 | GEnx-1B SERVICE BULLETIN - 73-0054 R01 | Revised: 05/26/2017 |
| SB 73-0054 R01 ENGINE FUEL AND CONTROL - Electronic Engine Control (73-21-20) - Release of EEC Software (Version B195) | Issued: 05/19/2017 | |
| GEnx-1B SERVICE BULLETIN - 73-0054 R01 | Revised: 05/26/2017 |
| SB 73-0054 R01 ENGINE FUEL AND CONTROL - Electronic Engine Control (73-21-20) - Release of EEC Software (Version B195) | Issued: 05/19/2017 | |
| GE PROPRIETARY INFORMATION | |
| The information contained in this document is GE proprietary information and is disclosed in confidence. It is the property of GE and shall not be used, disclosed to others or reproduced without the express written consent of GE, including, but without limitation, it is not to be used in the creation, manufacture, development, or derivation of any repairs, modifications, spare parts, designs, or configuration changes or to obtain FAA or any other government or regulatory approval to do so. If consent is given for reproduction in whole or in part, this notice and the notice set forth on each page of this document shall appear in any such reproduction in whole or in part. | |
| 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. |
| TRANSMITTAL INFORMATION |
| REVISION 1 TO SERVICE BULLETIN 73-0054 |
| Revision 1 is issued to update paragraphs 1.A., Effectivity, 1.C., Compliance, 2.C., Configuration Chart, and 4., APPENDIX A - EEC REPROGRAMMING AND NVM RETRIEVAL. |
| The original was issued May 19, 2017. 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, 1B76A/P2 |
| This Service Bulletin has been introduced in production to these GEnx-1B engines: |
| • |
|
| These serial numbers are the best available data. |
| This Service Bulletin is applicable to all GEnx-1B engines. |
| The electronic engine control (EEC) software (version B190) P/N 2124M23P22 and earlier are affected by this Service Bulletin. |
| B. | Description |
| This Service Bulletin releases the new EEC software (version B195) P/N 2124M23P23 and provides reprogramming instructions. |
| C. | Compliance |
| Category 2 |
| GE recommends that you do this Service Bulletin as soon as possible without effect on revenue service but before 30 days from the original Service Bulletin date issued May 19, 2017. |
| Impact C |
| This recommendation is to address a condition that may result in a Non-Event operational disruption, Unscheduled Engine Removals (UER), Out-Station-Removals or Aircraft on the Ground (AOG). |
| NOTE: |
|
| 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. |
| (2) | Condition: |
| Improvements to the EEC software have been identified. |
| (3) | Cause: |
| Revenue service experience has identified opportunities for the EEC software improvements. |
| (4) | Improvement: |
| The following changes are included in the EEC software (version B195): |
| • |
|
| • |
|
| • |
|
| (5) | Substantiation: |
| Substantiation is by analysis, 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 EEC, you will need approximately 1.0 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 114001, GEnx-1B Component Maintenance Manual (CMM) 73-21-50 |
| NOTE: |
|
| J. | Publications Affected |
| GEK 112864, GEnx-1B Engine Illustrated Parts Catalog (EIPC) |
| K. | Interchangeability |
| One-way interchangeable. |
| NOTE: |
|
| 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 |
| *Part not supplied by GE Engine Services Distribution L.L.C. To procure parts, contact the following: |
| FADEC International C/O BAE Systems Controls ATTN: Manager Spare Parts Sales P.O. Box 2232 Fort Wayne, IN 46801-2232 U.S.A. |
| Phone: (260) 434-5664 Fax: (260) 434-5616 |
| NOTE: |
|
| NOTE: |
|
| (2) | Other Spare Parts: |
| None. |
| (3) | Consumables: |
| None. |
| B. | Industry Support Information |
| None. |
| C. | Configuration Chart |
|
| Operation Codes RM=Remains RW=Rework SU=Superseded |
| Change Codes 1=One-way interchangeable. |
| Support Codes A=Old parts will no longer be supplied. |
| D. | Parts Disposition |
| Rework. |
| E. | Tooling - Price and Availability |
|
| NOTE: |
|
| (1) | Operators performing the EEC software reprogramming procedure must request the following master CD-ROM from BAE Systems Controls Product Support Engineering: |
|
| NOTE: |
|
| 3. | ACCOMPLISHMENT INSTRUCTIONS |
| A. | General |
| (1) | EEC onboard flight deck reprogramming procedure: |
| (a) | Start the onboard loadable software (LSAP). Refer to the GEnx-1B Boeing 787 AMM, TASK DMC-B787-A-45-13-00-02A-110B-A, Start the Onboard Data Load Function - Software Operation. |
| (b) | Load the software to the EEC. Refer to the GEnx-1B Boeing 787 AMM, TASK DMC-B787-A-G73-21-05-00B-750A-A, Electronic Engine Control (with Onboard Data Load Function) - Software Installation. |
| (c) | Start the CMC. Refer to the GEnx-1B Boeing 787 AMM, TASK DMC-B787-A-45-11-00-00A-110B-A, Central Maintenance Computing Function - Software Operation. |
| (d) | Examine the software configuration. Refer to the GEnx-1B Boeing 787 AMM, TASK DMC-B787-A-45-11-00-02A-300D-A, Airplane Component with Loadable Software - Software Check. |
| NOTE: |
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| NOTE: |
|
| (2) | Engine shop reprogramming and verification procedure: |
| (a) | Prepare a 615 working copy disk of the software. Refer to the instructions embedded on CD-ROM P/N 362A9836P16. |
| (b) | Reprogram the EEC with the PDL reprogramming disk working copy. Refer to Figure 1, paragraph 4., APPENDIX A - EEC REPROGRAMMING AND NVM RETRIEVAL, and GEnx-1B EM, 72-00-00, SPECIAL PROCEDURE 001. |
| (3) | EEC shop reprogramming and verification procedure: |
| (a) | Prepare a 615 working copy disk of the software. Refer to the instructions embedded on CD-ROM P/N 362A9836P16. |
| (b) | Reprogram the EEC with the PDL reprogramming disk working
copy. Refer to the GEnx-1B CMM, 73-21-50, APPENDIX
A - EEC REPROGRAMMING AND NVM RETRIEVAL and paragraph 4., APPENDIX A - EEC REPROGRAMMING AND NVM RETRIEVAL. |
| 4. | APPENDIX A - EEC REPROGRAMMING AND NVM RETRIEVAL |
| EEC/GSE Software Configuration |
| GE Software Part Number: 2124M23P23 |
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