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Copyright (2024) General Electric Company, U.S.A.
1.PLANNING INFORMATION
A.Effectivity
* * * FOR GEnx-1B64, -1B64/P1, -1B64/P2, -1B67, -1B67/P1, -1B67/P2, -1B70, -1B70/75/P1, -1B70/75/P2, -1B70/P1, -1B70/P2, -1B70C/P1, -1B70C/P2, -1B74/75/P1, -1B74/75/P2, -1B76/P2, -1B76A/P2
This Service Bulletin is applicable to all GEnx-1B engines.
The machine bolt (bolt) P/N J334P08A is affected by this Service Bulletin.
B.Description
This Service Bulletin releases a new spacer P/N 2991M40P01, bolt P/N J334P10A, and alternate bolt P/N MS9697-10 to the combustor discharge manifold to improve the clamp.
C.Compliance
Category 5
GE recommends that you do this Service Bulletin as soon as the combustor discharge manifold is removed from the engine.
Impact E
This recommendation is to improve the cost of ownership, reduce maintenance requirements or is a product improvement.
NOTE:
This Service Bulletin can be done in shop.
This Service Bulletin is offered to improve the reliability or performance of your GE product, or to help prevent the occurrence of the event or condition described in this Service Bulletin. If the operator elects not to participate in the bulletin, that decision will be taken into consideration by GE in evaluating future product performance issues that may arise in the operator’s fleet.
D.Concurrent Requirements
None.
E.Reason
(1)Objective:
To introduce new parts.
(2)Condition:
Cracks and missing material are found on the combustor discharge manifold.
(3)Cause:
Residual motion between the combustor discharge manifold and surrounding hardware can lead to cracking on the combustor discharge manifold.
(4)Improvement:
Adding the new spacer with longer bolt in order to increase the clamp on the combustor discharge manifold.
(5)Substantiation:
Substantiation is by analysis.
F.Approval
The data contained in this Service Bulletin has been reviewed by the FAA or authorized entity representing the FAA and the repair(s) and modification(s) herein comply with the applicable Aviation Regulations and are 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
Weight and balance are not changed.
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)
NOTE:
The reference documents listed below are for the engine manufacturer's internal use only:
CID: 8003061, 8013889
J.Publications Affected
GEK 112851, GEnx-1B Engine Manual (EM)
GEK 112864, GEnx-1B Engine Illustrated Parts Catalog (EIPC)
K.Interchangeability
Qualified interchangeability.
The new longer bolt and spacer are one-way interchangeable with the old bolt and must be used as a set together when accomplishing this Service Bulletin.
Bolt P/N MS9697-10 is two-way interchangeable with bolt P/N J334P10A.
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
 
J334P10A
(11)
Bolt, Machine
Quote
(-)
--
 
MS9697-10
(ALT)
Bolt, Machine
Quote
(-)
--
 
2991M40P01
(11)
Spacer
Quote
(-)
--
NOTE:
Prices are found in the GE Materials Catalog.
(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
 
2376M54G02/
G03/G04/G05/
G06/G07/G08/
G09/G10/G11/
G12
(X)
Combustor Diffuser Assembly
2376M54G02/
G03/G04/G05/
G06/G07/G08/
G09/G10/G11/
G12
(X)
RM
-/-
 
.J334P10A
01-170A, 72-41-00

(11)
Bolt, Machine
(SIN 09820)
.J334P08A
01-170, 72-41-00

(11)
RE
5/A
 
.MS9697-10
01-170B, 72-41-00

(ALT)
Bolt, Machine
(SIN 09820)
--
(-)
AD
5/-
 
.2991M40P01
01-173, 72-41-00

(11)
Spacer
(SIN 09830)
--
(-)
AD
5/-
Operation Codes
AD=Added
RE=Replace
RM=Remains
Change Codes
5=Qualified interchangeability. Refer to paragraph 1.K., Interchangeability.
Support Codes
A=Old parts will no longer be supplied.
D.Parts Disposition
Scrap removed hardware.
E.Tooling - Price and Availability
None.
3.ACCOMPLISHMENT INSTRUCTIONS
A.Disassembly
(1)Disassemble the combustor diffuser assembly and remove the old bolt (1, Figure 1). Refer to the GEnx-1B EM, 72-41-00, DISASSEMBLY 001, CONFIG 01 or CONFIG 02.
B.Assembly
(1)Assemble the combustor diffuser assembly with the new bolt (1, Figure 1) and spacer (2). Refer to the GEnx-1B EM, 72-41-00, ASSEMBLY 001, CONFIG 01 or CONFIG 02.
Combustor Discharge Manifold Location
Figure 1