# Boeing Alert Service Bulletin 747-28A2280: Revision 1 - Rights: © The Boeing Company. Filed by the FAA in regulations.gov docket FAA-2009-0454; AD 2010-14-08 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. - Document: [Boeing Alert Service Bulletin 747-28A2280](https://openairdocs.org/service-documents/boeing/747-28a2280.md) - Title as filed: The Boeing Company - Service Bulletin - Pages: 1162 - PDF: https://openairdocs.org/files/sha256/f8/ad/f8ad0efae5b647179c67a66415e3cf889a15e3b93cc9afae8e35e511a92c07c7 - Page: https://openairdocs.org/service-documents/boeing/747-28a2280/file/f8ad0efae5b6 ## Text Some pages are OCR from a scan. OCR can misread letters and numbers. Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 1 of 1162 Commercial Airplanes 747 Service Bulletin Number: 747-28A2280 Original Issue: August 07, 2008 Revision 1: November 25, 2009 ATA System: 2831 SUBJECT: FUEL - Fuel Jettison System - Center Tank Override/Jettison Fuel Pumps - Main 2 and Main 3 Tank Override/Jettison Fuel Pumps - Change to Give Redundant Control of the Fuel Pumps BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET Copyright © 2008 The Boeing Company Unpublished Work - All Rights Reserved Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable subject matter. Boeing also claims copyright in this document as a compilation and/or collective work. This document includes proprietary information owned by The Boeing Company and/or one or more third parties. Treatment of the document and the information it contains is governed by contract with Boeing. For more information, contact The Boeing Company, P.O. Box 3707, Seattle, Washington 98124. Boeing, 707, 717, 727, 737, 747, 757, 767, 777, BBJ, BOEING BUSINESS JET, DC-8, DC-9, DC-10, MD-10, MD-11, MD-80, MD-90, the Boeing logo and the Boeing livery are among the trademarks owned by Boeing or its subsidiaries. No intellectual property license (express or implied) is granted in connection with this document or otherwise. ### Page 2 BLANK PAGE Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 2 of 1162 BOEING SERVICE BULLETIN 747-28A2280 BLANK PAGE ### Page 3 Table of Contents Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 3 of 1162 BOEING SERVICE BULLETIN 747-28A2280 Table of Contents Revision Transmittal Sheet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13 1. PLANNING INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17 A. Effectivity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17 1. Airplanes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17 2. Spares Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 46 B. Concurrent Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 46 C. Reason . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47 D. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 48 E. Compliance. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 48 F. Approval . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49 G. Manpower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 49 H. Weight and Balance Changes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 50 I. Electrical Load Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 50 J. References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 51 1. Existing Data: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 51 2. Data supplied with this Service Bulletin: . . . . . . . . . . . . . . . . . . . . . . . . . 51 3. Installation Drawings Used in the Preparation of this Service Bulletin: . . . . . . . . . . 52 K. Publications Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 53 L. Interchangeability and Intermixability of Parts . . . . . . . . . . . . . . . . . . . . . . . . . 53 2. MATERIAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 55 A. Material - Price and Availability. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 55 B. Industry Support Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61 C. Parts Necessary For Each Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61 1. Kits/Parts: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61 2. Parts and Materials Supplied by the Operator: . . . . . . . . . . . . . . . . . . . . . . 251 3. Parts Modified and Reidentified: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 251 4. Parts Removed and Not Replaced: . . . . . . . . . . . . . . . . . . . . . . . . . . . . 251 D. Parts Necessary to Change Spares . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 251 E. Special Tooling - Price and Availability. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 252 F. Special Tooling Necessary to do this Service Bulletin . . . . . . . . . . . . . . . . . . . . . 252 3. ACCOMPLISHMENT INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 253 A. GENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 253 B. WORK INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 54 FIGURE 1: P914 RELAY PANEL SUPPORT BRACKET - INSTALLATION. . . . . . . . . . . . . . . 397 FIGURE 2: P915 RELAY PANEL SUPPORT BRACKET - INSTALLATION. . . . . . . . . . . . . . . 401 FIGURE 3: MAIN EQUIPMENT CENTER - P914 RELAY PANEL - INSTALLATION . . . . . . . . . . 405 FIGURE 4: MAIN EQUIPMENT CENTER - P915 RELAY PANEL - INSTALLATION . . . . . . . . . . 409 FIGURE 5: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . . . 413 FIGURE 6: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . . . 419 FIGURE 7: MAIN EQUIPMENT CENTER - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . 425 FIGURE 8: MAIN EQUIPMENT CENTER - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . 454 FIGURE 9: MAIN EQUIPMENT CENTER - P414-1 PANEL - WIRING CHANGE . . . . . . . . . . . 486 FIGURE 10: MAIN EQUIPMENT CENTER - P414 PANEL - WIRING CHANGE . . . . . . . . . . . . 489 FIGURE 11: MAIN EQUIPMENT CENTER - P414 PANEL - WIRING CHANGE . . . . . . . . . . . . 494 ### Page 4 Table of Contents Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 4 of 1162 BOEING SERVICE BULLETIN 747-28A2280 FIGURE 12: MAIN EQUIPMENT CENTER - P414 PANEL - WIRING CHANGE . . . . . . . . . . . 499 FIGURE 13: MAIN EQUIPMENT CENTER - P414 PANEL - WIRING CHANGE . . . . . . . . . . . 504 FIGURE 14: MAIN EQUIPMENT CENTER - P415-1 PANEL - WIRING CHANGE . . . . . . . . . . 509 FIGURE 15: MAIN EQUIPMENT CENTER - P415 PANEL - WIRING CHANGE . . . . . . . . . . . 512 FIGURE 16: MAIN EQUIPMENT CENTER - P415 PANEL - WIRING CHANGE . . . . . . . . . . . 517 FIGURE 17: MAIN EQUIPMENT CENTER - P414 PANEL - WIRING CHANGE . . . . . . . . . . . 522 FIGURE 18: MAIN EQUIPMENT CENTER - P415 PANEL - WIRING CHANGE . . . . . . . . . . . 527 FIGURE 19: MAIN EQUIPMENT CENTER - P415 PANEL - WIRING CHANGE . . . . . . . . . . . 532 FIGURE 20: MAIN EQUIPMENT CENTER - P414 PANEL - WIRING CHANGE . . . . . . . . . . . 537 FIGURE 21: MAIN EQUIPMENT CENTER - P180 PANEL - WIRING CHANGE . . . . . . . . . . . 542 FIGURE 22: MAIN EQUIPMENT CENTER - P180 PANEL - WIRING CHANGE . . . . . . . . . . . 546 FIGURE 23: MAIN EQUIPMENT CENTER - P414 PANEL - WIRING CHANGE . . . . . . . . . . . 550 FIGURE 24: MAIN EQUIPMENT CENTER - E2-6 SHELF - WIRING CHANGE . . . . . . . . . . . . 555 FIGURE 25: MAIN EQUIPMENT CENTER - E2-6 SHELF - WIRING CHANGE . . . . . . . . . . . . 558 FIGURE 26: MAIN EQUIPMENT CENTER - E2-6 SHELF - WIRING CHANGE . . . . . . . . . . . . 561 FIGURE 27: MAIN EQUIPMENT CENTER - E2-6 SHELF - WIRING CHANGE . . . . . . . . . . . . 564 FIGURE 28: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 567 FIGURE 29: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 569 FIGURE 30: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 571 FIGURE 31: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 573 FIGURE 32: OVERRIDE/JETTISON PUMPS - MAIN 3 FORWARD - WIRING CHANGE . . . . . . . 575 FIGURE 33: OVERRIDE/JETTISON PUMPS - MAIN 3 FORWARD - WIRING CHANGE . . . . . . . 577 FIGURE 34: OVERRIDE/JETTISON PUMPS - MAIN 3 FORWARD - WIRING CHANGE . . . . . . . 579 FIGURE 35: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGE . . . . . . . 581 FIGURE 36: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGE . . . . . . . 586 FIGURE 37: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 589 FIGURE 38: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 591 FIGURE 39: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 593 FIGURE 40: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 595 FIGURE 41: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 597 FIGURE 42: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 598 FIGURE 43: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 599 FIGURE 44: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 600 FIGURE 45: OVERRIDE/JETTISON PUMPS - WIRING CHANGES . . . . . . . . . . . . . . . . . 602 FIGURE 46: OVERRIDE/JETTISON PUMPS - WIRING CHANGES . . . . . . . . . . . . . . . . . 604 FIGURE 47: OVERRIDE/JETTISON PUMPS - WIRING CHANGES . . . . . . . . . . . . . . . . . 605 FIGURE 48: OVERRIDE/JETTISON PUMPS - WIRING CHANGES . . . . . . . . . . . . . . . . . 607 FIGURE 49: OVERRIDE/JETTISON PUMPS - WIRING CHANGES . . . . . . . . . . . . . . . . . 609 FIGURE 50: OVERRIDE/JETTISON PUMPS - WIRING CHANGES . . . . . . . . . . . . . . . . . 611 ### Page 5 Table of Contents Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 5 of 1162 BOEING SERVICE BULLETIN 747-28A2280 FIGURE 51: OVERRIDE/JETTISON PUMPS - MAIN 2 AFT - WIRING CHANGES . . . . . . . . . . 612 FIGURE 52: OVERRIDE/JETTISON PUMPS - MAIN 2 AFT - WIRING CHANGES . . . . . . . . . . 614 FIGURE 53: OVERRIDE/JETTISON PUMPS - MAIN 2 AFT - WIRING CHANGES . . . . . . . . . . 616 FIGURE 54: OVERRIDE/JETTISON PUMPS - MAIN 2 AFT - WIRING CHANGES . . . . . . . . . . 618 FIGURE 55: OVERRIDE/JETTISON PUMPS - MAIN 2 AFT - WIRING CHANGES . . . . . . . . . . 620 FIGURE 56: OVERRIDE/JETTISON PUMPS - MAIN 3 AFT - WIRING CHANGES . . . . . . . . . . 622 FIGURE 57: OVERRIDE/JETTISON PUMPS - MAIN 3 AFT - WIRING CHANGES . . . . . . . . . . 624 FIGURE 58: OVERRIDE/JETTISON PUMPS - MAIN 3 AFT - WIRING CHANGES . . . . . . . . . . 626 FIGURE 59: OVERRIDE/JETTISON PUMPS - MAIN 2 AFT - WIRING CHANGES . . . . . . . . . . 628 FIGURE 60: OVERRIDE/JETTISON PUMPS - MAIN 2 AFT - WIRING CHANGES . . . . . . . . . . 630 FIGURE 61: OVERRIDE/JETTISON PUMPS - MAIN 3 AFT - WIRING CHANGES . . . . . . . . . . 632 FIGURE 62: OVERRIDE/JETTISON PUMPS - MAIN 3 AFT - WIRING CHANGES . . . . . . . . . . 634 FIGURE 63: OVERRIDE/JETTISON PUMPS - MAIN 3 AFT - WIRING CHANGES . . . . . . . . . . 636 FIGURE 64: OVERRIDE/JETTISON PUMPS - MAIN 3 AFT - WIRING CHANGES . . . . . . . . . . 638 FIGURE 65: OVERRIDE/JETTISON PUMPS - MAIN 3 AFT - WIRING CHANGES . . . . . . . . . . 640 FIGURE 66: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGES. . . . . . . 642 FIGURE 67: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGES. . . . . . . 645 FIGURE 68: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGES. . . . . . . 651 FIGURE 69: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGES. . . . . . . 653 FIGURE 70: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGES. . . . . . . 655 FIGURE 71: OVERRIDE/JETTISON PUMPS - WIRING CHANGES . . . . . . . . . . . . . . . . . . 657 FIGURE 72: OVERRIDE/JETTISON PUMPS - WIRING CHANGES . . . . . . . . . . . . . . . . . . 659 FIGURE 73: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGES. . . . . . . 661 FIGURE 74: FUEL JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . 663 FIGURE 75: OVERRIDE/JETTISON PUMPS - MAIN 3 FORWARD - WIRING CHANGE . . . . . . . 665 FIGURE 76: OVERRIDE/JETTISON PUMPS - MAIN 3 FORWARD - WIRING CHANGE . . . . . . . 667 FIGURE 77: OVERRIDE/JETTISON PUMPS - MAIN 3 FORWARD - WIRING CHANGE . . . . . . . 669 FIGURE 78: OVERRIDE/JETTISON PUMPS - MAIN 3 FORWARD - WIRING CHANGE . . . . . . . 671 FIGURE 79: OVERRIDE/JETTISON PUMPS - MAIN 3 FORWARD - WIRING CHANGE . . . . . . . 673 FIGURE 80: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .6 7 5 FIGURE 81: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .6 7 6 FIGURE 82: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .6 7 7 FIGURE 83: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .6 7 9 FIGURE 84: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .6 8 1 FIGURE 85: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .6 8 2 FIGURE 86: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .6 8 3 FIGURE 87: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .6 8 4 FIGURE 88: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .6 8 5 ### Page 6 Table of Contents Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 6 of 1162 BOEING SERVICE BULLETIN 747-28A2280 FIGURE 89: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 686 FIGURE 90: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 687 FIGURE 91: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 688 FIGURE 92: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 689 FIGURE 93: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 690 FIGURE 94: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 691 FIGURE 95: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 692 FIGURE 96: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 693 FIGURE 97: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 694 FIGURE 98: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 696 FIGURE 99: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 698 FIGURE 100: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 700 FIGURE 101: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 702 FIGURE 102: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 704 FIGURE 103: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 706 FIGURE 104: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 708 FIGURE 105: FUEL JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . 710 FIGURE 106: OVERRIDE/JETTISON PUMPS - MAIN 3 FORWARD - WIRING CHANGE . . . . . . 711 FIGURE 107: FUEL JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . 713 FIGURE 108: FUEL JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . 715 FIGURE 109: FUEL JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . 717 FIGURE 110: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 718 FIGURE 111: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 720 FIGURE 112: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 722 FIGURE 113: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 724 FIGURE 114: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 728 FIGURE 115: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 730 FIGURE 116: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 732 FIGURE 117: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 736 FIGURE 118: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 741 FIGURE 119: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 746 FIGURE 120: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 751 FIGURE 121: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 756 FIGURE 122: FUEL LOW PRESSURE WARNING - BOOSTER PUMPS - OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 761 FIGURE 123: FUEL LOW PRESSURE WARNING - BOOSTER PUMPS - OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 763 FIGURE 124: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 765 ### Page 7 Table of Contents Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 7 of 1162 BOEING SERVICE BULLETIN 747-28A2280 FIGURE 125: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7 7 1 FIGURE 126: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7 7 7 FIGURE 127: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7 8 3 FIGURE 128: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7 8 9 FIGURE 129: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7 9 5 FIGURE 130: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 0 1 FIGURE 131: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 0 7 FIGURE 132: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 1 3 FIGURE 133: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 1 9 FIGURE 134: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 2 5 FIGURE 135: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 3 1 FIGURE 136: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 3 7 FIGURE 137: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 4 3 FIGURE 138: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 4 9 FIGURE 139: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 5 5 FIGURE 140: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 6 1 FIGURE 141: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 6 7 FIGURE 142: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 7 3 FIGURE 143: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 7 9 FIGURE 144: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 8 5 FIGURE 145: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 9 1 FIGURE 146: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 9 7 FIGURE 147: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 903 FIGURE 148: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 904 FIGURE 149: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 905 FIGURE 150: OVERRIDE/JETTISON PUMPS - MAIN 2 AFT - WIRING CHANGE. . . . . . . . . . . 906 FIGURE 151: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING ### Page 8 Table of Contents Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 8 of 1162 BOEING SERVICE BULLETIN 747-28A2280 CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 908 FIGURE 152: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 910 FIGURE 153: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 911 FIGURE 154: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 912 FIGURE 155: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 914 FIGURE 156: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 915 FIGURE 157: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 916 FIGURE 158: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 918 FIGURE 159: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 919 FIGURE 160: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 920 FIGURE 161: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 922 FIGURE 162: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 924 FIGURE 163: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 926 FIGURE 164: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 928 FIGURE 165: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 930 FIGURE 166: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 932 FIGURE 167: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 934 FIGURE 168: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGE . . . . . . 936 FIGURE 169: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGE . . . . . . 938 FIGURE 170: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGE . . . . . . 940 FIGURE 171: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGE . . . . . . 942 FIGURE 172: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGE . . . . . . 944 FIGURE 173: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGE . . . . . . 946 FIGURE 174: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGE . . . . . . 948 FIGURE 175: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 950 FIGURE 176: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 952 FIGURE 177: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 954 FIGURE 178: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 956 FIGURE 179: OVERRIDE/JETTISON PUMPS - WIRING CHANGE. . . . . . . . . . . . . . . . . . 958 FIGURE 180: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGE . . . . . . 960 FIGURE 181: FUEL LOW PRESSURE WARNING - BOOSTER PUMPS 1, 2 FWD - 3, 4 AFT - LEFT, RIGHT OVERRIDE JETTISON - WIRING CHANGE . . . . . . . . . . . . . . . . . . 962 ### Page 9 Table of Contents Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 9 of 1162 BOEING SERVICE BULLETIN 747-28A2280 FIGURE 182: FUEL LOW PRESSURE WARNING - BOOSTER PUMPS 1, 2 FWD - 3, 4 AFT - LEFT, RIGHT OVERRIDE JETTISON - WIRING CHANGE . . . . . . . . . . . . . . . . . . . 964 FIGURE 183: FUEL LOW PRESSURE WARNING - JETTISON PUMPS - MAIN 2 AND 3 AFT - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .9 6 6 FIGURE 184: FUEL LOW PRESSURE WARNING - JETTISON PUMPS - MAIN 2 AND 3 AFT - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .9 6 7 FIGURE 185: OVERRIDE/JETTISON PUMPS - MAIN 3 AFT - WIRING CHANGE. . . . . . . . . . . 968 FIGURE 186: OVERRIDE/JETTISON PUMPS - MAIN 3 AFT - WIRING CHANGE. . . . . . . . . . . 970 FIGURE 187: OVERRIDE/JETTISON PUMPS - MAIN 3 AFT - WIRING CHANGE. . . . . . . . . . . 972 FIGURE 188: OVERRIDE/JETTISON PUMPS - MAIN 3 AFT - WIRING CHANGE. . . . . . . . . . . 974 FIGURE 189: OVERRIDE/JETTISON PUMPS - MAIN 3 AFT - WIRING CHANGE. . . . . . . . . . . 976 FIGURE 190: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 978 FIGURE 191: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 980 FIGURE 192: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 982 FIGURE 193: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 984 FIGURE 194: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 986 FIGURE 195: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 988 FIGURE 196: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 990 FIGURE 197: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 992 FIGURE 198: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 994 FIGURE 199: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 996 FIGURE 200: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . 998 FIGURE 201: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . 1000 FIGURE 202: FUEL LOW PRESSURE WARNING - BOOSTER PUMPS 1, 2 FWD - 3, 4 AFT - LEFT, RIGHT OVERRIDE JETTISON - WIRING CHANGE . . . . . . . . . . . . . . . . . . 1002 FIGURE 203: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . 1004 FIGURE 204: OVERRIDE/JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . 1006 FIGURE 205: MAIN EQUIPMENT CENTER - P415 PANEL - WIRING CHANGE . . . . . . . . . . 1008 FIGURE 206: MAIN EQUIPMENT CENTER - P415 PANEL - WIRING CHANGE . . . . . . . . . . 1013 FIGURE 207: MAIN EQUIPMENT CENTER - E2-6 SHELF - WIRING CHANGE . . . . . . . . . . . 1018 FIGURE 208: MAIN EQUIPMENT CENTER - E2-6 SHELF - WIRING CHANGE . . . . . . . . . . . 1021 FIGURE 209: MAIN EQUIPMENT CENTER - P414 PANEL - WIRING CHANGE . . . . . . . . . . 1024 FIGURE 210: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . 1029 FIGURE 211: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . 1030 FIGURE 212: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . 1031 FIGURE 213: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . 1032 FIGURE 214: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . 1033 FIGURE 215: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . 1034 FIGURE 216: MAIN EQUIPMENT CENTER - P415 PANEL - WIRING CHANGE . . . . . . . . . . 1035 FIGURE 217: MAIN EQUIPMENT CENTER - LEFT SIDE - TERMINAL MODULE AND NUT SPACER - INSTALLATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1040 FIGURE 218: MAIN EQUIPMENT CENTER - RIGHT SIDE - TERMINAL MODULE AND NUT SPACER - INSTALLATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1044 FIGURE 219: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGES . . . . . 1048 FIGURE 220: FUEL JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . 1051 FIGURE 221: OVERRIDE/JETTISON PUMPS - MAIN 3 FORWARD - WIRING CHANGE . . . . . . 1053 ### Page 10 Table of Contents Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 10 of 1162 BOEING SERVICE BULLETIN 747-28A2280 FIGURE 222: FUEL JETTISON PUMPS - WIRING CHANGE . . . . . . . . . . . . . . . . . . . . . 1055 FIGURE 223: OVERRIDE/JETTISON PUMPS - MAIN 2 AFT - WIRING CHANGE . . . . . . . . . . 1057 FIGURE 224: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . 1059 FIGURE 225: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . 1065 FIGURE 226: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . 1071 FIGURE 227: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . 1077 FIGURE 228: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . 1078 FIGURE 229: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . 1079 FIGURE 230: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . 1080 FIGURE 231: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . 1081 FIGURE 232: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . 1082 FIGURE 233: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . 1083 FIGURE 234: FUEL LOW PRESSURE WARNING - WIRING CHANGE . . . . . . . . . . . . . . . 1084 FIGURE 235: MAIN EQUIPMENT CENTER - WIRING CHANGE . . . . . . . . . . . . . . . . . . . 1085 FIGURE 236: MAIN EQUIPMENT CENTER - WIRING CHANGE . . . . . . . . . . . . . . . . . . . 1114 FIGURE 237: MAIN EQUIPMENT CENTER - P414 PANEL - WIRING CHANGE . . . . . . . . . . . 1142 FIGURE 238: OVERRIDE/JETTISON PUMPS - MAIN 3 FORWARD - WIRING CHANGE . . . . . . 1147 FIGURE 239: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGES . . . . . 1149 FIGURE 240: OVERRIDE/JETTISON PUMPS - WIRING CHANGES . . . . . . . . . . . . . . . . . 1151 FIGURE 241: OVERRIDE/JETTISON PUMPS - MAIN 3 FORWARD - WIRING CHANGE . . . . . . 1153 FIGURE 242: FUEL LOW PRESSURE WARNING - JETTISON PUMPS MAIN 2 AND 3 FWD - WIRING CHANGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1155 FIGURE 243: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGE . . . . . . 1157 FIGURE 244: OVERRIDE/JETTISON PUMPS - MAIN 2 FORWARD - WIRING CHANGE . . . . . . 1159 FIGURE 245: MAIN EQUIPMENT CENTER - P415 PANEL - WIRING CHANGE . . . . . . . . . . . 1161 ### Page 11 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 11 of 1162 Commercial Airplanes 747 Service Bulletin Number: 747-28A2280 Revision Transmittal Sheet Original Issue: August 07, 2008 Revision 1: November 25, 2009 ATA System: 2831 SUBJECT: FUEL - Fuel Jettison System - Center Tank Override/Jettison Fuel Pumps - Main 2 and Main 3 Tank Override/Jettison Fuel Pumps - Change to Give Redundant Control of the Fuel Pumps This Revision includes all pages of the service bulletin. COMPLIANCE INFORMATION RELATED TO THIS REVISION No more work is necessary on airplanes changed as shown in the original issue of this service bulletin. REASON FOR REVISION As a part of a service bulletin validation program, this change was completed on airplane RM084 by Service Bulletin 747-28A2280 Original Issue before the release of Revision 1 of this service bulletin. The change completed on airplane RM084 by Service Bulletin 747-28A2280 Original Issue is equivalent to the release of Revision 1 of this service bulletin. Airplane RM084 has the configuration of a Group 131 airplane. This revision is sent to update the wire diagrams and wire installation figures, include more information on access, and update the material information section because more wiring parts are needed to complete the change. Also more figures are needed to show the configuration of the validation airplane. The effectivity group assignment for RM084 was changed from Group 2 to new Group 131 to show the correct wiring configuration for this airplane. The following sections were changed: 1. In Summary, Planning Information, Material Information, Accomplishment Instructions, and all applicable figures, updated to specify the new group. 2. In Summary, and Planning Information, Paragraph 1.D., updated the access instructions. 3. In Material Information, Paragraph 2.A., updated the price and availability of the Top Kit. 4. In Material Information, Paragraph 2.C., updated the parts list. 5. In Accomplishment Instructions, Paragraph 3.A., added a note to follow the existing wire bundle routing when possible. 6. In Accomplishment Instructions, Paragraph 3.B., updated steps for ceiling panels and floor panels removal to specify stations. ### Page 12 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 12 of 1162 BOEING SERVICE BULLETIN 747-28A2280 7. In Figure 1 and 2, revised step tables to show new fasteners for brackets. 8. In Figure 7, 8, 235, and 236, revised step tables to correct the separation code for W4727. 9. In Figure 7, 8, 235, and 236, revised step tables to include colored plastic tie straps as an alternative to lacing tape. 10. In Figure 51 - 55, added new flag notes for BACC47CP2S contact at DM7867 and updated quantity of BACC47CP1S contact. 11. In Figure 67 - 70 and 73, revised illustrations to show M7869 on the left side. 12. In Figure 67 - 70, and 73, added new flag notes for BACC47CP2S contact at DM7869 and updated quantity of BACC47CP1S contact. 13. In Figure 76 - 79, added new flag notes for BACC47CP2S contact at DM7868 and updated quantity of BACC47CP1S contact. 14. In Figure 186 - 189, added new flag notes for BACC47CP2S contact at DM7866 and updated quantity of BACC47CP1S contact. 15. In Figure 187, revised illustration to show wire W4748-012-20 termination at SP14401. 16. In Figure 217 and 218, revised step tables to specify ground ID labels. 17. Added 6 new figures for new group 131 to show new wire positions and terminations for connector D40280P. 18. Added 2 new figures for new group 131 to show new wire positions for connector D40368P. 19. Added 1 new figure to install hardware for new receptacle connectors and updated Accomplishment Instructions to include the new figure. The data given in Information Notice 747-28-2280 IN 01 is included in this revision with one exception. In Figures 113, 116, 117, 118, 119, 120, 121, the wires W3942-8FE, W3942-8FF, and W3942-8FH are specified as size 20 wire but they are size 22 wire. This statement in IN 01 is incorrect and the wire size should be size 20. Paragraph 1.A., Effectivity, shows changes of airplane operators. Each operator should examine the Effectivity paragraph for changes. Vertical lines are put on the left edge of each page, except in Paragraph 1.A., Effectivity, to show the location of important changes. Pages with no vertical lines have no important changes. REVISION HISTORY Original Issue August 07, 2008 Revision 1: November 25, 2009 ### Page 13 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 13 of 1162 Commercial Airplanes 747 Service Bulletin Number: 747-28A2280 Summary Original Issue: August 07, 2008 Revision 1: November 25, 2009 ATA System: 2831 SUBJECT: FUEL - Fuel Jettison System - Center Tank Override/Jettison Fuel Pumps - Main 2 and Main 3 Tank Override/Jettison Fuel Pumps - Change to Give Redundant Control of the Fuel Pumps CONCURRENT REQUIREMENTS Refer to Paragraph 1.B for the list of concurrent requirements. BACKGROUND Accomplishment of the changes in this service bulletin will help prevent an ignition source in a fuel tank as a result of a override/jettison fuel pump that continues to run after it has been commanded OFF. An ignition source in a fuel tank could result in a fire or an explosion. A safety assessment conducted by Boeing under Special Federal Aviation Regulation (SFAR) 88, "Fuel Tank System Fault Tolerance Evaluation Requirements" indicates that there is a small risk of an ignition source in a fuel tank if a override/jettison fuel pump continues to run for an extended time after fuel level goes below the pump inlet. When the Engine Indicating and Alert System (EICAS) status message "FUEL TANK/ENGINE" is received (all main tanks are equal), the inboard main override/jettison pumps are normally commanded off. When the fuel quantity in the center tank goes below the specified weight, the center override/jettison pumps are normally commanded off. However, if a single failure in the pump control circuitry occurs, a pump can continue to run after it is commanded off. When a pump runs after the fuel level goes below the pump inlet, there is a small risk that the pump can cause an ignition source in the fuel tank from an overheat condition, electrical arcs or frictional sparks. This service bulletin gives the instructions to install new pump control relays and time delay relays in the circuitry for the center fuel tank override/jettison fuel pumps and the main fuel tank override/jettison fuel pumps. The new pump control relays provide a redundant power control if a failure of the existing relays occurs. The new time delay relays do an automatic shutoff of the override/jettison fuel pumps in the center tank or the main tank 15 seconds after a low pressure indication. The time delay relays provide redundant power control if a failure of a flight deck switch in the on position occurs. Each set of relays have a new EICAS status message to annunciate a fault in a pump control relay. For the center tank, the EICAS status messages are "FUEL CMD CTR L" and "FUEL CMD CTR R". For the main tank, the EICAS status messages are "FUEL CMD OVD 2" and "FUEL CMD OVD 3". These messages are enabled by a fuels pseudo hardware program pin on the Electronic Flight Indication System (EFIS)/EICAS Interface Units (EIU). These changes help make sure that the risk of an ignition source in a fuel tank is kept to a minimum. The changes are identical to the changes to airplanes in production. ### Page 14 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 14 of 1162 BOEING SERVICE BULLETIN 747-28A2280 This change affects Section 9 of the 747-400 Maintenance Planning Data (MPD) document. New Airworthiness Limitations (AWL) "28-AWL-26" will be added to Section 9 of the MPD to include an operational test of the uncommanded on system for the override/jettison fuel pumps in the main 2 and main 3 fuel tanks. ACTION (PRR 85539-8) Group 1-2, 5-10, 12-28, 30, 32-47, 49-71, 75-115, 117-120, 123-131: Get access to the main equipment center. Get access to the wire bundles in the ceiling from station 400 to station 970 in the forward cargo compartment on the right and left sides. Get access to the wiring below the floor panels from station 900 to station 1200 to the AL1201 and AL1202 disconnect brackets in the passenger cabin on the right and left sides. Install the new P914 panel assembly on the left side of the airplane. Install the new P915 panel assembly on the right side of the airplane. Change the airplane wiring. Do a functional test. Close access. Group 121-122: Get access to the main equipment center. Install the new P914 panel assembly on the left side of the airplane. Install the new P915 panel assembly on the right side of the airplane. Change the airplane wiring. Do a functional test. Close access. Group 3-4, 11, 29, 31, 48, 72-74, 116: Get access to the main equipment center. Get access to the wire bundles in the ceiling from station 400 to station 970 in the forward cargo compartment on the right and left sides. Get access to the wiring below the floor panels from station 900 to station 1200 to the AL1201 and AL1202 disconnect brackets on the main deck on the right and left sides. Get access to the AF0314 disconnect bracket on the right side wall in the cargo compartment on the main deck. Install the new P914 panel assembly on the left side of the airplane. Install the new P915 panel assembly on the right side of the airplane. Change the airplane wiring. Do a functional test. Close access. Boeing Service Bulletin 747-28-2145 and 747-28-2149 have some wiring changes that are related to the wiring changes in this service bulletin. EFFECTIVITY 747-400/-400D/-400F Airplanes. Refer to Paragraph 1.A.1., Airplanes for the list of affected airplanes. COMPLIANCE The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to this service bulletin. The Airworthiness Directive will make the compliance tasks and times given in this service bulletin mandatory. Boeing recommends that this service bulletin be incorporated within 60 months after the original issue date of this service bulletin. INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the configuration changes given in this service bulletin. ### Page 15 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 15 of 1162 BOEING SERVICE BULLETIN 747-28A2280 MANPOWER MATERIAL INFORMATION Boeing Supplied Kits/Parts. Refer to Paragraph 2.A., Material - Price and Availability. Airplanes Total Task Hours Elapsed Hours Group 1-2, 5-10, 12-28, 30, 32-47, 49-71, 75-115, 117-120, 123-131: 409.50 109.75 Group 3-4, 11, 29, 31, 48, 72-74, 116, 121-122: 383.50 101.75 ### Page 16 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 16 of 1162 BOEING SERVICE BULLETIN 747-28A2280 FWD MAIN EQUIPMENT CENTER FWD UP INSTALL NEW P914 AND P915 PANELS AND CHANGE A/P WIRING. P415-1 OR P415 AUXILIARY PANEL P414-1 OR P414 AUXILIARY PANEL 1309606 ### Page 17 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 17 of 1162 Commercial Airplanes 747 Service Bulletin Number: 747-28A2280 Original Issue: August 07, 2008 Revision 1: November 25, 2009 ATA System: 2831 SUBJECT: FUEL - Fuel Jettison System - Center Tank Override/Jettison Fuel Pumps - Main 2 and Main 3 Tank Override/Jettison Fuel Pumps - Change to Give Redundant Control of the Fuel Pumps 1. PLANNING INFORMATION A. Effectivity 1. Airplanes This service bulletin is for the airplanes shown below. An equivalent change is on subsequent production airplanes. Refer to PRR 85539-8 for data about this change. GROUP CONFIGURATION DESCRIPTION 1 - 747-400 airplanes with different wiring configurations 2 - 747-400 airplanes with different wiring configurations 3 - 747-400F airplanes with different wiring configurations 4 - 747-400F airplanes with different wiring configurations 5 - 747-400 airplanes with different wiring configurations 6 - 747-400 airplanes with different wiring configurations 7 - 747-400 airplanes with different wiring configurations 8 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 ### Page 18 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 18 of 1162 BOEING SERVICE BULLETIN 747-28A2280 9 - 747-400D airplanes with different wiring configurations 10 - 747-400 airplanes with different wiring configurations 11 - 747-400F airplanes with different wiring configurations 12 - 747-400 airplanes with different wiring configurations 13 - 747-400 airplanes with different wiring configurations 14 - 747-400 airplanes with different wiring configurations 15 - 747-400 airplanes with different wiring configurations 16 - 747-400 airplanes with different wiring configurations 17 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 18 - 747-400 airplanes with different wiring configurations 19 - 747-400 airplanes with different wiring configurations 20 - 747-400 airplanes with different wiring configurations 21 - 747-400 airplanes with different wiring configurations 22 - 747-400 airplanes with different wiring configurations GROUP CONFIGURATION DESCRIPTION ### Page 19 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 19 of 1162 BOEING SERVICE BULLETIN 747-28A2280 23 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 24 - 747-400 airplanes with different wiring configurations 25 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 26 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 27 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 GROUP CONFIGURATION DESCRIPTION ### Page 20 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 20 of 1162 BOEING SERVICE BULLETIN 747-28A2280 28 - 747-400 airplanes with different wiring configurations 29 - 747-400F airplanes with different wiring configurations 30 - 747-400 airplanes with different wiring configurations 31 - 747-400F airplanes with different wiring configurations 32 - 747-400 airplanes with different wiring configurations 33 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 34 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 35 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 GROUP CONFIGURATION DESCRIPTION ### Page 21 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 21 of 1162 BOEING SERVICE BULLETIN 747-28A2280 36 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 37 - 747-400 airplanes with different wiring configurations 38 - 747-400 airplanes with different wiring configurations 39 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 40 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 GROUP CONFIGURATION DESCRIPTION ### Page 22 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 22 of 1162 BOEING SERVICE BULLETIN 747-28A2280 41 - 747-400 airplanes with different wiring configurations 42 - 747-400 airplanes with different wiring configurations 43 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 44 - 747-400 airplanes with different wiring configurations 45 - 747-400 airplanes with different wiring configurations 46 - 747-400 airplanes with different wiring configurations 47 - 747-400 airplanes with different wiring configurations 48 - 747-400F airplanes with different wiring configurations 49 - 747-400 airplanes with different wiring configurations 50 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 51 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 52 - 747-400 airplanes with different wiring configurations 53 - 747-400 airplanes with different wiring configurations GROUP CONFIGURATION DESCRIPTION ### Page 23 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 23 of 1162 BOEING SERVICE BULLETIN 747-28A2280 54 - 747-400 airplanes with different wiring configurations 55 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 56 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 57 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 58 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 59 - 747-400 airplanes with different wiring configurations 60 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 61 - 747-400 airplanes with different wiring configurations GROUP CONFIGURATION DESCRIPTION ### Page 24 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 24 of 1162 BOEING SERVICE BULLETIN 747-28A2280 62 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 63 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 64 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 65 - 747-400 airplanes with different wiring configurations 66 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 GROUP CONFIGURATION DESCRIPTION ### Page 25 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 25 of 1162 BOEING SERVICE BULLETIN 747-28A2280 67 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 68 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 69 - 747-400 airplanes with different wiring configurations 70 - 747-400 airplanes with different wiring configurations 71 - 747-400 airplanes with different wiring configurations 72 - 747-400F airplanes with different wiring configurations 73 - 747-400F airplanes with different wiring configurations 74 - 747-400F airplanes with different wiring configurations 75 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 76 - 747-400 airplanes with different wiring configurations GROUP CONFIGURATION DESCRIPTION ### Page 26 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 26 of 1162 BOEING SERVICE BULLETIN 747-28A2280 77 - 747-400 airplanes with different wiring configurations 78 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 79 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 80 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 GROUP CONFIGURATION DESCRIPTION ### Page 27 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 27 of 1162 BOEING SERVICE BULLETIN 747-28A2280 81 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 82 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 83 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 84 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 GROUP CONFIGURATION DESCRIPTION ### Page 28 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 28 of 1162 BOEING SERVICE BULLETIN 747-28A2280 85 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 86 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 87 - 747-400 airplanes with different wiring configurations 88 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 89 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 90 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 GROUP CONFIGURATION DESCRIPTION ### Page 29 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 29 of 1162 BOEING SERVICE BULLETIN 747-28A2280 91 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 92 - 747-400 airplanes with different wiring configurations 93 - 747-400 airplanes with different wiring configurations 94 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 95 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 GROUP CONFIGURATION DESCRIPTION ### Page 30 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 30 of 1162 BOEING SERVICE BULLETIN 747-28A2280 96 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 97 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 98 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 99 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 100 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 GROUP CONFIGURATION DESCRIPTION ### Page 31 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 31 of 1162 BOEING SERVICE BULLETIN 747-28A2280 101 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 102 - 747-400 airplanes with different wiring configurations 103 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 104 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 105 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 GROUP CONFIGURATION DESCRIPTION ### Page 32 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 32 of 1162 BOEING SERVICE BULLETIN 747-28A2280 106 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 107 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 108 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 109 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2145 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2145 3 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 4 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 110 - 747-400 airplanes with different wiring configurations 1 747-400 airplanes with different wiring configurations without the incorporation of Boeing Service Bulletin 747-28-2149 2 747-400 airplanes with different wiring configurations with the incorporation of Boeing Service Bulletin 747-28-2149 GROUP CONFIGURATION DESCRIPTION ### Page 33 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 33 of 1162 BOEING SERVICE BULLETIN 747-28A2280 Airplane models: 111 - 747-400 airplanes with different wiring configurations 112 - 747-400 airplanes with different wiring configurations 113 - 747-400 airplanes with different wiring configurations 114 - 747-400 airplanes with different wiring configurations 115 - 747-400 airplanes with different wiring configurations 116 - 747-400F airplanes with different wiring configurations 117 - 747-400 airplanes with different wiring configurations 118 - 747-400 airplanes with different wiring configurations 119 - 747-400 airplanes with different wiring configurations 120 - 747-400D airplanes with different wiring configurations 121 - 747-400 airplanes with different wiring configurations 122 - 747-400 airplanes with different wiring configurations 123 - 747-400 airplanes with different wiring configurations 124 - 747-400 airplanes with different wiring configurations 125 - 747-400 airplanes with different wiring configurations 126 - 747-400 airplanes with different wiring configurations 127 - 747-400 airplanes with different wiring configurations 128 - 747-400 airplanes with different wiring configurations 129 - 747-400 airplanes with different wiring configurations 130 - 747-400 and 747-400D airplanes with different wiring configurations 131 - 747-400 airplanes with different wiring configurations GROUP CONFIGURATION DESCRIPTION ### Page 34 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 34 of 1162 BOEING SERVICE BULLETIN 747-28A2280 747-400 747-400D 747-400F IDENTIFICATION BY CUSTOMER, CUSTOMER CODE, GROUP AND VARIABLE NUMBER AEROLINEAS ARGENTINAS (ARG) 100 RT702 102 RT704 99 RT701 AIR ATLANTA ICELANDIC (AID) 106 RT751 123 RT515 AIR CHINA (BEJ) 1R M 3 4 1 118 RT878–RT880 128 RT034–RT035 22 RM811–RM813 AIR CHINA CARGO (CGC) 4 RL501–RL502 40 RT031–RT033 53 RT101 77 RT103 AIR FRANCE (AFA) 103 RT711 104 RT712 117 RT074 RT713–RT716 129 RT121 2 RM401–RM403 21 RT073 29 RL671–RL673 3 RL674–RL675 52 RT071–RT072 76 RT075 94 RT591 AIR INDIA (AIN) 118 RU001–RU006 AIR NEW ZEALAND (ANZ) 101 RT703 124 RT932 17 RT671–RT672 2R M 0 8 2 47 RM191–RM192 6 RT673 AIR PACIFIC (APC) 35 RT502 RT504 ### Page 35 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 35 of 1162 BOEING SERVICE BULLETIN 747-28A2280 AIR PULLMANTUR (PUL) 123 RT523 RT525 18 RT749 ALL NIPPON AIRWAYS (ANA) 108 RT776 124 RT753–RT755 69 RT777 9 RU831 RU833–RU841 AMIRI FLIGHT (ABD) 124 RT137 131 RM084 ASIANA AIRLINES (AAR) 116 RR746–RR747 124 RT131–RT136 RU032 2R M 0 7 1 3 RM861–RM863 ATLAS AIR (TLS) 107 RT752 116 RR748 3 RM891–RM899 RM901–RM906 AVION AIRCRAFT TRADING H.F. (VNG) 123 RT633–RT634 9 RT756 BAHRAIN ROYAL FLIGHT (BHR) 7R M 4 2 6 BRITISH AIRWAYS (BAB) 1 RM096–RM097 RM136–RM145 RM261–RM264 10 RT490–RT499 RU121 111 RU123 112 RU132 113 RU126–RU131 119 RU122 15 RU124–RU125 60 RT486–RT487 61 RT488–RT489 8 RT471–RT485 CARGOLUX AIRLINES (CLX) 11 RM881–RM889 RR723–RR724 48 RR721–RR722 72 RR701 ### Page 36 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 36 of 1162 BOEING SERVICE BULLETIN 747-28A2280 CATHAY PACIFIC AIRWAYS (CAT) 109 RT781 110 RT782 123 RT514 RT517 RT522 RT529 RT837 17 RT451–RT455 24 RT518 RT528 31 RM856–RM859 6 RT458–RT469 63 RT511–RT512 73 RR951 74 RR952 78 RT456 79 RT457 81 RT508 CHINA AIRLINES (CHI) 1 RM021–RM024 123 RT636–RT640 29 RL430 3 RL411–RL429 30 RM441–RM443 RM445 CHINA CARGO (CIQ) 3 RL521 CHINA SOUTHERN AIRLINES (GUN) 4 RL751–RL752 CORSAIR (COR) 123 RT613–RT614 RT616 RT618–RT619 RT621 DRAGONAIR (DRG) 123 RT519 24 RT513 RT516 42 RT524 83 RT510 DUBAI AIR WING (DAW) 1R M 1 6 7 5R M 1 6 8 53 RT102 EL AL ISRAEL AIRLINES (ELA) 123 RT527 2R M 0 9 1 37 RU081–RU083 EVA AIR (EVA) 124 RT162–RT163 RT165–RT168 RT951–RT955 2 RM116–RM117 3 RL401–RL403 ### Page 37 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 37 of 1162 BOEING SERVICE BULLETIN 747-28A2280 EVERGREEN INTERNATIONAL A/L (EVR) 121 RT631–RT632 122 RT876 37 RT743 EXPORT RESTRICTED AIRPLANES (YWV) 123 RT620 36 RT606 96 RT602 GARUDA INDONESIA (GIA) 124 RT931 RU061–RU062 GECAS (GEF) 123 RT615 RT622 126 RT412 GOVERNMENT OF JAPAN (JAG) 67 RT681–RT682 GRAND STAR (GCG) 4 RR861 GREAT WALL AIRLINES (GWL) 3R M 8 5 2 42 RT520 HIS MAJESTY THE SULTAN'S FLIGHT (BWN) 12 RT440 JADE CARGO INTERNATIONAL (JDE) 3 RL511 JAL INTERNATIONAL (JAL) 114 RM130–RM132 RM317–RM318 120 RU801 13 RM126–RM129 RM316 130 RT652–RT654 RT966–RT967 RU802–RU809 26 RT641–RT645 27 RT646–RT650 28 RT861–RT864 3 RL461–RL462 44 RT655–RT657 97 RT651 KALITTA AIR (KAC) 39 RT021–RT022 KINGDOM HOLDING COMPANY (KBA) 118 RT877 ### Page 38 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 38 of 1162 BOEING SERVICE BULLETIN 747-28A2280 KLM - ROYAL DUTCH AIRLINES (KLM) 127 RT012–RT014 20 RM801–RM803 23 RT001–RT005 3 RL681–RL683 32 RT008–RT011 49 RT006–RT007 64 RT531–RT532 65 RT534–RT535 84 RT533 KOREAN AIR (KAL) 1 RM011–RM013 123 RT577–RT588 RT590 RT811–RT814 4 RL451–RL456 RM871–RM880 RR862 75 RT061 88 RT571 89 RT572 90 RT573 91 RT574 92 RT575 93 RT576 KUWAIT AIRWAYS (KUW) 54 RT151 LION AIR (MLI) 35 RT503 RT505 LUFTHANSA GERMAN AIRLINES (DLH) 12 RT439 RT441–RT447 16 RM001–RM007 34 RT433–RT436 41 RT045–RT047 50 RT041–RT042 51 RT043–RT044 58 RT431–RT432 59 RT437–RT438 MALAYSIA AIRLINES (MAS) 124 RU017 18 RT744 RT746 RT748 RT750 2 RM036–RM040 RM366–RM367 28 RU016 4 RL491–RL492 MARTINAIR HOLLAND (MTH) 62 RT506–RT507 80 RT501 82 RT509 NIPPON CARGO AIRLINES (NCA) 3 RL471–RL473 ### Page 39 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 39 of 1162 BOEING SERVICE BULLETIN 747-28A2280 NORTHWEST AIRLINES (NWA) 14 RM241–RM246 33 RT407–RT410 55 RT401 RT406 56 RT402–RT403 57 RT404–RT405 OMAN ROYAL FLIGHT (RFO) 7R M 0 1 0 PHILIPPINE AIRLINES (PAL) 124 RU059 45 RU051–RU052 RU060 54 RT152 POLAR AIR CARGO (PAO) 3 RL651–RL655 QANTAS (QAN) 1 RM331–RM333 105 RT742 124 RU031 19 RF001–RF006 25 RT552–RT556 39 RT741 43 RT557–RT559 6 RT562–RT568 85 RT551 86 RT560 87 RT561 ROYAL AIR MAROC (RAM) 9 RT717 SAUDI ARABIAN AIRLINES (SVA) 2 RM156–RM157 71 RU101–RU102 SAUDI ROYAL FLIGHT (SRF) 2R M 1 5 8 SIACARGO (SIT) 3 RL431–RL436 RM851 RM853–RM855 RR851–RR856 SINGAPORE AIRLINES (SIA) 1 RM041–RM045 123 RT521 RT831–RT835 24 RT526 42 RT530 SONAIR (SON) 115 RM231–RM233 ### Page 40 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 40 of 1162 BOEING SERVICE BULLETIN 747-28A2280 SOUTH AFRICAN AIRWAYS (SAA) 38 RM081 RM083 46 RM147 THAI AIRWAYS INTERNATIONAL (TII) 125 RT694–RT699 RT801–RT803 68 RT691–RT692 7 RM026–RM030 RM431 98 RT693 TRANSAERO AIRLINES (TRX) 46 RM146 70 RT783–RT784 UNITED AIR LINES (UAL) 1R M 1 6 6 123 RT609–RT612 RT617 RT623–RT630 126 RT411 36 RT605 RT607–RT608 5 RM169–RM177 66 RT603–RT604 95 RT601 UPS (UPS) 124 RT161 RT164 US AIR FORCE (USF) 3R M 9 1 1 VIRGIN ATLANTIC AIRWAYS (VAA) 124 RT945–RT949 2 RM051–RM053 RM351–RM355 WORLD AIRWAYS, INC. (WLD) 18 RT745 RT747 YANGTZE RIVER EXPRESS (YTH) 9 RT757 IDENTIFICATION BY VARIABLE NUMBER Variable Group RF001–RF006 19 RL401–RL403 3 RL411–RL429 3 RL430 29 RL431–RL436 3 RL451–RL456 4 RL461–RL462 3 RL471–RL473 3 ### Page 41 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 41 of 1162 BOEING SERVICE BULLETIN 747-28A2280 RL491–RL492 4 RL501–RL502 4 RL511 3 RL521 3 RL651–RL655 3 RL671–RL673 29 RL674–RL675 3 RL681–RL683 3 RL751–RL752 4 RM001–RM007 16 RM010 7 RM011–RM013 1 RM021–RM024 1 RM026–RM030 7 RM036–RM040 2 RM041–RM045 1 RM051–RM053 2 RM071 2 RM081 38 RM082 2 RM083 38 RM084 131 RM091 2 RM096–RM097 1 RM116–RM117 2 RM126–RM129 13 RM130–RM132 114 RM136–RM145 1 RM146–RM147 46 RM156–RM158 2 RM166–RM167 1 RM168–RM177 5 RM191–RM192 47 RM231–RM233 115 RM241–RM246 14 RM261–RM264 1 RM316 13 RM317–RM318 114 RM331–RM333 1 Variable Group ### Page 42 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 42 of 1162 BOEING SERVICE BULLETIN 747-28A2280 RM341 1 RM351–RM355 2 RM366–RM367 2 RM401–RM403 2 RM426 7 RM431 7 RM441–RM443 30 RM445 30 RM801–RM803 20 RM811–RM813 22 RM851–RM855 3 RM856–RM859 31 RM861–RM863 3 RM871–RM880 4 RM881–RM889 11 RM891–RM899 3 RM901–RM906 3 RM911 3 RR701 72 RR721–RR722 48 RR723–RR724 11 RR746–RR748 116 RR851–RR856 3 RR861–RR862 4 RR951 73 RR952 74 RT001–RT005 23 RT006–RT007 49 RT008–RT011 32 RT012–RT014 127 RT021–RT022 39 RT031–RT033 40 RT034–RT035 128 RT041–RT042 50 RT043–RT044 51 RT045–RT047 41 RT061 75 RT071–RT072 52 RT073 21 Variable Group ### Page 43 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 43 of 1162 BOEING SERVICE BULLETIN 747-28A2280 RT074 117 RT075 76 RT101–RT102 53 RT103 77 RT121 129 RT131–RT137 124 RT151–RT152 54 RT161–RT168 124 RT401 55 RT402–RT403 56 RT404–RT405 57 RT406 55 RT407–RT410 33 RT411–RT412 126 RT431–RT432 58 RT433–RT436 34 RT437–RT438 59 RT439–RT447 12 RT451–RT455 17 RT456 78 RT457 79 RT458–RT469 6 RT471–RT485 8 RT486–RT487 60 RT488–RT489 61 RT490–RT499 10 RT501 80 RT502–RT505 35 RT506–RT507 62 RT508 81 RT509 82 RT510 83 RT511–RT512 63 RT513 24 RT514–RT515 123 RT516 24 RT517 123 RT518 24 RT519 123 Variable Group ### Page 44 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 44 of 1162 BOEING SERVICE BULLETIN 747-28A2280 RT520 42 RT521–RT523 123 RT524 42 RT525 123 RT526 24 RT527 123 RT528 24 RT529 123 RT530 42 RT531–RT532 64 RT533 84 RT534–RT535 65 RT551 85 RT552–RT556 25 RT557–RT559 43 RT560 86 RT561 87 RT562–RT568 6 RT571 88 RT572 89 RT573 90 RT574 91 RT575 92 RT576 93 RT577–RT588 123 RT590 123 RT591 94 RT601 95 RT602 96 RT603–RT604 66 RT605–RT608 36 RT609–RT630 123 RT631–RT632 121 RT633–RT634 123 RT636–RT640 123 RT641–RT645 26 RT646–RT650 27 RT651 97 RT652–RT654 130 Variable Group ### Page 45 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 45 of 1162 BOEING SERVICE BULLETIN 747-28A2280 RT655–RT657 44 RT671–RT672 17 RT673 6 RT681–RT682 67 RT691–RT692 68 RT693 98 RT694–RT699 125 RT701 99 RT702 100 RT703 101 RT704 102 RT711 103 RT712 104 RT713–RT716 117 RT717 9 RT741 39 RT742 105 RT743 37 RT744–RT750 18 RT751 106 RT752 107 RT753–RT755 124 RT756–RT757 9 RT776 108 RT777 69 RT781 109 RT782 110 RT783–RT784 70 RT801–RT803 125 RT811–RT814 123 RT831–RT835 123 RT837 123 RT861–RT864 28 RT876 122 RT877–RT880 118 RT931–RT932 124 RT945–RT949 124 RT951–RT955 124 RT966–RT967 130 Variable Group ### Page 46 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 46 of 1162 BOEING SERVICE BULLETIN 747-28A2280 2. Spares Affected None. B. Concurrent Requirements The service bulletin(s) listed below must be done before or at the same time as this service bulletin: RU001–RU006 118 RU016 28 RU017 124 RU031–RU032 124 RU051–RU052 45 RU059 124 RU060 45 RU061–RU062 124 RU081–RU083 37 RU101–RU102 71 RU121 10 RU122 119 RU123 111 RU124–RU125 15 RU126–RU131 113 RU132 112 RU801 120 RU802–RU809 130 RU831–RU841 9 Group 1-131: Company Service Bulletin Description Notes Boeing 747-31-2376, Original Issue Installs new Integrated Display System (IDS) software (a)(c) Boeing 747-31-2377, Original Issue Installs new Integrated Display System (IDS) software (b)(d) Boeing 747-31-2378, Original Issue Installs new Integrated Display System (IDS) software (e) (a) This service bulletin is not a concurrent or prior requirement for airplanes RL429, RL430, RL473, RL511, RL521. These airplanes received the new software in production. (b) This service bulletin is not a concurrent or prior requirement for airplanes RL456, RL492, RL502. These airplanes received the new software in production. Variable Group ### Page 47 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 47 of 1162 BOEING SERVICE BULLETIN 747-28A2280 C. Reason Accomplishment of the changes in this service bulletin will help prevent an ignition source in a fuel tank as a result of a override/jettison fuel pump that continues to run after it has been commanded OFF. An ignition source in a fuel tank could result in a fire or an explosion. A safety assessment conducted by Boeing under Special Federal Aviation Regulation (SFAR) 88, "Fuel Tank System Fault Tolerance Evaluation Requirements" indicates that there is a small risk of an ignition source in a fuel tank if a override/jettison fuel pump continues to run for an extended time after fuel level goes below the pump inlet. When the Engine Indicating and Alert System (EICAS) status message "FUEL TANK/ENGINE" is received (all main tanks are equal), the inboard main override/ jettison pumps are normally commanded off. When the fuel quantity in the center tank goes below the specified weight, the center override/jettison pumps are normally commanded off. However, if a single failure in the pump control circuitry occurs, a pump can continue to run after it is commanded off. When a pump runs after the fuel level goes below the pump inlet, there is a small risk that the pump can cause an ignition source in the fuel tank from an overheat condition, electrical arcs or frictional sparks. This service bulletin gives the instructions to install new pump control relays and time delay relays in the circuitry for the center fuel tank override/jettison fuel pumps and the main fuel tank override/jettison fuel pumps. The new pump control relays provide a redundant power control if a failure of the existing relays occurs. The new time delay relays do an automatic shutoff of the override/jettison fuel pumps in the center tank or the main tank 15 seconds after a low pressure indication. The time delay relays provide redundant power control if a failure of a flight deck switch in the on position occurs. Each set of relays have a new EICAS status message to annunciate a fault in a pump control relay. For the center tank, the EICAS status messages are "FUEL CMD CTR L" and "FUEL CMD CTR R". For the main tank, the EICAS status messages are "FUEL CMD OVD 2" and "FUEL CMD OVD 3". These messages are enabled by a fuels pseudo hardware program pin on the Electronic Flight Indication System (EFIS)/EICAS Interface Units (EIU). These changes help make sure that the risk of an ignition source in a fuel tank is kept to a minimum. The changes are identical to the changes to airplanes in production. This change affects Section 9 of the 747-400 Maintenance Planning Data (MPD) document. New Airworthiness Limitations (AWL) "28-AWL-26" will be added to Section 9 of the MPD to include an operational test of the uncommanded on system for the override/jettison fuel pumps in the main 2 and main 3 fuel tanks. As a part of a service bulletin validation program, this change was completed on airplane RM084 by Service Bulletin 747-28A2280 Original Issue before the release of Revision 1 of this service bulletin. The change completed on airplane RM084 by Service Bulletin 747-28A2280 Original Issue is equivalent to the release of Revision 1 of this service bulletin. Airplane RM084 has the configuration of a Group 131 airplane. (c) This service bulletin is applicable for General Electric powered airplanes. (d) This service bulletin is applicable for Pratt and Whitney powered airplanes. (e) This service bulletin is applicable for Rolls Royce powered airplanes. Group 1-131: Company Service Bulletin Description Notes ### Page 48 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 48 of 1162 BOEING SERVICE BULLETIN 747-28A2280 Revision 1 is sent to update the wire diagrams and wire installation figures, include more information on access, and update the material information section because more wiring parts are needed to complete the change. Also more figures are needed to show the configuration of the validation airplane. The effectivity group assignment for RM084 was changed from Group 2 to new Group 131 to show the correct wiring configuration for this airplane. The data given in Information Notice 747-28-2280 IN 01 is included in this revision with one exception. In Figures 113, 116, 117, 118, 119, 120, 121, the wires W3942-8FE, W3942-8FF, and W3942-8FH are specified as size 20 wire but they are size 22 wire. This statement in IN 01 is incorrect and the wire size should be size 20. D. Description Group 1-2, 5-10, 12-28, 30, 32-47, 49-71, 75-115, 117-120, 123-131: Get access to the main equipment center. Get access to the wire bundles in the ceiling from station 400 to station 970 in the forward cargo compartment on the right and left sides. Get access to the wiring below the floor panels from station 900 to station 1200 to the AL1201 and AL1202 disconnect brackets in the passenger cabin on the right and left sides. Install the new P914 panel assembly on the left side of the airplane. Install the new P915 panel assembly on the right side of the airplane. Change the airplane wiring. Do a functional test. Close access. Group 121-122: Get access to the main equipment center. Install the new P914 panel assembly on the left side of the airplane. Install the new P915 panel assembly on the right side of the airplane. Change the airplane wiring. Do a functional test. Close access. Group 3-4, 11, 29, 31, 48, 72-74, 116: Get access to the main equipment center. Get access to the wire bundles in the ceiling from station 400 to station 970 in the forward cargo compartment on the right and left sides. Get access to the wiring below the floor panels from station 900 to station 1200 to the AL1201 and AL1202 disconnect brackets on the main deck on the right and left sides. Get access to the AF0314 disconnect bracket on the right side wall in the cargo compartment on the main deck. Install the new P914 panel assembly on the left side of the airplane. Install the new P915 panel assembly on the right side of the airplane. Change the airplane wiring. Do a functional test. Close access. Boeing Service Bulletin 747-28-2145 and 747-28-2149 have some wiring changes that are related to the wiring changes in this service bulletin. Revision 1 - No more work is necessary on airplanes changed as shown in the original issue of this service bulletin. E. Compliance The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to this service bulletin. The Airworthiness Directive will make the compliance tasks and times given in this service bulletin mandatory. Boeing recommends that this service bulletin be incorporated within 60 months after the original issue date of this service bulletin. ### Page 49 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 49 of 1162 BOEING SERVICE BULLETIN 747-28A2280 F. Approval This service bulletin was examined by the Federal Aviation Administration (FAA). The changes specified in this service bulletin comply with the applicable regulations and are FAA approved, as well as European Aviation Safety Agency (EASA)/Joint Aviation Authorities (JAA) approved for all EASA/ JAA approved airplanes listed in the service bulletin effectivity. This service bulletin and its approval were based on the airplane in its original Boeing delivery configuration or as modified by other approved Boeing changes. If an airplane has a non-Boeing modification or repair that affects a component or system also affected by this service bulletin, the operator is responsible for obtaining appropriate regulatory agency approval before incorporating this service bulletin. G. Manpower The table below shows an estimate of the task hours necessary to do this change for each airplane. This estimate is for direct labor only, done by an experienced crew. Adjust the estimate with operator task hour data if necessary. The estimate does not include lost time. These are some examples of lost time: — Time to adjust to the workplace — Time to schedule the work — Time to inspect the work — Time to cure the materials — Time to make the parts — Time to find the tools. Group 1-2, 5-10, 12-28, 30, 32-47, 49-71, 75-115, 117-120, 123-131: Task Number of Persons Task-Hours Elapsed Hours Open Access 2 7.50 3.75 Figure 1 1 1.00 1.00 Figure 2 1 1.00 1.00 Figure 3 1 0.75 0.75 Figure 4 1 0.75 0.75 Wiring changes (Multiple Figures) 4 385.50 95.25 Test 2 4.00 2.00 Close Access 2 7.50 3.75 TOTAL FOR EACH AIRPLANE 409.50 109.75 Group 3-4, 11, 29, 31, 48, 72-74, 116, 121-122: Task Number of Persons Task-Hours Elapsed Hours Open Access 2 4.50 2.25 Figure 1 1 1.00 1.00 Figure 2 1 1.00 1.00 Figure 3 1 0.75 0.75 ### Page 50 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 50 of 1162 BOEING SERVICE BULLETIN 747-28A2280 H. Weight and Balance Changes I. Electrical Load Data 1. Direct Current (DC) Loads 2. Alternating Current (AC) Loads None 3. Type Continuous Figure 4 1 0.75 0.75 Wiring changes (Multiple Figures) 4 365.50 90.25 Test 2 4.00 2.00 Close Access 2 4.50 2.25 TOTAL FOR EACH AIRPLANE 383.50 101.75 Group 3-4, 11, 29, 31, 48, 72-74, 116: Airplane Change in Weight (Pounds) Change in Moment (Pound-Inches) Group 3-4, 11, 29, 31, 48, 72-74, 116 +83.6 +37620.0 Group 1-2, 5-10, 12-28, 30, 32-47, 49-71, 75-115, 117-120, 123-131: Airplane Change in Weight (Pounds) Change in Moment (Pound-Inches) Group 1-2, 5-10, 12-28, 30, 32-47, 49-71, 75-115, 117, 123- 130 +84.2 +37890.0 Group 121-122: Airplane Change in Weight (Pounds) Change in Moment (Pound-Inches) Group 121-122 +80.6 +36270.0 Airplanes Amperes Bus Group 1-131 0.79 D2P180 0.79 D3P180 1.58 D2P180 1.58 D4P180 0.08 DGHBP414A Group 3-4, 11, 29, 31, 48, 72-74, 116, 121-122: Task Number of Persons Task-Hours Elapsed Hours ### Page 51 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 51 of 1162 BOEING SERVICE BULLETIN 747-28A2280 Intermittent J. References 1. Existing Data: a. PRR 85539-8 b. 747-400 Aircraft Maintenance Manual (AMM) 12-11-00, 20-41-03, 24-22-00, 24-52-01, 25-25-00, 25-27-00, 25-59-01, 28-26-00, 28-31-00, 31-61-00, 32-09-02, 34-61-02, 45-10-00, 53-21-02 c. 747-400 Structural Repair Manual (SRM) 50-41-02, 51-40-02, 51-40-06, 51-41-06 d. 747-400 Wiring Diagram Manual (WDM) 28-21-11, 28-31-21, 28-31-22, 28-31-23, 28-31-24, 28-31-25, 28-31-26, 28-42-11, 28-42-12, 28-42-13, 28-42-14 e. Boeing Drawing 012W6100 f. Boeing Parts Standards Document D-590 g. Boeing Service Bulletin 747-28-2145, 747-28-2149, 747-31-2376, 747-31-2377, 747-31-2378 h. Standard Overhaul Practices Manual (SOPM) 20-50-05 i. Standard Wiring Practices Manual (SWPM) 20-10-11, 20-10-12, 20-10-14, 20-10-19, 20-20-00, 20-20-11, 20-30-11, 20-30-12, 20-60-08, 20-61-11, 20-71-14, 20-72-17, 20-81-12, 20-81-19, 20-90-11 2. Data supplied with this Service Bulletin: None. ### Page 52 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 52 of 1162 BOEING SERVICE BULLETIN 747-28A2280 3. Installation Drawings Used in the Preparation of this Service Bulletin: These drawings were used to prepare this service bulletin. These drawings are not necessary to make the specified changes, and are not supplied with this service bulletin. These drawings may not be applicable to all airplane configurations or operators. Drawing Number Title 284U0914 P914 PANEL EQUIPMENT ASSEMBLY AND INSTALLATION 284U0915 P915 PANEL EQUIPMENT ASSEMBLY AND INSTALLATION 288U3026 E2-6 RIGHT MAIN EQUIPMENT CENTER 288U4122 WIRE BUNDLE INSTALLATION UPPER DECK SIDEWALL RH, STA 243 THRU 403 288U4126 WIRE BUNDLE INSTALLATION MAIN DECK AREA SIDEWALL RH, STA 243 THRU 403 288U4127 WIRE BUNDLE INSTALLATION LOWER SIDEWALL LH, STA 243 THRU 403 288U4128 WIRE BUNDLE INSTALLATION LOWER SIDEWALL RH, STA 243 THRU 403 288U4129 WIRE BUNDLE INSTALLATION NOSE WHEEL WELL RH AND FWD 400 BULKHEAD RH 288U4132 WIRE BUNDLE INSTALLATION BULKHEAD AFT SIDE STA 400 288U4147 WIRE BUNDLE INSTALLATION LOWER SIDEWALL LH, STA 403 THRU 523 288U4150 WIRE BUNDLE INSTALLATION MAIN DECK FLOOR BEAMS RH, STA 403 THRU 523 AND AFT 400 BULKHEAD RH 288U4151 WIRE BUNDLE INSTALLATION MAIN DECK FLOOR BEAMS LH, STA 403 THRU 523 AND AFT BULKHEAD LH 288U4156 WIRE BUNDLE INSTALLATION MAIN DECK FLOOR BEAMS, STA 403 THRU 523, LBL 50 TO RBL 60 65B07936 BULKHEAD INSTL - STA 400, NOSE WHEEL WELL 828B8000 WIRE BUNDLE INSTAL - 747-400 LARGE CARGO FREIGHTER - SHIPS 828B8101 WIRE BUNDLE INSTALLATION - NOSE SECTION 41 828B8104 WIRE BUNDLE INSTALLATION - LOWER LOBE ### Page 53 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 53 of 1162 BOEING SERVICE BULLETIN 747-28A2280 K. Publications Affected L. Interchangeability and Intermixability of Parts Accomplishment of this service bulletin does not affect interchangeability or intermixability of parts. Publication Chapter-Section 747 Maintenance Manual 28-31 747 Wiring Diagram Manual 28-31, 28-42 747 Fault Reporting Manual EICAS Status Messages 747 Fault Isolation Manual 28-31 747 Illustrated Parts Catalog 28-31 747 System Schematic Manual 28-31, 28-42 747-400 Maintenance Planning Data (MPD) Section 9 ### Page 54 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 54 of 1162 BOEING SERVICE BULLETIN 747-28A2280 BLANK PAGE ### Page 55 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 55 of 1162 BOEING SERVICE BULLETIN 747-28A2280 2. MATERIAL INFORMATION A. Material - Price and Availability Boeing can supply the kits shown in Paragraph 2.C., Parts Necessary For Each Airplane as shown below. If there is a limit to the quantity (QTY) of available kits, a supply sequence is given by Spares. More kits become available as shown in the Reorder Lead Time (ROLT). ROLT is calculated from the date Boeing gets the purchase order. Group 2, 21, 24, 28, 42, 52, 63, 69, 71, 83, 92-93, 112-113, 123-125, 127, 129, 131: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-1 Top Kit 08/14/09 19 35 $75,525 Group 3, 29, 31, 72: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-2 Top Kit 08/14/09 9 35 $75,470 Group 6, 10, 61, 70, 79, 87, 110: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-3 Top Kit 08/14/09 4 35 $75,524 Group 8, 17, 43: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-4 Top Kit 08/14/09 2 35 $75,302 Group 4: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-5 Top Kit 08/14/09 2 35 $75,503 Group 27, 36, 68, 75, 90, 106-107: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-6 Top Kit 08/14/09 1 35 $75,007 Group 53, 77, 101-102, 126: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-7 Top Kit 11/05/09 1 35 $75,525 ### Page 56 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 56 of 1162 BOEING SERVICE BULLETIN 747-28A2280 Group 11, 48: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-8 Top Kit 11/05/09 1 35 $75,503 Group 18, 37, 105: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-9 Top Kit 08/14/09 1 35 $75,525 Group 26, 66: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-10 Top Kit 08/14/09 1 35 $75,848 Group 12: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-11 Top Kit 08/14/09 1 35 $75,525 Group 32, 49: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-12 Top Kit 08/14/09 1 35 $75,412 Group 23: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-13 Top Kit 08/14/09 1 35 $75,894 Group 35, 62: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-14 Top Kit 08/14/09 1 35 $75,007 Group 25, 85: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-15 Top Kit 08/14/09 1 35 $75,007 Group 33, 99: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-16 Top Kit 08/14/09 1 35 $75,007 ### Page 57 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 57 of 1162 BOEING SERVICE BULLETIN 747-28A2280 Group 30: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-17 Top Kit 08/14/09 1 35 $75,130 Group 51: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-18 Top Kit 08/14/09 1 35 $75,894 Group 55, 57: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-19 Top Kit 08/14/09 1 35 $75,007 Group 34: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-20 Top Kit 08/14/09 1 35 $75,007 Group 60, 78, 86: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-21 Top Kit 08/14/09 1 35 $75,523 Group 91, 98, 108: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-22 Top Kit 08/14/09 1 35 $75,525 Group 39: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-23 Top Kit 08/14/09 1 35 $75,524 Group 41: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-24 Top Kit 08/14/09 1 35 $75,412 Group 88-89, 94: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-25 Top Kit 08/14/09 1 35 $75,007 ### Page 58 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 58 of 1162 BOEING SERVICE BULLETIN 747-28A2280 Group 45: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-26 Top Kit 10/06/09 1 35 $75,525 Group 73-74: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-27 Top Kit 08/14/09 1 35 $75,503 Group 54: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-28 Top Kit 08/14/09 1 35 $75,033 Group 56: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-29 Top Kit 08/14/09 1 35 $75,444 Group 58: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-30 Top Kit 08/14/09 1 35 $75,007 Group 59: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-31 Top Kit 08/14/09 1 35 $75,525 Group 81-82: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-32 Top Kit 08/14/09 1 35 $75,524 Group 64: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-33 Top Kit 05/27/08 1 35 $75,894 Group 95-96: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-34 Top Kit 08/14/09 1 35 $75,848 ### Page 59 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 59 of 1162 BOEING SERVICE BULLETIN 747-28A2280 Group 67: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-35 Top Kit 08/14/09 1 35 $75,007 Group 80: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-36 Top Kit 08/14/09 1 35 $75,444 Group 100: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-37 Top Kit 08/14/09 1 35 $75,524 Group 109: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-38 Top Kit 08/14/09 1 35 $75,305 Group 9, 15, 44, 76, 97, 104, 114, 117-118, 120, 128, 130: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-39 Top Kit 08/14/09 7 35 $75,525 Group 111, 119: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-40 Top Kit 08/14/09 1 35 $75,524 Group 65: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-41 Top Kit 08/14/09 1 35 $75,412 Group 40: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-42 Top Kit 08/14/09 1 35 $75,848 Group 84: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-43 Top Kit 08/14/09 1 35 $75,894 ### Page 60 Original Issue: August 07, 2008 Revision 1: November 25, 2009 747-28A2280 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 60 of 1162 BOEING SERVICE BULLETIN 747-28A2280 The kits are subject to the terms and conditions of the Boeing standard purchase order acknowledgment. After the Unit Price date, new price and ROLT data is applicable. Prices are in United States dollars. Terms: Net 30 days. Group 103: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-44 Top Kit 08/14/09 1 35 $75,524 Group 50: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-45 Top Kit 08/14/09 1 35 $75,894 Group 116: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-46 Top Kit 08/14/09 1 35 $75,503 Group 121: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-47 Top Kit 10/29/09 1 35 $75,307 Group 1, 5, 7, 19-20, 38, 46-47, 115: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-48 Top Kit 10/29/09 1 35 $75,589 Group 14: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-49 Top Kit 10/29/09 1 35 $75,589 Group 13, 16, 22: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-50 Top Kit 10/29/09 1 35 $75,589 Group 122: Kit Number Name Date QTY ROLT (Weeks) Unit Price thru DEC 31/09 015U1807-51 Top Kit (a) - 35 $75,589 (a) Contact Boeing Spares The text continues at https://openairdocs.org/service-documents/boeing/747-28a2280/file/f8ad0efae5b6.md?from=61 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.