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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 (2017) General Electric Company, U.S.A.
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, -1B76A/P2
This Service Bulletin is applicable to all GEnx-1B engines.
This Service Bulletin has been introduced in production to these GEnx-1B engines:
GEnx-1B engines, serial numbers 958-032 and up.
These serial numbers are the best available data.
The engine monitoring unit (EMU) software VIN 271-127-981-004 (P/N 2462M81P04) and VIN 271-127-982-004 (P/N 2462M82P04) are affected by this Service Bulletin.
B.Description
This Service Bulletin introduces new EMU software EA65 VIN 271-127-981-005 (P/N 2462M81P05) and VIN 271-127-982-005 (P/N 2462M82P05) and provides the EMU reprogramming instructions.
C.Compliance
Category 2
GE recommends that you do this Service Bulletin as soon as possible without effect on revenue service but within 12 months from this Service Bulletin issue date.
Impact E
This recommendation is to improve the cost of ownership, reduce maintenance requirements or is a product improvement.
NOTE:
This Service Bulletin can be accomplished on wing or 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 parts, improve maintainability, update the current EMU software version, and correct a mistake in the previous software version drawing.
(2)Condition:
Improvements to the current EMU software have been identified.
(3)Cause:
The current EA57 version of the software requires logic changes in order to address EMU functional updates.
(4)Improvement:
The new software EA65 improvements are as follows:
Update of the high speed engine serial bus (HSESB) input definition so the EMU can retrieve new parameters.
Diagnostic data indicating root cause has been added to the common data network (CDN) faults.
Engine and aircraft oil level filter data in the flight phases post-flight summary (PFS) additions.
Update of the aircraft communication addressing and reporting system (ACARS) reports with the new content to enhance the analytical capabilities.
Water wash counting events addition to the takeoff report.
Use turbine center frame (TCF) accelerometers to monitor the fuel couple dynamic vibrations.
Simplification of the balancing instructions to avoid extra re-flight.
Removal of the gas path report ACARS transmission due to no value for diagnostics.
Addition of position information and true heading to the ACARS reports.
Fix trim balance keep weight command to prevent storage of invalid data.
Change transmission of the takeoff report to the end of the takeoff phase.
Updates in compressed engine data (CED) file to add header and pilot and main fuel modes parameters.
Improvement of the CED compression algorithm.
Creation of exceedance reports for the study of anomalies during flight.
Creation of logic to predict hardware damages based on the temperature at the engine station 3 (T3) and exhaust gas temperature (EGT) data.
Improvement of the stable cruise report with a snapshot trigger of more stable data.
Addition of recording vibe data from the accelerometers 1 and 2 to monitor the gearbox vibes.
Independent identification number for each full flight data (FFD) files to avoid maintenance laptop operation failures.
Automatic wireless transmission of continuous engine operation data (CEOD) and CED data files at the end of the flight to speed transmission on ground.
Separation of level E and level C software for improved release control.
Integration of header to the FFD report.
Addition of version number to the non-volatile memory (NVM) files and redefinition of NVM file functions.
To include new full authority digital electronic control (FADEC), EMU, and aircraft data in the FFD.
Fix of lube event report content.
Crew information system (CIS) responses were delayed, causing the EMU to not correctly transmit data (application software).
Engine position fixes for the engine indication crew alerting system (EICAS) display.
If only one CDN bus has failed, maintenance fault logic will not blank the EICAS display.
(5)Substantiation:
Substantiation is by comparative analysis and test.
F.Approval
The data contained in this Service Bulletin has been reviewed by the FAA or authorized entity representing the FAA and the repair(s) and modification(s) herein comply with the applicable Aviation Regulations and are APPROVED for installation in the model(s) listed in this Service Bulletin.
G.Manpower
After you get access to the EMU, you will need approximately 1 man-hour for each engine or component.
H.Weight and Balance
Weight and balance are not changed.
I.References (Use the latest version of these documents)
GEnx-1B, Boeing 787 Aircraft Maintenance Manual (AMM)
GEK 112851, GEnx-1B Engine Manual (EM)
GEK 112864, GEnx-1B Engine Illustrated Parts Catalog (EIPC)
GEK 114063, GEnx-1B Component Maintenance Manual (CMM), 77-35-03
NOTE:
The reference documents listed below are for the engine manufacturer's internal use only:
CID: 575952
BPP/EPEX No.: 16-71-00-55373.A
J.Publications Affected
GEK 112864, GEnx-1B Engine Illustrated Parts Catalog (EIPC)
K.Interchangeability
One-way interchangeable.
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
 
VIN 271-127-981-005*
(2462M81P05)
(GEC4F-2462-8105)**
(1)
Software
(Level C SW - Part 1)
NP
(-)
--
 
VIN 271-127-982-005*
(2462M82P05)
(GEC4C-2462-8205)**
(1)
Software
(Level E SW - Part 2)
NP
(-)
--
NP = Not Provisioned
NOTE:
Prices are provided for planning purposes and are subject to change.
*Part not supplied by GE Engine Services Distribution L.L.C. To procure parts, contact the following:
Meggitt Aerospace Spares Department Meggitt S.A.
Route de Moncor 4 P.O. Box 1616 CH-1701 Fribourg Switzerland
OR
Fax: +(41) (26) 407 1555 Phone: +(41) (26) 407 1352
OR
E-mail: csssales.emea@meggitt.com
**Boeing part number.
(2)Other Spare Parts:
None.
(3)Consumables:
None.
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
 
GEnx-1B64G03/
G04
(X)
GEnx Model
GEnx-1B64G03/
G04
(X)
RM
-/-
 
GEnx-1B64/P1G01/
P2G01/P2G02
(X)
GEnx Model
GEnx-1B64/P1G01/
P2G01/P2G02
(X)
RM
-/-
 
GEnx-1B67G03/
G04
(X)
GEnx Model
GEnx-1B67G03/
G04
(X)
RM
-/-
 
GEnx-1B67/P1G01/
P2G01/P2G02
(X)
GEnx Model
GEnx-1B67/P1G01/
P2G01/P2G02
(X)
RM
-/-
 
GEnx-1B70G03/
G04
(X)
GEnx Model
GEnx-1B70G03/
G04
(X)
RM
-/-
 
GEnx-1B70/P1G01/
P2G01/P2G02
(X)
GEnx Model
GEnx-1B70/P1G01/
P2G01/P2G02
(X)
RM
-/-
 
GEnx-1B70C/P1G01/
P2G01/P2G02
(X)
GEnx Model
GEnx-1B70C/P1G01/
P2G01/P2G02
(X)
RM
-/-
 
GEnx-1B70/75/P1G01/
P2G01/P2G02
(X)
GEnx Model
GEnx-1B70/75/P1G01/
P2G01/P2G02
(X)
RM
-/-
 
GEnx-1B74/75/P1G01/
P2G01/P2G02
(X)
GEnx Model
GEnx-1B74/75/P1G01/
P2G01/P2G02
(X)
RM
-/-
 
GEnx-1B76A/P2G01
(X)
GEnx Model
GEnx-1B76A/P2G01
(X)
RM
-/-
 
.738L787G05
01-050D, 77-32-10

(1)
EMU Kit
(SIN 00040)
.738L787G04
01-050C, 77-32-10

(1)
RW
5/A
 
..VIN 271-127-981-005
(2462M81P05)
01-070D, 77-32-10

(1)
Software
(SIN 66H06)
..VIN 271-127-981-004
(2462M81P04)
01-070C, 77-32-10

(1)
RE
5/A
 
..VIN 271-127-982-005
(2462M82P05)
01-080D, 77-32-10

(1)
Software
(SIN 66H07)
..VIN 271-127-982-004
(2462M82P04)
01-080C, 77-32-10

(1)
RE
5/A
Operation Codes
RE=Replace
RM=Remains
RW=Rework
Change Codes
5=Qualified interchangeability. Refer to paragraph 1.K., Interchangeability.
Support Codes
A=Old parts will no longer be supplied.
D.Parts Disposition
Rework.
E.Tooling - Price and Availability
 
Tool Number
Description
 
PMAT 2000
Portable Maintenance Access Terminal
(PMAT)
 
11C4299
Cable, Reprogramming EMU
 
See NOTES
CD-ROM Reprogramming Retrieve Software
NOTE:
Tooling and CD-ROM only required for shop/bench loading of the software.
NOTE:
To perform the EMU shop/bench reprogramming, CD-ROM disks are provided on request from Meggitt Aerospace Spares Department as listed in Material Information.
3.ACCOMPLISHMENT INSTRUCTIONS
A.General
(1)For the EMU (Figure 1) on-board flight deck reprogramming procedures, do as follows:
CAUTION:
THE EMU (FIGURE 1) MUST NOT BE POWERED OFF WHILE THE INSTALLATION IS IN PROGRESS. IF THE EMU IS POWERED OFF, IT WILL BE UNABLE TO BE PROGRAMMED.
(a)Install the new software on the EMU (Figure 1) with the on-board data load function. Refer to the GEnx-1B Boeing 787 AMM, 77-31-01, TASK B787-A-G77-31-01-00B-750A-A.
NOTE:
The operator can get the on-board software loadable software airplane part (LSAP) through the Boeing software library. Refer to paragraph 2., MATERIAL INFORMATION for the Boeing part numbers.
NOTE:
It will take several minutes (up to 15 minutes) for the EMU (Figure 1) to complete the software installation. The software installation will be complete when the cockpit vibration display is populated. While the installation is in progress, the cockpit vibration display, cockpit vibration data on the Performance Maintenance Data Page, and the EMU Maintenance Data Page will be blank. After the cockpit vibration display is populated, the B787 System Configuration Page can be examined.
(2)For the EMU (Figure 1) reprogramming and verification procedure at the engine shop, do as follows:
(a)Install the new software. Refer to the GEnx-1B EM, 72-00-00, SPECIAL PROCEDURE 005.
(3)For the EMU (Figure 1) reprogramming and verification procedure at the EMU shop, do as follows:
(a)Install the new software. Refer to the GEnx-1B CMM, 77-35-03, SPECIAL PROCEDURES, paragraph 5., Installation of the GE Application Software
.
EMU Location
Figure 1  
4.APPENDIX A
 
Software Supplier:
GE Aviation
One Neumann Way
Cincinnati, OH 45215
U.S.A.
 
Engine Model:
GEnx-1B
 
Software Item(s):
Application Software, OS
 
Software Version:
EA65
 
Software Build Number:
138
 
Software Quality Level:
Production
 
Release Date:
5/18/2017
 
GE Software Part Number(s):
2462M81P05, 2462M82P05
 
OEM Software Part Number:
See Material Information
 
Airframer Part Number(s):
GEC4F-2462-8105, GEC4C-2462-8205
 
GE Hardware Drawing:
2122M32
 
Files:
 
EA65_PART1
 
Load Disk for ARINC 615
 
AFDX, VSM, CPM OS, Level C AS
 
Loader Configuration File
config.ldr
 
OS Software (AFDX) ARINC 615 Load File
AFDX502.615
 
OS Software (CPM CPU 1) ARINC 615 Load File
CPU1_046.615
 
OS Software (CPM CPU 2) ARINC 615 Load File
CPU2_046.615
 
OS Software (VSM) ARINC 615 Load File
VD01.615
 
AS Software (AS1) ARINC 615 Load File
EA65AS1.615
 
AS Software (AS2) ARINC 615 Load File
EA65AS2.615
 
 
Load Disk for ARINC 615A (Note: Compatible with P08 and future hardware only)
 
AFDX, VSM, CPM OS, Level C AS
 
615A Loadable Upload Part Header File
GEC4F24628105.LUH
 
OS Software (AFDX) ARINC 615A Load File
AFDX502.LUP
 
OS Software (CPM CPU 1) ARINC 615A Load File
CPU1_046.LUP
 
OS Software (CPM CPU 2) ARINC 615A Load File
CPU2_046.LUP
 
OS Software (VSM) ARINC 615A Load File
VD01.LUP
 
AS Software (AS1) ARINC 615A Load File
EA65AS1.LUP
 
AS Software (AS2) ARINC 615A Load File
EA65AS2.LUP
 
 
EA65_PART2
 
Load Disk for ARINC 615_123
 
Level E AS
 
Loader Configuration File
config.ldr
 
AS Software (AS4) ARINC 615 Load File
EA65AS4.615
 
AS Software (AS5) ARINC 615 Load File
EA65AS5.615
 
AS Software (AS7) ARINC 615 Load File
EA65AS7.615
 
 
Load Disk for ARINC 615A (Note: Compatible with P08 and future hardware only)
 
Level E AS
 
615A Loadable Upload Part Header File
GEC4C24628205.LUH
 
AS Software (AS4) ARINC 615A Load File
EA65AS4.LUP
 
AS Software (AS5) ARINC 615A Load File
EA65AS5.LUP
 
AS Software (AS7) ARINC 615A Load File
EA65AS7.LUP
 
 
EA65_RIG
 
Rig Files
 
Adjustment File
adf-EA65.xml
 
Monitoring File
mdf-EA65.xml
 
ARINC 429 Monitoring Primary FM List
cfg-EA65.xml
 
AFDX Configuration File
afdx-EA65.xml