![]() | GEnx-1B SERVICE BULLETIN - 79-0003 R01 | Revised: 12/03/2018 |
SB 79-0003 R01 OIL - Oil Tank Scavenge Tube (79-22-20) - Introduction of New Oil Scavenge Tube and Support Bracket | Issued: 12/19/2011 | |
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Copyright (2018) General Electric Company, U.S.A. |
TRANSMITTAL INFORMATION |
REVISION 1 TO SERVICE BULLETIN 79-0003 |
Revision 1 is issued to update paragraphs 1., PLANNING INFORMATION, 2., MATERIAL INFORMATION, and 3., ACCOMPLISHMENT INSTRUCTIONS. |
The original was issued December 19, 2011. Revision bars in the left margin identify changes. |
1. | PLANNING INFORMATION |
A. | Effectivity |
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This Service Bulletin is applicable to these GEnx-1B engines: |
• |
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These serial numbers are the best available data. |
The oil return tube (oil scavenge tube) P/N 2366M93G01 is affected by this Service Bulletin. |
B. | Description |
This Service Bulletin introduces the new oil scavenge tube P/N 2379M80G01 and support bracket P/N 2447M79G01. |
C. | Compliance |
Category 7 |
GE recommends that you do this Service Bulletin at customer's convenience. |
Impact F |
Implement as deemed necessary per the Service Bulletin Category. |
NOTE: |
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D. | Concurrent Requirements |
None. |
E. | Reason |
(1) | Objective: |
To introduce new parts and improve maintainability. |
(2) | Condition: |
Current oil scavenge tube interferes with the removal path of the oil tank level sensor. |
(3) | Cause: |
This condition causes delays and additional operations at removal of the oil tank level sensor. |
(4) | Improvement: |
The new oil scavenge tube was re-routed to allow the proper removal of the oil tank level sensor. |
(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 |
After you get access to the oil tank, you will need approximately 1.0 man-hour for each engine. |
H. | Weight and Balance |
The complete compliance with this Service Bulletin increases weight by 0.36 lb (0.16 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) |
GEnx-1B Boeing 787 Aircraft Maintenance Manual (AMM) |
NOTE: |
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J. | Publications Affected |
GEK 112851, GEnx-1B Engine Manual (EM) |
GEK 112864, GEnx-1B Engine Illustrated Parts Catalog (EIPC) |
GEnx-1B Boeing 787 Aircraft Maintenance Manual (AMM) |
K. | Interchangeability |
The new oil scavenge tube P/N 2379M80G01 needs to be installed as a set with the new support bracket P/N 2447M79G01. |
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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NP = Not Provisioned |
*Part not supplied by GE Engine Services Distribution L.L.C. |
NOTE: |
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(2) | Other Spare Parts: |
None. |
(3) | Consumables: |
|
B. | Industry Support Information |
None. |
C. | Configuration Chart |
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Operation Codes AD=Add QTC=Quantity Change RE=Replace RM=Remains |
Change Code 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 |
None. |
E. | Tooling - Price and Availability |
None. |
3. | ACCOMPLISHMENT INSTRUCTIONS |
A. | Removal of the Oil Scavenge Tube |
(1) | Removal instructions for the oil scavenge tube (1, Figure 1) have not changed. Refer to the GEnx-1B EM, 72-00-01, DISASSEMBLY 001, Subtask 72-00-01-040-053. |
B. | Installation of the Oil Scavenge Tube |
(1) | Install the support bracket (01-030, 72-00-01) and support bracket (1, Figure 2) to the forward ring where the fan case assembly and the fan aft case are connected at boltholes No. 30 and 31. Refer to Figure 2 and do as follows: |
WARNING: |
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(a) | Apply C03-001 primer or C03-100 primer to the threads and friction surfaces of the bolts (01-050), the internal diameter (ID) of the boltholes, and the surface of the support bracket (01-030) and support bracket (1) that contacts the fan case. |
WARNING: |
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(b) | Apply C02-058 thread lubricant to the threads of the bolts (01-050) and the self-locking nuts (01-060). |
(c) | Install the bolts (01-050) in the boltholes on the forward side of the fan case forward ring. |
(d) | Install the support bracket (01-030) and support bracket (1) on the aft side of the split flange at boltholes No. 30 and 31. Refer to Figure 2. |
(e) | Install the self-locking nuts (01-060) on the bolts (01-050) on the aft side of the fan case forward ring. |
(f) | Torque the self-locking nuts (01-060) to 202-238 lb in. (22.9-26.9 Nm). |
(g) | Torque the self-locking nuts (01-060) again to 202-238 lb in. (22.9-26.9 Nm). |
(2) | Install the oil scavenge tube (1, Figure 1) to the oil tank (01-010, 79-11-10) assembly. Refer to Figure 1 and do as follows: |
WARNING: |
|
(a) | Apply C02-019 engine oil or C02-023 engine oil to the flange seal gasket (01-030, 79-22-20). |
(b) | Install the gasket (01-030) on the lubriclone assembly (01-010, 79-21-20) and attach the oil scavenge tube (1, Figure 1) with the machine bolts (01-020, 79-22-20) at four locations. Do not torque the machine bolts (01-020) at this time. |
(c) | Install the gasket (01-030) on the oil return tube (01-090) or (01-090A) and attach the oil scavenge tube (1) with the machine bolts (01-060) at four locations. Do not torque the machine bolts (01-060) at this time. |
(d) | Install a P-clamp (3) on the support bracket (2) with the bolt (4). |
(e) | Install the remaining P-clamps (3) around the oil scavenge tube (1) at three locations with the remaining bolts (4). |
(f) | Torque the bolts (01-020) that attach the oil scavenge tube (1) to the lubriclone assembly (01-010, 79-21-20) to 106 to 124 lb in. (11.9 to 14.0 Nm). |
(g) | Torque the bolts (01-060, 79-22-20) that attach the oil scavenge tube (1) to the oil return tube (01-090) or (01-090A) to 106 to 124 lb in. (11.9 to 14.0 Nm). |
(h) | Torque the bolt (4) on the P-clamp (3) to 51 to 59 lb in. (5.7 to 6.6 Nm). |