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Commercial Airplanes DC10 Service Bulletin Number: DC10-28-244 Original Issue: February 25, 2010 ATA System: 2811 SUBJECT: FUEL - Integral Fuel Tanks - Inspection and Replacement of Wire Shielding above Center Upper Auxiliary Fuel Tank 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BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET Copyright © 2010 The Boeing Company Unpublished Work - All Rights Reserved Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable subject matter.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.
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 25, 2010 DC10-28-244 1 of 130
2.0
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 25, 2010 DC10-28-244 2 of 130 BOEING SERVICE BULLETIN DC10-28-244
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Table of Contents
Summary5
1. PLANNING INFORMATION9
A. Effectivity9
1. Airplanes9
2. Spares Affected ........................................ 1 3 B. Concurrent Requirements ...................................... 1 3 C. Reason ................................................ 1 4 D. Description .............................................. 1 4 E. Compliance .............................................. 1 5 F. Approval ............................................... 1 5 G. Manpower .............................................. 1 6 H. Weight and Balance Changes .................................... 1 7 I. Electrical Load Data ......................................... 1 8 J. References .............................................. 1 8
1. Existing Data: ......................................... 1 8
2. Data supplied with this Service Bulletin: ........................... 1 8
3. Installation Drawings Used in the Preparation of this Service Bulletin: ........... 1 8 K. Publications Affected ........................................ 1 8 L. Interchangeability and Intermixability of Parts ........................... 1 9
2. MATERIAL INFORMATION ........................................ 2 1 A. Material - Price and Availability ................................... 2 1 B. Industry Support Information .................................... 2 1 C. Parts Necessary For Each Airplane ................................. 2 1
1. Kits/Parts: ........................................... 2 1
2. Parts and Materials Supplied by the Operator: ........................ 2 6
3. Parts Modified and Reidentified: ............................... 2 6
4. Parts Removed and Not Replaced: .............................. 2 6 D. Parts Necessary to Change Spares ................................. 2 7 E. Special Tooling - Price and Availability ............................... 2 7 F. Special Tooling Necessary to do this Service Bulletin ....................... 2 7
3. ACCOMPLISHMENT INSTRUCTIONS .................................. 2 9 A. GENERAL INFORMATION ..................................... 2 9 B. WORK INSTRUCTIONS ....................................... 3 2 FIGURE 1: WIRES ABOVE AUXILIARY FUEL TANK LEFT SIDE - FLOOR BEAM CLAMPS - REMOVAL [Group 1] ............................................ 4 0 FIGURE 2: WIRES ABOVE AUXILIARY FUEL TANK LEFT SIDE - BARRIER/SHIELD SLEEVING - INSTALLATION [Group 1] ................................... 4 6 FIGURE 3: WIRES ABOVE AUXILIARY FUEL TANK LEFT SIDE - CLAMPS AND EXTRUDED CHANNEL
- INSTALLATION [Group 1] .................................. 4 9 FIGURE 4: WIRES ABOVE AUXILIARY FUEL TANK RIGHT SIDE - FLOOR BEAM CLAMPS - REMOVAL [Group 1-2, 4] .......................................... 5 5 FIGURE 5: WIRES ABOVE AUXILIARY FUEL TANK RIGHT SIDE - BARRIER/SHIELD SLEEVING - INSTALLATION [Group 1-2, 4] ................................ 6 0 FIGURE 6: WIRES ABOVE AUXILIARY FUEL TANK RIGHT SIDE - CLAMPS AND EXTRUDED CHANNEL
- INSTALLATION [Group 1-2, 4] ................................ 6 3
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FIGURE 7: WIRES ABOVE AUXILIARY FUEL TANK LEFT SIDE - FLOOR BEAM CLAMPS - REMOVAL [Group 2] ............................................ 6 8 FIGURE 8: WIRES ABOVE AUXILIARY FUEL TANK LEFT SIDE - BARRIER/SHIELD SLEEVING - INSTALLATION [Group 2] ................................... 7 4 FIGURE 9: WIRES ABOVE AUXILIARY FUEL TANK LEFT SIDE - CLAMPS AND EXTRUDED CHANNEL
- INSTALLATION [Group 2] .................................. 7 7 FIGURE 10: FORWARD CARGO D SECTION RIGHT SIDE - BARRIER/SHIELD SLEEVING - INSTALLATION [Group 2] ............................................ 8 4 FIGURE 11: WIRES ABOVE AUXILIARY FUEL TANK LEFT SIDE - FLOOR BEAM CLAMPS - REMOVAL [Group 3] ............................................ 8 6 FIGURE 12: WIRES ABOVE AUXILIARY FUEL TANK LEFT SIDE - BARRIER/SHIELD SLEEVING - INSTALLATION [Group 3] ................................... 9 2 FIGURE 13: WIRES ABOVE AUXILIARY FUEL TANK LEFT SIDE - CLAMPS AND EXTRUDED CHANNEL
- INSTALLATION [Group 3] .................................. 9 5 FIGURE 14: WIRES ABOVE AUXILIARY FUEL TANK RIGHT SIDE - FLOOR BEAM CLAMPS - REMOVAL [Group 3] ............................................ 1 0 1 FIGURE 15: WIRES ABOVE AUXILIARY FUEL TANK RIGHT SIDE - BARRIER/SHIELD SLEEVING - INSTALLATION [Group 3] .................................. 1 0 7 FIGURE 16: WIRES ABOVE AUXILIARY FUEL TANK RIGHT SIDE - CLAMPS AND EXTRUDED CHANNEL
- INSTALLATION [Group 3] .................................. 1 1 0 FIGURE 17: WIRES ABOVE AUXILIARY FUEL TANK LEFT SIDE - FLOOR BEAM CLAMPS - REMOVAL [Group 4] ............................................ 1 1 6 FIGURE 18: WIRES ABOVE AUXILIARY FUEL TANK LEFT SIDE - BARRIER/SHIELD SLEEVING - INSTALLATION [Group 4] .................................. 1 2 1 FIGURE 19: WIRES ABOVE AUXILIARY FUEL TANK LEFT SIDE - CLAMPS AND EXTRUDED CHANNEL
- INSTALLATION [Group 4] .................................. 1 2 4 APPENDIX A: TYPICAL CLAMP ATTACHMENTS ............................. 1 3 0
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Original Issue: February 25, 2010 DC10-28-244 4 of 130 BOEING SERVICE BULLETIN DC10-28-244
Commercial Airplanes DC10 Service Bulletin SummaryNumber: DC10-28-244Original Issue: February 25, 2010 ATA System: 2811 SUBJECT: FUEL - Integral Fuel Tanks - Inspection and Replacement of Wire Shielding above Center Upper Auxiliary Fuel Tank
CONCURRENT REQUIREMENTS None.
BACKGROUND Boeing Special Federal Aviation Regulations (SFAR) 88 engineering investigations have determined that wires routed above the center upper auxiliary fuel tank are in close proximity to the upper surface of the tank. In addition, some wire harness mounts may have loosened, allowing the wires to contact the tank. This condition can cause wire damage or chafing that could lead to possible arcing and sparking on the fuel tank upper surface.
Inspection will determine the condition of the wires. Installation of nonmetallic barrier/shield sleeving, new clamps, and new extruded channels to support the wires will minimize the possibility of wires contacting the fuel tank upper surface. If not corrected, wires in contact with the fuel tank could become damaged, and the resulting possible arcing and sparking could lead to burn-through of the upper surface of the fuel tank and potentially result in an explosion.
This service bulletin resulted from the safety assessments conducted by Boeing under Special Federal Aviation Regulations (SFAR) 88, Fuel Tank System Fault Tolerance Evaluation Requirements.
ACTION This service bulletin provides instructions to do as follows:
1. Does a General Visual Inspection of the wire bundles to determine if wires touch the upper surface of the center upper auxiliary fuel tank and marks those locations.
2. Does a Detailed Inspection of the wires routed above the center upper auxiliary fuel tank for splices and other damage (such as wire chafing, arcing, and broken insulation) to wire bundles and does corrective action as necessary.
3. Does a Detailed Inspection of the upper surface of the center upper auxiliary fuel tank for damage to the fuel barrier seal and does corrective action as necessary.
4. Installs nonmetallic barrier/shield sleeving to the wire harnesses, new clamps, new attaching hardware, and new extruded channels to raise the wire harnesses off the upper surface of the center upper auxiliary fuel tank.
This service bulletin assumes that the area above the center upper auxiliary fuel tank is open and access is available to all the floor beams for maintenance.
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Original Issue: February 25, 2010 DC10-28-244 5 of 130
EFFECTIVITY 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 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 the inspection and change given in this service bulletin be done within 5 years, after the original issue date of this service bulletin.
INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the inspection and configuration changes given in this service bulletin.
MANPOWER Group 1:
Elapsed HoursTotal Task HoursAirplanes
79.5216.0DC-10-30, DC-10-30F and DC-10-30F (KDC-10) Group 2:
Elapsed HoursTotal Task HoursAirplanes
74.0248.0DC-10-30F (KC-10A) Group 3:
Elapsed HoursTotal Task HoursAirplanes
79.5216.0DC-10-30F and MD-10-30F Group 4:
Elapsed HoursTotal Task HoursAirplanes
79.5216.0DC-10-40 and DC-10-40F
MATERIAL INFORMATION Boeing Supplied Kits/Parts.
Refer to Paragraph 2.A., Material - Price and Availability.
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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BOEING SERVICE BULLETIN DC10-28-244
INSPECTION AND REPLACEMENT OF WIRE SHIELDING
ABOVE CENTER UPPER AUXILIARY FUEL TANK 1695773 Original Issue: February 25, 2010 BOEING PROPRIETARY - DC10-28-244 Copyright © Unpublished Work - See page 1 for details. 7 of 130
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Commercial Airplanes DC10 Service Bulletin Number: DC10-28-244 Original Issue: February 25, 2010 ATA System: 2811 SUBJECT: FUEL - Integral Fuel Tanks - Inspection and Replacement of Wire Shielding above Center Upper Auxiliary Fuel Tank
1. PLANNING INFORMATION A. Effectivity
1. Airplanes This service bulletin is for the airplanes shown below.
NOTE: When any Group 1 airplane shown below is modified to a freighter configuration by Boeing Passenger to Freighter (P to F) engineering, it will become a Group 3 airplane.
DESCRIPTIONCONFIGURATIONGROUP DC-10-30, DC-10-30F and DC-10-30F (KDC-10) Airplanes-1 DC-10-30F (KC-10A) Airplanes-2 DC-10-30F and MD-10-30F Airplanes-3 DC-10-40 and DC-10-40F Airplanes-4 Airplane Models:
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 1100 3103 1106 3110 1114 - 115 1117
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GroupFuselage Number 1121 - 123 1127 1129 1131 - 135 1137 1146 - 147 1149 - 150 1152 1156 - 160 1165 - 166 1170 - 171 1174 1178 - 179 1183 - 184 1186 - 190 1192 1195 - 196 1199 1201 1204 4206 1211 4212 1213 - 215 4216 1217 3219 4220 1221 1223 4224 1225 - 227
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GroupFuselage Number 1229 4230 1231 - 232 1234 - 236 1239 - 242 1244 - 246 1248 1253 - 256 3257 1259 - 261 4262 1263 - 264 4265 1266 - 268 4274 1275 3277 1278 1280 - 281 3282 1286 - 293 1295 1299 - 303 4304 1305 4306 4308 4310 2311 1312 4313 1314 - 316
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GroupFuselage Number 3317 1324 - 325 3326 1327 1329 3330 1331 - 332 2333 1334 - 339 4340 1341 - 342 4343 1345 4349 1352 1355 - 356 2359 - 361 2363 1364 4366 - 367 1368 - 370 2373 2375 - 378 2380 4381 2383 - 408 3409 2410 - 411 3412 2413 - 415 3416 2417 - 418
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