B757 – MSN 25622 Document No: AMS-757-25622
Intro Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
HIGHLIGHTS Issue 2 Wiring Diagram Manual 34-22-16, 34-22-26 Changed 34-22-36 Added
Issue 3 Aircraft Maintenance Manual 31-31-00-PB1, 31-31-01-PB201 31-31-01-PB501 Added Note: Issue 1 thru 3 supplied by AERODEC
Issue 4 onwards supplied by 365 Aerospace Ltd. Issue 4 Document re-written as a 365 Aerospace document Supplemental information added throughout to include 365 Aerospace Mod-0006
Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
RECORD OF REVISION
2 MAR 01/12 3 APR 01/12
Issue 1 thru 3 supplied by AERODEC
Issue 4 onwards supplied by 365 Aerospace Ltd. 4 APR 01/16
The Aircraft Manual Supplement (AMS) is to be used in conjunction with the related aircraft’s manuals. The information contained within this manual relates to various alterations/changes/modifications that have been carried out on the associated aircraft. A list of effective alterations/changes/modifications can be found in the Introduction pages to this manual. These alterations/changes/modifications are in addition to the initial design of the aircraft and are therefore detailed within this manual using appropriate and related convention. This manual complies with EASA Regulations CS-25.1529 and CS-25 Appendix H, which in turn mirror the FAA regulation 14 CFR 25.1529.
RRA-00 Page 1
Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
INTRODUCTION
1. General A. This publication was prepared on behalf of 365 Aerospace Ltd and is in accordance with Air Transport Association of America
Specification No. 100, Specification for Manufacturers Technical Data. The data contained within is related to certain changes/modifications/alterations that are in addition to the associated airplane’s type design.
NOTE: THIS MANUAL IS PREPARED SPECIFICALLY TO COVER THE AIRPLANE LISTED IN THE "INTRODUCTION"
SECTION, FOR THE OWNER/OPERATOR NAMED ON THE TITLE PAGE.
THIS MANUAL IS NOT SUITABLE FOR USE, INCLUDING WITHOUT LIMITATION, GENERAL INSTRUCTIONS OR TRAINING, FOR ANY AIRPLANES NOT LISTED HEREIN.
B. The convention for the use of this publication is in the same convention (ATA 100) as the associated manufacturers AMM,
WDM, and IPC. Therefore, this publication is a SUPPLEMENT to the associated AMM, WDM, and IPC, and instructions on how to use this manual are equivalent to the instructions on how to use the manufacturers AMM, WDM and IPC.
C. This Manual Supplement has been raised to give historic design information pertaining to the following related aircraft
manuals:
IPC – Illustrated Parts Catalogue
AMM – Aircraft Maintenance Manual D. For information on the approval of the technical content of this document, please refer to the Change/Mod/Alteration listing E. Aircraft Effectivity Information:
MODEL/ TYPE
INTRO-00 Page 1 APR 01/16
Produced on behalf of 365 Aerospace Limited, UK. 365 Aerospace own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission In writing from the owner.
INTRODUCTION
Mod/STC Ref: Title:
MOD-0006 Installation of a Controller Pilot Data Link Communications (CPDLC) System MOD-0123 Change for the Introduction of Bose A20 Headsets
B. Owner/Operator/Supplier Mod/STC Information – Table 2.2
Mod/STC Ref: Title: Supplier:
MOD-1038 EFIS Strapping Change AERODEC MOD-1039 EGPWS Callout Change AERODEC MOD-1040 SELCAL Code Change AERODEC MOD-1041 Mode S Code Change AERODEC MOD-1042 Introduction of Mini QAR AERODEC MOD-1043 Installation of a Hot Jug in the Galley AERODEC MOD-1044 Installation of SSFDR AERODEC
3. Approval
A. With reference to any Mod/STC indicated in Table 2.1 above, the technical content of the supplement information associated
with any listed Mod/STC above is approved under the authority of DOA No. EASA.21J.575. B. With reference to any Mod/STC indicated in Table 2.2 above, the technical content of the supplement information associated
with any listed Mod/STC above is approved under the authority of the named Owner/Operator/Supplier of the document. The Owner/Operator/Supplier of the document has given the compiler of this supplement rights to use their information in order to produce this manual supplement.
C. The Checking process will include a verification of technical consistency with the associated Mod/STC and Compliance
documentation which may relate to effectivity, description, effects on airworthiness and environmental protection especially when limitations are changed or affected.
Checked: Print Name:
Approved: Print Name:
Mitchellh
23-71-11 – VOICE RECORDER
Chapter 31 INDICATING/RECORDING SYSTEMS
31-31-41 – FLIGHT DATA RECORDER SYSTEM – DIGITAL
31-33-01 – PRINTER INTERFACE
Chapter 32 LANDING GEAR
32-44-11 – PARKING BRAKE SYSTEM
34-46-11 – GROUND PROXIMITY WARNING SYSTEM PROGRAM PINS
34-53-12 – ATC NO.1 MODE S TRANSPONDER ADDRESS AND AIRSPEED CODING
34-53-22 – ATC NO.2 MODE S TRANSPONDER ADDRESS AND AIRSPEED CODING
34-61-15 – LEFT FMC/EFIS/DATA LOADER GENERAL – OUTPUTS
WDM-CONTENTS Page 2
Chapter 35 OXYGEN
Chapter 36 PNEUMATIC
Chapter 38 WATER/WASTE
Chapter 52 DOORS
Chapter 53 FUSELAGE
Chapter 74 IGNITION
Chapter 75 AIR
Description Page No. Date Description Page No. Date
WDM Front Page WDM Contents 1 WDM Contents 2 WDM-List of Effective Pages 1 Chapter 23 Front Page 23-12-31 1 APR 01/16 23-21-12 1 APR 01/16 23-22-11 1 SHT 1 APR 01/16 23-22-11 1 SHT 2 APR 01/16 23-22-11 1 SHT 3 APR 01/16 23-22-11 1 SHT 4 APR 01/16 23-71-11 1 APR 01/16 Chapter 25 Front Page 25-32-34 1 APR 01/16 Chapter 28 Front Page 28-41-11 1 APR 01/16 Chapter 31 Front Page 31-31-01 1 APR 01/16 31-31-41 1 APR 01/16 31-33-01 1 APR 01/16 31-51-33 1 APR 01/16 Chapter 32 Front Page 32-44-11 1 APR 01/16 Chapter 34 Front Page 34-22-16 1 APR 01/16 34-22-26 1 APR 01/16 34-22-36 1 APR 01/16 34-46-11 1 SHT 1 APR 01/16 34-46-11 1 SHT 2 APR 01/16 34-53-12 1 APR 01/16 34-53-22 1 APR 01/16 34-61-15 1 APR 01/16 Chapter 52 Front Page 52-71-11 1 APR 01/16
CHAPTER
VHF COMMUNICATIONS - CENTRE 23-12-31 INCORPORATES: 23-12-31 365 AEROSPACE MOD 0006
Page 1 Page 1
APR 01/16 APR 01/16 Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
B757 WIRING DIAGRAM MANUAL
Page 1 Page 1
APR 01/16 APR 01/16 Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
B757 WIRING DIAGRAM MANUAL
Page 1 Page 1 Sheet 1 Sheet 1
APR 01/16 APR 01/16 Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
B757 WIRING DIAGRAM MANUAL
Page 1 Page 1 Sheet 2 Sheet 2
APR 01/16 APR 01/16 Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
B757 WIRING DIAGRAM MANUAL
Page 1 Page 1 Sheet 3 Sheet 3
APR 01/16 APR 01/16 Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
B757 WIRING DIAGRAM MANUAL
Page 1 Page 1 Sheet 4 Sheet 4
APR 01/16 APR 01/16 Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
B757 WIRING DIAGRAM MANUAL
NB239
VOICE RECORDER 23-71-11 INCORPORATES: 23-71-11 365 AEROSPACE MOD 0006 Page 1 Page 1
APR 01/16 APR 01/16
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
CHAPTER
Page (See Note) Page (See Note)

















































































































































































































































Page (See Note) Page (See Note)






























































































































































































































FUEL QUANTITY INDICATION 28-41-11 INCORPORATES: 28-41-11 365 AEROSPACE MOD 0006 Page 1 Page 1
APR 01/16 APR 01/16
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
CHAPTER
FDRS – INTERCONNECT GROUP 1 31-31-01 INCORPORATES: 31-31-01 AERODEC MOD 1042
Page 1 Page 1
















































































































































































































































































































































































































FLIGHT DATA RECORDER SYSTEM - DIGITAL INTERFACE GROUP 1 31-31-41 INCORPORATES: 31-31-41 365 AEROSPACE MOD 0006
Page 1 Page 1
APR 01/16 APR 01/16 Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
B757 WIRING DIAGRAM MANUAL
Page 1 Page 1
APR 01/16 APR 01/16 Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
B757 WIRING DIAGRAM MANUAL
NB239
AURAL WARNING – BELL CHIME 31-51-33 INCORPORATES: 31-51-33 365 AEROSPACE MOD 0006 Page 1 Page 1
APR 01/16 APR 01/16
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
CHAPTER
NB239
PARKING BRAKE SYSTEM 32-44-11 INCORPORATES: 32-44-11 365 AEROSPACE MOD 0006 Page 1 Page 1
APR 01/16 APR 01/16
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
CHAPTER
34-22-16 INCORPORATES: 34-22-16 AERODEC MOD 1038
Page 1 Page 1

























































































































































































































































































































































34-22-26 INCORPORATES: 34-22-26 AERODEC MOD 1038
Page 1 Page 1
































































































































































































































































































34-22-36 INCORPORATES: 34-22-36 AERODEC MOD 1038
Page 1 Page 1

































































































































































































Page 1 Page 1 Sheet 1 Sheet 1




























































































































































































































































































Page 1 Page 1 Sheet 2 Sheet 2































































































































































































































ATC NO 1 MODE S TRANSPONDER ADDRESS AND AIRSPEED CODING
34-53-12 INCORPORATES: 34-53-12 AERODEC MOD 1041
Page 1 Page 1
























































































ATC NO 2 MODE S TRANSPONDER ADDRESS AND AIRSPEED CODING
34-53-22 INCORPORATES: 34-53-22 AERODEC MOD 1041
Page 1 Page 1
























































































Page 1 Page 1
APR 01/16 APR 01/16 Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
CHAPTER
DOORS
DOOR WARNING INDICATION – LEFT AND ACCESS 52-71-11 INCORPORATES: 52-71-11 365 AEROSPACE MOD 0006
Page 1 Page 1
APR 01/16 APR 01/16 Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
Produced by 365 Aerospace Limited, UK, who own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission in writing from the owner.
EQUIPMENT
LIST
INDEX
INCORPORATES: EQUIPMENT LIST Section INDEX 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
SECTION PAGE NO. DATE SECTION PAGE NO. DATE
M09000 1 APR 01/16
B757 WIRING DIAGRAM MANUAL
INCORPORATES: EQUIPMENT LIST Section M09000 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Equip Part Number Used on Dwg Qty Diagram Effectivity Part Description Vendor Location
M09000 14114-1-02 (MOD 3) 2-59475-702 1 23-22-11 NB239 UNIT – DLINK+ ACARS EMTEQ P8 AFT PILOT CONTROL STAND M09001 12854-4 1 23-22-11 NB239 UNIT – PERSONALITY MODULE P8 AFT PILOT CONTROL STAND M09002 81194 365-25-0003 1 23-12-31 NB239 ANTENNA - GPS 365 AEROSPACE LTD STA 690 RBL 5.00 M09003 8055515-4503 2-59475-704 1 23-22-11 NB239 PRINTER – DATA (PTA-45B) EMTEQ P8 AFT PILOT CONTROL STAND M09004 84327-50-200B 365-25-0005 1 23-12-31 NB239 SENSOR – GPS/WAAS 365 AEROSPACE LTD E4-4 SHELF
Produced by 365 Aerospace Limited, UK, who own the copyright of the format of this Manual Supplement, which is supplied in confidence. The contents must not be reproduced without permission in writing from the owner.
WIRE
LIST
INDEX
INCORPORATES: WIRE LIST Section INDEX 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
SECTION PAGE NO. DATE SECTION PAGE NO. DATE
W0069 1 APR 01/16 W0110 1 APR 01/16 W0124 1 APR 01/16 W1161 1 APR 01/16 W1163 1 APR 01/16 W1171 1 APR 01/16 W1260 1 APR 01/16 W1275 1 APR 01/16 W1280 1 APR 01/16 W1433 1 APR 01/16 W1447 1 APR 01/16 W1451 1 APR 01/16 W2069 1 APR 01/16 W2653 1 APR 01/16 W4228 1 APR 01/16 W4471 1 APR 01/16 W9001 1 APR 01/16 W9002 1 APR 01/16 W9003 1 APR 01/16 W9004 1-3 APR 01/16 W9008 1 APR 01/16
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W0069 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W0069 286N0069 FLIGHT RECORDER CONTROL, P61 9200B 24 23-22-11 SHT 4 P61 D40003P 38 P61 D9007J 1 NB239 MOD-0006 9200WB 24 23-22-11 SHT 4 P61 D40003P 39 P61 D9007J 2 NB239 MOD-0006 9200O 24 23-22-11 SHT 4 P61 D40003P 35 P61 D9007J 3 NB239 MOD-0006 9200WO 24 23-22-11 SHT 4 P61 D40003P 36 P61 D9007J 6 NB239 MOD-0006 9200Z 24 23-22-11 SHT 4 P61 D40003P 40 NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W0110 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W0110 286N0110 P11-1 MODULE WIRING – LEFT BUSSES 0900 12 23-22-11 SHT 1 P11-1 C539 B P11-1 C9000 B NB239 MOD-0006 0901 16 31-33-01 P11-1 C592 B P11-1 C9001 B NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W0124 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W0124 286N0124 P11-1 MODULE WIRING – LEFT – STBY – LOAD SIDE 0110 16 23-12-31. P11-1 C546 L P11-1 C9002 L NB239 MOD-0006 9000 16 23-22-11 SHT 1 P11-1 C9000 L P11-1 D40616J 7 NB239 MOD-0006 9001 22 31-33-01 P11-1 C9001 L P11-1 D40616J 2 NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W1161 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W1161 286N1161 E4-4 INTEGRATION 001CX BA5903 23-12-31. E4-4 D847C 1 E4-4 CAPPED AND STOWED NB239 MOD-0006 0029 24 23-12-31. E4-4 D847B C13 E4-4 CAPPED AND STOWED NB239 MOD-0006 0030 24 23-12-31. E4-4 D847B D13 E4-4 CAPPED AND STOWED NB239 MOD-0006 0031 24 23-12-31. E4-4 D847B B14 E4-4 D41529P 2 NB239 MOD-0006 0033 24 23-12-31. E4-4 D847B D1 E4-4 CAPPED AND STOWED NB239 MOD-0006 0036 16 23-12-31. E4-4 D847C 4 E4-4 CAPPED AND STOWED NB239 MOD-0006 0038 22 23-12-31. E4-4 D847B D3 E4-4 CAPPED AND STOWED NB239 MOD-0006 0039 24 23-12-31. E4-4 D847B A3 E4-4 CAPPED AND STOWED NB239 MOD-0006 0040 24 23-12-31. E4-4 D847B B3 E4-4 CAPPED AND STOWED NB239 MOD-0006 0041 24 23-12-31. E4-4 D847B C3 E4-4 CAPPED AND STOWED NB239 MOD-0006 0042 24 23-12-31. E4-4 D847B C1 E4-4 CAPPED AND STOWED NB239 MOD-0006 2041R 24 23-12-31. E4-4 D847B A1 E4-4 CAPPED AND STOWED NB239 MOD-0006 2041B 24 23-12-31. E4-4 D847B B1 E4-4 CAPPED AND STOWED NB239 MOD-0006 2042R 24 23-12-31. E4-4 D847B A15 E4-4 CAPPED AND STOWED NB239 MOD-0006 2042B 24 23-12-31. E4-4 D847B B15 E4-4 CAPPED AND STOWED NB239 MOD-0006 2043R 24 23-12-31. E4-4 D847B A13 E4-4 CAPPED AND STOWED NB239 MOD-0006 2043B 24 23-12-31. E4-4 D847B B13 E4-4 CAPPED AND STOWED NB239 MOD-0006 5018R 24 23-12-31. E4-4 D847B A7 E4-4 D9008-P1 13 NB239 MOD-0006 5018B 24 23-12-31. E4-4 D847B B7 E4-4 D9008-P1 14 NB239 MOD-0006 9001 22 23-12-31. E4-4 D847B D5 E4-4 CAPPED AND STOWED NB239 MOD-0006 9002 20 23-12-31. E4-4 SM35 E4-4 D9008-P1 1 NB239 MOD-0006 9003 20 23-12-31. E4-4 D9008-P1 2 E4-4 GD1765-DC NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W1163 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W1163 286N1163 E4-3 SHELF 9001 24 23-71-11 E4-3 DE9201J 52 E4-3 D41551J 20 NB239 MOD-0006 9002R 24 23-71-11 E4-3 DE9201J 53 E4-3 D41551J 21 NB239 MOD-0006 9002B 24 23-71-11 E4-3 DE9201J 54 E4-3 D41551J 22 NB239 MOD-0006 9002Z 24 23-71-11 E4-3 DE9201J 55 E4-3 D41551J 23 NB239 MOD-0006 9003R 24 23-71-11 E4-3 DE9201J 49 E4-3 D41551J 29 NB239 MOD-0006 9003B 24 23-71-11 E4-3 DE9201J 50 E4-3 D41551J 30 NB239 MOD-0006 9003Z 24 23-71-11 E4-3 DE9201J 51 E4-3 D41551J 31 NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W1171 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W1171 286N1171 E2-1 INTEGRATION BUNDLE 0900 20 23-22-11 SHT 2 E2-1 D41391J 29 E2-1 GD1814-ST NB239 MOD-0006 0901 20 23-22-11 SHT 2 E2-1 D41391J 28 E2-1 GD1816-ST NB239 MOD-0006 0902 20 23-22-11 SHT 2 E2-1 D41391J 15 E2-1 GD1811-ST NB239 MOD-0006 5152B 24 23-22-11 SHT 2 E3-3 TB201 Z103 E3-3 TB201 Z106 NB239 MOD-0006 5152R 24 23-22-11 SHT 2 E3-3 TB201 Z104 E3-3 TB201 Z107 NB239 MOD-0006 9001R 24 23-71-11 E2-1 D41420J 20 E2-1 TB201 YC100 NB239 MOD-0006 9001B 24 23-71-11 E2-1 D41420J 21 E2-1 TB201 YC99 NB239 MOD-0006 9001Z 24 23-71-11 E2-1 D41420J 22 E2-1 GD1813 ST NB239 MOD-0006 9200R 24 23-22-11 SHT 2 E2-1 D41391J 18 E2-1 TB201 Z107 NB239 MOD-0006 9200B 24 23-22-11 SHT 2 E2-1 D41391J 13 E2-1 TB201 Z106 NB239 MOD-0006 9200Z 24 23-22-11 SHT 2 E2-1 D41391J 53 E2-1 NB239 MOD-0006 9201R 24 23-22-11 SHT 2 E2-1 D41391J 8 E2-1 TB201 Z122 NB239 MOD-0006 9201B 24 23-22-11 SHT 2 E2-1 D41391J 7 E2-1 TB201 Z121 NB239 MOD-0006 9201Z 24 23-22-11 SHT 2 E2-1 D41391J 9 E2-1 NB239 MOD-0006 9202R 24 23-22-11 SHT 2 E2-1 D41391J 43 E2-1 TB201 Z94 NB239 MOD-0006 9202B 24 23-22-11 SHT 2 E2-1 D41391J 44 E2-1 TB201 Z93 NB239 MOD-0006 9202Z 24 23-22-11 SHT 2 E2-1 D41391J 45 E2-1 NB239 MOD-0006 JPR-Z103 24 23-22-11 SHT 2 E2-1 TB201 Z103 E2-1 TB201 Z106 NB239 MOD-0006 JPR-Z104 24 23-22-11 SHT 2 E2-1 TB201 Z104 E2-1 TB201 Z107 NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W1260 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W1260 286N1260 INTERNAL P36- PLATES (A,B,D,E,F) 9001 20 32-44-11 P36 D2768 1 P36 GD1671-DC NB239 MOD-0006 9002 20 32-44-11 P36 D2768 2 P36 D40914J 2 NB239 MOD-0006 9003 20 23-12-31. P36 D40914P 2 P8 D9002 K- NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W1275 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W1275 286N1275 E4-2 SHELF –(N2) 9001 24 23-12-31 P8 D9002 Y- E4-2 D41628P 53 NB239 MOD-0006 9002 24 52-71-11 E4-2 D41628J 53 E4-2 TB207 YC80 NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W1280 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W1280 286N1280 E3-4 SHELF HARNESS 9001 24 31-51-33 E3-4 D42012J 13 E3-4 D41311J 19 NB239 MOD-0006 9002R 24 23-22-11 SHT 4 E3-4 D41445J 18 E3-4 TB182 YA3 NB239 MOD-0006 9002B 24 23-22-11 SHT 4 E3-4 D41445J 19 E3-4 TB182 YA5 NB239 MOD-0006 9002Z 24 23-22-11 SHT 4 E3-4 D41445J 17 E3-4 TB182 YA1 NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W1433 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W1433 286N1433 E3-3 SHELF BUNDLE 0901 20 23-22-11 SHT 4 E3-3 D40670P 41 E3-3 GD1944-ST NB239 MOD-0006 0902 20 23-22-11 SHT 4 E3-3 D40670P 44 E3-3 GD1944-ST NB239 MOD-0006 5020R 24 23-22-11 SHT 4 E3-3 D11D C14 E3-3 TB181 YA120 NB239 MOD-0006 5020B 24 23-22-11 SHT 4 E3-3 D11D D14 E3-3 TB181 YC120 NB239 MOD-0006 5020Z 24 23-22-11 SHT 4 E3-3 TB181 YA121 NB239 MOD-0006 9200R 24 23-22-11 SHT 4 E3-3 D40670P 42 E3-3 TB181 YC120 NB239 MOD-0006 9200B 24 23-22-11 SHT 4 E3-3 D40670P 43 E3-3 TB181 YA120 NB239 MOD-0006 9200Z 24 23-22-11 SHT 4 E3-3 D40670P 41 NB239 MOD-0006 9201R 24 23-22-11 SHT 4 E3-3 D11D C14 E3-3 TB181 YC120 NB239 MOD-0006 9201B 24 23-22-11 SHT 4 E3-3 D11D D14 E3-3 TB181 YA120 NB239 MOD-0006 9201Z 24 23-22-11 SHT 4 E3-3 TB181 YA121 NB239 MOD-0006 9300R 24 23-22-11 SHT 4 E3-3 D40670P 45 E3-3 D11D H3 NB239 MOD-0006 9300B 24 23-22-11 SHT 4 E3-3 D40670P 46 E3-3 D11D H4 NB239 MOD-0006 9300Z 24 23-22-11 SHT 4 E3-3 D40670P 44 E3-3 GD1944-ST NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W1447 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W1447 286N1447 E2-1 SHELF TO E4-3 SHELF 9001R 24 23-71-11 E2-1 D41420P 20 E4-3 DE9201P 49 NB239 MOD-0006 9001B 24 23-71-11 E2-1 D41420P 21 E4-3 DE9201P 50 NB239 MOD-0006 9001Z 24 23-71-11 E2-1 D41420P 22 E4-3 DE9201P 51 NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W1451 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W1451 286N1451 P-51 WIRE BUNDLE 0253 24 31-51-33 P51 D41059J 30 P51 SP9113 NB239 MOD-0006 9001 24 31-51-33 P51 D41481J 8 P51 SP9113 NB239 MOD-0006 9002 24 31-51-33 P51 D41059J 30 P51 SP9113 NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W2069 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W2069 286N2069 VHF-C CONTROL, P8 TO E4-4 0001 20 23-12-31. P8 D891 1 P8 CAPPED AND STOWED NB239 MOD-0006 0002 20 23-12-31. P8 D891 2 P8 CAPPED AND STOWED NB239 MOD-0006 0003 18 23-12-31. P8 D891 13 P8 CAPPED AND STOWED NB239 MOD-0006 0005 24 23-12-31. P8 D891 5 P8 CAPPED AND STOWED NB239 MOD-0006 0006 24 23-12-31. P8 D891 6 P8 CAPPED AND STOWED NB239 MOD-0006 0007 24 23-12-31. P8 D891 7 P8 CAPPED AND STOWED NB239 MOD-0006 0008 24 23-12-31. P8 D891 8 P8 CAPPED AND STOWED NB239 MOD-0006 0009 24 23-12-31. P8 D891 9 P8 CAPPED AND STOWED NB239 MOD-0006 0010 20 23-12-31. P8 D891 14 P8 CAPPED AND STOWED NB239 MOD-0006 5001R 24 23-12-31. P8 D891 17 P8 D9002 E- NB239 MOD-0006 5001B 24 23-12-31. P8 D891 18 P8 D9002 D- NB239 MOD-0006 5001Z 24 23-12-31. P8 D891 19 P8 D9002 S- NB239 MOD-0006 9001 22 23-12-31. P8 D891 4 P8 CAPPED AND STOWED NB239 MOD-0006 9002 24 23-12-31. P8 D9002 j E4-4 D41529J 2 NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W2653 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W2653 286N2653 VOICE RECORDER TO E/E RACK 9001 24 23-71-11 E4-3 D41551P 20 STA1615
WL290 BL5 CAP AND STOW IN VICINITY OF M201
NB239 MOD-0006 9002R 24 23-71-11 E4-3 D41551P 21 STA1615
WL290 BL5 CAP AND STOW IN VICINITY OF M201
NB239 MOD-0006 9002B 24 23-71-11 E4-3 D41551P 22 STA1615
WL290 BL5 CAP AND STOW IN VICINITY OF M201
NB239 MOD-0006 9002Z 24 23-71-11 E4-3 D41551P 23 STA1615
WL290 BL5 CAP AND STOW IN VICINITY OF M201
NB239 MOD-0006 9003 24 23-71-11 STA1615 GD180 DC STA1615
WL290 BL5 CAP AND STOW IN VICINITY OF M201
NB239 MOD-0006 WL290 BL5 9004R 24 23-71-11 E4-3 D41551P 29 STA1615
WL290 BL5 CAP AND STOW IN VICINITY OF M201
NB239 MOD-0006 9004B 24 23-71-11 E4-3 D41551P 30 STA1615
WL290 BL5 CAP AND STOW IN VICINITY OF M201
NB239 MOD-0006 9004Z 24 23-71-11 E4-3 D41551P 31 STA1615
WL290 BL5 CAP AND STOW IN VICINITY OF M201
NB239 MOD-0006
INCORPORATES: WIRE LIST Section W4228 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W4228 286N4228 E/E SHELF DISC TO LEFT WING BODY DISC 9001 24 31-51-33 P8 D9002 G E3-4 D42012P 13 NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W4471 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W4471 286N4471 E/E RACK, INTERRACK LEFT 9001 24 31-51-33 E3-4 D41311P 19 P51 D41481P 8 NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W9001 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W9001 9000 16 23-22-11 SHT 4 P8 D9001 A P11-1 D40616P 7 NB239 MOD-0006 9001 16 23-22-11 SHT 4 P8 D9001 B P8 GD2303-DC NB239 MOD-0006 9002 20 23-22-11 SHT 4 P8 D9001 G P8 TB58 Z3 NB239 MOD-0006 9003 20 23-22-11 SHT 4 P8 D9001 H P8 GD2303-AC NB239 MOD-0006 9004 16 23-22-11 SHT 4 P8 D9001 J P8 GD2303-DC NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W9002 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W9002 9100R 24 23-22-11 SHT 2 P8 D9002 U E2-1 D41391P 30 NB239 MOD-0006 9100B 24 23-22-11 SHT 2 P8 D9002 V E2-1 D41391P 31 NB239 MOD-0006 9100Z 24 23-22-11 SHT 2 P8 D9002 A- E2-1 D41391P 29 NB239 MOD-0006 9101R 24 23-22-11 SHT 2 P8 D9002 W E2-1 D41391P 23 NB239 MOD-0006 9101B 24 23-22-11 SHT 2 P8 D9002 X E2-1 D41391P 24 NB239 MOD-0006 9101Z 24 23-22-11 SHT 2 P8 D9002 I- E2-1 D41391P 28 NB239 MOD-0006 9102B 24 23-22-11 SHT 4 P8 D9002 D P61 D40003P 38 NB239 MOD-0006 9102WB 24 23-22-11 SHT 4 P8 D9002 E P61 D40003P 39 NB239 MOD-0006 9102O 24 23-22-11 SHT 4 P8 D9002 B P61 D40003P 35 NB239 MOD-0006 9102WO 24 23-22-11 SHT 4 P8 D9002 C P61 D40003P 36 NB239 MOD-0006 9102Z 24 23-22-11 SHT 4 P8 D9002 F P61 D40003P 40 NB239 MOD-0006 9103R 24 23-22-11 SHT 4 P8 D9002 S E3-3 D40670P 42 NB239 MOD-0006 9103B 24 23-22-11 SHT 4 P8 D9002 T E3-3 D40670P 43 NB239 MOD-0006 9103Z 24 23-22-11 SHT 4 P8 D9002 N E3-3 D40670P 41 NB239 MOD-0006 9104R 24 31-33-01 P8 D9006 V P8 D9002 AA NB239 MOD-0006 9104B 24 31-33-01 P8 D9006 W P8 D9002 BB NB239 MOD-0006 9104Z 24 31-33-01 P8 D9002 Z- NB239 MOD-0006 9105R 24 31-33-01 P8 D9006 E P8 D9002 CC NB239 MOD-0006 9105B 24 31-33-01 P8 D9006 F P8 D9002 DD NB239 MOD-0006 9105Z 24 31-33-01 P8 D9002 Z- NB239 MOD-0006 9106R 24 23-22-11 SHT 2 P8 D9002 Y E2-1 D41391P 43 NB239 MOD-0006 9106B 24 23-22-11 SHT 2 P8 D9002 Z E2-1 D41391P 44 NB239 MOD-0006 9106Z 24 23-22-11 SHT 2 P8 D9002 P- E2-1 D41391P 15 NB239 MOD-0006 9107R 24 23-22-11 SHT 4 P8 D9002 EE E3-4 D41445P 18 NB239 MOD-0006 9107B 24 23-22-11 SHT 4 P8 D9002 FF E3-4 D41445P 19 NB239 MOD-0006 9107Z 24 23-22-11 SHT 4 P8 D9002 GG E3-4 D41445P 17 NB239 MOD-0006 9108A 24 23-22-11 SHT 4 FLIGHT DECK D9002 J P10 D40901P 17 NB239 MOD-0006 9108B 24 23-22-11 SHT 4 FLIGHT DECK D40901J 17 FLIGHT DECK SP9108 NB239 MOD-0006 9108C 24 23-22-11 SHT 4 FLIGHT DECK D40677P 16 FLIGHT DECK SP9108 NB239 MOD-0006 9108D 24 23-22-11 SHT 3 FLIGHT DECK D40677J 16 FLIGHT DECK R9004 NB239 MOD-0006 9108F 24 23-22-11 SHT 4 FLIGHT DECK D41170P 16 FLIGHT DECK SP9108 NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W9002 365 Aerospace MOD-0006 Page 2
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W9002 (Continued…) 9108G 24 23-22-11 SHT 3 FLIGHT DECK D41170J 16 FLIGHT DECK D40249P 6 NB239 MOD-0006 9108H 24 23-22-11 SHT 3 FLIGHT DECK D40249J 6 FLIGHT DECK R9008 NB239 MOD-0006 9109A 24 23-22-11 SHT 4 FLIGHT DECK D9002 H P10 D40901P 28 NB239 MOD-0006 9109B 24 23-22-11 SHT 4 FLIGHT DECK D40901J 28 FLIGHT DECK SP9109 NB239 MOD-0006 9109C 24 23-22-11 SHT 3 FLIGHT DECK D40677P 21 FLIGHT DECK SP9109 NB239 MOD-0006 9109D 24 23-22-11 SHT 3 FLIGHT DECK D40677J 21 FLIGHT DECK R9001 NB239 MOD-0006 9109F 24 23-22-11 SHT 4 FLIGHT DECK D41170P 21 FLIGHT DECK SP9109 NB239 MOD-0006 9109G 24 23-22-11 SHT 3 FLIGHT DECK D41170J 21 FLIGHT DECK D40249P 7 NB239 MOD-0006 9109H 24 23-22-11 SHT 3 FLIGHT DECK D40249J 7 FLIGHT DECK R9005 NB239 MOD-0006 9110A 24 23-22-11 SHT 4 FLIGHT DECK D9002 N- P10 D40901P 29 NB239 MOD-0006 9110B 24 23-22-11 SHT 4 FLIGHT DECK D40901J 29 E5-1 SHELF D41325P 15 NB239 MOD-0006 9110C 24 23-22-11 SHT 4 E5-1 SHELF D41325J 15 M10331 D3312B D8 NB239 MOD-0006 9110D 24 23-22-11 SHT 4 E5-1 SHELF SP9114 M10331 D3312B D8 NB239 MOD-0006 9111R 24 23-22-11 SHT 4 P8 D9002 B- E4-3 DE9201P 30 NB239 MOD-0006 9111B 24 23-22-11 SHT 4 P8 D9002 C- E4-3 DE9201P 31 NB239 MOD-0006 9111Z 24 23-22-11 SHT 4 P8 D9002 KK E4-3 DE9201P 32 NB239 MOD-0006 9112R 24 23-22-11 SHT 4 P8 D9002 V- E4-3 DE9201P 33 NB239 MOD-0006 9112B 24 23-22-11 SHT 4 P8 D9002 W- E4-3 DE9201P 34 NB239 MOD-0006 9112Z 24 23-22-11 SHT 4 P8 D9002 X- E4-3 DE9201P 35 NB239 MOD-0006 9118R 24 23-71-11 SHT 1 FLIGHT DECK D9002 P E4-3 SHELF DE9201P 53 NB239 MOD-0006 9118B 24 23-71-11 SHT 1 FLIGHT DECK D9002 R E4-3 SHELF DE9201P 54 NB239 MOD-0006 9118Z 24 23-71-11 SHT 1 FLIGHT DECK D9002 A E4-3 SHELF DE9201P 55 NB239 MOD-0006 9119 24 23-71-11 SHT 1 E4-3 SHELF DE9201P 52 FLIGHT DECK D40901J 16 NB239 MOD-0006 9120A 24 23-22-11 SHT 4 FLIGHT DECK D40901P 16 FLIGHT DECK D40901P 23 NB239 MOD-0006 9120B 24 23-22-11 SHT 4 FLIGHT DECK D40901J 23 FLIGHT DECK D40677P 15 NB239 MOD-0006 9120C 24 23-22-11 SHT 3 FLIGHT DECK D40677J 15 FLIGHT DECK R9010 NB239 MOD-0006 9121A 24 23-22-11 SHT 3 FLIGHT DECK R9010 FLIGHT DECK SM9010 NB239 MOD-0006 9121B 24 23-22-11 SHT 3 FLIGHT DECK D9100 G FLIGHT DECK SM9010 NB239 MOD-0006 9121C 24 23-22-11 SHT 3 FLIGHT DECK R9009 FLIGHT DECK SM9010 NB239 MOD-0006 9122A 24 23-22-11 SHT 3 FLIGHT DECK R9009 FLIGHT DECK SM9002 NB239 MOD-0006 9122B 24 23-22-11 SHT 3 FLIGHT DECK R9002 FLIGHT DECK SM9002 NB239 MOD-0006 9122C 24 23-22-11 SHT 3 FLIGHT DECK R9003 FLIGHT DECK SM9002 NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W9002 365 Aerospace MOD-0006 Page 3
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W9002 (Continued…) 9122D 24 23-22-11 SHT 3 FLIGHT DECK TB64 Z18 FLIGHT DECK SM9002 NB239 MOD-0006 9123A 24 23-22-11 SHT 3 FLIGHT DECK TB64 Z17 FLIGHT DECK SM9001 NB239 MOD-0006 9123B 24 23-22-11 SHT 3 FLIGHT DECK SM9001 FLIGHT DECK SM9009 NB239 MOD-0006 9123C 24 23-22-11 SHT 3 FLIGHT DECK SM9001 FLIGHT DECK SM9003 NB239 MOD-0006 9123D 24 23-22-11 SHT 3 FLIGHT DECK D9100 D FLIGHT DECK SM9009 NB239 MOD-0006 9123E 24 23-22-11 SHT 3 FLIGHT DECK D9100 A FLIGHT DECK SM9009 NB239 MOD-0006 9123F 24 23-22-11 SHT 3 FLIGHT DECK D9100 B FLIGHT DECK SM9009 NB239 MOD-0006 9123G 24 23-22-11 SHT 3 FLIGHT DECK D9100 C FLIGHT DECK SM9009 NB239 MOD-0006 9123H 24 23-22-11 SHT 3 FLIGHT DECK D9101 D FLIGHT DECK SM9003 NB239 MOD-0006 9123J 24 23-22-11 SHT 3 FLIGHT DECK D9101 C FLIGHT DECK SM9003 NB239 MOD-0006 9123K 24 23-22-11 SHT 3 FLIGHT DECK D9101 B FLIGHT DECK SM9003 NB239 MOD-0006 9123L 24 23-22-11 SHT 3 FLIGHT DECK D9101 A FLIGHT DECK SM9003 NB239 MOD-0006 9124A 24 23-22-11 SHT 3 FLIGHT DECK R9001 FLIGHT DECK SM9004 NB239 MOD-0006 9124B 24 23-22-11 SHT 3 FLIGHT DECK R9002 FLIGHT DECK SM9004 NB239 MOD-0006 9124C 24 23-22-11 SHT 3 FLIGHT DECK D9101 G FLIGHT DECK SM9004 NB239 MOD-0006 9125A 24 23-22-11 SHT 3 FLIGHT DECK R9003 FLIGHT DECK SM9005 NB239 MOD-0006 9125B 24 23-22-11 SHT 3 FLIGHT DECK R9004 FLIGHT DECK SM9005 NB239 MOD-0006 9125C 24 23-22-11 SHT 3 FLIGHT DECK D9101 F FLIGHT DECK SM9005 NB239 MOD-0006 9126A 24 23-22-11 SHT 3 FLIGHT DECK SM2 FLIGHT DECK SM9006 NB239 MOD-0006 9126B 24 23-22-11 SHT 3 FLIGHT DECK D9102 D FLIGHT DECK SM9006 NB239 MOD-0006 9126C 24 23-22-11 SHT 3 FLIGHT DECK D9102 C FLIGHT DECK SM9006 NB239 MOD-0006 9126D 24 23-22-11 SHT 3 FLIGHT DECK D9102 B FLIGHT DECK SM9006 NB239 MOD-0006 9126E 24 23-22-11 SHT 3 FLIGHT DECK D9102 A FLIGHT DECK SM9006 NB239 MOD-0006 9127A 24 23-22-11 SHT 3 FLIGHT DECK R9005 FLIGHT DECK SM9007 NB239 MOD-0006 9127B 24 23-22-11 SHT 3 FLIGHT DECK R9006 FLIGHT DECK SM9007 NB239 MOD-0006 9127C 24 23-22-11 SHT 3 FLIGHT DECK D9102 G FLIGHT DECK SM9007 NB239 MOD-0006 9127D 24 23-22-11 SHT 3 FLIGHT DECK R9006 FLIGHT DECK SM1 NB239 MOD-0006 9128A 24 23-22-11 SHT 3 FLIGHT DECK R9008 FLIGHT DECK SM9008 NB239 MOD-0006 9128B 24 23-22-11 SHT 3 FLIGHT DECK R9007 FLIGHT DECK SM9008 NB239 MOD-0006 9128C 24 23-22-11 SHT 3 FLIGHT DECK D9102 F FLIGHT DECK SM9008 NB239 MOD-0006 9128D 24 23-22-11 SHT 3 FLIGHT DECK R9007 FLIGHT DECK SM1 NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W9003 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W9003 9000 CX1 23-22-11 SHT 1 P8 D9003 1 P8 D169 A1 NB239 MOD-0006 9000X CX1 23-22-11 SHT 1 P8 D9003 C1 P8 D169 C1 NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W9004 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W9004 9201 22 31-33-01 P8 D40616P 2 P8 D9006 R NB239 MOD-0006 9202 20 31-33-01 P8 D9006 N P8 GD2303-AC NB239 MOD-0006 9203 20 31-33-01 P8 D9006 L P8 GD2303-ST NB239 MOD-0006 9204 20 31-33-01 P8 D9006 M P8 GD2303-AC NB239 MOD-0006 9205 20 31-33-01 P8 D9006 E- P8 TB58 Z3 NB239 MOD-0006
B757 WIRING DIAGRAM MANUAL
INCORPORATES: WIRE LIST Section W9008 365 Aerospace MOD-0006 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information. APR 01/16
Bundle No. Part Number Description From To Info Wire No. GA Diagram Location Equip Term Location Equip Term Effectivity Mod No. W9008 9001 CX1 23-12-31. E4-4 D9008-P2 =A STA 690 D9005 A1 NB239 MOD-0006 9001Z CX1 23-12-31. E4-4 D9008-P2 =C STA 690 D9005 C1 NB239 MOD-0006
ILLUSTRATED
PARTS
CATALOGUE
Contents
Chapter 21 AIR CONDITIONING
Chapter 22 AUTO FLIGHT
23-22-92-99Z – ANNUNCIATOR INSTL – PANELS P1-3 & P3-3
23-22-95-99Z – PRINTER INSTL – P8 ELECTRONIC (DLINK+ ACARS PRINTER ONLY)
23-51-51-99Z – HEADPHONE ASSY - ELECTRICAL
Chapter 24 ELECTRICAL POWER
Chapter 25 EQUIPMENT/FURNISHINGS
Chapter 26 FIRE PROTECTION
Chapter 27 FLIGHT CONTROLS
Chapter 31 INDICATING/RECORDING SYSTEMS
31-31-99-01Z – EQUIPMENT INSTL – MINI QAR
Chapter 32 LANDING GEAR
Chapter 52 DOORS
Chapter 53 FUSELAGE
Chapter 74 IGNITION
Chapter 75 AIR
Description Page No. Date Description Page No. Date
IPC Front Page IPC Contents 1 IPC Contents 2 IPC-List of Effective Pages 1 Chapter 11 Front Page 11-31-04-01Z 0 APR 01/16 11-31-04-01Z 1 APR 01/16 Chapter 23 Front Page 23-22-06-99Z 0 APR 01/16 23-22-06-99Z 1 APR 01/16 23-22-90-99Z 0 APR 01/16 23-22-90-99Z 1 APR 01/16 23-22-92-99Z 0 APR 01/16 23-22-92-99Z 1 APR 01/16 23-22-95-99Z 0 APR 01/16 23-22-95-99Z 1 APR 01/16 23-51-51-99Z 0 APR 01/16 23-51-51-99Z 1 APR 01/16 Chapter 24 Front Page 24-51-53-99Z 0 APR 01/16 24-51-53-99Z 1 APR 01/16 Chapter 25 Front Page 25-31-99-01Z 0 APR 01/16 25-31-99-01Z 1 APR 01/16 25-31-99-01Z 3 APR 01/16 25-31-99-01Z 4 APR 01/16 Chapter 31 Front Page 31-31-01-01Z 0 APR 01/16 31-31-01-01Z 1 APR 01/16 31-31-99-01Z 0 APR 01/16 31-31-99-01Z 1 APR 01/16 Chapter 34 Front Page 34-58-01-99Z 0 APR 01/16 34-58-01-99Z 1 APR 01/16 34-58-05-99Z 0 APR 01/16 34-58-05-99Z 1 APR 01/16
CHAPTER
B757 ILLUSTRATED PARTS CATALOGUE
11-31-04-01Z 11-31-04 AERODEC MOD 1040 Fig 1Z APR 01/16 Page 0
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
PLACARD INSTL – SELCAL AND REGISTRATION FIGURE 1Z
B757 ILLUSTRATED PARTS CATALOGUE
11-31-04-01Z 11-31-04 AERODEC MOD 1040 Fig 1Z APR 01/16 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
FIG ITEM PART NUMBER NOMENCLATURE EFF
CODE UNITS PER
ASSY 1234567
1Z --1 MEO-1040-001 SELCAL ADDRESS CODE PIN PROGRAMMING CHANGE 239239 RF
10 AL232-1613-001 • PLACARD - SELCAL 2 20 MS24617-2 • SCREW 4
-- ITEMS NOT ILLUSTRATED
23-22-06-99Z 23-22-06 MOD-0006 Fig 99Z APR 01/16 Page 0
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
PANEL INSTL – P8 ELECTRONIC (DLINK+ ACARS UNIT ONLY) FIGURE 99Z
B757 ILLUSTRATED PARTS CATALOGUE
23-22-06-99Z 23-22-06 MOD-0006 Fig 99Z APR 01/16 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
FIG ITEM PART NUMBER NOMENCLATURE EFF
CODE UNITS PER
ASSY 1234567
99Z --1 EO-0006-001 INSTL OF A CPDLC SYSTEM 239239 RF --1 2-59475-702 DLINK+ UNIT INSTL (EMTEQ DRAWING) 239239 RF
10 14114-1-02 (MOD 3) • UNIT – DLINK+ ACARS 1 EQUIPMENT NUMBER: M9000
--20 CCD-14513-* • CONFIGURATION FILE 1 (* LATEST REVISION)
--30 12854-4 • UNIT – PERSONALITY MODULE 1 EQUIPMENT NUMBER: M9001
-- ITEMS NOT ILLUSTRATED
23-22-90-99Z 23-22-90 MOD-0006 Fig 99Z APR 01/16 Page 0
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
ETHERNET RECEPTACLE INSTL – P61 PANEL (CPDLC SYSTEM ONLY) FIGURE 99Z
B757 ILLUSTRATED PARTS CATALOGUE
23-22-90-99Z 23-22-90 MOD-0006 Fig 99Z APR 01/16 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
FIG ITEM PART NUMBER NOMENCLATURE EFF
CODE UNITS PER
ASSY 1234567
99Z --1 EO-0006-001 INSTL OF A CPDLC SYSTEM 239239 RF --1 2-59475-703-101 ETHERNET RECEPT INSTL (EMTEQ DRAWING) 239239 RF
20 2-59475-101-104 • ETHERNET HARNESS ASSY 1 30 MS35206-215 • SCREW 4 40 NAS1149FN416P • WASHER 8 50 MS21042-04 • NUT 4 60 RJFC2B • CAP 1 70 2-59475-401-015 • PLACARD (DLINK+ ETHERNET) 1
-- ITEMS NOT ILLUSTRATED
23-22-92-99Z 23-22-92 MOD-0006 Fig 99Z APR 01/16 Page 0
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
ANNUNCIATOR INSTL – PANELS P1-3 & P3-3 FIGURE 99Z
B757 ILLUSTRATED PARTS CATALOGUE
23-22-92-99Z 23-22-92 MOD-0006 Fig 99Z APR 01/16 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
FIG ITEM PART NUMBER NOMENCLATURE EFF
CODE UNITS PER
ASSY 1234567
99Z --1 EO-0006-001 INSTL OF A CPDLC SYSTEM 239239 RF --1 365-23-0005 INSTL OF A CPDLC SYSTEM (365 AEROSPACE DRAWING) 239239 RF
10 95-41-12-B6-E1EXM • ANNUNCIATOR – ATC/ACARS 2 20 95-41-11-B6-E0YKD • ANNUNCIATOR – DLINK REC 1
--30 18-200 • CONNECTOR 3
23-22-95-99Z 23-22-95 MOD-0006 Fig 99Z APR 01/16 Page 0
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
PRINTER INSTL – P8 ELECTRONIC (DLINK+ ACARS PRINTER ONLY) FIGURE 99Z
B757 ILLUSTRATED PARTS CATALOGUE
23-22-95-99Z 23-22-95 MOD-0006 Fig 99Z APR 01/16 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
FIG ITEM PART NUMBER NOMENCLATURE EFF
CODE UNITS PER
ASSY 1234567
99Z --1 EO-0006-001 INSTL OF A CPDLC SYSTEM 239239 RF --1 2-59475-704 DATA PRINTER UNIT INSTL (EMTEQ DRAWING) 239239 RF
10 8055515-4503 • PRINTER – DATA (PTA-45B) V97896 1 EQUIPMENT NUMBER: M9003 OPTIONAL PART: 8055515-4502 8055515-4506
--20 8050917-0006 • PAPER ROLL – DATA PRINTER V97896 1
-- ITEMS NOT ILLUSTRATED
23-51-51-99Z 23-51-51 MOD-0123 Fig 99Z APR 01/16 Page 0
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
HEADPHONE ASSY - ELECTRICAL FIGURE 99Z
B757 ILLUSTRATED PARTS CATALOGUE
23-51-51-99Z 23-51-51 MOD-0123 Fig 99Z APR 01/16 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
FIG ITEM PART NUMBER NOMENCLATURE EFF
CODE UNITS PER
ASSY 1234567
99Z --1 EO-0123-001 CHANGE FOR THE INTRODUCTION OF A BOSE A20 HEADSET RF
10 324843-2020 • HEADSET – NOISE CANCELLING (MODEL: BOSE A20) 3 (11-08728)
-- ITEMS NOT ILLUSTRATED
24-51-53-99Z 24-51-53 MOD-0006 Fig 99Z APR 01/16 Page 0
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
CIRCUIT BREAKER INSTL – P11-1 FIGURE 99Z
B757 ILLUSTRATED PARTS CATALOGUE
24-51-53-99Z 24-51-53 MOD-0006 Fig 99Z APR 01/16 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
FIG ITEM PART NUMBER NOMENCLATURE EFF
CODE UNITS PER
ASSY 1234567
99Z --1 EO-0006-001 INSTL OF A CPDLC SYSTEM 239239 RF --1 2-59475-603 INSTL – CIRCUIT BREAKER (EMTEQ DRAWING) 239239 RF
10 MS22073-3 • CIRCUIT BREAKER – 3 AMPS 1 20 MS22073-7 1/2 • CIRCUIT BREAKER – 7.5 AMPS 1 30 2-59475-401-002 • PLACARD - “PRINTER” 1 40 2-59475-401-001 • PLACARD - “ACARS” 1
--50 2-59475-401-004 • PLACARD - “C9001” 1 --60 2-59475-401-003 • PLACARD - “C9000” 1
-- ITEMS NOT ILLUSTRATED
B757 ILLUSTRATED PARTS CATALOGUE
25-31-99-01Z 25-31-99 AERODEC MOD 1043 Fig 1Z APR 01/16 Page 0
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
HOT JUG INSTL – GALLEY NO.1A FIGURE 1Z (SHEET 1 OF 2)
B757 ILLUSTRATED PARTS CATALOGUE
25-31-99-01Z 25-31-99 AERODEC MOD 1043 Fig 1Z APR 01/16 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
HOT JUG INSTL – GALLEY NO.1A FIGURE 1Z (SHEET 1 OF 2)
B757 ILLUSTRATED PARTS CATALOGUE
25-31-99-01Z 25-31-99 AERODEC MOD 1043 Fig 1Z APR 01/16 Page 2
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
FIG ITEM PART NUMBER NOMENCLATURE EFF
CODE UNITS PER
ASSY 1234567
1Z --1 MEO-1043-001 REPLACEMENT OF EXISTING WATER BOILER WITH HOT JUG 239239 RF --1 AL253-1608 DRIESSEN COMBO (HOT JUG) INSTL – GALLEY NO.1A 239239 RF --1 AL253-1681 CLOSING PANEL DRIESSEN GALLEY G1A 239239 RF --1 AL253-1682 COMBO ADAPTER PANEL ASSY DRIESSEN GALLEY G1A 239239 RF --1 AL253-0247 BRACKET – DRIESSEN COMBO CONNECTOR 239239 RF --1 AL253-0248 PLACARD – DRIESSEN COMBO USER INSTRUCTIONS 239239 RF --1 AL253-0524 PLACARD – MODIFICATION 239239 RF
10 JF003001 • COMBO ASSY – HOT JUG 1
--20 AL253-1682-001 • ADAPTER PANEL 1 ATTACHING PARTS
--21 NAS604-14 • SCREW 4 --22 NAS1149F0463P • WASHER 4
- - - - - - - - - - * - - - - - - - - - - --30 34-00318 • BRACKET 1
- - - - - - - - - - * - - - - - - - - - - --40 AL253-0247-001 • BRACKET 1
ATTACHING PARTS --41 NAS603-12 • SCREW 4 --42 NAS1149F0332J • WASHER 4
- - - - - - - - - - * - - - - - - - - - - --50 AL253-1681-001 • CLOSING PANEL 1
ATTACHING PARTS --51 NAS603-12 • SCREW 5 --52 NAS1149F0332J • WASHER 5
- - - - - - - - - - * - - - - - - - - - - --60 AC16707 • CONNECTOR 1
ATTACHING PARTS --61 MS51960-31 • SCREW 4 --62 NAS1149D0616J • WASHER 4 --63 AN935-6 • WASHER 4 --64 MS35650-364 • NUT 4
- - - - - - - - - - * - - - - - - - - - - 70 MS51505-B4-4S • ELBOW 1 80 BACC18R4A • CIRCUIT BREAKER 1 90 AL253-1608-129 • PLACARD – “DO NOT USE…” 1
100 AL253-1608-128 • PLACARD – “WATER BOILER” 1 110 AL253-1608-127 • PLACARD – “COMBO” 1
--120 9-028-13 • SCREW 2
B757 ILLUSTRATED PARTS CATALOGUE
25-31-99-01Z 25-31-99 AERODEC MOD 1043 Fig 1Z APR 01/16 Page 3
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
FIG ITEM PART NUMBER NOMENCLATURE EFF
CODE UNITS PER
--131 NAS603-7 • SCREW 3 --132 NAS1149D0332J • WASHER 5
- - - - - - - - - - * - - - - - - - - - - --140 AL113-0524-001 • PLACARD – MOD DATA 1 --150 AL113-0248-001 • PLACARD – USER INSTRUCTIONS 1
-- ITEMS NOT ILLUSTRATED
B757 ILLUSTRATED PARTS CATALOGUE
31-31-01-01Z 31-31-01 AERODEC MOD 1044 Fig 1Z APR 01/16 Page 0
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
EQUIPMENT INSTL – SOLID STATE FLIGHT DATA RECORDER FIGURE 1Z
B757 ILLUSTRATED PARTS CATALOGUE
31-31-01-01Z 31-31-01 AERODEC MOD 1044 Fig 1Z APR 01/16 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
FIG ITEM PART NUMBER NOMENCLATURE EFF
CODE UNITS PER
ASSY 1234567
1Z --1 MEO-1044-001 INSTALLATION OF A SOLID STATE FLIGHT DATA RECORDER 239239 RF
10 980-4700-042 • RECORDER – FLIGHT DATA (FDR) 1 (ALT PART NO. 980-4700-001 & 980-4700-003)
-- ITEMS NOT ILLUSTRATED
B757 ILLUSTRATED PARTS CATALOGUE
31-31-99-01Z 31-31-99 AERODEC MOD 1042 Fig 1Z APR 01/16 Page 0
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
EQUIPMENT INSTL – MINI QAR FIGURE 1Z
B757 ILLUSTRATED PARTS CATALOGUE
31-31-99-01Z 31-31-99 AERODEC MOD 1042 Fig 1Z APR 01/16 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
FIG ITEM PART NUMBER NOMENCLATURE EFF
CODE UNITS PER
ASSY 1234567
1Z --1 MEO-1042-001 INSTALLATION OF A MINI QUICK ACCESS RECORDER (QAR) 239239 RF
10 804-0005 • RECORDER – MINI QUICK ACCESS (QAR) 1
-- ITEMS NOT ILLUSTRATED
34-58-01-99Z 34-58-01 MOD-0006 Fig 99Z APR 01/16 Page 0
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
ANTENNA INSTL – GPS FIGURE 99Z
B757 ILLUSTRATED PARTS CATALOGUE
34-58-01-99Z 34-58-01 MOD-0006 Fig 99Z APR 01/16 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
FIG ITEM PART NUMBER NOMENCLATURE EFF
CODE UNITS PER
ASSY 1234567
99Z --1 EO-0006-001 INSTL OF A CPDLC SYSTEM 239239 RF --1 365-25-0003 GPS ANTENNA INSTL (365 AEROSPACE DRAWING) 239239 RF
10 81194 • ANTENNA - GPS 1 EQUIPMENT NUMBER: M9002
20 NAS1473C3 • NUTPLATE 4 --30 365-23-0005-101 • PLACARD (GPS M9002) 1 50 PM570 • EROSION BOOT 1 60 TA71000438 • GASKET - GEL 1
--80 365-23-0005-104 • PLACARD (D9005) 1 110 AN510C10R16 • SCREW 4 120 365-25-0003-101 • GPS PLATE 1
-- ITEMS NOT ILLUSTRATED
34-58-05-99Z 34-58-05 MOD-0006 Fig 99Z APR 01/16 Page 0
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
SENSOR INSTL – GPS FIGURE 99Z
B757 ILLUSTRATED PARTS CATALOGUE
34-58-05-99Z 34-58-05 MOD-0006 Fig 99Z APR 01/16 Page 1
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
FIG ITEM PART NUMBER NOMENCLATURE EFF
CODE UNITS PER
99Z --1 EO-0006-001 INSTL OF A CPDLC SYSTEM 239239 RF
10 84327-50-200B • SENSOR – GPS/WAAS 1 EQUIPMENT NUMBER: M9004
--20 365-23-0005-201 • GPS – MOUNTING BRACKET 1
-- ITEMS NOT ILLUSTRATED
PAGE BLOCK 201 – SOFTWARE INSTALLATION
PAGE BLOCK 501 – ADJUSTMENT/TEST
23-22-01 – ACARS DLINK+ UNIT
23-22-02 – PERSONALITY MODULE
Chapter 24 ELECTRICAL POWER
Chapter 31 INDICATING/RECORDING SYSTEMS
PAGE BLOCK 1 – DESCRIPTION AND OPERATION
PAGE BLOCK 501 – ADJUSTMENT/TEST
31-31-01 – FLIGHT DATA RECORDER
31-33-00 – DATA PRINTER
PAGE BLOCK 501 – ADJUSTMENT/TEST
AMM-CONTENTS Page 2
PAGE BLOCK 501 – ADJUSTMENT/TEST
PAGE BLOCK 501 – ADJUSTMENT/TEST
PAGE BLOCK 501 – ADJUSTMENT/TEST
Chapter 35 OXYGEN
Chapter 36 PNEUMATIC
Chapter 38 WATER/WASTE
Chapter 52 DOORS
Chapter 53 FUSELAGE
Chapter 74 IGNITION
Chapter 75 AIR
Description Page No. Date Description Page No. Date
AMM Front Page 31-31-00 528 AMM Contents 1 31-31-00 529 AMM Contents 2 31-31-00 530 AMM-List of Effective Pages 1 31-31-00 531 Chapter 23 Front Page 31-31-00 532 23-22-00 1 APR 01/16 31-31-00 533 23-22-00 2 APR 01/16 31-31-00 534 23-22-00 3 APR 01/16 31-31-00 535 23-22-00 201 APR 01/16 31-31-00 536 23-22-00 501 APR 01/16 31-31-01 201 23-22-00 502 APR 01/16 31-31-01 202 23-22-00 503 APR 01/16 31-31-01 203 23-22-00 504 APR 01/16 31-31-99 201 23-22-00 505 APR 01/16 31-31-99 202 23-22-01 401 APR 01/16 31-33-00 1 23-22-01 402 APR 01/16 31-33-00 2 23-22-02 401 APR 01/16 31-33-00 3 23-22-02 402 APR 01/16 31-33-00 201 Chapter 31 Front Page 31-33-00 202 31-31-00 1 APR 01/16 31-33-00 203 31-31-00 2 APR 01/16 31-33-00 501 31-31-00 3 APR 01/16 31-33-00 502 31-31-00 4 APR 01/16 31-33-01 401 31-31-00 5 APR 01/16 31-33-01 402 31-31-00 6 APR 01/16 Chapter 34 Front Page 31-31-00 501 APR 01/16 34-22-00 501 31-31-00 502 APR 01/16 34-46-00 501 31-31-00 503 APR 01/16 34-46-00 502 31-31-00 504 APR 01/16 34-53-00 501 31-31-00 505 APR 01/16 34-58-01 401 31-31-00 506 APR 01/16 34-58-01 402 31-31-00 507 APR 01/16 34-58-01 403 31-31-00 508 APR 01/16 34-58-01 404 31-31-00 509 APR 01/16 34-58-01 405 31-31-00 510 APR 01/16 31-31-00 512 APR 01/16 31-31-00 513 APR 01/16 31-31-00 514 APR 01/16 31-31-00 515 APR 01/16 31-31-00 516 APR 01/16 31-31-00 517 APR 01/16 31-31-00 518 APR 01/16 31-31-00 519 APR 01/16 31-31-00 520 APR 01/16 31-31-00 521 APR 01/16 31-31-00 522 APR 01/16 31-31-00 523 APR 01/16 31-31-00 524 APR 01/16 31-31-00 525 APR 01/16 31-31-00 526 APR 01/16 31-31-00 527 APR 01/16
CHAPTER
EFFECTIVITY
23-22-00 AIRPLANES WITH SPECTRALUX DLINK+ ACARS Page 1 MOD-0006 APR 01/16
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
ACARS – DESCRIPTION AND OPERATION 1. General
A. ACARS (Aircraft Communications Addressing and Reporting System) is a digital data link system that enhances two-way communications between the airplane and a ground station.
B. ACARS enhances air/ground communications by easing the flight compartment work load, and
eliminating much of the air/ground voice communication traffic. ACARS enables a high-speed computer controlled digital data link between the airplane and ground facilities using: a VHF transceiver, ARINC or other data link stations, landlines, a central control station, and airline terminals. The data link exchanges routing airlines operations information.
C. ACARS receives data inputs from airplane sensors, external systems, and the pilot inputs.
Data communications is displayed to the pilot via Dlink+ ACARS Display. Outgoing data communications are sent automatically or manually. Data is sent using ARINC assigned frequencies in ARINC encoded audio frequency tone modulation over the ground data link stations.
D. ACARS receives power from the left 28v dc bus. The system circuit breaker is on the
overhead panel P11. 2. Component Details (Fig. 1)
A. Dlink+ ACARS Unit.
(1) The Dlink+ ACARS Unit provides Aircraft Communication Addressing and Reporting System (ACARS) message functionality by combining three ARINC devices into one cockpit equipment panel mounted device. The three devices are: (a) ARINC 7248 Communication Management Unit (CMU) (b) ARINC 750 VHF Data Link (VDL) Radio (c) ARINC 739 Multi-purpose Control Display Unit (MCDU)
Dlink+ ACARS Unit provides air to ground and ground to air data only communication. The system sends and receives free text messages and ACARS messages to support Aircraft Operational Control (AOC) communications over the ACARS VHF data link. The system has a Personality Module (PM) which is a serial EEPROM that houses the unit's configuration and database. When the unit power-up it reads the configuration from the PM into its internal Random Access Memory (RAM). This defines the system's hardware configuration and many of its settings.
(2) The Dlink+ ACARS Unit design features are:
(a) Keyboard & display assembly (b) Display unit/power supply printed circuit assembly (DU/PS PCA) (c) Single board computer printed circuit assembly (SBC PCA) (d) Auxiliary input/output printed circuit assembly (AI/O PCA) (e) VHF data link PCA (VDL PCA) (118-136.975MHz Receiver and 15W Transmitter) (f) Electronic assembly (g) Soft keys
B757 AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
23-22-00 AIRPLANES WITH SPECTRALUX DLINK+ ACARS Page 2 MOD-0006 APR 01/16
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
ACARS – Component Location
EFFECTIVITY
23-22-00 AIRPLANES WITH SPECTRALUX DLINK+ ACARS Page 3 MOD-0006 APR 01/16
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
B. Personality Module (PM).
(1) The personality Module (PM) stores database used by the DI ink+ ACARS Unit. When the Dlink+ Unit is power-up it reads the configuration from the (PM) into its internal Random Access Memory (RAM). This defines the system's hardware configuration and many of its settings.
(2) The Personality Module (PM) is a cable wrapped to one of the Dlink+ ACARS Unit mating
connector's cable. The Personality Module has a pigtail of four wires that are inserted into the associated mating connector. These wires are used to load the stored database to the Dlink+ ACARS Unit (RAM) and download new database information.
C. Data Printer
(1) The printer is used to print the various Dlink+ ACARS Unit screen forms. Additionally,
if connected to other compatible subsystem, it will also print the screen forms for that subsystem.
3. Operation
A. Functional Description
(1) Off mode
(a) Dlink+ ACARS Unit is off when 28v de left bus power is removed from the unit. There is no system activity or indications.
(2) Operation
(a) When the Dlink+ ACARS Unit is power on, the unit reads the configuration of the
Personality Module PM to random access memory (RAM), internal to the Dlink+. Once powered, the unit can provide the capabilities for sending and receiving free text messages and ACARS messages to support end-to-end Aircraft Operational Control (AOC) communication over the ACARS data link.
B757 AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
23-22-00 AIRPLANES WITH SPECTRALUX DLINK+ ACARS Page 201 MOD-0006 APR 01/16
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
ACARS - SOFTWARE INSTALLATION 1. General
A. This procedure contains the task to install the Spectralux Dlink+ ACARS Unit software into the Personality Module using a Laptop computer and the Ethernet maintenance port located on the P61 maintenance panel.
2. ACARS Software Installation with a Laptop Computer
A. References
B. Access
(a) P11-1 Overhead Circuit Breaker:
1) ACARS
(2) On the P61 maintenance panel, connect the Laptop computer containing the Laptop Loader Software to the Ethernet port.
(3) Turn the Laptop computer ON and start the Laptop Loader Software containing the Dlink+
configuration files for the aircraft.
(4) To load the Dlink+ ACARS configuration to the personality module click on the Write Config button and select the appropriated file that is provided for the aircraft.
(5) Once the appropriated file is selected, click OPEN to access the configuration software
file.
(6) Enter the Tail Number and the ICAO address for the aircraft and press OK.
NOTE: The Laptop Loader will close and the DI ink+ ACARS Unit will reboot.
(7) After the Dlink+ ACARS Unit reboot is completed, start the Laptop Loader Software and click the Write DB button.
(8) Select the customer or test database file provided for the aircraft and click OPEN.
NOTE: The Laptop Loader will close and the Dlink+ Unit will reboot
(9) Turn off the Laptop and disconnect the Ethernet cable from the P61 maintenance panel's
Ethernet port.
B757 AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
23-22-00 AIRPLANES WITH SPECTRALUX DLINK+ ACARS Page 501 MOD-0006 APR 01/16
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
ACARS – ADJUSTMENT/TEST 1. General
A. There are two tasks in this procedure. The first task is the operational test of the Dlink+ Aircraft Communications Addressing and Reporting System (ACARS). The second is the system test of the ACARS.
B. The operational test is a minimum check of the basic ACARS System.
C. The system test contains checks of all of the primary ACARS functions. The test includes
checks of the OOOI operation, and the ACARS interfaces.
D. When the ACARS cannot make a link with the ground station it is not a system failure. This is usually one of the following conditions:
(1) The RF path between the VHF antenna and the ground station is blocked. It can help to
move the airplane to a better position.
(2) The ground station has a problem. Tell them that you cannot make a link. If they have a problem, other airplanes that use the data link will also get no ACARS communication.
E. If you tow the airplane, or move it with its power, open the ACARS circuit breaker. If you
do not, the ACARS may transmit the Out time. 2. ACARS Operational Test
A. References
B. Prepare for the Operational Test
(1) Supply electrical power (AMM 24-22-00/201)
(2) Make sure these circuit breakers are closed:
(a) P11-1 Overhead Circuit Breaker Panel: 1) ACARS 2) Data Printer
C. Procedure
(1) Test Setup
(a) Locate the aircraft on the airfield away from any existing structures that may
shadow the reception from a remote VHF ground station.
(b) From the main menu of the Dlink+ ACARS Unit, locate the maintenance menu by navigating thru the unit's menu selection.
NOTE: The menus will look different depending on specific aircraft type and
installation. The maintenance menu can be located from a MISC or MAINT selection on the Dlink+ ACARS Unit main menu.
(c) From the Dlink+ ACARS Unit main menu, select the Line Select Key (LSK) adjacent to
the MISC or MAINT menu option as required to access the maintenance menu pages.
NOTE: The Dlink+ ACARS Maintenance Menu pages will normally contain radio status and OOOI status on the A half of the first page and typically contains a menu to check specific systems on page B.
B757 AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
23-22-00 AIRPLANES WITH SPECTRALUX DLINK+ ACARS Page 502 MOD-0006 APR 01/16
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
(2) Dlink+ VHF Ping Test
(a) From the Dlink+ ACARS Unit maintenance menu (page B), select the Line Select Key
(LSK) adjacent to the PING TEST prompt.
(b) From the PING TEST screen, select the Line Select Key (LSK) L2 adjacent to the TEST CONTROL prompt and verify that the display changes form STOP to GO.
(c) Verify for proper VHF connection and that the Ping Test passes by verifying that
the TEST CONTROL display changes to WAIT and then returns to STOP.
NOTE: The DELAY CNT will count the seconds until the response is received. The AVG SEC will show the time it takes to receive a response. If no test response is received after the timeout period the TEST CONTROL will display a FAIL message.
(3) Annunciator Lights Test
(a) On the Dlink+ ACARS Unit, press and hold the A/B Line Select Key (LSK).
(b) Verify that the Dlink+ ACARS Unit annunciator lights (MSG, TEMP and FAIL) come on.
D. Put the Airplane back to its Initial Condition
(1) Return the Dlink+ ACARS display to the main menu page.
(2) Remove electrical power (AMM 24-22-00/201).
3. ACARS System Test
A. References (1) AMM 24-22-00/201, Electrical Power- Control (2) AMM 31-31-00/501, Flight Data Recorder System (3) AMM 31-41-00/501, EICAS System (4) AMM 32-09-02/501, Air/Ground Relay System (5) AMM 32-44-00/501, Parking Brake System (6) AMM 33-13-00/501, Integral Panel Lights (7) AMM 34-12-00/501, Left Air Data Computer System (8) AMM 34-21-00/501, Inertial Reference System (9) AMM 34-61-00/501, Left Flight Management System (10) AMM 52-71-00/501, Door Warning System Proximity Sensors
B. Prepare for the System Test
(1) Supply electrical power (AMM 24-22-00/201)
(2) Make sure all aircraft doors are closed.
(3) Make sure the parking brake is set.
(4) Make sure these circuit breakers are closed:
(a) P11-1 Overhead Circuit Breaker Panel:
1) A CARS 2) Data Printer
C. Procedure
(1) Test Setup
(a) Locate the aircraft on the airfield away from any existing structures that may shadow the reception from a remote VHF ground station.
B757 AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
23-22-00 AIRPLANES WITH SPECTRALUX DLINK+ ACARS Page 503 MOD-0006 APR 01/16
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
(b) From the main menu of the Dlink+ ACARS Unit, locate the maintenance menu by navigating thru the unit's menu selection.
NOTE: The menus will look different depending on specific aircraft type and
installation. The maintenance menu can be located from a MISC or MAINT selection on the Dlink+ ACARS Unit main menu.
(c) From the Dlink+ ACARS Unit main menu, select the Line Select Key (LSK) adjacent to
the MISC or MAINT menu option as required to access the maintenance menu pages.
NOTE: The Dlink+ ACARS Maintenance Menu pages will normally contain radio status and OOOI status on the A half of the first page and typically contains a menu to check specific systems on page B
(2) Annunciator Lights Test
(a) On the Dlink+ ACARS Unit, press and hold the NB Line Select Key (LSK).
(b) Verify that the Dlink+ ACARS Unit annunciator lights (MSG, TEMP and FAIL) come on.
(3) Dlink+ OOOI Interface Test
(a) From the Dlink+ ACARS Unit maintenance (page A}, verify that the OOOI are
operating by changing the discrete states on the aircraft and verifying that they change state in the OOOI status maintenance menu screen:
DOORS (L1 & L2) Open/Close BRAKES (Parking Brake Set/Release) On/Off SQUAT (Aircraft Air/Ground Logic) Air/Ground
(4) Dlink+ Application Software Version Test
(a) From the Dlink+ ACARS Unit maintenance menu (page B), select the Line Select Key
(LSK) adjacent to the DUNK CONFIG prompt.
(b) From the CONFIG screen, select the Line Select Key (LSK) adjacent to the VERSION menu option.
(c) From the VERSION screen, Verify that the following Application Software are being
used: SBC 6B70 10 5D58 DU D849
NOTE: The Application Software versions are provided by Spectralux.
(d) Return to the Dlink+ ACARS Unit CONFIG menu screen.
(5) Dlink+ Aircraft Registration & ICAO Address Test
(a) From the CONFIG screen, select the Line Select Key (LSK) adjacent to the USER EDIT
prompt.
NOTE: The USER EDIT option can edit the user's configurations.
(b) Verify that the PASSWORD menu screen is displayed.
(c) Type in the user password in the proper location and press the ENTER key.
NOTE: The default user password is "USEROO"
(d) Verify that the EDIT CONFIGURATION 1/3 menu screen is displayed.
B757 AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
23-22-00 AIRPLANES WITH SPECTRALUX DLINK+ ACARS Page 504 MOD-0006 APR 01/16
Page produced by 365 Aerospace Limited, UK. Copyright ©. See Manual Supplement Introduction pages for information.
(e) From the EDIT CONFIGURATION screen (page 1), verify that the correct aircraft registration number and ICAO address is displayed.
(f) Return to the Dlink+ ACARS Unit to the maintenance menu screen.
(g) If any changes were made to the EDIT CONFIGURATION screen. Follow the steps to
return to the Dlink+ ACARS Unit maintenance menu screen.
1) Select the Line Select Key (LSK) adjacent to the RETURN prompt, and verify that the CONFIRMATION menu is displayed.
2) On the CONFIRMATION menu screen, press the Line Select Key (LSK) until the NO
or YES option is displayed.
NOTE: Pressing the LSK will cycle the selection to NO, CANCEL and YES.
3) Once the NO or YES option is selected, select the Line Select Key (LSK) adjacent to the RETURN prompt to return the Dlink+ ACARS Unit to the maintenance menu screen.
(6) Dlink+ Monitor Bus Status Test
(a) From the Dlink+ ACARS Unit maintenance menu (page B), select the Line Select Key
(LSK) adjacent to the MONITOR prompt.
NOTE: The Monitor menu will display the status of each of the 429 busses and some of the key variables interfaced to the Dlink+ ACARS Unit.
(b) From the MONITOR Bus Status screen, verify that each of the following 429 busses
EICAS, FMC, ADC and IRU display a GOOD status.
(c) Open each of the respective C/B for the EICAS, FMC, ADC and IRU systems. Verify that each of the respective 429 busses EICAS, FMC, ADC, and IRU display a FAIL status.
(d) Reset the C/B for the EICAS, FMC, ADC and IRU systems. Verify that each of the
following 429 busses EICAS, FMC, ADC, and IRU display a GOOD status.
(e) If there are any Variables displayed on the MONITOR Bus Status screen, verify that each of the variables display a value and not XXX.
(f) Return to the Dlink+ ACARS Unit maintenance menu screen.
(7) Dlink+ Printer Interface Test
(a) From the Dlink+ ACARS Unit maintenance menu (page B), select the Line Select Key
(LSK) adjacent to the PRINT TEST prompt.
(b) From the PRINTER TEST screen, select the Line Select Key (LSK) adjacent to the PRINT prompt and verify that the data printer prints the information selected on the Dlink+ ACARS screen.
(c) Return to the Dlink+ ACARS Unit maintenance menu screen.
(8) Dlink+ VHF Ping Test
(a) From the Dlink+ ACARS Unit maintenance menu (page B}, select the Line Select Key
(LSK) adjacent to the PING TEST prompt.
(b) From the PING TEST screen, select the Line Select Screen (LSK) L2 adjacent to the TEST CONTROL prompt and verify that the display changes form STOP to GO.
B757 AIRCRAFT MAINTENANCE MANUAL
EFFECTI