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Copyright (2017) General Electric Company, U.S.A.
TRANSMITTAL INFORMATION
REVISION 2 TO SERVICE BULLETIN 79-0007
Revision 2 is issued to update paragraphs 1.A., Effectivity and 2.C., Configuration Chart.
Revision 1 was issued April 21, 2014. The original was issued July 20, 2012. Revision bars in the left margin identify changes.
1.PLANNING INFORMATION
A.Effectivity
 
* * * FOR GEnx-1B64, -1B64/P1, -1B64/P2, -1B67, -1B67/P1, -1B67/P2, -1B70, -1B70/75/P1, -1B70/75/P2, -1B70/P1, -1B70/P2, -1B70C/P1, -1B70C/P2, -1B74/75/P1, -1B74/75/P2
 This Service Bulletin is applicable to all GEnx-1B, GEnx-PIP1 and GEnx- PIP2 engines.
This Service Bulletin will be introduced on 2nd Q 2012.
The oil vent manifold P/N 2378M31G01 is affected by this Service Bulletin.
B.Description
This Service Bulletin releases an improved oil vent manifold P/N 2506M09G01 for production and provides instructions to install the new parts.
C.Compliance
Category 3
GE recommends that you do this Service Bulletin at the next shop visit of the engine/module.
NOTE:
This Service Bulletin can be done in shop.
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 new part, improve maintainability, and reduce weight.
(2)Condition:
The turbine center frame (TCF) vent strut tubes were damaged by incorrect installation of vent oil manifold when the flange protrusion was inserted into the mating strut tube hole during development testing.
(3)Cause:
The shorter protrusion was intended to help in the manifold installation. Installation was particularly difficult, which has no additional flange in the circumferential run.
(4)Improvement:
The removal of the four machine bolts P/N AS3237-14 of the oil vent manifold reduces tangential tolerance stack up of the triangular flange attached to TCF strut.
(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
The complete compliance with this Service Bulletin decreases weight by 0.67 lb (0.30 kg).
I.References (Use the latest version of these documents)
GEK 112851, GEnx-1B Engine Manual
GEK 112864, GEnx-1B Engine Illustrated Parts Catalog (EIPC)
NOTE:
The reference documents listed below are for the engine manufacturer's internal use only:
 
CID: 573394
 
BPP: 11-79-00-02
J.Publications Affected
GEK 112851, GEnx-1B Engine Manual
GEK 112864, GEnx-1B Engine Illustrated Parts Catalog (EIPC)
K.Interchangeability
All parts introduced need to be introduced as an engine set.
L.Software Accomplishment Summary
Not applicable.
2.MATERIAL INFORMATION
A. Material - Price and Availability
(1)Parts necessary to do this Service Bulletin:
 
Part Number
Qty/ Eng
Part Name
Unit ($) Price
Pkg Qty
Lead Time Days
 
2506M09G01
(1)
Oil Vent Manifold
3,119.00
(1)
5
 
2497M18P01
(1)
Insulation Blanket
734.00
(1)
5
 
2497M18P02
(1)
Insulation Blanket
257.75
(1)
30
 
2497M18P03
(1)
Insulation Blanket
257.75
(1)
30
 
2497M18P04
(1)
Insulation Blanket
238.00
(1)
5
NOTE:
Prices are provided for planning purposes and are subject to change.
(2)Other Spare Parts:
None.
(3)Consumables:
 
Code Number
Description
 
C02-019
Oil, Engine Lubricating (engine oil)
 
C02-023
Oil, Engine Lubricating (engine oil)
B.Industry Support Information
None.
C.Configuration Chart
 
New Part Number
Qty/ Eng
Part Name
Old Part Number
Qty/ Eng
Op Code
Chg/ Sprt Code
 
2376M20G05/
G06/G08
(X)
Propulsor Module Assembly
2376M20G05/
G06/G08
(X)
RM
-/-
 
2447M20G01
(X)
Propulsor Module Assembly
2447M20G01
(X)
RM
-/-
 
.2506M09G01
05-111, 79-22-30

(1)
Manifold, Oil Vent
(SIN 46101)
.2378M31G01
05-110, 79-22-30

(1)
RE
5/A
 
--
(-)
Tube, Oil Vent
(SIN 46103)
.2320M99G01
05-160, 79-22-30

(1)
DE
5/A
 
.AS3237-14
05-130A, 79-22-30

(4)
Bolt, Machine
(SIN 46121)
.AS3237-14
05-130, 79-22-30

(8)
QTC
5/E
 
.AS3486-10
05-050A, 79-22-30

(8)
Nut, Self-Locking
(SIN 46141)
.AS3486-10
05-050, 79-22-30

(12)
QTC
5/E
 
.1508M13P117
05-140A, 79-22-30

(1)
Gasket, Seal Flange
(SIN 46151)
.1508M13P117
05-140, 79-22-30

(2)
QTC
5/E
 
.2497M18P02
05-181, 79-22-30

(1)
Insulation Blanket
(SIN 46190)
.2379M34P01
05-180, 79-22-30

(1)
RE
5/A
 
.2497M18P01
05-191, 79-22-30

(1)
Insulation Blanket
(SIN 46191)
.2379M34P02
05-190, 79-22-30

(1)
RE
5/A
 
--
(-)
Insulation Blanket
(SIN 46194)
.2326M36P05
05-260, 79-22-30

(1)
DE
5/A
 
--
(-)
Blanket
(SIN 46195)
.2326M36P06
05-270, 79-22-30

(1)
DE
5/A
 
.2497M18P03
05-291, 79-22-30

(1)
Insulation Blanket
(SIN 4619F)
.2326M38P01
05-290, 79-22-30

(1)
RE
5/A
 
.2497M18P04
05-281, 79-22-30

(1)
Insulation Blanket
(SIN 4619G)
.2326M38P02
05-280, 79-22-30

(1)
RE
5/A
 
.1443M45P02
05-170A, 79-22-30

(21)
Strap, Tiedown
(SIN 4619H)
.1443M45P02
05-170, 79-22-30

(22)
QTC
5/E
Operation Codes
DE=Delete
QTC=Quantity Change RE=Replace
RM=Remains
Change Codes
5=Qualified interchangeability. Refer to paragraph 1.K., Interchangeability.
Support Codes
A=Old parts will no longer be supplied. E=Old parts will be supplied, and can be used at other engine locations.
D.Parts Disposition
Discard old parts.
E.Tooling - Price and Availability
None.
3.ACCOMPLISHMENT INSTRUCTIONS
A.Removal
(1)Removal instructions of the oil vent manifolds (1, 6, and 05-150, 79-22-30, Figure 1) have not changed. Refer to the GEnx-1B EM, 72-00-02, DISASSEMBLY 002, Subtask 72-00-02-030-429.
B.Installation
(1)Install the insulation blankets in the oil vent manifold (1, Figure 1) as follows:
(a)Install the insulation blanket (2) and insulation blanket (3) on the oil vent manifold (1).
(b)Attach the insulation blankets (2 and 3) with the tiedown straps (straps) (05-170, 79-22-30). Align the ends of the straps.
(c)Install the insulation blanket (05-240) and insulation blanket (05-250) on the oil vent manifold (1). Attach the insulation blankets with straps (05-170).
(d)Install the insulation blanket (05-220) and insulation blanket (05-230) on the oil vent manifold (1). Attach the insulation blankets with straps (05-170).
(e)Install the insulation blanket (05-200) and insulation blanket (05-210) on the oil vent manifold (1). Attach the insulation blankets with a strap (05-170).
(f)Install the insulation blanket (4) and insulation blanket (5) on the oil vent manifold (1). Attach the insulation blankets with straps (05-170).
(2)Install the oil vent manifold (1) on the TCF vent tube (01-570, 72-54-00) as follows:
WARNING:
LUBRICATING OILS MAY CAUSE SKIN, EYE AND RESPIRATORY IRRITATION WITH PROLONGED OR REPEATED CONTACT. USE PROPER PERSONAL PROTECTIVE EQUIPMENT TO PREVENT SKIN AND EYE CONTACT. IF EYE OR SKIN CONTACT OCCURS FLUSH EYES WITH WATER AND/OR WASH SKIN THOROUGHLY WITH SOAP AND WATER.
(a)Apply C02-019 engine oil or C02-023 engine oil to the outer seal (05-351, 79-22-30).
(b)Put the outer seal (05-351) on the oil vent manifold (1).
(c)Put the oil vent manifold (1) and outer seal (05-351) on the TCF vent tube (01-570, 72-54-00).
(d)Attach the oil vent manifold (1) to the TCF vent tube (01-570) with bolts (05-340, 79-22-30), support bracket (05-361), and nuts (05-050).
(e)Torque the nuts (05-050) on the oil vent manifold (1) to 106-124 lb in. (12.0-14.0 N.m).
(3)Install the oil vent tube (05-150) on the oil vent manifold (1). Refer to the GEnx-1B EM, 72-00-02, ASSEMBLY 005, Subtask 72-00-02-440-187.
Installation of the B-Sump Vent System
Figure 1   (Sheet 1)
Installation of the B Sump Vent System
Figure 1   (Sheet 2)
Installation of the B Sump Vent System
Figure 1   (Sheet 3)