![]() | GEnx-1B SERVICE BULLETIN - 79-0004 R01 | Revised: 01/17/2013 |
SB 79-0004 R01 OIL - Lubrication Unit (79-21-10) - Introduction of New Screen Assemblies with Improved MCD | Issued: 04/02/2012 | |
TRANSMITTAL INFORMATION |
REVISION 1 TO SERVICE BULLETIN 79-0004 |
Revision 1 is issued to effectively cancel the intent of this Service Bulletin. GE Aviation no longer recommends the accomplishment of this Service Bulletin. |
The original was issued April 02, 2012. Revision bars in the left margin identify changes. |
1. | PLANNING INFORMATION |
A. | Effectivity |
|
This change was cancelled and was removed from production. |
The screen assemblies P/N LR47504, P/N LR47505, and P/N LR47507 that belong to the lube unit P/N LR47760E1 are affected by this Service Bulletin. |
B. | Description |
GE Aviation no longer recommends the accomplishment of this Service Bulletin. |
The alternative preformed packings, P/N J1438P916, P/N J1438P918, and P/N J1438P924 are still acceptable alternative parts for the current screen assemblies. |
This Service Bulletin releases the screen assemblies with new magnetic chip detector (MCD) P/N LR48211, P/N LR48212, and P/N LR48214 on the lube and scavange pump (lube unit) P/N LR47760E1. This Service Bulletin also adds the alternative preformed packings P/N J1438P916, P/N J1438P918, and P/N J1438P924 to the lube unit. |
C. | Compliance |
Category 9 |
Information only. GE Aviation no longer recommends the accomplishment of this Service Bulletin. |
NOTE: |
|
D. | Concurrent Requirements |
None. |
E. | Reason |
(1) | Objective: |
To introduce new parts. |
(2) | Condition: |
Under certain engine conditions, the capture efficiency of the MCD located in the screen assembly can be insufficient. |
(3) | Cause: |
Insufficient capture efficiency of the MCD. |
(4) | Improvement: |
The new screen assembly contains a more powerful magnet with better capture efficiency. |
(5) | Substantiation: |
Substantiation is by comparative analysis, analysis, and test. |
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 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 |
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: |
|
NP = Not Provisioned |
NOTE: |
|
*Part not supplied by GE Engine Services Distribution L.L.C. To procure parts, contact the following: |
Fiatavio SPA Corso Ferrucci 112 Turin Italy |
(2) | Other Spare Parts: |
|
NOTE: |
|
(3) | Consumables: |
|
B. | Industry Support Information |
None. |
C. | Configuration Chart |
NOTE: |
|
|
Operation Codes AD=Add RE=Replace RM=Remains |
Change Codes 2=Two-way interchangeable. 5=Qualified interchangeability. Refer to paragraph 1.K., Interchangeability. |
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. | Removal |
(1) | Remove the five screen assemblies (1, 3, and 5, Figure 1)from the lube unit (01-010, 79-21-10) as follows: |
(a) | Do not remove the contamination caught in the screen assemblies and on the MCDs when the screen assemblies (1, 3, and 5) are removed. |
(b) | Put the 1.0 gal (3.8 liter) oil resistant container below the lube unit (01-010). |
NOTE: |
|
(c) | Remove the screen assemblies (1, 3, and 5) from the lube unit (01-010). |
(d) | Put the oil drain into the oil resistant container. |
(e) | Install the protective covers on the open ports of the lube unit (01-010). |
(f) | Remove and discard the preformed packings (2, 4, and 6) from the lube unit (01-010). |
B. | Installation |
(1) | Install the screen assemblies (1, 3, and 5, Figure 1)in the lube unit (01-010, 79-21-10) as follows: |
WARNING: |
|
CAUTION: |
|
(a) | Apply a light layer of C02-019 engine oil to the new preformed packings (2, 4, and 6). |
(b) | Install the new preformed packings (2, 4, and 6) into the groove below the flange of the screen assemblies (1, 3, and 5). |
(c) | Remove the protective covers from the open ports of the lube unit (01-010). |
(d) | Install the new screen assemblies (1, 3, and 5) into the lube unit (01-010). |
(e) | Tighten the new screen assemblies (1, 3, and 5) and torque to 100-120 lb in. (11.3-13.6 N.m). |