GE PROPRIETARY INFORMATION
The information contained in this document is GE proprietary information and is disclosed in confidence. It is the property of GE and shall not be used, disclosed to others or reproduced without the express written consent of GE, including, but without limitation, it is not to be used in the creation, manufacture, development, or derivation of any repairs, modifications, spare parts, designs, or configuration changes or to obtain FAA or any other government or regulatory approval to do so. If consent is given for reproduction in whole or in part, this notice and the notice set forth on each page of this document shall appear in any such reproduction in whole or in part.
This technical data is considered EAR controlled pursuant to 15 CFR Parts 730-774 respectively. Transfer of this data by any means to a Non-US Person, whether in the United States or abroad, without the proper U.S. Government authorization (e.g., License, exemption, NLR, etc.), is strictly prohibited.
Copyright (2018) 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, -1B75/P1, -1B76A/P2
B.Description
This Service Bulletin releases two new catalog sequence numbers (CSNs)/significant item number (SIN).
C.Compliance
Category 9
Information only
Impact E
This recommendation is to improve the cost of ownership, reduce maintenance requirements, or is a product improvement.
D.Concurrent Requirements
None.
E.Reason
(1)Objective:
To improve maintainability and move the oil return tube hardware parts to the engine assembly level.
(2)Condition:
Currently, the test assembly has to remove the oil return tube and its attaching hardware in order to install the test enabling hardware. This removal and reinstallation increases the assembly time and could cause damage to the hardware during removal.
(3)Cause:
The current oil return tube, support brackets, machine bolts, cushioned clamps and seals need to be removed when the engine reaches the test site to attach the test enabling hardware.
(4)Improvement:
Moving the oil return tube to the engine assembly level will reduce the assembly time and prevent any risk for hardware damage during removal.
(5)Substantiation:
Substantiation is by comparative analysis.
F.Approval
This Service Bulletin contains no modification information that revises the approved configuration and therefore does not require FAA or regulatory approval.
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: 575561
J.Publications Affected
GEK 112851, GEnx-1B Engine Manual (EM)
GEK 112864, GEnx-1B Engine Illustrated Parts Catalog (EIPC)
K.Interchangeability
Not applicable.
L.Software Accomplishment Summary
Not applicable.
2.MATERIAL INFORMATION
A.Material - Price and Availability
(1)Parts necessary to do this Service Bulletin:
None.
(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
 
2305M10G03/
G06/G07
(X)
GEnx Engine Assembly
2305M10G03/
G06/G07
(X)
RM
-/-
 
2447M10G01/
G02/G03
(X)
GEnx Engine Assembly
2447M10G01/
G02/G03
(X)
RM
-/-
 
.MS9556-08
01-041, 79-22-20

(10)
Bolt, Machine
(SIN 4532C)
--
(-)
AD
5/-
 
.M85449-3-20
01-051, 79-22-20

(5)
Clamp, Cushioned
(SIN 45384)
--
(-)
AD
5/-
 
.2305M15G04/
G05/G06/G08/
G09/G10/G11
(X)
Fan, Stator Module Assembly
(SIN 00103)
.2305M15G04/
G05/G06/G08/
G09/G10/G11
(X)
RM
-/-
 
..MS9556-08
01-040B, 79-22-20

(6)
Bolt, Machine
(SIN 45323)
..MS9556-08
01-040A, 79-22-20

(16)
QTC
5/-
 
..M85449-3-20
01-050B, 79-22-20

(3)
Clamp, Cushioned
(SIN 45381)
..M85449-3-20
01-050A, 79-22-20

(8)
QTC
5/-
Operation Codes
AD=Add
QTC=Quantity Change RM=Remains
Change Codes
5=Qualified interchangeability. Refer to paragraph 1.K., Interchangeability.
Support Codes
None.
D.Parts Disposition
None.
E.Tooling - Price and Availability
None.
3.ACCOMPLISHMENT INSTRUCTIONS
A.General
(1)Not applicable.