![]() | GEnx-1B SERVICE BULLETIN - 72-0106 R01 | Revised: 12/17/2012 |
SB 72-0106 R01 ENGINE - Propulsor Module Assembly (72-00-00) - Introduction of New Seal P/N 2503M02P01 | Issued: 08/29/2012 | |
TRANSMITTAL INFORMATION |
REVISION 1 TO SERVICE BULLETIN 72-0106 |
Revision 1 is issued to update paragraphs 1.A., Effectivity and 2., MATERIAL INFORMATION. |
The original was issued on the August 29, 2012. Revision bars in the left margin identify changes. |
1. | PLANNING INFORMATION |
A. | Effectivity |
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This Service Bulletin has been introduced in production to these GEnx-1B engines: |
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These serial numbers are the best available data. |
The seal P/N 2301M68P01 is affected by this Service Bulletin. |
B. | Description |
This Service Bulletin releases a new seal P/N 2503M02P01. |
C. | Compliance |
Category 4 |
GE recommends that you do this Service Bulletin when the seal is exposed. |
NOTE: |
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NOTE: |
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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 operators fleet. |
D. | Concurrent Requirements |
None. |
E. | Reason |
(1) | Objective: |
To introduce a new part and improve reliability. |
(2) | Condition: |
Heavy rubs can occur on the aft No. 4 bearing seal with the potential for the rubs to increase the clearances and the oil consumption rate to be affected. |
(3) | Cause: |
The current seal is susceptible to a transient thermal instability, and depending upon the assembly tolerance stack-up, a heavy rub could occur on the aft No. 4 bearing seal. |
(4) | Improvement: |
The new seal has improved cooling and is thermally stable, which results in more consistent stator clearance control and improved reliability. |
(5) | Substantiation: |
Substantiation is by analysis and 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 112862, GEnx-1B Cleaning, Inspection, and Repair Manual (CIR) |
GEK 112864, GEnx-1B Engine Illustrated Parts Catalog (EIPC) |
GEnx-1B SB 79-0012, OIL SYSTEM - Lubrication Unit (79-21-10) - Replacement Interval for Oil Filter Element |
NOTE: |
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J. | Publications Affected |
GEK 112851, GEnx-1B Engine Manual (EM) |
GEK 112862, GEnx-1B Cleaning, Inspection, and Repair Manual (CIR) |
GEK 112864, GEnx-1B Engine Illustrated Parts Catalog (EIPC) |
K. | Interchangeability |
One-way interchangeable. |
L. | Software Accomplishment Summary |
Not applicable. |
2. | MATERIAL INFORMATION |
A. | Material - Price and Availability |
(1) | Parts necessary to do this Service Bulletin: |
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NOTE: |
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(2) | Other Spare Parts: |
None. |
(3) | Consumables: |
None. |
B. | Industry Support Information |
Contact your Customer Support Manager (CSM) for support details. |
C. | Configuration Chart |
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Operation Codes RE=Replace RM=Remains |
Change Code 1=One-way interchangeable. |
Support Code A=Old parts will no longer be supplied. |
D. | Parts Disposition |
Discard old parts. |
E. | Tooling - Price and Availability |
None. |
3. | ACCOMPLISHMENT INSTRUCTIONS |
A. | General |
(1) | Removal instructions for the seal have not changed. Refer to the GEnx-1B EM, 72-00-02, DISASSEMBLY 004, Subtask 72-00-02-030-366. |
(2) | Installation instructions for the seal have not changed. Refer to the GEnx-1B EM, 72-00-02, ASSEMBLY 002, Subtask 72-00-02-430-731. |