GE PROPRIETARY INFORMATION
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This technical data is considered EAR controlled pursuant to 15 CFR Parts 730-774 respectively. Transfer of this data by any means to a Non-US Person, whether in the United States or abroad, without the proper U.S. Government authorization (e.g., License, exemption, NLR, etc.), is strictly prohibited.
Copyright (2013) General Electric Company, U.S.A.
1.PLANNING INFORMATION
A.Effectivity
* * * FOR GEnx-1B54, -1B58, -1B64, -1B67, -1B70, -1B54/P1, -1B58/P1, -1B64/P1, -1B67/P1, -1B70/P1, -1B70/72/P1, -1B70/75/P1, -1B74/75/P1, -1B75/P1
This Service Bulletin has been introduced in production to these GEnx-1B engines:
GEnx-1B engines, serial numbers 956-226 and up.
These serial numbers are the best available data.
The PHS tubehose P/N 2422M64P01, CCC valve head end tubehose P/N 2366M10P01, and oil supply tube P/N 2317M69P01 are affected by this Service Bulletin.
B.Description
This Service Bulletin provides an installation procedure and releases new tubes to replace tube hoses and thus reduces weight.
C.Compliance
Category 7
GE recommends that you do this Service Bulletin at customer's convenience or option.
NOTE:
This Service Bulletin can be accomplished in shop.
D.Concurrent Requirements
None.
E.Reason
(1)Objective:
To introduce new parts and to reduce weight.
(2)Condition:
The current tube hose configuration on the core compartment cooling (CCC) actuation lines and accessory gear box (AGB) main fuel heat exchanger lines has no immediate negative impact on the engine, apart from adding an extra weight of 1.98 lbs (0.90 kg) which can be removed if hoses are changed to tubes.
(3)Cause:
Tube hoses were added for maintainability at early stages of the engine development.
(4)Improvement:
The proposed hard tube designs result in a total weight reduction of 1.98 lbs (0.90 kg) per engine.
(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 propulsor assembly module, you will need approximately 1 man-hour per engine to do the replacement portion of this Service Bulletin.
H.Weight and Balance
The complete compliance with this Service Bulletin decreases weight by 1.98 lb (0.90 kg).
I.References (Use the latest version of these documents)
GEK 9250, Commercial Engine Standard Practices Manual (SPM)
GEK 112851, GEnx-1B Engine Manual (EM)
GEK 112862, GEnx-1B Cleaning, Inspection, and Repair Manual (CIR)
GEK 112863, GEnx-1B System Description Section (SDS)
GEK 112864, GEnx-1B Engine Illustrated Parts Catalog (EIPC)
GEK 112866, GEnx-1B Illustrated Tool and Equipment Manual (ITEM)
NOTE:
The reference documents listed below are for the engine manufacturer's internal use only:
 
CID: 573615, 573686
 
BPP: 11-79-00-05
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
(1)AGB heat exchanger line:
The oil supply tube P/N 2317M69P01 is replaced with the oil supply tube P/N 2519M35G01 and is two way interchangeable.
(2)CCC valve actuation head and rod lines have been introduced as qualified interchangeable:
The PHS tubehose P/N 2422M64P01 is replaced with two tubes: fuel core compartment cooling rod tube (fuel tube) P/N 2519M38G01 and fuel core compartment cooling rod manifold (fuel manifold) P/N 2519M41G01.
The CCC valve head end tubehose P/N 2366M10P01 is replaced with two tubes: fuel core compartment cooling valve tube (fuel tube) P/N 2519M36G01 and fuel core compartment cooling valve tube (fuel tube) P/N 2519M40G01.
The preformed packing P/N J222P013 (SIN 34751) increase in quantity from 3 to 4 and preformed packing J222P013 (SIN 38C51) increase in quantity from 1 to 2. These changes must be done as a complete set on a given engine.
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
 
2519M38G01
(1)
Tube, Fuel - Core Compartment Cooling Rod
11,840.00
(1)
Quote
 
2519M41G01
(1)
Manifold, Fuel - Core Compartment Cooling Rod
3,589.00
(1)
Quote
 
J222P013
(6)
Packing, Preformed
105.00
(50)
30
 
2519M35G01
(1)
Tube, Oil Supply
9,172.00
(1)
Quote
 
2519M36G01
(1)
Tube, Fuel - Core Compartment Cooling Valve
Quote
(X)
Quote
 
2519M40G01
(1)
Tube, Fuel - Core Compartment Cooling Valve
Quote
(X)
Quote
NOTE:
Prices are provided for planning purposes and are subject to change.
(2)Other Spare Parts:
 
Part Number
Qty/ Eng
Part Name
Unit ($) Price
Pkg Qty
Lead Time Days
 
J222P015
(2)
Packing, Preformed
0.95
(50)
30
 
J1215P20
(2)
Gasket, Seal Flange
76.50
(5)
5
 
J1215P17
(2)
Gasket, Seal Flange
54.50
(5)
5
NOTE:
Prices are provided for planning purposes and are subject to change.
(3)Consumables:
 
Code Number
Description
 
C02-019
Engine Oil
 
C02-023
Engine Oil
 
C10-071
Safety Wire
 
C10-143
Safety Cable
B.Industry Support Information
None.
C.Configuration Chart
 
New Part Number
Qty/ Eng
Part Name
Old Part Number/ IPC Location
Qty/ Eng
Op Code
Chg/ Sprt Code
 
2376M20G02-G09
(X)
Propulsor Module Assembly
2376M20G02-G09
(X)
RM
-/-
 
2447M20G01-G03
(X)
Propulsor Module Assembly
2447M20G01-G03
(X)
RM
-/-
 
.2519M38G01
20-120A, 73-11-40

(1)
Tubehose, PHS
(Old Name)
Tube, Fuel - Core Compartment Cooling Rod
(New Name)
(SIN 34700)
.2422M64P01
20-120, 73-11-40

(1)
RE
5/B
 
.2519M41G01
20-125, 73-11-40

(1)
Manifold, Fuel - Core Compartment Cooling Rod
(SIN 34703)
--
(-)
AD
5/-
 
.J222P013
20-210A, 73-11-40

(4)
Packing, Preformed
(SIN 34751)
.J222P013
20-210, 73-11-40

(3)
QTC
5/-
 
.2519M36G01
20-130A, 73-11-40

(1)
Tubehose, CCC Valve Head End
(Old Name)
Tube, Fuel - Core Compartment Cooling Valve
(New Name)
(SIN 38C00)
.2366M10P01
20-130, 73-11-40

(1)
RE
5/B
 
.2519M40G01
20-135, 73-11-40

(1)
Tube, Fuel - Core Compartment Cooling Valve
(SIN 38C02)
--
(-)
AD
5/-
 
.J222P013
20-160A, 73-11-40

(2)
Packing, Preformed
(SIN 38C51)
.J222P013
20-160, 73-11-40

(1)
QTC
5/-
 
2305M70G01-G08
(X)
Accessory Gearbox Module Assembly
2305M70G01-G08
(X)
RM
-/-
 
.2519M35G01
10-380A, 79-22-10

(1)
Tube, Oil Supply
(SIN 44700)
.2317M69P01
10-380, 79-22-10

(1)
RE
2/B
Operation Codes
AD=Add
RE=Replace
RM=Remains
QTC=Quantity Change
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.Disassembly
(1)Remove the PHS tubehose (1, Figure 1, Sheet 2) and the CCC valve head end tubehose (2). Refer to the GEnx-1B EM, 72-00-02, DISASSEMBLY 003, Subtask 72-00-02-030-391.
(2)Remove the oil supply tube/hose (1, Figure 2, Sheet 1). Refer to the GEnx-1B EM 72-00-05, DISASSEMBLY 001, Subtask 72-00-05-030-028.
B.Assembly
(1)Install the fuel manifold (3, Figure 1, Sheet 3), fuel tube (4), fuel tube (5), and fuel tube (6) as follows:
WARNING:
REFER TO THE PRODUCT LABEL AND THE MANUFACTURERS (MATERIAL) SAFETY DATA SHEET FOR INSTRUCTIONS ON THE HAZARDS, STORAGE, SAFE HANDLING AND PROPER USE OF THIS PRODUCT.
(a)Apply C02-019 engine oil or C02-023 engine oil to the preformed packings (20-150, 73-11-40) and preformed packings (20-210).
(b)Install a preformed packing (20-150) on the fuel manifold (3).
(c)Install a preformed packing (20-150) on the manifold (20-230).
(d)Connect the fuel manifold (3) to the hose manifold (20-010).
(e)Attach the fuel manifold (3) to the bracket (20-250) with cushioned loop clamps (cushioned clamp) (20-180) and bolts (20-170).
(f)Attach the fuel manifold (3) to the bracket (20-350) with a cushioned clamp (20-180) and a bolt (20-170).
(g)Connect the manifold (20-230) to the fuel manifold (3).
(h)Attach the manifold (20-230) to the bracket (20-280) with a cushioned clamp (20-180) and a bolt (20-170).
(i)Attach the manifold (20-230) to the bracket (01-060, 75-24-10) with a cushioned clamp (20-310, 73-11-40) and a bolt (20-170).
(j)Attach the fuel manifold (20-230) to the tabs on the tube (30-080) and the tabs on the tube (25-050) with cushioned clamps (20-310) and bolts (20-300).
(k)Install a preformed packing (7) on the fuel tube (3).
(l)Connect the fuel manifold (3) to the fuel tube (4).
(m)Torque the B-nut on the hose manifold (20-010) as follows:
1Torque the B-nut to 55-65 lb ft (75-88 N.m).
2Loosen the B-nut and then torque again to 55-65 lb ft (75-88 N.m).
3Apply a final torque of 55-65 lb ft (75-88 N.m) to the B-nut.
(n)Torque the B-nut on the fuel tube (4) as follows:
1Torque the B-nut to 55-65 lb ft (75-88 N.m).
2Loosen the B-nut and then torque again to 55-65 lb ft (75-88 N.m).
3Apply a final torque of 55-65 lb ft (75-88 N.m) to the B-nut.
(o)Torque the B-nut on the fuel manifold (3) as follows:
1Torque the B-nut to 55-65 lb ft (75-88 N.m).
2Loosen the B-nut and then torque again to 55-65 lb ft (75-88 N.m).
3Apply a final torque of 55-65 lb ft (75-88 N.m) to the B-nut.
(p)Safety the B-nut on the hose manifold (20-010), fuel manifold (3) and fuel tube (4) with C10-071 safety wire or C10-143 safety cable.
(q)Torque the bolts (20-170) to 32-38 lb in. (3.6-4.3 N.m).
(r)Torque the bolts (20-300) to 32-38 lb in. (3.6-4.3 N.m).
WARNING:
REFER TO THE PRODUCT LABEL AND THE MANUFACTURERS (MATERIAL) SAFETY DATA SHEET FOR INSTRUCTIONS ON THE HAZARDS, STORAGE, SAFE HANDLING AND PROPER USE OF THIS PRODUCT.
(s)Apply C02-019 engine oil or C02-023 engine oil to preformed packings (20-160).
(t)Install preformed packings (8) on the fuel tube (5).
(u)Connect the fuel tube (5) to the hose manifold (20-010).
(v)Attach the fuel tube (5) to the bracket (20-250) with cushioned loop clamps (cushioned clamp) (20-200) and bolts (20-190).
(w)Connect the fuel tube (5) to the fuel tube (6).
(x)Torque the B-nut on the hose manifold (20-010) as follows:
1Torque the B-nut to 460-540 lb in. (52.0-61.0 N.m).
2Loosen the B-nut until the B-nut is loose and then apply torque again to 460-540 lb in. (52.0-61.0 N.m).
3Apply a final torque of 460-540 lb in. (52.0-61.0 N.m) to the B-nut.
(y)Torque the B-nut on the fuel tube (6) as follows:
1Torque the B-nut to 55-65 lb ft (75-88 N.m).
2Loosen the B-nut and then torque again to 55-65 lb ft (75-88 N.m).
3Apply a final torque of 55-65 lb ft (75-88 N.m) to the B-nut.
(z)Safety the B-nut on the hose manifold (20-010) and fuel tube (6) with C10-071 safety wire or C10-143 safety cable.
(aa)Torque the bolts (20-190) to 32-38 lb in. (3.6-4.3 N.m).
(2)Install the oil supply tube/hose (1, Figure 2). Refer to GEnx-1B EM, 72-00-05, ASSEMBLY 001, Subtask 72-00-05-430-022.
Installation of the Fuel Hydraulic System
Figure 1   (Sheet 1)
Installation of the Fuel Hydraulic System
Figure 1   (Sheet 2)
Installation of the Fuel Hydraulic System
Figure 1   (Sheet 3)
Installation of the Fuel Hydraulic System
Figure 1   (Sheet 4)
Installation of the Fuel Hydraulic System
Figure 1   (Sheet 5)
Installation of the Oil Supply Tube/Hose
Figure 2   (Sheet 1)
Installation of the Oil Supply Tube/Hose
Figure 2   (Sheet 2)