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 (2013) General Electric Company, U.S.A.
1.PLANNING INFORMATION
A.Effectivity
* * * FOR GEnx-1B54, -1B58, -1B64, -1B67, -1B70
This Service Bulletin is applicable to all GEnx-1B engines.
B.Description
This Service Bulletin introduces new part numbers to the Engine Illustrated Parts Catalog (EIPC).
C.Compliance
Category 9
Information only.
D.Concurrent Requirements
None.
E.Reason
(1)Objective:
To introduce new parts.
(2)Condition:
The GEnx-1B EIPC needs to be updated.
(3)Cause:
There are some vendor parts that need to be added to the GEnx-1B EIPC and some GE parts that need to be updated in the EIPC that are on the IP baseline list.
(4)Improvement:
Include new parts to the GEnx-1B EIPC.
(5)Substantiation:
The new parts need to be included in the GEnx-1B EIPC.
F.Approval
This Service Bulletin contains no modification information that revises the approved configuration and therefore does not require FAA 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 9250, Commercial Engine Standard Practices Manual (SPM)
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: 573975, 573978, and 575004
 
Certification Report R2004AE380 Vol. 1
J.Publications Affected
GEK 112864, GEnx-1B Engine Illustrated Parts Catalog (EIPC)
K.Interchangeability
Parts added.
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:
 
Code Number
Description
 
C02-058
Compound, Thread Lubricating (lubricant)
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
 
2376M20G05
(X)
Propulsor Module Assembly
2376M20G05
(X)
RM
-/-
 
.2305M56G05
34-010, 72-00-02

(1)
Nozzle Assembly, HPT Stage 2
(SIN 17400)
.2305M56G05
34-010, 72-00-02

(1)
RM
-/-
 
.2305M56G03
34-010A, 72-00-02

(ALT)
Nozzle Assembly, HPT Stage 2
(SIN 17400)
--
(-)
AD
5/-
 
2305M31G12
(X)
Fan Hub Frame
2305M31G12
(X)
RM
-/-
 
.10090496
01-490D, 72-26-00

(1)
Frame, Assembly Fan Hub
(SIN 840A0)
--
(-)
AD
5-
 
..J644P09F
01-530, 72-26-00

(16)
Bolt, Machine
(SIN 840FD)
--
(-)
AD
5/-
 
..10024746
01-540, 72-26-00

(4)
Gasket
(SIN 840N7)
--
(-)
AD
5/-
 
..10029374
01-550, 72-26-00

(4)
Plug, Blanking
(SIN 840S0)
--
(-)
AD
5/-
 
2305M32G03
(X)
Gearbox, Inlet
2305M32G03
(X)
RM
-/-
 
.2312M46P01
01-340B, 72-61-00

(1)
Bearing, Ball
(SIN 030A2)
--
(-)
AD
5/-
 
.2312M48P01
01-320B, 72-61-00

(1)
Bearing, Roller
(SIN 030A3)
--
(-)
AD
5/-
 
.2312M55P01
01-260B, 72-61-00

(1)
Bearing, Roller
(SIN 030AK)
--
(-)
AD
5/-
 
2305M33G01
(X)
Transfer Gearbox
2305M33G01
(X)
RM
-/-
 
.2312M46P01
01-120B, 72-62-00

(1)
Bearing, Ball
(SIN 032A4)
--
(-)
AD
5/-
 
.2312M49P01
01-110B, 72-62-00

(1)
Bearing, Roller
(SIN 032A5)
--
(-)
AD
5/-
 
.2312M47P01
01-250B, 72-62-00

(1)
Bearing, Ball
(SIN 032AA)
--
(-)
AD
5/-
 
.2312M51P01
01-230B, 72-62-00

(1)
Bearing, Roller
(SIN 032AF)
--
(-)
AD
5/-
 
.2312M50P01
01-270B, 72-62-00

(1)
Bearing, Roller
(SIN 032AH)
--
(-)
AD
5/-
Operation Codes
AD=Add
RM=Remains
Change Code
5=Qualified interchangeability. Refer to paragraph 1.K., Interchangeability.
D.Parts Disposition
None.
E.Tooling - Price and Availability
None.
3.ACCOMPLISHMENT INSTRUCTIONS
A.General.
(1)Install the blanking plugs (1, Figure 1) to the assembly fan hub frame (fan hub frame) (2). Refer to Figure 1 and do as follows:
(a)Install one gasket (3) on each of the four blanking plugs (1).
WARNING:
REFER TO THE PRODUCT LABEL AND THE MANUFACTURERS (MATERIAL) SAFETY DATA SHEET FOR INSTRUCTIONS ON THE HAZARDS, STORAGE, SAFE HANDLING AND PROPER USE OF THIS PRODUCT.
(b)Apply C02-058 lubricant to the machine bolts (bolts) (4) threads.
(c)Install the blanking plugs (1) on the fan hub frame (2) with four bolts (4) for each cover. Install plugs to the aft side of the fan hub frame at the 3:00, 5:30, 9:00, and 11:00 oclock positions.
(d)Torque the bolts (4) to 19-21 lb. in (2.1-2.4 N.m) and secure them with safety wire.
Installation of the Blanking plugs to the Fan Hub Frame
Figure 1