![]() | GEnx-1B SERVICE BULLETIN - 72-0019 R00 | Revised: 06/01/2011 |
SB 72-0019 R00 ENGINE - Mid Fan Shaft Assembly (72-58-00) - Introduction of New A/O Vent Center Tube | Issued: 06/01/2011 | |
1. | PLANNING INFORMATION |
A. | Effectivity |
* * * FOR GEnx-1B54, -1B58, -1B64, -1B67, -1B70 |
This Service Bulletin has been introduced in production to these GEnx-1B engines: |
• |
|
These serial numbers are the best available data. |
The old A/O vent center tube P/N 2331M21G01 is affected by this Service Bulletin. |
B. | Description |
This Service Bulletin releases a new A/O vent center tube P/N 2331M21G02 that removes features from the inner flowpath to reduce oil retention. |
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 improve maintainability. |
(2) | Condition: |
Oil retention has been observed in the A/O vent center tube post engine shutdown. |
(3) | Cause: |
The A/O vent center tube inner tab creates a damming feature in the flowpath, this prevents the oil from draining at engine shutdown. |
(4) | Improvement: |
The A/O vent center tube inner tab feature is removed. |
(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 |
An estimate of the labor cost to accomplish this Service Bulletin may be obtained from any GEnx-1B GEAE authorized Service or Overhaul facility upon request. |
H. | Weight and Balance |
The complete compliance with this Service Bulletin decreases weight by 0.02 lb (0.009 kg). |
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 |
Two-way interchangeable. |
L. | Software Accomplishment Summary |
Not applicable. |
2. | MATERIAL INFORMATION |
A. | Material - Price and Availability |
(1) | Parts necessary to do this Service Bulletin: |
|
NOTE: |
|
(2) | Other Spare Parts: |
None. |
(3) | Consumables: |
None. |
B. | Industry Support Information |
None. |
C. | Configuration Chart |
|
Operation Codes RM=Remains RE=Replace |
Change Code 2=Two-way interchangeable. |
Support Code B=Old parts will be supplied until all old parts are sold. |
D. | Parts Disposition |
Use serviceable old parts for engines that have not changed. |
E. | Tooling - Price and Availability |
None. |
3. | ACCOMPLISHMENT INSTRUCTIONS |
A. | General |
(1) | Remove the low pressure turbine (LPT) module assembly and the mid fan shaft assembly from the propulsor assembly. Refer to the GEnx-1B EM, 72-00-04, REMOVAL 001. |
(2) | Disassemble the LPT module assembly and the mid fan shaft assembly. Refer to the GEnx-1B EM, 72-00-04, DISASSEMBLY 001. |
(3) | Remove the old A/O vent center tube (1, Figure 1). Refer to the GEnx-1B EM, 72-58-00, DISASSEMBLY 001, Subtask 72-58-00-030-002. |
(4) | Install the new A/O vent center tube (1, Figure 1). Refer to the GEnx-1B EM, 72-58-00, ASSEMBLY 001, Subtask 72-58-00-440-009. |
(5) | Assemble the LPT module assembly and the mid fan shaft assembly. Refer to the GEnx-1B EM, 72-00-04, ASSEMBLY 001. |
(6) | Install the LPT module assembly and mid fan shaft assembly to the propulsor assembly. Refer to the GEnx-1B EM, 72-00-04, INSTALLATION 001. |