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McDonnell DouglasCommercial Airplanes DC9 Service Bulletin Number: DC9-28-212 Original Issue: February 22, 2008 Revision 1: June 16, 2009 ATA System: 2822 SUBJECT: FUEL - Pump Fuel Boost - Change or Replace Fuel Boost Pumps Export of this technology is controlled under the United States Export Administration Regulations (EAR) (15 CFR 730-774). An export license may be required before it is used for development, production or use by foreign persons from specific countries. The controller of this data has the individual responsibility to abide by all export laws.
9E991ECCN:
BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET Copyright © 2008 The Boeing Company Unpublished Work - All Rights Reserved Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable subject matter.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, the Boeing signature, the Boeing symbol, 707, 717, 727, 737, 747, 757, 767, 777, 787, Dreamliner, BBJ, DC-8, DC-9, DC-10, MD-10, MD-11, MD-80, MD-88, MD-90, P-8A, Poseidon and the Boeing livery are all trademarks owned by The Boeing Company; and no trademark license is granted in connection with this document unless provided in writing by Boeing.
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 22, 2008 DC9-28-212Revision 1: June 16, 2009 1 of 48
2.0
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 22, 2008 DC9-28-212Revision 1: June 16, 2009 2 of 48 BOEING SERVICE BULLETIN DC9-28-212
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Table of Contents
Revision Transmittal Sheet5
Summary7
1. PLANNING INFORMATION ........................................ 1 1 A. Effectivity ............................................... 1 1
1. Airplanes ............................................ 1 1
2. Spares Affected ........................................ 3 1 B. Concurrent Requirements ...................................... 3 2 C. Reason ................................................ 3 2 D. Description .............................................. 3 2 E. Compliance .............................................. 3 5 F . Approval ............................................... 3 5 G. Manpower .............................................. 3 5 H. Weight and Balance Changes .................................... 3 7 I. Electrical Load Data ......................................... 3 7 J. References .............................................. 3 7
1. Existing Data: .......................................... 3 7
2. Data supplied with this Service Bulletin: ........................... 3 7
3. Installation Drawings Used in the Preparation of this Service Bulletin: ........... 3 7 K. Publications Affected ......................................... 3 8 L. Interchangeability and Intermixability of Parts ........................... 3 8
2. MATERIAL INFORMATION ........................................ 3 9 A. Material - Price and Availability ................................... 3 9 B. Industry Support Information .................................... 3 9 C. Parts Necessary For Each Airplane ................................. 3 9
1. Kits/Parts: ............................................ 3 9
2. Parts and Materials Supplied by the Operator: ........................ 3 9
3. Parts Modified and Reidentified: ................................ 4 0
4. Parts Removed and Not Replaced: .............................. 4 0 D. Parts Necessary to Change Spares ................................. 4 0 E. Special Tooling - Price and Availability ............................... 4 0 F . Special Tooling Necessary to do this Service Bulletin ....................... 4 0
3. ACCOMPLISHMENT INSTRUCTIONS .................................. 4 1 A. GENERAL INFORMATION ..................................... 4 1 B. WORK INSTRUCTIONS ....................................... 4 1 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 22, 2008 DC9-28-212Revision 1: June 16, 2009 3 of 48 BOEING SERVICE BULLETIN DC9-28-212
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 22, 2008 DC9-28-212Revision 1: June 16, 2009 4 of 48 BOEING SERVICE BULLETIN DC9-28-212
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McDonnell DouglasCommercial Airplanes DC9 Service Bulletin Revision Transmittal SheetNumber: DC9-28-212Original Issue: February 22, 2008 Revision 1: June 16, 2009 ATA System: 2822 SUBJECT: FUEL - Pump Fuel Boost - Change or Replace Fuel Boost Pumps This revision includes all pages of the service bulletin.
COMPLIANCE INFORMATION RELATED TO THIS REVISION Federal Aviation Administration (FAA) Notice of Proposed Rule Making 2008-NM-113-AD, is related to this service bulletin.
No more work is necessary on airplanes changed in accordance with the original issue of this service bulletin.
REASON FOR REVISION This revision is sent to change the Revision level of Argo-Tech Service Bulletin 398000-28-2 to Revision 1.
These sections were changed:
1. In Paragraph 1.B., Concurrent Requirements, changed Argo-Tech Service Bulletin Revision level.
2. In Paragraph 1.D., Description, added Affected Maintenance Zones Table.
3. In Paragraph 1.E., Compliance, added Notice of Proposed Rule Making (NPRM) statements.
4. In Paragraph 1.F ., Approval, added Revision 1.
5. In Paragraph 1.J.1., Existing Data, changed Argo-Tech Bulletin 398000-28-2 Revision level and added FAA Notice of Proposed Rule Making.
6. In Paragraph 1.K., Publication Affected, removed Special Compliance Item Report Revision level.
7. In Paragraph 3.B., Work Instructions, changed Argo-Tech Service Bulletin 398000-28-2 Revision level.
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 February 22, 2008Original Issue:
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 22, 2008 DC9-28-212Revision 1: June 16, 2009 5 of 48
June 16, 2009Revision 1:
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 22, 2008 DC9-28-212Revision 1: June 16, 2009 6 of 48 BOEING SERVICE BULLETIN DC9-28-212
McDonnell DouglasCommercial Airplanes DC9 Service Bulletin SummaryNumber: DC9-28-212Original Issue: February 22, 2008 Revision 1: June 16, 2009 ATA System: 2822 SUBJECT: FUEL - Pump Fuel Boost - Change or Replace Fuel Boost Pumps
CONCURRENT REQUIREMENTS Refer to Paragraph 1.B., Concurrent Requirements.
BACKGROUND The Special Federal Aviation Regulation (SFAR 88) safety review has determined the need to protect the fuel boost pump stator lead wires from being able to contact the pump rotor/shaft assembly. Lead wire contact and the resulting chafing may result in an ignition source (energized rotor assembly) being produced in the fuel boost pump inlet that could propagate into the fuel tank when the fuel boost pump inlet is not fully covered by fuel.
Replacement of the fuel boost pump will minimize the risk of a potential arc/spark condition that may occur within the airplane's fuel tanks at critical fuel boost pumps in the center wing, forward and aft auxiliary fuel tanks. If not corrected, there is a potential that an arc/spark condition could occur within the fuel boost pumps and propagate into the fuel tank.
This service bulletin is the result of the safety assessments conducted by Boeing under SFAR 88, "Fuel Tank System Fault Tolerance Evaluation Requirements".
ACTION Refer to Paragraph 1.D., Description.
EFFECTIVITY All MD-80 and DC-9-31, DC-9-32, DC-9-32(VC9C), DC-9-32F , DC-9-32F(C-9A), DC-9-32F(C-9B), DC-9-33F , DC-9-34, DC-9-34F , DC-9-41 and DC-9-51 Airplanes. Refer to Paragraph 1.A.1., Airplanes for affected airplanes.
COMPLIANCE Federal Aviation Administration (FAA) Notice of Proposed Rule Making 2008-NM-113-AD, is related to this service bulletin.
Boeing recommends accomplishment of this service bulletin within 5 years after original issue date of service bulletin.
INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the configuration changes given in this service bulletin.
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 22, 2008 DC9-28-212Revision 1: June 16, 2009 7 of 48
MANPOWER Refer to Paragraph 1.G., Manpower.
MATERIAL INFORMATION Refer to Paragraph 2.A., Material - Price and Availability.
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 22, 2008 DC9-28-212Revision 1: June 16, 2009 8 of 48 BOEING SERVICE BULLETIN DC9-28-212
BOEING SERVICE BULLETIN DC9-28-212 MD-80 AND DC-9 (FORWARD AUXILIARY TANK) MD-80 (CENTER WING TANK) MD-80 AND DC-9 (AFT AUXILIARY TANK) CHANGE OR REPLACE FUEL BOOST PUMPS 1399743 Original Issue: February 22, 2008 Revision 1: June 16, 2009 DC9-28-212 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 9 of 48
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 22, 2008 DC9-28-212Revision 1: June 16, 2009 10 of 48 BOEING SERVICE BULLETIN DC9-28-212
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McDonnell DouglasCommercial Airplanes DC9 Service Bulletin Number: DC9-28-212 Original Issue: February 22, 2008 Revision 1: June 16, 2009 ATA System: 2822 SUBJECT: FUEL - Pump Fuel Boost - Change or Replace Fuel Boost Pumps
1. PLANNING INFORMATION A. Effectivity
1. Airplanes This service bulletin is for the airplanes shown below.
DESCRIPTIONCONFIGURATIONGROUP Change or replace fuel boost pumps in the center wing tank.-1 Applicable to MD-80 airplanes with fuel boost pump 398000-1.1 Applicable to MD-80 airplanes with fuel boost pump 65-5093-4.2 Change or replace fuel boost pumps in the center wing and aft auxiliary tanks.
-2 Applicable to MD-80 airplanes with fuel boost pump 398000-1.1 Applicable to MD-80 airplanes with fuel boost pump 65-5093-4.2 Change or replace fuel boost pumps in the center wing, forward and aft auxiliary tanks.
-3 Applicable to MD-80 airplanes with fuel boost pump 398000-1.1 Applicable to MD-80 airplanes with fuel boost pump 65-5093-4.2 Change or replace single fuel boost pump in the forward auxiliary tank.
-4 Applicable to DC-9 airplanes with fuel boost pump 398000-1.1 Applicable to DC-9 airplanes with fuel boost pump 65-5093-4.2 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 22, 2008 DC9-28-212Revision 1: June 16, 2009 11 of 48
DESCRIPTIONCONFIGURATIONGROUP Change or replace single fuel boost pump in the forward auxiliary tank and dual fuel boost pumps on the aft auxiliary tank.
-5 Applicable to DC-9 airplanes with fuel boost pump 398000-1.1 Applicable to DC-9 airplanes with fuel boost pump 65-5093-4.2 Change or replace dual fuel boost pumps in the forward auxiliary tank.
-6 Applicable to DC-9 airplanes with fuel boost pump 398000-1.1 Applicable to DC-9 airplanes with fuel boost pump 65-5093-4.2 Change or replace dual fuel boost pumps in the forward and aft auxiliary tanks.
-7 Applicable to DC-9 airplanes with fuel boost pump 398000-1.1 Applicable to DC-9 airplanes with fuel boost pump 65-5093-4.2 Change or replace dual fuel boost pumps in the aft auxiliary tank.-8 Applicable to DC-9 airplanes with fuel boost pump 398000-1.1 Applicable to DC-9 airplanes with fuel boost pump 65-5093-4.2 Airplane Models:
DC-9-31, DC-9-32, DC-9-32(VC-9C), DC-9-32F , DC-9-32F(C-9A), DC-9-32F(C-9B), DC-9-33F , DC-9-34, DC-9-34F , DC-9-41, DC-9-51, DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), MD-88 GroupFuselage Number 11000 - 1006 11011 - 1013 11015 - 1016 11018 - 1020 11025 11028 11031 - 1032 11034 - 1035 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 22, 2008 DC9-28-212Revision 1: June 16, 2009 12 of 48 BOEING SERVICE BULLETIN DC9-28-212