![]() | GEnx-1B SERVICE BULLETIN - 72-0208 R00 | Revised: 05/02/2014 |
SB 72-0208 R00 ENGINE - High Pressure Compressor Module Assembly (72-30-00) - Introduction of Alternative Compressor Rotor Part Number to PRE-PIP HPC Modules | Issued: 05/02/2014 | |
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 (2014) General Electric Company, U.S.A. |
1. | PLANNING INFORMATION |
A. | Effectivity |
|
This Service Bulletin is applicable to these GEnx-1B engines: |
• |
|
These serial numbers are the best available data. |
B. | Description |
This Service Bulletin releases an alternative HPC rotor assembly P/N 2305M51G05 for HPC modules P/N 2305M53G06/G09. |
C. | Compliance |
Category 9 |
Information only. |
D. | Concurrent Requirements |
None. |
E. | Reason |
(1) | Objective: |
To introduce new parts. |
(2) | Condition: |
HPC rotor module P/N 2305M51G05 is a certified alternative to the P/N 2305M51G06 and is used in compliance engines. |
(3) | Cause: |
All required HPC rotor modules are not in the EIPC. The P/N 2305M51G05 needs to be added to the EIPC as an alternative to P/N 2305M51G06 for HPC modules P/N 2305M53G06/G09. |
(4) | Improvement: |
The addition of the alternative HPC rotor assembly will make the EIPC consistent with hardware delivered to customers. |
(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 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 this document) |
GEK 112864, GEnx-1B Engine Illustrated Parts Catalog (EIPC) |
NOTE: |
|
J. | Publications Affected |
GEK 112864, GEnx-1B Engine Illustrated Parts Catalog (EIPC) |
K. | Interchangeability |
The proposed P/N 2305M51G05 and P/N 2305M51G06 are interchangeable as full modules. Either can be used with P/N 2305M53G06 or P/N 2305M53G09. |
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 |
|
Operation Codes AD=Add RM=Remains |
Change Code 5=Qualified interchangeability. Refer to paragraph 1.K., Interchangeability. |
Support Code A=Old parts will no longer be supplied. |
D. | Parts Disposition |
None. |
E. | Tooling - Price and Availability |
None. |
3. | ACCOMPLISHMENT INSTRUCTIONS |
A. | General |
(1) | Removal, installation, cleaning, and inspection procedures have not changed. |