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Commercial Airplanes DC10 Service Bulletin Number: DC10-28-256 Original Issue: June 24, 2014 ATA System: 2800 SUBJECT: FUEL - Fuel Systems - Change Fuel Pump Control and Indication System Wiring Export of this technology is controlled under the United States Export Administration Regulations (EAR) (15 CFR 300-774). 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 © 2014 Boeing.
Unpublished Work. All Rights Reserved.
Treatment of this document and its content is governed by contract with Boeing. Rights to use this document are licensed on a per aircraft basis and such rights may not be transferable. For more information, contact The Boeing Company.
Boeing, the Boeing signature, the Boeing symbol, 707, 717, 727, 737, 747, 757, 767, 777, 787, Dreamliner, BBJ, DC-8, DC-9, DC-10, KC-10, KC-46, KDC-10, MD-10, MD-11, MD-80, MD-88, MD-90, P-8, Poseidon and Boeing liveries 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.
Original Issue: June 24, 2014 DC10-28-256 1 of 99
4.0
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: June 24, 2014 DC10-28-256 2 of 99 BOEING SERVICE BULLETIN DC10-28-256
BLANK PAGE
Table of Contents
Summary5
1. PLANNING INFORMATION9
A. Effectivity9
1. Airplanes9
2. Spares Affected ........................................ 1 4 B. Concurrent Requirements ...................................... 1 4 C. Reason ................................................ 1 5 D. Description .............................................. 1 5 E. Compliance .............................................. 1 7 F. Approval ............................................... 1 7 G. Manpower .............................................. 1 7 H. Weight and Balance Changes .................................... 2 0 I. Electrical Load Data ......................................... 2 1 J. References .............................................. 2 5
1. Existing Data: ......................................... 2 5
2. Data Supplied with this Service Bulletin: ........................... 2 5
3. Installation Drawings Used in the Preparation of this Service Bulletin: ........... 2 6
4. Process Data: ......................................... 2 6 K. Publications Affected ........................................ 2 6 L. Interchangeability and Intermixability of Parts ........................... 2 6 M. Software Accomplishment Summary ................................ 2 6
2. MATERIAL INFORMATION ........................................ 2 7 A. Material - Price and Availability ................................... 2 7 B. Industry Support Information .................................... 2 7 C. Parts Necessary for Each Airplane ................................. 2 7
1. Kits/Parts ............................................ 2 7
2. Parts and Materials Supplied by the Operator ........................ 3 9
3. Parts Modified and Reidentified ................................ 3 9
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 2 APPENDIX A: FUEL PUMPS UNCOMMANDED ON DETECTION CIRCUIT TEST PROCEDURE [Group 1, 4] .................................................. 4 7 APPENDIX B: FUEL PUMPS UNCOMMANDED ON DETECTION CIRCUIT TEST PROCEDURE [Group 2-3, 5-6] ............................................... 5 3 APPENDIX C: FUEL PUMPS UNCOMMANDED ON DETECTION CIRCUIT TEST PROCEDURE [Group 9] .................................................. 6 3 APPENDIX D: FUEL PUMPS UNCOMMANDED ON DETECTION CIRCUIT TEST PROCEDURES [Group 8] .................................................. 7 4 APPENDIX E: INPUT SURVEY ........................................ 9 9 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: June 24, 2014 DC10-28-256 3 of 99 BOEING SERVICE BULLETIN DC10-28-256
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: June 24, 2014 DC10-28-256 4 of 99 BOEING SERVICE BULLETIN DC10-28-256
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Commercial Airplanes DC10 Service Bulletin SummaryNumber: DC10-28-256Original Issue: June 24, 2014 ATA System: 2800 SUBJECT: FUEL - Fuel Systems - Change Fuel Pump Control and Indication System Wiring
CONCURRENT REQUIREMENTS Refer to Paragraph 1.B., Concurrent Requirements.
BACKGROUND Frictional heating or sparking resulting from fuel pump failure, wear of fuel pump rotating components, or ingestion of debris by the fuel pump, may result in development of a fuel tank ignition source. Frictional heating or sparking in fuel pump inlets or priming system outlets exposed (i.e. not covered by fuel) to the tank ullage in combination with the ullage being flammable, may result in a fuel tank ignition event. Center wing auxiliary, fuselage auxiliary, and wing tip compartment (KC-10 only) fuel tanks may be subject to this condition since they are normally pumped dry over the course of a mission. A fuel tank ignition event could develop with a fuel pump running in an empty tank if the normal shutoff command is delayed or as a result of control system failures that keep the fuel pump in a latent uncommanded running condition. To ensure a timely fuel pump shutoff command revise flight crew shutoff procedures for center wing auxiliary, fuselage auxiliary, and wing tip compartment (KC-10 only) fuel tanks. To address the latent fuel pump uncommanded running condition change center wing auxiliary, fuselage auxiliary, and wing tip compartment (KC-10 only) fuel pump control and indication system wiring to detect and indicate fuel pump uncommanded running conditions. If not corrected, a fuel tank pump running in an empty fuel tank may result in a fuel tank ignition event.
This service bulletin is the result of the safety assessments conducted by Boeing under a Special Federal Aviation Regulation (SFAR) 88, Fuel Tank System Fault Tolerance Evaluation Requirements.
Boeing Fleet Team Digest (FTD) DC-10, MD-10 FTD 28-13001 and DC-10, MD-10 FTD 28-13003 are related to this service bulletin.
ACTION This service bulletin changes fuel pump control and indication system wiring.
EFFECTIVITY DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F, DC-10-30F(KC-10A), DC-10-30F(KDC-10), DC-10-40, DC-10-40F and MD-10-30F Airplanes. Refer to Paragraph 1.A.1., Airplanes for the list of affected airplanes.
COMPLIANCE Federal Aviation Administration (FAA) Airworthiness Directive AD 2013-08-23 is related to this service bulletin.
Boeing recommends that the change given in this service bulletin be done within 60 months after the effective date of AD 2013-08-23.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: June 24, 2014 DC10-28-256 5 of 99
INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the configuration changes given in this service bulletin.
MANPOWER Elapsed HoursTotal Task HoursGroup(s)
18.436.81
31.462.82-3, 9
25.651.24
10.120.25
31.663.26
41.583.07
48.697.28
MATERIAL INFORMATION Boeing Supplied Kits/Parts.
Refer to Paragraph 2.A., Material - Price and Availability.
Operators are encouraged to complete the survey provided in APPENDIX E of this service bulletin to help Boeing predict the quantity and timing of the Boeing Supplied Kits/Parts.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: June 24, 2014 DC10-28-256 6 of 99 BOEING SERVICE BULLETIN DC10-28-256
BOEING SERVICE BULLETIN DC10-28-256
CENTER ACCESSORY
COMPARTMENT
FORWARD CARGO
COMPARTMENT
RIGHT SIDE
AIR CONDITIONING
COMPARTMENT
RIGHT SIDE
ELECTRICAL POWER CENTER
FORWARD CARGO
COMPARTMENT
LEFT SIDE
AIR CONDITIONING
LOWER NOSE AND AVIONICS LEFT SIDE COMPARTMENT
COMPARTMENT CHANGE FUEL PUMP CONTROL 1845432
AND INDICATION SYSTEM WIRING Original Issue: June 24, 2014 Export Controlled ECCN: 9E991 - BOEING DC10-28-256 PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 7 of 99
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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Commercial Airplanes DC10 Service Bulletin Number: DC10-28-256 Original Issue: June 24, 2014 ATA System: 2800 SUBJECT: FUEL - Fuel Systems - Change Fuel Pump Control and Indication System Wiring
1. PLANNING INFORMATION A. Effectivity
1. Airplanes This service bulletin is for the airplanes shown below.
DESCRIPTIONCONFIGURATIONGROUP DC-10-10 and DC-10-15 Airplanes that change fuel pump control and indication system wiring to detect and indicate uncommanded fuel pump running conditions in accordance with SR10280072-7001, -7002 and SR10280073-7001 drawing configurations.
-1 DC-10-30, DC-10-30F and DC-10-30F (KDC-10) Airplanes that change fuel pump control and indication system wiring to detect and indicate uncommanded fuel pump running conditions in accordance with SR10280072-7003, -7004 and SR10280073-7003 drawing configurations.
-2 DC-10-30, DC-10-30F, DC-10-40 and DC-10-40F Airplanes that change fuel pump control and indication system wiring to detect and indicate uncommanded fuel pump running conditions in accordance with SR10280072-7005, -7006 and SR10280073-7005 drawing configurations.
-3 DC-10-10F Airplanes that change fuel pump control and indication system wiring to detect and indicate uncommanded fuel pump running conditions in accordance with SR10280072-7007, -7008 and SR10280073-7007 drawing configurations.
-4 DC-10-30F Airplanes that change fuel pump control and indication system wiring to detect and indicate uncommanded fuel pump running conditions in accordance with SR10280072-7009, -7010 and SR10280073-7009 drawing configurations.
-5 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: June 24, 2014 DC10-28-256 9 of 99
DESCRIPTIONCONFIGURATIONGROUP DC-10-30 Airplanes that change fuel pump control and indication system wiring to detect and display uncommanded fuel pump running conditions in accordance with SR10280072-7011, -7012 and SR10280073-7011 drawing configurations.
-6 DC-10-30F (KC-10A) Airplanes that change fuel pump control and indication system wiring to detect and indicate uncommanded fuel pump running conditions in accordance with SR10280072-7013, -7014 and SR10280073-7013 drawing configurations.
-7 DC-10-30F and MD-10-30F Airplanes that change fuel pump control and indication system wiring to detect and indicate uncommanded fuel pump running conditions in accordance with SR10280069-7001, -7002 and SR10280070-7001 drawing configurations.
-8 DC-10-30 Airplanes with AFT AUX tank that change fuel pump control and indication system wiring to detect and indicate uncommanded fuel pump running conditions in accordance with SR10280072-7005, -7006 and SR10280073-7005 drawing configurations.
-9 Airplane Models:
DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F, DC-10-30F (KC-10A), DC-10-30F (KDC-10), DC-10-40, DC-10-40F, MD-10-30F GroupFuselage Number 12 360 165 371 172 483 390 896 399 3100 8103 2106 8110 3114 - 115 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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GroupFuselage Number 3117 3122 - 123 2127 3129 3131 - 135 3137 3146 - 147 3150 3152 3156 - 158 3160 2165 3166 3170 - 171 3174 3178 - 179 3183 - 184 3187 - 189 3190 3192 3195 - 196 3199 3201 3204 3206 3211 - 216 8219 3220 - 221 3223 - 227 3229 3230 3232 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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GroupFuselage Number 3234 2235 3236 3239 3240 3242 3244 - 246 2248 1251 - 252 2253 3254 2255 3256 8257 3261 - 263 2264 3265 - 266 2267 3268 3274 - 275 8277 3281 8282 1285 3286 3289 3290 - 291 9292 3299 3300 - 301 5302 - 303 3304 - 306 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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