Commercial 

Airplanes 757

Service Bulletin

SPECIAL ATTENTION

Number: 757-24-0132

Original Issue: April 14, 2011

Revision 1: June 19, 2012

ATA System: 2431

SUBJECT: ELECTRICAL POWER - Batteries - Change to the Battery Charger System Wiring for

Extended Flight on Limited Standby Power

Export of this technology is controlled under the United States Export Administration Regulations (EAR) (15

CFR 300-774). An export license may be required before it is used for development, production or use by foreign

persons from specific countries. The controller of this data has the individual responsibility to abide by all export

laws.

ECCN: 9E991

BOEING PROPRIETARY, CONFIDENTIAL AND/OR TRADE SECRET

Copyright © 2011 Boeing.

Unpublished Work. All Rights Reserved.

Treatment of this document and its content is governed by contract with Boeing. Rights to use this document

are licensed on a per aircraft basis and such rights may not be transferable. For more information, contact The

Boeing Company.

Boeing, the Boeing signature, the Boeing symbol, 707, 717, 727, 737, 747, 757, 767, 777, 787, DreamlinerTM,

BBJ, DC-8, DC-9, DC-10, KC-10, KDC-10, MD-10, MD-11, MD-80, MD-88, MD-90, P-8A, Poseidon and Boeing

liveries are all trademarks owned by The Boeing Company; and no trademark license is granted in connection

with this document unless provided in writing by Boeing. BOEING is a trademark of Boeing Management

Company.

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11.0
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BLANK PAGE
Table of Contents

Revision Transmittal Sheet ............................................ 5

Summary ...................................................... 9

1. PLANNING INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

A. Effectivity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

1. Airplanes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

2. Spares Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17

B. Concurrent Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17

C. Reason . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18

D. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18

E. Compliance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

F. Approval . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

G. Manpower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20

H. Weight and Balance Changes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

I. Electrical Load Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

J. References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

1. Existing Data: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

2. Data Supplied with this Service Bulletin: . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

3. Installation Drawings Used in the Preparation of this Service Bulletin: . . . . . . . . . . . 24

K. Publications Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24

L. Interchangeability and Intermixability of Parts . . . . . . . . . . . . . . . . . . . . . . . . . . . 24

M. Software Accomplishment Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24

2. MATERIAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25

A. Material - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25

B. Industry Support Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25

C. Parts Necessary for Each Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26

1. Kits/Parts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26

2. Parts and Materials Supplied by the Operator . . . . . . . . . . . . . . . . . . . . . . . . 29

3. Parts Modified and Reidentified . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29

4. Parts Removed and Not Replaced . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29

D. Parts Necessary to Change Spares . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29

E. Special Tooling - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29

F. Special Tooling Necessary to do this Service Bulletin . . . . . . . . . . . . . . . . . . . . . . . 29

3. ACCOMPLISHMENT INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31

A. GENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31

B. WORK INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31

FIGURE 1: WIRE ROUTING FOR WIRE BUNDLE W2078 . . . . . . . . . . . . . . . . . . . . . . . . 36

FIGURE 2: WIRING CHANGE FOR WIRE BUNDLE W2078 [Group 1] . . . . . . . . . . . . . . . . . 42

FIGURE 3: WIRING CHANGE FOR WIRE BUNDLE W2078 [Group 2] . . . . . . . . . . . . . . . . . 45

FIGURE 4: WIRING CHANGE FOR WIRE BUNDLE W2078 [Group 3] . . . . . . . . . . . . . . . . . 48

FIGURE 5: WIRING CHANGE FOR WIRE BUNDLE W2078 [Group 4] . . . . . . . . . . . . . . . . . 51

FIGURE 6: WIRING CHANGE FOR WIRE BUNDLE W2078 [Group 6] . . . . . . . . . . . . . . . . . 54

FIGURE 7: WIRING CHANGE FOR WIRE BUNDLE W2078 [Group 7] . . . . . . . . . . . . . . . . . 57

FIGURE 8: WIRING CHANGE FOR WIRE BUNDLE W2078 [Group 5, 8] . . . . . . . . . . . . . . . . 60

FIGURE 9: WIRE ROUTING FOR WIRE BUNDLE W1260 . . . . . . . . . . . . . . . . . . . . . . . . 63

FIGURE 10: WIRING CHANGE FOR WIRE BUNDLE W1260 [Group 1, 8] . . . . . . . . . . . . . . . . 65

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BOEING SERVICE BULLETIN 757-24-0132
FIGURE 11: WIRING CHANGE FOR WIRE BUNDLE W1260 [Group 2, 6] . . . . . . . . . . . . . . . . 67

FIGURE 12: WIRING CHANGE FOR WIRE BUNDLE W1260 [Group 3] . . . . . . . . . . . . . . . . . 69

FIGURE 13: WIRING CHANGE FOR WIRE BUNDLE W1260 [Group 4, 7] . . . . . . . . . . . . . . . . 71

FIGURE 14: WIRING CHANGE FOR WIRE BUNDLE W1260 [Group 5] . . . . . . . . . . . . . . . . . 73

FIGURE 15: INSTALLATION OF RELAY ON P36 PANEL . . . . . . . . . . . . . . . . . . . . . . . . . 75

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BOEING SERVICE BULLETIN 757-24-0132
Commercial 

Airplanes 757

Service Bulletin

SPECIAL ATTENTION

Revision Transmittal Sheet Number: 757-24-0132

Original Issue: April 14, 2011

Revision 1: June 19, 2012

ATA System: 2431

SUBJECT: ELECTRICAL POWER - Batteries - Change to the Battery Charger System Wiring for

Extended Flight on Limited Standby Power

This revision includes all pages of the service bulletin.

COMPLIANCE INFORMATION RELATED TO THIS REVISION

No more work is necessary on the airplane(s) changed in accordance with the original issue of this service

bulletin.

REASON FOR REVISION

As a part of a service bulletin validation program, this change was completed on airplane ND049 by Service

Bulletin 757-24-0132 Original Issue before the release of Revision 1 of this service bulletin. The changes

completed on airplane ND049 by Service Bulletin 757-24-0132 Original Issue is equivalent to the release of

Revision 1 of this service bulletin. Airplane ND049 has the configuration of a Group 1 airplane.

The original issue of this service bulletin did not provide the split configurations for wires installed in the flight

deck in TB111 terminal track. As a result, airplanes in Group 1, Group 2 and Group 4 were moved into new

Group 8, Group 6 and Group 7 respectively and to provides the new changed instructions for those airplanes.

This revision is sent to change the original issue service bulletin to correct the groupings in the effectivity

applicabilities of section 1.A as follows:

– Airplanes moved from Group 2 to Group 6:

NB561-NB561

– Airplanes moved from Group 4 to Group 7:

NA237-NA239

– Airplanes moved from Group 1 to Group 8:

NA585-NA586, NB148, NB161-NB162, NB168, NB221-NB228, NB230, NB236, NB294-NB299,

NB301-NB302, NB431-NB438, NB446, NB453-NB454, NB511-NB523, NB571, NB581-NB583,

NC058-NC062, NC068-NC084, NC091-NC094, NC151, NC161, NC936-NC950, ND111-ND113,

ND189-ND199, ND224-ND225, ND244-ND248, ND301-ND322, ND401, NE006-NE008, NE091-NE094,

NE301-NE302, NE311-NE325, NL001-NL002, NL006-NL017, NN001-NN002, NN051-NN052, NP901-NP904,

NS601-NS616, NT001-NT009, NT201-NT202, NT231-NT234, NT237-NT240, NT242, NT245-NT248,

NT281-NT289, NT341-NT347, NT351-NT360, NT371-NT373, NT375-NT379, NT381-NT386, NT401-NT409,

NT411-NT412, NT426-NT427, NT431-NT432, NT436-NT438, NT441-NT442, NT446, NT701-NT769,

NT791-NT796, NT861-NT862, NT881-NT885, NT901-NT916, NT971-NT985, NU031-NU038, NU701-NU705,

NU721-NU728, NU731-NU732

These sections were changed:

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1. Summary Background: Clarified to include reference to wire changes.

2. Summary Action: Clarified to include reference to wire changes.

3. Summary Manpower:

– Added new hour table for new Group 6, Group 7 and Group 8.

– Included note regarding optional open/close access hours.

4. Paragraph 1.A. Effectivity: Defined new Group 6, Group 7 and Group 8 airplanes.

5. Paragraph 1.C. Reason: Added information about the changes made as a result of the service bulletin

validation.

6. Paragraph 1.D. Description: Added data for Group 6, Group 7 and Group 8 airplanes.

7. Paragraph 1.G. Manpower: Added note for optional access hours and new tables for Group 6, Group

7 and Group 8 airplanes.

8. Paragraph 1.K. Publications Affected: Added 757 Flight Crew Operations Manual NNC 06.

9. Paragraph 2.A. Material: Changed price and available date(s) of top kits (remove this paragraph if top

kit price does not change).

10. Paragraph 2.C. Parts Necessary for Each Airplane: Replaced existing wire subkit kit 280N3373-101

with new wire subkit 280N3372-104 that contains new parts and wires needed to complete the service

bulletin.

11. Paragraph 3.A. General Information:

– Deleted existing Note 1.

– Renumbered existing Notes 2-5 to Notes 1-4.

– Added new Note 5.

12. Paragraph 3.B. Effectivity:

a. Divided work instructions into four parts:

– Part 1 - Open Access.

– Part 2 - Rework Instructions.

– Part 3 - Close Access.

– Part 4 - Test.

b. Changed functional test steps.

13. Figure 2 - Added new terminal block (if needed), wire, I.D. tape and splice.

14. Figure 3 - Added new terminal block (if needed), wire, I.D. tape and splice.

15. Figure 4 - Added new terminal block (if needed), wire, I.D. tape and splice.

16. Figure 5 - Added new terminal block (if needed), wire, I.D. tape and splice.

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BOEING SERVICE BULLETIN 757-24-0132
17. Figure 6:

– Moved existing Figure 6 to Figure 9.

– Limited new Figure 6 to Group 6 airplanes.

– Added new terminal block (if needed), wire, I.D. tape and splice.

18. Figure 7:

– Moved existing Figure 7 to Figure 10.

– Limited new Figure 7 to Group 7 airplanes.

– Added new terminal block (if needed), wire, I.D. tape and splice.

19. Figure 8:

– Moved existing Figure 8 to Figure 11.

– Limited new Figure 8 to Group 5 and Group 8 airplanes.

– Added new terminal block (if needed), wire, I.D. tape and splice.

20. Figure 9:

– Moved existing Figure 9 to Figure 12.

– Was old Figure 6.

21. Figure 10:

– Moved existing Figure 10 to Figure 13.

– Was old Figure 7.

– Limited new Figure 10 to Group 1 and Group 8 airplanes.

– Added Flag Note 9.

22. Figure 11:

– Moved existing Figure 11 to Figure 14.

– Was old Figure 8.

– Limited new Figure 11 to Group 2 and Group 6 airplanes.

– Added Flag Note 9.

23. Figure 12:

– Moved existing Figure 12 to Figure 15.

– Was old Figure 9.

– Limited new Figure 12 to Group 3 airplanes.

– Added Flag Note 9.

24. Figure 13:

– Was old Figure 10.

– Limited new Figure 13 to Group 4 and Group 7 airplanes.

– Added Flag Note 9.

25. Figure 14:

– Was old Figure 11.

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BOEING SERVICE BULLETIN 757-24-0132
– Limited new Figure 14 to Group 5 airplanes.

– Added Flag Note 9.

26. Figure 15: Was old Figure 12.

Vertical lines are put on the left edge of each page, except in Paragraph 1.A., Effectivity, to show the location

of important changes.

Pages with no vertical lines have no important changes.

REVISION HISTORY

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BOEING SERVICE BULLETIN 757-24-0132
Commercial 

Airplanes 757

Service Bulletin

SPECIAL ATTENTION

Summary Number: 757-24-0132

Original Issue: April 14, 2011

Revision 1: June 19, 2012

ATA System: 2431

SUBJECT: ELECTRICAL POWER - Batteries - Change to the Battery Charger System Wiring for

Extended Flight on Limited Standby Power

BOEING RECOMMENDS THAT EACH OPERATOR EXAMINE THIS SERVICE BULLETIN IMMEDIATELY.

CONCURRENT REQUIREMENTS

None.

BACKGROUND

Accomplishment of this service bulletin will let the main battery charger stay powered when the right main AC

bus is powered and when the standby power switch is set to the BAT position during flight. This will prevent

discharge of the main battery. If this service bulletin is not done, the battery will discharge and could cause the

airplane to lose battery power. This would result in the loss of airplane systems connected to the standby buses,

and could affect flight and landing operations.

During the flight of a 757 airplane, the standby power OFF indication came on. The flight crew set the standby

power switch to the BAT position and continued with the flight. The flight continued beyond the battery's capability

to supply power to the standby loads and a number of system annunciations came on. The hot battery bus,

battery bus, DC standby bus and AC standby bus had lost power. The pilots found that the horizontal stabilizer

trim was not available and lateral control was affected. During landing, the inboard tires blew due to lack of

inboard anti-skid. When the airplane stopped, the engines could not be powered off until the standby power

switch was set back to the AUTO position and main generators were switched on to put back power to the

battery charger, battery and the fuel shutoff valves. Some of these conditions would also be found on 767

airplanes.

This service bulletin gives instructions to change wiring and add a new air/ground relay to the battery charger

system. This change will keep the main battery charger powered when right main AC power is available through

the ground service bus and when the standby power switch is in the BAT position during flight. This will prevent

discharge of the main battery.

Boeing Service Related Problem (SRP) 757-SRP-24-0135 is related to this service bulletin.

ACTION (PRR 54530-290RS)

Do the wiring changes between the P5 overhead panel and P36 miscellaneous electronics equipment panel.

Get access to the P36 miscellaneous electronics equipment panel and install a new relay and wires. Do a test

to make sure the change operates correctly.

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EFFECTIVITY

757-200/-200CB/-200PF/-300 Airplanes. Refer to Paragraph 1.A.1., Airplanes, for the list of affected airplanes.

COMPLIANCE

The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to this service

bulletin. The Airworthiness Directive will make the compliance tasks and times given in this service bulletin

mandatory.

Boeing recommends that the change given in this service bulletin be done within 60 months after the Revision

1 date of this service bulletin.

INDUSTRY SUPPORT INFORMATION

Boeing warranty remedies are not available for the configuration changes given in this service bulletin.

MANPOWER

Airplanes Total Task Hours Elapsed Hours

Group 1 Airplanes 22.5* 12.9*

Group 2 Airplanes 22.5* 12.9*

Group 3 Airplanes 22.5* 12.9*

Group 4 Airplanes 22.5* 12.9*

Group 5 Airplanes 22.5* 12.9*

Group 6 Airplanes 22.5* 12.9*

Group 7 Airplanes 22.5* 12.9*

Group 8 Airplanes 22.5* 12.9*

* Hours do not include optional open/close access steps.

MATERIAL INFORMATION

Boeing Supplied Kits/Parts.

Refer to Paragraph 2.A., Material - Price and Availability.

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BLANK PAGE
Commercial 

Airplanes 757

Service Bulletin

SPECIAL ATTENTION

Number: 757-24-0132

Original Issue: April 14, 2011

Revision 1: June 19, 2012

ATA System: 2431

SUBJECT: ELECTRICAL POWER - Batteries - Change to the Battery Charger System Wiring for

Extended Flight on Limited Standby Power

BOEING RECOMMENDS THAT EACH OPERATOR EXAMINE THIS SERVICE BULLETIN IMMEDIATELY.

1. PLANNING INFORMATION

A. Effectivity

1. Airplanes

This service bulletin is for the airplanes shown below. Refer to PRR 54530-290RS for data about

this change.

Refer to Service Bulletin Index Document D624N001 Part 3 for Airplane Variable Number, Line

Number, and Serial Number data.

GROUP CONFIGURATION DESCRIPTION

1 - Airplanes with different wire configurations.

2 - Airplanes with different wire configurations.

3 - Airplanes with different wire configurations.

4 - Airplanes with different wire configurations.

5 - Airplanes with different wire configurations.

6 - Airplanes with different wire configurations.

7 - Airplanes with different wire configurations.

8 - Airplanes with different wire configurations.

Airplane Models:

757-200, 757-200CB, 757-200PF, 757-300

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Variable Number Group

NA002 - NA021 3

NA022 - NA028 2

NA191 - NA192 3

NA193 - NA199 2

NA201 - NA236 4

NA237 - NA239 7

NA301 - NA305 4

NA341 - NA352 4

NA391 - NA399 4

NA401 - NA408 1

NA441 - NA447 1

NA501 - NA584 1

NA585 - NA586 8

NB001 - NB004 1

NB021 - NB023 1

NB036 - NB041 1

NB051 - NB053 1

NB061 - NB073 1

NB079 1

NB131 - NB147 1

NB148 8

NB161 - NB162 8

NB166 - NB167 1

NB168 8

NB201 - NB204 1

NB221 - NB228 8

NB230 8

NB236 8

NB239 1

NB261 - NB267 1

NB291 - NB293 1

NB294 - NB299 8

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BOEING SERVICE BULLETIN 757-24-0132
Variable Number Group

NB301 - NB302 8

NB311 - NB312 1

NB321 - NB331 1

NB421 - NB430 1

NB431 - NB438 8

NB446 8

NB451 - NB452 1

NB453 - NB454 8

NB501 - NB510 1

NB511 - NB523 8

NB561 6

NB571 8

NB581 - NB583 8

NC001 - NC033 1

NC041 - NC042 1

NC051 - NC052 1

NC056 - NC057 1

NC058 - NC062 8

NC066 - NC067 1

NC068 - NC084 8

NC091 - NC094 8

NC151 8

NC161 8

NC901 - NC935 1

NC936 - NC950 8

NC951 1

NC971 - NC974 1

ND001 - ND007 1

ND011 - ND059 1

ND111 - ND113 8

ND161 - ND188 1

ND189 - ND199 8

ND201 - ND203 1

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BOEING SERVICE BULLETIN 757-24-0132
Variable Number Group

ND221 - ND223 1

ND224 - ND225 8

ND241 - ND243 1

ND244 - ND248 8

ND301 - ND322 8

ND401 8

ND891 1

ND895 1

NE001 - NE005 1

NE006 - NE008 8

NE011 - NE088 1

NE091 - NE094 8

NE141 - NE150 1

NE161 - NE177 1

NE201 - NE204 1

NE301 - NE302 8

NE311 - NE325 8

NJ001 - NJ004 5

NJ031 - NJ032 5

NJ551 - NJ555 5

NL001 - NL002 8

NL006 - NL017 8

NL101 - NL109 5

NL141 5

NL601 - NL616 5

NN001 - NN002 8

NN051 - NN052 8

NP901 - NP904 8

NS601 - NS616 8

NT001 - NT009 8

NT201 - NT202 8

NT231 - NT234 8

NT237 - NT240 8

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BOEING SERVICE BULLETIN 757-24-0132
Variable Number Group

NT242 8

NT245 - NT248 8

NT281 - NT289 8

NT341 - NT347 8

NT351 - NT360 8

NT371 - NT373 8

NT375 - NT379 8

NT381 - NT386 8

NT401 - NT409 8

NT411 - NT412 8

NT426 - NT427 8

NT431 - NT432 8

NT436 - NT438 8

NT441 - NT442 8

NT446 8

NT701 - NT769 8

NT791 - NT796 8

NT861 - NT862 8

NT881 - NT885 8

NT901 - NT916 8

NT971 - NT985 8

NU031 - NU038 8

NU701 - NU705 8

NU721 - NU728 8

NU731 - NU732 8

2. Spares Affected

None.

B. Concurrent Requirements

None.

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BOEING SERVICE BULLETIN 757-24-0132
C. Reason

Accomplishment of this service bulletin will let the main battery charger stay powered when the right

main AC bus is powered and when the standby power switch is set to the BAT position during flight.

This will prevent discharge of the main battery. If this service bulletin is not done, the battery will

discharge and could cause the airplane to lose battery power. This would result in the loss of airplane

systems connected to the standby buses and could affect flight and landing operations.

During the flight of a 757 airplane, the standby power OFF indication came on. The flight crew set the

standby power switch to the BAT position and continued with the flight. The flight continued beyond

the battery's capability to supply power to the standby loads and a number of system annunciations

came on. The hot battery bus, battery bus, DC standby bus and AC standby bus had lost power. The

pilots found that the horizontal stabilizer trim was not available and lateral control was affected. During

landing, the inboard tires blew due to lack of inboard anti-skid. When the airplane stopped, the engines

could not be powered off until the standby power switch was set back to the AUTO position and main

generators were switched on to put back power to the battery charger, battery and the fuel shutoff

valves. Some of these conditions would also be found on 767 airplanes.

This service bulletin gives instructions to change wiring and add a new air/ground relay to the battery

charger system. This change will keep the main battery charger powered when right main AC power

is available through the ground service bus and when the standby power switch is in the BAT position

during flight. This will prevent discharge of the main battery.

Boeing Service Related Problem (SRP) 757-SRP-24-0135 is related to this service bulletin.

As a part of a service bulletin validation program, this change was completed on airplane ND049 by

Service Bulletin 757-24-0132 Original Issue before the release of Revision 1 of this service bulletin.

The changes completed on airplane ND049 by Service Bulletin 757-24-0132 Original Issue is equivalent

to the release of Revision 1 of this service bulletin. Airplane ND049 has the configuration of a Group

1 airplane.

Revision 1 is sent to include the changes found during the validation of this service bulletin on Group

1 airplane ND049. The changes include:

– Adding a new burndy block in terminal track TB111 (if necessary).

– Installation of new splice and new wire to increase the length of an existing rerouted wire.

– Made clarifications to the functional test.

– Provide additional open/close access instructions in the flight compartment.

D. Description

Do the wiring changes between the P5 overhead panel and P36 miscellaneous electronics equipment

panel. Get access to the P36 miscellaneous electronics equipment panel and install a new relay and

wires. Do a test to make sure the change operates correctly.

The work in this service bulletin is done in the maintenance zone(s) given below.

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Group 1:

Affected Maintenance Zones

Model Zone

757-200, 757-200CB, 757- 118, 119, 122

200PF

Group 2-4, 6-7:

Affected Maintenance Zones

Model Zone

757-200 118, 119, 122

Group 5:

Affected Maintenance Zones

Model Zone

757-200, 757-300 118, 119, 122

Group 8:

Affected Maintenance Zones

Model Zone

757-200, 757-200PF, 757-300 118, 119, 122

E. Compliance

The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to

this service bulletin. The Airworthiness Directive will make the compliance tasks and times given in this

service bulletin mandatory.

Boeing recommends that the change given in this service bulletin be done within 60 months after the

Revision 1 date of this service bulletin.

F. Approval

This service bulletin was examined by the Federal Aviation Administration (FAA). The changes specified

in this service bulletin comply with the applicable regulations and are FAA approved, as well as European

Aviation Safety Agency (EASA)/Joint Aviation Authorities (JAA) approved for all EASA/JAA approved

airplanes listed in the service bulletin effectivity. This service bulletin and its approval were based on

the airplane in its original Boeing delivery configuration or as modified by other approved Boeing

changes.

If an airplane has a non-Boeing modification or repair that affects a component or system also affected

by this service bulletin, the operator is responsible for obtaining appropriate regulatory agency approval

before incorporating this service bulletin.

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G. Manpower

The table below shows an estimate of the task hours necessary to do this configuration change for

each airplane. This estimate is for direct labor only, done by an experienced crew. Adjust the estimate

with operator task hour data if necessary. The estimate does not include lost time. These are some

examples of lost time:

• Time to adjust to the workplace

• Time to schedule the work

• Time to inspect the work

• Time to cure the materials

• Time to make the parts

• Time to find the tools.

Group 1:

Task Number of Persons Task Hours Elapsed Hours

Open Access 1 1.5* 1.5*

FIGURE 1 and FIG- 2 12.0 6.0

URE 2

FIGURE 9 and FIG- 2 4.8 2.4

URE 10

FIGURE 15 1 0.25 0.25

Close Access 1 1.5* 1.5*

Test 2 2.5 1.25

TOTAL FOR EACH AIRPLANE 22.5 12.9

* Hours do not include optional open/close access steps.

Group 2:

Task Number of Persons Task Hours Elapsed Hours

Open Access 1 1.5* 1.5*

FIGURE 1 and FIG- 2 12.0 6.0

URE 3

FIGURE 9 and FIG- 2 4.8 2.4

URE 11

FIGURE 15 1 0.25 0.25

Close Access 1 1.5* 1.5*

Test 2 2.50 1.25

TOTAL FOR EACH AIRPLANE 22.5 12.9

* Hours do not include optional open/close access steps.

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Group 3:

Task Number of Persons Task Hours Elapsed Hours

Open Access 1 1.5* 1.5*

FIGURE 1 and FIG- 2 12.0 6.0

URE 4

FIGURE 9 and FIG- 2 4.8 2.4

URE 12

FIGURE 15 1 0.25 0.25

Close Access 1 1.5* 1.5*

Test 2 2.5 1.25

TOTAL FOR EACH AIRPLANE 22.5 12.9

* Hours do not include optional open/close access steps.

Group 4:

Task Number of Persons Task Hours Elapsed Hours

Open Access 1 1.5* 1.5*

FIGURE 1 and FIG- 2 12.0 6.0

URE 5

FIGURE 9 and FIG- 2 4.8 2.4

URE 13

FIGURE 15 1 0.25 0.25

Close Access 1 1.5* 1.5*

Test 2 2.5 1.25

TOTAL FOR EACH AIRPLANE 22.5 12.9

* Hours do not include optional open/close access steps.

Group 5:

Task Number of Persons Task Hours Elapsed Hours

Open Access 1 1.5* 1.5*

FIGURE 1 and FIG- 2 12.0 6.0

URE 8

FIGURE 9 and FIG- 2 4.8 2.4

URE 14

FIGURE 15 1 0.25 0.25

Close Access 1 1.5* 1.5*

Test 2 2.5 1.25

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Group 5:

Task Number of Persons Task Hours Elapsed Hours

TOTAL FOR EACH AIRPLANE 22.5 12.9

* Hours do not include optional open/close access steps.

Group 6:

Task Number of Persons Task Hours Elapsed Hours

Open Access 1 1.5* 1.5*

FIGURE 1 and FIG- 2 12.0 6.0

URE 6

FIGURE 9 and FIG- 2 4.8 2.4

URE 11

FIGURE 15 1 0.25 0.25

Close Access 1 1.5* 1.5*

Test 2 2.5 1.25

TOTAL FOR EACH AIRPLANE 22.5 12.9

* Hours do not include optional open/close access steps.

Group 7:

Task Number of Persons Task Hours Elapsed Hours

Open Access 1 1.5* 1.5*

FIGURE 1 and FIG- 2 12.0 6.0

URE 7

FIGURE 9 and FIG- 2 4.8 2.4

URE 13

FIGURE 15 1 0.25 0.25

Close Access 1 1.5* 1.5*

Test 2 2.5 1.25

TOTAL FOR EACH AIRPLANE 22.5 12.9

* Hours do not include optional open/close access steps.

Group 8:

Task Number of Persons Task Hours Elapsed Hours

Open Access 1 1.5* 1.5*

FIGURE 1 and FIG- 2 12.0 6.0

URE 8

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Group 8:

Task Number of Persons Task Hours Elapsed Hours

FIGURE 9 and FIG- 2 4.8 2.4

URE 10

FIGURE 15 1 0.25 0.25

Close Access 1 1.5* 1.5*

Test 2 2.5 1.25

TOTAL FOR EACH AIRPLANE 22.5 12.9

* Hours do not include optional open/close access steps.

H. Weight and Balance Changes

Change in Moment

(Pound-Inches)

Change in Weight

Airplane (Pounds)

757-200 Airplanes +1.0 +386.0

757-300 Airplanes +1.0 +226.0

I. Electrical Load Data

Not changed.

J. References

1. Existing Data:

a. Engineering Change Memo PRR 54530-290RS

b. Boeing Service Related Problem (SRP) 757-SRP-24-0135

c. Standard Overhaul Practices Manual (SOPM) 20-50-05, 20-50-10

d. Standard Wiring Practices Manual (SWPM) 20-10-11, 20-10-12, 20-10-19, 20-30-12, 20-61-11,

20-81-12, 20-81-22, 20-90-11

e. 757 Aircraft Maintenance Manual (AMM) 24-22-00, 24-33-04, 25-25-01, 25-27-01, 25-31-01,

30-31-00, 33-16-00, 52-34-00, 53-01-01

f. 757 Wiring Diagram Manual (WDM) 24-31-11, 32-09-11

g. Service Bulletin Index Document D624N001

2. Data Supplied with this Service Bulletin:

None.

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BOEING SERVICE BULLETIN 757-24-0132
3. Installation Drawings Used in the Preparation of this Service Bulletin:

Drawing Number Title

SUB KIT - EQUIPMENT / WIRE INSTALLATION. EXTENDED

FLIGHT ON LIMITED STANDBY POWER.

012N0032

280N3373 WIRE KIT - EXTENDED FLIGHT ON LIMITED STANDBY POWER

These drawings were used to prepare this service bulletin. These drawings are not necessary to

make the specified changes, and are not supplied with this service bulletin. These drawings may

not be applicable to all airplane configurations or operators.

K. Publications Affected

1. Publications:

Publication Chapter-Section

757 Flight Crew Operations Manual NNC 06 (a)

757 Aircraft Maintenance Manual 24-30

757 Wiring Diagram Manual 24-31, 32-09, Equipment List

757 Illustrated Parts Catalog 32-09

757 System Schematic Manual 24-31, 32-09

(a) FCOM NNC 06 will be removed from the FCOM QRH after each operator has

notified Boeing that they have completed the incorporation of this service

bulletin on their fleet..

2. Damage Tolerance Based Structural Inspections:

Boeing has evaluated the repairs and/or changes in this service bulletin for effects on Fatigue

Critical Structure (FCS) and for changes to Damage Tolerance Inspections (DTI) required in the

Maintenance Program. This service bulletin does not affect FCS, therefore DTIs are not necessary.

L. Interchangeability and Intermixability of Parts

Accomplishment of this service bulletin does not affect interchangeability or intermixability of parts.

M. Software Accomplishment Summary

Not affected.

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2. MATERIAL INFORMATION

A. Material - Price and Availability

Boeing can supply the kits shown in Paragraph 2.C., Parts Necessary for Each Airplane, as shown

below. If there is a limit to the quantity of available kits, a supply sequence is given by Spares. More

kits become available as shown in the Reorder Lead Time (ROLT). ROLT is calculated from the date

Boeing gets the purchase order.

Group 1-4, 6-8:

Unit Price thru

January 13,

2013

ROLT

(Weeks)

Kit Number Name Date QTY

May 7, 5 23 $728.00

2012

TOP KIT - RETROFIT

KIT FOR EXTENDED

FLIGHT ON LIMITED

STANDBY POWER

012N8929-20

May 4 23 $728.00

21,2012

Group 5:

Unit Price thru

January 13,

2013

ROLT

(Weeks)

Kit Number Name Date QTY

TOP KIT - RETROFIT - - 23 $733.00

KIT FOR EXTENDED

FLIGHT ON LIMITED

STANDBY POWER

012N8929-25

The kits are subject to the terms and conditions of the Boeing standard purchase order acknowledgment.

After the Unit Price date, new price and ROLT data is applicable. Prices are in United States dollars.

Terms: Net 30 days.

Reference this service bulletin and submit your purchase order by one of the methods that follow:

1. Order on-line via ATA Spec 2000 or Boeing Part Page

2. Fax to (206) 662-7145

3. Mail to:

Spares Customer Support - MC 36-65

Boeing Spares Department

P.O. Box 3707

Seattle, Washington 98124-2207 USA

B. Industry Support Information

Boeing warranty remedies are not available for the configuration changes given in this service bulletin.

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BOEING SERVICE BULLETIN 757-24-0132
C. Parts Necessary for Each Airplane

1. Kits/Parts

To get the kits/parts shown below, refer to Paragraph 2.A., Material - Price and Availability.

NOTE: One top kit and the items shown in Paragraph 2.C.2., Parts and Materials Supplied by

the Operator, are necessary for each airplane. The Top Kit is divided into Figure kits for

each installation figure shown in the table below.

Figure Kit

Top Kit 1 9 15

012N8929-20 1 1 1

012N8929-25 1 1 1

Top Kit

Wire Kit 012N8929-20 012N8929-25

280N3373- 1 -

102

280N3373- 1 1

104

280N3373- - 1

103

Group 1-4, 6-8:

KIT 012N8929-20

Notes

Existing Part

Name Number

Figure

New Part Number

1 9 15

Qty

012N0032-2 . . 1 BRADY LABEL

LACING TAPE - (a)

WHITE

280N3373-2001 . 1 .

LACING TAPE - (a)

BLUE

280N3373-2002 1 . .

BACR13CF2AB . . 1 RELAY

(a) There are more parts than are necessary.

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Group 5:

KIT 012N8929-25

Notes

Existing Part

Name Number

Figure

New Part Number

1 9 15

Qty

012N0032-2 . . 1 BRADY LABEL

LACING TAPE - (a)

WHITE

280N3373-2001 . 1 .

LACING TAPE - (a)

BLUE

280N3373-2002 1 . .

BACR13CF2AB . . 1 RELAY

(a) There are more parts than are necessary.

Group 1-4, 6-8:

KIT 280N3373-102

New Part Number Qty Name Notes

New cut

and coded wires

for wire

bundle

W1260

280N3373-102W 1 WIRE LIST

CONNECTOR I.D.

TAPE - D41850J

280N3373-10201 1

CONNECTOR I.D.

TAPE - D11738

280N3373-10202 1

CONNECTOR I.D.

TAPE - D00596

280N3373-10203 1

BACC47CN1S 3 CONTACT, PIN

CONTACT, SOCKETBACC47DJ1 5

CONTACT, SOCKETBACC47DJ2 3

CONTACT, SOCKETBACC47DJ3 3

BACS16X1A 1 RELAY SOCKET

(a) There are more parts than are necessary.

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Group 5:

KIT 280N3373-103

New Part Number Qty Name Notes

New cut

and coded wires

for wire

bundle

W1260

280N3373-103W 1 WIRE LIST

CONNECTOR I.D.

TAPE - D41850J

280N3373-10201 1

CONNECTOR I.D.

TAPE - D11738

280N3373-10202 1

CONNECTOR I.D.

TAPE - D00596

280N3373-10203 1

BACC47CN1S 3 CONTACT, PIN

CONTACT, SOCKETBACC47DJ1 5

CONTACT, SOCKETBACC47DJ2 3

BACS16X1A 1 RELAY SOCKET

KIT 280N3373-104

New Part Number Qty Name Notes

New cut

and coded wires

for wire

bundle

W2078

280N3373-104W 1 WIRE LIST

CONNECTOR I.D.

TAPE - D03508

280N3373-10101 1

CONNECTOR I.D.

TAPE - D41850P

280N3373-10102 1

SPLICE I.D.

SLEEVE - SM28

280N3373-10401 1

CONTACT, SOCKETBACC47CP1S 4

CLAMP ASSEMBLYBACC49A2 2

BACM15C3D 1 TERMINAL BLOCK

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KIT 280N3373-104

New Part Number Qty Name Notes

BACS18AR1 2 SPACER

SPLICE SEALED

CRIMP

D-436-36 2

CONTACT, PIN,

CRIMP REMOVABLE, PER MIL-C39029/11

M39029/11-145 5

2. Parts and Materials Supplied by the Operator

None.

3. Parts Modified and Reidentified

None.

4. Parts Removed and Not Replaced

None.

D. Parts Necessary to Change Spares

None.

E. Special Tooling - Price and Availability

None.

F. Special Tooling Necessary to do this Service Bulletin

No special tools or equipment are necessary to do the change in this service bulletin. But, maintenance

and overhaul tools in the manuals given in Paragraph 1.J., References, can be necessary. Examine

operator tool supply to make sure all necessary tools are available.

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BLANK PAGE
3. ACCOMPLISHMENT INSTRUCTIONS

A. GENERAL INFORMATION

CAUTION: KEEP THE WORK AREA, WIRES AND ELECTRICAL BUNDLES CLEAN OF METAL

PARTICLES OR CONTAMINATION WHEN YOU USE TOOLS. UNWANTED MATERIAL,

METAL PARTICLES OR CONTAMINATION CAUGHT IN WIRE BUNDLES CAN CAUSE

DAMAGE TO THE BUNDLES. DAMAGED WIRE BUNDLES CAN CAUSE SPARKS OR

OTHER ELECTRICAL DAMAGE.

NOTE: 1. Manual titles are referred to by acronyms. Refer to Paragraph 1.J., References, for

definition of the acronyms.

2. Obey all of the warnings and cautions given in the specified manual sections.

3. Refer to the SWPM 20-10-11 and SWPM 20-10-12 for the wire installation procedures,

and SWPM 20-10-19 for the wire separation requirements, as accepted procedures.

4. These work instructions refer to procedures included in other Boeing documents.

When the words "refer to" are used and the operator has an accepted alternative

procedure, the accepted alternative procedure can be used. When the words "in

accordance with" are included in the instruction, the procedure in the Boeing document

must be used.

5. If it is necessary to remove more parts for access, you can remove those parts. If

you can get access without removing identified parts, it is not necessary to remove

all of the identified parts. Jacking and shoring limitations must be observed.

B. WORK INSTRUCTIONS

1. Part 1 - Open Access:

a. In the forward cargo compartment, get access to the P36 miscellaneous electronics equipment

panel assembly and wiring by opening the forward cargo compartment door. Refer to 757

AMM 52-34-00 as an accepted procedure.

b. Remove electrical power from the airplane. Refer to 757 AMM 24-22-00 as an accepted

procedure.

c. In the flight compartment:

(1) Open the right forward ceiling lining to get access to the wire bundles.

(2) Open the P11 circuit breaker panel to get access the wire bundles and terminal track

TB111.

(3) On the P5 panel, remove the Standby Power Control Panel M10062 . Refer to 757 AMM

24-33-04 as an accepted procedure.

(4) Remove the P26 Lighting Equipment Panel to access wire bundles outboard of P6 and

P61 panels (if necessary)

d. In the Passenger Cabin:

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(1) If necessary to access wire bundle outboard of the P61 panel and P6 circuit breaker

panel, remove the G1A galley. Refer to 757 AMM 25-31-01 as an accepted procedure.

(2) Between Stations 460-540 right side, remove items below to access wire bundle located

above the E4 equipment rack drip shield:

(a) Remove and keep the passenger seats. Refer to 757 AMM 25-25-01 as an accepted

procedure.

(b) Remove and keep the floor carpets. Refer to 757 AMM 25-27-01 as an accepted

procedure

(c) Remove and keep the outboard floor panel(s). Refer to 757 AMM 53-01-01 as an

accepted procedure.

(d) As an alternative to the items open access steps above, operators can remove and

keep the E4 equipment rack drip shield to access the wire bundle from below the

floor.

e. End Part 1.

2. If necessary, remove electrical power from the airplane. Refer to 757 AMM 24-22-00 as an accepted

procedure.

3. Part 2 - Rework Instructions:

a. Group 1:

From the P5 overhead panel and the P36 disconnect panel, do the wiring change for wire

bundle W2078 in accordance with FIGURE 1 and FIGURE 2.

b. Group 2:

From the P5 overhead panel and the P36 disconnect panel, do the wiring change for wire

bundle W2078 in accordance with FIGURE 1 and FIGURE 3.

c. Group 3:

From the P5 overhead panel and the P36 disconnect panel, do the wiring change for wire

bundle W2078 in accordance with FIGURE 1 and FIGURE 4.

d. Group 4:

From the P5 overhead panel and the P36 disconnect panel, do the wiring change for wire

bundle W2078 in accordance with FIGURE 1 and FIGURE 5.

e. Group 5, 8:

From the P5 overhead panel and the P36 disconnect panel, do the wiring change for wire

bundle W2078 in accordance with FIGURE 1 and FIGURE 8.

f. Group 6:

From the P5 overhead panel and the P36 disconnect panel, do the wiring change for wire

bundle W2078 in accordance with FIGURE 1 and FIGURE 6.

g. Group 7:

From the P5 overhead panel and the P36 disconnect panel, do the wiring change for wire

bundle W2078 in accordance with FIGURE 1 and FIGURE 7.

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h. Group 1, 8:

In the P36 miscellaneous electronics equipment panel, do the wiring change for wire bundle

W1260 in accordance with FIGURE 9 and FIGURE 10.

i. Group 2, 6:

In the P36 miscellaneous electronics equipment panel, do the wiring change for wire bundle

W1260 in accordance with FIGURE 9 and FIGURE 11.

j. Group 3:

In the P36 miscellaneous electronics equipment panel, do the wiring change for wire bundle

W1260 in accordance with FIGURE 9 and FIGURE 12.

k. Group 4, 7:

In the P36 miscellaneous electronics equipment panel, do the wiring change for wire bundle

W1260 in accordance with FIGURE 9 and FIGURE 13.

l. Group 5:

In the P36 miscellaneous electronics equipment panel, do the wiring change for wire bundle

W1260 in accordance with FIGURE 9 and FIGURE 14.

m. On the P36 miscellaneous electronics equipment panel, install a new relay in accordance with

FIGURE 15 .

n. End Part 2.

4. Part 3 - Close Access

a. In the flight compartment:

(1) Install the right forward ceiling lining that were removed to get access to the wire bundles.

(2) Close the P11 circuit breaker panel.

(3) On the P5 panel, install the Standby Power Control Panel M10062 . Refer to 757 AMM

24-33-04 as an accepted procedure.

(4) If removed, install the P26 Lighting Equipment Panel.

b. In the passenger cabin:

(1) If removed, install the G1A galley. Refer to 757 AMM 25-31-01 as an accepted procedure.

(2) In the passenger cabin between Stations 460-540 right side:

(a) If removed, install kept outboard floor panel(s). Refer to 757 AMM 53-01-01 as an

accepted procedure.

(b) If removed, install kept floor carpets. Refer to 757 AMM 25-27-01 as an accepted

procedure.

(c) If removed, install kept passenger seats. Refer to 757 AMM 25-25-01 as an accepted

procedure.

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(d) If removed, install kept drip shield located above the E4 equipment rack.

c. Apply electrical power to the airplane. Refer to 757 AMM 24-22-00 as an accepted procedure.

d. If the P26 Lighting Equipment Panel was removed and installed, perform the Master Dim and

Test - Adjustment Test. Refer to 757 AMM 33-16-00 as an approved procedure.

e. End Part 3.

5. If necessary, apply electrical power to the airplane. Refer to 757 AMM 24-22-00 as an accepted

procedure.

6. Part 4 - Test

a. Do the steps that follow to test the battery charger:

(1) On the P11 overhead circuit breaker panel, make sure the six EICAS circuit breakers are

closed.

Location Circuit Breaker Description

P11-3 C04078 EICAS CMPTR L

P11-3 C04081 EICAS UPPER IND

P11-4 C04079 EICAS CMPTR R

P11-4 C04082 EICAS LOWER IND

P11-4 C04189 EICAS DISPLAY SW

P11-4 C04094 EICAS PILOTS DSP

(2) On the P61 right side panel, push the ELEC HYD switch on the EICAS MAINT panel.

(3) On the P5 pilots' overhead panel, push the BAT switch to the ON position.

(4) On the P5 pilots' overhead panel, turn the STBY POWER switch to the BAT position.

(5) Make sure the value shown below the STBY/BAT on the bottom of EICAS display for

DC-V is 24 to 32 volts.

(6) Turn the STBY POWER switch to the AUTO position and make sure these values show

below STBY/BAT on the bottom EICAS display.

NOTE: These values will occur quickly. Make sure you monitor the bottom EICAS display

carefully.

(a) DC-A is 33-43 amps.

(b) DC-V increases to 28-36 volts dc then decreases to 24 to 32 volts dc.

(7) Make sure the DC-A value that shows below STBY/BAT on the bottom EICAS display is

positive.

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BOEING SERVICE BULLETIN 757-24-0132
(8) On the P5 pilots' overhead panel, turn the STBY POWER switch to the BAT position.

(9) Make sure the MAIN BAT DISCH LT (P5) is illuminated.

(10) At the main landing gear, install switch de-actuators on the proximity sensor S10060,

SYS 1 RIGHT MAIN GEAR TRUCK NOT TILT, and S10062, SYS 1 LEFT MAIN GEAR

TRUCK NOT TILT to place the airplane in airmode.

(11) Make sure the MAIN BAT DISCH LT (P5) is not illuminated.

(12) At the main landing gear, remove the switch de-actuators on the proximity sensor S10060,

SYS 1 RIGHT MAIN GEAR TRUCK NOT TILT, and S10062, SYS 1 LEFT MAIN GEAR

TRUCK NOT TILT.

b. Do the Operational Test for the Pitot Probe Anti-Icing System. Refer to 757 AMM 30-31-00

as an accepted procedure.

c. End Part 4.

7. Put the airplane back to a serviceable condition.

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35 of 76

BOEING SERVICE BULLETIN 757-24-0132
FIGURE 1: WIRE ROUTING FOR WIRE BUNDLE W2078

(SHEET 1 OF 6)

Export Controlled ECCN: 9E991 - BOEING

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36 of 76

BOEING SERVICE BULLETIN 757-24-0132
FIGURE 1: WIRE ROUTING FOR WIRE BUNDLE W2078

(SHEET 2 OF 6)

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished

Work - See page 1 for details.

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Revision 1 June 19, 2012 757-24-0132

37 of 76

BOEING SERVICE BULLETIN 757-24-0132
FIGURE 1: WIRE ROUTING FOR WIRE BUNDLE W2078

(SHEET 3 OF 6)

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished

Work - See page 1 for details.

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Revision 1 June 19, 2012 757-24-0132

38 of 76

BOEING SERVICE BULLETIN 757-24-0132
FIGURE 1: WIRE ROUTING FOR WIRE BUNDLE W2078

(SHEET 4 OF 6)

Export Controlled ECCN: 9E991 - BOEING

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39 of 76

BOEING SERVICE BULLETIN 757-24-0132
FIGURE 1: WIRE ROUTING FOR WIRE BUNDLE W2078

(SHEET 5 OF 6)

Export Controlled ECCN: 9E991 - BOEING

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40 of 76

BOEING SERVICE BULLETIN 757-24-0132
The parts shown in the table below are provided as extra parts for this figure.

Name Identification Qty More Data

Use quantity as necessary when

making changes to wire bundle

W2078. Refer to SWPM 20-10-11

and SWPM 20-10-19 as accepted

procedures.

LACING TAPE - BLUE 280N3373-2002 1

FIGURE 1: WIRE ROUTING FOR WIRE BUNDLE W2078

(SHEET 6 OF 6)

Export Controlled ECCN: 9E991 - BOEING

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41 of 76

BOEING SERVICE BULLETIN 757-24-0132
This Figure applies only to: Group 1.

FIGURE 2: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 1 OF 3)

Export Controlled ECCN: 9E991 - BOEING

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42 of 76

BOEING SERVICE BULLETIN 757-24-0132
REFERENCE: 757 WDM 24-31-11

The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

1 WIRE BMS13-48T10C01G022 1

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

2 WIRE BMS13-48T10C01G020 2

Refer to SWPM 20-61-11 as an

accepted procedure.

3 CONTACT, SOCKET BACC47CP1S 3

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10101 1

D03508

4

If necessary, install burndy block

in terminal track TB111 Positions

22 and 23. Refer to SWPM 20-90-

11 as an accepted procedure.

5 TERMINAL BLOCK BACM15C3D 1

If necessary, install end caps to

secure new burndy block in track.

Refer to SWPM 20-90-11 as an

accepted procedure.

CLAMP ASSEMBLY BACC49A2 2

If necessary, install spacers to secure burdy block in track. Refer to

SWPM 20-90-11 as an accepted

procedure.

SPACER BACS18AR1 2

If TB111 Positions 22 and 23 are

not labled, mark "22" and "23" in

12 point character with black

marker on track. Locate positions

22 and 23 using existing terminal

track marker as a guide. Refer to

SOPM 20-50-10 as an accepted

procedure to write numbers on

track. As an alternative to writing

on track, operators can install an

equivalent ID label or marker locating position 22 and 23. Refer to

SOPM 20-50-05 as an accepted

procedure to install marker on

track.

- - -

FIGURE 2: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 2 OF 3)

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished

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Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

43 of 76

BOEING SERVICE BULLETIN 757-24-0132
Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11and SWPM 20-10-12 as an accepted procedures.6 WIRE BMS13-48T10C01G022 1

Refer to SWPM 20-90-11 as an

accepted procedure.

CONTACT, PIN, CRIMP M39029/11-145 4

REMOVABLE, PER MIL-C39029/11

7

Refer to SWPM 20-30-12 as an

accepted procedure. Splice

M81824/1-1 is equivalent part

number to D-436-36.

8 SPLICE SEALED CRIMP D-436-36 1

Refer to SWPM 20-10-11 as an

accepted procedure.

SPLICE I.D. SLEEVE - 280N3373-10401 1

SM28

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10102 1

D41850P

9

FIGURE 2: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 3 OF 3)

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished

Work - See page 1 for details.

Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

44 of 76

BOEING SERVICE BULLETIN 757-24-0132
This Figure applies only to: Group 2.

FIGURE 3: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 1 OF 3)

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished

Work - See page 1 for details.

Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

45 of 76

BOEING SERVICE BULLETIN 757-24-0132
REFERENCE: 757 WDM 24-31-11

The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

1 WIRE BMS13-48T10C01G022 1

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

2 WIRE BMS13-48T10C01G020 2

Refer to SWPM 20-61-11 as an

accepted procedure.

3 CONTACT, SOCKET BACC47CP1S 3

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10101 1

D03508

4

If necessary, install burndy block

in terminal track TB111 Position

22 and 23. Refer to SWPM 20-90-

11 as an accepted procedure.

5 TERMINAL BLOCK BACM15C3D 1

If necessary, install end caps to

secure new burndy block in track.

Refer to SWPM 20-90-11 as an

accepted procedure.

CLAMP ASSEMBLY BACC49A2 2

If necessary, install spacers to secure burdy block in track. Refer to

SWPM 20-90-11 as an accepted

procedure.

SPACER BACS18AR1 2

If TB111 Positions 22 and 23 are

not labled, mark "22" and "23" in

12 point character with black

marker on track. Locate positions

22 and 23 using existing terminal

track marker as a guide. Refer to

SOPM 20-50-10 as an accepted

procedure to write numbers on

track. As an alternative to writing

on track, operators can install an

equivalent ID label or marker locating position 22 and 23. Refer to

SOPM 20-50-05 as an accepted

procedure to install marker on

track.

- - -

FIGURE 3: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 2 OF 3)

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished

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Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

46 of 76

BOEING SERVICE BULLETIN 757-24-0132
Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as an accepted

procedures.

6 WIRE BMS13-48T10C01G022 1

Refer to SWPM 20-90-11 as an

accepted procedure.

CONTACT, PIN, CRIMP M39029/11-145 4

REMOVABLE, PER MIL-C39029/11

7

Refer to SWPM 20-30-12 as an

accepted procedure. Splice

M81824/1-1 is equivalent part

number to D-436-36.

8 SPLICE SEALED CRIMP D-436-36 1

SPLICE I.D. SLEEVE - 280N3373-10401 1

SM28

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10102 1

D41850P

9

FIGURE 3: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 3 OF 3)

Export Controlled ECCN: 9E991 - BOEING

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Work - See page 1 for details.

Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

47 of 76

BOEING SERVICE BULLETIN 757-24-0132
This Figure applies only to: Group 3.

FIGURE 4: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 1 OF 3)

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished

Work - See page 1 for details.

Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

48 of 76

BOEING SERVICE BULLETIN 757-24-0132
REFERENCE: 757 WDM 24-31-11

The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

1 WIRE BMS13-48T10C01G022 1

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

2 WIRE BMS13-48T10C01G020 2

Refer to SWPM 20-61-11 as an

accepted procedure.

3 CONTACT, SOCKET BACC47CP1S 3

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10101 1

D03508

4

If necessary, install burndy block

in terminal track TB111 Position

22 and 23. Refer to SWPM 20-90-

11 as an accepted procedure.

5 TERMINAL BLOCK BACM15C3D 1

If necessary, install end caps to

secure new burndy block in track.

Refer to SWPM 20-90-11 as an

accepted procedure.

CLAMP ASSEMBLY BACC49A2 2

If necessary, install spacers to secure burdy block in track. Refer to

SWPM 20-90-11 as an accepted

procedure.

SPACER BACS18AR1 2

If TB111 Positions 22 and 23 are

not labled, mark "22" and "23" in

12 point character with black

marker on track. Locate positions

22 and 23 using existing terminal

track marker as a guide. Refer to

SOPM 20-50-10 as an accepted

procedure to write numbers on

track. As an alternative to writing

on track, operators can install an

equivalent ID label or marker locating position 22 and 23. Refer to

SOPM 20-50-05 as an accepted

procedure to install marker on

track.

- - -

FIGURE 4: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 2 OF 3)

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished

Work - See page 1 for details.

Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

49 of 76

BOEING SERVICE BULLETIN 757-24-0132
Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as an accepted

procedures.

6 WIRE BMS13-48T10C01G022 1

Refer to SWPM 20-90-11 as an

accepted procedure.

CONTACT, PIN, CRIMP M39029/11-145 4

REMOVABLE, PER MIL-C39029/11

7

Refer to SWPM 20-30-12 as an

accepted procedure. Splice

M81824/1-1 is equivalent part

number to D-436-36.

8 SPLICE SEALED CRIMP D-436-36 1

Refer to SWPM 20-10-11 as an

accepted procedure.

SPLICE I.D. SLEEVE - 280N3373-10401 1

SM28

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10102 1

D41850P

9

FIGURE 4: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 3 OF 3)

Export Controlled ECCN: 9E991 - BOEING

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Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

50 of 76

BOEING SERVICE BULLETIN 757-24-0132
This Figure applies only to: Group 4.

FIGURE 5: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 1 OF 3)

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished

Work - See page 1 for details.

Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

51 of 76

BOEING SERVICE BULLETIN 757-24-0132
REFERENCE: 757 WDM 24-31-11

The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

1 WIRE BMS13-48T10C01G022 1

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

2 WIRE BMS13-48T10C01G020 2

Refer to SWPM 20-61-11 as an

accepted procedure.

3 CONTACT, SOCKET BACC47CP1S 3

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10101 1

D03508

4

If necessary, install burndy block

in terminal track TB111 Position

22 and 23. Refer to SWPM 20-90-

11 as an accepted procedure.

5 TERMINAL BLOCK BACM15C3D 1

If necessary, install end caps to

secure new burndy block in track.

Refer to SWPM 20-90-11 as an

accepted procedure.

CLAMP ASSEMBLY BACC49A2 2

If necessary, install spacers to secure burdy block in track. Refer to

SWPM 20-90-11 as an accepted

procedure.

SPACER BACS18AR1 2

If TB111 Positions 22 and 23 are

not labled, mark "22" and "23" in

12 point character with black

marker on track. Locate positions

22 and 23 using existing terminal

track marker as a guide. Refer to

SOPM 20-50-10 as an accepted

procedure to write numbers on

track. As an alternative to writing

on track, operators can install an

equivalent ID label or marker locating position 22 and 23. Refer to

SOPM 20-50-05 as an accepted

procedure to install marker on

track.

- - -

FIGURE 5: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 2 OF 3)

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished

Work - See page 1 for details.

Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

52 of 76

BOEING SERVICE BULLETIN 757-24-0132
Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as an accepted

procedures.

6 WIRE BMS13-48T10C01G022 1

Refer to SWPM 20-90-11 as an

accepted procedure.

CONTACT, PIN, CRIMP M39029/11-145 4

REMOVABLE, PER MIL-C39029/11

7

Refer to SWPM 20-30-12 as an

accepted procedure. Splice

M81824/1-1 is equivalent part

number to D-436-36.

8 SPLICE SEALED CRIMP D-436-36 1

Refer to SWPM 20-10-11 as an

accepted procedure.

SPLICE I.D. SLEEVE - 280N3373-10401 1

SM28

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10102 1

D41850P

9

FIGURE 5: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 3 OF 3)

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished

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Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

53 of 76

BOEING SERVICE BULLETIN 757-24-0132
This Figure applies only to: Group 6.

FIGURE 6: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 1 OF 3)

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished

Work - See page 1 for details.

Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

54 of 76

BOEING SERVICE BULLETIN 757-24-0132
REFERENCE: 757 WDM 24-31-11

The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

1 WIRE BMS13-48T10C01G022 1

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

2 WIRE BMS13-48T10C01G020 2

Refer to SWPM 20-61-11 as an

accepted procedure.

3 CONTACT, SOCKET BACC47CP1S 3

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10101 1

D03508

4

If necessary, install burndy block

in terminal track TB111 Position

12 and 13. Refer to SWPM 20-90-

11 as an accepted procedure.

5 TERMINAL BLOCK BACM15C3D 1

If necessary, install end caps to

secure new burndy block in track.

Refer to SWPM 20-90-11 as an

accepted procedure.

CLAMP ASSEMBLY BACC49A2 2

If necessary, install spacers to secure burdy block in track. Refer to

SWPM 20-90-11 as an accepted

procedure.

SPACER BACS18AR1 2

If TB111 Positions 12 and 13 are

not labled, mark "12" and "13" in

12 point character with black

marker on track. Locate positions

12 and 13 using existing terminal

track marker as a guide. Refer to

SOPM 20-50-10 as an accepted

procedure to write numbers on

track. As an alternative to writing

on track, operators can install an

equivalent ID label or marker locating position 12 and 13. Refer to

SOPM 20-50-05 as an accepted

procedure to install marker on

track.

- - -

FIGURE 6: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 2 OF 3)

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished

Work - See page 1 for details.

Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

55 of 76

BOEING SERVICE BULLETIN 757-24-0132
Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as an accepted

procedures.

6 WIRE BMS13-48T10C01G022 1

Refer to SWPM 20-90-11 as an

accepted procedure.

CONTACT, PIN, CRIMP M39029/11-145 4

REMOVABLE, PER MIL-C39029/11

7

Refer to SWPM 20-30-12 as an

accepted procedure. Splice

M81824/1-1 is equivalent part

number to D-436-36.

8 SPLICE SEALED CRIMP D-436-36 1

Refer to SWPM 20-10-11 as an

accepted procedure.

SPLICE I.D. SLEEVE - 280N3373-10401 1

SM28

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10102 1

D41850P

9

FIGURE 6: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 3 OF 3)

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished

Work - See page 1 for details.

Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

56 of 76

BOEING SERVICE BULLETIN 757-24-0132
This Figure applies only to: Group 7.

FIGURE 7: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 1 OF 3)

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished

Work - See page 1 for details.

Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

57 of 76

BOEING SERVICE BULLETIN 757-24-0132
REFERENCE: 757 WDM 24-31-11

The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

1 WIRE BMS13-48T10C01G022 1

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

2 WIRE BMS13-48T10C01G020 2

Refer to SWPM 20-61-11 as an

accepted procedure.

3 CONTACT, SOCKET BACC47CP1S 3

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10101 1

D03508

4

If necessary, install burndy block

in terminal track TB111 Position

12 and 13. Refer to SWPM 20-90-

11 as an accepted procedure.

5 TERMINAL BLOCK BACM15C3D 1

If necessary, install end caps to

secure new burndy block in track.

Refer to SWPM 20-90-11 as an

accepted procedure.

CLAMP ASSEMBLY BACC49A2 2

If necessary, install spacers to secure burdy block in track. Refer to

SWPM 20-90-11 as an accepted

procedure.

SPACER BACS18AR1 2

If TB111 Positions 12 and 13 are

not labled, mark "12" and "13" in

12 point character with black

marker on track. Locate positions

12 and 13 using existing terminal

track marker as a guide. Refer to

SOPM 20-50-10 as an accepted

procedure to write numbers on

track. As an alternative to writing

on track, operators can install an

equivalent ID label or marker locating position 12 and 13. Refer to

SOPM 20-50-05 as an accepted

procedure to install marker on

track.

- - -

FIGURE 7: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 2 OF 3)

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished

Work - See page 1 for details.

Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

58 of 76

BOEING SERVICE BULLETIN 757-24-0132
Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as an accepted

procedures.

6 WIRE BMS13-48T10C01G022 1

Refer to SWPM 20-90-11 as an

accepted procedure.

CONTACT, PIN, CRIMP M39029/11-145 4

REMOVABLE, PER MIL-C39029/11

7

Refer to SWPM 20-30-12 as an

accepted procedure. Splice

M81824/1-1 is equivalent part

number to D-436-36.

8 SPLICE SEALED CRIMP D-436-36 1

Refer to SWPM 20-10-11 as an

accepted procedure.

SPLICE I.D. SLEEVE - 280N3373-10401 1

SM28

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10102 1

D41850P

9

FIGURE 7: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 3 OF 3)

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59 of 76

BOEING SERVICE BULLETIN 757-24-0132
This Figure applies only to: Group 5, 8.

FIGURE 8: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 1 OF 3)

Export Controlled ECCN: 9E991 - BOEING

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60 of 76

BOEING SERVICE BULLETIN 757-24-0132
REFERENCE: 757 WDM 24-31-11

The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

1 WIRE BMS13-48T10C01G022 1

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

2 WIRE BMS13-48T10C01G020 2

Refer to SWPM 20-61-11 as an

accepted procedure.

3 CONTACT, SOCKET BACC47CP1S 3

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10101 1

D03508

4

If necessary, install burndy block

in terminal track TB111 Position

12 and 13. Refer to SWPM 20-90-

11 as an accepted procedure.

5 TERMINAL BLOCK BACM15C3D 1

If necessary, install end caps to

secure new burndy block in track.

Refer to SWPM 20-90-11 as an

accepted procedure.

CLAMP ASSEMBLY BACC49A2 2

If necessary, install spacers to secure burdy block in track. Refer to

SWPM 20-90-11 as an accepted

procedure.

SPACER BACS18AR1 2

If TB111 Positions 12 and 13 are

not labled, mark "12" and "13" in

12 point character with black

marker on track. Locate positions

12 and 13 using existing terminal

track marker as a guide. Refer to

SOPM 20-50-10 as an accepted

procedure to write numbers on

track. As an alternative to writing

on track, operators can install an

equivalent ID label or marker locating position 12 and 13. Refer to

SOPM 20-50-05 as an accepted

procedure to install marker on

track.

- - -

FIGURE 8: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 2 OF 3)

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61 of 76

BOEING SERVICE BULLETIN 757-24-0132
Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as an accepted

procedures.

6 WIRE BMS13-48T10C01G022 1

Refer to SWPM 20-90-11 as an

accepted procedure.

CONTACT, PIN, CRIMP M39029/11-145 4

REMOVABLE, PER MIL-C39029/11

7

Refer to SWPM 20-30-12 as an

accepted procedure. Splice

M81824/1-1 is equivalent part

number to D-436-36.

8 SPLICE SEALED CRIMP D-436-36 1

Refer to SWPM 20-10-11 as an

accepted procedure.

SPLICE I.D. SLEEVE - 280N3373-10401 1

SM28

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10102 1

D41850P

9

FIGURE 8: WIRING CHANGE FOR WIRE BUNDLE W2078

(SHEET 3 OF 3)

Export Controlled ECCN: 9E991 - BOEING

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62 of 76

BOEING SERVICE BULLETIN 757-24-0132
FIGURE 9: WIRE ROUTING FOR WIRE BUNDLE W1260

(SHEET 1 OF 2)

Export Controlled ECCN: 9E991 - BOEING

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63 of 76

BOEING SERVICE BULLETIN 757-24-0132
The parts shown in the table below are provided as extra parts for this figure.

Name Identification Qty More Data

Use quantity as necessary when

making changes to wire bundle

W1260. Refer to SWPM 20-10-11

and SWPM 20-10-19 as accepted

procedures.

LACING TAPE - 280N3373-2001 1

WHITE

FIGURE 9: WIRE ROUTING FOR WIRE BUNDLE W1260

(SHEET 2 OF 2)

Export Controlled ECCN: 9E991 - BOEING

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64 of 76

BOEING SERVICE BULLETIN 757-24-0132
This Figure applies only to: Group 1, 8.

REFERENCE: 757 WDM 24-31-11, 757 WDM 32-09-11

The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

1 WIRE BMS13-48T10C01G022 4

Use the applicable size as necessary. Refer to SWPM 20-81-12 as

an accepted procedure.

2 CONTACT, SOCKET BACC47DJ3 2

Use the applicable size as necessary. Refer to SWPM 20-81-12 as

an accepted procedure.

CONTACT, SOCKET BACC47DJ2 2

Refer to SWPM 20-81-12 as an

accepted procedure.

3 CONTACT, SOCKET BACC47DJ1 4

FIGURE 10: WIRING CHANGE FOR WIRE BUNDLE W1260

(SHEET 1 OF 2)

Export Controlled ECCN: 9E991 - BOEING

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65 of 76

BOEING SERVICE BULLETIN 757-24-0132
Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-61-11 as an

accepted procedure.

4 CONTACT, PIN BACC47CN1S 2

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10203 1

D00596

5

Refer to SWPM 20-81-22 as an

accepted procedure. (a)

6 RELAY SOCKET BACS16X1A 1

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10202 1

D11738

7

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10201 1

D41850J

8

9 - - - (b)

(a) If location is used, the new relay can be installed anywhere on the same row.

(b) Wire at connector D569 Pins X1 and X2 have multiple configurations. Contacts provided in kit allow operators to double or triple stake existing wire(s) with new added wire as required.

FIGURE 10: WIRING CHANGE FOR WIRE BUNDLE W1260

(SHEET 2 OF 2)

Export Controlled ECCN: 9E991 - BOEING

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Revision 1 June 19, 2012 757-24-0132

66 of 76

BOEING SERVICE BULLETIN 757-24-0132
This Figure applies only to: Group 2, 6.

REFERENCE: 757 WDM 24-31-11, 757 WDM 32-09-11

The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

1 WIRE BMS13-48T10C01G022 4

Use the applicable size as necessary. Refer to SWPM 20-81-12 as

an accepted procedure.

2 CONTACT, SOCKET BACC47DJ3 2

As necessary. Refer to SWPM 20-

81-12 as an accepted procedure.

CONTACT, SOCKET BACC47DJ2 2

Refer to SWPM 20-81-12 as an

accepted procedure.

3 CONTACT, SOCKET BACC47DJ1 4

Refer to SWPM 20-61-11 as an

accepted procedure.

4 CONTACT, PIN BACC47CN1S 2

FIGURE 11: WIRING CHANGE FOR WIRE BUNDLE W1260

(SHEET 1 OF 2)

Export Controlled ECCN: 9E991 - BOEING

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Work - See page 1 for details.

Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

67 of 76

BOEING SERVICE BULLETIN 757-24-0132
Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10203 1

D00596

5

Refer to SWPM 20-81-22 as an

accepted procedure. (a)

6 RELAY SOCKET BACS16X1A 1

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10202 1

D11738

7

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10201 1

D41850J

8

9 - - - (b)

(a) If location is used, the new relay can be installed anywhere on the same row.

(b) Wire at connector D569 Pins X1 and X2 have multiple configurations. Contacts provided in kit allow operators to double or triple stake existing wire(s) with new added wire as required.

FIGURE 11: WIRING CHANGE FOR WIRE BUNDLE W1260

(SHEET 2 OF 2)

Export Controlled ECCN: 9E991 - BOEING

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68 of 76

BOEING SERVICE BULLETIN 757-24-0132
This Figure applies only to: Group 3.

REFERENCE: 757 WDM 24-31-11, 757 WDM 32-09-11

The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

1 WIRE BMS13-48T10C01G022 4

Use the applicable size as necessary. Refer to SWPM 20-81-12 as

an accepted procedure.

2 CONTACT, SOCKET BACC47DJ3 2

Use the applicable size as necessary. Refer to SWPM 20-81-12 as

an accepted procedure.

CONTACT, SOCKET BACC47DJ2 2

Refer to SWPM 20-81-12 as an

accepted procedure.

3 CONTACT, SOCKET BACC47DJ1 4

FIGURE 12: WIRING CHANGE FOR WIRE BUNDLE W1260

(SHEET 1 OF 2)

Export Controlled ECCN: 9E991 - BOEING

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69 of 76

BOEING SERVICE BULLETIN 757-24-0132
Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-61-11 as an

accepted procedure.

4 CONTACT, PIN BACC47CN1S 2

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10203 1

D00596

5

Refer to SWPM 20-81-22 as an

accepted procedure. (a)

6 RELAY SOCKET BACS16X1A 1

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10202 1

D11738

7

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10201 1

D41850J

8

9 - - - (b)

(a) If location is used, the new relay can be installed anywhere on the same row.

(b) Wire at connector D569 Pins X1 and X2 have multiple configurations. Contacts provided in kit allow operators to double or triple stake existing wire(s) with new added wire as required.

FIGURE 12: WIRING CHANGE FOR WIRE BUNDLE W1260

(SHEET 2 OF 2)

Export Controlled ECCN: 9E991 - BOEING

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Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

70 of 76

BOEING SERVICE BULLETIN 757-24-0132
This Figure applies only to: Group 4, 7.

REFERENCE: 757 WDM 24-31-11, 757 WDM 32-09-11

The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

1 WIRE BMS13-48T10C01G022 4

Use the applicable size as necessary. Refer to SWPM 20-81-12 as

an accepted procedure.

2 CONTACT, SOCKET BACC47DJ3 2

Use the applicable size as necessary. Refer to SWPM 20-81-12 as

an accepted procedure.

CONTACT, SOCKET BACC47DJ2 2

Refer to SWPM 20-81-12 as an

accepted procedure.

3 CONTACT, SOCKET BACC47DJ1 4

FIGURE 13: WIRING CHANGE FOR WIRE BUNDLE W1260

(SHEET 1 OF 2)

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished

Work - See page 1 for details.

Original Issue: April 14, 2011

Revision 1 June 19, 2012 757-24-0132

71 of 76

BOEING SERVICE BULLETIN 757-24-0132
Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-61-11 as an

accepted procedure.

4 CONTACT, PIN BACC47CN1S 2

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10203 1

D00596

5

Refer to SWPM 20-81-22 as an

accepted procedure. (a)

6 RELAY SOCKET BACS16X1A 1

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10202 1

D11738

7

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10201 1

D41850J

8

9 - - - (b)

(a) If location is used, the new relay can be installed anywhere on the same row.

(b) Wire at connector D569 Pins X1 and X2 have multiple configurations. Contacts provided in kit allow operators to double or triple stake existing wire(s) with new added wire as required.

FIGURE 13: WIRING CHANGE FOR WIRE BUNDLE W1260

(SHEET 2 OF 2)

Export Controlled ECCN: 9E991 - BOEING

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Revision 1 June 19, 2012 757-24-0132

72 of 76

BOEING SERVICE BULLETIN 757-24-0132
This Figure applies only to: Group 5.

REFERENCE: 757 WDM 24-31-11, 757 WDM 32-09-11

The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-10-11 and

SWPM 20-10-12 as accepted procedures.

1 WIRE BMS13-48T10C01G022 4

Refer to SWPM 20-81-12 as an

accepted procedure.

2 CONTACT, SOCKET BACC47DJ2 2

Refer to SWPM 20-81-12 as an

accepted procedure.

3 CONTACT, SOCKET BACC47DJ1 4

Refer to SWPM 20-61-11 as an

accepted procedure.

4 CONTACT, PIN BACC47CN1S 2

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10203 1

D00596

5

FIGURE 14: WIRING CHANGE FOR WIRE BUNDLE W1260

(SHEET 1 OF 2)

Export Controlled ECCN: 9E991 - BOEING

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73 of 76

BOEING SERVICE BULLETIN 757-24-0132
Name Identification Qty More Data

Flag

Note

Refer to SWPM 20-81-22 as an

accepted procedure. (a)

6 RELAY SOCKET BACS16X1A 1

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10202 1

D11738

7

Refer to SWPM 20-10-11 as an

accepted procedure.

CONNECTOR I.D. TAPE - 280N3373-10201 1

D41850J

8

9 - - - (b)

(a) If location is used, the new relay can be installed anywhere on the same row.

(b) Wire at connector D569 Pins X1 and X2 have multiple configurations. Contacts provided in kit allow operators to double or triple stake existing wire(s) with new added wire as required.

FIGURE 14: WIRING CHANGE FOR WIRE BUNDLE W1260

(SHEET 2 OF 2)

Export Controlled ECCN: 9E991 - BOEING

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BOEING SERVICE BULLETIN 757-24-0132
FIGURE 15: INSTALLATION OF RELAY ON P36 PANEL

(SHEET 1 OF 2)

Export Controlled ECCN: 9E991 - BOEING

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75 of 76

BOEING SERVICE BULLETIN 757-24-0132
The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY

numbers shown below are the number of parts necessary for one airplane.

STEP TASK NAME IDENTIFICATION QTY MORE DATA

1 Install (New) RELAY BACR13CF2AB 1 (a)

Refer to SOPM 20-

50-05 as an accepted procedure.

2 Install (New) BRADY LABEL 012N0032-2 1

(a) If location is used, the new relay can be installed anywhere on the same row.

FIGURE 15: INSTALLATION OF RELAY ON P36 PANEL

(SHEET 2 OF 2)

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76 of 76

BOEING SERVICE BULLETIN 757-24-0132