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Copyright (2015) General Electric Company, U.S.A.
TRANSMITTAL INFORMATION
REVISION 1 TO SERVICE BULLETIN 74-0003
Revision 1 is issued to update paragraphs 1.I., References
and 2., MATERIAL INFORMATION
.
The original was issued May 2, 2014. Revision bars in the left margin identify changes.
1.PLANNING INFORMATION
A.Effectivity
* * * FOR GEnx-1B54, -1B54/P1, -1B54/P2, -1B58, -1B58/P1, -1B58/P2, -1B64, -1B64/P1, -1B64/P2, -1B67, -1B67/P1, -1B67/P2, -1B70, -1B70/P1, -1B70/P2, -1B70/72/P1, -1B70/72/P2, -1B70/75/P1, -1B70/75/P2, -1B74/75/P1, -1B74/75/P2, -1B75/P1, -1B75/P2, -1B78/P2
This Service Bulletin has been introduced in production to these GEnx-1B engines:
GEnx-1B engines, serial numbers 956-360 and up.
The exciter box base support bracket (exciter bracket) P/N 2343M35G01 and double hexagon head machine bolts (machine bolts) P/N AS3237-26 are affected by this Service Bulletin.
B.Description
This Service Bulletin introduces new exciter bracket P/N 2586M20G01 and provides instructions to replace the old part with a new exciter bracket.
C.Compliance
Category 7
GE recommends that you do this Service Bulletin at customer's convenience.
NOTE:
This Service Bulletin can be done on wing or in shop.
D.Concurrent Requirements
None.
E.Reason
(1)Objective:
To improve manufacturing producibility and isolator use standardization.
(2)Condition:
The current design requires more manufacturing resources than desired and uses isolators that are not standardized with the other isolators used on the externals hardware. This condition drives up manufacturing time.
(3)Cause:
A unique, low volume isolator is used only on the GEnx-1B isolator box.
(4)Improvement:
Release design using standard isolator used on other mount locations on the GEnx-1B engine and used on the GEnx-2B isolator base which improves manufacturing producibility of the GEnx-1B exciter base enclosure.
(5)Substantiation:
Substantiation is by comparative analysis.
F.Approval
This Service Bulletin has been reviewed by the FAA and the repair (s) and modification(s) herein comply with the applicable Federal Aviation Regulations and are FAA APPROVED for installation in the model(s) listed in this Service Bulletin.
G.Manpower
No additional man-hours are required to comply with this Service Bulletin.
H.Weight and Balance
The complete compliance with this Service Bulletin decreases 0.36 lb (0.2 kg).
I.References (Use the latest version of these documents)
GEK 112851, GEnx-1B Engine Manual (EM)
GEK 112864, GEnx-1B Engine Illustrated Parts Catalog (EIPC)
GEnx-1B Boeing 787 Aircraft Maintenance Manual (AMM)
  NOTE:
The reference documents listed below are for the engine manufacturer's internal use only:
 
CID: 575079, 575291
 
BPP: 13-74-00-01
J.Publications Affected
GEK 112851, GEnx-1B Engine Manual (EM)
K.Interchangeability
The new parts introduced by this Service Bulletin, the exciter bracket P/N 2586M20G01 and machine bolts P/N AS3237-22, must be installed as an engine set. Mixing parts of new and old configurations is not allowed.
L.Software Accomplishment Summary
Not applicable.
2.MATERIAL INFORMATION
A.Material - Price and Availability
(1)Parts necessary to do this Service Bulletin:
 
Part Number
Qty/ Eng
Part Name
Unit ($) Price
Pkg Qty
Lead Time Days
 
2586M20G01
(1)
Bracket, Exciter Box Base Support
16,280.00
(1)
Quote
 
AS3237-22*
(4)
Bolt, Machine
NP
(-)
--
 
AS3237-08*
(2)
Bolt, Machine
NP
(-)
--
 
NAS1149C0432R*
(2)
Washer
NP
(-)
--
 
J1092P04
(2)
Nut, Self-locking
8.50
(25)
5
*Part not supplied by GE Engine Services Distribution L.L.C. Procure through local purchase.
NP = Not Provisioned
NOTE:
Prices are provided for planning purposes and are subject to change.
(2)Other Spare Parts:
None.
(3)Consumables:
None.
B.Industry Support Information
None.
C.Configuration Chart
 
New Part Number
Qty/ Eng
Part Name
Old Part Number/ IPC Location
Qty/ Eng
Op Code
Chg/ Sprt Code
 
2447M20G01/ G02/G03
(X)
Propulsor Module Assembly
2447M20G01/ G02/G03
(X)
RM
-/-
 
2376M20G05/ G06/G07/G08/ G09
(X)
Propulsor Module Assembly
2376M20G05/ G06/G07/G08/ G09
(X)
RM
-/-
 
.2586M20G01
01-081, 74-11-10

(1)
Bracket, Exciter Box Base Support
(SIN 65810)
.2343M35G01
01-080, 74-11-10

(1)
RE
5/B
 
.AS3237-22
01-091, 74-11-10

(4)
Bolt, Double Hexagon Head Machine
(SIN 65821)
.AS3237-26
01-090, 74-11-10

(4)
RE
5/E
 
.AS3237-08
05-131, 75-23-10

(2)
Bolt, Machine
(SIN 62521)
.AS3237-06
05-130, 75-23-10

(2)
RE
5/E
 
.NAS1149C0432R
05-170, 75-23-10

(2)
Washer
(SIN 62531)
--
(-)
AD
5/-
 
.J1092P04
05-180, 75-23-10

(2)
Nut, Self-locking
(SIN 62542)
--
(-)
AD
5/-
 Operation Codes
AD=Add RE=Replace RM=Remains
Change Code
5=Qualified interchangeability. Refer to paragraph 1.K., Interchangeability.
Support Codes
B=Old parts will be supplied until all old parts are sold. E=Old parts will be supplied and can be used at other locations.
D.Parts Disposition
Use serviceable old parts at other engine locations or for engines that have not changed.
E.Tooling - Price and Availability
None.
3.ACCOMPLISHMENT INSTRUCTIONS
A.On Wing
(1)Refer to the GEnx-1B Boeing 787 AMM, DMC-B787-A-G73-22-01-00A-520A-A, for removal and DMC-B787-A-G73-22-01-00A-720A-A, for installation.
B.Removal In Shop
(1)Remove the ignition cooling system. Refer to the GEnx-1B EM, 72-00-02, DISASSEMBLY 002, Subtask 72-00-02-030-401.
NOTE:
Removal of the ignition cooling system can be limited to the necessary parts to remove the exciter bracket cover (01-010, 74-11-10) and replace the exciter bracket (1, Figure 1).
(2)Remove the exciter bracket cover (01-010, 74-11-10) and disconnect the ignition leads from the igniters and ignition exciters. Refer to the GEnx-1B EM, 72-00-02, DISASSEMBLY 002, Subtask 72-00-02-030-402.
(3)Disconnect the W9 and W10 harnesses from the ignition exciters. Refer to the GEnx-1B EM, 72-00-00, DISASSEMBLY 001, Subtask 72-00-00-030-230 and Subtask 72-00-00-030-231.
(4)Remove the ignition exciters and the old exciter bracket (1, Figure 1). Refer to the GEnx-1B EM, 72-00-02, DISASSEMBLY 002, Subtask 72-00-02-030-402.
C.Installation in Shop
(1)Install the ignition exciters and the new exciter bracket with new machine bolts (2, Figure 1). Refer to the GEnx-1B EM, 72-00-02, ASSEMBLY 005, Subtask 72-00-02-440-157.
(2)Connect back the W9 and W10 harnesses. Refer to the GEnx-1B EM, 72-00-00, ASSEMBLY 001, Subtask 72-00-00-440-012 and Subtask 72-00-00-440-011.
(3)Install the exciter bracket cover (01-010, 74-11-10) and connect the ignition leads to the igniters and the exciter boxes. Refer to the GEnx-1B EM, 72-00-02, ASSEMBLY 005, Subtask 72-00-02-440-157.
(4)Install and connect back the ignition cooling system. Refer to the GEnx-1B EM, 72-00-02, ASSEMBLY 005, Subtask 72-00-02-440-164.
Location of Exciter Bracket
Figure 1