# Boeing Alert Service Bulletin 767-28A0083: Commercial Airplane Group - Service Bulletin - Rights: © The Boeing Company. Filed by the FAA in regulations.gov docket FAA-2007-29173; AD 2009-16-06 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. - Document: [Boeing Alert Service Bulletin 767-28A0083](https://openairdocs.org/service-documents/boeing/767-28a0083.md) - Title as filed: Commercial Airplane Group - Service Bulletin - Pages: 339 - PDF: https://openairdocs.org/files/sha256/1a/28/1a282b05feefd6fdc3e76f4a3b8285ab9e6bc16e31654be244d84ba3770492f4 - Page: https://openairdocs.org/service-documents/boeing/767-28a0083/file/1a282b05feef ## Text Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 1 of 339 Commercial Airplane Group 767 Service Bulletin Number: 767-28A0083 Date: May 03, 2006 Revision 2: February 12, 2009 ATA System: 2822 2842 SUBJECT: FUEL SYSTEM - Engine Fuel Feed System - Fuel Pump Inlet Protection - Auxiliary Fuel Tank Pump Automatic Shut Off Installation BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET Copyright © 2006 The Boeing Company Unpublished Work - All Rights Reserved Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable subject matter.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, 707, 717, 727, 737, 747, 757, 767, 777, BBJ, BOEING BUSINESS JET, DC-8, DC-9, DC-10, MD-10, MD-11, MD-80, MD-90, the Boeing logo and the Boeing livery are among the trademarks owned by Boeing or its subsidiaries. No intellectual property license (express or implied) is granted in connection with this document or otherwise. ### Page 2 BLANK PAGE May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 2 of 339 BOEING SERVICE BULLETIN 767-28A0083 BLANK PAGE ### Page 3 Table of Contents May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 3 of 339 BOEING SERVICE BULLETIN 767-28A0083 Table of Contents Revision Transmittal Sheet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 1. PLANNING INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15 A. Effectivity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15 1. Airplanes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15 2. Spares Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37 B. Concurrent Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37 C. Reason . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37 D. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40 E. Compliance. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40 F. Approval . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40 G. Manpower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 41 H. Weight and Balance Changes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44 I. Electrical Load Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44 J. References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44 1. Existing Data: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44 2. Data supplied with this Service Bulletin: . . . . . . . . . . . . . . . . . . . . . . . . . 44 3. Installation Drawings Used in the Preparation of this Service Bulletin: . . . . . . . . . . 45 K. Publications Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 45 L. Interchangeability and Intermixability of Parts . . . . . . . . . . . . . . . . . . . . . . . . . 45 2. MATERIAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47 A. Material - Price and Availability. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47 B. Industry Support Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47 C. Parts Necessary For Each Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47 1. Kits/Parts: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47 2. Parts and Materials Supplied by the Operator: . . . . . . . . . . . . . . . . . . . . . . 52 3. Parts Modified and Reidentified: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 52 4. Parts Removed and Not Replaced: . . . . . . . . . . . . . . . . . . . . . . . . . . . . 52 D. Parts Necessary to Change Spares . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 52 E. Special Tooling - Price and Availability. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 52 F. Special Tooling Necessary to do this Service Bulletin . . . . . . . . . . . . . . . . . . . . . 52 3. ACCOMPLISHMENT INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 53 A. GENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 53 B. WORK INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 53 FIGURE 1: P36 Panel - Bracket Installation, Groups 1-39 and 82-87 Airplanes . . . . . . . . . . . . 62 FIGURE 2: P37 Panel - Bracket Installation, Groups 1-39 and 82-87 Airplanes . . . . . . . . . . . . 66 FIGURE 3: P33 Panel - Wiring changes W/B146, Group 1-39 and 82-87 Airplanes . . . . . . . . . . 69 FIGURE 4: P36 Panel - Wiring changes W/B0176, Groups 1-2, 5, 82, 85 Airplanes. . . . . . . . . . . 70 FIGURE 5: P36 Panel - Wiring changes W/B0176, Groups 3-4, 83-84 Airplanes. . . . . . . . . . . . 72 FIGURE 6: P36 Panel - Wiring Changes W/B0176, Group 6 Airplanes.. . . . . . . . . . . . . . . . . 74 FIGURE 7: P36 Panel - Wiring Changes W/B0176, Group 7, 86 Airplanes.. . . . . . . . . . . . . . . 76 FIGURE 8: P36 Panel - Wiring Changes W/B0176, Group 8, 87 Airplanes . . . . . . . . . . . . . . . 78 FIGURE 9: P36 Panel - Wiring Changes W/B0176, Groups 9, 11-16,18, 21-22, 25-34 airplanes. . . . 80 FIGURE 10: P36 Panel - Wiring Changes W/B0176, Groups 10, 20 Airplanes.. . . . . . . . . . . . . 82 FIGURE 11: P36 Panel - Wiring Changes W/B0176, Group 17 Airplanes. . . . . . . . . . . . . . . . 84 ### Page 4 Table of Contents May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 4 of 339 BOEING SERVICE BULLETIN 767-28A0083 FIGURE 12: P36 Panel - Wiring Changes W/B0176, Group 19 airplanes. . . . . . . . . . . . . . . . . 86 FIGURE 13: P36 Panel - Wiring Changes W/B0176, Groups 23-24 Airplanes. . . . . . . . . . . . . . 88 FIGURE 14: P36 Panel - Wiring Changes W/B0176, Group 35 Airplanes.. . . . . . . . . . . . . . . . 90 FIGURE 15: P36 Panel - Wiring Changes W/B0176, Group 36 Airplanes.. . . . . . . . . . . . . . . . 92 FIGURE 16: P36 Panel - Wiring Changes W/B0176, Group 37 Airplanes.. . . . . . . . . . . . . . . . 94 FIGURE 17: P36 Panel - Wiring Changes W/B0176, Group 38 Airplanes.. . . . . . . . . . . . . . . . 96 FIGURE 18: P36 Panel - Wiring Changes W/B0176, Group 39 Airplanes.. . . . . . . . . . . . . . . . 98 FIGURE 19: P36 Panel - Wiring Changes W/B0184, Groups 1-2, 5, 8, 82, 85, 87 Airplanes. . . . . . 100 FIGURE 20: P36 Panel - Wiring Changes W/B0184, Groups 3-4, 83-84 Airplanes. . . . . . . . . . . 102 FIGURE 21: P36 Panel - Wiring Changes W/B0184, Group 6 Airplanes. . . . . . . . . . . . . . . . 104 FIGURE 22: P36 Panel - Wiring Changes W/B0184, Group 7, 86 Airplanes. . . . . . . . . . . . . . 106 FIGURE 23: P36 Panel - Wiring Changes W/B0184, Groups 9, 11-15, 18-19, 21-24, 26-31, 33-34 airplanes 108 FIGURE 24: P36 Panel - Wiring Changes W/B0184, Groups 10, 20 Airplanes. . . . . . . . . . . . . 110 FIGURE 25: P36 Panel - Wiring Changes W/B0184, Group 16 Airplanes.. . . . . . . . . . . . . . . 112 FIGURE 26: P36 Panel - Wiring Changes W/B0184, Group 17 Airplanes.. . . . . . . . . . . . . . . 114 FIGURE 27: P36 Panel - Wiring Changes W/B0184, Groups 25, 32 Airplanes. . . . . . . . . . . . . 116 FIGURE 28: P36 Panel - Wiring Changes W/B0184, Group 35 Airplanes.. . . . . . . . . . . . . . . 118 FIGURE 29: P36 Panel - Wiring Changes W/B0184, Group36 Airplanes. . . . . . . . . . . . . . . . 120 FIGURE 30: P36 Panel - Wiring Changes W/B0184, Group 37 Airplanes.. . . . . . . . . . . . . . . 122 FIGURE 31: P36 Panel - Wiring Changes W/B0184, Group 38 Airplanes.. . . . . . . . . . . . . . . 124 FIGURE 32: P36 Panel - Wiring Changes W/B0184, Group 39 Airplanes.. . . . . . . . . . . . . . . 126 FIGURE 33: P36 Panel - Relay Installation, Groups 1-39, 82-87 Airplanes . . . . . . . . . . . . . . 128 FIGURE 34: P37 Panel - Wiring Changes W/B0188, Group 1 Airplanes. . . . . . . . . . . . . . . . 130 FIGURE 35: P37 Panel - Wiring Changes W/B0188, Groups 2-5, 7-9, 16, 82-87 Airplanes. . . . . . 132 FIGURE 36: P37 Panel - Wiring Changes W/B0188, Group 6 Airplanes. . . . . . . . . . . . . . . . 134 FIGURE 37: P37 Panel - Wiring Changes W/B0188, Groups 10-12, 14-15, 17-21, 23, 25-26, 28, 32-34, 36- 37 Airplanes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 136 FIGURE 38: P37 Panel - Wiring Changes W/B0188, Groups 13, 22, 24, 27, 29-31, 38-39 Airplanes. 138 FIGURE 39: P37 Panel - Wiring Changes W/B0188, Group 35 Airplanes.. . . . . . . . . . . . . . . 139 FIGURE 40: P37 Panel - Wiring Changes W/B0192, Group 1 Airplanes. . . . . . . . . . . . . . . . 140 FIGURE 41: P37 Panel - Wiring Changes W/B0192, Groups 2-3, 82-83 Airplanes. . . . . . . . . . . 142 FIGURE 42: P37 Panel - Wiring Changes W/B0192, Group 4, 84 Airplanes. . . . . . . . . . . . . . 144 FIGURE 43: P37 Panel - Wiring Changes W/B0192, Groups 5, 8-9, 16, 85, 87 Airplanes . . . . . . 146 FIGURE 44: P37 Panel - Wiring Changes W/B0192, Group 6 Airplanes. . . . . . . . . . . . . . . . 148 FIGURE 45: P37 Panel - Wiring Changes W/B0192, Group 7, 86 Airplanes. . . . . . . . . . . . . . 150 FIGURE 46: P37 Panel - Wiring Changes W/B0192, Group 10 Airplanes.. . . . . . . . . . . . . . . 152 FIGURE 47: P37 Panel - Wiring Changes W/B0192, Groups 11-12, 14-15, 17, 19, 21, 23, 25-26, 28, 36 Airplanes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 154 FIGURE 48: P37 Panel - Wiring Changes W/B0192, Groups 13, 22, 24, 27, 29-31 Airplanes. . . . . 156 FIGURE 49: P37 Panel - Wiring Changes W/B0192, Groups 18, 20, 32-34 Airplanes. . . . . . . . . 158 FIGURE 50: P37 Panel - Wiring Changes W/B0192, Group 35 Airplanes.. . . . . . . . . . . . . . . 160 FIGURE 51: P37 Panel - Wiring Changes W/B0192, Group 37 Airplanes.. . . . . . . . . . . . . . . 162 FIGURE 52: P37 Panel - Wiring Changes W/B0192, Group 38 Airplanes.. . . . . . . . . . . . . . . 164 FIGURE 53: P37 Panel - Wiring Changes W/B0192, Group 39 Airplanes.. . . . . . . . . . . . . . . 166 FIGURE 54: P37 Panel - Wiring Changes W/B0198, Groups 1, 5-6, 8-9, 14, 16-17, 19, 25, 28, 36, 85, 87 ### Page 5 Table of Contents May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 5 of 339 BOEING SERVICE BULLETIN 767-28A0083 Airplanes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 168 FIGURE 55: P37 Panel - Wiring Changes W/B0198, Groups 2-3, 10 82-83 Airplanes. . . . . . . . . . 169 FIGURE 56: P37 Panel - Wiring Changes W/B0198, Group 4, 84 Airplanes. . . . . . . . . . . . . . . 170 FIGURE 57: P37 Panel - Wiring Changes W/B0198, Group 7, 86 Airplanes. . . . . . . . . . . . . . . 171 FIGURE 58: P37 Panel - Wiring Changes W/B0198, Groups 11, 21 Airplanes.. . . . . . . . . . . . . 172 FIGURE 59: P37 Panel - Wiring Changes W/B0198, Groups 12, 15, 23, 26 Airplanes.. . . . . . . . . 173 FIGURE 60: P37 Panel - Wiring Changes W/B0198, Groups 13, 24, 27 Airplanes.. . . . . . . . . . . 174 FIGURE 61: P37 Panel - Wiring Changes W/B0198, Groups 18, 20, 32-34 Airplanes. . . . . . . . . . 175 FIGURE 62: P37 Panel - Wiring Changes W/B0198, Group 22 Airplanes. . . . . . . . . . . . . . . . 176 FIGURE 63: P37 Panel - Wiring Changes W/B0198, Group 29-30 Airplanes. . . . . . . . . . . . . . 177 FIGURE 64: P37 Panel - Wiring Changes W/B0198, Group 31 Airplanes. . . . . . . . . . . . . . . . 178 FIGURE 65: P37 Panel - Wiring Changes W/B0198, Group 35 Airplanes. . . . . . . . . . . . . . . . 179 FIGURE 66: P37 Panel - Wiring Changes W/B0198, Group 37 Airplanes. . . . . . . . . . . . . . . . 180 FIGURE 67: P37 Panel - Relay Installation, Groups 1-39, 82-87 Airplanes. . . . . . . . . . . . . . . 181 FIGURE 68: P37 Panel - Wiring Changes W/B0198, Group 38 Airplanes. . . . . . . . . . . . . . . . 183 FIGURE 69: P33 to P36 Panel - Wiring Changes W/B0264, Groups 1-6, 8-15, 17-24, 26-31, 33-35, 37-39, 82-85, 87 Airplanes.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 184 FIGURE 70: P33 to P36 Panel - Wiring Changes W/B0264, Groups 7, 16, 86 Airplanes. . . . . . . . 185 FIGURE 71: P33 to P36 Panel - Wiring Changes W/B0264, Groups 25, 32 Airplanes. . . . . . . . . . 186 FIGURE 72: P33 to P36 Panel - Wiring Changes W/B0264, Group 36 Airplanes. . . . . . . . . . . . 187 FIGURE 73: P36 to P37 Panel - Wiring Changes W/B0590, Groups 1-6, 8-10, 14, 16-20, 25, 28-30, 32-34, 36, 82-85, 87 Airplanes.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 188 FIGURE 74: P36 to P37 Panel - Wiring Changes W/B0590, Group 31 Airplanes. . . . . . . . . . . . 189 FIGURE 75: P36 to P37 Panel - Wiring Changes W/B0590, Group 35 Airplanes. . . . . . . . . . . . 190 FIGURE 76: P36 to P37 Panel - Wiring Changes W/B0590, Groups 7, 11, 21-22, 86 Airplanes. . . . . 191 FIGURE 77: P36 to P37 Panel - Wiring Changes W/B0590, Groups 12-13, 15, 23-24, 26-27, 38 Airplanes. 192 FIGURE 78: P36 to P37 Panel - Wiring Changes W/B0942, Groups 37, 39 Airplanes. . . . . . . . . . 193 FIGURE 79: P37 Panel - Wiring Changes W/B1118, Group 39 Airplanes. . . . . . . . . . . . . . . . 194 FIGURE 80: P37 Panel - Wiring Changes W/B1118, Group 37 Airplanes. . . . . . . . . . . . . . . . 195 FIGURE 81: Wire Bundle Routing, P36 to P37 Panel, Groups 1-39, 82-87 Airplanes. . . . . . . . . . 196 FIGURE 82: P36 Panel - Bracket Installation, Group 40-79, 88 Airplanes. . . . . . . . . . . . . . . . 199 FIGURE 83: P37 Panel - Bracket Installation, Groups 40-79, 88 Airplanes.. . . . . . . . . . . . . . . 203 FIGURE 84: P36 Panel - Wiring Changes W/B0176, Group 40 Airplanes. . . . . . . . . . . . . . . . 206 FIGURE 85: P36 Panel - Wiring Changes W/B0176, Groups 42, 67-68 Airplanes. . . . . . . . . . . . 208 FIGURE 86: P36 Panel - Wiring Change W/B0176, Group 76 Airplanes. . . . . . . . . . . . . . . . . 210 FIGURE 87: P36 Panel - Wiring Changes W/B0176, Group 55 Airplanes. . . . . . . . . . . . . . . . 212 FIGURE 88: P36 Panel - Wiring Changes W/B0176, Group 49 Airplanes. . . . . . . . . . . . . . . . 214 FIGURE 89: P36 Panel - Wiring Changes W/B0176, Groups 54, 79 Airplanes.. . . . . . . . . . . . . 216 FIGURE 90: P36 Panel - Wiring Changes W/B0176, Group 66 Airplanes. . . . . . . . . . . . . . . . 218 FIGURE 91: P36 Panel - Wiring Changes W/B0176, Groups 44, 72, 74 Airplanes.. . . . . . . . . . . 220 FIGURE 92: P36 Panel - Wiring Changes W/B0176, Group 62 Airplanes. . . . . . . . . . . . . . . . 222 FIGURE 93: P36 Panel - Wiring Changes W/B0176, Groups 41, 43, 64 Airplanes.. . . . . . . . . . . 224 FIGURE 94: P36 Panel - Wiring Changes W/B0176, Group 69 Airplanes. . . . . . . . . . . . . . . . 226 FIGURE 95: P36 Panel - Wiring Changes W/B0176, Group 61 Airplanes. . . . . . . . . . . . . . . . 228 FIGURE 96: P36 Panel - Wiring Changes W/B0176, Group 70 Airplanes. . . . . . . . . . . . . . . . 230 ### Page 6 Table of Contents May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 6 of 339 BOEING SERVICE BULLETIN 767-28A0083 FIGURE 97: P36 Panel - Wiring Changes W/B0176, Groups 73, 75 Airplanes. . . . . . . . . . . . . 232 FIGURE 98: P36 Panel - Wiring Changes W/B0176, Group 56 Airplanes.. . . . . . . . . . . . . . . 234 FIGURE 99: P36 Panel - Wiring Changes W/B0176, Group 71 Airplanes.. . . . . . . . . . . . . . . 236 FIGURE 100: P36 Panel - Wiring Changes W/B0176, Group 65 Airplanes. . . . . . . . . . . . . . . 238 FIGURE 101: P36 Panel - Wiring Changes W/B0176, Group 63 Airplanes. . . . . . . . . . . . . . . 240 FIGURE 102: P36 Panel - Wiring Changes W/B0176, Groups 52-53, 78 Airplanes.. . . . . . . . . . 242 FIGURE 103: P36 Panel - Wiring Changes W/B0176, Groups 46-48, 50-51, 58, 60, 77 Airplanes. . . 244 FIGURE 104: P36 Panel - Wiring Changes W/B0176, Groups 45, 57, 59 Airplanes. . . . . . . . . . 246 FIGURE 105: P36 Panel - Wiring Changes W/B0184, Group 61 Airplanes. . . . . . . . . . . . . . . 248 FIGURE 106: P36 Panel - Wiring Changes W/B0184, Groups 62-63 Airplanes.. . . . . . . . . . . . 250 FIGURE 107: P36 Panel - Wiring Changes W/B0184, Group 56 Airplanes. . . . . . . . . . . . . . . 252 FIGURE 108: P36 Panel - Wiring Changes W/B0184, Groups 44, 72-75 Airplanes.. . . . . . . . . . 254 FIGURE 109: P36 Panel - Wiring Changes W/B0184, Groups 65, 69 Airplanes. . . . . . . . . . . . 256 FIGURE 110: P36 Panel - Wiring Changes W/B0184, Groups 52-53, 78 Airplanes.. . . . . . . . . . 258 FIGURE 111: P36 Panel - Wiring Changes W/B0184, Groups 40-41, 43, 45-48, 50-51, 57-60, 64, 66, 70- 71, 77 Airplanes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 260 FIGURE 112: P36 Panel - Wiring Changes W/B0184, Groups 54-55, 79 Airplanes.. . . . . . . . . . 262 FIGURE 113: P36 Panel - Wiring Changes W/B0184, Groups 42, 49, 67-68, 76, 88 Airplanes.. . . . 264 FIGURE 114: P36 Panel - Relay Installation, Groups 40-79, 88 Airplanes. . . . . . . . . . . . . . . 266 FIGURE 115: P37 Panel - Wiring Changes W/B0188, Group 55 Airplanes. . . . . . . . . . . . . . . 268 FIGURE 116: P37 Panel - Wiring Changes W/B0188, Groups 40-45, 57, 59, 64, 66, 68-70, 72, 74, 76 Airplanes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 270 FIGURE 117: P37 Panel - Wiring Changes W/B0188, Groups 46-53, 58, 60, 65, 67, 71, 73, 75, 77-79, 88 Airplanes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 272 FIGURE 118: P37 Panel - Wiring Changes W/B0188, Groups 54, 56 Airplanes. . . . . . . . . . . . 274 FIGURE 119: P37 Panel - Wiring Changes W/B0188, Groups 61-62 Airplanes.. . . . . . . . . . . . 276 FIGURE 120: P37 Panel - Wiring Changes W/B0188, Group 63 Airplanes. . . . . . . . . . . . . . . 277 FIGURE 121: P37 Panel - Wiring Changes W/B0192, Group 61 Airplanes. . . . . . . . . . . . . . . 279 FIGURE 122: P37 Panel - Wiring Changes W/B0192, Group 62 Airplanes. . . . . . . . . . . . . . . 281 FIGURE 123: P37 Panel - Wiring Changes W/B0192, Groups 41, 43-45, 57, 59, 64, 69-70, 72, 74, Airplanes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 283 FIGURE 124: P37 Panel - Wiring Changes W/B0192, Groups 42, 67-68, 76 Airplanes.. . . . . . . . 285 FIGURE 125: P37 Panel - Wiring Changes W/B0192, Groups 40, 66 Airplanes. . . . . . . . . . . . 287 FIGURE 126: P37 Panel - Wiring Changes W/B0192, Group 55 Airplanes. . . . . . . . . . . . . . . 289 FIGURE 127: P37 Panel - Wiring Changes W/B0192, Group 56 Airplanes. . . . . . . . . . . . . . . 291 FIGURE 128: P37 Panel - Wiring Changes W/B0192, Group 54 Airplanes. . . . . . . . . . . . . . . 293 FIGURE 129: P37 Panel - Wiring Changes W/B0192, Groups 49, 79, 88 Airplanes. . . . . . . . . . 295 FIGURE 130: P37 Panel - Wiring Changes W/B0192, Groups 48, 50-53, 78 Airplanes.. . . . . . . . 297 FIGURE 131: P37 Panel - Wiring Changes W/B0192, Groups 46-47, 58, 60, 65, 71, 73, 75, 77 Airplanes. 299 FIGURE 132: P37 Panel - Wiring Changes W/B0192, Group 63 Airplanes. . . . . . . . . . . . . . . 301 FIGURE 133: P37 Panel - Wiring Changes W/B0198, Group 61 Airplanes. . . . . . . . . . . . . . . 303 FIGURE 134: P37 Panel - Wiring Changes W/B0198, Group 62 Airplanes. . . . . . . . . . . . . . . 304 FIGURE 135: P37 Panel - Wiring Changes W/B0198, Group 63 Airplanes. . . . . . . . . . . . . . . 305 FIGURE 136: P37 Panel - Wiring Changes W/B0198, Groups 40-41, 43-45, 57, 64, 69, 70, 72 Airplanes. 306 ### Page 7 Table of Contents May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 7 of 339 BOEING SERVICE BULLETIN 767-28A0083 FIGURE 137: P37 Panel - Wiring Changes W/B0198, Groups 59, 66, 74 Airplanes. . . . . . . . . . . 307 FIGURE 138: P37 Panel - Wiring Changes W/B0198, Groups 46, 58, 65, 71, 73 Airplanes. . . . . . . 308 FIGURE 139: P37 Panel - Wiring Changes W/B0198, Groups 47, 60, 75, 77 Airplanes. . . . . . . . . 309 FIGURE 140: P37 Panel - Wiring Changes W/B0198, Group 51 Airplanes.. . . . . . . . . . . . . . . 310 FIGURE 141: P37 Panel - Wiring Changes W/B0198, Groups 48, 50, 53, 78 Airplanes. . . . . . . . . 311 FIGURE 142: P37 Panel - Wiring changes W/B0198, Groups 52, 56 Airplanes. . . . . . . . . . . . . 312 FIGURE 143: P37 Panel - Relay Installation, Groups 40-79, 88 Airplanes. . . . . . . . . . . . . . . . 313 FIGURE 144: P36 to P37 Panel - Wiring Changes W/B0590, Groups 47-48, 50, 53, 59-60, 66, 74-75, 77- 78 Airplanes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 315 FIGURE 145: P36 to P37 Panel - Wiring Changes W/B0590, Groups 61-63 Airplanes. . . . . . . . . 316 FIGURE 146: P36 to P37 Panel - Wiring Changes W/B0590, Groups 40-41, 43-46, 51, 57-58, 64-65, 69- 73 Airplanes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 317 FIGURE 147: P36 to P37 Panel - Wiring Changes W/B0590, Groups 52, 56 Airplanes. . . . . . . . . 318 FIGURE 148: P36 to P37 Panel - Wiring Changes W/B0942, Groups 42, 49, 54, 67-68, 76, 79 Airplanes. 319 FIGURE 149: P36 to P37 Panel - Wiring Changes W/B0942, Group 55 Airplane. . . . . . . . . . . . 320 FIGURE 150: P37 Panel - Wiring Changes W/B1118, Groups 49, 54, 79, 88 Airplanes. . . . . . . . . 321 FIGURE 151: P37 Panel - Wiring Changes W/B1118, Groups 42, 67-68, 76 Airplanes. . . . . . . . . 322 FIGURE 152: Wiring Bundle Routing, P36 to P37 Panel, Groups 40-79 and 88 Airplanes. . . . . . . . 323 FIGURE 153: P36 Panel - Wiring Changes W/B0175, Group 80-81 and 89 Airplanes. . . . . . . . . . 326 FIGURE 154: P36 Panel - Relay Installation, Group 80-81 and 89 Airplanes. . . . . . . . . . . . . . 327 FIGURE 155: P37 Panel - Wiring Changes W/B0192 and W/B1118, Group 80 Airplanes. . . . . . . . 329 FIGURE 156: P37 Panel - Wiring Changes W/B0192 and W/B0188, Group 81 Airplanes. . . . . . . . 330 FIGURE 157: P37 Panel - Relay Installation, Group 80-81 and 89 Airplanes. . . . . . . . . . . . . . 331 FIGURE 158: P37 Panel - Wiring Changes W/B0188, Groups 82-87 airplanes. . . . . . . . . . . . . 334 FIGURE 159: P37 Panel - Wiring Changes W/B0176 Group 88. . . . . . . . . . . . . . . . . . . . . 336 FIGURE 160: P36 to P37 Panel - Wiring Changes W/B0942, Groups 88 . . . . . . . . . . . . . . . . 338 FIGURE 161: P37 Panel - Wiring Changes W/B0192 and W/B198, Group 89 . . . . . . . . . . . . . 339 ### Page 8 Table of Contents May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 8 of 339 BOEING SERVICE BULLETIN 767-28A0083 BLANK PAGE ### Page 9 Original Issue: May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 9 of 339 Commercial Airplanes 767 Service Bulletin Number: 767-28A0083 Revision Transmittal Sheet Original Issue: May 03, 2006 Revision 2: February 12, 2009 ATA System: 2822 2842 SUBJECT: FUEL SYSTEM - Engine Fuel Feed System - Fuel Pump Inlet Protection - Auxiliary Fuel Tank Pump Automatic Shut Off Installation This Revision includes all pages of the service bulletin. COMPLIANCE INFORMATION RELATED TO THIS REVISION Federal Aviation Administration (FAA) Notice of Proposed Rule Making 2006-NM-283-AD, is related to this service bulletin. No more work is necessary on airplanes changed as shown in Revision 1 or initial release of this service bulletin. No airplanes were added to the service bulletin effectivity. REASON FOR REVISION This revision is sent to address the comments received from operators since the release of Revision 1 of the service bulletin. The effectivity group assignments were changed to show the correct wiring configuration for the affected airplanes. The following sections of the service bulletin are changed: — The Summary illustration, revised to show the wire bundle routing more accurately and show an alternate wire routing configuration. — Summary - BackGround, Planning Information - Reason and Compliance Section, revised AD reference to remove AD 94-11-05. The AD 94-11-05 is superseded by AD 2001-15-08. — Group and Configuration tables in Section 1.A, Description Section 1.D, Man-power tables Section 1.G, Weight and Balance Section H, Accomplishment Instructions Section 3, added new Groups 88 and 89 airplanes. Airplanes Affected Old Airplane Groups Airplane Groups VL891-VL900 49 88 (new) VR087 80 89 (new) VR106 80 89 (new) VR901 81 80 (existing) VT521-VT522 80 81 (existing) ### Page 10 Original Issue: May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 10 of 339 BOEING SERVICE BULLETIN 767-28A0083 — In Paragraph 2.K, Publications Affected, 767 Flight Crew Operating Manual, impacts 0.6 Preface, NP.21 and chapter 12. — In Paragraph 3.B, Work Instructions, Part 1, new step 37, added for Groups 82-87, Figure 158. — In Paragraph 3.B, Work Instructions, Part 1, step 68, the text has been corrected to read Figure 68. — In Paragraph 3.B, Work Instructions, Part 1, step 69, the text has been corrected to read Figure 67. — In Paragraph 3.B, Work Instructions, Part 2, new step 9 added for new Figure 159, Group 88. — In Paragraph 3.B, Work Instructions, Part 2, step 31, added Group 78. — In Paragraph 3.B, Work Instructions, Part 2, new step 71 added for new Figure 160, Group 88. — In Paragraph 3.B, Work Instructions, Part 2, steps 1-3, 34-35, 38, 50, 64, 71-71 and 74-77 added Group 88. — In Paragraph 3.B, Work Instructions, Part 3, steps 1-4 and 7-12, added Group 89. — Figures 1 and 82, revised to show a alternate configuration for the relay mounting holes. — Figures 53, revised wire bundle reference on terminal YC12 from W198 to W1118. — Figures 4-32, 34-66, 68, 79-80, 84-113, 115-142, 150-151 and 158, revised Flag Note Table to add Burndy terminal block information. — Figures 78, 148 and 149, revised to remove the shield reference for wire 942-011-24. — Figures 81 and 152, revised to show the wire bundle routing more accurately and show an alternate wire routing configuration. Wire bundle routing from P36 to P33 was added to Figure 81. — Figures 82-83, 113-114, 117, 129, 143, 150, 152 added Group 88. — Figure 124, revised to correct a typographical error on the Burndy block call out and show wire W198-188- 24 as a deleted wire. — Figure 153 added Group 89. — Figure 154, added Group 89, added relay mounting hardware information and revised Circle Note 3. — Figure 155, revised to show the correct connector number. Airplanes VR087 and VR106 were moved to new Figure 161and revised to be Group 89 airplanes. — Figure 156, revised to show the correct connector number. — Figure 157, added Group 89 and added relay mounting hardware information. — Figures 159 and 160, created new figures for new Group 88 airplanes. Group 88 airplanes required the use of pin 40 in connector D5658J and D5658P. — Figures 161, created new figure for new Group 89 airplanes. Group 89 airplanes required the use of wire W198-02A-24 and pin 8 in connector D5052J and D5052P. The data given in Information Notice 767-28A0083 IN 02 is included in this revision. Paragraph 1.A., Effectivity, shows changes of airplane operators. Each operator should examine the Effectivity paragraph for changes. 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 Original Issue: May 03, 2006 Revision 1: April 26, 2007 Revision 2: February 12, 2009 ### Page 11 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 11 of 339 Commercial Airplane Group 767 Service Bulletin Number: 767-28A0083 Summary Date: May 03, 2006 Revision 2: February 12, 2009 ATA System: 2822 2842 SUBJECT: FUEL SYSTEM - Engine Fuel Feed System - Fuel Pump Inlet Protection - Auxiliary Fuel Tank Pump Automatic Shut Off Installation CONCURRENT REQUIREMENTS None. BACKGROUND This service bulletin is the result of the safety assessments conducted by Boeing under SFAR 88, "Fuel Tank System Fault Tolerance Evaluation Requirements". Initial results from the Fuel System Safety Analysis show that fuel pumps that run dry could cause an overheat condition external of the pump explosion resistance area that is open to the pump inlet. An overheat condition in this area could possibly cause an unwanted ignition source for the fuel vapors in the fuel tank. Ignition of flammable fuel vapors could cause a fire or explosion which could put the airplane in an unsafe condition. Installation of the automatic shut off system adds fuel pump inlet protection against sparks caused by friction overheat damage in the fuel tanks. This service bulletin gives the instructions and a kit of parts to install an automatic shut off system for the center wing tank override boost pumps. Installation of the automatic system will prevent a potential ignition source in the tank by making sure the pumps do not run for an extended period of time when the fuel level is below pump inlet or the pump has failed. Currently the flight crew turns off the pumps when a pump low pressure message is displayed on EICAS. The automatic shut off system installed by this service bulletin will make sure that the pumps will not run for more than 15 seconds with continuous low fuel pressure if the flight crew does not respond to the EICAS message sooner. The flight crew remains in primary control, with this automatic shut off system as a backup, to turn the pumps off after continuous low pressure indication. This change affects Section 9 of the Maintenance Planning Data (MPD) Document. New Airworthiness Limitations (AWL) "28-AWL-20" will be added to Section 9 of the MPD to include a functional check of the center tank fuel boost pump automatic shut off system. This change also affects Section 1 and 3.1 of the FAA Approved Airplane Flight Manual. Federal Aviation Administration (FAA) Airworthiness Directive 2001-15-08 is related to this service bulletin. ### Page 12 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 12 of 339 BOEING SERVICE BULLETIN 767-28A0083 As a part of a service bulletin validation program, this change was completed on airplane VN791 by initial release of Service Bulletin 767-28A0083 and before the release of Revision 1 of this service bulletin. The change was completed on airplane VN791 by Service Bulletin 767-28A0083 is equivalent to Revision 1 of this service bulletin. Airplane VN791 has the configuration of a Group 59 airplane. ACTION (PRR B13421-4) For Part 1 (Groups 1-39, 82-87 airplanes), in P36 and P37 panels, install a new relay bracket and two new relays. Change the wiring in P36 panel, P37 panel and P33 panel. Install wiring between P36 panel, P37 panel and P33 panel. Do a functional test. For Part 2 (Groups 40-79, 88 airplanes), in P36 and P37 panels, install a new relay bracket and two new relays. Change the wiring in the P36 panel and P37 panel. Install wiring between P36 panel and P37 panel. Do a functional test For Part 3 (Groups 80-81, 89 airplanes), install two new relays in the P36 panel and two new relays in the P37 panel. Rework two wires in the P36 panel and two wires in the P37 panel. Do a functional test. EFFECTIVITY 767-200, 767-300, 767-300F Airplanes. See Service Bulletin Paragraph 1.A.1 for effectivity. COMPLIANCE Federal Aviation Administration (FAA) Airworthiness Directive 2001-15-08 is related to this service bulletin. Federal Aviation Administration (FAA) Notice of Proposed Rule Making 2006-NM-283-AD, is related to this service bulletin. Boeing recommends that the operators incorporate this service bulletin within 36 months after the release date on this service bulletin. INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the configuration changes given in this service bulletin. MANPOWER MATERIAL INFORMATION Boeing Supplied Kits/Parts. Refer to Paragraph 2.A., Material - Price and Availability. Airplanes Total Task Hours Elapsed Hours Groups 1-39, 82-87 33.0 16.5 Groups 40-79, 88 29.0 14.5 Groups 80-81, 89 5.0 4.0 ### Page 13 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 13 of 339 BOEING SERVICE BULLETIN 767-28A0083 IN THE P37 PANEL, INSTALL A NEW RELAY BRACKET AND TWO RELAYS. CHANGE THE PANEL WIRING. ALTERNATE WIRE ROUTING CONFIGURATION IN THE P33 PANEL, CHANGE THE PANEL WIRING. MAIN EQUIPMENT CENTER IN THE P36 PANEL, INSTALL A NEW RELAY BRACKET AND TWO RELAYS. CHANGE THE PANEL WIRING.WB264 WB590 WB942 ROUTING FWD 497138 ### Page 14 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 14 of 339 BOEING SERVICE BULLETIN 767-28A0083 BLANK PAGE ### Page 15 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 15 of 339 Commercial Airplane Group 767 Service Bulletin Number: 767-28A0083 Date: May 03, 2006 Revision 2: February 12, 2009 ATA System: 2822 2842 SUBJECT: FUEL SYSTEM - Engine Fuel Feed System - Fuel Pump Inlet Protection - Auxiliary Fuel Tank Pump Automatic Shut Off Installation 1. PLANNING INFORMATION A. Effectivity 1. Airplanes Refer to Service Bulletin Index Document D624T001 Part 3 for Airplane Variable Number, Line Number, and Serial Number data. This service bulletin is for the airplanes shown below. An equivalent change is on subsequent production airplanes. Refer to PRR B13421-4 for data about this change. GROUP CONFIGURATION DESCRIPTION 1 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 2 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 3 - Airplanes which had the provisions for the service bulletin installed in production. 4 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 5 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 6 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 7 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. ### Page 16 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 16 of 339 BOEING SERVICE BULLETIN 767-28A0083 8 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 9 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 10 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 11 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 12 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 13 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 14 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 15 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 16 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 17 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 18 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 19 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 20 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 21 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 22 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. GROUP CONFIGURATION DESCRIPTION ### Page 17 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 17 of 339 BOEING SERVICE BULLETIN 767-28A0083 23 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 24 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 25 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 26 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 27 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 28 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 29 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 30 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 31 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 32 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 33 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 34 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 35 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 36 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 37 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. GROUP CONFIGURATION DESCRIPTION ### Page 18 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 18 of 339 BOEING SERVICE BULLETIN 767-28A0083 38 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 39 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 40 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 41 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 42 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 43 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 44 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 45 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 46 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 47 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 48 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 49 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 50 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 51 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 52 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. GROUP CONFIGURATION DESCRIPTION ### Page 19 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 19 of 339 BOEING SERVICE BULLETIN 767-28A0083 53 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 54 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 55 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 56 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 57 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 58 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 59 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 60 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 61 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 62 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 63 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 64 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 65 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 66 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 67 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. GROUP CONFIGURATION DESCRIPTION ### Page 20 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 20 of 339 BOEING SERVICE BULLETIN 767-28A0083 68 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 69 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 70 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 71 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 72 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 73 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 74 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 75 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 76 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 77 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 78 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 79 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-3. 80 - Airplanes which received the intent of the service bulletin in production but the system was not activated. Use Top Kit 015T1775-4 for parts to activate the system. 81 - Airplanes which received the intent of the service bulletin in production but the system was not activated. Use Top Kit 015T1775-4 for parts to activate the system. 82 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. GROUP CONFIGURATION DESCRIPTION ### Page 21 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 21 of 339 BOEING SERVICE BULLETIN 767-28A0083 Airplane models: 767-200 767-300 767-300F IDENTIFICATION BY CUSTOMER, CUSTOMER CODE, GROUP AND VARIABLE NUMBER 767-200ER TANKER-JAPAN (YTD) 89 VR106 AA 767 LLC (SVX) 14 VE067 ABX AIR (ABX) 2 VA311–VA315 3V A 5 0 8 7 VB105–VB123 VB125 82 VA301 VA303–VA306 VA309–VA310 85 VA803 VA807–VA809 86 VB101–VB104 9V B 3 0 2 AEROFLOT (ARO) 57 VN471–VN472 79 VS216–VS217 VS321–VS324 VS392 88 VL896–VL897 83 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 84 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 85 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 86 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 87 - Airplanes with different wiring configurations on the P33, P36, and P37 panels using wire kit 289T1144-2. 88 - Airplanes with different wiring configurations on the P36, and P37 panels using wire kit 289T1144-3 89 - Airplanes which received the intent of the service bulletin in production but the system was not activated. Use Top Kit 015T1775-4 for parts to activate the system. GROUP CONFIGURATION DESCRIPTION ### Page 22 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 22 of 339 BOEING SERVICE BULLETIN 767-28A0083 AEROMEXICO (AMX) 42 VF071 43 VF093 45 VF162 79 VS211 AEROSVIT (UKA) 19 VN154–VN155 64 VN157 AEROTURBINE (AUB) 10 VB321 5 VB055 85 VB051 VB054 AIR ALGERIE (ALG) 25 VK131–VK133 AIR ASTANA (AKZ) 88 VL899–VL900 AIR CANADA (ACN) 18 VN051–VN054 VN056–VN058 4 VA706–VA709 VA711–VA719 57 VN059–VN062 VN531 VN541 VN811–VN812 59 VN546–VN547 VN751–VN752 VN931 6 VB001–VB002 60 VN932–VN936 79 VS381–VS382 VS546–VS549 84 VA701–VA705 85 VB201–VB202 AIR CHINA (BEJ) 14 VE064 17 VE083 VE085–VE086 28 VK161–VK162 29 VK163–VK164 79 VS206 VS208 VS274 AIR DO (HIA) 79 VS176–VS177 AIR EUROPA (ARE) 73 VN638 79 VS292–VS293 AIR ITALY (RIT) 14 VF001–VF002 51 VL913 AIR MADAGASCAR (MAD) 57 VN167 VN731 ### Page 23 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 23 of 339 BOEING SERVICE BULLETIN 767-28A0083 AIR NEW ZEALAND (ANZ) 59 VN653 60 VN655–VN658 AIR PACIFIC (APC) 77 VN676 AIR SEYCHELLES (ASY) 51 VL941 79 VS526 AIR TRANSPORT INTERNATIONAL (TIN) 3 VA509 VA511–VA512 AIR ZIMBABWE (ZMB) 40 VF061 41 VF062 ALITALIA (ALI) 47 VL701–VL702 57 VN813 58 VN423–VN427 VN732 79 VS366–VS367 VS401 ALL NIPPON AIRWAYS (ANA) 23 VK081–VK107 24 VK108–VK113 38 VR401 55 VT501 59 VN193–VN195 60 VN196–VN198 66 VN191–VN192 79 VS721–VS730 80 VS731–VS732 81 VT521–VT522 AMERICAN AIRLINES (AAL) 3 VA514–VA523 VA525 VA527–VA530 33 VN001–VN010 34 VN011–VN015 57 VN016–VN034 58 VN035–VN041 79 VS196–VS203 VS751–VS759 83 VA501–VA505 AMIRI FLIGHT (ABD) 79 VS391 ARAMCO ASSOCIATED COMPANY (RAS) 52 VR084 ### Page 24 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 24 of 339 ARKEFLY (HXL) 57 VN164–VN165 64 VN156 ASIANA AIRLINES (AAR) 26 VK143 27 VK144–VK148 38 VR426 55 VW851 AUSTRIAN AIRLINES AG (AUL) 69 VN242–VN243 76 VN671 79 VS301–VS303 AVIANCA (AVI) 19 VE171–VE172 VN152 42 VF072 43 VF092 45 VF161 57 VN532 AWAS (AWW) 10 VB325 58 VN436 BELAIR AIRLINES (BLB) 50 VL932 BELLVIEW AIRLINES (BEB) 18 VE125–VE126 BLUE CITY HOLDING (BCY) 14 VE069 BLUE PANORAMA AIRLINES (BPA) 59 VN681 65 VN174 79 VS061 BOEING (TBC) 1V A 0 0 1 BRAVO AIRLINES (BVA) 18 VE104 BRISTOL AIR LIMITED (BMD) 85 VA804 ### Page 25 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 25 of 339 BOEING SERVICE BULLETIN 767-28A0083 BRITISH AIRWAYS (BAB) 35 VN111–VN114 61 VN118–VN122 VN124–VN127 62 VN133 63 VN134–VN137 79 VS246–VS248 CAMEROON AIRLINES (CAM) 79 VS308 85 VA801 CARGOJET AIRWAYS LTD. (WNT) 3V A 5 1 0 V A 5 1 3 CHINA EASTERN AIRLINES (CEA) 48 VL871–VL873 CONDOR (CDF) 59 VN683–VN688 60 VN689–VN691 CONTINENTAL AIRLINES (CAL) 52 VR051–VR060 CROCUS CORPORATION (CCS) 79 VS825 CSDS AVIATION (CSO) 3V A 5 0 7 83 VA506 DELTA AIR LINES (DAL) 14 VK036 VK038–VK056 39 VR471–VR472 48 VL753 70 VN251–VN264 71 VN265–VN276 74 VN301–VN306 79 VS066–VS070 VS073–VS078 VS266–VS273 VS466–VS472 82 VA302 EL AL ISRAEL AIRLINES (ELA) 44 VF101–VF102 57 VN537 59 VN682 78 VN972 8 VB282–VB284 87 VB281 ERITREAN AIR LINES (ERJ) 14 VE066 ### Page 26 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 26 of 339 ETHIOPIAN AIRLINES (ETH) 14 VE002 79 VS306 VS496–VS497 VS506–VS507 VS881 80 VS882–VS883 88 VL898 EUROATLANTIC AIRWAYS (MAE) 19 VN151 57 VN551 VN561–VN562 EVERGREEN MAINTENANCE CENTER (EAC) 14 VE061 FIRST CHOICE AIRWAYS (ATZ) 48 VL751–VL752 VL754 57 VN921 59 VN791–VN792 FLORIDA WEST INTERNATIONAL (PAI) 55 VR260 FLYGLOBESPAN.COM (FGS) 60 VN654 79 VS112–VS113 GABON AIRLINES (GBO) 1 VA017–VA018 GECAS (GEF) 18 VE123 GENERIC CUSTOMER/SUPPLIER (XXX) 1V A 0 0 8 GULF AIR (GUL) 32 VL004–VL006 74 VN308 VN310 75 VN314 HAINAN AIRLINES (HNA) 79 VS426–VS428 HAWAIIAN AIRLINES (HWI) 14 VK031–VK034 17 VN171–VN173 57 VN381 79 VS309–VS311 VS821–VS824 VS841–VS843 HEWA BORA AIRWAYS (EXD) 16 VE021 IBA GROUP LIMITED (IBA) 1 VA004–VA005 ### Page 27 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 27 of 339 BOEING SERVICE BULLETIN 767-28A0083 ICELANDAIR (ICE) 36 VN211 64 VN158 INTEGRATED DEFENSE SYSTEMS (BAC) 80 VV001 85 VA806 ITALIAN AIR FORCE (ZSV) 52 VR086 89 VR087 ITOCHU CORPORATION (CIT) 46 VF181–VF184 JAL INTERNATIONAL (JAL) 11 VB371–VB373 VK021–VK022 21 VK001–VK011 22 VK012–VK016 31 VK181 VK186 39 VR441 VR461 79 VS701–VS709 80 VS710–VS714 JETAIRFLY (TLB) 59 VN234 KALAIR (BERMUDA) (KLB) 74 VN311 KAM AIR (KMC) 1V A 0 1 9 KENYA AIRWAYS (KEN) 26 VK141 32 VL003 58 VN421 79 VS331–VS333 KRASAIR (ZXD) 14 VE001 VF051 16 VE022–VE023 LAN AIRLINES (LAN) 47 VL703 55 VR251 VR256–VR259 57 VN063–VN064 VN166 VN168 78 VN966–VN971 79 VS111 VS131–VS133 80 VS901 81 VT511–VT512 ### Page 28 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 28 of 339 BOEING SERVICE BULLETIN 767-28A0083 LATCHARTER (LCH) 57 VN536 VN542 LOT POLISH AIRLINES (LOT) 20 VF041–VF042 59 VN233 VN652 72 VN291 73 VN292–VN293 MALEV HUNGARIAN AIRLINES (HGA) 45 VF172 79 VS136 MARTINAIR HOLLAND (MTH) 37 VN221 57 VN385 67 VN222–VN224 76 VN672 MAXJET AIRWAYS (SLQ) 11 VE041 14 VE063 9 VB301 MEXICANA (CMA) 32 VL001–VL002 MID EAST JET (SKL) 46 VF251 MYTRAVEL AIRWAYS (GUE) 78 VN951–VN953 NATIONWIDE AIRLINES (NWR) 57 VN556 NEOS (NEO) 88 VL892 VL894 NORTH AMERICAN AIRLINES (NNA) 48 VL755 51 VL911 57 VN922 79 VS316 88 VL895 OCEANAIR AIRLINES (OAL) 57 VN376 VN495 VN500 PACE AIRLINES (PIE) 85 VB053 ### Page 29 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 29 of 339 BOEING SERVICE BULLETIN 767-28A0083 PHOENIX AIRCRAFT LEASING, INC. (PLB) 5V A 8 1 0 PLUNA (PLU) 59 VN651 PRIVATAIR (PTS) 79 VS137 QANTAS (QAN) 15 VN081–VN085 35 VN115 59 VN086–VN093 60 VN094–VN099 61 VN116–VN117 VN123 62 VN130–VN132 79 VS186–VS187 VS486 ROSSIYA RUSSIAN AIRLINES (STG) 79 VS263 ROYAL AIR MAROC (RAM) 73 VN636 79 VS336–VS337 ROYAL BRUNEI AIRLINES (RBA) 57 VN372 VN382–VN384 VN386–VN387 RYAN INTERNATIONAL AIRLINES (RYN) 14 VK035 SAFI AIRWAYS (FFI) 17 VE084 SALAMIS AVIATION (LMV) 14 VE068 SHANGHAI AIRLINES (SHA) 30 VK171 39 VR421–VR423 79 VS207 SILVERJET (SVJ) 10 VB329–VB330 14 VE117 SKYMARK AIRLINES (SKM) 79 VS231 VS261–VS262 VS861 SKYSTAR (SYW) 1 VA011–VA012 ### Page 30 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 30 of 339 BOEING SERVICE BULLETIN 767-28A0083 STAR AIR (SBJ) 10 VB323 VB328 12 VB441 13 VB442–VB444 18 VE101–VE103 82 VA307–VA308 STATE AIR COMPANY "BERKUT" (ORE) 53 VR081 TAA (TNL) 1 VA002–VA003 VA014–VA015 VA020 TAMPA CARGO (TMP) 18 VE121–VE122 VE124 TEEBAH AIRLINES (EBH) 4 VA710 THE SULTAN'S FLIGHT (BWN) 45 VF180 THOMSONFLY (BRI) 10 VB331–VB332 51 VL912 VL914 79 VS051–VS056 TRANS-AUSTRALIA AIRLINES (TAA) 1 VA007 TRANSAERO AIRLINES (TRX) 14 VE116 VE118 18 VE143 57 VN371 72 VN631–VN633 74 VN307 VN309 75 VN313 TRANSATLANTIC INTL AIRLINES (TIB) 1 VA016 TURKMENISTAN AIRLINES (TUE) 80 VS891 UNITED AIR LINES (UAL) 57 VN491–VN494 VN496–VN499 VN501–VN513 79 VS091–VS104 UPS (UPS) 54 VR201–VR211 56 VW701–VW721 ### Page 31 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 31 of 339 BOEING SERVICE BULLETIN 767-28A0083 US AIRWAYS (USA) 18 VE141–VE142 VE144–VE149 VE151–VE152 UZBEKISTAN AIRWAYS (UZB) 49 VL806–VL807 79 VS844 80 VS896 VARIG AIRLINES (VAR) 59 VN231–VN232 VISION AIR (VEG) 1 VA006 VA009–VA010 VIVA MACAU (VMC) 26 VK142 43 VF091 VOLARE S.P.A (VLR) 50 VL931 VRG LINHAS AEREAS S.A. (VGG) 18 VN055 45 VF171 57 VN163 VN557 58 VN388 VN422 59 VN753 68 VN225 73 VN637 79 VS307 WEST DOVER LLC (WDR) 14 VK037 XL AIRWAYS (SBE) 10 VB326–VB327 17 VL011 19 VN153 YONA (IOP) 75 VN312 ZOOM AIRLINES (YFM) 72 VN634–VN635 79 VS291 88 VL891 VL893 ### Page 32 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 32 of 339 BOEING SERVICE BULLETIN 767-28A0083 IDENTIFICATION BY VARIABLE NUMBER Variable Group VA001–VA020 1 VA301–VA310 82 VA311–VA315 2 VA501–VA506 83 VA507–VA530 3 VA701–VA705 84 VA706–VA719 4 VA801–VA809 85 VA810 5 VB001–VB002 6 VB051–VB054 85 VB055 5 VB101–VB104 86 VB105–VB125 7 VB201–VB202 85 VB281 87 VB282–VB284 8 VB301–VB302 9 VB321–VB332 10 VB371–VB373 11 VB441 12 VB442–VB444 13 VE001–VE003 14 VE021–VE023 16 VE041–VE043 11 VE061–VE069 14 VE083–VE086 17 VE101–VE104 18 VE116–VE118 14 VE121–VE126 18 VE141–VE152 18 VE171–VE172 19 VF001–VF002 14 VF041–VF042 20 VF051 14 VF061 40 VF062 41 ### Page 33 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 33 of 339 BOEING SERVICE BULLETIN 767-28A0083 VF071–VF072 42 VF091–VF093 43 VF101–VF102 44 VF161–VF162 45 VF171–VF172 45 VF180 45 VF181–VF184 46 VF251 46 VK001–VK011 21 VK012–VK016 22 VK021–VK022 11 VK031–VK056 14 VK081–VK107 23 VK108–VK113 24 VK131–VK133 25 VK141–VK143 26 VK144–VK148 27 VK161–VK162 28 VK163–VK164 29 VK171 30 VK181 31 VK186 31 VL001–VL006 32 VL011 17 VL701–VL703 47 VL751–VL755 48 VL806–VL807 49 VL871–VL873 48 VL891–VL900 88 VL911–VL914 51 VL931–VL932 50 VL941 51 VN001–VN010 33 VN011–VN015 34 VN016–VN034 57 VN035–VN041 58 VN051–VN058 18 VN059–VN064 57 VN081–VN085 15 Variable Group ### Page 34 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 34 of 339 BOEING SERVICE BULLETIN 767-28A0083 VN086–VN093 59 VN094–VN099 60 VN111–VN115 35 VN116–VN127 61 VN130–VN133 62 VN134–VN137 63 VN151–VN155 19 VN156–VN158 64 VN163–VN168 57 VN171–VN173 17 VN174 65 VN191–VN192 66 VN193–VN195 59 VN196–VN198 60 VN211–VN212 36 VN221 37 VN222–VN224 67 VN225 68 VN231–VN234 59 VN242–VN243 69 VN251–VN264 70 VN265–VN276 71 VN291 72 VN292–VN293 73 VN301–VN311 74 VN312–VN314 75 VN371–VN372 57 VN376 57 VN381–VN387 57 VN388 58 VN421–VN427 58 VN436 58 VN471–VN472 57 VN491–VN513 57 VN531–VN532 57 VN536–VN537 57 VN541–VN542 57 VN546–VN547 59 VN551 57 Variable Group ### Page 35 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 35 of 339 BOEING SERVICE BULLETIN 767-28A0083 VN556–VN557 57 VN561–VN562 57 VN631–VN635 72 VN636–VN638 73 VN651–VN653 59 VN654–VN658 60 VN671–VN672 76 VN676 77 VN681–VN688 59 VN689–VN691 60 VN731 57 VN732 58 VN751–VN753 59 VN791–VN792 59 VN811–VN813 57 VN921–VN922 57 VN931 59 VN932–VN936 60 VN951–VN953 78 VN966–VN972 78 VR051–VR060 52 VR081 53 VR084 52 VR086 52 VR087 89 VR106 89 VR201–VR211 54 VR251 55 VR256–VR260 55 VR401 38 VR421–VR423 39 VR426 38 VR441 39 VR461 39 VR471–VR472 39 VS051–VS056 79 VS061 79 VS066–VS070 79 VS073–VS078 79 Variable Group ### Page 36 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 36 of 339 BOEING SERVICE BULLETIN 767-28A0083 VS091–VS104 79 VS111–VS113 79 VS131–VS133 79 VS136–VS137 79 VS176–VS177 79 VS186–VS187 79 VS196–VS203 79 VS206–VS208 79 VS211 79 VS216–VS217 79 VS231 79 VS246–VS248 79 VS261–VS263 79 VS266–VS274 79 VS291–VS293 79 VS301–VS303 79 VS306–VS311 79 VS316 79 VS321–VS324 79 VS331–VS333 79 VS336–VS337 79 VS366–VS367 79 VS381–VS382 79 VS391–VS392 79 VS401 79 VS426–VS428 79 VS466–VS472 79 VS486 79 VS496–VS497 79 VS506–VS507 79 VS526 79 VS546–VS549 79 VS701–VS709 79 VS710–VS714 80 VS721–VS730 79 VS731–VS732 80 VS751–VS759 79 VS821–VS825 79 VS841–VS844 79 Variable Group ### Page 37 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 37 of 339 BOEING SERVICE BULLETIN 767-28A0083 2. Spares Affected None. B. Concurrent Requirements None. C. Reason This service bulletin is the result of the safety assessments conducted by Boeing under SFAR 88, "Fuel Tank System Fault Tolerance Evaluation Requirements". Initial results from the Fuel System Safety Analysis show that fuel pumps that run dry could cause an overheat condition external of the pump explosion resistance area that is open to the pump inlet. An overheat condition in this area could possibly cause an unwanted ignition source for the fuel vapors in the fuel tank. Ignition of flammable fuel vapors could cause a fire or explosion which could put the airplane in an unsafe condition. Installation of the automatic shut off system adds fuel pump inlet protection against sparks caused by friction overheat damage in the fuel tanks. This service bulletin gives the instructions and a kit of parts to install an automatic shut off system for the center wing tank override boost pumps. Installation of the automatic system will prevent a potential ignition source in the tank by making sure the pumps do not run for an extended period of time when the fuel level is below pump inlet or the pump has failed. Currently the flight crew turns off the pumps when a pump low pressure message is displayed on EICAS. The automatic shut off system installed by this service bulletin will make sure that the pumps will not run for more than 15 seconds with continuous low fuel pressure if the flight crew does not respond to the EICAS message sooner. The flight crew remains in primary control, with this automatic shut off system as a backup, to turn the pumps off after continuous low pressure indication. This change affects Section 9 of the Maintenance Planning Data (MPD) Document. New Airworthiness Limitations (AWL) "28-AWL-20" will be added to Section 9 of the MPD to include a functional check of the center tank fuel boost pump automatic shut off system. This change also affects Section 1 and 3.1 of the FAA Approved Airplane Flight Manual. VS861 79 VS881 79 VS882–VS883 80 VS891 80 VS896 80 VS901 80 VT501 55 VT511–VT512 81 VT521–VT522 81 VV001 80 VW701–VW721 56 VW851 55 Variable Group ### Page 38 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 38 of 339 BOEING SERVICE BULLETIN 767-28A0083 Federal Aviation Administration (FAA) Airworthiness Directive 2001-15-08 are related to this service bulletin. As a part of a service bulletin validation program, this change was completed on airplane VN791 by initial release of Service Bulletin 767-28A0083 and before the release of Revision 1 of this service bulletin. The change was completed on airplane VN791 by Service Bulletin 767-28A0083 is equivalent to Revision 1 of this service bulletin. Airplane VN791 has the configuration of a Group 59 airplane. Revision 1 is sent to address the comments received from operators since the initial release of the service bulletin and incorporate differences identified during the validation of the service bulletin. The following sections of the service bulletin are changed in Revision 1: — The Summary Section, Group and Configuration tables in Section 1.A, Description Section 1.D, Man-power tables Section 1.G, Accomplishment Instructions Section 3 and Figures 1-5, 7-8, 19- 20, 22, 33, 41-43, 45, 54- 57, 68-70, 73, 76, 81 and 158 are revised by the following new airplane Groups: — Approval Section 1.F, to include new requirements. — Weight and Balance table Section1.H, to show new information based on airplane model. — Material - Price and Availability to add new pricing and Groups to -2 Top-Kit. — Accomplishment Instructions Section 3. to clarify airplane Groups applicability and added Airplane Maintenance Manual (AMM) for Functional Test Requirements. — Figures 1-5, 7-8, 19-20, 22-23, 33, 41-43, 45, 54-57, 68-70, 73, 76, 81, 102, 111, 117, 130, 136, 139, 146, 151 to correct or add in effectivity and groups changed. — Figures 4-18, 34, 36, 69-77, 84-104, 115-120, 122, 124, 128-129, 132, 144-147 revised to correct typographical error. — Figures 1-2 added groups 82-87 and removed the bonding requirement from the relay mounting bracket. — Figures 33, 68 to clarify the relay location and add groups 82-87. — Figures 82-83 removed the bonding requirement from the relay mounting bracket. — Figures 114 and 143 revised to clarify the relay location. — Figure 158 added new figure for group 82-87 airplanes. — Figures 1 and 82 revised FWD locator direction on views A-A and B-B. The data given in Information Notice 767-28A0083 IN 01 is included in this revision. Revision 2 is sent to address the comments received from operators since the release of Revision 1 of the service bulletin. Airplanes Affected Old Airplane Group New Airplane Group VA301-VA310 2 82 VA501-VA506 3 83 VA701-VA705 4 84 VA801-VA809 VB051-VB054 VB201-VB202 58 5 VB101-VB104 7 86 VB281 8 87 ### Page 39 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 39 of 339 BOEING SERVICE BULLETIN 767-28A0083 The effectivity group assignments were changed to show the correct wiring configuration for the affected airplanes. The following sections of the service bulletin are changed: — The Summary illustration, revised to show the wire bundle routing more accurately and show an alternate wire routing configuration. — Summary - BackGround, Planning Information - Reason and Compliance Section, revised AD reference to remove AD 94-11-05. The AD 94-11-05 is superseded by AD 2001-15-08. — Group and Configuration tables in Section 1.A, Description Section 1.D, Man-power tables Section 1.G, Weight and Balance Section H, Accomplishment Instructions Section 3, added new Groups 88 and 89 airplanes. — In Paragraph 2.K, Publications Affected, 767 Flight Crew Operating Manual, impacts 0.6 Preface, NP.21 and chapter 12. — In Paragraph 3.B, Work Instructions, Part 1, new step 37, added for Groups 82-87, Figure 158. — In Paragraph 3.B, Work Instructions, Part 1, step 68, the text has been corrected to read Figure 68. — In Paragraph 3.B, Work Instructions, Part 1, step 69, the text has been corrected to read Figure 67. — In Paragraph 3.B, Work Instructions, Part 2, new step 9 added for new Figure 159, Group 88. — In Paragraph 3.B, Work Instructions, Part 2, step 31, added Group 78. — In Paragraph 3.B, Work Instructions, Part 2, new step 71 added for new Figure 160, Group 88. — In Paragraph 3.B, Work Instructions, Part 2, steps 1-3, 34-35, 38, 50, 64, 71-71 and 74-77 added Group 88. — In Paragraph 3.B, Work Instructions, Part 3, steps 1-4 and 7-12, added Group 89. — Figures 1 and 82, revised to show a alternate configuration for the relay mounting holes. — Figures 53, revised wire bundle reference on terminal YC12 from W198 to W1118. — Figures 4-32, 34-66, 68, 79-80, 84-113, 115-142, 150-151 and 158, revised Flag Note Table to add Burndy terminal block information. — Figures 78, 148 and 149, revised to remove the shield reference for wire 942-011-24. — Figures 81 and 152, revised to show the wire bundle routing more accurately and show an alternate wire routing configuration. Wire bundle routing from P36 to P33 was added to Figure 81. — Figures 82-83, 113-114, 117, 129, 143, 150, 152 added Group 88. — Figure 124, revised to correct a typographical error on the Burndy block call out and show wire W198-188-24 as a deleted wire. — Figure 153 added Group 89. — Figure 154, added Group 89, added relay mounting hardware information and revised Circle Note 3. — Figure 155, revised to show the correct connector number. Airplanes VR087 and VR106 were moved to new Figure 161and revised to be Group 89 airplanes. — Figure 156, revised to show the correct connector number. — Figure 157, added Group 89 and added relay mounting hardware information. — Figures 159 and 160, created new figures for new Group 88 airplanes. Group 88 airplanes required the use of pin 40 in connector D5658J and D5658P. Airplanes Affected Old Airplane Groups Airplane Groups VL891-VL900 49 88 (new) VR087 80 89 (new) VR106 80 89 (new) VR901 81 80 (existing) VT521-VT522 80 81 (existing) ### Page 40 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 40 of 339 BOEING SERVICE BULLETIN 767-28A0083 — Figures 161, created new figure for new Group 89 airplanes. Group 89 airplanes required the use of wire W198-02A-24 and pin 8 in connector D5052J and D5052P. The data given in Information Notice 767-28A0083 IN 02 is included in this revision. D. Description For Part 1 (Groups 1-39, 82-87 airplanes), in P36 and P37 panels, install a new relay bracket and two new relays. Change the wiring in P36 panel, P37 panel and P33 panel. Install wiring between P36 panel, P37 panel and P33 panel. Do a functional test. For Part 2 (Groups 40-79, 88 airplanes), in P36 and P37 panels, install a new relay bracket and two new relays. Change the wiring in the P36 panel and P37 panel. Install wiring between P36 panel and P37 panel. Do a functional test For Part 3 (Groups 80-81, 89 airplanes), install two new relays in P36 panel and two new relays in P37 panel. Rework two wires in P36 panel and two wires in P37 panel. Do a functional test. Revision 1 - No more work is necessary on airplanes changed as shown in the original issue of this service bulletin. Revision 2 - No more work is necessary on airplanes changed as shown in Revision 1 or the initial release of this service bulletin. E. Compliance Federal Aviation Administration (FAA) Notice of Proposed Rule Making 2006-NM-283-AD, is related to this service bulletin. Federal Aviation Administration (FAA) Airworthiness Directive 2001-15-08 is related to this service bulletin. Boeing recommends operators incorporate this service bulletin within 36 months after the release date on the service bulletin. F. Approval This service bulletin was examined by the Federal Aviation Administration (FAA). The changes specified in this service bulletin comply with the applicable regulations and are FAA approved, as well as European Aviation Safety Agency (EASA)/Joint Aviation Authorities (JAA) approved for all EASA/ JAA approved airplanes listed in the service bulletin effectivity. This service bulletin and its approval were based on the airplane in its original Boeing delivery configuration or as modified by other approved Boeing changes. If an airplane has a non-Boeing modification or repair that affects a component or system also affected by this service bulletin, the operator is responsible for obtaining appropriate regulatory agency approval before incorporating this service bulletin. ### Page 41 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 41 of 339 BOEING SERVICE BULLETIN 767-28A0083 This service bulletin has been approved by the FAA. In addition, the Manager of the FAA Seattle Aircraft Certification Office approves the action (i.e. inspection or modification) defined in this service bulletin as an Alternative Method Of Compliance (AMOC) to the requirements of paragraphs (b) (1), (b) (2), (b) (3), (b) (4), (c) (1), (c) (2), (c) (3), and (c) (4) of AD 2001-15-08. All provisions of AD 2001- 15-08 that are not specifically referenced in the above statement remain fully applicable and must be complied with. Compliance with the conditions of this AMOC approval requires concurrent incorporation of the associated revisions to Airplane Flight Manual Section 1 and 3.1, and incorporation of the related Airworthiness Limitations (AWL) in Section 9 of the MPD into the operator’s maintenance documentation. The following information was given by Information Notice 767-28A0083 IN 01, dated June 19, 2006. The FAA has informed Boeing that Paragraph 1.F, Approval, which states that the Manager of the FAA Seattle Aircraft Certification Office has approved the action defined in this service bulletin as an alternative method of compliance to the requirements of paragraph (b) and (c) of AD 2001-15-08 is not complete. The FAA approval includes a condition as part of the approval of the AMOC. This condition of approval is not listed in Paragraph 1.F of Revision 0 of the service bulletin and is not part of the existing Airworthiness Directive, AD 2001-15-08. The condition of approval specified by the FAA addresses mixed fleet operations and requires work to be done on unmodified airplanes in addition to the actions defined in the service bulletin, to achieve an alternative method of compliance to the requirements of paragraph (b) and (c) of AD 2001-15-08. Additional information is in FAA AMOC approval letter 140S-07-63 containing the AMOC approval, copies of the FAA letter are available upon request. G. Manpower The table below shows an estimate of the task-hours necessary to do this modification for each airplane. This estimate is for direct labor only, done by an experienced crew. Adjust the estimate with operator task-hour data if necessary. The estimate does not include lost time. These are some examples of lost time: — Time to adjust to the workplace — Time to schedule the work — Time to examine the work — Time to cure the materials — Time to make the parts — Time to find the tools. Group 1-39, 82-87: Task Number of Persons Task-Hours Elapsed Hours Open Access 2 1.0 0.50 Figure 1, P36, Bracket installation 20 . 7 5 0 . 3 8 Figure 2, P37 Bracket Installation 20 . 7 5 0 . 3 8 ### Page 42 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 42 of 339 BOEING SERVICE BULLETIN 767-28A0083 Figure 3, P33 Panel Wiring change. 2 0.50 0.25 Figures 4-32, P36 Panel wiring change. 28 . 9 4 . 4 5 Figures 33, P36 Panel relay installation. 2 0.75 0.38 Figures 34-67, 79- 80, 158, P37 Panel wiring changes. 2 8.70 4.35 Figures 68, P37 Panel relay installation. 2 0.75 0.38 Figures 69-72, P33 to P36 Wiring changes. 2 4.00 2.00 Figures 73-78, P33 to P37 Wiring changes. 2 3.90 1.95 Figure 81, P36 to P37, Wire Bundle Routing. n/a n/a n/a Close Access 2 1.0 0.50 Test 2 2.0 1.0 TOTAL FOR EACH AIRPLANE 33.0 16.5 Group 40-79, 88: Task Number of Persons Task-Hours Elapsed Hours Open Access 2 1.0 0.50 Figure 82, P36 Panel, Bracket Installation 2 0.75 0.38 Figure 83, P37 Panel Bracket Installation 2 0.75 0.38 Figures 84-113, 159, P36 Panel, Wiring changes. 2 8.90 4.45 Group 1-39, 82-87: Task Number of Persons Task-Hours Elapsed Hours ### Page 43 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 43 of 339 BOEING SERVICE BULLETIN 767-28A0083 Figure 114, P36 Panel, Relay Installation. 20 . 7 5 0 . 3 8 Figures 115-142, 150-151, P37 Panel, Wiring Changes. 28 . 7 0 4 . 3 5 Figure 143, P37 Panel Relay installation. 20 . 7 5 0 . 3 8 Figures 144-149, 160, P36 to P37 Panel Wiring Changes. 24 . 0 0 2 . 0 0 Figure 152, P36 to P37 Panel wire bundle routing. n/a n/a n/a Close Access 2 1.0 0.50 Test 2 2.0 1.0 TOTAL FOR EACH AIRPLANE 29.0 14.5 Group 80-81, 89: Task Number of Persons Task-Hours Elapsed Hours Open Access 1 0.25 .25 Figure 153, P36 Panel wiring Changes 11 . 1 0 1 . 1 0 Figure 154, P36 Panel Relay installation. 10 . 1 5 0 . 1 5 Figures 155, 156, 161, P37 Panel Wiring changes. 11 . 1 0 1 . 1 0 Figure 157, P37 Panel Relay installation. 10 . 1 5 0 . 1 5 Close Access 1 0.25 0.25 Test 2 2.0 1.0 TOTAL FOR EACH AIRPLANE 5.00 4.00 Group 40-79, 88: Task Number of Persons Task-Hours Elapsed Hours ### Page 44 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 44 of 339 BOEING SERVICE BULLETIN 767-28A0083 H. Weight and Balance Changes I. Electrical Load Data Not changed. J. References 1. Existing Data: a. Engineering Change Memo PRR B13421-4 b. 767 Aircraft Maintenance Manual (AMM) 20-10-11, 20-10-12, 20-10-19, 24-22-00, 28-22-00, 28-31-00 c. 767 Maintenance Planning Document (MPD) Section 9 d. 767 Wiring Diagram 28-22-12, 28-42-12 e. 767 Wiring Diagram Manual (WDM) 28-22-12, 28-22-12, 28-42-12, 28-42-12 f. Boeing Drawing 012W6100 g. Boeing Parts Standards Document D-590 h. FAA Airworthiness Directive 2001-15-08 i. Standard Wiring Practices Manual (SWPM) 20-10-11, 20-10-11, 20-10-12, 20-10-22, 20-20-00, 20-30-11, 20-60-00, 20-61-11, 20-81-12, 20-81-19, 20-81-22, 20-90-11 2. Data supplied with this Service Bulletin: None. Airplane Group Airplane Model Change in Weight (Pounds) Change in Moment (Pound-Inches) Groups 1-39, 82-87 -200 +2.7 +891.0 -300 +2.7 +564.3 Groups 40-79, 88 -200 +2.5 +825.0 -300 +2.5 +522.5 Groups 80-81, 89 N/A 0.0 0.0 ### Page 45 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 45 of 339 BOEING SERVICE BULLETIN 767-28A0083 3. Installation Drawings Used in the Preparation of this Service Bulletin: These drawings were used to prepare this service bulletin. These drawings are not necessary to make the specified changes, and are not supplied with this service bulletin. These drawings may not be applicable to all airplane configurations or operators. K. Publications Affected L. Interchangeability and Intermixability of Parts Accomplishment of this service bulletin does not affect interchangeability or intermixability of parts. Drawing Number Title 284T3600 Panel Installation Left P36 Panel 284T3601 Equip Assy Left P36 Panel 284T3700 Panel Installation Right P37 Panel 284T3701 Equip Assy Right P37 Panel Publication Chapter-Section 767 FAA Approved Airplane Flight Manual * 767 Flight Crew Operating Manual 0.6 Preface, NP.21 and chapter 12 767 Maintenance Planning Data Document (MPD) Section 6, Section 9 767 Maintenance Manual 28-22 767 Wiring Diagram Manual 28-22-12, 28-42-12 767 Fault Isolation Manual 28-22 767 Schematic Diagram Manual 28-22-01 767 Illustrated Parts Catalog 28-22 * This change affects Section 1 and 3.1 of the FAA Approved Airplane Flight Manual. Operators will receive applicable data. ### Page 46 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 46 of 339 BOEING SERVICE BULLETIN 767-28A0083 BLANK PAGE ### Page 47 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 47 of 339 BOEING SERVICE BULLETIN 767-28A0083 2. MATERIAL INFORMATION A. Material - Price and Availability Boeing can supply the kits shown in Paragraph 2.C., Parts Necessary For Each Airplane as shown below. If there is a limit to the quantity (QTY) of available kits, a supply sequence is given by Spares. More kits become available as shown in the Reorder Lead Time (ROLT). ROLT is calculated from the date Boeing gets the purchase order. The kits are subject to the terms and conditions of the Boeing standard purchase order acknowledgment. After the Unit Price date, new price and ROLT data is applicable. Prices are in United States dollars. Terms: Net 30 days. Reference this service bulletin and submit your purchase order by one of the methods that follow: 1. Order on-line via ATA Spec 2000 or Boeing Part Page 2. Fax to (206) 662-7145 3. Spares Customer Support - MC 36-65 Boeing Spares Department P.O. Box 3707 Seattle, Washington 98124-2207 USA B. Industry Support Information Boeing warranty remedies are not available for the configuration changes given in this service bulletin. C. Parts Necessary For Each Airplane 1. Kits/Parts: To get the kits/parts shown below, refer to Paragraph 2.A., Material - Price and Availability. Kit Number Name Date QTY ROLT (Weeks) Unit Price thru July 31, 07 015T1775-2 Top Kit, Auxiliary Fuel Tank Pump Inlet Protection Installation, Groups 1 through 39 and Groups 82 through 87 Airplanes. AVAILABLE 75 20 $9,374.00 015T1775-3 Top Kit, Auxiliary Fuel Tank Pump Inlet Protection Installation, Group 40 through 79 and 88 Airplanes. AVAILABLE 124 20 $8,924.00 015T1775-4 Top Kit, Auxiliary Fuel Tank Pump Inlet Protection Installation, Groups 80, 81 and 89 Airplanes AVAILABLE 5 20 $421.00 ### Page 48 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 48 of 339 BOEING SERVICE BULLETIN 767-28A0083 NOTE: One top kit and the items shown in Paragraph 2.C.2., Parts and Materials Supplied by the Operator, are necessary for each airplane. Kit 015T1775 New Part Number QTY Name Existing Part Number Notes-4 -3 -2 015T1775-2 . . - Top Kit, Auxiliary Fuel Tank Pump Inlet Protection Installation, Groups 1 through 39 Airplanes. -- -- 015T1775-3 . - . Top Kit, Auxiliary Fuel Tank Pump Inlet Protection Installation, Groups 40 through 79 Airplanes. -- -- 015T1775-4 - . . Top Kit, Auxiliary Fuel Tank Pump Inlet Protection Installation, Groups 80 and 81 Airplanes. -- -- 289T1144-2 - - 1 Wire Kit -- -- 289T1144-3 - 1 - Wire Kit -- -- 284T0378-233 - 1 1 Bracket -- -- 284T0378-234 - 1 1 Bracket -- -- BACR13CD2 2 2 2 Relay -- (b) TDH-1852-1402 2 2 2 Relay -- (b) BACS12GU3K7 - 4 4 Screw -- (a) NAS1149D0332H - 4 4 Washer -- -- MS39029/11-145 3 - - Contact -- -- (a) If grip length shown is not available at Boeing, fasteners supplied in kits may be one grip length longer than indicated. Also, if any fasteners part numbers listed are not available or have been superseded, substitute fasteners may be supplied in kits. Boeing Document D-590 and Boeing Drawing 012W6100 are used to determine the part numbers used as substitutes. (b) For mounting hardware information, refer to SWPM 20-81-22 as an accepted procedure. Kit 289T1144 New Part Number QTY Name Existing Part Number Notes-104 -103 -102 -101 -3 -2 2 8 9 T 1 1 4 4 - 2 ..... - - W i r e K i t - - ( a ) 2 8 9 T 1 1 4 4 - 3 .... - - . W i r e K i t - - ( a ) 289T1144-101 . . . -- . 1 Subkit (W0146) -- (a) 289T1144-102 . . -- . 1 1 Subkit (W0176) -- (a) 289T1144-103 . -- . . 1 1 Subkit (W0184) -- (a) 289T1144-104 -- . . . 1 1 Subkit (W0188) -- (a) 289T1144-101W . . . 1 . . Wire -- -- 289T1144-10101 . . . 1 . . Lacing tape -- -- ### Page 49 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 49 of 339 BOEING SERVICE BULLETIN 767-28A0083 289T1144-10102 . . . 1 . . Identification Tape -- -- 289T1144-102W . . 1 . . . Wire 289T1144-10201 . . 1 . . . Lacing Tape -- -- 289T1144-10202 . . 1 . . . Identification Tape -- -- 289T1144-10203 . . 1 . . . Identification Tape -- -- 289T1144-10204 . . 1 . . . Identification Tape -- -- 289T1144-10205 . . 1 . . . Identification Tape -- -- 289T1144-10206 . . 1 . . . Identification Tape -- -- 289T1144-10207 . . 1 . . . Identification Tape -- -- 289T1144-10208 . . 1 . . . Identification Tape -- -- 289T1144-10209 . . 1 . . . Identification Tape -- -- 289T1144-10210 . . 1 . . . Identification Tape -- -- 289T1144-10211 . . 1 . . . Identification Tape -- -- 2 8 9 T 1 1 4 4 - 1 0 3 W . 1 .... W i r e - - - - 2 8 9 T 1 1 4 4 - 1 0 3 0 1 . 1 .... L a c i n g T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 3 0 2 . 1 .... I d e n t i f i c a t i o n T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 3 0 3 . 1 .... I d e n t i f i c a t i o n T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 3 0 4 . 1 .... I d e n t i f i c a t i o n T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 3 0 5 . 1 .... I d e n t i f i c a t i o n T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 3 0 6 . 1 .... I d e n t i f i c a t i o n T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 3 0 7 . 1 .... I d e n t i f i c a t i o n T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 4 W 1 ..... W i r e - - - - 2 8 9 T 1 1 4 4 - 1 0 4 0 1 1 ..... L a c i n g T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 4 0 2 1 ..... I d e n t i f i c a t i o n T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 4 0 3 1 ..... I d e n t i f i c a t i o n T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 4 0 4 1 ..... I d e n t i f i c a t i o n T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 4 0 5 1 ..... I d e n t i f i c a t i o n T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 4 0 6 1 ..... I d e n t i f i c a t i o n T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 4 0 7 1 ..... I d e n t i f i c a t i o n T a p e - - - - B A C C 4 7 C N 1 S 2141 . . C o n t a c t - - - - M39029/11-145 4 3 11 1 . . Contact -- -- B A C S 1 6 A G 1 .. 1 ... R e l a y S o c k e t - - - - BACS16AH1 . . 1 . . . Relay Socket -- -- BACT12AR222 . . 1 . . . Terminal Lug -- -- BACC47FJ2A . . 1 . . . Contact -- -- BACC47FJ1A 1 . 1 . . . Contact -- -- BACC47FK1A . 1 2 . . . Contact -- -- Kit 289T1144 New Part Number QTY Name Existing Part Number Notes-104 -103 -102 -101 -3 -2 ### Page 50 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 50 of 339 BOEING SERVICE BULLETIN 767-28A0083 B A C C 4 7 D J 1 .. 2 ... C o n t a c t - - - - BACC47ER1 . 1 8 . . . Contact -- -- B A C C 4 7 C P 1 S 2 1 .... C o n t a c t - - - - B A C C 4 7 C N 2 . 2 .... C o n t a c t - - - - B A C C 4 7 F J 2 A . 1 .... C o n t a c t (a) There are more parts than are necessary. Kit 289T1144 New Part Number QTY Name Existing Part Number Notes-108 -107 -106 -105 -3 -2 2 8 9 T 1 1 4 4 - 2 ..... - - W i r e K i t - - ( a ) 2 8 9 T 1 1 4 4 - 3 .... - - . W i r e K i t - - ( a ) 289T1144-105 . . . -- 1 1 Subkit (W0192) -- (a) 289T1144-106 . . -- . 1 1 Subkit (W0198) -- (a) 289T1144-107 . -- . . . 1 Subkit (W0264) -- (a) 289T1144-108 -- . . . 1 1 Subkit (W0590) -- (a) 289T1144-105W . . . 1 . . Wire -- -- 289T1144-10501 . . . 1 . . Lacing tape -- -- 289T1144-10502 . . . 1 . . Identification Tape -- -- 289T1144-10503 . . . 1 . . Identification Tape -- -- 289T1144-10504 . . . 1 . . Identification Tape -- -- 289T1144-10505 . . . 1 . . Identification Tape -- -- 289T1144-10506 . . . 1 . . Identification Tape -- -- 289T1144-10507 . . . 1 . . Identification Tape -- -- 289T1144-10508 . . . 1 . . Identification Tape -- -- 289T1144-106W . . 1 . . . Wire -- -- 289T1144-10601 . . 1 . . . Lacing Tape -- -- 289T1144-10602 . . 1 . . . Identification Tape -- -- 2 8 9 T 1 1 4 4 - 1 0 7 W . 1 .... W i r e - - - - 2 8 9 T 1 1 4 4 - 1 0 7 0 2 . 1 .... L a c i n g T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 7 0 3 . 1 .... I d e n t i f i c a t i o n T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 7 0 4 . 1 .... I d e n t i f i c a t i o n T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 8 W 1 ..... W i r e - - - - 2 8 9 T 1 1 4 4 - 1 0 8 0 2 1 ..... L a c i n g T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 8 0 3 1 ..... I d e n t i f i c a t i o n T a p e - - - - 2 8 9 T 1 1 4 4 - 1 0 8 0 4 1 ..... I d e n t i f i c a t i o n T a p e - - - - B A C C 4 7 C N 1 S 1 ..... C o n t a c t - - - - Kit 289T1144 New Part Number QTY Name Existing Part Number Notes-104 -103 -102 -101 -3 -2 ### Page 51 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 51 of 339 BOEING SERVICE BULLETIN 767-28A0083 M39029/11-145 . . 2 12 . . Contact -- (a) BACS16AG1 . . . 1 . . Relay Socket -- -- BACS16AH1 . . . 1 . . Relay Socket -- -- BACT12AR222 . . . 2 . . Terminal Lug -- -- B A C C 4 7 F J 2 A ...... C o n t a c t - - - - BACC47FJ1A . . . 2 . . Contact -- -- BACC47FK1A . . . 1 . . Contact -- -- BACC47DJ1 . . . 2 . . Contact -- -- BACC47ER1 . . . 8 . . Contact -- -- B A C C 4 7 C P 1 S 1223 . . C o n t a c t - - - - Y-9015-C 1 . 1 . . . Eyelet -- -- BACC47CP3T . . 1 . . . Contact -- -- B A C C 4 7 C N 3 1 ..... C o n t a c t - - - - (a) There are more parts than are necessary. Kit 289T1144 New Part Number QTY Name Existing Part Number Notes-201 -110 -109 -3 -2 2 8 9 T 1 1 4 4 - 2 .... - - W i r e K i t - - ( a ) 289T1144-3 . . . -- . Wire Kit -- (a) 289T1144-109 . . -- 1 1 Subkit (W0942) -- (a) 289T1144-110 . -- . 1 1 Subkit (W1118) -- (a) 289T1144-201 -- . . 1 1 Spares (a) 289T1144-109W . . 1 . . Wire -- -- 289T1144-10901 . . 1 . . Lacing tape -- -- 289T1144-10902 . . 1 . . Identification Tape -- -- 289T1144-10903 . . 1 . . Identification Tape -- -- 289T1144-10904 . . 1 . . Identification Tape -- -- 289T1144-10905 . . 1 . . Identification Tape -- -- 289T1144-10906 . . 1 . . Identification Tape -- -- 289T1144-110W . 1 . . . Wire -- -- 289T1144-11001 . 1 . . . Lacing Tape -- -- 289T1144-11002 . 1 . . . Identification Tape -- -- 289T1144-11003 . 1 . . . Identification Tape -- -- BACC47CN1S 2 1 1 . . Contact -- -- M39029/11-145 2 1 . . . Contact -- -- B A C T 1 2 A R 2 2 22 .... T e r m i n a l L u g - - - - Kit 289T1144 New Part Number QTY Name Existing Part Number Notes-108 -107 -106 -105 -3 -2 ### Page 52 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 52 of 339 BOEING SERVICE BULLETIN 767-28A0083 2. Parts and Materials Supplied by the Operator: None. 3. Parts Modified and Reidentified: None. 4. Parts Removed and Not Replaced: None. D. Parts Necessary to Change Spares None. E. Special Tooling - Price and Availability None. F. Special Tooling Necessary to do this Service Bulletin No special tools or equipment are necessary to do the change in this service bulletin. But, maintenance and overhaul tools in the manuals given in Paragraph 1.J., References, can be necessary. Examine operator tool supply to make sure all necessary tools are available. B A C C 4 7 F J 2 A 2 .... C o n t a c t - - - - BACC47FJ1A 2 1 1 . . Contact -- -- BACC47FK1A 2 . 1 . . Contact -- -- B A C C 4 7 D J 1 2 .... C o n t a c t - - - - BACC47ER1 2 . . . Contact -- -- BACC47CP1S 2 . 2 . . Contact -- -- B A C C 4 7 C N 2 2 .... C o n t a c t - - - - Y - 9 0 1 5 - C 1 .... E y e l e t - - - - B A C M 1 5 C 3 C 2 .... B u r n d y B l o c k - - ( b ) B A C M 1 5 C 3 B 2 .... B u r n d y B l o c k - - ( b ) (a) There are more parts than are necessary. Kit 289T1144 New Part Number QTY Name Existing Part Number Notes-201 -110 -109 -3 -2 ### Page 53 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 53 of 339 BOEING SERVICE BULLETIN 767-28A0083 3. ACCOMPLISHMENT INSTRUCTIONS A. GENERAL INFORMATION CAUTION: KEEP THE WORK AREA, WIRES AND ELECTRICAL BUNDLES CLEAN OF METAL PARTICLES OR CONTAMINATION WHEN YOU USE TOOLS. UNWANTED MATERIAL, METAL PARTICLES OR CONTAMINATION CAUGHT IN WIRE BUNDLES CAN CAUSE DAMAGE TO THE BUNDLES. DAMAGED WIRE BUNDLES CAN CAUSE SPARKS OR OTHER ELECTRICAL DAMAGE. NOTE: 1. Manual titles are referred to by acronyms. Refer to Paragraph 1.J., References, for definition of the acronyms. 2. Obey all of the warnings and cautions given in the specified manual sections. 3. Unless shown differently, these dimensions and tolerances are used: — Linear dimensions are in inches — Tolerance on linear dimensions, other than rivet and bolt edge margins, is plus or minus 0.03 inch. — Tolerance on rivet and bolt edge margin is plus or minus 0.05 inch — Angular tolerance is plus or minus 2 degrees — Hole dimensions for standard solid rivets are given in 767 Structural Repair Manual, Chapter 51 — Torque limits to tighten nuts and bolts are given in 767 Structural Repair Manual, Chapter 51. 4. For approved fastener and process material substitutions, refer to 767 Structural Repair Manual, Chapter 51, Alternate fasteners are given in 767 Structural Repair Manual Chapter 51 and Boeing Drawing 012W6100. 5. Refer to the Boeing Standard Wiring Practices Manuals, 767 AMM 20-10-11 and 767 AMM 20-10-12 for the wire installation procedures, and 767 AMM 20-10-19 for the wire separation requirements. 6. If the length of fasteners specified in this service bulletin do not meet the installation standards, fasteners of the same specification, or an approved substitute, one grip length longer or shorter may be used. 7. The work instructions are divided into 3 parts. Part 1 are airplanes in Groups 1-39, 82- 87, Part 2 are airplanes in Groups 40-79, 88 and Part 3 are airplanes in Groups 80-81, 89 because of the different wiring changes and testing requirements. Task-Hours and Elapsed-Hours for each group are given in Paragraph 1.G., Manpower. B. WORK INSTRUCTIONS PART 1 - GROUPS 1-39, 82-87 AIRPLANES 1. Group 1-39, 82-87: Remove electrical power from the airplane as specified in767 AMM 24-22-00. 2. Group 1-39, 82-87: Install new relay bracket in P36 panel as specified in Figure 1. ### Page 54 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 54 of 339 BOEING SERVICE BULLETIN 767-28A0083 3. Group 1-39, 82-87: Install new relay bracket in P37 panel as specified in Figure 2. 4. Group 1-39, 82-87: Make wiring changes (W/B 0146) in P33 panel as specified in Figure 3. 5. Group 1-2, 5, 82, 85: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 4. 6. Group 3-4, 83-84: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 5. 7. Group 6: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 6. 8. Group 7, 86: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 7. 9. Group 8, 87: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 8. 10. Group 11-16, 18, 21-22, 25-34, 9: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 9. 11. Group 10, 20: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 10. 12. Group 17: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 11. 13. Group 19: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 12. 14. Group 23-24: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 13. 15. Group 35: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 14. 16. Group 36: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 15. 17. Group 37: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 16. 18. Group 38: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 17. 19. Group 39: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 18. 20. Group 1-2, 5, 8, 82, 85, 87: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 19. 21. Group 3-4, 83-84: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 20. 22. Group 6: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 21. 23. Group 7, 86: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 22. 24. Group 9, 11-15, 18-19, 21-24, 26-31, 33-34: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 23. 25. Group 10, 20: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 24. 26. Group 16: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 25. 27. Group 17: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 26. ### Page 55 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 55 of 339 BOEING SERVICE BULLETIN 767-28A0083 28. Group 25, 32: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 27. 29. Group 35: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 28. 30. Group 36: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 29. 31. Group 37: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 30. 32. Group 38: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 31. 33. Group 39: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 32. 34. Group 1-39, 82-87: Install relays in P36 panel as specified in Figure 33. 35. Group 1: Make wiring changes (W/B 0188) in P37 panel as specified in Figure 34. 36. Group 2-5, 7-9, 16: Make wiring changes (W/B 0188) in P37 panel as specified in Figure 35. 37. Group 82-87: Make wiring changes (W/B 0188) in P37 panel as specified in Figure 158. 38. Group 6: Make wiring changes (W/B 0188) in P37 panel as specified in Figure 36. 39. Group 10-12, 14-15, 17-21, 23, 25-26, 28, 32-34, 36-37: Make wiring changes (W/B 0188) in P37 panel as specified in Figure 37. 40. Group 13, 22, 24, 27, 29-31, 38-39: Make wiring changes (W/B 0188) in P37 panel as specified in Figure 38. 41. Group 35: Make wiring changes (W/B 0188) in P37 panel as specified in Figure 39. 42. Group 1: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 40. 43. Group 2-3, 82-83: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 41. 44. Group 4, 84: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 42. 45. Group 5, 8-9, 16, 85, 87: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 43. 46. Group 6: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 44. 47. Group 7, 86: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 45. 48. Group 10: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 46. 49. Group 11-12, 14-15, 17, 19, 21, 23, 25-26, 28, 36: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 47. 50. Group 13, 22, 24, 27, 29-31: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 48. 51. Group 18, 20, 32-34: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 49. 52. Group 35: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 50. ### Page 56 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 56 of 339 BOEING SERVICE BULLETIN 767-28A0083 53. Group 37: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 51. 54. Group 38: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 52. 55. Group 39: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 53. 56. Group 1, 5-6, 8-9, 14, 16-17, 19, 25, 28, 36, 85, 87: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 54. 57. Group 2-3, 10, 82-83: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 55. 58. Group 4, 84: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 56. 59. Group 7, 86: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 57. 60. Group 11, 21: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 58. 61. Group 12, 15, 23, 26: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 59. 62. Group 13, 24, 27: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 60. 63. Group 18, 20, 32-34: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 61. 64. Group 22: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 62. 65. Group 29-30: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 63. 66. Group 31: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 64. 67. Group 35: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 65. 68. Group 37: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 66. 69. Group 38: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 68. 70. Group 1-39, 82-87: Install relays in P37 Panel as specified in Figure 67. 71. Group 1-6, 8-15, 17-24, 26-31, 33-35, 37-39, 82-85, 87: Make wiring changes (W/B 0264) P33 to P36 panel as specified in Figure 69. See Figure 81 for wire bundle routing information. 72. Group 7, 16, 86: Group 7, 16, 86: Make wiring changes (W/B 0264) P33 to P36 panel as specified in Figure 70. See Figure 81 for wire bundle routing information. 73. Group 25, 32: Make wiring changes (W/B 0264) P33 to P36 panel as specified in Figure 71. See Figure 81 for wire bundle routing information. 74. Group 36: Make wiring changes (W/B 0264) P33 to P36 panel as specified in Figure 72. See Figure 81 for wire bundle routing information. 75. Group 1-6, 8-10, 14, 16-20, 25, 28-30, 32-34, 36, 82-85, 87: Make wiring changes (W/B 0590) P36 to P37 panel as specified in Figure 73. See Figure 81 for wire bundle routing information. ### Page 57 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 57 of 339 BOEING SERVICE BULLETIN 767-28A0083 76. Group 31: Make wiring changes (W/B 0590) P36 to P37 panel as specified in Figure 74. See Figure 81 for wire bundle routing information. 77. Group 35: Make wiring changes (W/B 0590) P36 to P37 panel as specified in Figure 75. See Figure 81 for wire bundle routing information. 78. Group 7, 11, 21-22, 86: Make wiring changes (W/B 0590) P36 to P37 panel as specified in Figure 76. See Figure 81 for wire bundle routing information. 79. Group 12-13, 15, 23-24, 26-27, 38: Make wiring changes (W/B 0590) P36 to P37 panel as specified in Figure 77. See Figure 81 for wire bundle routing information. 80. Group 37, 39: Make wiring changes (W/B 0942) P36 to P37 panel as specified in Figure 78. See Figure 81 for wire bundle routing information. 81. Group 39: Make wiring changes (W/B 1118) in P37 panel as specified in Figure 79. 82. Group 37: Make wiring changes (W/B 1118) in P37 panel as specified in Figure 80. 83. Group 1-39, 82-87: Provide electrical power to the airplane as specified in 767 AMM 24-22-00. 84. Group 1-39, 82-87: Do the following Functional Tests: a. Do the "Override Pump Auto Shutoff Functional Test" as given in 767 AMM 28-22-00. b. For airplanes with Jettison System, Do the following Operational Tests: (1) Do the "Test of the Left Override/Jettison Pump" as given in 767 AMM 28-31-00. (2) Do the "Test of the Right Override/Jettison Pump" as given in 767 AMM 28-31-00. 85. Group 1-39, 82-87: Install covers on P36 and P37 Panels. 86. Group 1-39, 82-87: Put the airplane back to a serviceable condition. PART 2 - GROUPS 40-79, 88 AIRPLANES 1. Group 40-79, 88: Remove electrical power from the airplane as specified in 767 AMM 24-22-00. 2. Group 40-79, 88: Install new relay bracket in P36 panel as specified in Figure 82. 3. Group 40-79, 88: Install new relay bracket in P37 panel as specified in Figure 83. 4. Group 40: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 84. 5. Group 42, 67-68: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 85. 6. Group 76: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 86. 7. Group 55: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 87. 8. Group 49: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 88. ### Page 58 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 58 of 339 BOEING SERVICE BULLETIN 767-28A0083 9. Group 88: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 159. 10. Group 54, 79: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 89. 11. Group 66: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 90. 12. Group 44, 72, 74: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 91. 13. Group 62: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 92. 14. Group 41, 43, 64: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 93. 15. Group 69: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 94. 16. Group 61: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 95. 17. Group 70: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 96. 18. Group 73, 75: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 97. 19. Group 56: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 98. 20. Group 71: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 99. 21. Group 65: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 100. 22. Group 63: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 101. 23. Group 52-53, 78: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 102. 24. Group 46-48, 50-51, 58, 60, 77: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 103. 25. Group 45, 57, 59: Make wiring changes (W/B 0176) in P36 panel as specified in Figure 104. 26. Group 61: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 105. 27. Group 62-63: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 106. 28. Group 56: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 107. 29. Group 44, 72-75: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 108. 30. Group 65, 69: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 109. 31. Group 52-53, 78: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 110. 32. Group 40-41, 43, 45-48, 50-51, 57-60, 64, 66, 70-71, 77: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 111. ### Page 59 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 59 of 339 BOEING SERVICE BULLETIN 767-28A0083 33. Group 54-55, 79: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 112. 34. Group 42, 49, 67-68, 76, 88: Make the wiring changes (W/B 0184) in the P36 panel as specified in Figure 113. 35. Group 40-79, 88: Install relays in P36 panel as specified in Figure 114. 36. Group 55: Make wiring changes (W/B 0188) in P37 panel as specified in Figure 115. 37. Group 40-45, 57, 59, 64, 66, 68-70, 72, 74, 76: Make wiring changes (W/B 0188) in P37 panel as specified in Figure 116. 38. Group 46-53, 58, 60, 65, 67, 71, 73, 75, 77-79, 88: Make wiring changes (W/B 0188) in P37 panel as specified in Figure 117. 39. Group 54, 56: Make wiring changes (W/B 0188) in P37 panel as specified in Figure 118. 40. Group 61-62: Make wiring changes (W/B 0188) in P37 panel as specified in Figure 119. 41. Group 63: Make wiring changes (W/B 0188) in P37 panel as specified in Figure 120. 42. Group 61: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 121. 43. Group 62: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 122. 44. Group 41, 43-45, 57, 59, 64, 69-70, 72, 74: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 123. 45. Group 42, 67-68, 76: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 124. 46. Group 40, 66: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 125. 47. Group 55: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 126. 48. Group 56: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 127. 49. Group 54: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 128. 50. Group 49, 79, 88: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 129. 51. Group 48, 50-53, 78: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 130. 52. Group 46-47, 58, 60, 65, 71, 73, 75, 77: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 131. 53. Group 63: Make wiring changes (W/B 0192) in P37 panel as specified in Figure 132. 54. Group 61: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 133. 55. Group 62: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 134. 56. Group 63: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 135. ### Page 60 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 60 of 339 BOEING SERVICE BULLETIN 767-28A0083 57. Group 40-41, 43-45, 57, 64, 69-70, 72: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 136. 58. Group 59, 66, 74: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 137. 59. Group 46, 58, 65, 71, 73: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 138. 60. Group 47, 60, 75, 77: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 139. 61. Group 51: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 140. 62. Group 48, 50, 53, 78: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 141. 63. Group 52, 56: Make wiring changes (W/B 0198) in P37 panel as specified in Figure 142. 64. Group 40-79, 88: Install relays in P37 Panel as specified in Figure 143. 65. Group 47-48, 50, 53, 59-60, 66, 74-75, 77-78: Make wiring changes (W/B 0590) P36 to P37 panel as specified in Figure 144. See Figure 152 for wire bundle routing information. 66. Group 61-63: Make wiring changes (W/B 0590) P36 to P37 panel as specified in Figure 145. See Figure 152 for wire bundle routing information. 67. Group 40-41, 43-46, 51, 57-58, 64-65, 69-73: Make wiring changes (W/B 0590) P36 to P37 panel as specified in Figure 146. See Figure 152 for wire bundle routing information. 68. Group 52, 56: Make wiring changes (W/B 0590) P36 to P37 panel as specified in Figure 147. See Figure 152 for wire bundle routing information. 69. Group 42, 49, 54, 67-68, 76, 79: Make wiring changes (W/B 0942) P36 to P37 panel as specified in Figure 148. See Figure 152 for wire bundle routing information. 70. Group 55: Make wiring changes (W/B 0942) P36 to P37 panel as specified in Figure 149. See Figure 152 for wire bundle routing information. 71. Group 88: Make wiring changes (W/B 0942) P36 to P37 panel as specified in Figure 160. See Figure 152 for wire bundle routing information. 72. Group 49, 54, 79, 88: Make wiring changes (W/B 1118) in P37 panel as specified in Figure 150. 73. Group 42, 67-68, 76: Make wiring changes (W/B 1118) in P37 panel as specified in Figure 151. 74. Group 40-79, 88: Provide electrical power to the airplane as specified in 767 AMM 24-22-00. 75. Group 40-79, 88: Do the following Functional Tests: a. Do the "Override Pump Auto Shutoff Functional Test" as given in 767 AMM 28-22-00. b. For airplanes with Jettison System, Do the following Operational Tests: (1) Do the "Test of the Left Override/Jettison Pump" as given in 767 AMM 28-31-00. The text continues at https://openairdocs.org/service-documents/boeing/767-28a0083/file/1a282b05feef.md?from=61 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.