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McDonnell DouglasCommercial Airplanes DC10 Service Bulletin ALERT Number: DC10-28A261 Original Issue: December 01, 2009 ATA System: 2822 SUBJECT: FUEL - Engine Fuel Supply - Fuel Pump Housing Electrical Connector Assembly and Fuel Boost/Transfer Pump - Inspection/Replacement 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BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET Copyright © 2009 The Boeing Company Unpublished Work - All Rights Reserved Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable subject matter.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, KC-10, KDC-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.
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3.0
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Table of Contents
Summary5
1. PLANNING INFORMATION7
A. Effectivity7
1. Airplanes7
2. Spares Affected ........................................ 1 3 B. Concurrent Requirements ...................................... 1 3 C. Reason ................................................ 1 3 D. Description .............................................. 1 3 E. Compliance .............................................. 1 4 F. Approval ............................................... 1 8 G. Manpower .............................................. 1 8 H. Weight and Balance Changes .................................... 2 0 I. Electrical Load Data ......................................... 2 0 J. References .............................................. 2 0
1. Existing Data .......................................... 2 0
2. Data supplied with this Service Bulletin ............................ 2 1
3. Installation Drawings Used in the Preparation of this Service Bulletin ............ 2 1 K. Publications Affected ........................................ 2 1 L. Interchangeability and Intermixability of Parts ........................... 2 2
2. MATERIAL INFORMATION ........................................ 2 3 A. Material - Price and Availability ................................... 2 3 B. Industry Support Information .................................... 2 3 C. Parts Necessary For Each Airplane ................................. 2 3
1. Kits/Parts ............................................ 2 3
2. Parts and Materials Supplied by the Operator ........................ 2 9
3. Parts Modified and Reidentified ................................ 3 0
4. Parts Removed and Not Replaced .............................. 3 1 D. Parts Necessary to Change Spares ................................. 3 1 E. Special Tooling - Price and Availability ............................... 3 1 F. Special Tooling Necessary to do this Service Bulletin ....................... 3 1
3. ACCOMPLISHMENT INSTRUCTIONS .................................. 3 3 A. GENERAL INFORMATION ..................................... 3 3 B. WORK INSTRUCTIONS ....................................... 3 5 APPENDIX A: FUEL BOOST/TRANSFER PUMP WIRING CHART FOR PART NUMBER 60-84355-1 . . 44 APPENDIX B: FUEL PUMP HOUSING ELECTRICAL CONNECTOR ASSEMBLY REPLACEMENT WITH P/N 60-84351 ............................................ 4 7 APPENDIX C: FUEL BOOST/TRANSFER PUMP WIRING CHART FOR PART NUMBER 60-84351 . . . 50 APPENDIX D: FUEL PUMP HOUSING ELECTRICAL CONNECTOR ASSEMBLY FOR PART NUMBER 60-84355-1 INSPECTION LOGIC DIAGRAM ......................... 5 4 APPENDIX E: FUEL PUMP HOUSING ELECTRICAL CONNECTOR ASSEMBLY FOR PART NUMBER 60-84351 INSPECTION LOGIC DIAGRAM .......................... 5 5
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McDonnell DouglasCommercial Airplanes DC10 Service Bulletin ALERT SummaryNumber: DC10-28A261Original Issue: December 01, 2009 ATA System: 2822 SUBJECT: FUEL - Engine Fuel Supply - Fuel Pump Housing Electrical Connector Assembly and Fuel Boost/Transfer Pump - Inspection/Replacement
THIS BULLETIN IS SENT TO THE OPERATORS OF RECORD OF THE AIRPLANES SHOWN IN PARAGRAPH
1.A., EFFECTIVITY. IF AN AIRPLANE HAS BEEN LEASED OR SOLD, SEND THIS SERVICE BULLETIN TO THE NEW OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS SERVICE BULLETIN TO THE NEW OWNER.
CONCURRENT REQUIREMENTS Refer to Paragraph 1.B., Concurrent Requirements.
BACKGROUND MD-11 and DC-10 operators have reported instances of fuel pump housing electrical connector assembly, part number 60-84355-1, failures. Inspecting the fuel boost/transfer pump housing electrical connector assembly, fuel boost/transfer pump and replacing any non-serviceable part with a serviceable part as required based on inspection results, will minimize the possibility of a potential ignition source in the fuel tanks and potential fuel tank explosion. If not corrected, insulation resistance degradation and/or arcing in the potted backside of the fuel boost/transfer pump housing electrical connector assembly could compromise the performance of the fuel boost/transfer pump housing electrical connector assembly and result in a failure that can introduce an ignition source into the fuel tank and potential fuel tank explosion.
ACTION This service bulletin provides instructions to inspect/replace each fuel pump housing electrical connector assembly and fuel boost/transfer pump.
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, MD-10-10F and MD-10-30F Airplanes. Refer to Paragraph 1.A.1., Airplanes, for the list of affected airplanes.
COMPLIANCE Refer to Paragraph 1.E., Compliance.
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INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the configuration changes and repair procedures given in this service bulletin.
MANPOWER Refer to Paragraph 1.G., Manpower.
MATERIAL INFORMATION Boeing Supplied Kits/Parts.
Refer to Paragraph 2.A., Material - Price and Availability.
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McDonnell DouglasCommercial Airplanes DC10 Service Bulletin ALERT Number: DC10-28A261 Original Issue: December 01, 2009 ATA System: 2822 SUBJECT: FUEL - Engine Fuel Supply - Fuel Pump Housing Electrical Connector Assembly and Fuel Boost/Transfer Pump - Inspection/Replacement
THIS BULLETIN IS SENT TO THE OPERATORS OF RECORD OF THE AIRPLANES SHOWN IN PARAGRAPH
1.A., EFFECTIVITY. IF AN AIRPLANE HAS BEEN LEASED OR SOLD, SEND THIS SERVICE BULLETIN TO THE NEW OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS SERVICE BULLETIN TO THE NEW OWNER.
1. PLANNING INFORMATION A. Effectivity
1. Airplanes This service bulletin is applicable to airplanes that have installed fuel pump housing electrical connector assembly part number 60-84355-1 in accordance with Service Bulletin DC10-28A259.
NOTE: The fuel pump housing electrical connector replacement with part number 60-84351 was done on airplane fuselage number 342 prior to the original issue of this service bulletin in accordance with Drawing SP10280068 and FAA Alternative Method of Compliance (AMOC) approval letter with referenced Boeing letter CP-L4L-09-00243.
NOTE: Group 3 airplanes with Aft Aux tank installed must inspect fuel boost/transfer pump installation per this procedure, unless deactivated per SR10280047 "C" change (or later) Service Rework Drawing.
NOTE: DC-10-10 Airplanes with auxiliary upper fuel tanks that are modified to MD-10-10F configuration by Boeing Engineering will become Group 5 airplanes.
DESCRIPTIONCONFIGURATIONGROUP Airplanes with 1, 2, 3, and Auxiliary Upper Fuel Tanks.-1 Airplanes with 1, 2, 3, Auxiliary Upper and Lower Fuel Tanks.-2 Airplanes with 1, 2, 3, Auxiliary Upper, Lower, and AFT Fuel Tanks.-3 Airplanes with 1, 2, 3, Auxiliary Upper, Lower, FWD, AFT, and Wing Tip Fuel Tanks.
-4
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DESCRIPTIONCONFIGURATIONGROUP Airplanes with 1, 2, and 3 Fuel Tanks.-5 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-10-10F, MD-10-30F GroupFuselage Number 2100 2103 2106 2110 5112 2114 - 115 2117 5119 2122 - 123 2127 2129 2131 - 135 2137 5138 - 140 5142 5144 - 145 2146 - 147 5148 515 2150 2152 5153 - 155 2156 - 158 2160 5162 2165 - 166
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GroupFuselage Number 5169 517 2170 - 171 5173 2174 5177 2178 - 179 2183 - 184 2187 - 190 2192 5194 2195 - 196 5198 2199 12 2201 5203 2204 5205 2206 5207 - 210 2211 - 216 2220 - 221 2223 - 227 2229 - 230 2232 2234 - 236 2239 - 240 2242 2244 - 246 5247 2248
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GroupFuselage Number 5249 525 5250 1251 - 252 2253 - 257 526 2261 - 268 1269 527 5270 - 271 1272 5273 2274 - 275 2277 2281 - 282 1285 2286 2289 - 291 3292 5294 5296 - 298 2299 - 306 5307 2308 5309 2310 4311 2312 - 317 1318 5319 532 5321
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GroupFuselage Number 5323 2324 - 327 2329 533 2330 2332 4333 2334 - 338 534 2340 3341 2342 - 343 5344 3345 1346 5347 2349 535 5351 5353 2355 - 356 5358 4359 - 361 4363 2366 - 367 1372 4373 4375 - 378 5379 4380 2381 4383 - 389
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GroupFuselage Number 539 4390 - 399 540 4400 - 408 2409 541 4410 - 411 2412 4413 - 415 2416 4417 - 418 2419 542 4420 - 421 2422 4423 - 429 543 4430 - 432 2433 3434 - 438 4439 2440 4441 2442 - 446 555 559 56 561 - 62 165 570 172 576
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