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McDonnell DouglasCommercial Airplanes DC10 Service Bulletin Number: DC10-28-252 Original Issue: November 25, 2008 Revision 1: January 06, 2010 ATA System: 2800 SUBJECT: FUEL - Fuel Systems - Install Fuel Tank Float Level Switch and Aft Auxiliary Tank Fuel Pump Pressure Switch In-line Fuses 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BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET Copyright © 2008 The Boeing Company Unpublished Work - All Rights Reserved Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable subject matter.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, 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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Table of Contents
Revision Transmittal Sheet5
Summary7
1. PLANNING INFORMATION9
A. Effectivity9
1. Airplanes9
2. Spares Affected ........................................ 1 5 B. Concurrent Requirements ...................................... 1 5 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 .................................... 1 9 I. Electrical Load Data ......................................... 1 9 J. References .............................................. 2 0
1. Existing Data: ......................................... 2 0
2. Data supplied with this Service Bulletin: ........................... 2 0
3. Installation Drawings Used in the Preparation of this Service Bulletin: ........... 2 0
4. Process Data: ......................................... 2 0 K. Publications Affected ........................................ 2 0 L. Interchangeability and Intermixability of Parts ........................... 2 1
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: ........................ 3 7
3. Parts Modified and Reidentified: ............................... 3 7
4. Parts Removed and Not Replaced: .............................. 3 7 D. Parts Necessary to Change Spares ................................. 3 7 E. Special Tooling - Price and Availability ............................... 3 7 F. Special Tooling Necessary to do this Service Bulletin ....................... 3 7
3. ACCOMPLISHMENT INSTRUCTIONS .................................. 3 9 A. GENERAL INFORMATION ..................................... 3 9 B. WORK INSTRUCTIONS ....................................... 4 0 Appendix A: FUEL TANK 1 - MD-10-10F AND MD-10-30F [Group 1-2] .................. 4 6 Appendix B: FUEL TANK 1 - DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30 W/AFT TANK 1500 AND 3200 GALLONS, DC-10-30F, DC-10-30F (KC-10A), DC-10-30F (KDC-10), DC-10-40, DC-10-40F [Group 3-7] ..................................... 4 7 Appendix C: FUEL TANK 2 - MD-10-10F AND MD-10-30F [Group 1-2] .................. 4 8 Appendix D: FUEL TANK 2 - 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 [Group 3, 6-7] ................. 4 9 Appendix E: FUEL TANK 2 - DC-10-30 W/AFT TANK 1500 AND 3200 GALLONS [Group 4-5] ..... 5 0 Appendix F: FUEL TANK 3 - MD-10-10F AND MD-10-30F [Group 1-2] .................. 5 1
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Appendix G: FUEL TANK 3 - DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30 W/AFT TANK 1500 AND 3200 GALLONS, DC-10-30F, DC-10-30F (KC-10A), DC-10-30F (KDC-10), DC-10-40, DC-10-40F [Group 3-7] ..................................... 5 2 Appendix H: UPPER AND LOWER AUXILIARY FUEL TANKS - MD-10-30F [Group 2] ......... 5 3 Appendix I: CENTER WING TANKS - DC-10-30F (KC-10A) AND DC-10-30F (KDC-10) [Group 6-7] . 54 Appendix J: FORWARD AND AFT AUXILIARY - DC-10-30F (KC-10A) [Group 6] ............ 5 5 Appendix K: AFT AUXILIARY FUEL TANK - DC-10-30 W/AFT TANK 1500 GALLONS [Group 4] .... 5 6 Appendix L: UPPER AND LOWER AUXILIARY TANKS - DC-10-30 W/AFT 1500 AND 3200 GALLONS [Group 4-5] ........................................... 5 7 Appendix M: AFT AUXILIARY FUEL TANK - DC-10-30 W/AFT 3200 GALLONS [Group 5] ....... 5 8 Appendix N: MD-10-10F - FUSE FUNCTIONAL TEST [Group 1] ..................... 5 9 Appendix O: MD-10-30F - FUSE FUNCTIONAL TEST [Group 2] ..................... 6 0 Appendix P: DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F, DC-10-40 AND DC-10-40F - FUSE FUNCTIONAL TEST [Group 3] ................................ 6 2 Appendix Q: DC-10-30 W/AFT TANK 1500 GALLONS - FUSE FUNCTIONAL TEST [Group 4] ..... 6 3 Appendix R: DC-10-30 W/AFT TANK 3200 GALLONS - FUSE FUNCTIONAL TEST [Group 5] ..... 7 1 Appendix S: DC-10-30F (KC-10A) - FUSE FUNCTIONAL TEST [Group 6] ................ 8 0 Appendix T: DC-10-30F (KDC-10) - FUSE FUNCTIONAL TEST [Group 7] ................ 8 2
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McDonnell DouglasCommercial Airplanes DC10 Service Bulletin Revision Transmittal SheetNumber: DC10-28-252Original Issue: November 25, 2008 Revision 1: January 06, 2010 ATA System: 2800 SUBJECT: FUEL - Fuel Systems - Install Fuel Tank Float Level Switch and Aft Auxiliary Tank Fuel Pump Pressure Switch In-line Fuses This revision includes all pages of the service bulletin.
COMPLIANCE INFORMATION RELATED TO THIS REVISION More work is necessary on airplane changed in accordance with the original issue of this service bulletin.
The more work involved is to change wire identifications Q 835 G22 and Q 835 H22 to Q 835 M22 and Q 835 N22 respectively in accordance with Drawing SR10280063 "D" change.
REASON FOR REVISION This revision is sent to change wire identifications Q 835 G22 and Q 835 H22 to Q 835 M22 and Q 835 N22 respectively in accordance with Drawing SR10280063 "D" change.
These sections were changed:
1. In Paragraph 1.A.1., Airplanes, moved airplanes from Group 3 to Groups 1 and 2.
2. In Paragraph 1.D., Description, added Maintenance Zones.
3. In Paragraph 1.F., Approval, change statement.
4. In Paragraph 1.J.2.a., Drawings, changed drawing change D.
5. In Paragraph 1.K., Publications Affected, added Tolerance Based Structural Inspections data.
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 November 25, 2008Original Issue:
January 06, 2010Revision 1:
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McDonnell DouglasCommercial Airplanes DC10 Service Bulletin SummaryNumber: DC10-28-252Original Issue: November 25, 2008 Revision 1: January 06, 2010 ATA System: 2800 SUBJECT: FUEL - Fuel Systems - Install Fuel Tank Float Level Switch and Aft Auxiliary Tank Fuel Pump Pressure Switch In-line Fuses
CONCURRENT REQUIREMENTS None.
BACKGROUND An investigation by Boeing has determined that float level switch wires located on the left and right wing forward spar, right main landing gear wheel well, forward and aft cargo compartments and fuel pump pressure switch wires located in the aft cargo compartment are routed in the same bundles as power wires. If a short circuit between a float level or fuel pump pressure switch wire and a power wire occurs, an over current can cause excessive temperatures in the float level or fuel pump pressure switch wires, resulting in damage. Adding an in-line fuse as a self-contained component in each float level and pressure switch circuit and sleeving the wires between the fuel tank and the in-line fuse will minimize the possibility of excessive temperatures in the float level or pressure switch wires. If not corrected, and there is a short circuit of the float level or pressure switch wire to a power wire, possible damage to the float level or fuel pump pressure switch wire could occur, and become a potential ignition source for the fuel tank.
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.
ACTION Group 1-3, 6-7:
This service bulletin installs fuel tank float level switch in-line fuses.
Group 4-5:
This service bulletin installs fuel tank float level switch and aft auxiliary tank fuel pump pressure switch in-line fuses.
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.
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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 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 configuration changes given in this service bulletin.
MANPOWER Refer to Paragraph 1.G., for Manpower information.
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 Number: DC10-28-252 Original Issue: November 25, 2008 Revision 1: January 06, 2010 ATA System: 2800 SUBJECT: FUEL - Fuel Systems - Install Fuel Tank Float Level Switch and Aft Auxiliary Tank Fuel Pump Pressure Switch In-line Fuses
1. PLANNING INFORMATION A. Effectivity
1. Airplanes NOTE: Any Group 3 DC-10-10, DC-10-10F, and DC-10-15 Airplane modified to MD-10-10F by Boeing Engineering, become Group 1 Airplanes.
Any Group 3 DC-10-30 and DC-10-30F Airplanes modified to MD-10-30F by Boeing Engineering, become Group 2 Airplanes.
Airplane fuselage number 404 had this modification incorporated at the operator's facility in accordance with Drawing SR10280063-7011.
DESCRIPTIONCONFIGURATIONGROUP Applicable to DC-10-10, DC-10-10F and MD-10-10F airplanes.-1 Applicable to DC-10-30F and MD-10-30F airplanes.-2 Applicable to DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F, DC-10-40 and DC-10-40F airplanes.
-3 Applicable to DC-10-30 airplanes with 1500 gallon aft auxiliary fuel tank.
-4 Applicable to DC-10-30 airplanes with 3200 gallon aft auxiliary fuel tank.
-5 Applicable to DC-10-30F (KC-10A) airplanes.-6 Applicable to DC-10-30F (KDC-10) airplanes.-7 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
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GroupFuselage Number 3100 2103 3106 2110 1112 3114 - 115 3117 1119 3122 - 123 3127 3129 3131 - 135 3137 1138 - 140 1142 1144 - 145 3146 - 147 1148 115 3150 3152 1153 - 155 3156 - 158 3160 3162 3165 - 166 1169 117 3170 - 171 1173 3174 1177
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GroupFuselage Number 3178 - 179 3183 - 184 3187 - 190 3192 1194 3195 - 196 1198 3199 32 3201 1203 3204 1205 3206 1207 - 210 3211 - 216 2219 3220 - 221 3223 - 227 3229 - 232 3234 7235 3236 3239 - 242 3244 - 246 1247 3248 1249 125 1250 3251 - 256 2257
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GroupFuselage Number 126 3261 - 263 7264 3265 - 268 1269 127 1270 - 273 3274 - 275 2277 3281 2282 3285 - 286 3289 - 291 4292 1294 3296 1297 - 298 3299 - 306 1307 3308 1309 3310 6311 3312 - 316 2317 3318 1319 132 1321 1323 3324 - 325 2326
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