![]() | GEnx-1B SERVICE BULLETIN - 72-0120 R01 | Revised: 04/16/2013 |
SB 72-0120 R01 ENGINE - Turbine Center Frame and No. 4 Bearing Related Parts (72-00-02) - Introduction of New Turbine Center Frame Module | Issued: 12/18/2012 | |
TRANSMITTAL INFORMATION |
REVISION 1 TO SERVICE BULLETIN 72-0120 |
Revision 1 is issued to update paragraphs 1., PLANNING INFORMATION and 2., MATERIAL INFORMATION. |
The original was issued on the December 18, 2012. Revision bars in the left margin identify changes. |
1. | PLANNING INFORMATION |
A. | Effectivity |
|
This Service Bulletin is applicable to all GEnx-1B engines. |
B. | Description |
This Service Bulletin introduces the turbine frames P/N 2304M99G09 and P/N 2304M99G16. |
C. | Compliance |
Category 7 |
GE recommends that you do this Service Bulletin at customer's option. |
NOTE: |
|
D. | Concurrent Requirements |
None. |
E. | Reason |
(1) | Objective: |
To introduce new parts. |
(2) | Condition: |
The turbine frame of the current TCF modules available in the EIPC are P/N 2304M99G10, P/N 2304M99G14, and P/N 2304M99G17. |
(3) | Cause: |
This Service Bulletin introduces new turbine frame P/N 2304M99G09 and P/N 2304M99G16 to the EIPC, which have been certified for the GEnx-1B engine. |
(4) | Improvement: |
This Service Bulletin allows the turbine frame P/N 2304M99G09 and P/N 2304M99G16 to be used on production engines. |
(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 |
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: |
|
J. | Publications Affected |
GEK 112864, GEnx-1B Engine Illustrated Parts Catalog (EIPC) |
K. | Interchangeability |
The turbine frame P/N 2304M99G09 is two-way interchangeable as a set with the turbine frame P/N 2304M99G10. The components of the turbine frame must be introduced as a complete turbine frame set and cannot be interchanged between assemblies. The turbine frame P/N 2304M99G09 will not be provisioned. |
The turbine frame P/N 2304M99G16 is two-way interchangeable as a set with the turbine frame P/N 2304M99G14. The components of the turbine frame must be introduced as a complete turbine frame set and cannot be interchanged between assemblies. The turbine frame P/N 2304M99G16 will not be provisioned. |
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: |
|
*Part not supplied by GE Engine Services Distribution L.L.C. |
NP = Not Provisioned |
(3) | Consumables: |
None. |
B. | Industry Support Information |
None. |
C. | Configuration Chart |
|
Operation Codes AD=Add RE=Replace RM=Remains |
Change Code 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) | Removal instructions for the TCF module have not changed. Refer to the GEnx-1B EM, 72-00-02, DISASSEMBLY 005, Subtask 72-00-02-030-322. |
(2) | Installation instructions for the TCF module have not changed. Refer to the GEnx-1B EM, 72-00-02, ASSEMBLY 002, Subtask 72-00-02-430-724. |