Panel Assembly - PC Power B RF

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(See IPL FIG 1 for NHA)
ATTACHING PARTS
10 NAS1352-06-6P • Screw - Socket HD Cap A 2
(Order Separately)
15 27SR1600315 • Rivet - Snap A 2
(Order Separately)
20 NAS1801-3-16 • Screw - HEX HD A 2
(Order Separately)
25 APPPHC810108 • Cover - Screw, Hinged A 2
(Order Separately)
* * *

30 1050092-301DTE • Lower SPM Panel - OUTBD B 1

35 1050092-302DTE • Lower SPM Panel - OUTBD B 1
ATTACHING PARTS
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

40 NAS601-5P • Screw - Pan HD B 2

* * *

45 1031728-065 • Bracket Assembly - Reinforcement B 1

ATTACHING PARTS
50 NAS601-6P • Screw - Pan HD B 4
* * *

55 SL211-3-1 • • Nut - Clip, Self-Locking B 2

Gutierrez
60 1027372-231 • • Bracket - Reinforcement B 1

65 1028283-651 • Lower Trim Bezel - Rear LH B 1

70 1028283-652 • Lower Trim Bezel - Rear RH B 1

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10129
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
19
75 1050090-301DTE • Panel - Lower SPM Shroud B 1
* * *

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10130
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10131
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

10

15
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

10

Gutierrez

Installation - Center Console

IPL Figure 20

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10132
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
20
-1 1027368-765 (NP) Installation - Center Console, Black Plug RF
(See IPL FIG 1 for NHA)

5 1027371-753MS08 Center Console Assembly - Non-Video RF

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(See IPL FIG 1 for NHA)
(See IPL FIG 21 for DET BKDN)
ATTACHING PARTS
10 NAS6604-1 • Bolt - HEX HD 4
(Order Separately)
15 2700 • Plug - Dome 2
(Order Separately)
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10133
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

25
35
30
15
20

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

30 20

40 20
35
30

5
20

10
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

10

Gutierrez

Center Console Assembly - Non-Video

IPL Figure 21 (Sheet 1 of 6)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10134
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

55
60
45
75 55
60

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

65

70

50
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

50

Gutierrez

Center Console Assembly - Non-Video

IPL Figure 21 (Sheet 2 of 6)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10135
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

95
90
100
80

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

85

85
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Center Console Assembly - Non-Video

IPL Figure 21 (Sheet 3 of 6)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10136
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

120 105

120

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

110
180

180 135

125
185
165

175
145

130

175
170
175
150 115
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

160 155

175
240

175

Gutierrez
175

Center Console Assembly - Non-Video

IPL Figure 21 (Sheet 4 of 6)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10137
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

205
210
200
200

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

215

300
280
B

220

275

285 220

280

A
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

280

255
285

255

250

230 270

225 Gutierrez
235

Center Console Assembly - Non-Video

IPL Figure 21 (Sheet 5 of 6)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10138
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

1.50" .25"
4x 2.75"

2x 1.34"

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

4x .50"

295

295

.25" 4x 2.75" 1.50"

2x 1.34"
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

4x .50"

295
295

Gutierrez
B

Center Console Assembly - Non-Video

IPL Figure 21 (Sheet 6 of 6)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10139
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10140
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
21
-1 1027371-753MS08 Center Console Assembly - Non-Video RF
(See IPL FIG 1 for NHA)

5 1027372-071MS08 • Armcap Assembly 2

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

ATTACHING PARTS
10 MS24693-25B • Screw - CSK 8
* * *

15 1027372-371FCJ • • Closeout - Armcap 1

ATTACHING PARTS
20 27SR0018 • • Rivet - Snap 7
* * *

25 1027372-651 • • Armcap Trim - Machined 1

ATTACHING PARTS
30 NAS6603-1 • • Bolt - HEX HD 3
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

35 0601-034 • • Bumper - Stem 2

(Attach with Loctite®-454)

40 1027372-073MS08 • • Armcap Assembly - Overmold 1

45 1021487-017MS02 • Cocktail Table Assembly - Fixed 1

ATTACHING PARTS
50 NAS1352-06-7 • Screw - Socket HD Cap 2
Gutierrez
55 NAS603-7B • Screw - Pan HD 2
60 APPPHC810108 • Cover - Screw, Hinged 2
* * *

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10141
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
21
65 MC37B0DY (REF) • • Body 1
(True P/N is MC-37-BODY)
ATTACHING PARTS
70 NAS1352-04-6P • • Screw - Socket HD Cap 4

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

* * *

75 1021487-097MS02 • • Cocktail Table Assembly - Fixed 1

80 1021487-015MS02 • Cocktail Table Assembly 1

(See IPL FIG 22 for DET BKDN)
ATTACHING PARTS
85 B1831AH030008L • Screw - Socket 4
* * *

90 1027372-203 • Bracket - Bumper Bar 1

ATTACHING PARTS
95 NAS601-5B • Screw - Pan HD 2
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

* * *

100 409615 • Grommet - Bumper 1

105 1027372-653 • Bezel - Rear Trim 1

ATTACHING PARTS
110 NAS1635-06-8 • Screw - Pan HD 2
* * *

Gutierrez
115 1027372-051MS02 • Rear Trim Assembly 1
ATTACHING PARTS
120 NAS1351-3-6P • Screw - Socket HD Cap 2
* * *

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10142
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
21
125 1027372-227 • • Support Bracket - Rear Panel 1
ATTACHING PARTS
130 NAS601-6P • • Screw - Pan HD 2

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

* * *

135 1027372-656 • • Rear Trim Bezel - Machined, RH 1

ATTACHING PARTS
-140 NAS601-6P • • Screw - Pan HD 2
* * *

145 1027372-655 • • Rear Trim Bezel - Machined, LH 1

ATTACHING PARTS
150 NAS601-6P • • Screw - Pan HD 2
* * *

155 1050253-301DTE • • Rear Panel 1

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

160 1023851-027MS02 • Button Assembly - Seat Control, LH 1

(See IPL FIG 23 for DET BKDN)
165 1023851-029MS02 • Button Assembly - Seat Control, RH 1
(See IPL FIG 23 for DET BKDN)

170 1040627-309DTF • Shroud - Side Panel, RH 1

ATTACHING PARTS
175 27SR0018WHITE (REF) • Rivet - Snap 8
(True P/N is 27SR0018-WHITE)
180 27SR0018 • Rivet - Snap 2 Gutierrez
* * *

185 1040627-310DTF • Shroud - Side Panel, LH 1

ATTACHING PARTS
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10143
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
21
-190 27SR0018WHITE (REF) • Rivet - Snap 8
(True P/N is 27SR0018-WHITE)
-195 27SR0018 • Rivet - Snap 2
* * *

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

200 JAH99-95 (REF) • Articulating Hinge Assembly 2
(True P/N is J-AH-99-95)
ATTACHING PARTS
205 MS24694C50 (REF) • Screw - CSK 2
(True P/N is MS24694-C50)
* * *

210 1027372-751MS02 • Pocket Assembly 1

(See IPL FIG 24 for DET BKDN)
ATTACHING PARTS
215 NAS6603-1 • Bolt - HEX HD 2
220 27SR0012 • Rivet - Snap 14
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

225 1063550-001MS02 • Door Assembly - Life Vest Box 1

ATTACHING PARTS
230 MS51576-10 • Screw - Socket HD 2
* * *

235 1055300-053 • • Latch Assembly - Life Vest Door 1

240 1055304-001 • • • Pull Strap - Life Vest 1
(Install to Item -245 by Wrapping
Pull Strap Around the Slot and Gutierrez
Engaging Hook and Loop
Securely)
-245 R4-99-421SLV (REF) • • • Dual Pawl Assembly 1
Non-Lockable
(True P/N is R4-99-421-SLV)

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10144
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
21
250 1063309-011 • Bottom Bezel Assembly - Front 1
ATTACHING PARTS
255 NAS1351-3-6 • Screw - Socket HD Cap 4

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

* * *

-260 1063309-111 • • Front Bottom Trim Bezel - RH 1

-265 1063309-113 • • Front Bottom Trim Bezel - LH 1
ATTACHING PARTS
270 MS24694C48 (REF) • • Screw - CSK 2
(True P/N is MS24694-C48)
* * *

275 1027372-047MS02 • Trim Assembly - Front 1

(See IPL FIG 25 for DET BKDN)
ATTACHING PARTS
280 NAS1351-3-6 • Screw - Socket HD Cap 4
285 NAS601-7P • Screw - Pan HD 2
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

-290 1027372-401 • Foam - Center Console 1

295 3M9485PC050 (REF) • 3M™ Adhesive Transfer Tape AR

(True P/N is 3M9485PC-050)

300 1052089-055FQ13 • Console structure Assembly - Non- 1

Video
(See IPL FIG 26 for DET BKDN)
* * * Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10145
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

10

10

35

45

25
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

20

30

15

40
Gutierrez

Cocktail Table Assembly

IPL Figure 22

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10146
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
22
-1 1021487-015MS02 Cocktail Table Assembly RF
(See IPL FIG 21 for NHA)

5 IK0ML9C1R160H (REF) • Carriage and Rail 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(True P/N is IKO-ML9C1R160HS2)
ATTACHING PARTS
10 NAS1352-06-4 • Screw - Socket HD Cap 3
* * *

15 RA22CSN (REF) • Magnetic Ring - CSK 1

(True P/N is RA22CS-N)
ATTACHING PARTS
20 MS24693C3 (REF) • Screw - CSK 1
(True P/N is MS24693-C3)
* * *

25 MC37BLK1STRK (REF) • Striker 1

(True P/N is MC-37BLK-1-STRK)
ATTACHING PARTS
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

30 SSD45BS • Rivet - Dome, Pop 2

35 VC156-4 (REF) • Cap - Vinyl 2
(True P/N is VC-156-4)
(Attach with Loctite®-454)
* * *

40 27SR0012WHITE (REF) • Rivet - Snap 1

(True P/N is 27SR0012-WHITE)

45 1021487-099MS02 • Table Assembly - Cocktail 1 Gutierrez

* * *

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10147
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

60
40
35

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

25

40

35

20

30 10

15

5
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

50

55

35
(REF)

Gutierrez

45

Button Assembly - Seat Control

IPL Figure 23

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10148
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
23
-1 1023851-027MS02 Button Assembly - Seat Control, LH A RF
(See IPL FIG 21 for NHA)
-1A 1023851-029MS02 Button Assembly - Seat Control, RH B RF
(See IPL FIG 21 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 1023851-111 • Button - Control, Recline A 1
-5A 1023851-112 • Button - Control, Recline B 1
10 1023851-115 • Button - Control, Footrest A 1
-10A 1023851-116 • Button - Control, Footrest B 1
15 1023851-113 • Button - Control, Footpad A 1
-15A 1023851-114 • Button - Control, Footpad B 1
ATTACHING PARTS
20 1052184-105 • Pin - Seat Control 1
25 MS16633-1012 • Retaining Ring - External 1
* * *

30 LC016C13M • Spring - Helical, Compression 3

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

35 1027372-075 • Retainer Assembly A 2

-35A 1027372-041 • Retainer Assembly B 2
ATTACHING PARTS
40 NAS514P440-4 • Screw - CSK 1
* * *

45 1027372-221 • • Retaining Clip 1

ATTACHING PARTS
Gutierrez
50 NAS1352-04-10 • • Screw - Socket HD Cap 1
* * *

55 1027372-337ZWZ • • Bezel - RJU and RJM A 1

-55A 1027372-359ZWZ • • Retainer - RJU and RJM B 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10149
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
23
60 1023851-323BWC • Housing - Seat Control A 1
-60A 1023851-324BWC • Housing - Seat Control B 1
* * *

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10150
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10151
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

10
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

10

15
5

10

Gutierrez

Pocket Assembly
IPL Figure 24 (Sheet 1 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10152
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

25

65

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

55

60

30
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

75

40

30

45
35 Gutierrez
40 40

Pocket Assembly
IPL Figure 24 (Sheet 2 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10153
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10154
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
24
-1 1027372-751MS02 Pocket Assembly RF
(See IPL FIG 21 for NHA)

5 1040966-355FCJ • Panel - Pocket, Side, LH 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

ATTACHING PARTS
10 27SR0012 • Rivet - Snap 4
* * *

15 1040966-356FCJ • Panel - Pocket, Side, RH 1

ATTACHING PARTS
-20 27SR0012 • Rivet - Snap 4
* * *

25 1027372-373FCJ • Panel - Pocket Shroud, PC Power 1

ATTACHING PARTS
30 27SR0012 • Rivet - Snap 4
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

35 1027372-311FCJ • Panel - Pocket, Lower, LH 1

ATTACHING PARTS
40 27SR0012 • Rivet - Snap 4
* * *

45 1027372-312FCJ • Panel - Pocket, Lower, RH 1

ATTACHING PARTS
-50 27SR0012 • Rivet - Snap 4 Gutierrez
* * *

55 1027372-317FCJ • Panel - Pocket, FWD, LH 1

ATTACHING PARTS
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10155
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
24
60 27SR0012 • Rivet - Snap 1
* * *

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

65 1027372-347FCJ • Panel - Pocket, FWD, RH 1
ATTACHING PARTS
-70 27SR0012 • Rivet - Snap 1
* * *

75 1053775-301FCJ • Panel - Pocket, Aft 1

* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10156
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10157
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

50

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

45

40

20

25

15
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

25

15

25
15
25

5 10
Gutierrez

10

Trim Assembly - Front

IPL Figure 25

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10158
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
25
-1 1027372-047MS02 Trim Assembly - Front RF
(See IPL FIG 21 for NHA)

5 1027372-307DSX • Panel - Life Vest Top Shroud 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

ATTACHING PARTS
10 NAS601-7P • Screw - Pan HD 2
15 SL210-06-1 • Nut - Clip 4
* * *

20 1027372-021 • Front Trim Assembly - Riveted 1

ATTACHING PARTS
25 NAS602-7B • Screw - Pan HD 6
* * *

-30 1021487-115 • • Latch Striker - Life Vest Box 1

ATTACHING PARTS
-35 MS16633-1018 • • Ring - Retaining, External 2
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

* * *

40 1027372-381DTF • Bottle Bucket 1

45 1027372-641 • Front Trim Bezel - Machined 1
50 1049965-301DTE • Trim Bezel 1
* * *

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10159
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

80

105

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

115

110
95
85 65
20 90 100

120

15

70
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

75
50

20
55

45
60 35

10

30 Gutierrez

25 30
40

Console Structure Assembly - Non-Video

IPL Figure 26 (Sheet 1 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10160
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

80 (REF)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

65 (REF)

120 (REF)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

90

75

Gutierrez

Console Structure Assembly - Non-Video

IPL Figure 26 (Sheet 2 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10161
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10162
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
26
-1 1052089-055FQ13 Console Structure Assembly - Non-Video RF
(See IPL FIG 21 for NHA)

5 1063309-039FQ13 • Life Vest Box Assembly 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

ATTACHING PARTS
10 NAS601-7P • Screw - Pan HD 4
* * *

15 1027372-107 • Cocktail Table 1

ATTACHING PARTS
20 NAS1352-08-8 • Screw - Socket HD Cap 4
* * *

25 1027372-065 • Bracket Assembly - Life Vest 1

ATTACHING PARTS
30 NAS601-7P • Screw - Pan HD 2
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

35 SL210-06-1 • • Nut - Clip, Self-Locking 4

40 1021487-205 • • Bracket Attachment - Life Vest 1

45 1027372-066 • Bracket Assembly - Life Vest 1

ATTACHING PARTS
50 NAS601-7P • Screw - Pan HD 2
* * *
Gutierrez
55 SL210-06-1 • • Nut - Clip, Self-Locking 4
60 1021487-206 • • Bracket Attachment - Life Vest 1

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10163
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
26
65 1049941-105 • Side Panel - Console 1
ATTACHING PARTS
70 NAS514P1032-8 • Screw - CSK 2

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

75 NAS601-7P • Screw - Pan HD 4
* * *

80 1049941-106 • Side Panel - Console 1

ATTACHING PARTS
85 NAS514P1032-8 • Screw - CSK 2
90 NAS601-7P • Screw - Pan HD 4
* * *

95 1027372-119 • Center Brace - Machined 1

ATTACHING PARTS
100 NAS6603-1 • Bolt - HEX HD 2
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

105 1027372-115 • Hinge Support 1

ATTACHING PARTS
110 MS35206-226 • Screw - Pan HD 1
115 NAS6603-1 • Bolt - HEX HD 2
* * *

120 1052040-007 • Bracket Assembly - PC Power 1

Gutierrez
-125 SL210-06-1 • • Nut - Clip, Self-Locking 2
-130 1053775-201 • • Bracket PC Power - Trim 1
* * *

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10164
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10165
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

10

5
TABLE MOUNT ASSEMBLY
(REF IPL FIG 39, ITEM 55)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Installation - Foodtray Assembly

IPL Figure 27

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10166
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
27
-1 1027368-791 (NP) Installation - Foodtray Assembly RF
(See IPL FIG 1 for NHA)

5 1027900-057MS02 Foodtray Assembly - Tablet RF

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(See IPL FIG 1 for NHA)
(See IPL FIG 28 for DET BKDN)
-5A 1027900-058MS02 Foodtray Assembly - Tablet RF
(See IPL FIG 1 for NHA)
(See IPL FIG 28 for DET BKDN)
-5B 1027900-067MS02 Foodtray Assembly - Tablet, Special RF
(See IPL FIG 1 for NHA)
(See IPL FIG 28 for DET BKDN)
-5C 1027900-068MS02 Foodtray Assembly - Tablet, Special RF
(See IPL FIG 1 for NHA)
(See IPL FIG 28 for DET BKDN)
ATTACHING PARTS
10 NAS1351-3-14 • Screw - Socket HD Cap 2
(Order Separately)
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10167
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

170

15

15 10

15

10
15
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Foodtray Assembly
IPL Figure 28 (Sheet 1 of 5)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10168
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

170 (REF)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

75 45
30

20

35

40
Gutierrez
25
50
55
65

70

Foodtray Assembly
IPL Figure 28 (Sheet 2 of 5)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10169
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

170 (REF)

90

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

95

95
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

100
105

105

105 Gutierrez

105

Foodtray Assembly
IPL Figure 28 (Sheet 3 of 5)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10170
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

145

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

125

115
140

140

125

120

115
110
115
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

130
135

115

1027989-057 Gutierrez
ARM LINKAGE - FOODTRAY

Foodtray Assembly
IPL Figure 28 (Sheet 4 of 5)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10171
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

170 (REF)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

150

160

155

155
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

155

155
165

155

155

150 Gutierrez

Foodtray Assembly
IPL Figure 28 (Sheet 5 of 5)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10172
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
28
-1 1027900-057MS02 Foodtray Assembly - Tablet A RF
(See IPL FIG 1 for NHA)
-1A 1027900-058MS02 Foodtray Assembly - Tablet B RF
(See IPL FIG 1 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

-1B 1027900-067MS02 Foodtray Assembly - Tablet, Special C RF
(See IPL FIG 1 for NHA)
-1C 1027900-068MS02 Foodtray Assembly - Tablet, Special D RF
(See IPL FIG 1 for NHA)

5 1021472-057MS02 • Foodtray Leaf Assembly - Folding AC 1

-5A 1021472-058MS02 • Foodtray Leaf Assembly - Folding BD 1
ATTACHING PARTS
10 47000283 • Hinge - Foodtray Leaf 2
15 1012042-115 • Pin - Hinge, Foodtray Leaf 4
(Cover the Head with Silicone Adhesive
P/N AD-RTVR-T)
* * *

20 1031754-137 • Latch Bracket 1

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

ATTACHING PARTS
25 NAS1352-06-6 • Screw - Socket HD Cap 4
* * *

30 1031754-139 • Socket Drive - Shoulder Post 1

35 MS21042-3 • Nut - LKG 1

40 1021684-137 • Forward Stop - Foodtray Table AB 1

-40A 1021684-139 • Forward Stop - Foodtray Table C 1
Gutierrez
-40B 1021684-140 • Forward Stop - Foodtray Table D 1
ATTACHING PARTS
45 NAS1801-3-12 • Screw - HEX HD 2
* * *
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10173
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
28
50 1021684-061 • Dampener Assembly - Foodtray AC 1
-50A 1021684-062 • Dampener Assembly - Foodtray BD 1
ATTACHING PARTS

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

55 NAS6603-1 • Bolt - HEX HD 2
* * *

-60 GSI1214-08 (REF) • • Bearing - Sleeve, IGUS 1

(True P/N is GSI-1214-08)

65 1021684-117 • • Housing - Dampener AC 1

-65A 1021684-118 • • Housing - Dampener BD 1

70 FYNP1L183 (REF) • Damper - Rotary AC 1

(True P/N is FYN-P1-L-183)
-70A FYNP1R183 (REF) • Damper - Rotary BD 1
(True P/N is FYN-P1-R-183)

75 1027879-051 • Closeout Assembly - Foodtray AC 1

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

-75A 1027879-052 • Closeout Assembly - Foodtray BD 1

-80 GFI0405-04 (REF) • • Bearing - Flange, IGUS 1

(True P/N is GFI-0405-04)

-85 1021684-141 • • Closeout - Foodtray, Deployed AC 1

-85A 1021684-142 • • Closeout - Foodtray, Deployed BD 1

90 1021684-303FCJ • Shroud - Door Cover 1 Gutierrez

ATTACHING PARTS
95 27SR102190 • Rivet - Snap 4
* * *

100 1027989-057 • Arm Linkage - Foodtray A 1

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10174
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
28
-100A 1027989-058 • Arm Linkage - Foodtray B 1
-100B 1027989-067 • Arm Linkage - Foodtray C 1
-100C 1027989-068 • Arm Linkage - Foodtray D 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

ATTACHING PARTS
105 NAS8302-4 • Screw - Washer HD 8
* * *

110 1027888-151 • • Strut - Tray Table AC 1

-110A 1027888-152 • • Strut - Tray Table BD 1
ATTACHING PARTS
115 MS16555-43 • • Pin - Dowel, Headless 4
(Refer to SL-18-017, for More Details
on Loctite® Information)
* * *

120 1027888-123 • • Pivot Link - Tray Table 1

ATTACHING PARTS
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

125 MS16555-43 • • Pin - Dowel, Headless 2

(Refer to SL-18-017, for More Details
on Loctite® Information)
* * *
130 1027888-303ZWZ • • Tray Table - Bumper 1
ATTACHING PARTS
135 MS24693C2 (REF) • • Screw - CSK 2
(True P/N is MS24693-C2)
* * *

140 MFI0304-04 (REF) • • Bearing - Flange, IGUS-Plastic 4 Gutierrez

(True P/N is MFI-0304-04)

145 1027877-107 • • Foodtray Paddle - STD AB 1

-145A 1027877-117 • • Foodtray Paddle - Special CD 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10175
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
28
150 1021684-111 • Rail - Milled Flange 2
ATTACHING PARTS
155 MS24693C24 (REF) • Screw - CSK 6
(True P/N is MS24693-C24)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

* * *

160 NW12-0832-27 (REF) • IGUS - Overmolded Carriage 2

(True P/N is NW-12-0832-27)
165 NW12-0832-27Z (REF) • IGUS - Overmolded Carriage 2
(True P/N is NW-12-0832-27Z)

170 1021473-057MS02 • Foodtray Main Leaf AC 1

-170A 1021473-058MS02 • Foodtray Main Leaf BD 1
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10176
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10177
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

SPREADER
ASSEMBLY (REF)

15
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

15

15

15

Gutierrez

Installation - Endbay
IPL Figure 29

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10178
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
29
-1 1027368-741 (NP) Installation - Endbay RF
(See IPL FIG 1 for NHA)

5 1060372-051MS08 Wall Endbay Assembly - Special RF

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(See IPL FIG 1 for NHA)
(See IPL FIG 36 for DET BKDN)
-5A 1060372-052MS08 Wall Endbay Assembly - Special RF
(See IPL FIG 1 for NHA)
(See IPL FIG 36 for DET BKDN)
-10 1076689-065MS08 Endbay Assembly - IUL RF
(See IPL FIG 1 for NHA)
(See IPL FIG 30 for DET BKDN)
-10A 1076689-076MS08 Endbay Assembly - IUL RF
(See IPL FIG 1 for NHA)
(See IPL FIG 30 for DET BKDN)
ATTACHING PARTS
15 NAS6604-11 • Bolt - HEX HD 4
(Order Separately)
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10179
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

20 45

30

35

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

50
35

25 35

55 35

35

25
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez
1076689-065
ENDBAY ASSEMBLY - IUL

Endbay Assembly - IUL

IPL Figure 30 (Sheet 1 of 8)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10180
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

100
95
70
90

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

75

135

75

65
85

60

75

135 80

105
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

130
110

65
130 125

130
1076689-065
ENDBAY ASSEMBLY - IUL
130 Gutierrez

Endbay Assembly - IUL

IPL Figure 30 (Sheet 2 of 8)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10181
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

13.29"
6.80" NOTE: 3M™ ADHESIVE TRANSFER TAPE (155) TO BE
155 155 1.76"
2X 1.50" APPLIED TO FOAM (145) AS SHOWN IN VIEW A.
4x .50" LOCATION IS NOT CRITICAL AND CAN BE
WITHIN 0.10" OF DIMENSIONS SHOWN.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

3x .25"
155 155

145 165
(REF)

2X 3.00" 10.16"
.15"

A
140
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

150

150

A Gutierrez
150
145
1076689-065
ENDBAY ASSEMBLY - IUL

Endbay Assembly - IUL

IPL Figure 30 (Sheet 3 of 8)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10182
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

20A
45A

30A

35

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

35 50A

25
35

55
35
35

25
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1076689-076 Gutierrez
ENDBAY ASSEMBLY - IUL

Endbay Assembly - IUL

IPL Figure 30 (Sheet 4 of 8)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10183
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

60A 100 95A

70A
90A

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

75

135
65
75

85

130A
135

5
75
80A 15

65
105A
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

110A
130A
125A
130A
120

130A

10
15
130A Gutierrez
1076689-076
ENDBAY ASSEMBLY - IUL

Endbay Assembly - IUL

IPL Figure 30 (Sheet 5 of 8)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10184
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

13.29"
6.80" NOTE: 3M™ ADHESIVE TRANSFER TAPE (155) TO BE
1.76" 155 155
2x 1.50" APPLIED TO FOAM (145A) AS SHOWN IN
4x .50" VIEW B. LOCATION IS NOT CRITICAL AND CAN
BE WITHIN 0.10" OF DIMENSIONS SHOWN.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

3x .25"
155 155

145A
(REF)

10.16" 2x 3.00"
.15"
165A

140A
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

150A

150A

B
145A Gutierrez
150A
1076689-076
ENDBAY ASSEMBLY - IUL

Endbay Assembly - IUL

IPL Figure 30 (Sheet 6 of 8)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10185
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

14.72"
D

.50"
(.15")
D

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

155

50 (REF) (.09") 1.00"

C C

160
.25"
1.50"
.50"

SECTION D-D
.67"

VIEW C-C 155

(REF)

APPLICATION OF TAPES ON BONDED SHROUD ASSEMBLY (50)

60 (REF) .25"
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1.50"
.50"
155

.65"
155 VIEW E-E
E E (REF)

APPLICATION OF TAPE ON BONDED SHROUD ASSEMBLY (60)

Gutierrez
NOTE: 3M™ ADHESIVE TRANSFER TAPE (155) TO BE APPLIED TO BONDED SHROUD
ASSEMBLIES (50, 50A, 60, 60A) AS SHOWN. LOCATION IS NOT CRITICAL AND CAN BE WITHIN 0.10"
OF DIMENSIONS SHOWN. TAPE APPLICATION PROCEDURE FOR BONDED SHROUD
ASSEMBLIES (50, 60) ARE SHOWN IN THE ABOVE ILLUSTRATION. TAPE APPLICATION
PROCEDURE FOR BONDED SHROUD ASSEMBLIES (50A, 60A) ARE SIMILAR.

Endbay Assembly - IUL

IPL Figure 30 (Sheet 7 of 8)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10186
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

3D ELECTRICAL INSTALLATION DRAWINGS ASSOCIATED WITH THIS CMM
ARE AVAILABLE BY REQUEST. REQUESTS FOR 3D PDFs SHOULD BE SENT TO
THE FOLLOWING:
ws_techpubs3d@collins.com

REFER TO USING 3D ELECTRICAL DRAWINGS (PAGE BLOCK 17000)

FOR INFORMATION AND INSTRUCTIONS FOR USING 3D
ELECTRICAL DRAWINGS REFERENCED IN THIS CMM.

REFER TO PART NUMBER(S) CONTAINED IN THE ILLUSTRATED PARTS LIST

FOR PART(S) ORDERING - DO NOT USE THE 3D PDF FOR PART(S) ORDERING.

REFER TO SCHEMATIC AND WIRING DIAGRAMS (PAGE BLOCK 2000)

FOR CABLE ROUTING AND GROUNDING STANDARDS AND PROCEDURES.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

REFER TO ASTRONICS BLOCK DIAGRAM CA7/VOZ 737-8 OF THE IFE SYSTEM FOR
MORE SPECIFIC DETAILS. CONTACT ASTRONICS FOR THE LATEST RELEASED
VERSION OF THIS DOCUMENT (REFER TO INTRODUCTION PAGE BLOCK OF THIS
CMM FOR VENDOR CONTACT INFORMATION).

Gutierrez

Endbay Assembly - IUL

IPL Figure 30 (Sheet 8 of 8)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10187
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10188
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
30
-1 1076689-065MS08 Endbay Assembly - IUL A RF
(See IPL FIG 1 for NHA)
-1A 1076689-076MS08 Endbay Assembly - IUL B RF
(See IPL FIG 1 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 1021685-330FCJ • EPL - Rear Access B 1
10 1021685-398FCJ • EPL - Front Access B 1
ATTACHING PARTS
15 NAS602-8B • Screw - pan HD B 2
* * *

20 1060340-051MS08 • Armcap Assembly - Endbay A 1

20A 1060340-052MS08 • Armcap Assembly - Endbay B 1
ATTACHING PARTS
25 NAS514P428-10B • Screw - CSK 2
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

30 1021685-351FCJ • • Closeout - Armcap, Endbay A 1

30A 1021685-352FCJ • • Closeout - Armcap, Endbay B 1
ATTACHING PARTS
35 27SR0018 • • Rivet - Snap 14
* * *

-40 3M9485PC050 (REF) • • 3M™ Adhesive Transfer Tape AR

(True P/N is 3M9485PC-050)
(Install on Items 45 and 45A Before
Installing Items 30 and 30A)
Gutierrez

45 1060340-053MS08 • • Armcap Subassembly A 1

45A 1060340-054MS08 • • Armcap Subassembly B 1

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10189
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
30
50 1060363-095MS02 • Shroud Assembly - Bonded, Endbay, A 1
PAX
(Refer to SL-21-015 Added as an
Attachment to this CMM for
Replacement of Endbay Shroud Clips)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

50A 1060363-096MS02 • Shroud Assembly - Bonded, Endbay, B 1
PAX
(Refer to SL-21-015 Added as an
Attachment to this CMM for
Replacement of Endbay Shroud Clips)
ATTACHING PARTS
55 27SR1600315 • Rivet - Snap 2
* * *

60 1060363-097MS02 • Shroud Assembly - Bonded, Endbay, A 1

PAX
(Refer to SL-21-015 Added as an
Attachment to this CMM for
Replacement of Endbay Shroud Clips)
60A 1060363-098MS02 • Shroud Assembly - Bonded, Endbay, B 1
PAX
(Refer to SL-21-015 Added as an
Attachment to this CMM for
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Replacement of Endbay Shroud Clips)

ATTACHING PARTS
65 MS24693C49 (REF) • Screw - CSK 2
(True P/N is MS24693-C49)
* * *

70 1047795-051 • Rubstrip Assembly - Endbay A 1

70A 1047795-052 • Rubstrip Assembly - Endbay B 1
ATTACHING PARTS
75 1012042-109 • Screw - Rubstrip 3 Gutierrez

* * *

80 1021685-663 • • Rubstrip - Front, Endbay A 1

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10190
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
30
80A 1021685-664 • • Rubstrip - Front, Endbay B 1
ATTACHING PARTS
85 NAS1352-08LB8P • • Screw - Socket HD, Cap 2

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

* * *

90 1021685-661 • • Rubstrip - FWD, Endbay A 1

90A 1021685-662 • • Rubstrip - FWD, Endbay B 1

95 1021685-665 • Rubstrip - Aft, Endbay A 1

95A 1021685-666 • Rubstrip - Aft, Endbay B 1
ATTACHING PARTS
100 NAS1352-08LB8P • Screw - Socket HD, Cap 2
* * *

105 1059281-057 • Button Assembly - Endbay Arm A 1

(See IPL FIG 31 for DET BKDN)
105A 1059281-062 • Button Assembly - Endbay Arm B 1
(See IPL FIG 31 for DET BKDN)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

ATTACHING PARTS
110 MS24694C4 (REF) • Screw - CSK A 1
(True P/N is MS24694-C4)
110A MS24694C5 (REF) • Screw - CSK B 1
(True P/N is MS24694-C5)
-115 VC161-3 (REF) • Cap - Vinyl B 1
(True P/N is VC-161-3)
120 NAS1801-08-4 • Screw - HEX HD B 1
* * *
Gutierrez
125 1048430-001MS02 • Shroud Assembly - Endbay A 1
125A 1048430-024MS02 • Shroud Assembly - Endbay B 1
ATTACHING PARTS
130 27SR2000370 • Rivet - Snap A 10
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10191
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
30
130A 27SR2000370 • Rivet - Snap B 9
135 NAS601-3P • Screw - Pan HD 2
* * *

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

140 1046962-303FCI • Shroud - Endbay, PAX Side A 1
140A 1054903-302FCI • Shroud - Endbay, PAX Side B 1

145 1021685-411 • Foam - Endbay Shroud, PAX Side A 1

145A 1021685-403 • Foam - Endbay Shroud, PAX Side B 1
ATTACHING PARTS
150 27SR2000370 • Rivet - Snap A 5
150A 27SR2000370 • Rivet - Snap B 4
* * *

155 3M9485PC050 (REF) • 3M™ Adhesive Transfer Tape AR

(True P/N is 3M9485PC-050)
160 3M5958-1 • 3M™ Tape - DBL Sided AR
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(Attach to Items 50 and 50A)

165 1060733-781 • Endbay Bracket Assembly - INBD A 1

(See IPL FIG 32 for DET BKDN)
165A 1060733-014 • Endbay Bracket Assembly - INBD B 1
(See IPL FIG 32 for DET BKDN)

-170 1076691-041 (NP) • Installation - Endbay Electrical, IUL A 1

(See SCHEMATIC AND WIRING
DIAGRAMS [Page Block 2000])
Gutierrez
(See USING 3D ELECTRICAL
DRAWINGS [Page Block 17000])
(3D PDF 1097112-703 and
1097112-707 [Available Upon
Request])

(3D Bubble Number 900)

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10192
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
30
-170A 1076691-058 (NP) • Installation - Endbay Electrical, IUL B 1

(See SCHEMATIC AND WIRING

DIAGRAMS [Page Block 2000])

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(See USING 3D ELECTRICAL
DRAWINGS [Page Block 17000])

(3D PDF 1097112-701 and

1097112-705 [Available Upon
Request])

(3D Bubble Number 900)

-175 1170821-44 • • Cable Assembly - ISPS to IUL 1

(Order Separately)
(3D Bubble Number 351)
-180 FTH3-01 (REF) • • Push Mount - Cable Tie A 3
(Order Separately by True P/N
FTH-3-01)
(3D Bubble Number 658)
-180A FTH3-01 (REF) • • Push Mount - Cable Tie B 6
(Order Separately by True P/N
FTH-3-01)
(3D Bubble Number 658)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

-185 MS3367-4-9 • • Strap - Tiedown, Adjustable 11

(Order Separately)
(3D Bubble Number 629)
-190 MS3367-5-9 • • Strap - Tiedown, Adjustable 11
(Order Separately)
(3D Bubble Number 631)
-195 5672500572 • • ROUNDIT® 2000 MA AR
(Order Separately)
(3D Bubble Number 700)
-200 5672500872 • • ROUNDIT® 2000 MA B AR
(Order Separately)
(3D Bubble Number 701)
-205 44960101 • • PMA _ Aisle Light Harness B 2 Gutierrez
(Order Separately)
(3D Bubble Number 550)
* * *

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10193
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5

20
35

15

10

15
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

25
30
Gutierrez

Button Assembly - Endbay Arm

IPL Figure 31

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10194
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
31
-1 1059281-057 Button Assembly - Endbay Arm, LH A RF
(See IPL FIG 30 for NHA)
-1A 1059281-062 Button Assembly - Endbay Arm, RH B RF
(See IPL FIG 30 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 1059281-161 • Button - Endbay Arm A 1
-5A 1059281-162 • Button - Endbay Arm B 1
ATTACHING PARTS
10 1021685-143 • Pin - Button 1
15 MS16633-1012 • Ring - Retaining, External 2
20 LE037C00M • Spring - Helical, Extension 1
* * *

25 SP2063 • Pulley 1
ATTACHING PARTS
30 MS51576-2 • Screw - Socket HD, Shoulder 1
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

35 1059281-165 • Button Housing - Endbay Arm A 1

-35A 1059281-172 • Button Housing - Endbay Arm B 1
* * *

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10195
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

5
10

35
40
25

25

20 Gutierrez

15

Endbay Bracket Assembly - INBD

IPL Figure 32

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10196
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
32
-1 1060733-014 Endbay Bracket Assembly - INBD A RF
(See IPL FIG 30 for NHA)
-1A 1060733-781 Endbay Bracket Assembly - INBD B RF
(See IPL FIG 30 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 1021685-137 • Handicap Latch - Discrete Button 1
(To be Installed After Item 15)
ATTACHING PARTS
10 MS24693C25 (REF) • Screw - CSK 1
(True P/N is MS24693-C25)
* * *

15 SP25897C1630 • Control Cable A 1

-15A SP25897C1430 • Control Cable B 1
20 1059281-105 • Ferrule - Cable 1
ATTACHING PARTS
25 MS16633-2025 • Ring - Retaining, External 2
-30 MS3367-4-0 • Strap - Tiedown, Adjustable B 2
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

* * *

35 1060357-788 • Side Bracket - Endbay PAX, RH A 1

-35A 1060357-781 • Side Bracket - Endbay PAX, LH B 1

40 1060355-004 • • Bowtie Assembly - Endbay Arm A 1

(See IPL FIG 33 for DET BKDN)
-40A 1060355-003 • • Bowtie Assembly - Endbay Arm B 1
(See IPL FIG 33 for DET BKDN)

Gutierrez
-45 1021685-758 • • Bracket Assembly - PAX Side A 1
(Must Purchase NHA - Item 35)
-45A 1021686-005 • • Bracket Assembly - PAX Side B 1
(Must Purchase NHA - Item -35A)

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10197
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
32
-50 1054904-051 • • • Fodder Guard Assembly 1
(Refer to SB 25-GENXMIQ-05 for
the Installation of Armrest FOD
Seal)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10198
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10199
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

15
10 45

Gutierrez
WARNING: USE EXTREME CAUTION WHEN CONNECTING OR DISCONNECTING THE SCREW (10)
OR INJURY CAN RESULT. THIS SCREW SECURES THE CABLE OF THE SPRING REEL
AND IS UNDER HIGH TENSION!

Bowtie Assembly - Endbay Arm

IPL Figure 33 (Sheet 1 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10200
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

105

35
130 40 145
115

125

60

110
55 120
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

110
20

135
50 110
140
65
110
30 55 60
25
110
100

Gutierrez

Bowtie Assembly - Endbay Arm

IPL Figure 33 (Sheet 2 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10201
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
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RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

70

90

95
80 75

90 90 85
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

1021685-015
PIVOT ASSEMBLY - ENDBAY ARM - LH

Gutierrez

Bowtie Assembly - Endbay Arm

IPL Figure 33 (Sheet 3 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10202
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
33
-1 1060355-003 Bowtie Assembly - Endbay Arm, LH A RF
(See IPL FIG 32 for NHA)
-1A 1060355-004 Bowtie Assembly - Endbay Arm, RH B RF
(See IPL FIG 32 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 1060358-003 • Endbay Arm Assembly - INBD, LH A 1
(See IPL FIG 34 for DET BKDN)
-5A 1060358-004 • Endbay Arm Assembly - INBD, RH B 1
(See IPL FIG 34 for DET BKDN)
ATTACHING PARTS
10 NAS602-20P • Screw - Pan HD 1
15 1021685-653 • Spacer - Bolt 1
* * *

20 ML1912 (REF) • Reel - Arbor Mount 1

(True P/N is ML-1912)
(Refer to SL-16-051 for Reel
Adjustment)
ATTACHING PARTS
25 MS24693-25B • Screw - CSK 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

30 NAS1169-8L • Washer - Dimpled, CSK 1

* * *

35 1058817-107 • Reel Adjuster - IAT 1

ATTACHING PARTS
40 NAS1352C06-6 • Screw - Socket HD Cap 1
* * *

45 1021685-071 • Bowtie Endbay Assembly - LH A 1 Gutierrez

-45A 1021685-072 • Bowtie Endbay Assembly - RH B 1

50 1021685-015 • • Pivot Assembly - Endbay Arm, LH A 1

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10203
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
33
-50A 1021685-016 • • Pivot Assembly - Endbay Arm, RH B 1
ATTACHING PARTS
55 NAS601-10P • • Screw - Pan HD 4

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

60 1021685-159 • • Cap - Latch, 1 piece A 2
-60A 1021685-160 • • Cap - Latch, 1 piece B 2
65 LE022B001M • • Spring - Helical, Extension 1
* * *

70 1031754-107 • • • Latch - Handicap, FWD, LH A 1

-70A 1031754-108 • • • Latch - Handicap, FWD, RH B 1
ATTACHING PARTS
75 NAS1352-06-6P • • • Screw - Socket HD Cap 1
(Torque to 26 ±2 IN-LB)
* * *

80 1021685-117 • • • Latch - Handicap, Aft 1

ATTACHING PARTS
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

85 NAS1352-06-6P • • • Screw - Socket HD Cap 1

(Torque to 26 ±2 IN-LB)
* * *

90 RFI0607-04 (REF) • • • Bearing - Flange 4

(True P/N is RFI-0607-04)

95 1021685-115 • • • Pivot - Endbay Arm 1

100 1021685-121 • • Rollon Rail - Trimmed Aft 1 Gutierrez

105 1021685-123 • • Rollon Rail - Trimmed FWD 1

ATTACHING PARTS
110 CBSTSE4-10 • • Screw - Socket HD Cap 5
* * *
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10204
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
33
115 1021685-061 • • Bowtie Endbay Assembly - Riveted, A 1
LH
-115A 1021685-062 • • Bowtie Endbay Assembly - Riveted, B 1
RH

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

120 1021685-193 • • • Strut - Stew Step A 1
-120A 1021685-194 • • • Strut - Stew Step B 1
ATTACHING PARTS
125 NAS1352-08-6P • • • Screw - Socket HD Cap 2
* * *

130 1059731-101 • • • Bracket - Adjuster Restrain 1

ATTACHING PARTS
135 NPS24693S49 (REF) • • • Screw - CSK 2
(True P/N is NPS24693-S49)
* * *

140 1021685-305ZYN • • • Cord Guide - Spring Reel 1

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

ATTACHING PARTS
145 SSDH43BS • • • Rivet - Dome, Pop 4
* * *

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10205
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

130
125

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

130
160 125

115 A
120 155

100
105
110
95

70 85
75 90
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

80
65 35
50
60
55

135

145
45
140 30
40

5
20 Gutierrez
150 15
10
25

Endbay Arm Assembly - INBD

IPL Figure 34

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10206
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
34
-1 1060358-003 Endbay Arm Assembly - INBD, LH A RF
(See IPL FIG 33 for NHA)
-1A 1060358-004 Endbay Arm Assembly - INBD, RH B RF
(See IPL FIG 33 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 CSW18-60-2RSU (REF) • C-Slider - Rollon, U-Type 1
(True P/N is CSW18-60-2RS-U)
ATTACHING PARTS
10 CBSM5-10 • Screw - Socket HD Cap 2
(Torque to 45 ±5 IN-LB)
15 NL5 • Washer - Nord-Lock 2
* * *

20 1021685-269 • Mount Plate - Carriage Arm 1

ATTACHING PARTS
25 NAS6603-1 • Bolt - HEX HD 2
(Torque to 60 ±5 IN-LB)
30 NL5 • Washer - Nord-Lock 2
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

35 CSW18-60-2RSU (REF) • C-Slider - Rollon, U-Type 1

(True P/N is CSW18-60-2RS-U)
ATTACHING PARTS
40 CBSM5-10 • Screw - Socket HD Cap 2
(Torque to 45 ±5 IN-LB)
45 NL5 • Washer - Nord-Lock 2
* * *

50 1021685-263 • Mount Plate - Carriage Arm 1 Gutierrez

ATTACHING PARTS
55 NAS6603-1 • Bolt - HEX HD 2
(Torque to 60 ±5 IN-LB)
60 NL5 • Washer - Nord-Lock 2
* * *
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10207
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
34
65 CSW18-60-2RST (REF) • C-Slider - Rollon, T-Type 1
(True P/N is CSW18-60-2RS-T)
ATTACHING PARTS
70 CBSM5-10 • Screw - Socket HD Cap 2

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(Torque to 45 ±5 IN-LB)
75 NL5 • Washer - Nord-Lock 2
* * *

80 1021685-269 • Mount Plate - Carriage Arm 1

ATTACHING PARTS
85 NAS6603-1 • Bolt - HEX HD 2
(Torque to 60 ±5 IN-LB)
90 NL5 • Washer - Nord-Lock 2
* * *

95 CSW18-60-2RST (REF) • C-Slider - Rollon, T-Type 1

(True P/N is CSW18-60-2RS-T)
ATTACHING PARTS
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

100 CBSM5-10 • Screw - Socket HD Cap 2

(Torque to 45 ±5 IN-LB)
105 NL5 • Washer - Nord-Lock 2
* * *

110 1021685-267 • Mount Plate - Carriage Arm 1

ATTACHING PARTS
115 NAS6603-1 • Bolt - HEX HD 2
(Torque to 60 ±5 IN-LB)
120 NL5 • Washer - Nord-Lock 2
Gutierrez
* * *

125 1021685-049 • Hinge Assembly - Armcap 2

ATTACHING PARTS

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10208
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
34
130 NAS1352-08LB6 • Screw - Socket HD Cap 2
* * *

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

135 1021685-195 • • Hinge - Machined, Endbay Arm 1
ATTACHING PARTS
140 MS20253-2-103 • • Pin - Hinge 1
(Assemble Item 140 into
Clearance Hole of Item 150, thru
Items 135 and 145, and Press Fit
into the Far Side of Item 150 Flush at
the End)
145 1021685-261 • • Spring - Hinge 1
* * *

150 1021686-131 • • Base - Hinge, Endbay Arm 1

155 1030130-303ZXK • Cover - Hinge 1

160 1060369-009 • Frame Assembly - Endbay Arm A 1

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

(See IPL FIG 35 for DET BKDN)

-160A 1060369-010 • Frame Assembly - Endbay Arm B 1
(See IPL FIG 35 for DET BKDN)
* * *

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10209
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

10

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

10
5

60
15

20
40

25 45 50
110
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

100
30 105
35

60 60

55

60

WARNING: USE EXTREME CAUTION WHEN CONNECTING OR DISCONNECTING THE BOLT (100)
OR INJURY CAN RESULT. THIS BOLT SECURES THE CABLE OF THE SPRING REEL Gutierrez
AND IS UNDER HIGH TENSION!

Frame Assembly - Endbay Arm

IPL Figure 35 (Sheet 1 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10210
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

70

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

70

70
65

85

75
90
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

80
85

95

Gutierrez
1060365-001
ENDBAY ARM FRAME ASSEMBLY - INNER

Frame Assembly - Endbay Arm

IPL Figure 35 (Sheet 2 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10211
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10212
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
35
-1 1060369-009 Frame Assembly - Endbay Arm A RF
(See IPL FIG 34 for NHA)
-1A 1060369-010 Frame Assembly - Endbay Arm B RF
(See IPL FIG 34 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 1021685-793 • Table Latch Assembly A 1
(See IPL FIG 38 for DET BKDN)
-5A 1021685-794 • Table Latch Assembly B 1
(See IPL FIG 38 for DET BKDN)
ATTACHING PARTS
10 MS24693-49B • Screw - CSK 4
* * *

15 MS16633-2025 • Ring - Retaining 1

20 1060363-081 • Door Assembly - Cord Reel Access A 1

-20A 1060363-082 • Door Assembly - Cord Reel Access B 1
ATTACHING PARTS
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

25 MS24693C47 (REF) • Screw - CSK 2

(True P/N is MS24693-C47)
30 MS24693-46B • Screw - CSK 1
* * *

35 1050222-451 • • Placard - Reel Under Tension 1

“ATTENTION - CORD REEL UNDER
TENSION REFER TO CMM FOR
MAINTENANCE INSTRUCTIONS”

40 1050222-151 • • Door - Cord Reel Access A 1 Gutierrez

-40A 1050222-152 • • Door - Cord Reel Access B 1

45 1058817-105 • Reel Adjuster - IAT 1

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10213
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
35
50 301344-1 • Reel - Mechanical 1
(Refer to SL-16-051 for Reel
Adjustment)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

55 1060365-001 • Endbay Arm Frame Assembly - Inner A 1
-55A 1060365-002 • Endbay Arm Frame Assembly - Inner B 1
ATTACHING PARTS
60 NAS1351-4-10 • Screw - Socket HD Cap 4
* * *

65 1060363-119 • • Handhold - Endbay Arm A 1

-65A 1060363-120 • • Handhold - Endbay Arm B 1
ATTACHING PARTS
70 MS24693-25B • • Screw - CSK 3
* * *

75 1021685-011 • • Stop Block Assembly - Endbay Arm 1

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

ATTACHING PARTS
80 MS27039-1-07 • • Screw - Pan HD 2
* * *

85 11528 • • • Bumper - Grommet 2

90 1021685-111 • • • Stop Block - Endbay Arm 1

95 1060695-051 • • Frame Assembly - Endbay Inner LH A 1

Gutierrez
-95A 1060695-052 • • Frame Assembly - Endbay Inner RH B 1

100 NAS1297-3-2 • Bolt - HEX, Shoulder 1

105 11528 • Bumper - Grommet 1

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10214
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
35
110 1060364-001 • Frame Assembly - Endbay Arm, Outer A 1
(See IPL FIG 39 for DET BKDN)
-110A 1060364-002 • Frame Assembly - Endbay Arm, Outer B 1
(See IPL FIG 39 for DET BKDN)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10215
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

50

45

10 20

55
20
50 30
20 15
20
20 5

60

10
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

40
50

40 40

40

40

40 Gutierrez
35

Wall Endbay Assembly - Special

IPL Figure 36 (Sheet 1 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10216
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

80

70
70

70
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

70

65

Gutierrez

Wall Endbay Assembly - Special

IPL Figure 36 (Sheet 2 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10217
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

90

90
85

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

85

120
A

115

135
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

95

105
100

125

110
Gutierrez
A

1060368-001 130
ENDBAY WALL ASSEMBLY - SPECIAL - OUTER

Wall Endbay Assembly - Special

IPL Figure 36 (Sheet 3 of 3)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10218
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
36
-1 1060372-051MS08 Wall Endbay Assembly - Special A RF
(See IPL FIG 1 for NHA)
-1A 1060372-052MS08 Wall Endbay Assembly - Special B RF
(See IPL FIG 1 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 1060340-051MS08 • Armcap Assembly - Endbay A 1
-5A 1060340-052MS08 • Armcap Assembly - Endbay B 1
ATTACHING PARTS
10 NAS514P428-10B • Screw - CSK 2
* * *

15 1021685-351FCJ • • Closeout - Armcap, Endbay A 1

-15A 1021685-352FCJ • • Closeout - Armcap, Endbay B 1
ATTACHING PARTS
20 27SR0018 • • Rivet - Snap 14
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

-25 3M9485PC050 (REF) • • 3M™ Adhesive Transfer Tape AR

(True P/N is 3M9485PC-050)
(Attach on Items 30 and -30A Before
Installing Items 15 and -15A)

30 1060340-053MS08 • • Armcap Subassembly A 1

-30A 1060340-054MS08 • • Armcap Subassembly B 1

35 1050222-363FCJ • Shroud - Wall PAX Side, Special A 1

Endbay
-35A 1050222-364FCJ • Shroud - Wall PAX Side, Special B 1 Gutierrez
Endbay
ATTACHING PARTS
40 27SR0020 • Rivet - Snap 8
* * *

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10219
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
36
45 1050222-369FCJ • Aft Shroud - Wall PAX, Special Endbay A 1
-45A 1050222-370FCJ • Aft Shroud - Wall PAX, Special Endbay B 1
ATTACHING PARTS

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

50 27SR1600315 • Rivet - Snap 6
* * *

55 1060363-091MS02 • Bonded Shroud Assembly - PAX, A 1

Special Endbay
(Refer to SL-21-015 Added as an
Attachment to this CMM for
Replacement of Endbay Shroud Clips)
-55A 1060363-092MS02 • Bonded Shroud Assembly - PAX, B 1
Special Endbay
(Refer to SL-21-015 Added as an
Attachment to this CMM for
Replacement of Endbay Shroud Clips)
ATTACHING PARTS
60 27SR1600315 • Rivet - Snap 1
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

65 1050222-305FCJ • Shroud - Wall Side, Special Endbay A 1

-65A 1050222-306FCJ • Shroud - Wall Side, Special Endbay B 1
ATTACHING PARTS
70 27SR1600315 • Rivet - Snap 4
* * *

-75 3M9485PC050 (REF) • 3M™ Adhesive Transfer Tape AR

(True P/N is 3M9485PC-050)

Gutierrez
80 1060368-001 • Endbay Wall Assembly - Special, Outer A 1
(Attach Edge with Structural Adhesive
Loctite®-3412)

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10220
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
36
-80A 1060368-002 • Endbay Wall Assembly - Special, Outer B 1
(Attach Edge with Structural Adhesive
Loctite®-3412)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

85 1021685-049 • • Hinge Assembly - Armcap 2
ATTACHING PARTS
90 NAS1352-08LB6 • • Screw - Socket HD Cap 2
* * *

95 1021685-195 • • • Hinge - Machined, Endbay Arm 1

ATTACHING PARTS
100 MS20253-2-103 • • • Pin - Hinge 1
(Assemble Item 100 into
Clearance Hole of Item 110, thru
Items 95 and 105, and Press Fit
into the Far Side of Item 110 Flush
at the End)
105 1021685-261 • • • Spring - Hinge 1
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

110 1021686-131 • • • Base - Hinge, Endbay Arm 1

115 1030130-301ZXK • • Cover - Hinge 1

ATTACHING PARTS
120 MS27039C0810 • • Screw - Pan HD 1
* * *

125 1021687-109 • • Baggage Bar - Wall, Special Endbay 1

Gutierrez
ATTACHING PARTS
130 NAS601-7B • • Screw - Pan HD 3
* * *

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10221
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
36
135 1060369-013 • • Endbay Wall Arm Assembly - Special A 1
(See IPL FIG 37 for DET BKDN)
-135A 1060369-014 • • Endbay Wall Arm Assembly - Special B 1
(See IPL FIG 37 for DET BKDN)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10222
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10223
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

10

10
5

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

15
50
45 75

25
60 65

60

30 20
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

35 40
60 70

60

60

55

60

Gutierrez

WARNING: USE EXTREME CAUTION WHEN CONNECTING OR DISCONNECTING THE BOLT (65)
OR INJURY CAN RESULT. THIS BOLT SECURES THE CABLE OF THE SPRING REEL
AND IS UNDER HIGH TENSION!

Endbay Wall Arm Assembly - Special

IPL Figure 37

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10224
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
37
-1 1060369-013 Endbay Wall Arm Assembly - Special A RF
(See IPL FIG 36 for NHA)
-1A 1060369-014 Endbay Wall Arm Assembly - Special B RF
(See IPL FIG 36 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 1021685-793 • Table Latch Assembly A 1
(See IPL FIG 38 for DET BKDN)
-5A 1021685-794 • Table Latch Assembly B 1
(See IPL FIG 38 for DET BKDN)
ATTACHING PARTS
10 MS24693-48B • Screw - CSK 4
* * *

15 MS16633-2025 • Ring - Retaining, External 1

20 1060363-081 • Door Assembly - Cord Reel Access A 1

-20A 1060363-082 • Door Assembly - Cord Reel Access B 1
ATTACHING PARTS
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

25 MS24693C47 (REF) • Screw - CSK 2

(True P/N is MS24693-C47)
30 MS24693-46B • Screw - CSK 1
* * *

35 1050222-451 • • Placard - Reel Under Tension 1

(“ATTENTION - CORD REEL
UNDER TENSION REFER TO CMM
FOR MAINTENANCE
INSTRUCTIONS”)

Gutierrez
40 1050222-151 • • Door - Cord Reel Access A 1
-40A 1050222-152 • • Door - Cord Reel Access B 1

45 1058817-105 • Reel Adjuster - IAT 1

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10225
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
37
50 301344-1 • Reel - Mechanical 1
(Refer to SL-16-051 for Reel
Adjustment)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

55 1060695-055 • Endbay Wall Assembly - Special A 1
-55A 1060695-056 • Endbay Wall Assembly - Special B 1
ATTACHING PARTS
60 NAS1351-4-10 • Screw - Socket HD Cap 7
* * *

65 NAS1297-3-2 • Bolt - HEX HD, Shoulder 1

70 11528 • Bumper - Grommet 1

75 1060364-005 • Endbay Wall Arm Assembly - Special, A 1

Outer
(See IPL FIG 39 for DET BKDN)
-75A 1060364-006 • Endbay Wall Arm Assembly - Special, B 1
Outer
(See IPL FIG 39 for DET BKDN)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

* * *

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10226
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10227
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

30

20
15

10
25
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

35
5

Gutierrez

Table Latch Assembly

IPL Figure 38

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10228
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
38
-1 1021685-793 Table Latch Assembly A RF
(See IPL FIGS 35 and 37 for NHA)
-1A 1021685-794 Table Latch Assembly B RF
(See IPL FIGS 35 and 37 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 1021685-677 • Latch - Table Release A 1
-5A 1021685-678 • Latch - Table Release B 1
ATTACHING PARTS
10 MS16555-32 • Pin - Dowel, Headless 1
* * *

15 EIM030D04M • Spring - Helical, Extension 1

(To be Securely Fastened to Item 5 and
Item 35 with Provided Holes.
To be Installed After Entire
Subassembly has been Assembled)

20 1021685-173 • Cable Adapter 1

ATTACHING PARTS
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

25 NAS1801-08-20 • Screw - HEX HD 1

(Torque to 15 ±4 IN-LB)
30 MS21042-08 • Nut - LKG 1
* * *

35 1021685-169 • Housing - Table Latch 1

* * *

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10229
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

20 10

25

75

80
35

80
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

80 65

40
30 15
60 45
55 50 100
70
60
Gutierrez

1060364-001
ENDBAY ARM FRAME ASSEMBLY - OUTER

Frame Assembly - Endbay Arm - Outer

IPL Figure 39 (Sheet 1 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10230
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

90

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

85
10
5A

95 20
25

75A

95 35
80

80
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

100B
95
80
65

40 15
30
45
50

60
55
60 70
80

Gutierrez

1060364-005
ENDBAY WALL ARM ASSEMBLY - SPECIAL - OUTER

Frame Assembly - Endbay Arm - Outer

IPL Figure 39 (Sheet 2 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10231
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10232
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
39
-1 1060364-001 Frame Assembly - Endbay Arm, Outer A RF
(See IPL FIG 35 for NHA)
-1A 1060364-002 Frame Assembly - Endbay Arm, Outer B RF
(See IPL FIG 35 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

-1B 1060364-005 Endbay Wall Arm Assembly - Special, C RF
Outer
(See IPL FIG 37 for NHA)
-1C 1060364-006 Endbay Wall Arm Assembly - Special, D RF
Outer
(See IPL FIG 37 for NHA)

5 AC11429-00 • Latch Cable - Foodtray AB 1

5A AC11427-00 • Latch Cable - Foodtray CD 1
ATTACHING PARTS
10 MS3367-5-9 • Strap - Tiedown, Adjustable 4
15 MS16633-2025 • Ring - Retaining, External 1
* * *

20 UP4125 • Pulley 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

ATTACHING PARTS
25 NAS6604-4 • Bolt - HEX HD 1
* * *

30 1030486-119 • Latch - Release 1

ATTACHING PARTS
35 MS24693S276 (REF) • Screw - CSK 1
(True P/N is MS24693-S276)
40 LC026EE10S • Spring - Helical, Compression 1
Gutierrez
45 NAS77-3-026 • Bushing - Flanged, Press Fit 1
50 MS21042-3 • Nut - LKG 1
* * *

55 1021685-001 • Table Mount Assembly AC 1

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10233
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
39
-55A 1021685-002 • Table Mount Assembly BD 1
ATTACHING PARTS
60 NA0069A030006 (REF) • Screw - Socket HD Cap 8
(True P/N is NA0069-A030006)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(Attach Loctite®-243 to Threads)
* * *

65 11528 • • Bumper - Grommet 1

70 1021685-101 • • Table Mount Block AC 1

-70A 1021685-102 • • Table Mount Block BD 1

75 2SRS9XMUU400 (REF) • Rail - Thick AB 1

(True P/N is 2SRS9XMUU+400LM)
75A 2SRS9XMUU375 (REF) • Rail - Thick CD 1
(True P/N is 2SRS9XMUU+375LM)
ATTACHING PARTS
80 NA0069A030006 (REF) • Screw - Socket HD Cap 7
(True P/N is NA0069-A030006)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

* * *

85 1050223-165 • Hinge - Support C 1

-85A 1050223-166 • Hinge - Support D 1
ATTACHING PARTS
90 MS27039C0805 • Screw - Pan HD CD 1
95 NAS514P832-5 • Screw - CSK CD 5
* * *
Gutierrez

100 1060694-051 • Endbay Arm Frame Assembly - Riveted A 1

-100A 1060694-052 • Endbay Arm Frame Assembly - Riveted B 1

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10234
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
39
100B 1060694-055 • Endbay Special Wall Assembly C 1
Riveted
-100C 1060694-056 • Endbay Special Wall Assembly D 1
Riveted

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10235
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

10

10

10
20 5
25
10
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

55 30
35
50 45
40

60
1097109-701
INSTALLATION - SHROUD

Gutierrez

Installation - Shroud
IPL Figure 40 (Sheet 1 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10236
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

95
100

105
85
110

100

115

95 100
110 100
100 90
95
105
110
100
105
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

80 65
1097109-701 70
INSTALLATION - SHROUD
75

Gutierrez

Installation - Shroud
IPL Figure 40 (Sheet 2 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10237
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10238
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
40
-1 1097109-701MS02 (NP) Installation - Shroud A RF
(See IPL FIG 1 for NHA)
-1A 1097109-703MS02 (NP) Installation - Shroud B RF
(See IPL FIG 1 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 1071964-055MS02 • Mount Plate / Shroud Assembly A 1
(Order Separately)
-5A 1071964-057MS02 • Mount Plate / Shroud Assembly B 1
(Order Separately)
ATTACHING PARTS
10 MS3367-7-9 • Strap - Tiedown, Adjustable 8
(Order Separately)
-15 3M5958-1 • 3M™ Tape - Double Sided AR
(Order Separately)
* * *

20 M225292-5R100 (REF) • • Grommet - Edging AR

(True P/N is M22529/2-5R-100)
(Attach with Loctite®-454)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

25 1071964-313DV0 (REF) • • Shroud - ISPS A 1

(True P/N is 1071964-313DVO)
-25A 1071964-314DV0 (REF) • • Shroud - ISPS B 1
(True P/N is 1071964-314DVO)

30 1064529-053MS02 • • Door Assembly - IFE Shroud 1

35 1064524-307DV0 (REF) • • • Face Plate - IFE Shroud 1

(True P/N is 1064524-307DVO)
ATTACHING PARTS
40 82-19-220-16 • • • Stud - Quarter-Turn 4 Gutierrez

45 43-13-1-24 • • • Spring - Conical 4

50 82-46-101-41 • • • Washer - Cupped 4
55 82-32-201-20 • • • Retainer - Push-On 4
* * *
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10239
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
40
60 1061798-711MS02 (NP) • Installation - Disconnect A 1
-60A 1061798-712MS02 (NP) • Installation - Disconnect B 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

65 1061798-061MS02 • • Disconnect Shroud Assembly A 1
(Order Separately)
-65A 1061798-062MS02 • • Disconnect Shroud Assembly B 1
(Order Separately)

70 1061798-307DV0 (REF) • • • Disconnect Shroud A 1

(True P/N is 1061798-307DVO)
-70A 1061798-308DV0 (REF) • • • Disconnect Shroud B 1
(True P/N is 1061798-308DVO)
ATTACHING PARTS
75 D8-316-716-190 • • • Stud - Quarter-Turn 4
80 D8-326-101-200 • • • Retainer - Push-On 4
* * *

85 1061798-069 • • Disconnect Bracket Assembly A 1

(Order Separately)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

-85A 1061798-070 • • Disconnect Bracket Assembly B 1

(Order Separately)
90 1061798-309DV0 (REF) • • Disconnect Leg Isolator A 1
(Order Separately by True P/N
1061798-309DVO)
-90A 1061798-310DV0 (REF) • • Disconnect Leg Isolator B 1
(Order Separately by True P/N
1061798-310DVO)
ATTACHING PARTS
95 NAS6604-18 • • Bolt - HEX HD 3
(Order Separately)
Gutierrez
100 98038241 • • Spacer - Nylon 10
(Order Separately)
105 42NKE048 (REF) • • Nut - LKG 3
(Order Separately by True P/N
42NKE-048)
* * *
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10240
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
40
110 D8-336-200-190 • • • Receptacle - Quarter-Turn 4

115 M225292-2R100 (REF) • • • Grommet - Edging AR

(True P/N is M22529/2-2R-100)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(Attach with Loctite®-454)

-120 3M5958-1 • • 3M™ Tape - Double Sided AR

(Order Separately)
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10241
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

CENTER CONSOLE
ASSEMBLY (REF)
FRAME ASSEMBLY (REF)

80 70

75

80
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

80

80

CENTER CONSOLE
ASSEMBLY (REF)

Gutierrez

Installation - Electrical Raceway

IPL Figure 41 (Sheet 1 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10242
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

20

15 20 35

35
30
65
30 35

20
20
15 50
20
35 60

35
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

20
40

45

5 10

Gutierrez

Installation - Electrical Raceway

IPL Figure 41 (Sheet 2 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10243
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10244
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
41
-1 1097110-701MS02 (NP) Installation - Electrical Raceway A RF
(See IPL FIG 1 for NHA)
-1A 1097110-703MS02 (NP) Installation - Electrical Raceway B RF
(See IPL FIG 1 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 1045427-337DV0 (REF) • Spreader Cover 2
(Order Separately by True P/N
1045427-337DVO)
ATTACHING PARTS
10 MS3367-5-9 • Strap - Tiedown, Adjustable 2
(Order Separately)
* * *

15 1040966-317ZYN • Pancake - Raceway 2

(Order Separately)
ATTACHING PARTS
20 MS3367-7-9 • Strap - Tiedown, Adjustable 4
(Order Separately)
-25 3M5958-1 • 3M™ Tape - Double Sided AR
(Order Separately)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

* * *

30 1041035-331DV0 (REF) • Pancake - Raceway 2

(Order Separately by True P/N
1041035-331DVO)
ATTACHING PARTS
35 MS3367-7-9 • Strap - Tiedown, Adjustable 4
(Order Separately)
40 3M5958-1 • 3M™ Tape - Double Sided AR
(Order Separately)
* * * Gutierrez

45 1061964-319ZYN • Pancake - Raceway 1

(Order Separately)
ATTACHING PARTS

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10245
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
41
50 MS3367-7-9 • Strap - Tiedown, Adjustable 2
(Order Separately)
-55 3M5958-1 • 3M™ Tape - Double Sided AR
(Order Separately)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

* * *

60 1050914-359DV0 (REF) • Shroud - Leg IFE Isolator 1

(Order Separately by True P/N
1050914-359DVO)
ATTACHING PARTS
65 MS3367-5-9 • Strap - Tiedown, Adjustable 2
(Order Separately)
* * *

70 1071964-311DV0 (REF) • Shroud - Console IFE 1

(Order Separately by True P/N
1071964-311DVO)
75 1027372-393DV0 (REF) • Shroud - Cable Protection 1
(Order Separately by True P/N
1027372-393DVO)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

ATTACHING PARTS
80 3M5958-1 • 3M™ Tape - Double Sided AR
(Order Separately)
* * *

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10246
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10247
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

IUL ENDBAY

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

ASSEMBLY
(REF)

LEG ASSEMBLY
(REF)

WALL ENDBAY
ASSEMBLY (REF)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

20
5

15
10

50 40

25

35
Gutierrez
30

Installation - Baggage Bar

IPL Figure 42

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10248
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
42
-1 1061905-003 (NP) Installation - Baggage Bar A RF
(See IPL FIG 1 for NHA)
-1A 1061905-004 (NP) Installation - Baggage Bar B RF
(See IPL FIG 1 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 1062416-137 • Tube - Baggage Bar, STD 1
(Order Separately)
ATTACHING PARTS
10 MS27039-1-14 • Screw - Pan HD 1
(Order Separately)
15 AN970-3 • Washer - Flat 1
(Order Separately)
20 AN565A1032H12 • Screw - Set 1
(Order Separately)
* * *

25 1062416-135 • Tube - Baggage Bar, Canted A 1

(Order Separately)
-25A 1062416-136 • Tube - Baggage Bar, Canted B 1
(Order Separately)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

ATTACHING PARTS
30 MS27039-1-14 • Screw - Pan HD 1
(Order Separately)
35 AN970-3 • Washer - Flat 1
(Order Separately)
40 AN565A1032H12 • Screw - Set 1
(Order Separately)
* * *

-45 1089825-101 • Doubler - Baggage Bar 1

(Order Separately) Gutierrez
50 1004710-007 • Plug - Baggage Bar 4
(Order Separately)
* * *

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10249
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

10

55
35

30
50

55

40
45
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

20

25
50

15 15

20

25

Gutierrez

Frame Assembly
IPL Figure 43

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10250
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
43
-1 1021505-057 Frame Assembly A RF
(See IPL FIG 1 for NHA)
-1A 1021505-058 Frame Assembly B RF
(See IPL FIG 1 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

5 1021981-052 • Spreader Assembly - Non-Lock (INBD) A 1
(See IPL FIG 44 for DET BKDN)
-5A 1021981-051 • Spreader Assembly - Non-Lock (INBD) B 1
(See IPL FIG 44 for DET BKDN)
10 1021981-051 • Spreader Assembly - Non-Lock A 1
(OUTBD)
(See IPL FIG 44 for DET BKDN)
-10A 1021981-052 • Spreader Assembly - Non-Lock B 1
(OUTBD)
(See IPL FIG 44 for DET BKDN)
ATTACHING PARTS
15 NAS6603-32 • Bolt - HEX HD 2
(Torque to 75 ±5 IN-LB)
20 MS21042-3 • Nut - LKG 2
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

25 1021980-019 • Leg Assembly 2

(See IPL FIG 45 for DET BKDN)

30 1021981-064 • Spreader Assembly - Lock (CTR-INBD) A 1

(See IPL FIG 44 for DET BKDN)
-30A 1021981-063 • Spreader Assembly - Lock (CTR-INBD) B 1
(See IPL FIG 44 for DET BKDN)
35 1021981-063 • Spreader Assembly - Lock A 1
(CTR-OUTBD)
(See IPL FIG 44 for DET BKDN)
-35A 1021981-064 • Spreader Assembly - Lock B 1 Gutierrez
(CTR-OUTBD)
(See IPL FIG 44 for DET BKDN)
ATTACHING PARTS
40 NAS6603-32 • Bolt - HEX HD 1
(Torque to 75 ±5 IN-LB)

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10251
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
43
45 NAS6603-34 • Bolt - HEX HD 1
(Torque to 75 ±5 IN-LB)
50 MS21042-3 • Nut - LKG 2
* * *

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

55 1063561-101 • Beam - Variable Wall 2
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10252
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10253
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

30
45

35

5
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

15

10
40

1021981-051 Gutierrez
SPREADER ASSEMBLY - NON-LOCK

Spreader Assembly
IPL Figure 44 (Sheet 1 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10254
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

30B 35
45B

25

40A

5
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

20

15

10
1021981-063
SPREADER ASSEMBLY - LOCK

Gutierrez

Spreader Assembly
IPL Figure 44 (Sheet 2 of 2)

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10255
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10256
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
44
-1 1021981-051 Spreader Assembly - Non-Lock A RF
(See IPL FIG 43 for NHA)
-1A 1021981-052 Spreader Assembly - Non-Lock B RF
(See IPL FIG 43 for NHA)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

-1B 1021981-063 Spreader Assembly - Lock C RF
(See IPL FIG 43 for NHA)
-1C 1021981-064 Spreader Assembly - Lock D RF
(See IPL FIG 43 for NHA)

5 1021981-301 • Roller - Articulation 1

ATTACHING PARTS
10 NPS27039-4-06 • Screw - Pan HD 1
15 AN970-4 • Washer - Large, Flat 1
* * *

20 1020222-111 • Eyebolt - Recline Lock CD 1

ATTACHING PARTS
25 MS16633-4050 • Ring - Retaining, External CD 1
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

* * *

30 1022493-051 • Spreader Assembly - Non-Lock A 1

-30A 1022493-052 • Spreader Assembly - Non-Lock B 1
30B 1022493-063 • Spreader Assembly - Lock C 1
-30C 1022493-064 • Spreader Assembly - Lock D 1

35 NAS77-6-024 • • Bushing - Flanged, Press Fit 1

Gutierrez
40 1022493-151 • • Machined Shaft - Roller, Non-Lock AB 1
40A 1022493-153 • • Machined Shaft - Roller, Lock CD 1

45 1021486-101 • • Spreader Assembly - Non-Lock A 1

-45A 1021486-102 • • Spreader Assembly - Non-Lock B 1
- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10257
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
44
45B 1021486-119 • • Spreader Assembly - Lock C 1
-45C 1021486-120 • • Spreader Assembly - Lock D 1
* * *

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10258
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10259
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

5 15

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

10

20

60
55 40
30
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

70

25 65

45

55
50
45 Gutierrez
35

Leg Assembly
IPL Figure 45

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10260
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
45
-1 1021980-019 Leg Assembly RF
(See IPL FIG 43 for NHA)
ATTACHING PARTS
5 NAS6604-9 • Bolt - HEX HD (Front) 1

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

(Torque to 84 -120 IN-LB)
10 MS21042L4 • Nut - LKG (Front) 1
15 NAS6606-7 • Bolt - HEX HD (Rear) 1
(Torque to 240 - 300 IN-LB)
20 MS21042-6 • Nut - LKG (Rear) 1
* * *

25 1057208-101 • Stud 1
(Torque to 180 ±10 IN-LB)
30 1057208-103 • Nut - Anti-Rattle 2

35 1012023-007 • Track Fitting 1

ATTACHING PARTS
40 NAS6606-18 • Bolt - HEX HD 1
(Torque to 110 ±24 IN-LB)
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

45 98038115 • Spacer - Nylon 2

50 52NKE064 (REF) • Nut - HEX HD 1
(True P/N is 52NKE-064)
(Torque to 110 ±24 IN-LB)
* * *

55 1003114-201 • Doubler 2
ATTACHING PARTS
60 NAS6604-19 • Bolt - HEX HD 1
(Torque to 96 ±24 IN-LB) Gutierrez
65 42NKE048 (REF) • Nut - HEX HD 1
(True P/N is 42NKE-048)
(Torque to 96 ±24 IN-LB)
* * *

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10261
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
45
70 1021507-107 • Leg - Machined 1
(Apply Loctite®-270 to Internal Threads
on Leading Edge of Leg. Loctite®
Cures Fully in 24 Hours. Loctite®-263
May be Used as an Alternate to

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Loctite®-270)
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10262
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10263
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

BACK PLATE - HEADREST
5
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

10

Gutierrez

Vendor Refurbishment Parts [REF No. WK0044]

IPL Figure 46

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10264
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

FIG. AIRLINE NOMENCLATURE EFF UNITS/

ITEM PART NUMBER PART NO. 1 2 3 4 5 6 7 CODE ASSY
46 VENDOR REFURBISHMENT PARTS
[REF No. WK0044]
(See IPL FIG 11 for Headrest Assembly)

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

-1 2500210-051 Back Plate Assembly - Headrest 1
ATTACHING PARTS
5 12-6-1 • Retainer - Push-On 2
10 12-99-1026 • Screw - Modified Fast Lead 2
* * *
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

- ITEM NOT ILLUSTRATED

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10265
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 10266
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

USING 3D ELECTRICAL DRAWINGS

1. Electrical Installation

NOTE: 3D PDF Electrical Installation drawings associated with this CMM are available upon
request. All 3D PDF electrical installations are listed in Table 17001. Requests for
3D PDFs should be sent to the following:

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

ws_techpubs3d@collins.com

To use the 3D PDF, you must have Adobe Acrobat® Reader DC or higher. Adobe offers Adobe
Acrobat® Reader DC at no cost.

The 3D PDF electrical installation drawings are large files. Depending upon the device and/or
network used to view the files, there can be a delay in the PDF file opening. This can take several
minutes. Click to open the file as normal and wait for it to open. The files can be in the process of
opening even if there is no visible hour glass on the screen.

Table 17001 shows the seat part numbers and their corresponding electrical installations.

NOTE: DO NOT use part numbers contained in the 3D PDF to order parts. Always use the part
numbers contained in the ILLUSTRATED PARTS LIST for parts ordering.

Table 17001
Electrical Installation Drawings

ELECTRICAL ELECTRICAL
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

INSTALLATION P/N IN INSTALLATION

SEAT PART NUMBER IPL FIG 18 3D PDF / REVISION
1367870-005MS08 1097452-705 1097112-705 - Revision B
1367870-008MS08 1097452-707 1097112-707 - Revision A
1367870-101MS08 1097452-701 1097112-701 - Revision B
1367870-104MS08 1097452-703 1097112-703 - Revision A

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 17001
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

2. Instruction Guide for 3D Interface

A. This section contains basic instructions for using the 3D PDF electrical installations
referenced in this CMM.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Page 1 of 3D PDF Notes Unactivated

Figure 17001
The “NOTES” are on the first page of the PDF drawings. Refer to Figure 17001 for an
example of the first page as shown when the PDF is initially opened. Gutierrez

Activate the notes by clicking on the text “CLICK TO ACTIVATE NOTES” in the middle of the
page. Refer to Figure 17001.

Refer to Figure 17002 for an example of how the 3D PDF appears once the notes are
activated.

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 17002
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Page 1 of 3D PDF Notes Activated

Figure 17002
Alternatively, you may choose to print the notes shown on page one of the 3D PDF. If this
option is desired, click on the “OPEN PRINTABLE NOTES” in the top right hand corner of the
3D PDF. Refer to Figure 17003.

Gutierrez

Open Printable Notes

Figure 17003
Once the “OPEN PRINTABLE NOTES” function is activated, the 3D PDF will generate a
printable version of the notes in a separate window. Refer to Figure 17004.

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 17003
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

Generated Example of 3D PDF Notes

Figure 17004

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 17004
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

The 3D functionality is on the second page of the PDF drawings. Refer to Figure 17005 for an
example of the second page.

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Second Page of 3D PDF Unactivated

Figure 17005
Activate the 3D PDF model on the second page by clicking on the poster (2D image of the
B/E Logo located in the center of the page). Refer to Figure 17005.

Refer to Figure 17006 for a view of an activated 3D PDF.

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 17005
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Activated 3D PDF
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Figure 17006
Alternatively, you may choose to export the electrical BOM embedded within the 3D PDF
shown on page two of the 3D PDF. If this option is desired, click on the “Export Electrical
BOM” button in the lower right hand corner right above the title block of the 3D PDF.
Refer to Figure 17007.

NOTE: DO NOT use part numbers contained in the 3D PDF electrical BOM to order parts.
Always use the part numbers contained in the ILLUSTRATED PARTS LIST for
parts ordering.

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 17006
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

Export Electrical BOM
Figure 17007
A “QuickStart Guide” for all other 3D PDF controls is contained within the 3D PDF. This guide
provides information and instructions for navigating the 3D PDF. In order to access this guide,
click on the “?” button located in the lower right hand corner of the 3D PDF right above the title
block. The “QuickStart Guide for B/E Aerospace 3D PDF Controls” will open in a separate
window. Refer to Figure 17008.

“?” QuickStart Guide

Figure 17008
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 17007
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023
 B/E AEROSPACE, INC., A PART OF COLLINS AEROSPACE
COMPONENT MAINTENANCE MANUAL
MiQ™ 1367870 SERIES

RELEASED ON 20OCT23 Original Released Date 20OCT23 Originator-Matthew Peddycord TPM-Jadon

THIS PAGE IS INTENTIONALLY LEFT BLANK.
Country of Export: US EAR 9E991 Country of Initial Classification: US EAR 9E991

Gutierrez

U.S. Export Classification: EAR 9E991 25-20-83-4667

COLLINS AEROSPACE PROPRIETARY Page 17008
523-0834997 Subject to the restriction on the cover page. Oct 20, 2023