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### 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## BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET Copyright © 2006 The Boeing Company Unpublished Work - All Rights Reserved Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable subject matter.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.

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### BOEING SERVICE BULLETIN 767-28A0083

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### 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

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### 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

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### 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.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 84 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

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### 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

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### 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

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### BOEING SERVICE BULLETIN 767-28A0083

BLANK PAGE

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### 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)

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### 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

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### 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.

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### 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

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### 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 FWD497138

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### BOEING SERVICE BULLETIN 767-28A0083

BLANK PAGE

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### 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.

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### 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**

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### 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**

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### 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**

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### 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**

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### 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**

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### 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 3 VA508 7 VB105–VB123 VB125 82 VA301 VA303–VA306 VA309–VA310 85 VA803 VA807–VA809 86 VB101–VB104 9 VB302 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**

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### 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

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### 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

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### 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) 1 VA001 BRAVO AIRLINES (BVA) 18 VE104 BRISTOL AIR LIMITED (BMD) 85 VA804

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### 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) 3 VA510 VA513 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) 3 VA507 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

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### 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) 1 VA008 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

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### 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) 1 VA019 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

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### 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

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### BOEING SERVICE BULLETIN 767-28A0083 PHOENIX AIRCRAFT LEASING, INC. (PLB) 5 VA810 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

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### 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

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### 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

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### 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

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### 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**

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### 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**

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### 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**

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### 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**

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### 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**

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### 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 5 85 VB101-VB104 7 86 VB281 8 87

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### 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)

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### 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.

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### 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 2 0.75 0.38 Figure 2, P37 Bracket Installation 2 0.75 0.38

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### BOEING SERVICE BULLETIN 767-28A0083

Figure 3, P33 Panel Wiring change. 2 0.50 0.25 Figures 4-32, P36 Panel wiring change. 2 8.9 4.45 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**

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Figure 114, P36 Panel, Relay Installation. 2 0.75 0.38 Figures 115-142, 150-151, P37 Panel, Wiring Changes. 2 8.70 4.35 Figure 143, P37 Panel Relay installation. 2 0.75 0.38 Figures 144-149, 160, P36 to P37 Panel Wiring Changes. 2 4.00 2.00 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 1 1.10 1.10 Figure 154, P36 Panel Relay installation. 1 0.15 0.15 Figures 155, 156, 161, P37 Panel Wiring changes. 1 1.10 1.10 Figure 157, P37 Panel Relay installation. 1 0.15 0.15 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**

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### 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

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### 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.

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BLANK PAGE

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### 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

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### 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**  289T1144-2 . . . . . -- Wire Kit -- (a) 289T1144-3 . . . . -- . Wire Kit -- (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 -- --

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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 -- -- 289T1144-103W . 1 . . . . Wire -- -- 289T1144-10301 . 1 . . . . Lacing Tape -- -- 289T1144-10302 . 1 . . . . Identification Tape -- -- 289T1144-10303 . 1 . . . . Identification Tape -- -- 289T1144-10304 . 1 . . . . Identification Tape -- -- 289T1144-10305 . 1 . . . . Identification Tape -- -- 289T1144-10306 . 1 . . . . Identification Tape -- -- 289T1144-10307 . 1 . . . . Identification Tape -- -- 289T1144-104W 1 . . . . . Wire -- -- 289T1144-10401 1 . . . . . Lacing Tape -- -- 289T1144-10402 1 . . . . . Identification Tape -- -- 289T1144-10403 1 . . . . . Identification Tape -- -- 289T1144-10404 1 . . . . . Identification Tape -- -- 289T1144-10405 1 . . . . . Identification Tape -- -- 289T1144-10406 1 . . . . . Identification Tape -- -- 289T1144-10407 1 . . . . . Identification Tape -- -- BACC47CN1S 2 1 4 1 . . Contact -- -- M39029/11-145 4 3 11 1 . . Contact -- -- BACS16AG1 . . 1 . . . Relay Socket -- -- 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** 

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BACC47DJ1 . . 2 . . . Contact -- -- BACC47ER1 . 1 8 . . . Contact -- -- BACC47CP1S 2 1 . . . . Contact -- -- BACC47CN2 . 2 . . . . Contact -- -- BACC47FJ2A . 1 . . . . Contact (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**  289T1144-2 . . . . . -- Wire Kit -- (a) 289T1144-3 . . . . -- . Wire Kit -- (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 -- -- 289T1144-107W . 1 . . . . Wire -- -- 289T1144-10702 . 1 . . . . Lacing Tape -- -- 289T1144-10703 . 1 . . . . Identification Tape -- -- 289T1144-10704 . 1 . . . . Identification Tape -- -- 289T1144-108W 1 . . . . . Wire -- -- 289T1144-10802 1 . . . . . Lacing Tape -- -- 289T1144-10803 1 . . . . . Identification Tape -- -- 289T1144-10804 1 . . . . . Identification Tape -- -- BACC47CN1S 1 . . . . . Contact -- -- **Kit 289T1144 New Part**  **Number QTY**  **Name Existing Part**  **Number Notes -104 -103 -102 -101 -3 -2** 

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M39029/11-145 . . 2 12 . . Contact -- (a) BACS16AG1 . . . 1 . . Relay Socket -- -- BACS16AH1 . . . 1 . . Relay Socket -- -- BACT12AR222 . . . 2 . . Terminal Lug -- -- BACC47FJ2A . . . . . . Contact -- -- BACC47FJ1A . . . 2 . . Contact -- -- BACC47FK1A . . . 1 . . Contact -- -- BACC47DJ1 . . . 2 . . Contact -- -- BACC47ER1 . . . 8 . . Contact -- -- BACC47CP1S 1 2 2 3 . . Contact -- -- Y-9015-C 1 . 1 . . . Eyelet -- -- BACC47CP3T . . 1 . . . Contact -- -- BACC47CN3 1 . . . . . Contact -- -- (a) There are more parts than are necessary. **Kit 289T1144 New Part**  **Number QTY**  **Name Existing Part**  **Number Notes -201 -110 -109 -3 -2**  289T1144-2 . . . . -- Wire Kit -- (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 -- -- BACT12AR222 2 . . . . Terminal Lug -- -- **Kit 289T1144 New Part**  **Number QTY**  **Name Existing Part**  **Number Notes -108 -107 -106 -105 -3 -2** 

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### 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. BACC47FJ2A 2 . . . . Contact -- -- BACC47FJ1A 2 1 1 . . Contact -- -- BACC47FK1A 2 . 1 . . Contact -- -- BACC47DJ1 2 . . . . Contact -- -- BACC47ER1 2 . . . Contact -- -- BACC47CP1S 2 . 2 . . Contact -- -- BACC47CN2 2 . . . . Contact -- -- Y-9015-C 1 . . . . Eyelet -- -- BACM15C3C 2 . . . . Burndy Block -- (b) BACM15C3B 2 . . . . Burndy Block -- (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** 

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### 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.

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### 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.

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### 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.

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### 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.

### 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.

### 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.

### 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.

### 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.

### May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 61 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 (2) Do the "Test of the Right Override/Jettison Pump" as given in 767 AMM 28-31-00. 76. Group 40-79, 88: Install covers on P36 and P37 panels. 77. Group 40-79, 88: Put the airplane back to a serviceable condition. **PART 3 - GROUPS 80-81, 89 AIRPLANES** 1. Group 80-81, 89: Remove electrical power from the airplane as specified in 767 AMM 24-22-00. 2. Group 80-81, 89: Gain the access to the P36 and P37 panels. 3. Group 80-81, 89: Make wiring changes to (W/B 0176) and (W/B0184) in P36 panel as specified in Figure 153. 4. Group 80-81, 89: Install relays in P36 panel as specified in Figure 154. 5. Group 80: Make wiring changes to (W/B 0192) and (W/B1118) in P37 panel as specified in Figure 155. 6. Group 81: Make wiring changes to (W/B 0192) and (W/B0188) in P37 panel as specified in Figure 156. 7. Group 89: Make wiring changes to (W/B 0192) and (W/B0198) in P37 panel as specified in Figure 161. 8. Group 80-81, 89: Install relays in P37 panel as specified in Figure 157. 9. Group 80-81, 89: Provide electrical power to the airplane as specified in 767 AMM 24-22-00. 10. Group 80-81, 89: Do the following Functional Tests: a. Do the "Override Pump Auto Shutoff Functional Test" as given in 767 AMM 28-22-00. b. Do the "Test of the Left Override/Jettison Pump" as given in 767 AMM 28-31-00. c. Do the "Test of the Right Override/Jettison Pump" as given in 767 AMM 28-31-00. 11. Group 80-81, 89: Close access to the P36 and P37 panel. 12. Group 80-81, 89: Put the airplane back to a serviceable condition.

### FIGURE 1: P36 Panel - Bracket Installation, Groups 1-39 and 82-87 Airplanes May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 62 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 1: P36 Panel - Bracket Installation, Groups 1-39 and 82-87 Airplanes**

P36 PANEL


### MAIN EQUIPMENT CENTER A A C

C

FWD FWD

1 4 SEE C-C FOR ALTERNATE CONFIGURATIOND59766



### (SHEET 1 OF 4)

### FIGURE 1: P36 Panel - Bracket Installation, Groups 1-39 and 82-87 Airplanes May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 63 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

A-A

B-B SUPPORT BRACKET STANCHION

1.25 ± 0.14 1.70 0.30

STANCHION
SUPPORT BRACKET B B FWD INBD 3

2 FWD UPD59769



### (SHEET 2 OF 4)

### FIGURE 1: P36 Panel - Bracket Installation, Groups 1-39 and 82-87 Airplanes May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 64 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 1-39, 82-87: 

### C-C

D-D STANCHION

1.25 ± 0.14 1.70 0.80

STANCHION ALTERNATE CONFIGURATION

ALTERNATE CONFIGURATION D D FWD INBD 3

2 FWD UP1561718



### (SHEET 3 OF 4)

### FIGURE 1: P36 Panel - Bracket Installation, Groups 1-39 and 82-87 Airplanes May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 65 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY numbers shown below are the number of parts necessary for bracket installation on the P36 panel. Use parts from Top Kit 015T1775-2 (Groups 1-39 and 82-87 airplanes). **STEP TASK NAME IDENTIFICATION QTY MORE DATA** 1 Remove (Keep) Cover P36 Panel 1 -- 2 Install (New) Bracket 284T0378-234 1 Position bracket with decal text K10691 and K10693 facing inboard. 3 Install (New) Screw BACS12GU3K7 2 Drill .218 - .2290 diameter Holes. Washer NAS1149D0332H 2 -- 4 Install (Kept) Cover P36 Panel 1 Do not install Cover if wiring installation will be completed next.

**(SHEET 4 OF 4)**

### FIGURE 2: P37 Panel - Bracket Installation, Groups 1-39 and 82-87 Airplanes May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 66 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 2: P37 Panel - Bracket Installation, Groups 1-39 and 82-87 Airplanes**



### MAIN EQUIPMENT CENTER A A P37 PANEL

FWD

1

FWD UP 4D59771



### (SHEET 1 OF 3)

### FIGURE 2: P37 Panel - Bracket Installation, Groups 1-39 and 82-87 Airplanes May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 67 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 1-39, 82-87: 

### A-A

B-B 1.25 ± 0.14 0.30

1.70 SUPPORT BRACKET STANCHION

SUPPORT BRACKET STANCHION B B FWD INBD

2 FWD UP 3D59774



### (SHEET 2 OF 3)

### FIGURE 2: P37 Panel - Bracket Installation, Groups 1-39 and 82-87 Airplanes May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 68 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY numbers shown below are the number of parts necessary for bracket installation on the P37 Panel. Use parts from Top Kit 015T1775-2 (Group 1-39 and 82-87 airplanes). **STEP TASK NAME IDENTIFICATION QTY MORE DATA** 1 Remove (Keep) Cover P37 Panel 1 -- 2 Install (New) Bracket 284T0378-233 1 Position bracket with decal text K10690 and K10692 facing inboard. 3 Install (New) Screw BACS12GU3K7 2 Drill .218 - .2290 diameter Holes. Washer NAS1149D0332H 2 -- 4 Install (Kept) Cover P37 Panel 1 Do not install Cover if wiring installation will be completed next.

**(SHEET 3 OF 3)**

### FIGURE 3: P33 Panel - Wiring changes W/B146, Group 1-39 and 82-87 Airplanes May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 69 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 3: P33 Panel - Wiring changes W/B146, Group 1-39 and 82-87 Airplanes**

This Figure applies to Group 1-39, 82-87: REFERENCE: 767 Wiring Diagrams 767 WDM 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from Wire Kit 289T1144-101. Route new wiring in the P33 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use color blue lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Pin BACC47CN1S 1 SWPM 20-61-11 2 Contact M39029/11-145 1 SWPM 20-90-11 3 Identification Tape 289T1144-10102 1 SWPM 20-10-11 4 Wire 289T1144-101W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10101 1 SWPM 20-10-11 3
REFERENCE 767 WIRE DIAGRAM 28-42-12 PANEL FOWARD MISCELLANEOUS ELECTRICAL W146- AE0203 TB186 YA11 P33 16A-22 W264 J 23 D4042P 2 1

4 5D59786 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 4: P36 Panel - Wiring changes W/B0176, Groups 1-2, 5, 82, 85 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 70 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 4: P36 Panel - Wiring changes W/B0176, Groups 1-2, 5, 82, 85 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 AE0223 J 4 D5658P TB216

YA10

YC10 TB216 4

W184 2

4

6
K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218

YC18

7 TB218

J D4672P 18 85W-24 02H-22 XB12 W184

K329 OVRD PUMP CONT RLY L FUEL X1 75W-22 02H-22 YA13 TB218 02F-24

2

2 5 3 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24 6

5

3 10 9

8 7 (9 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS)

AE0209 11 12D59791



### (SHEET 1 OF 2)

### FIGURE 4: P36 Panel - Wiring changes W/B0176, Groups 1-2, 5, 82, 85 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 71 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 1-2, 5, 82, 85: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 767 WDM 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Terminal Lug BACT12AR222 1 SWPM 20-30-11 4 Relay Socket BACS16AH1 1 SWPM 20-81-22 5 Relay Socket BACS16AG1 1 SWPM 20-81-22 6 Pin BACC47CN1S 2 SWPM 20-61-11 7 Identification Tape 289T1144-10202 1 SWPM 20-10-11 8 Identification Tape 289T1144-10203 1 SWPM 20-10-11 9 Identification Tape 289T1144-10209 1 SWPM 20-10-11 10 Identification Tape 289T1144-10210 1 SWPM 20-10-11 11 Wire 289T1144-102W 1 SWPM 20-10-11 12 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 5: P36 Panel - Wiring changes W/B0176, Groups 3-4, 83-84 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 72 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 5: P36 Panel - Wiring changes W/B0176, Groups 3-4, 83-84 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184 2

4

6
K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218

YC9

7 TB218

J D4672P 18 85W-24 02H-22 XB12 W184

K329 OVRD PUMP CONT RLY L FUEL X1 75W-22 02H-22 YA14 TB218 02F-24

2

2 5 3 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24 6

5

3 10 9

8 7 (9 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 11 12D59801



### (SHEET 1 OF 2)

### FIGURE 5: P36 Panel - Wiring changes W/B0176, Groups 3-4, 83-84 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 73 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 3-4, 83-84: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 767 WDM 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Terminal Lug BACT12AR222 1 SWPM 20-30-11 4 Relay Socket BACS16AH1 1 SWPM 20-81-22 5 Relay Socket BACS16AG1 1 SWPM 20-81-22 6 Pin BACC47CN1S 2 SWPM 20-61-11 7 Identification Tape 289T1144-10202 1 SWPM 20-10-11 8 Identification Tape 289T1144-10203 1 SWPM 20-10-11 9 Identification Tape 289T1144-10209 1 SWPM 20-10-11 10 Identification Tape 289T1144-10210 1 SWPM 20-10-11 11 Wire 289T1144-102W 1 SWPM 20-10-11 12 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 6: P36 Panel - Wiring Changes W/B0176, Group 6 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 74 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 6: P36 Panel - Wiring Changes W/B0176, Group 6 Airplanes.** 

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184 2

4

6
K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218

YC18

7 TB218

J D4672P 18 85W-24 02H-22 XC12 W184

K329 OVRD PUMP CONT RLY L FUEL X1 75W-22 02H-22 YA13 TB218 02F-24

2

2 5 3 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24 1 6

5

3 10 9

8 7 1 (9 LOCATIONS) (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 12 11D59811



### (SHEET 1 OF 2)

### FIGURE 6: P36 Panel - Wiring Changes W/B0176, Group 6 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 75 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 6: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 767 WDM 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer toSWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Terminal Lug BACT12AR222 1 SWPM 20-30-11 4 Relay Socket BACS16AH1 1 SWPM 20-81-22 5 Relay Socket BACS16AG1 1 SWPM 20-81-22 6 Pin BACC47CN1S 2 SWPM 20-61-11 7 Identification Tape 289T1144-10202 1 SWPM 20-10-11 8 Identification Tape 289T1144-10203 1 SWPM 20-10-11 9 Identification Tape 289T1144-10209 1 SWPM 20-10-11 10 Identification Tape 289T1144-10210 1 SWPM 20-10-11 11 Wire 289T1144-102W 1 SWPM 20-10-11 12 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 7: P36 Panel - Wiring Changes W/B0176, Group 7, 86 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 76 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 7: P36 Panel - Wiring Changes W/B0176, Group 7, 86 Airplanes.**

YC6

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184 2

4

6
K10691 L/H HOLD RELAY D11629 TB222 Z17 TB218 7 TB218

J D4672P 18 85W-24 02H-22 XB12 W184

K329 OVRD PUMP CONT RLY L FUEL X1 75W-22 02H-22 YA14 TB218 02F-24

2

2 5 3 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24 6

5

3 10 9

8 7 (9 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 12 11D59816



### (SHEET 1 OF 2)

### FIGURE 7: P36 Panel - Wiring Changes W/B0176, Group 7, 86 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 77 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 7, 86: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 767 WDM 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Terminal Lug BACT12AR222 1 SWPM 20-30-11 4 Relay Socket BACS16AH1 1 SWPM 20-81-22 5 Relay Socket BACS16AG1 1 SWPM 20-81-22 6 Pin BACC47CN1S 2 SWPM 20-61-11 7 Identification Tape 289T1144-10202 1 SWPM 20-10-11 8 Identification Tape 289T1144-10203 1 SWPM 20-10-11 9 Identification Tape 289T1144-10209 1 SWPM 20-10-11 10 Identification Tape 289T1144-10210 1 SWPM 20-10-11 11 Wire 289T1144-102W 1 SWPM 20-10-11 12 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 8: P36 Panel - Wiring Changes W/B0176, Group 8, 87 Airplanes May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 78 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 8: P36 Panel - Wiring Changes W/B0176, Group 8, 87 Airplanes**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184 2

4

6
K10691 L/H HOLD RELAY D11629 TB222 Z17 TB218

YC18

7 TB218

J D4672P 18 85W-24 02H-22 XB12 W184

K329 OVRD PUMP CONT RLY L FUEL X1 75W-22 02H-22 YA13 TB218 02F-24

2

2 5 3 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24 6

5

3 10 9

8 7 (9 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 12 11D59827



### (SHEET 1 OF 2)

### FIGURE 8: P36 Panel - Wiring Changes W/B0176, Group 8, 87 Airplanes May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 79 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 8, 87: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Terminal Lug BACT12AR222 1 SWPM 20-30-11 4 Relay Socket BACS16AH1 1 SWPM 20-81-22 5 Relay Socket BACS16AG1 1 SWPM 20-81-22 6 Pin BACC47CN1S 2 SWPM 20-61-11 7 Identification Tape 289T1144-10202 1 SWPM 20-10-11 8 Identification Tape 289T1144-10203 1 SWPM 20-10-11 9 Identification Tape 289T1144-10209 1 SWPM 20-10-11 10 Identification Tape 289T1144-10210 1 SWPM 20-10-11 11 Wire 289T1144-102W 1 SWPM 20-10-11 12 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 9: P36 Panel - Wiring Changes W/B0176, Groups 9, 11-16,18, 21-22, 25-34 airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 80 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 9: P36 Panel - Wiring Changes W/B0176 , Groups 9, 11-16,18, 21-22, 25-34 airplanes.** 

This Figure applies to Group 11-16, 18, 21-22, 25-34, 9: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184 2

4

6
K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218

YC5

7 TB218

J D4672P 18 85W-24 02H-22 XB12 W184

K329 OVRD PUMP CONT RLY L FUEL X1 75W-22 02H-22 YA5 TB218 02F-24

2

2 5 3 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24 6

5 3 10 9

8 7 (9 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS)

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 AE0223

AE0209 11 12

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD59848



### (SHEET 1 OF 2)

### FIGURE 9: P36 Panel - Wiring Changes W/B0176, Groups 9, 11-16,18, 21-22, 25-34 airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 81 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Terminal Lug BACT12AR222 1 SWPM 20-30-11 4 Relay Socket BACS16AH1 1 SWPM 20-81-22 5 Relay Socket BACS16AG1 1 SWPM 20-81-22 6 Pin BACC47CN1S 2 SWPM 20-61-11 7 Identification Tape 289T1144-10202 1 SWPM 20-10-11 8 Identification Tape 289T1144-10203 1 SWPM 20-10-11 9 Identification Tape 289T1144-10209 1 SWPM 20-10-11 10 Identification Tape 289T1144-10210 1 SWPM 20-10-11 11 Wire 289T1144-102W 1 SWPM 20-10-11 12 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.

**(SHEET 2 OF 2)**

### FIGURE 10: P36 Panel - Wiring Changes W/B0176, Groups 10, 20 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 82 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 10: P36 Panel - Wiring Changes W/B0176, Groups 10, 20 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184 2

4

6
K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218

YC5

7 TB218

J D4672P 18 85W-24 02H-22 XC12 W184

K329 OVRD PUMP CONT RLY L FUEL X1 75W-22 02H-22 YA5 TB218 02F-24

2

2 5 3 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24 6

5

3 10 9

8 7 (9 LOCATIONS) 11 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 12D59856



### (SHEET 1 OF 2)

### FIGURE 10: P36 Panel - Wiring Changes W/B0176, Groups 10, 20 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 83 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 10, 20: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Terminal Lug BACT12AR222 1 SWPM 20-30-11 4 Relay Socket BACS16AH1 1 SWPM 20-81-22 5 Relay Socket BACS16AG1 1 SWPM 20-81-22 6 Pin BACC47CN1S 2 SWPM 20-61-11 7 Identification Tape 289T1144-10202 1 SWPM 20-10-11 8 Identification Tape 289T1144-10203 1 SWPM 20-10-11 9 Identification Tape 289T1144-10209 1 SWPM 20-10-11 10 Identification Tape 289T1144-10210 1 SWPM 20-10-11 11 Wire 289T1144-102W 1 SWPM 20-10-11 12 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 11: P36 Panel - Wiring Changes W/B0176, Group 17 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 84 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 11: P36 Panel - Wiring Changes W/B0176, Group 17 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184 2

4

6
K10691 L/H HOLD RELAY D11629 TB216 Z19 TB218

YA9

7 TB218

J D4672P 18 85W-24 02H-22 XB12 W184

K329 OVRD PUMP CONT RLY L FUEL X1 75W-22 02H-22 YA7 TB218 02F-24

2

2 5 3 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24 6

5

3 10 9

8 7 (9 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 12 11D59858



### (SHEET 1 OF 2)

### FIGURE 11: P36 Panel - Wiring Changes W/B0176, Group 17 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 85 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 17: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Terminal Lug BACT12AR222 1 SWPM 20-30-11 4 Relay Socket BACS16AH1 1 SWPM 20-81-22 5 Relay Socket BACS16AG1 1 SWPM 20-81-22 6 Pin BACC47CN1S 2 SWPM 20-61-11 7 Identification Tape 289T1144-10202 1 SWPM 20-10-11 8 Identification Tape 289T1144-10203 1 SWPM 20-10-11 9 Identification Tape 289T1144-10209 1 SWPM 20-10-11 10 Identification Tape 289T1144-10210 1 SWPM 20-10-11 11 Wire 289T1144-102W 1 SWPM 20-10-11 12 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 12: P36 Panel - Wiring Changes W/B0176, Group 19 airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 86 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 12: P36 Panel - Wiring Changes W/B0176, Group 19 airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184 2

4

6
K10691 L/H HOLD RELAY D11629 TB216 Z19 TB218

YC5

7 TB218

J D4672P 18 85W-24 02H-22 XB12 W184

K329 OVRD PUMP CONT RLY L FUEL X1 75W-22 02H-22 YA5 TB218 02F-24

2

2 5 3 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24 6

5

3 10 9

8 7 (9 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 12 11D59861



### (SHEET 1 OF 2)

### FIGURE 12: P36 Panel - Wiring Changes W/B0176, Group 19 airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 87 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 19: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Terminal Lug BACT12AR222 1 SWPM 20-30-11 4 Relay Socket BACS16AH1 1 SWPM 20-81-22 5 Relay Socket BACS16AG1 1 SWPM 20-81-22 6 Pin BACC47CN1S 2 SWPM 20-61-11 7 Identification Tape 289T1144-10202 1 SWPM 20-10-11 8 Identification Tape 289T1144-10203 1 SWPM 20-10-11 9 Identification Tape 289T1144-10209 1 SWPM 20-10-11 10 Identification Tape 289T1144-10210 1 SWPM 20-10-11 11 Wire 289T1144-102W 1 SWPM 20-10-11 12 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 13: P36 Panel - Wiring Changes W/B0176, Groups 23-24 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 88 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 13: P36 Panel - Wiring Changes W/B0176, Groups 23-24 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184 2

4

6
K10691 L/H HOLD RELAY D11629 TB318 Z9 TB218

YC5

7 TB218

J D4672P 18 85W-24 02H-22 XB12 W184

K329 OVRD PUMP CONT RLY L FUEL X1 75W-22 02H-22 YA5 TB218 02F-24

2

2 5 3 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24 6

5

3 10 9

8 7 (9 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 12 11D59866



### (SHEET 1 OF 2)

### FIGURE 13: P36 Panel - Wiring Changes W/B0176, Groups 23-24 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 89 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 23-24: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Terminal Lug BACT12AR222 1 SWPM 20-30-11 4 Relay Socket BACS16AH1 1 SWPM 20-81-22 5 Relay Socket BACS16AG1 1 SWPM 20-81-22 6 Pin BACC47CN1S 2 SWPM 20-61-11 7 Identification Tape 289T1144-10202 1 SWPM 20-10-11 8 Identification Tape 289T1144-10203 1 SWPM 20-10-11 9 Identification Tape 289T1144-10209 1 SWPM 20-10-11 10 Identification Tape 289T1144-10210 1 SWPM 20-10-11 11 Wire 289T1144-102W 1 SWPM 20-10-11 12 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 14: P36 Panel - Wiring Changes W/B0176, Group 35 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 90 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 14: P36 Panel - Wiring Changes W/B0176, Group 35 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184 2

4

6
K10691 L/H HOLD RELAY D11629 TB318 Z9 TB218

YC14

7 TB218

J D4672P 18 85W-24 02H-22 XB12 W184

K329 OVRD PUMP CONT RLY L FUEL X1 75W-22 02H-22 YA14 TB218 02F-24

2

2 5 3 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24 6

5

3 10 9

8 7 (9 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 12 11D59878



### (SHEET 1 OF 2)

### FIGURE 14: P36 Panel - Wiring Changes W/B0176, Group 35 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 91 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 35: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wireSWPM 20-10-11 kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Terminal Lug BACT12AR222 1 SWPM 20-30-11 4 Relay Socket BACS16AH1 1 SWPM 20-81-22 5 Relay Socket BACS16AG1 1 SWPM 20-81-22 6 Pin BACC47CN1S 2 SWPM 20-61-11 7 Identification Tape 289T1144-10202 1 SWPM 20-10-11 8 Identification Tape 289T1144-10203 1 SWPM 20-10-11 9 Identification Tape 289T1144-10209 1 SWPM 20-10-11 10 Identification Tape 289T1144-10210 1 SWPM 20-10-11 11 Wire 289T1144-102W 1 SWPM 20-10-11 12 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 15: P36 Panel - Wiring Changes W/B0176, Group 36 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 92 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 15: P36 Panel - Wiring Changes W/B0176, Group 36 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184 2

4

6
K10691 L/H HOLD RELAY D11629 TB318 Z9 TB218

YA9

7 TB218

J D4672P 18 85W-24 02H-22 XB12 W184

K329 OVRD PUMP CONT RLY L FUEL X1 75W-22 02H-22 YA7 TB218 02F-24

2

2 5 3 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24 6

5

3 10 9

8 7 (9 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) 11 12 AE0223

AE0209D59882



### (SHEET 1 OF 2)

### FIGURE 15: P36 Panel - Wiring Changes W/B0176, Group 36 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 93 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 36: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Terminal Lug BACT12AR222 1 SWPM 20-30-11 4 Relay Socket BACS16AH1 1 SWPM 20-81-22 5 Relay Socket BACS16AG1 1 SWPM 20-81-22 6 Pin BACC47CN1S 2 SWPM 20-61-11 7 Identification Tape 289T1144-10202 1 SWPM 20-10-11 8 Identification Tape 289T1144-10203 1 SWPM 20-10-11 9 Identification Tape 289T1144-10209 1 SWPM 20-10-11 10 Identification Tape 289T1144-10210 1 SWPM 20-10-11 11 Wire 289T1144-102W 1 SWPM 20-10-11 12 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 16: P36 Panel - Wiring Changes W/B0176, Group 37 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 94 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 16: P36 Panel - Wiring Changes W/B0176, Group 37 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 YC10 TB216 4

W184

4

6
K10691 L/H HOLD RELAY D11629 TB216 Z19 TB218

YC5

7 J D4672P 18 85W-24 02H-22

K329 OVRD PUMP CONT RLY L FUEL X1 75W-22 02H-22 YA5 TB218 2

2 5 3 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

5

3 10 8 7 02F-24

5 J

D4906P 4

J D5658P W0942 TB216

YA10 6 02F-24

6 11 9 2 (8 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 13 12D59888



### (SHEET 1 OF 2)

### FIGURE 16: P36 Panel - Wiring Changes W/B0176, Group 37 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 95 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 37: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 8 SWPM 20-90-11 See note (a) 3 Terminal Lug BACT12AR222 1 SWPM 20-30-11 4 Relay Socket BACS16AH1 1 SWPM 20-81-22 5 Relay Socket BACS16AG1 1 SWPM 20-81-22 6 Pin BACC47CN1S 3 SWPM 20-61-11 7 Identification Tape 289T1144-10202 1 SWPM 20-10-11 8 Identification Tape 289T1144-10203 1 SWPM 20-10-11 9 Identification Tape 289T1144-10209 1 SWPM 20-10-11 10 Identification Tape 289T1144-10210 1 SWPM 20-10-11 11 Identification Tape 289T1144-10211 1 SWPM 20-10-11 12 Wire 289T1144-102W 1 SWPM 20-10-11 13 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 17: P36 Panel - Wiring Changes W/B0176, Group 38 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 96 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 17: P36 Panel - Wiring Changes W/B0176, Group 38 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184 2

4

6
K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218

YA20

7 TB218

J D4672P 18 85W-24 02H-22 XB12 W184

K329 OVRD PUMP CONT RLY L FUEL X1 75W-22 02H-22 YC20 TB218 02F-24

2

2 5 3 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24 6

5

3 10 9

8 7 (9 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 11 12D59900



### (SHEET 1 OF 2)

### FIGURE 17: P36 Panel - Wiring Changes W/B0176, Group 38 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 97 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 38: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Terminal Lug BACT12AR222 1 SWPM 20-30-11 4 Relay Socket BACS16AH1 1 SWPM 20-81-22 5 Relay Socket BACS16AG1 1 SWPM 20-81-22 6 Pin BACC47CN1S 2 SWPM 20-61-11 7 Identification Tape 289T1144-10202 1 SWPM 20-10-11 8 Identification Tape 289T1144-10203 1 SWPM 20-10-11 9 Identification Tape 289T1144-10209 1 SWPM 20-10-11 10 Identification Tape 289T1144-10210 1 SWPM 20-10-11 11 Wire 289T1144-102W 1 SWPM 20-10-11 12 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 18: P36 Panel - Wiring Changes W/B0176, Group 39 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 98 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 18: P36 Panel - Wiring Changes W/B0176, Group 39 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 YC10 TB216 4

W184 2

4

6
K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218

YA20

7 J D4672P 18 85W-24 02H-22

K329 OVRD PUMP CONT RLY L FUEL X1 75W-22 02H-22 YC20 TB218 2

2 5 3 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

5

3 10 8 7 (8 LOCATIONS) 02F-24

5 J

D4906P 4

J D5658P W0942 TB216

YA10 6 02F-24

6 11 9 1

1 (4 LOCATIONS)

(4 LOCATIONS) 12 13 AE0223

AE0209D59907



### (SHEET 1 OF 2)

### FIGURE 18: P36 Panel - Wiring Changes W/B0176, Group 39 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 99 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 39: This Figure applies to Group 39 REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 8 SWPM 20-90-11 See note (a) 3 Terminal Lug BACT12AR222 1 SWPM 20-30-11 4 Relay Socket BACS16AH1 1 SWPM 20-81-22 5 Relay Socket BACS16AG1 1 SWPM 20-81-22 6 Pin BACC47CN1S 3 SWPM 20-61-11 7 Identification Tape 289T1144-10202 1 SWPM 20-10-11 8 Identification Tape 289T1144-10203 1 SWPM 20-10-11 9 Identification Tape 289T1144-10209 1 SWPM 20-10-11 10 Identification Tape 289T1144-10210 1 SWPM 20-10-11 11 Identification Tape 289T1144-10211 1 SWPM 20-10-11 12 Wire 289T1144-102W 1 SWPM 20-10-11 13 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 19: P36 Panel - Wiring Changes W/B0184, Groups 1-2, 5, 8, 82, 85, 87 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 100 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 19: P36 Panel - Wiring Changes W/B0184, Groups 1-2, 5, 8, 82, 85, 87 Airplanes.**

This Figure applies to Group 1-2, 5, 8, 82, 85, 87:

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YC18 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P
W176 TB218 YA13 J 41 D8026P W264 16A-22 1

6 2

2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XB12 02K-24 13 W590 2 5

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12

11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD59910



### (SHEET 1 OF 2)

### FIGURE 19: P36 Panel - Wiring Changes W/B0184, Groups 1-2, 5, 8, 82, 85, 87 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 101 of 339 

### BOEING SERVICE BULLETIN 767-28A0083
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.

**(SHEET 2 OF 2)**

### FIGURE 20: P36 Panel - Wiring Changes W/B0184, Groups 3-4, 83-84 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 102 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 20: P36 Panel - Wiring Changes W/B0184, Groups 3-4, 83-84 Airplanes.**

This Figure applies to Group 3-4, 83-84:

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YC9 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P
W176 TB218 YA14 J 41 D8026P W264 16A-22 1

6 2

2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XB12 02K-24 13 W590 2 5

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD59923



### (SHEET 1 OF 2)

### FIGURE 20: P36 Panel - Wiring Changes W/B0184, Groups 3-4, 83-84 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 103 of 339 

### BOEING SERVICE BULLETIN 767-28A0083
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.

**(SHEET 2 OF 2)**

### FIGURE 21: P36 Panel - Wiring Changes W/B0184, Group 6 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 104 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 21: P36 Panel - Wiring Changes W/B0184, Group 6 Airplanes.**

This Figure applies to Group 6:

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YC18 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P
W176 TB218 YA13 J 41 D8026P W264 16A-22 1

6 2

2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XC12 02K-24 13 W590 2 5

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12

11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD59927



### (SHEET 1 OF 2)

### FIGURE 21: P36 Panel - Wiring Changes W/B0184, Group 6 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 105 of 339 

### BOEING SERVICE BULLETIN 767-28A0083
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.

**(SHEET 2 OF 2)**

### FIGURE 22: P36 Panel - Wiring Changes W/B0184, Group 7, 86 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 106 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 22: P36 Panel - Wiring Changes W/B0184, Group 7, 86 Airplanes.**

This Figure applies to Group 7, 86:

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YC6 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P
W176 TB218 YA14 J 54 D8026P W264 16A-22 1

6 2

2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XB12 02K-24 13 W590 2 5

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12

11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD59951



### (SHEET 1 OF 2)

### FIGURE 22: P36 Panel - Wiring Changes W/B0184, Group 7, 86 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 107 of 339 

### BOEING SERVICE BULLETIN 767-28A0083
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.

**(SHEET 2 OF 2)**

### FIGURE 23: P36 Panel - Wiring Changes W/B0184, Groups 9, 11-15, 18-19, 21-24, 26-31, 33-34 air**planes** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 108 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 23: P36 Panel - Wiring Changes W/B0184, Groups 9, 11-15, 18-19, 21-24, 26-31, 33-34 airplanes**

This Figure applies to Group 9, 11-15, 18-19, 21-24, 26-31, 33-34: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YC5 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P
W176 TB218 YA5 J 41 D8026P W264 16A-22 1

6 2

2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XB12 02K-24 13 W590 2 5

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD59956



### (SHEET 1 OF 2)

### FIGURE 23: P36 Panel - Wiring Changes W/B0184, Groups 9, 11-15, 18-19, 21-24, 26-31, 33-34 air**planes** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 109 of 339 

### BOEING SERVICE BULLETIN 767-28A0083
5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 24: P36 Panel - Wiring Changes W/B0184, Groups 10, 20 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 110 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 24: P36 Panel - Wiring Changes W/B0184, Groups 10, 20 Airplanes.**

This Figure applies to Group 10, 20: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YC5 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P
W176 TB218 YA5 J 41 D8026P W264 16A-22 1

6 2

2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XC12 02K-24 13 W590 2 10 11 5

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD59977



### (SHEET 1 OF 2)

### FIGURE 24: P36 Panel - Wiring Changes W/B0184, Groups 10, 20 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 111 of 339 

### BOEING SERVICE BULLETIN 767-28A0083
5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 25: P36 Panel - Wiring Changes W/B0184, Group 16 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 112 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 25: P36 Panel - Wiring Changes W/B0184, Group 16 Airplanes.**

This Figure applies to Group 16: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YC5 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P
W176 TB218 YA5 J 54 D8026P W264 16A-22 1

6 2

2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XB12 02K-24 13 W590 2 5

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12

11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD59990



### (SHEET 1 OF 2)

### FIGURE 25: P36 Panel - Wiring Changes W/B0184, Group 16 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 113 of 339 

### BOEING SERVICE BULLETIN 767-28A0083
5 Contact BACC47CN1S 2 SWPM 20-61-11See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 26: P36 Panel - Wiring Changes W/B0184, Group 17 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 114 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 26: P36 Panel - Wiring Changes W/B0184, Group 17 Airplanes.**

This Figure applies to Group 17: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YA9 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P
W176 TB218 YA7 J 41 D8026P W264 16A-22 1

6 2

2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XB12 02K-24 13 W590 2 5

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD59994



### (SHEET 1 OF 2)

### FIGURE 26: P36 Panel - Wiring Changes W/B0184, Group 17 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 115 of 339 

### BOEING SERVICE BULLETIN 767-28A0083
5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 27: P36 Panel - Wiring Changes W/B0184, Groups 25, 32 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 116 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 FIGURE 27: P36 Panel - Wiring Changes W/B0184, Groups 25, 32 Airplanes.

This Figure applies to Group 25, 32: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YC5 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P
W176 TB218 YA5 J 40 D8026P W264 16A-22 1

6 2

2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XB12 02K-24 13 W590 2 5

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD59999



### (SHEET 1 OF 2)

### FIGURE 27: P36 Panel - Wiring Changes W/B0184, Groups 25, 32 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 117 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 28: P36 Panel - Wiring Changes W/B0184, Group 35 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 118 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 FIGURE 28: P36 Panel - Wiring Changes W/B0184, Group 35 Airplanes.

This Figure applies to Group 35: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YC14 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P
W176 TB218 YA14 J 41 D8026P W264 16A-22 1

6 2

2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XB12 02K-24 2 W590 2 5

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60001



### (SHEET 1 OF 2)

### FIGURE 28: P36 Panel - Wiring Changes W/B0184, Group 35 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 119 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 29: P36 Panel - Wiring Changes W/B0184, Group36 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 120 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 29: P36 Panel - Wiring Changes W/B0184, Group36 Airplanes.**

This Figure applies to Group 36: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YA9 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P
W176 TB218 YA7 J 34 D8026P W264 16A-22 1

6 2

2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XB12 02K-24 13 W590 2 5

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12

11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60004



### (SHEET 1 OF 2)

### FIGURE 29: P36 Panel - Wiring Changes W/B0184, Group36 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 121 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 30: P36 Panel - Wiring Changes W/B0184, Group 37 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 122 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 30: P36 Panel - Wiring Changes W/B0184, Group 37 Airplanes.**

This Figure applies to Group 37: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 2 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 AE0209
J 22 D4856P 

# W184
763-24 767-24 TB216

YA10 763-24

YC5 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P
W176 TB218 YA5 J 41 D8026P W264 16A-22 1

6 2

2 3 7

4 8

5 9
REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60013



### (SHEET 1 OF 2)

### FIGURE 30: P36 Panel - Wiring Changes W/B0184, Group 37 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 123 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

5 Contact BACC47CN1S 1 SWPM 20-61-11 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 31: P36 Panel - Wiring Changes W/B0184, Group 38 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 124 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 31: P36 Panel - Wiring Changes W/B0184, Group 38 Airplanes.**

This Figure applies to Group 38: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YA20 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P
W176 TB218 YC20 J 41 D8026P W264 16A-22 1

6 2

2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XB12 02K-24 13 W590 2 5

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60014



### (SHEET 1 OF 2)

### FIGURE 31: P36 Panel - Wiring Changes W/B0184, Group 38 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 125 of 339 

### BOEING SERVICE BULLETIN 767-28A0083
5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 32: P36 Panel - Wiring Changes W/B0184, Group 39 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 126 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 32: P36 Panel - Wiring Changes W/B0184, Group 39 Airplanes.**

This Figure applies to Group 39: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 2 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 AE0209
J 22 D4856P 

# W184
763-24 767-24 TB216

YA10 763-24

YA20 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P
W176 TB218 YC20 J 41 D8026P W264 16A-22 1

6 2

2 3 7

4 8

5 9
REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60022



### (SHEET 1 OF 2)

### FIGURE 32: P36 Panel - Wiring Changes W/B0184, Group 39 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 127 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

5 Contact BACC47CN1S 1 SWPM 20-61-11 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 33: P36 Panel - Relay Installation, Groups 1-39, 82-87 Airplanes May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 128 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 33: P36 Panel - Relay Installation, Groups 1-39, 82-87 Airplanes**

P36 PANEL


### MAIN EQUIPMENT CENTER

A
A

FWD FWDD60051



### (SHEET 1 OF 2)

### FIGURE 33: P36 Panel - Relay Installation, Groups 1-39, 82-87 Airplanes May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 129 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 1-39, 82-87: The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY numbers shown below are the number of parts necessary for each airplane. Use parts from Top Kit 015T1775- 2 (Group 1-39 and Group 82-87 airplanes). **STEP TASK NAME IDENTIFICATION QTY MORE DATA** 1 Install Relay BACR13CD2 1 -- 2 Install Relay TDH-1852-1402 1 --K10693K10691



### UP FWD 

### A-A 1 2D60052



### (SHEET 2 OF 2)

### FIGURE 34: P37 Panel - Wiring Changes W/B0188, Group 1 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 130 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 34: P37 Panel - Wiring Changes W/B0188, Group 1 Airplanes.**

This Figure applies to Group 1: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-104. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 2 Contact BACC47CN1S 2 SWPM 20-61-11 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Identification Tape 289T1144-10402 1 SWPM 20-10-11 5 Identification Tape 289T1144-10403 1 SWPM 20-10-11 6 Identification Tape 289T1144-10405 1 SWPM 20-10-11 P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL AE0218

W192 TB274
YC4 TB274 J 22 D5330P

J 3 D5506P

J 5 D5372P 

# W188 074-22

075-22

073-24 1 074-22

075-22

073-24

2

2

3 6 4

5 Z36

REFERENCE: 767 WIRE DIAGRAMS 28-42-12 7 8



### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60055



### (SHEET 1 OF 2)

### FIGURE 34: P37 Panel - Wiring Changes W/B0188, Group 1 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 131 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

7 Wire 289T1144-104W 1 SWPM 20-10-11 8 Lacing Tape 289T1144-10401 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 35: P37 Panel - Wiring Changes W/B0188, Groups 2-5, 7-9, 16, 82-87 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 132 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 35: P37 Panel - Wiring Changes W/B0188, Groups 2-5, 7-9, 16, 82-87 Airplanes.**

This Figure applies to Group 2-5, 7-9, 16: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-104. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 2 Contact BACC47CN1S 2 SWPM 20-61-11 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Identification Tape 289T1144-10402 1 SWPM 20-10-11 5 Identification Tape 289T1144-10403 1 SWPM 20-10-11 6 Identification Tape 289T1144-10405 1 SWPM 20-10-11 P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL AE0218

W192 TB304
W192 YC14 TB304 J 22 D5330P

J 3 D5506P

J 5 D5372P 

# W188 074-22

075-22

073-24 1 074-22

075-22

073-24

2

2

3 6 4

5 Z26

REFERENCE: 767 WIRE DIAGRAMS 28-42-12 7 8



### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60057



### (SHEET 1 OF 2)

### FIGURE 35: P37 Panel - Wiring Changes W/B0188, Groups 2-5, 7-9, 16, 82-87 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 133 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

7 Wire 289T1144-104W 1 SWPM 20-10-11 8 Lacing Tape 289T1144-10401 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 36: P37 Panel - Wiring Changes W/B0188, Group 6 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 134 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 36: P37 Panel - Wiring Changes W/B0188, Group 6 Airplanes.**

This Figure applies to Group 6: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-104. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 2 Contact BACC47CN1S 2 SWPM 20-61-11 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Identification Tape 289T1144-10402 1 SWPM 20-10-11 5 Identification Tape 289T1144-10403 1 SWPM 20-10-11 6 Identification Tape 289T1144-10405 1 SWPM 20-10-11 P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL AE0218

W192 TB212 J 22 D5330P

J 3 D5506P

J 5 D5372P 

# W188 074-22

075-22

073-24 1 074-22

075-22

073-24

2

2

3 6 4

5 Z20

REFERENCE: 767 WIRE DIAGRAMS 28-42-12 YC4 TB274 7 8



### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60061



### (SHEET 1 OF 2)

### FIGURE 36: P37 Panel - Wiring Changes W/B0188, Group 6 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 135 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

7 Wire 289T1144-104W 1 SWPM 20-10-11 8 Lacing Tape 289T1144-10401 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 37: P37 Panel - Wiring Changes W/B0188, Groups 10-12, 14-15, 17-21, 23, 25-26, 28, 32-34, **36-37 Airplanes.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 136 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 37: P37 Panel - Wiring Changes W/B0188, Groups 10-12, 14-15, 17-21, 23, 25-26, 28, 32-34, 36- 37 Airplanes.** 

This Figure applies to Group 10-12, 14-15, 17-21, 23, 25-26, 28, 32-34, 36-37: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-104. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 2 Contact BACC47CN1S 2 SWPM 20-61-11 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Identification Tape 289T1144-10402 1 SWPM 20-10-11 5 Identification Tape 289T1144-10403 1 SWPM 20-10-11 6 Identification Tape 289T1144-10405 1 SWPM 20-10-11 P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL AE0218

W192 TB212
W192 YC14 TB304 J 22 D5330P

J 3 D5506P

J 5 D5372P 

# W188 074-22

075-22

073-24 1 074-22

075-22

073-24

2

2

3 6 4

5 Z19

REFERENCE: 767 WIRE DIAGRAMS 28-42-12 7 8D60151 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 2)

### FIGURE 37: P37 Panel - Wiring Changes W/B0188, Groups 10-12, 14-15, 17-21, 23, 25-26, 28, 32-34, **36-37 Airplanes.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 137 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

7 Wire 289T1144-104W 1 SWPM 20-10-11 8 Lacing Tape 289T1144-10401 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 38: P37 Panel - Wiring Changes W/B0188, Groups 13, 22, 24, 27, 29-31, 38-39 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 138 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 38: P37 Panel - Wiring Changes W/B0188, Groups 13, 22, 24, 27, 29-31, 38-39 Airplanes.**

This Figure applies to Group 13, 22, 24, 27, 29-31, 38-39: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-104. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 2 Contact BACC47CN1S 2 SWPM 20-61-11 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Identification Tape 289T1144-10402 1 SWPM 20-10-11 5 Identification Tape 289T1144-10403 1 SWPM 20-10-11 6 Identification Tape 289T1144-10404 1 SWPM 20-10-11 7 Wire 289T1144-104W 1 SWPM 20-10-11 8 Lacing Tape 289T1144-10401 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL AE0218

W192 TB212
W192 YC14 TB304 J 22 D5330P

J 3 D5506P

J 5 D5372P 

# W188 074-22

075-22

073-24 1 074-22

075-22

073-24

2

2

3 6 4

5 Z19

REFERENCE: 767 WIRE DIAGRAMS 28-42-12 7 8D60154 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 39: P37 Panel - Wiring Changes W/B0188, Group 35 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 139 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 39: P37 Panel - Wiring Changes W/B0188, Group 35 Airplanes.**

This Figure applies to Group 35: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-104. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 2 Contact BACC47CN1S 2 SWPM 20-61-11 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Identification Tape 289T1144-10402 1 SWPM 20-10-11 5 Identification Tape 289T1144-10403 1 SWPM 20-10-11 6 Identification Tape 289T1144-10405 1 SWPM 20-10-11 7 Wire 289T1144-104W 1 SWPM 20-10-11 8 Lacing Tape 289T1144-10401 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL AE0218

W192 TB274
W192 YC14 TB304 J 22 D5330P

J 3 D5506P

J 5 D5372P 

# W188 074-22

075-22

073-24 1 074-22

075-22

073-24

2

2

3 6 4

5 Z2

REFERENCE: 767 WIRE DIAGRAMS 28-42-12 7 8D60157 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 40: P37 Panel - Wiring Changes W/B0192, Group 1 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 140 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 40: P37 Panel - Wiring Changes W/B0192, Group 1 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10692 R/H TIME DELAY

W198 D31186 

# W192

79H-24 YC6 TB212 4

8 3

6 K10690 R/H HOLD RELAY D31184 TB274 Z35 TB274 Z36 7

X2 J D4284P 12 W198

79X-24 004-24 W188

K330 OVRD PUMP R FUEL X1 004-24

78U-24 AE0218 YA7 TB212 2

2 5 3 7 79J-24

3 79G-24 79Q-24 79B-24

79V-24

1

5

4 7

9 1 78T-24

CONT RLY (4 LOCATIONS)

(2 LOCATIONS) (4 LOCATIONS) 2 (2 LOCATIONS)

2 (7 LOCATIONS) 11 10D60187



### (SHEET 1 OF 2)

### FIGURE 40: P37 Panel - Wiring Changes W/B0192, Group 1 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 141 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 1: REFERENCE: 767 Wire Diagram 28-22-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Contact BACT12AR222 2 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Identification Tape 289T1144-10502 1 SWPM 20-10-11 8 Identification Tape 289T1144-10503 1 SWPM 20-10-11 9 Identification Tape 289T1144-10505 1 SWPM 20-10-11 10 Wire 289T1144-105W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 41: P37 Panel - Wiring Changes W/B0192, Groups 2-3, 82-83 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 142 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 41: P37 Panel - Wiring Changes W/B0192, Groups 2-3, 82-83 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10692 R/H TIME DELAY

W198 D31186 

# W192

79H-24 YC7 TB212 4

8 3

6 K10690 R/H HOLD RELAY D31184 TB304 Z25 TB304 Z26 7

X2 J D4284P 12 W198

79X-24 004-24 W188

K330 OVRD PUMP R FUEL X1 004-24

78U-24 AE0218 YA7 TB212 2

2 5 3 7 79J-24

3 79G-24 79Q-24 79B-24

79V-24

1

5

4 7

9 1 78T-24

CONT RLY (4 LOCATIONS)

(2 LOCATIONS) (4 LOCATIONS) 2 (2 LOCATIONS)

2 (7 LOCATIONS) 11 10D60191



### (SHEET 1 OF 2)

### FIGURE 41: P37 Panel - Wiring Changes W/B0192, Groups 2-3, 82-83 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 143 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 2-3, 82-83: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Contact BACT12AR222 2 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Identification Tape 289T1144-10502 1 SWPM 20-10-11 8 Identification Tape 289T1144-10503 1 SWPM 20-10-11 9 Identification Tape 289T1144-10505 1 SWPM 20-10-11 10 Wire 289T1144-105W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 42: P37 Panel - Wiring Changes W/B0192, Group 4, 84 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 144 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 42: P37 Panel - Wiring Changes W/B0192, Group 4, 84 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10692 R/H TIME DELAY

W198 D31186 

# W192

79H-24 YA10 TB190 4 2

8 3

6 K10690 R/H HOLD RELAY D31184 TB304 Z25 TB304 Z26 7

X2 J D4284P 12 W198

79X-24 004-24 W188

K330 OVRD PUMP R FUEL X1 004-24

78U-24 AE0218 YA11 TB190 2

2 5 3 7 79J-24

3 79G-24 79Q-24 79B-24

79V-24 1

5

4 7

9 1 78T-24

CONT RLY (4 LOCATIONS)

(2 LOCATIONS) (4 LOCATIONS) (2 LOCATIONS)

2 (7 LOCATIONS) 10 11D60193



### (SHEET 1 OF 2)

### FIGURE 42: P37 Panel - Wiring Changes W/B0192, Group 4, 84 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 145 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 4, 84: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Contact BACT12AR222 2 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Identification Tape 289T1144-10502 1 SWPM 20-10-11 8 Identification Tape 289T1144-10503 1 SWPM 20-10-11 9 Identification Tape 289T1144-10505 1 SWPM 20-10-11 10 Wire 289T1144-105W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 43: P37 Panel - Wiring Changes W/B0192, Groups 5, 8-9, 16, 85, 87 Airplanes May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 146 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 43: P37 Panel - Wiring Changes W/B0192, Groups 5, 8-9, 16, 85, 87 Airplanes**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10692 R/H TIME DELAY

W198 D31186 

# W192

79H-24 YC6 TB212 4

8 3

6 K10690 R/H HOLD RELAY D31184 TB304 Z25 TB304 Z26 7

X2 J D4284P 12 W198

79X-24 004-24 W188

K330 OVRD PUMP R FUEL X1 004-24

78U-24 AE0218 YA7 TB212 2

2 5 3 7 79J-24

3 79G-24 79Q-24 79B-24

79V-24

1

5

4 7

9 1 78T-24

CONT RLY (4 LOCATIONS)

(2 LOCATIONS) (4 LOCATIONS) 2 (2 LOCATIONS)

2 (7 LOCATIONS) 11 10D60194



### (SHEET 1 OF 2)

### FIGURE 43: P37 Panel - Wiring Changes W/B0192, Groups 5, 8-9, 16, 85, 87 Airplanes May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 147 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 5, 8-9, 16, 85, 87: 767 WDM 28-22-12REFERENCE: 767 Wire Diagram 767 WDM 28-22-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Contact BACT12AR222 2 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Identification Tape 289T1144-10502 1 SWPM 20-10-11 8 Identification Tape 289T1144-10503 1 SWPM 20-10-11 9 Identification Tape 289T1144-10505 1 SWPM 20-10-11 10 Wire 289T1144-105W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 44: P37 Panel - Wiring Changes W/B0192, Group 6 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 148 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 44: P37 Panel - Wiring Changes W/B0192, Group 6 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10692 R/H TIME DELAY

W198 D31186 

# W192

79H-24 YC6 TB212 4

8 3

6 K10690 R/H HOLD RELAY D31184 TB212 Z19 TB212 Z20 7

X2 J D4284P 12 W198

79X-24 004-24 W188

K330 OVRD PUMP R FUEL X1 004-24

78U-24 AE0218 YA7 TB212 2

2 5 3 7 79J-24

3 79G-24 79Q-24 79B-24

79V-24

1

5

4 7

9 1 78T-24

CONT RLY (4 LOCATIONS)

(2 LOCATIONS) (4 LOCATIONS) 2 (2 LOCATIONS)

2 (7 LOCATIONS) 11 10D60197



### (SHEET 1 OF 2)

### FIGURE 44: P37 Panel - Wiring Changes W/B0192, Group 6 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 149 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 6: REFERENCE: 767 Wire Diagram767 WDM 28-22-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Contact BACT12AR222 2 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Identification Tape 289T1144-10502 1 SWPM 20-10-11 8 Identification Tape 289T1144-10503 1 SWPM 20-10-11 9 Identification Tape 289T1144-10505 1 SWPM 20-10-11 10 Wire 289T1144-105W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 45: P37 Panel - Wiring Changes W/B0192, Group 7, 86 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 150 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 45: P37 Panel - Wiring Changes W/B0192, Group 7, 86 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10692 R/H TIME DELAY

W198 D31186 

# W192

79H-24 YC7 TB212 4

8 3

6 K10690 R/H HOLD RELAY D31184 TB304 Z25 TB304 Z26 7

X2 J D4284P 12 W198

79X-24 004-24 W188

K330 OVRD PUMP R FUEL X1 004-24

78U-24 AE0218 YA9 TB212 2

2 5 3 7 79J-24

3 79G-24 79Q-24 79B-24

79V-24

1

5

4 7

9 1 78T-24

CONT RLY (4 LOCATIONS)

(2 LOCATIONS) (4 LOCATIONS) 2 (2 LOCATIONS)

2 (7 LOCATIONS) 11 10D60202



### (SHEET 1 OF 2)

### FIGURE 45: P37 Panel - Wiring Changes W/B0192, Group 7, 86 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 151 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 7, 86: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Contact BACT12AR222 2 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Identification Tape 289T1144-10502 1 SWPM 20-10-11 8 Identification Tape 289T1144-10503 1 SWPM 20-10-11 9 Identification Tape 289T1144-10505 1 SWPM 20-10-11 10 Wire 289T1144-105W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 46: P37 Panel - Wiring Changes W/B0192, Group 10 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 152 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 46: P37 Panel - Wiring Changes W/B0192, Group 10 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10692 R/H TIME DELAY

W198 D31186 

# W192

79H-24 YC7 TB212 4

8 3

6 K10690 R/H HOLD RELAY D31184 TB212 Z17 TB212 Z19 7

X2 J D4284P 12 W198

79X-24 004-24 W188

K330 OVRD PUMP R FUEL X1 004-24

78U-24 AE0218 YA7 TB212 2

2 5 3 7 79J-24

3 79G-24 79Q-24 79B-24

79V-24

1

5

4 7

9 1 78T-24

CONT RLY (4 LOCATIONS)

(2 LOCATIONS) (4 LOCATIONS) 2 (2 LOCATIONS)

2 (7 LOCATIONS) 11 10D60224



### (SHEET 1 OF 2)

### FIGURE 46: P37 Panel - Wiring Changes W/B0192, Group 10 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 153 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 10: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Contact BACT12AR222 2 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Identification Tape 289T1144-10502 1 SWPM 20-10-11 8 Identification Tape 289T1144-10503 1 SWPM 20-10-11 9 Identification Tape 289T1144-10505 1 SWPM 20-10-11 10 Wire 289T1144-105W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 47: P37 Panel - Wiring Changes W/B0192, Groups 11-12, 14-15, 17, 19, 21, 23, 25-26, 28, 36 **Airplanes.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 154 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 47: P37 Panel - Wiring Changes W/B0192, Groups 11-12, 14-15, 17, 19, 21, 23, 25-26, 28, 36 Airplanes.** 

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10692 R/H TIME DELAY

W198 D31186 

# W192
79H-24 YC6 TB212 4

8 3

6 K10690 R/H HOLD RELAY D31184 TB212 Z17 TB212 Z19 7

X2 J D4284P 12 W198

79X-24 004-24 W188

K330 OVRD PUMP R FUEL X1 004-24

78U-24 AE0218 YA7 TB212 2

2 5 3 7 79J-24

3 79G-24 79Q-24 79B-24

79V-24

1

5

4 7

9 1 78T-24

CONT RLY (4 LOCATIONS)

(2 LOCATIONS) (4 LOCATIONS) 2 (2 LOCATIONS)

2 (7 LOCATIONS) 11 10D60228



### (SHEET 1 OF 2)

### FIGURE 47: P37 Panel - Wiring Changes W/B0192, Groups 11-12, 14-15, 17, 19, 21, 23, 25-26, 28, 36 **Airplanes.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 155 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 11-12, 14-15, 17, 19, 21, 23, 25-26, 28, 36: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Contact BACT12AR222 2 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Identification Tape 289T1144-10502 1 SWPM 20-10-11 8 Identification Tape 289T1144-10503 1 SWPM 20-10-11 9 Identification Tape 289T1144-10505 1 SWPM 20-10-11 10 Wire 289T1144-105W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 48: P37 Panel - Wiring Changes W/B0192, Groups 13, 22, 24, 27, 29-31 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 156 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 48: P37 Panel - Wiring Changes W/B0192, Groups 13, 22, 24, 27, 29-31 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10692 R/H TIME DELAY

W198 D31186 

# W192

TB212 4

8 3

6 K10690 R/H HOLD RELAY D31184 TB212 Z17 TB212 Z19 7 J D4284P 12 79X-24 004-24 W188 AE0218 YA7 TB212 2

2 5 3 7

3 79G-24 79Q-24 79B-24

79V-24

1

5 7

9 1 (4 LOCATIONS)

(4 LOCATIONS)

78U-24 79H-24

TB212 YA14 K330 OVRD PUMP CONT RLY R FUEL X1 78U-24 004-24 YA12

4 79J-24 2

2 (7 LOCATIONS) 11 10D60236



### (SHEET 1 OF 2)

### FIGURE 48: P37 Panel - Wiring Changes W/B0192, Groups 13, 22, 24, 27, 29-31 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 157 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 13, 22, 24, 27, 29-31: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 8 SWPM 20-90-11 See note (a) 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Contact BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Identification Tape 289T1144-10502 1 SWPM 20-10-11 8 Identification Tape 289T1144-10503 1 SWPM 20-10-11 9 Identification Tape 289T1144-10505 1 SWPM 20-10-11 10 Wire 289T1144-105W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 49: P37 Panel - Wiring Changes W/B0192, Groups 18, 20, 32-34 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 158 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 49: P37 Panel - Wiring Changes W/B0192, Groups 18, 20, 32-34 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10692 R/H TIME DELAY

W198 D31186 

# W192

79H-24 YA6 TB212 4

8 3

6 K10690 R/H HOLD RELAY D31184 TB212 Z17 TB212 Z19 7

X2 J D4284P 12 W198

79X-24 004-24 W188

K330 OVRD PUMP R FUEL X1 004-24

78U-24 AE0218 YA7 TB212 2

2 5 3 7 79J-24

3 79G-24 79Q-24 79B-24

79V-24

1

5

4 7

9 1 78T-24

CONT RLY (4 LOCATIONS)

(2 LOCATIONS) (4 LOCATIONS) 2 (2 LOCATIONS)

2 (7 LOCATIONS) 11 10D60239



### (SHEET 1 OF 2)

### FIGURE 49: P37 Panel - Wiring Changes W/B0192, Groups 18, 20, 32-34 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 159 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 18, 20, 32-34: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Contact BACT12AR222 2 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Identification Tape 289T1144-10502 1 SWPM 20-10-11 8 Identification Tape 289T1144-10503 1 SWPM 20-10-11 9 Identification Tape 289T1144-10505 1 SWPM 20-10-11 10 Wire 289T1144-105W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 50: P37 Panel - Wiring Changes W/B0192, Group 35 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 160 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 50: P37 Panel - Wiring Changes W/B0192, Group 35 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10692 R/H TIME DELAY

W198 D31186 

# W192

79H-24 YA10 TB190 4

8 3

6 K10690 R/H HOLD RELAY D31184 TB274 Z1 TB274 Z2 7

X2 J D4284P 12 W198

79X-24 004-24 W188

K330 OVRD PUMP R FUEL X1 004-24

78U-24 AE0218 YA11 TB190 2

2 5 3 7 79J-24

3 79G-24 79Q-24 79B-24

79V-24

1

5

4 7

9 1 78T-24

CONT RLY (4 LOCATIONS)

(2 LOCATIONS) (4 LOCATIONS) 2 (2 LOCATIONS)

2 (7 LOCATIONS) 11 10D60242



### (SHEET 1 OF 2)

### FIGURE 50: P37 Panel - Wiring Changes W/B0192, Group 35 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 161 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 35: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Contact BACT12AR222 2 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Identification Tape 289T1144-10502 1 SWPM 20-10-11 8 Identification Tape 289T1144-10503 1 SWPM 20-10-11 9 Identification Tape 289T1144-10505 1 SWPM 20-10-11 10 Wire 289T1144-105W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 51: P37 Panel - Wiring Changes W/B0192, Group 37 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 162 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 51: P37 Panel - Wiring Changes W/B0192, Group 37 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10692 R/H TIME DELAY

W198 D31186 

# W192

79H-24 YC6 TB212 4

8 3

6 K10690 R/H HOLD RELAY D31184 TB212 Z17 TB212 Z19 7

X2 J D4284P 12 W198

79X-24 004-24 W188

K330 OVRD PUMP R FUEL X1 004-24

78U-24 AE0218 YA7 TB212 2

2 5 3 7 79J-24

3 79G-24 79Q-24 79B-24

79V-24

1

5

4 7

9 1 78T-24

CONT RLY (4 LOCATIONS)

(2 LOCATIONS) (4 LOCATIONS) 2 (2 LOCATIONS)

2 (7 LOCATIONS) 11 10D60244



### (SHEET 1 OF 2)

### FIGURE 51: P37 Panel - Wiring Changes W/B0192, Group 37 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 163 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 37: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 9 SWPM 20-90-11 See note (a) 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Contact BACT12AR222 2 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Identification Tape 289T1144-10502 1 SWPM 20-10-11 8 Identification Tape 289T1144-10503 1 SWPM 20-10-11 9 Identification Tape 289T1144-10505 1 SWPM 20-10-11 10 Wire 289T1144-105W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 52: P37 Panel - Wiring Changes W/B0192, Group 38 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 164 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 52: P37 Panel - Wiring Changes W/B0192, Group 38 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10692 R/H TIME DELAY

W198 D31186 

# W192

TB212 4

8 3

6 K10690 R/H HOLD RELAY D31184 TB212 Z17 TB212 Z19 7 J D4284P 12 79X-24 004-24 W188 AE0218 YC12 TB212 2

2 5 3 7

3 79G-24 79Q-24 79B-24

79V-24

1

5 7

9 1 (4 LOCATIONS)

(4 LOCATIONS)

78U-24 79H-24

TB212 YA14 K330 OVRD PUMP CONT RLY R FUEL X1 78U-24 004-24 YA12

4 79J-24 2

2 (7 LOCATIONS) 11 10D60246



### (SHEET 1 OF 2)

### FIGURE 52: P37 Panel - Wiring Changes W/B0192, Group 38 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 165 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 38: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 8 SWPM 20-90-11 See note (a) 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Contact BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Identification Tape 289T1144-10502 1 SWPM 20-10-11 8 Identification Tape 289T1144-10503 1 SWPM 20-10-11 9 Identification Tape 289T1144-10505 1 SWPM 20-10-11 10 Wire 289T1144-105W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 53: P37 Panel - Wiring Changes W/B0192, Group 39 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 166 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 53: P37 Panel - Wiring Changes W/B0192, Group 39 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10692 R/H TIME DELAY

W1118 D31186 

# W192

TB212 4

8 3

6 K10690 R/H HOLD RELAY D31184 TB212 Z17 TB212 Z19 7 J D4284P 12 79X-24 004-24 W188 AE0218 YC12 TB212 2

2 5 3 7

3 79G-24 79Q-24 79B-24

79V-24

1

5 7

9 1 (4 LOCATIONS)

(4 LOCATIONS)

78U-24 79H-24

TB212 YA14 K330 OVRD PUMP CONT RLY R FUEL X1 78U-24 004-24 YA12

4 79J-24 2

2 (7 LOCATIONS) 11 10D60247



### (SHEET 1 OF 2)

### FIGURE 53: P37 Panel - Wiring Changes W/B0192, Group 39 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 167 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 39: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 8 SWPM 20-90-11 See note (a) 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Contact BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Identification Tape 289T1144-10502 1 SWPM 20-10-11 8 Identification Tape 289T1144-10503 1 SWPM 20-10-11 9 Identification Tape 289T1144-10505 1 SWPM 20-10-11 10 Wire 289T1144-105W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 54: P37 Panel - Wiring Changes W/B0198, Groups 1, 5-6, 8-9, 14, 16-17, 19, 25, 28, 36, 85, 87 **Airplanes.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 168 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 54: P37 Panel - Wiring Changes W/B0198, Groups 1, 5-6, 8-9, 14, 16-17, 19, 25, 28, 36, 85, 87 Airplanes.** 

This Figure applies to Group 1, 5-6, 8-9, 14, 16-17, 19, 25, 28, 36, 85, 87: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 2 SWPM 20-61-11 2 Contact M39029/11-145 2 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 3 AE0224 2 W590

1 12 1

D5052P YA7

J W192

P37 TB212

RIGHT MISCELLANEOUS ELECTRICAL PANEL 23 02A-24 520-24 189-24 

# W198
X2 K330 R FUEL OVRD PUMP CONT RLY 2 YC6 TB212 W192

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5D60250 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 55: P37 Panel - Wiring Changes W/B0198, Groups 2-3, 10 82-83 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 169 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 55: P37 Panel - Wiring Changes W/B0198, Groups 2-3, 10 82-83 Airplanes.**

This Figure applies to Group 2-3, 10, 82-83: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 2 SWPM 20-61-11 2 Contact M39029/11-145 2 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 3 AE0224 2 W590

1 12 1

D5052P YA7

J W192

P37 TB212

RIGHT MISCELLANEOUS ELECTRICAL PANEL 23 02A-24 520-24 189-24 

# W198
X2 K330 R FUEL OVRD PUMP CONT RLY 2 YC7 TB212 W192

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5D60255 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 56: P37 Panel - Wiring Changes W/B0198, Group 4, 84 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 170 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 56: P37 Panel - Wiring Changes W/B0198, Group 4, 84 Airplanes.**

This Figure applies to Group 4, 84: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 2 SWPM 20-61-11 2 Contact M39029/11-145 2 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 3 AE0224 2 W590

1 12 1

D5052P YA11

J W192

P37 TB190

RIGHT MISCELLANEOUS ELECTRICAL PANEL 23 02A-24 520-24 189-24 

# W198
X2 K330 R FUEL OVRD PUMP CONT RLY 2 YA10 TB190 W192

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5D60258 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 57: P37 Panel - Wiring Changes W/B0198, Group 7, 86 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 171 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 57: P37 Panel - Wiring Changes W/B0198, Group 7, 86 Airplanes.**

This Figure applies to Group 7, 86: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 2 SWPM 20-90-11 See note (a) 3 Contact BACC47CP3T 1 SWPM 20-61-11 4 Contact Y-9015-C 1 SWPM 20-60-00 5 Identification Tape 289T1144-10602 1 SWPM 20-10-11 6 Wire 289T1144-106W 1 SWPM 20-10-11 7 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 5 23 189-24 520-24 3 W590

1 2 AE0224

D5052P 6

J W192

P37 RIGHT MISCELLANEOUS ELECTRICAL PANEL YC7 K330 OVRD PUMP CONT RLY R FUEL TB212 YA9 02A-24

2 X2 4 TB212 

# W198

W192

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 6 7D60263 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 58: P37 Panel - Wiring Changes W/B0198, Groups 11, 21 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 172 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 58: P37 Panel - Wiring Changes W/B0198, Groups 11, 21 Airplanes.**

This Figure applies to Group 11, 21: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 2 SWPM 20-90-11 See note (a) 3 Contact BACC47CP3T 1 SWPM 20-61-11 4 Contact Y-9015-C 1 SWPM 20-60-00 5 Identification Tape 289T1144-10602 1 SWPM 20-10-11 6 Wire 289T1144-106W 1 SWPM 20-10-11 7 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 189-24

1 520-24 3

5 W590 W192

P37 RIGHT MISCELLANEOUS ELECTRICAL PANEL

J AE0224

D5052P 6
YC6 2

TB212 YA7 TB212
K330 R FUEL OVRD PUMP CONT RLY 02A-24

2 

# W198
X2 4 W192 23

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 6 7D60268 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 59: P37 Panel - Wiring Changes W/B0198, Groups 12, 15, 23, 26 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 173 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 59: P37 Panel - Wiring Changes W/B0198, Groups 12, 15, 23, 26 Airplanes.**

This Figure applies to Group 12, 15, 23, 26: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 2 SWPM 20-61-11 2 Contact M39029/11-145 2 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 3 23 189-24 520-24 1 W590

1 2 AE0224

D5052P 19

J W192

P37 RIGHT MISCELLANEOUS ELECTRICAL PANEL YC6 K330 OVRD PUMP CONT RLY R FUEL TB212 YA7 02A-24

2 X2 TB212 

# W198

W192

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5D60270 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 60: P37 Panel - Wiring Changes W/B0198, Groups 13, 24, 27 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 174 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 60: P37 Panel - Wiring Changes W/B0198, Groups 13, 24, 27 Airplanes.**

This Figure applies to Group 13, 24, 27: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 3 19 02A-24 AE0224
D5052P J P37 RIGHT MISCELLANEOUS ELECTRICAL PANEL YA7 TB212 

# W198 W192 W590 1 2

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5D60272 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 61: P37 Panel - Wiring Changes W/B0198, Groups 18, 20, 32-34 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 175 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 61: P37 Panel - Wiring Changes W/B0198, Groups 18, 20, 32-34 Airplanes.**

This Figure applies to Group 18, 20, 32-34: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 2 SWPM 20-61-11 2 Contact M39029/11-145 2 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 3 23 189-24 520-24 1 W590

1 2 AE0224

D5052P 12

J W192

P37 RIGHT MISCELLANEOUS ELECTRICAL PANEL YA6 K330 OVRD PUMP CONT RLY R FUEL TB212 YA7 02A-24

2 X2 TB212 

# W198

W192

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5D60276 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 62: P37 Panel - Wiring Changes W/B0198, Group 22 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 176 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 62: P37 Panel - Wiring Changes W/B0198, Group 22 Airplanes.**

This Figure applies to Group 22: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 2 Contact BACC47CP3T 1 SWPM 20-61-11 3 Contact Y-9015-C 1 SWPM 20-60-00 4 Identification Tape 289T1144-10602 1 SWPM 20-10-11 5 Wire 289T1144-106W 1 SWPM 20-10-11 6 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 4 AE0224 1 W590 3 02A-24 W198- 6 2 D5052P YA7 J W192

P37 TB212
RIGHT MISCELLANEOUS ELECTRICAL PANEL 5 6

REFERENCE: 767 WIRE DIAGRAMS 28-22-12D60350 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 63: P37 Panel - Wiring Changes W/B0198, Group 29-30 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 177 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 63: P37 Panel - Wiring Changes W/B0198, Group 29-30 Airplanes.**

This Figure applies to Group 29-30: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 3 1 W590 2 AE0224
D5052P 12 J W192

P37 RIGHT MISCELLANEOUS ELECTRICAL PANEL W198- TB212 YA7 02A-24

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5D60353 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 64: P37 Panel - Wiring Changes W/B0198, Group 31 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 178 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 64: P37 Panel - Wiring Changes W/B0198, Group 31 Airplanes.**

This Figure applies to Group 31: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 3 13 02A-24 1 AE0224
D5052P J P37 RIGHT MISCELLANEOUS ELECTRICAL PANEL YA7 2 TB212 

# W198 W192 W590

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5D60355 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 65: P37 Panel - Wiring Changes W/B0198, Group 35 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 179 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 65: P37 Panel - Wiring Changes W/B0198, Group 35 Airplanes.**

This Figure applies to Group 35: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 189-24

1 520-24 1

3 W590 W192

P37 RIGHT MISCELLANEOUS ELECTRICAL PANEL

J AE0224

D5052P 19
YA10 2

TB190 YA11 TB190
K330 R FUEL OVRD PUMP CONT RLY 02A-24

2 

# W198
X2 23 W192

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5D60356 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 66: P37 Panel - Wiring Changes W/B0198, Group 37 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 180 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 66: P37 Panel - Wiring Changes W/B0198, Group 37 Airplanes.**

This Figure applies to Group 37: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 3 23 189-24 520-24

1 AE0224
D5052P J P37 RIGHT MISCELLANEOUS ELECTRICAL PANEL YC6 K330 OVRD PUMP CONT RLY R FUEL 2 X2 TB212 

# W198 W192

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5D60357 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 67: P37 Panel - Relay Installation, Groups 1-39, 82-87 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 181 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 67: P37 Panel - Relay Installation, Groups 1-39, 82-87 Airplanes.**



### MAIN EQUIPMENT CENTER P37 PANEL

A A FWD

FWD UPD60360



### (SHEET 1 OF 2)

### FIGURE 67: P37 Panel - Relay Installation, Groups 1-39, 82-87 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 182 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 1-39, 82-87: The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY numbers shown below are the number of parts necessary for each airplane. Use parts from Top Kit 015T1775- 2 (Group 1-39, 82-87 airplanes). **STEP TASK NAME IDENTIFICATION QTY MORE DATA** 1 Install Relay BACR13CD2 1 -- 2 Install Relay TDH-1852-1402 1 -- 

### A-AK10692K10690



### FWD UP 1 2D60361



### (SHEET 2 OF 2)

### FIGURE 68: P37 Panel - Wiring Changes W/B0198, Group 38 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 183 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 68: P37 Panel - Wiring Changes W/B0198, Group 38 Airplanes.**

This Figure applies to Group 38: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 

### AE0224 2 W590 3 02A-24 W198- 19 1 D5052P YC12 J W192

P37 TB212
RIGHT MISCELLANEOUS ELECTRICAL PANEL

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60358



### (SHEET 1 OF 1)

### 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.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 184 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **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.** 

This Figure applies to Group 1-6, 8-15, 17-24, 26-31, 33-35, 37-39, 82-85, 87: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-107. Route new wiring from the P36 panel to P33 panel, see figure 81 for wire bundle routing information, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 2 SWPM 20-61-11 2 Identification Tape 289T1144-10703 1 SWPM 20-10-11 3 Identification Tape 289T1144-10704 1 SWPM 20-10-11 4 Wire 289T1144-107W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10702 1 SWPM 20-10-11 ELECTRICAL PANEL 3 FOWARD MISC. W264- AE0209 AE0203

P33 16A-22 W184 D8026P 41 J 23 D4042P W146 J 1 1

LEFT MISC. ELECTRICAL EQPT PANEL 2 P36

REFERENCE: 767 WIRE DIAGRAMS 28-42-12 4 5D60362 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 70: P33 to P36 Panel - Wiring Changes W/B0264, Groups 7, 16, 86 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 185 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 70: P33 to P36 Panel - Wiring Changes W/B0264, Groups 7, 16, 86 Airplanes.**

This Figure applies to Group 7, 16, 86: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-107. Route new wiring from the P36 panel to P33 panel, see figure 81 for wire bundle routing information, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 2 SWPM 20-61-11 2 Identification Tape 289T1144-10703 1 SWPM 20-10-11 3 Identification Tape 289T1144-10704 1 SWPM 20-10-11 4 Wire 289T1144-107W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10702 1 SWPM 20-10-11 ELECTRICAL PANEL P36 3 FOWARD MISC. W264- AE0209 AE0203

P33 16A-22 W184 D8026P 54 J 23 D4042P W146 J 1 1

LEFT MISC. ELECTRICAL EQPT PANEL 2

REFERENCE: 767 WIRE DIAGRAMS 28-42-12 4 5D60363 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 71: P33 to P36 Panel - Wiring Changes W/B0264, Groups 25, 32 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 186 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 71: P33 to P36 Panel - Wiring Changes W/B0264, Groups 25, 32 Airplanes.**

This Figure applies to Group 25, 32: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-107. Route new wiring from the P36 panel to P33 panel, see figure 81 for wire bundle routing information, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 2 SWPM 20-61-11 2 Identification Tape 289T1144-10703 1 SWPM 20-10-11 3 Identification Tape 289T1144-10704 1 SWPM 20-10-11 4 Wire 289T1144-107W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10702 1 SWPM 20-10-11 ELECTRICAL PANEL 3 FOWARD MISC. W264- AE0209 AE0203

P33 16A-22 W184 D8026P 40 J 23 D4042P W146 J 1 1

LEFT MISC. ELECTRICAL EQPT PANEL 2 P36

REFERENCE: 767 WIRE DIAGRAMS 28-42-12 4 5D60365 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 72: P33 to P36 Panel - Wiring Changes W/B0264, Group 36 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 187 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 72: P33 to P36 Panel - Wiring Changes W/B0264, Group 36 Airplanes.**

This Figure applies to Group 36: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-107. Route new wiring from the P36 panel to P33 panel, see figure 81 for wire bundle routing information, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 2 SWPM 20-61-11 2 Identification Tape 289T1144-10703 1 SWPM 20-10-11 3 Identification Tape 289T1144-10704 1 SWPM 20-10-11 4 Wire 289T1144-107W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10702 1 SWPM 20-10-11 ELECTRICAL PANEL P36 3 FOWARD MISC. W264- AE0209 AE0203

P33 16A-22 W184 D8026P 34 J 23 D4042P W146 J 1 1

LEFT MISC. ELECTRICAL EQPT PANEL 2

REFERENCE: 767 WIRE DIAGRAMS 28-42-12 4 5D60366 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### 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.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 188 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **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.** 

This Figure applies to Group 1-6, 8-10, 14, 16-20, 25, 28-30, 32-34, 36, 82-85, 87: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-108. Reference Figure 81 for wire bundle routing information. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact BACC47CN1S 1 SWPM 20-61-11 3 Identification Tape 289T1144-10803 1 SWPM 20-10-11 4 Identification Tape 289T1144-10804 1 SWPM 20-10-11 5 Wire 289T1144-108W 1 SWPM 20-10-11 6 Lacing Tape 289T1144-10802 1 SWPM 20-10-11 ELECTRICAL EQPT PANEL 4 RIGHT MISC. W590- AE0209 AE0224

P37 021-24 W184 D4856P 13 J 12 D5052P W198 J 2 1

LEFT MISC. ELECTRICAL EQPT PANEL 3 P36 5 6

REFERENCE: 767 WIRE DIAGRAMS 28-42-12D60380 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 74: P36 to P37 Panel - Wiring Changes W/B0590, Group 31 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 189 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 74: P36 to P37 Panel - Wiring Changes W/B0590, Group 31 Airplanes.**

This Figure applies to Group 31: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-108. Reference Figure 81 for wire bundle routing information. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact BACC47CN1S 1 SWPM 20-61-11 3 Identification Tape 289T1144-10803 1 SWPM 20-10-11 4 Identification Tape 289T1144-10804 1 SWPM 20-10-11 5 Wire 289T1144-108W 1 SWPM 20-10-11 6 Lacing Tape 289T1144-10802 1 SWPM 20-10-11 ELECTRICAL EQPT PANEL P36 4 FRIGHT MISC. W590- AE0209 AE0224

P37 021-24 W184 D4856P 13 J D5052P W198 J 2 1

LEFT MISC. ELECTRICAL EQPT PANEL 3 13 5 6

REFERENCE: 767 WIRE DIAGRAMS 28-42-12D60383 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 75: P36 to P37 Panel - Wiring Changes W/B0590, Group 35 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 190 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 75: P36 to P37 Panel - Wiring Changes W/B0590, Group 35 Airplanes.**

This Figure applies to Group 35: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-108. Reference Figure 81 for wire bundle routing information. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact BACC47CN1S 1 SWPM 20-61-11 3 Identification Tape 289T1144-10803 1 SWPM 20-10-11 4 Identification Tape 289T1144-10804 1 SWPM 20-10-11 5 Wire 289T1144-108W 1 SWPM 20-10-11 6 Lacing Tape 289T1144-10802 1 SWPM 20-10-11 ELECTRICAL EQPT PANEL 4 RIGHT MISC. W590- AE0209 AE0224

P37 021-24 W184 D4856P 2 J 19 D5052P W146 J 2 1

LEFT MISC. ELECTRICAL EQPT PANEL 3 P36

REFERENCE: 767 WIRE DIAGRAMS 28-42-12 5 6D60393 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 76: P36 to P37 Panel - Wiring Changes W/B0590, Groups 7, 11, 21-22, 86 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 191 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 76: P36 to P37 Panel - Wiring Changes W/B0590, Groups 7, 11, 21-22, 86 Airplanes.**

This Figure applies to Group 7, 11, 21-22, 86: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-108. Reference Figure 81 for wire bundle routing information. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact BACC47CN3 1 SWPM 20-61-11 3 Eyelet Y-9015-C 1 SWPM 20-60-00 4 Identification Tape 289T1144-10803 1 SWPM 20-10-11 5 Identification Tape 289T1144-10804 1 SWPM 20-10-11 6 Wire 289T1144-108W 1 SWPM 20-10-11 7 Lacing Tape 289T1144-10802 1 SWPM 20-10-11 ELECTRICAL EQPT PANEL P36 5 FRIGHT MISC. W590- AE0209 AE0224

P37 021-24 W184 D4856P 13 J 6 D5052P W198 J 2 1

LEFT MISC. ELECTRICAL EQPT PANEL 4 3

REFERENCE: 767 WIRE DIAGRAMS 28-42-12 6 7D60401 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 77: P36 to P37 Panel - Wiring Changes W/B0590, Groups 12-13, 15, 23-24, 26-27, 38 Air**planes.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 192 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 77: P36 to P37 Panel - Wiring Changes W/B0590, Groups 12-13, 15, 23-24, 26-27, 38 Airplanes.**

This Figure applies to Group 12-13, 15, 23-24, 26-27, 38: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-108. Reference Figure 81 for wire bundle routing information. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact BACC47CN1S 1 SWPM 20-61-11 3 Identification Tape 289T1144-10803 1 SWPM 20-10-11 4 Identification Tape 289T1144-10804 1 SWPM 20-10-11 5 Wire 289T1144-108W 1 SWPM 20-10-11 6 Lacing Tape 289T1144-10802 1 SWPM 20-10-11 ELECTRICAL EQPT PANEL P36 4 FRIGHT MISC. W590- AE0209 AE0224

P37 021-24 W184 D4856P 13 J 19 D5052P W198 J 2 1

LEFT MISC. ELECTRICAL EQPT PANEL 3

REFERENCE: 767 WIRE DIAGRAMS 28-42-12 5 6D60403 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 78: P36 to P37 Panel - Wiring Changes W/B0942, Groups 37, 39 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 193 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 78: P36 to P37 Panel - Wiring Changes W/B0942, Groups 37, 39 Airplanes.**

This Figure applies to Group 37, 39: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-109. Reference Figure 81 for wire bundle routing information. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 2 SWPM 20-61-11 2 Identification Tape 289T1144-10904 1 SWPM 20-10-11 3 Identification Tape 289T1144-10905 1 SWPM 20-10-11 4 Wire 289T1144-109W 1 SWPM 20-10-22 5 Lacing Tape 289T1144-10901 1 SWPM 20-10-22 ELECTRICAL EQPT PANEL P36 3 FRIGHT MISC. W942- AE0209 AE0218

P37 011-24 W176 D4906P 5 J D6658P W1118 J 1 1

LEFT MISC. ELECTRICAL EQPT PANEL 2 13

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60437



### (SHEET 1 OF 1)

### FIGURE 79: P37 Panel - Wiring Changes W/B1118, Group 39 Airplanes May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 194 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 79: P37 Panel - Wiring Changes W/B1118, Group 39 Airplanes**

This Figure applies to Group 39: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-110. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 2 Contact BACC47CN1S 1 SWPM 20-61-11 3 Identification Tape 289T1144-11003 1 SWPM 20-10-11 4 Wire 289T1144-110W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-11001 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 1 14A-24 W1118- 13 D6658P W942 YC12 2
3 AE0218
J W192

P37 RIGHT MISCELLANEOUS ELECTRICAL PANEL TB212

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5D60457 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 80: P37 Panel - Wiring Changes W/B1118, Group 37 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 195 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 80: P37 Panel - Wiring Changes W/B1118, Group 37 Airplanes.**

This Figure applies to Group 37: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-110. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 2 Contact BACC47CN1S 1 SWPM 20-61-11 3 Identification Tape 289T1144-11003 1 SWPM 20-10-11 4 Wire 289T1144-110W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-11001 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 2
3 W942 W192

P37

J AE0218
D6658P 13
RIGHT MISCELLANEOUS ELECTRICAL PANEL 1 W1118- YA7 TB212 14A-24

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5D60468 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 81: Wire Bundle Routing, P36 to P37 Panel, Groups 1-39, 82-87 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 196 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 81: Wire Bundle Routing, P36 to P37 Panel, Groups 1-39, 82-87 Airplanes.** 

P36 P37

P33

FWD 3 1

2 3D60470



### (SHEET 1 OF 3)

### FIGURE 81: Wire Bundle Routing, P36 to P37 Panel, Groups 1-39, 82-87 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 197 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 1-39, 82-87: P36 P37

P33 ALTERNATE WIRE ROUTING CONFIGURATION

FWD 3 1

2 31561302



### (SHEET 2 OF 3)

### FIGURE 81: Wire Bundle Routing, P36 to P37 Panel, Groups 1-39, 82-87 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 198 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY numbers shown below are the number of parts necessary for each airplane. Use lacing tape supplied as required for wire bundle installation. **STEP TASK NAME IDENTIFICATION QTY MORE DATA**

1 Install Wire Bundle - W/B 590 or W/B 942 -- -- Gain access to the P36 and P37 Panels. Install the new wiring between the P36 and P37 panels using the existing wire bundle routing for W/B 590 or W/B 942 (use alternate wire routing when applicable). Refer to SWPM 20-10-11 and SWPM 20-10-12 for wire installation procedures.

2 Install Wire Bundle - W/B 264 -- Gain access to P36 panel and P33 panels. Install the new wiring following the existing wire bundle routing for W/B 264. Refer to SWPM 20-10-11 and SWPM 20-10-12 for wire installation procedures. 3 Install Lacing Tape 289T1144-( ) -- --

**(SHEET 3 OF 3)**

### FIGURE 82: P36 Panel - Bracket Installation, Group 40-79, 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 199 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 82: P36 Panel - Bracket Installation, Group 40-79, 88 Airplanes.**

P36 PANEL


### MAIN EQUIPMENT CENTER A A C

C

FWD FWD

1 4 SEE C-C FOR ALTERNATE CONFIGURATIONJ82159



### (SHEET 1 OF 4)

### FIGURE 82: P36 Panel - Bracket Installation, Group 40-79, 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 200 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

A-A

B-B SUPPORT BRACKET STANCHION

1.25 ± 0.14 1.70 0.30

STANCHION
SUPPORT BRACKET B B FWD INBD 3

2 FWD UPJ82158



### (SHEET 2 OF 4)

### FIGURE 82: P36 Panel - Bracket Installation, Group 40-79, 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 201 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 40-79, 88: 

### C-C

D-D STANCHION

1.25 ± 0.14 1.70 0.80

STANCHION ALTERNATE CONFIGURATION

ALTERNATE CONFIGURATION D D FWD INBD 3

2 FWD UP1561717



### (SHEET 3 OF 4)

### FIGURE 82: P36 Panel - Bracket Installation, Group 40-79, 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 202 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY numbers shown below are the number of parts necessary for bracket installation on the P36 panel. Use parts from Top Kit 015T1775-3. **STEP TASK NAME IDENTIFICATION QTY MORE DATA** 1 Remove (Keep) Cover P36 Panel 1 -- 2 Install (New) Bracket 284T0378-234 1 Position bracket with decal text K10691 and K10693 facing inboard. 3 Install (New) Screw BACS12GU3K7 2 Drill .218 - .2290 diameter Holes. Washer NAS1149D0332H 2 -- 4 Install (Kept) Cover P36 Panel 1 Do not install Cover if wiring installation will be completed next.

**(SHEET 4 OF 4)**

### FIGURE 83: P37 Panel - Bracket Installation, Groups 40-79, 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 203 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 83: P37 Panel - Bracket Installation, Groups 40-79, 88 Airplanes.**



### MAIN EQUIPMENT CENTER A A P37 PANEL

FWD

1

FWD UP 4J82157



### (SHEET 1 OF 3)

### FIGURE 83: P37 Panel - Bracket Installation, Groups 40-79, 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 204 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 40-79, 88: 

### A-A

B-B 1.25 ± 0.14 0.30

1.70 SUPPORT BRACKET STANCHION

SUPPORT BRACKET STANCHION B B FWD INBD

2 FWD UP 3J82156



### (SHEET 2 OF 3)

### FIGURE 83: P37 Panel - Bracket Installation, Groups 40-79, 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 205 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY numbers shown below are the number of parts necessary for bracket installation on the P37 Panel. Use parts from Top Kit 015T1775-3. **STEP TASK NAME IDENTIFICATION QTY MORE DATA** 1 Remove (Keep) Cover P37 Panel 1 -- 2 Install (New) Bracket 284T0378-233 1 Position bracket with decal text K10690 and K10692 facing inboard. 3 Install (New) Screw BACS12GU3K7 2 Drill .218 - .2290 diameter Holes. Washer NAS1149D0332H 2 4 Install (Kept) Cover P37 Panel 1 Do not install Cover if wiring installation will be completed next.

**(SHEET 3 OF 3)**

### FIGURE 84: P36 Panel - Wiring Changes W/B0176, Group 40 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 206 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 84: P36 Panel - Wiring Changes W/B0176, Group 40 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 YC10 TB216 4

4

6
K10691 L/H HOLD RELAY D11629 TB216 Z19 TB218 YC5

7 J D4672P 18 85W-24 02H-22 02H-22 YA5 TB218 2

2 5 3 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

5 12

8 7

TB74 YA13 51

K329 OVRD PUMP CONT RLY L FUEL X1 75W-22 53E-24 75W-22 53E-24 XD3 50
D5658P TB218 53C-22 53C-22 W184
6
3 02F-24 J 4 D5658P 02F-24 TB216

YA10 TB218

XB12 6 9 W184

W184 2 (11 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) 11

10 AE0223

AE0209D59731



### (SHEET 1 OF 2)

### FIGURE 84: P36 Panel - Wiring Changes W/B0176, Group 40 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 207 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 40: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 11 SWPM 20-90-11 See note (a) 3 Terminal Lug BACT12AR222 1 SWPM 20-30-11 4 Relay Socket BACS16AH1 1 SWPM 20-81-22 5 Relay Socket BACS16AG1 1 SWPM 20-81-22 6 Pin BACC47CN1S 4 SWPM 20-61-11 7 Identification Tape 289T1144-10202 1 SWPM 20-10-11 8 Identification Tape 289T1144-10203 1 SWPM 20-10-11 9 Identification Tape 289T1144-10209 1 SWPM 20-10-11 10 Identification Tape 289T1144-10210 1 SWPM 20-10-11 11 Wire 289T1144-102W 1 SWPM 20-10-11 12 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 85: P36 Panel - Wiring Changes W/B0176, Groups 42, 67-68 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 208 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 85: P36 Panel - Wiring Changes W/B0176, Groups 42, 67-68 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24

5 J

D4906P 4

J D5658P W0942 TB216

YA10

YC10 TB216 4

W184

5

7 7

K10691 L/H HOLD RELAY D11629 TB216 Z19 TB218 YC5

7

TB74 J D4672P 18

YA13 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YA5 TB218 02F-24

2

2 5 3

B1 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 13 11

10 9 8 3 (10 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 14 15D59736



### (SHEET 1 OF 2)

### FIGURE 85: P36 Panel - Wiring Changes W/B0176, Groups 42, 67-68 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 209 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 42, 67-68: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 3 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Identification Tape 289T1144-10211 1 SWPM 20-10-11 14 Wire 289T1144-102W 1 SWPM 20-10-11 15 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 86: P36 Panel - Wiring Change W/B0176, Group 76 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 210 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 86: P36 Panel - Wiring Change W/B0176, Group 76 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24

5 J

D4906P 4

J D5658P W0942 TB216

YA10

YC10 TB216 4

W184

5

7 7

K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218 YC5

7

TB74 J D4672P 18

YA13 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YA5 TB218 02F-24

2

2 5 3

B1 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 13 11

10 9 8 3 (10 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 14 15D59738



### (SHEET 1 OF 2)

### FIGURE 86: P36 Panel - Wiring Change W/B0176, Group 76 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 211 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 76: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 3 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Identification Tape 289T1144-10211 1 SWPM 20-10-11 14 Wire 289T1144-102W 1 SWPM 20-10-11 15 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 87: P36 Panel - Wiring Changes W/B0176, Group 55 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 212 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 87: P36 Panel - Wiring Changes W/B0176, Group 55 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24

5 J

D4906P 4

J D5658P W0942 TB216

YA10

YC10 TB216 4

W184

5

7 7

K10691 L/H HOLD RELAY D11629 TB216 Z8 TB218 YA20

7

TB218 J D4672P 18

YA20 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YC20 TB218 02F-24

2

2 5 3

B1 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 13 11

10 9 8 3 (10 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) 14 15 AE0223

AE0209D59740



### (SHEET 1 OF 2)

### FIGURE 87: P36 Panel - Wiring Changes W/B0176, Group 55 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 213 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 55: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 3 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Identification Tape 289T1144-10211 1 SWPM 20-10-11 14 Wire 289T1144-102W 1 SWPM 20-10-11 15 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 88: P36 Panel - Wiring Changes W/B0176, Group 49 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 214 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 88: P36 Panel - Wiring Changes W/B0176, Group 49 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24

5 J

D4906P 4

J D5658P W0942 TB216

YA10

YC10 TB216 4

W184

5

7 7

K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218 YC5

7

TB218 J D4672P 18

YA20 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YA5 TB218 02F-24

2

2 5 3

B1 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 13 11

10 9 8 3 (10 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 14 15D59741



### (SHEET 1 OF 2)

### FIGURE 88: P36 Panel - Wiring Changes W/B0176, Group 49 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 215 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 49: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 3 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Identification Tape 289T1144-10211 1 SWPM 20-10-11 14 Wire 289T1144-102W 1 SWPM 20-10-11 15 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 89: P36 Panel - Wiring Changes W/B0176, Groups 54, 79 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 216 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 89: P36 Panel - Wiring Changes W/B0176, Groups 54, 79 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24

5 J

D4906P 4

J D5658P W0942 TB216

YA10

YC10 TB216 4

W184

5

7 7

K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218 YA20

7

TB218 J D4672P 18

YA20 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YC20 TB218 02F-24

2

2 5 3

B1 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 13 11

10 9 8 3 (10 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) 14 15 AE0223

AE0209D59742



### (SHEET 1 OF 2)

### FIGURE 89: P36 Panel - Wiring Changes W/B0176, Groups 54, 79 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 217 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 54, 79: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 3 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Identification Tape 289T1144-10211 1 SWPM 20-10-11 14 Wire 289T1144-102W 1 SWPM 20-10-11 15 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 90: P36 Panel - Wiring Changes W/B0176, Group 66 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 218 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 90: P36 Panel - Wiring Changes W/B0176, Group 66 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 YC10 TB216 4

4

6
K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218 YC5

7 J D4672P 18 85W-24 02H-22 02H-22 YA5 TB218 2

2 5 3 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

5 10

8 7

TB74 YA13 51

K329 OVRD PUMP CONT RLY L FUEL X1 75W-22 53E-24 75W-22 53E-24 XD3 50
D5658P TB218 53C-22 53C-22 W184
6
3 02F-24 J 4 D5658P 02F-24 TB216

YA10 TB218

XB12 6 9 W184

W184 2 (11 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) 11 12 AE0223

AE0209D59744



### (SHEET 1 OF 2)

### FIGURE 90: P36 Panel - Wiring Changes W/B0176, Group 66 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 219 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 66: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 11 SWPM 20-90-11 See note (a) 3 Terminal Lug BACT12AR222 1 SWPM 20-30-11 4 Relay Socket BACS16AH1 1 SWPM 20-81-22 5 Relay Socket BACS16AG1 1 SWPM 20-81-22 6 Pin BACC47CN1S 4 SWPM 20-61-11 7 Identification Tape 289T1144-10202 1 SWPM 20-10-11 8 Identification Tape 289T1144-10203 1 SWPM 20-10-11 9 Identification Tape 289T1144-10209 1 SWPM 20-10-11 10 Identification Tape 289T1144-10210 1 SWPM 20-10-11 11 Wire 289T1144-102W 1 SWPM 20-10-11 12 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 91: P36 Panel - Wiring Changes W/B0176, Groups 44, 72, 74 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 220 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 91: P36 Panel - Wiring Changes W/B0176, Groups 44, 72, 74 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184

5

7
K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218 YC5

7

TB74 J D4672P 18

YA13 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YA5 TB218 W184 TB218 02F-24

2

2 5 3

B1 XC12

7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 11

10 9 8 3 (11 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) 13 14 AE0223

AE0209D59747



### (SHEET 1 OF 2)

### FIGURE 91: P36 Panel - Wiring Changes W/B0176, Groups 44, 72, 74 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 221 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 44, 72, 74: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 11 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 2 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Wire 289T1144-102W 1 SWPM 20-10-11 14 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 92: P36 Panel - Wiring Changes W/B0176, Group 62 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 222 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 92: P36 Panel - Wiring Changes W/B0176, Group 62 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184

5

7
K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218 YA9

7

TB74 J D4672P 18

YA13 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YA7 TB218 W184 TB218 02F-24

2

2 5 3

B1 XB12

7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 11

10 9 8 3 (11 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) 13 14 AE0223

AE0209D59750



### (SHEET 1 OF 2)

### FIGURE 92: P36 Panel - Wiring Changes W/B0176, Group 62 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 223 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 62: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 11 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 2 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Wire 289T1144-102W 1 SWPM 20-10-11 14 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 93: P36 Panel - Wiring Changes W/B0176, Groups 41, 43, 64 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 224 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 93: P36 Panel - Wiring Changes W/B0176, Groups 41, 43, 64 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184

5

7
K10691 L/H HOLD RELAY D11629 TB216 Z19 TB218 YC5

7

TB74 J D4672P 18

YA13 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YA5 TB218 W184 TB218 02F-24

2

2 5 3

B1 XB12

7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 11

10 9 8 3 (11 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) 13 14 AE0223

AE0209D59751



### (SHEET 1 OF 2)

### FIGURE 93: P36 Panel - Wiring Changes W/B0176, Groups 41, 43, 64 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 225 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 41, 43, 64: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 11 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 2 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Wire 289T1144-102W 1 SWPM 20-10-11 14 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 94: P36 Panel - Wiring Changes W/B0176, Group 69 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 226 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 94: P36 Panel - Wiring Changes W/B0176, Group 69 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184

5

7
K10691 L/H HOLD RELAY D11629 TB216 Z19 TB218 YA9

7

TB74 J D4672P 18

YA13 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YA7 TB218 W184 TB218 02F-24

2

2 5 3

B1 XB12

7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 11

10 9 8 3 (11 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) 13 14 AE0223

AE0209D59754



### (SHEET 1 OF 2)

### FIGURE 94: P36 Panel - Wiring Changes W/B0176, Group 69 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 227 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 69: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 11 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 2 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Wire 289T1144-102W 1 SWPM 20-10-11 14 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 95: P36 Panel - Wiring Changes W/B0176, Group 61 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 228 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 95: P36 Panel - Wiring Changes W/B0176, Group 61 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184

5

7
K10691 L/H HOLD RELAY D11629 TB318 Z9 TB218 YC14

7

TB74 J D4672P 18

YA13 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YA14 TB218 W184 TB218 02F-24

2

2 5 3

B1 XB12

7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 11

10 9 8 3 (11 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) 13 14 AE0223

AE0209D59756



### (SHEET 1 OF 2)

### FIGURE 95: P36 Panel - Wiring Changes W/B0176, Group 61 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 229 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 61: This Figure applies to REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 11 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 2 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Wire 289T1144-102W 1 SWPM 20-10-11 14 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 96: P36 Panel - Wiring Changes W/B0176, Group 70 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 230 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 96: P36 Panel - Wiring Changes W/B0176, Group 70 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184

5

7
K10691 L/H HOLD RELAY D11629 TB318 Z9 TB218 YC5

7

TB74 J D4672P 18

YA13 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YA5 TB218 W184 TB218 02F-24

2

2 5 3

B1 XB12

7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 11

10 9 8 3 (11 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) 13 14 AE0223

AE0209D59759



### (SHEET 1 OF 2)

### FIGURE 96: P36 Panel - Wiring Changes W/B0176, Group 70 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 231 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 70: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 11 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 2 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Wire 289T1144-102W 1 SWPM 20-10-11 14 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 97: P36 Panel - Wiring Changes W/B0176, Groups 73, 75 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 232 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 97: P36 Panel - Wiring Changes W/B0176, Groups 73, 75 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184

5

7
K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218 YC5

7

TB218 J D4672P 18

YA20 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YA5 TB218 W184 TB218 02F-24

2

2 5 3

B1 XC12

7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 11

10 9 8 3 (11 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) 13 14 AE0223

AE0209D59763



### (SHEET 1 OF 2)

### FIGURE 97: P36 Panel - Wiring Changes W/B0176, Groups 73, 75 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 233 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 73, 75: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 11 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 2 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Wire 289T1144-102W 1 SWPM 20-10-11 14 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 98: P36 Panel - Wiring Changes W/B0176, Group 56 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 234 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 98: P36 Panel - Wiring Changes W/B0176, Group 56 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184

5

7
K10691 L/H HOLD RELAY D11629 TB216 Z8 TB218 YA20

7

TB218 J D4672P 18

YA20 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YC20 TB218 W184 TB218 02F-24

2

2 5 3

B1 XC4

7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 11

10 9 8 3 (11 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 13 14D59988



### (SHEET 1 OF 2)

### FIGURE 98: P36 Panel - Wiring Changes W/B0176, Group 56 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 235 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 56: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 11 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 2 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Wire 289T1144-102W 1 SWPM 20-10-11 14 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 99: P36 Panel - Wiring Changes W/B0176, Group 71 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 236 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 99: P36 Panel - Wiring Changes W/B0176, Group 71 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184

5

7
K10691 L/H HOLD RELAY D11629 TB216 Z9 TB218 YC5

7

TB218 J D4672P 18

YA20 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YA5 TB218 W184 02F-24

2

2 5 3

B1 XB12

7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 11

10 9 8 3 (11 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) TB218 AE0223

AE0209 13 14D59991



### (SHEET 1 OF 2)

### FIGURE 99: P36 Panel - Wiring Changes W/B0176, Group 71 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 237 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 71: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 11 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 2 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Wire 289T1144-102W 1 SWPM 20-10-11 14 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 100: P36 Panel - Wiring Changes W/B0176, Group 65 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 238 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 100: P36 Panel - Wiring Changes W/B0176, Group 65 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184

5

7
K10691 L/H HOLD RELAY D11629 TB216 Z19 TB218 YA9

7

TB218 J D4672P 18

YA20 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YA7 TB218 W184 TB218 02F-24

2

2 5 3

B1 XB12

7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 11

10 9 8 3 (11 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 13 14D59993



### (SHEET 1 OF 2)

### FIGURE 100: P36 Panel - Wiring Changes W/B0176, Group 65 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 239 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 65: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 11 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 2 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Wire 289T1144-102W 1 SWPM 20-10-11 14 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 101: P36 Panel - Wiring Changes W/B0176, Group 63 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 240 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 101: P36 Panel - Wiring Changes W/B0176, Group 63 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184

5

7
K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218 YA9

7

TB218 J D4672P 18

YA20 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YA7 TB218 W184 TB218 02F-24

2

2 5 3

B1 XB12

7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 11

10 9 8 3 (11 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 13 14D59995



### (SHEET 1 OF 2)

### FIGURE 101: P36 Panel - Wiring Changes W/B0176, Group 63 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 241 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 63: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 11 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 2 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Wire 289T1144-102W 1 SWPM 20-10-11 14 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 102: P36 Panel - Wiring Changes W/B0176, Groups 52-53, 78 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 242 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 102: P36 Panel - Wiring Changes W/B0176, Groups 52-53, 78 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184

5

7
K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218 YA20

7

TB218 J D4672P 18

YA20 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YC20 TB218 W184 TB218 02F-24

2

2 5 3

B1 XB12

7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 11

10 9 8 3 (11 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 13 14D59996



### (SHEET 1 OF 2)

### FIGURE 102: P36 Panel - Wiring Changes W/B0176, Groups 52-53, 78 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 243 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 52-53, 78: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 11 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 2 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Wire 289T1144-102W 1 SWPM 20-10-11 14 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 103: P36 Panel - Wiring Changes W/B0176, Groups 46-48, 50-51, 58, 60, 77 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 244 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 103: P36 Panel - Wiring Changes W/B0176, Groups 46-48, 50-51, 58, 60, 77 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184

5

7
K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218 YC5

7

TB218 J D4672P 18

YA20 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YA5 TB218 W184 TB218 02F-24

2

2 5 3

B1 XB12

7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 11

10 9 8 3 (11 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) 13 14 AE0223

AE0209D59998



### (SHEET 1 OF 2)

### FIGURE 103: P36 Panel - Wiring Changes W/B0176, Groups 46-48, 50-51, 58, 60, 77 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 245 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 46-48, 50-51, 58, 60, 77: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 11 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 2 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Wire 289T1144-102W 1 SWPM 20-10-11 14 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 104: P36 Panel - Wiring Changes W/B0176, Groups 45, 57, 59 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 246 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 104: P36 Panel - Wiring Changes W/B0176, Groups 45, 57, 59 Airplanes.**

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4 D5658P TB216

YA10

YC10 TB216 4

W184

5

7
K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218 YC5

7

TB74 J D4672P 18

YA13 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YA5 TB218 W184 TB218 02F-24

2

2 5 3

B1 XB12

7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 11

10 9 8 3 (11 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223

AE0209 13 14D60028



### (SHEET 1 OF 2)

### FIGURE 104: P36 Panel - Wiring Changes W/B0176, Groups 45, 57, 59 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 247 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 45, 57, 59: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 11 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 2 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Wire 289T1144-102W 1 SWPM 20-10-11 14 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 105: P36 Panel - Wiring Changes W/B0184, Group 61 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 248 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 105: P36 Panel - Wiring Changes W/B0184, Group 61 Airplanes.**

This Figure applies to Group 61: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YC14 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P

TB218 XD3 J 5 D8026P 10D-22 1

6 2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XB12 02K-24 2 W590 2 5

YA14 TB218 W176 10D-22 2

REFERENCE: 767 WIRING DIAGRAM 28-22-12, 28-42-12 11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60029



### (SHEET 1 OF 2)

### FIGURE 105: P36 Panel - Wiring Changes W/B0184, Group 61 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 249 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.

**(SHEET 2 OF 2)**

### FIGURE 106: P36 Panel - Wiring Changes W/B0184, Groups 62-63 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 250 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 106: P36 Panel - Wiring Changes W/B0184, Groups 62-63 Airplanes.**

This Figure applies to Group 62-63: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YA9 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P

TB218 XD3 J 5 D8026P 10D-22 1

6 2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XB12 02K-24 2 W590 2

YA7 TB218 W176 10D-22 2

REFERENCE: 767 WIRING DIAGRAM 28-22-12, 28-42-12 5 11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60266



### (SHEET 1 OF 2)

### FIGURE 106: P36 Panel - Wiring Changes W/B0184, Groups 62-63 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 251 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.

**(SHEET 2 OF 2)**

### FIGURE 107: P36 Panel - Wiring Changes W/B0184, Group 56 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 252 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 107: P36 Panel - Wiring Changes W/B0184, Group 56 Airplanes.**

This Figure applies to Group 56: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YA20 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P

TB218 XD3 J 5 D8026P 10D-22 1

6 2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XC4 02K-24 13 W590 2

YC20 TB218 W176 10D-22 2

REFERENCE: 767 WIRING DIAGRAM 28-22-12, 28-42-12 5 11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60318



### (SHEET 1 OF 2)

### FIGURE 107: P36 Panel - Wiring Changes W/B0184, Group 56 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 253 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.

**(SHEET 2 OF 2)**

### FIGURE 108: P36 Panel - Wiring Changes W/B0184, Groups 44, 72-75 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 254 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 108: P36 Panel - Wiring Changes W/B0184, Groups 44, 72-75 Airplanes.**

This Figure applies to Group 44, 72-75: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YC5 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P

TB218 XD3 J 5 D8026P 10D-22 1

6 2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XC12 02K-24 13 W590 2

YA5 TB218 W176 10D-22 2

REFERENCE: 767 WIRING DIAGRAM 28-22-12, 28-42-12 5 11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60319



### (SHEET 1 OF 2)

### FIGURE 108: P36 Panel - Wiring Changes W/B0184, Groups 44, 72-75 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 255 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.

**(SHEET 2 OF 2)**

### FIGURE 109: P36 Panel - Wiring Changes W/B0184, Groups 65, 69 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 256 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 109: P36 Panel - Wiring Changes W/B0184, Groups 65, 69 Airplanes.**

This Figure applies to Group 65, 69: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YA9 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P

TB218 XD3 J 5 D8026P 10D-22 1

6 2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XB12 02K-24 13 W590 2

YA7 TB218 W176 10D-22 2

REFERENCE: 767 WIRING DIAGRAM 28-22-12, 28-42-12 5 11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60320



### (SHEET 1 OF 2)

### FIGURE 109: P36 Panel - Wiring Changes W/B0184, Groups 65, 69 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 257 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.

**(SHEET 2 OF 2)**

### FIGURE 110: P36 Panel - Wiring Changes W/B0184, Groups 52-53, 78 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 258 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 110: P36 Panel - Wiring Changes W/B0184, Groups 52-53, 78 Airplanes.**

This Figure applies to Group 52-53, 78: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YA20 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P

TB218 XD3 J 5 D8026P 10D-22 1

6 2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XB12 02K-24 13 W590 2

YC20 TB218 W176 10D-22 2

REFERENCE: 767 WIRING DIAGRAM 28-22-12, 28-42-12 5 11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60321



### (SHEET 1 OF 2)

### FIGURE 110: P36 Panel - Wiring Changes W/B0184, Groups 52-53, 78 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 259 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.

**(SHEET 2 OF 2)**

### FIGURE 111: P36 Panel - Wiring Changes W/B0184, Groups 40-41, 43, 45-48, 50-51, 57-60, 64, 66, 70- **71, 77 Airplanes.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 260 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 111: P36 Panel - Wiring Changes W/B0184, Groups 40-41, 43, 45-48, 50-51, 57-60, 64, 66, 70-71, 77 Airplanes.** 

This Figure applies to Group 40-41, 43, 45-48, 50-51, 57-60, 64, 66, 70-71, 77: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YC5 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P

TB218 XD3 J 5 D8026P 10D-22 1

6 2 3 7

4 8

5 9 AE0209

22 D4856P W176 TB218 XB12 02K-24 13 W590 2

YA5 TB218 W176 10D-22 2

REFERENCE: 767 WIRING DIAGRAM 28-22-12, 28-42-12 5 11 10

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60322



### (SHEET 1 OF 2)

### FIGURE 111: P36 Panel - Wiring Changes W/B0184, Groups 40-41, 43, 45-48, 50-51, 57-60, 64, 66, 70- **71, 77 Airplanes.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 261 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACC47CN1S 2 SWPM 20-61-11 See spares kit 289T1144-201 for additional contact if required. 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.

**(SHEET 2 OF 2)**

### FIGURE 112: P36 Panel - Wiring Changes W/B0184, Groups 54-55, 79 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 262 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 112: P36 Panel - Wiring Changes W/B0184, Groups 54-55, 79 Airplanes.**

This Figure applies to Group 54-55, 79: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YA20 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P

TB218 XD3 J 5 D8026P 10D-22 1

6 2 3 7

4 8

5 9 AE0209 22 D4856P

YC20 TB218 W176 10D-22 2

REFERENCE: 767 WIRING DIAGRAM 28-22-12, 28-42-12 11 10D60323 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 2)

### FIGURE 112: P36 Panel - Wiring Changes W/B0184, Groups 54-55, 79 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 263 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 2 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACC47CN1S 1 SWPM 20-30-11 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.

**(SHEET 2 OF 2)**

### FIGURE 113: P36 Panel - Wiring Changes W/B0184, Groups 42, 49, 67-68, 76, 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 264 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 113: P36 Panel - Wiring Changes W/B0184, Groups 42, 49, 67-68, 76, 88 Airplanes.**

This Figure applies to Group 42, 49, 67-68, 76, 88: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K633 OVERRIDE PUMP GROUND ENABLE RELAY D10068 5 J 

# W184
763-24 767-24 TB216

YA10 763-24

YC5 TB218

YC10 TB216 W176 768-24 768-24 J 42 D4992P

TB218 XD3 J 5 D8026P 10D-22 1

6 2 3 7

4 8

5 9 AE0209 22 D4856P

YA5 TB218 W176 10D-22 2

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12

11 10D60324 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 2)

### FIGURE 113: P36 Panel - Wiring Changes W/B0184, Groups 42, 49, 67-68, 76, 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 265 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **NOTE:** Use the parts from wire kit 289T1144-103. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 1 SWPM 20-81-19 2 Contact M39029/11-145 2 SWPM 20-90-11 See note (a) 3 Contact BACC47CN2 1 SWPM 20-61-11 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACC47CN1S 1 SWPM 20-30-11 6 Identification Tape 289T1144-10302 1 SWPM 20-10-11 7 Identification Tape 289T1144-10305 1 SWPM 20-10-11 8 Identification Tape 289T1144-10306 1 SWPM 20-10-11 9 Identification Tape 289T1144-10307 1 SWPM 20-10-11 10 Wire 289T1144-103W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10301 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.

**(SHEET 2 OF 2)**

### FIGURE 114: P36 Panel - Relay Installation, Groups 40-79, 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 266 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 114: P36 Panel - Relay Installation, Groups 40-79, 88 Airplanes.**



### P36 PANEL


### MAIN EQUIPMENT CENTER

A
A

FWD FWDJ82100



### (SHEET 1 OF 2)

### FIGURE 114: P36 Panel - Relay Installation, Groups 40-79, 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 267 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 40-79, 88: The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY numbers shown below are the number of parts necessary for each airplane. Use parts from Top Kit 015T1775- 3 (Groups 40-79, 88). **STEP TASK NAME IDENTIFICATION QTY MORE DATA** 1 Install Relay BACR13CD2 1 -- 2 Install Relay TDH-1852-1402 1 --K10693K10691



### UP FWD 

### A-A 1 2J82099



### (SHEET 2 OF 2)

### FIGURE 115: P37 Panel - Wiring Changes W/B0188, Group 55 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 268 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 115: P37 Panel - Wiring Changes W/B0188, Group 55 Airplanes.**

This Figure applies to Group 55: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-104. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact M39029/11-145 4 SWPM 20-90-11 See note (a) 2 Contact BACC47CN1S 2 SWPM 20-61-11 3 Contact BACC47CP1S 2 SWPM 20-61-11 4 Identification Tape 289T1144-10402 1 SWPM 20-10-11 5 Identification Tape 289T1144-10403 1 SWPM 20-10-11 6 Identification Tape 289T1144-10404 1 SWPM 20-10-11 6 4

5

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL AE0218

W192 Z20 TB212
W192 YC14 TB304

W192 YC12 TB212 J 22 D5330P

J 3 D5506P

J 5 D5372P

J 15 D7352P W942 

# W188 074-22

075-22

073-24

14A-24 1 074-22

075-22

073-24 1 2

2

3

3 7 REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 8 9D60325 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 2)

### FIGURE 115: P37 Panel - Wiring Changes W/B0188, Group 55 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 269 of 339 

### BOEING SERVICE BULLETIN 767-28A0083
7 Identification Tape 289T1144-10406 1 SWPM 20-10-11 8 Wire 289T1144-104W 1 SWPM 20-10-11 9 Lacing Tape 289T1144-10401 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 116: P37 Panel - Wiring Changes W/B0188, Groups 40-45, 57, 59, 64, 66, 68-70, 72, 74, 76 Air**planes.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 270 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 116: P37 Panel - Wiring Changes W/B0188, Groups 40-45, 57, 59, 64, 66, 68-70, 72, 74, 76 Airplanes.** 

This Figure applies to Group 40-45, 57, 59, 64, 66, 68-70, 72, 74, 76: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-104. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 2 Contact BACC47CN1S 2 SWPM 20-61-11 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Identification Tape 289T1144-10402 1 SWPM 20-10-11 5 Identification Tape 289T1144-10403 1 SWPM 20-10-11 6 Identification Tape 289T1144-10405 1 SWPM 20-10-11 6 4

5

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL AE0218

W192 TB212
W192 YC14 TB304 J 22 D5330P

J 3 D5506P

J 5 D5372P 

# W188 074-22

075-22

073-24 1 074-22

075-22

073-24

2

2

3 Z19

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 7 8D60538 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 2)

### FIGURE 116: P37 Panel - Wiring Changes W/B0188, Groups 40-45, 57, 59, 64, 66, 68-70, 72, 74, 76 Air**planes.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 271 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

7 Wire 289T1144-104W 1 SWPM 20-10-11 8 Lacing Tape 289T1144-10401 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 117: P37 Panel - Wiring Changes W/B0188, Groups 46-53, 58, 60, 65, 67, 71, 73, 75, 77-79, 88 **Airplanes.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 272 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 117: P37 Panel - Wiring Changes W/B0188, Groups 46-53, 58, 60, 65, 67, 71, 73, 75, 77-79, 88 Airplanes.** 

This Figure applies to Group 46-53, 58, 60, 65, 67, 71, 73, 75, 77-79, 88: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. 6 4

5

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL AE0218

W192 TB212
W192 YC14 TB304 J 22 D5330P

J 3 D5506P

J 5 D5372P 

# W188 074-22

075-22

073-24 1 074-22

075-22

073-24

2

2

3 Z19

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 7 8D60540 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 2)

### FIGURE 117: P37 Panel - Wiring Changes W/B0188, Groups 46-53, 58, 60, 65, 67, 71, 73, 75, 77-79, 88 **Airplanes.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 273 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **NOTE:** Use the parts from wire kit 289T1144-104. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 2 Contact BACC47CN1S 2 SWPM 20-61-11 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Identification Tape 289T1144-10402 1 SWPM 20-10-11 5 Identification Tape 289T1144-10403 1 SWPM 20-10-11 6 Identification Tape 289T1144-10404 1 SWPM 20-10-11 7 Wire 289T1144-104W 1 SWPM 20-10-11 8 Lacing Tape 289T1144-10401 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.

**(SHEET 2 OF 2)**

### FIGURE 118: P37 Panel - Wiring Changes W/B0188, Groups 54, 56 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 274 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 118: P37 Panel - Wiring Changes W/B0188, Groups 54, 56 Airplanes.**

This Figure applies to Group 54, 56: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-104. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 2 Contact BACC47CN1S 2 SWPM 20-61-11 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Identification Tape 289T1144-10402 1 SWPM 20-10-11 6 4

5

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL AE0218

W192 TB212
W192 YC14 TB304 J 22 D5330P

J 3 D5506P

J 5 D5372P 

# W188 074-22

075-22

073-24 1 074-22

075-22

073-24

2

2

3 Z20

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 7 8D60543 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 2)

### FIGURE 118: P37 Panel - Wiring Changes W/B0188, Groups 54, 56 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 275 of 339 

### BOEING SERVICE BULLETIN 767-28A0083
5 Identification Tape 289T1144-10403 1 SWPM 20-10-11 6 Identification Tape 289T1144-10404 1 SWPM 20-10-11 7 Wire 289T1144-104W 1 SWPM 20-10-11 8 Lacing Tape 289T1144-10401 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 119: P37 Panel - Wiring Changes W/B0188, Groups 61-62 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 276 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 119: P37 Panel - Wiring Changes W/B0188, Groups 61-62 Airplanes.**

This Figure applies to Group 61-62: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-104. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 2 Contact BACC47CN1S 2 SWPM 20-61-11 3 Contact BACC47CP1S 2 SWPM 20-61-11 4 Identification Tape 289T1144-10402 1 SWPM 20-10-11 5 Identification Tape 289T1144-10403 1 SWPM 20-10-11 6 Identification Tape 289T1144-10405 1 SWPM 20-10-11 7 Wire 289T1144-104W 1 SWPM 20-10-11 8 Lacing Tape 289T1144-10401 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 6 4

5

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL AE0218

W192 TB274
W192 YC14 TB304 J 22 D5330P

J 3 D5506P

J 5 D5372P 

# W188 074-22

075-22

073-24 1 074-22

075-22

073-24

2

2

3 Z2

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 7 8D60547 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 120: P37 Panel - Wiring Changes W/B0188, Group 63 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 277 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 120: P37 Panel - Wiring Changes W/B0188, Group 63 Airplanes.**

This Figure applies to Group 63: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-104. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 2 Contact BACC47CN1S 2 SWPM 20-61-11 3 Contact BACC47CP1S 1 SWPM 20-61-11 4 Identification Tape 289T1144-10402 1 SWPM 20-10-11 5 Identification Tape 289T1144-10403 1 SWPM 20-10-11 6 Identification Tape 289T1144-10404 1 SWPM 20-10-11 6 4

5

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL AE0218

W192 TB274
W192 YC14 TB304 J 22 D5330P

J 3 D5506P

J 5 D5372P 

# W188 074-22

075-22

073-24 1 074-22

075-22

073-24

2

2

3 Z2

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 7 8D60550 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 2)

### FIGURE 120: P37 Panel - Wiring Changes W/B0188, Group 63 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 278 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

7 Wire 289T1144-104W 1 SWPM 20-10-11 8 Lacing Tape 289T1144-10401 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 121: P37 Panel - Wiring Changes W/B0192, Group 61 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 279 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 121: P37 Panel - Wiring Changes W/B0192, Group 61 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10692 R/H TIME DELAY

W198 D31186

AE0218

2 

# W192

79H-24

63E-24 YA3 TB82 4 3

10 4

7 K10690 R/H HOLD RELAY D31184 TB274 Z1 TB274 Z2 7

TB82 

### J D4284P 12

YC3 79X-24 004-24

C1 K2090 W188

K330 OVRD PUMP R FUEL X1 D12158 RIGHT 78U-24 004-24

YC14 YA11 TB190

W188 2

2 5 3

TB304 7 79J-24

3 79G-24 79Q-24 79B-24

JETTISON RLY B1 79V-24

63E-24 63C-22 1

6

5 8

11 1

63C-22 9

CONT RLY (4 LOCATIONS)

(4 LOCATIONS) (10 LOCATIONS) 12 13D60553



### (SHEET 1 OF 2)

### FIGURE 121: P37 Panel - Wiring Changes W/B0192, Group 61 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 280 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 61: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-19 3 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACT12AR222 1 SWPM 20-30-11 6 Relay Socket BACS16AH1 1 SWPM 20-81-22 7 Relay Socket BACS16AG1 1 SWPM 20-81-22 8 Identification Tape 289T1144-10502 1 SWPM 20-10-11 9 Identification Tape 289T1144-10503 1 SWPM 20-10-11 10 Identification Tape 289T1144-10504 1 SWPM 20-10-11 11 Identification Tape 289T1144-10505 1 SWPM 20-10-11 12 Wire 289T1144-105W 1 SWPM 20-10-11 13 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 122: P37 Panel - Wiring Changes W/B0192, Group 62 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 281 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 122: P37 Panel - Wiring Changes W/B0192, Group 62 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10692 R/H TIME DELAY

W198 D31186

AE0218 

# W192

79H-24

63E-24 YA3 TB82 4

10 4

7 K10690 R/H HOLD RELAY D31184 TB274 Z1 TB274 Z2 7

TB82 

### J D4284P 12

YC3 79X-24 004-24

C1 K2090 W188

K330 OVRD PUMP R FUEL X1 D12158 RIGHT 78U-24 004-24

YC14 YC11 TB212

W188 2

2 5 3

TB304 7 79J-24

3 79G-24 79Q-24 79B-24

JETTISON RLY B1 79V-24

63E-24 63C-22 1

6

5 8

11 1

63C-22 9

CONT RLY (4 LOCATIONS)

(4 LOCATIONS)

2 3 (10 LOCATIONS) 12 13D60642



### (SHEET 1 OF 2)

### FIGURE 122: P37 Panel - Wiring Changes W/B0192, Group 62 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 282 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 62: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-19 3 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACT12AR222 1 SWPM 20-30-11 6 Relay Socket BACS16AH1 1 SWPM 20-81-22 7 Relay Socket BACS16AG1 1 SWPM 20-81-22 8 Identification Tape 289T1144-10502 1 SWPM 20-10-11 9 Identification Tape 289T1144-10503 1 SWPM 20-10-11 10 Identification Tape 289T1144-10504 1 SWPM 20-10-11 11 Identification Tape 289T1144-10505 1 SWPM 20-10-11 12 Wire 289T1144-105W 1 SWPM 20-10-11 13 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 123: P37 Panel - Wiring Changes W/B0192, Groups 41, 43-45, 57, 59, 64, 69-70, 72, 74, Air**planes.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 283 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 123: P37 Panel - Wiring Changes W/B0192, Groups 41, 43-45, 57, 59, 64, 69-70, 72, 74, Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10692 R/H TIME DELAY

W198 D31186

AE0218 

# W192

79H-24

63E-24 YA3 TB82 4

10 4

7 K10690 R/H HOLD RELAY D31184 TB212 Z17 TB212 Z19 7

TB82 

### J D4284P 12

YC3 79X-24 004-24

C1 K2090 W188

K330 OVRD PUMP R FUEL X1 D12158 RIGHT 78U-24 004-24

YC14 YA7 TB212

W188 2

2 5 3

TB304 7 79J-24

3 79G-24 79Q-24 79B-24

JETTISON RLY B1 79V-24

63E-24 63C-22 1

6

5 8

11 1

63C-22 9

CONT RLY (4 LOCATIONS)

(4 LOCATIONS)

2 3 (10 LOCATIONS) 12 13D60557



### (SHEET 1 OF 2)

### FIGURE 123: P37 Panel - Wiring Changes W/B0192, Groups 41, 43-45, 57, 59, 64, 69-70, 72, 74, Air**planes.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 284 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 41, 43-45, 57, 59, 64, 69-70, 72, 74: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-19 3 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACT12AR222 1 SWPM 20-30-11 6 Relay Socket BACS16AH1 1 SWPM 20-81-22 7 Relay Socket BACS16AG1 1 SWPM 20-81-22 8 Identification Tape 289T1144-10502 1 SWPM 20-10-11 9 Identification Tape 289T1144-10503 1 SWPM 20-10-11 10 Identification Tape 289T1144-10504 1 SWPM 20-10-11 11 Identification Tape 289T1144-10505 1 SWPM 20-10-11 12 Wire 289T1144-105W 1 SWPM 20-10-11 13 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 124: P37 Panel - Wiring Changes W/B0192, Groups 42, 67-68, 76 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 285 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 124: P37 Panel - Wiring Changes W/B0192, Groups 42, 67-68, 76 Airplanes.**

TB212

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10692 R/H TIME DELAY

W1118 D31186

AE0218 

# W192

79H-24

63E-24 YA3 TB82 4

10 4

7 K10690 R/H HOLD RELAY D31184 TB212 Z17 Z19 7

TB82 

### J D4284P 12

YC3 79X-24 004-24

C1 K2090 W188

K330 OVRD PUMP R FUEL X1 D12158 RIGHT 78U-24 004-24

YC14 YA7 TB212

W188 2

2 5 3

TB304 7 79J-24

3 79G-24 79Q-24 79B-24

JETTISON RLY B1 79V-24

63E-24 63C-22 6

5 8

11 1

63C-22 9

CONT RLY (4 LOCATIONS) 1 (4 LOCATIONS)

2 3 (10 LOCATIONS)

W198-188-24 12 13D60558



### (SHEET 1 OF 2)

### FIGURE 124: P37 Panel - Wiring Changes W/B0192, Groups 42, 67-68, 76 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 286 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 42, 67-68, 76: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-19 3 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACT12AR222 1 SWPM 20-30-11 6 Relay Socket BACS16AH1 1 SWPM 20-81-22 7 Relay Socket BACS16AG1 1 SWPM 20-81-22 8 Identification Tape 289T1144-10502 1 SWPM 20-10-11 9 Identification Tape 289T1144-10503 1 SWPM 20-10-11 10 Identification Tape 289T1144-10504 1 SWPM 20-10-11 11 Identification Tape 289T1144-10505 1 SWPM 20-10-11 12 Wire 289T1144-105W 1 SWPM 20-10-11 13 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 125: P37 Panel - Wiring Changes W/B0192, Groups 40, 66 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 287 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 125: P37 Panel - Wiring Changes W/B0192, Groups 40, 66 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL 

# W192

K10692 R/H TIME DELAY

W198 D31186 79H-24

63E-24 YA3 TB82 4

8 3

6 K10690 R/H HOLD RELAY D31184 TB212 Z17 TB212 Z19 7

TB82 J D4284P 12

YC3 79X-24 004-24 W188 AE0218

K330 OVRD PUMP CONT RLY R FUEL X1 004-24

W188 11 7 YC14 YA7 TB212 2

2 5 3

TB304 7 79J-24

3 79G-24 79Q-24 79B-24

79V-24

63E-24 63C-22 5

4 7

9 1

63C-22

78U-24 (3 LOCATIONS) (4 LOCATIONS) 1 (4 LOCATIONS) 2 (10 LOCATIONS) 10 11D60562



### (SHEET 1 OF 2)

### FIGURE 125: P37 Panel - Wiring Changes W/B0192, Groups 40, 66 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 288 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 40, 66: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 3 Contact BACC47CP1S 3 SWPM 20-61-11 4 Contact BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Identification Tape 289T1144-10502 1 SWPM 20-10-11 8 Identification Tape 289T1144-10503 1 SWPM 20-10-11 9 Identification Tape 289T1144-10505 1 SWPM 20-10-11 10 Wire 289T1144-105W 1 SWPM 20-10-11 11 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 126: P37 Panel - Wiring Changes W/B0192, Group 55 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 289 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 126: P37 Panel - Wiring Changes W/B0192, Group 55 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10692 R/H TIME DELAY

W188 D31186

AE0218

78U-24 

# W192

79H-24

63E-24 YA12 TB212 4

10 4
11 K10690 R/H HOLD RELAY D31184 TB212 Z19 TB212 Z20 7

TB212 J D4284P 12

YA14 79X-24 004-24

C1 K2090 W188

K330 OVRD PUMP CONT RLY R FUEL X1 D12158 RIGHT 78U-24 004-24

YC14 YC12 TB212

W188 2

2 5 3

TB304 7 79J-24

3 79G-24 79Q-24 79B-24

JETTISON RLY B1 79V-24

63E-24 63C-22 9

5 7 8 1

63C-22 6 (4 LOCATIONS) 1 (4 LOCATIONS)

2 3 (10 LOCATIONS) 12 13D60564



### (SHEET 1 OF 2)

### FIGURE 126: P37 Panel - Wiring Changes W/B0192, Group 55 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 290 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 55: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-19 3 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACT12AR222 1 SWPM 20-30-11 6 Relay Socket BACS16AH1 1 SWPM 20-81-22 7 Relay Socket BACS16AG1 1 SWPM 20-81-22 8 Identification Tape 289T1144-10502 1 SWPM 20-10-11 9 Identification Tape 289T1144-10503 1 SWPM 20-10-11 10 Identification Tape 289T1144-10504 1 SWPM 20-10-11 11 Identification Tape 289T1144-10505 1 SWPM 20-10-11 12 Wire 289T1144-105W 1 SWPM 20-10-11 13 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 127: P37 Panel - Wiring Changes W/B0192, Group 56 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 291 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 127: P37 Panel - Wiring Changes W/B0192, Group 56 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10692 R/H TIME DELAY

W188 D31186

AE0218

78U-24 

# W192

79H-24

63E-24 YA12 TB212 4

10 4
11 K10690 R/H HOLD RELAY D31184 TB212 Z19 TB212 Z20 7

TB212 J D4284P 12

YA14 79X-24 004-24

C1 K2090 W188

K330 OVRD PUMP CONT RLY R FUEL X1 D12158 RIGHT 78U-24 004-24

YC14 YC12 TB212

W188 2

2 5 3

TB304 7 79J-24

3 79G-24 79Q-24 79B-24

JETTISON RLY B1 79V-24

63E-24 63C-22 9

5 7 8 1

63C-22 6 (4 LOCATIONS) 1 (4 LOCATIONS)

2 3 (10 LOCATIONS) 12 13D60566



### (SHEET 1 OF 2)

### FIGURE 127: P37 Panel - Wiring Changes W/B0192, Group 56 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 292 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 56: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-19 3 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACT12AR222 1 SWPM 20-30-11 6 Relay Socket BACS16AH1 1 SWPM 20-81-22 7 Relay Socket BACS16AG1 1 SWPM 20-81-22 8 Identification Tape 289T1144-10502 1 SWPM 20-10-11 9 Identification Tape 289T1144-10503 1 SWPM 20-10-11 10 Identification Tape 289T1144-10504 1 SWPM 20-10-11 11 Identification Tape 289T1144-10505 1 SWPM 20-10-11 12 Wire 289T1144-105W 1 SWPM 20-10-11 13 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 128: P37 Panel - Wiring Changes W/B0192, Group 54 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 293 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 128: P37 Panel - Wiring Changes W/B0192, Group 54 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10692 R/H TIME DELAY

W1118 D31186

AE0218

78U-24 

# W192

79H-24

63E-24 YA12 TB212 4

10 4

11 K10690 R/H HOLD RELAY D31184 TB212 Z19 TB212 Z20 7

TB212 J D4284P 12

YA14 79X-24 004-24

C1 K2090 W188

K330 OVRD PUMP CONT RLY R FUEL X1 D12158 RIGHT 78U-24 004-24

YC14 YC12 TB212

W188 2

2 5 3

TB304 7 79J-24

3 79G-24 79Q-24 79B-24

JETTISON RLY B1 79V-24

63E-24 63C-22 9

5 7 8 1

63C-22 6 (4 LOCATIONS) 1 (4 LOCATIONS)

2 3 (10 LOCATIONS) 12 13D60568



### (SHEET 1 OF 2)

### FIGURE 128: P37 Panel - Wiring Changes W/B0192, Group 54 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 294 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 54: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-19 3 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACT12AR222 1 SWPM 20-30-11 6 Relay Socket BACS16AH1 1 SWPM 20-81-22 7 Relay Socket BACS16AG1 1 SWPM 20-81-22 8 Identification Tape 289T1144-10502 1 SWPM 20-10-11 9 Identification Tape 289T1144-10503 1 SWPM 20-10-11 10 Identification Tape 289T1144-10504 1 SWPM 20-10-11 11 Identification Tape 289T1144-10505 1 SWPM 20-10-11 12 Wire 289T1144-105W 1 SWPM 20-10-11 13 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 129: P37 Panel - Wiring Changes W/B0192, Groups 49, 79, 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 295 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 129: P37 Panel - Wiring Changes W/B0192, Groups 49, 79, 88 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10692 R/H TIME DELAY

W1118 D31186

AE0218

78U-24 

# W192

79H-24

63E-24 YA12 TB212 4

10 4
11 K10690 R/H HOLD RELAY D31184 TB212 TB212 Z19 7

TB212 J D4284P 12

YA14 79X-24 004-24

C1 K2090 W188

K330 OVRD PUMP CONT RLY R FUEL X1 D12158 RIGHT 78U-24 004-24

YC14 YC12 TB212

W188 2

2 5 3

TB304 7 79J-24

3 79G-24 79Q-24 79B-24

JETTISON RLY B1 79V-24

63E-24 63C-22 9

5 7 8 1

63C-22 6 (4 LOCATIONS)

Z17 1 (4 LOCATIONS)

2 3 (10 LOCATIONS) 12 13D60571



### (SHEET 1 OF 2)

### FIGURE 129: P37 Panel - Wiring Changes W/B0192, Groups 49, 79, 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 296 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 49, 79, 88: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-19 3 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACT12AR222 1 SWPM 20-30-11 6 Relay Socket BACS16AH1 1 SWPM 20-81-22 7 Relay Socket BACS16AG1 1 SWPM 20-81-22 8 Identification Tape 289T1144-10502 1 SWPM 20-10-11 9 Identification Tape 289T1144-10503 1 SWPM 20-10-11 10 Identification Tape 289T1144-10504 1 SWPM 20-10-11 11 Identification Tape 289T1144-10505 1 SWPM 20-10-11 12 Wire 289T1144-105W 1 SWPM 20-10-11 13 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 130: P37 Panel - Wiring Changes W/B0192, Groups 48, 50-53, 78 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 297 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 130: P37 Panel - Wiring Changes W/B0192, Groups 48, 50-53, 78 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10692 R/H TIME DELAY

W198 D31186

AE0218

78U-24 

# W192

79H-24

63E-24 YA12 TB212 4

10 4
11 K10690 R/H HOLD RELAY D31184 TB212 TB212 Z19 7

TB212 J D4284P 12

YA14 79X-24 004-24

C1 K2090 W188

K330 OVRD PUMP CONT RLY R FUEL X1 D12158 RIGHT 78U-24 004-24

YC14 YC12 TB212

W188 2

2 5 3

TB304 7 79J-24

3 79G-24 79Q-24 79B-24

JETTISON RLY B1 79V-24

63E-24 63C-22 9

5 7 8 1

63C-22 6 (4 LOCATIONS)

Z17 1 (4 LOCATIONS)

2 3 (10 LOCATIONS) 12 13D60572



### (SHEET 1 OF 2)

### FIGURE 130: P37 Panel - Wiring Changes W/B0192, Groups 48, 50-53, 78 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 298 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 48, 50-53, 78: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-19 3 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACT12AR222 1 SWPM 20-30-11 6 Relay Socket BACS16AH1 1 SWPM 20-81-22 7 Relay Socket BACS16AG1 1 SWPM 20-81-22 8 Identification Tape 289T1144-10502 1 SWPM 20-10-11 9 Identification Tape 289T1144-10503 1 SWPM 20-10-11 10 Identification Tape 289T1144-10504 1 SWPM 20-10-11 11 Identification Tape 289T1144-10505 1 SWPM 20-10-11 12 Wire 289T1144-105W 1 SWPM 20-10-11 13 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 131: P37 Panel - Wiring Changes W/B0192, Groups 46-47, 58, 60, 65, 71, 73, 75, 77 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 299 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 131: P37 Panel - Wiring Changes W/B0192, Gr oups 46-47, 58, 60, 65, 71, 73, 75, 77 Airplanes.** 

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10692 R/H TIME DELAY

W198 D31186

AE0218

78U-24 

# W192

79H-24

63E-24 YA12 TB212 4

10 4
11 K10690 R/H HOLD RELAY D31184 TB212 Z17 TB212 Z19 7

TB212 J D4284P 12

YA14 79X-24 004-24

C1 K2090 W188

K330 OVRD PUMP CONT RLY R FUEL X1 D12158 RIGHT 78U-24 004-24

YC14 YA7 TB212

W188 2

2 5 3

TB304 7 79J-24

3 79G-24 79Q-24 79B-24

JETTISON RLY B1 79V-24

63E-24 63C-22 9

5 7 8 1

63C-22 6 (4 LOCATIONS) 1 (4 LOCATIONS)

2 3 (10 LOCATIONS) 12 13D60573



### (SHEET 1 OF 2)

### FIGURE 131: P37 Panel - Wiring Changes W/B0192, Groups 46-47, 58, 60, 65, 71, 73, 75, 77 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 300 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 46-47, 58, 60, 65, 71, 73, 75, 77: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-19 3 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACT12AR222 1 SWPM 20-30-11 6 Relay Socket BACS16AH1 1 SWPM 20-81-22 7 Relay Socket BACS16AG1 1 SWPM 20-81-22 8 Identification Tape 289T1144-10502 1 SWPM 20-10-11 9 Identification Tape 289T1144-10503 1 SWPM 20-10-11 10 Identification Tape 289T1144-10504 1 SWPM 20-10-11 11 Identification Tape 289T1144-10505 1 SWPM 20-10-11 12 Wire 289T1144-105W 1 SWPM 20-10-11 13 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 132: P37 Panel - Wiring Changes W/B0192, Group 63 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 301 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 132: P37 Panel - Wiring Changes W/B0192, Group 63 Airplanes.**

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL

K10692 R/H TIME DELAY

W198 D31186

AE0218

78U-24 

# W192

79H-24

63E-24 YA12 TB212 4

10 4

11 K10690 R/H HOLD RELAY D31184 TB274 Z1 TB274 Z2 7

TB212 J D4284P 12

YA14 79X-24 004-24

C1 K2090 W188

K330 OVRD PUMP CONT RLY R FUEL X1 D12158 RIGHT 78U-24 004-24

YC14 YC11 TB212

W188 2

2 5 3

TB304 7 79J-24

3 79G-24 79Q-24 79B-24

JETTISON RLY B1 79V-24

63E-24 63C-22 9

5 7 8 1

63C-22 6 (4 LOCATIONS) 1 (4 LOCATIONS)

2 3 (10 LOCATIONS) 12 13D60574



### (SHEET 1 OF 2)

### FIGURE 132: P37 Panel - Wiring Changes W/B0192, Group 63 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 302 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 63: REFERENCE: 767 Wire Diagram 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-105. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-19 3 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 4 Contact BACC47CP1S 1 SWPM 20-61-11 5 Contact BACT12AR222 1 SWPM 20-30-11 6 Relay Socket BACS16AH1 1 SWPM 20-81-22 7 Relay Socket BACS16AG1 1 SWPM 20-81-22 8 Identification Tape 289T1144-10502 1 SWPM 20-10-11 9 Identification Tape 289T1144-10503 1 SWPM 20-10-11 10 Identification Tape 289T1144-10504 1 SWPM 20-10-11 11 Identification Tape 289T1144-10505 1 SWPM 20-10-11 12 Wire 289T1144-105W 1 SWPM 20-10-11 13 Lacing Tape 289T1144-10501 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 133: P37 Panel - Wiring Changes W/B0198, Group 61 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 303 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 133: P37 Panel - Wiring Changes W/B0198, Group 61 Airplanes.**

This Figure applies to Group 61: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 3 1 W590 2 AE0224
D5052P 19 J W192

P37 RIGHT MISCELLANEOUS ELECTRICAL PANEL YC3 K330 OVRD PUMP CONT RLY R FUEL TB190

YA11 02A-24 188-24 X1 TB82 

# W198

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 4 5D60578 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 134: P37 Panel - Wiring Changes W/B0198, Group 62 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 304 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 134: P37 Panel - Wiring Changes W/B0198, Group 62 Airplanes.**

This Figure applies to Group 62: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 1
3 W590 W192

P37 RIGHT MISCELLANEOUS ELECTRICAL PANEL

J AE0224
D5052P 19 YC3 2

TB82 YC11 TB212 K330 R FUEL OVRD PUMP CONT RLY 188-24 02A-24 

# W198
X1

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 4 5D60582 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 135: P37 Panel - Wiring Changes W/B0198, Group 63 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 305 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 135: P37 Panel - Wiring Changes W/B0198, Group 63 Airplanes.**

This Figure applies to Group 63: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. APPLICABLE TO AIRPLANES VN134-VN137 ONLY AE0224 2 W590 3 02A-24 W198- 19 1 D5052P YC11 J W192

P37 TB212
RIGHT MISCELLANEOUS ELECTRICAL PANEL

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 4 5D60586 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 136: P37 Panel - Wiring Changes W/B0198, Groups 40-41, 43-45, 57, 64, 69, 70, 72 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 306 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 136: P37 Panel - Wiring Changes W/B0198, Groups 40-41, 43-45, 57, 64, 69, 70, 72 Airplanes.**

This Figure applies to Group 40-41, 43-45, 57, 64, 69-70, 72: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 3 1 W590 2 AE0224
D5052P 12 J W192

P37 RIGHT MISCELLANEOUS ELECTRICAL PANEL YC3 K330 OVRD PUMP CONT RLY R FUEL TB212 YA7 02A-24 188-24 X1 TB82 

# W198

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 4 5D60589 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 137: P37 Panel - Wiring Changes W/B0198, Groups 59, 66, 74 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 307 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 137: P37 Panel - Wiring Changes W/B0198, Groups 59, 66, 74 Airplanes.**

This Figure applies to Group 59, 66, 74: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 3 1 W590 2 AE0224
D5052P 19 J W192

P37 RIGHT MISCELLANEOUS ELECTRICAL PANEL YC3 K330 OVRD PUMP CONT RLY R FUEL TB212 YA7 02A-24 188-24 X1 TB82 

# W198

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 4 5D60592 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 138: P37 Panel - Wiring Changes W/B0198, Groups 46, 58, 65, 71, 73 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 308 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 138: P37 Panel - Wiring Changes W/B0198, Groups 46, 58, 65, 71, 73 Airplanes.**

This Figure applies to Group 46, 58, 65, 71, 73: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. AE0224 2 W590 3 02A-24 W198- 12 1 D5052P YA7 J W192

P37 TB212
RIGHT MISCELLANEOUS ELECTRICAL PANEL REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 4 5D60594 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 139: P37 Panel - Wiring Changes W/B0198, Groups 47, 60, 75, 77 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 309 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 139: P37 Panel - Wiring Changes W/B0198, Groups 47, 60, 75, 77 Airplanes.**

This Figure applies to Group 47, 60, 75, 77: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. AE0224 2 W590 3 02A-24 W198- 19 1 D5052P YA7 J W192

P37 TB212
RIGHT MISCELLANEOUS ELECTRICAL PANEL

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 4 5D60596 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 140: P37 Panel - Wiring Changes W/B0198, Group 51 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 310 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 140: P37 Panel - Wiring Changes W/B0198, Group 51 Airplanes.**

This Figure applies to Group 51: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. AE0224 2 W590 3 02A-24 W198- 12 1 D5052P YC12 J W192

P37 TB212
RIGHT MISCELLANEOUS ELECTRICAL PANEL

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 4 5D60599 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 141: P37 Panel - Wiring Changes W/B0198, Groups 48, 50, 53, 78 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 311 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 141: P37 Panel - Wiring Changes W/B0198, Groups 48, 50, 53, 78 Airplanes.**

This Figure applies to Group 48, 50, 53, 78: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. AE0224 2 W590 3 02A-24 W198- 19 1 D5052P YC12 J W192

P37 TB212
RIGHT MISCELLANEOUS ELECTRICAL PANEL REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5D60601 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 142: P37 Panel - Wiring changes W/B0198, Groups 52, 56 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 312 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 142: P37 Panel - Wiring changes W/B0198, Groups 52, 56 Airplanes.**

This Figure applies to Group 52, 56: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-106. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact M39029/11-145 1 SWPM 20-90-11 See note (a) 3 Identification Tape 289T1144-10602 1 SWPM 20-10-11 4 Wire 289T1144-106W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10601 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. AE0224 2 W590 3 02A-24 W198- 13 1 D5052P YC12 J W192

P37 TB212
RIGHT MISCELLANEOUS ELECTRICAL PANEL REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5D60604 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 143: P37 Panel - Relay Installation, Groups 40-79, 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 313 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 143: P37 Panel - Relay Installation, Groups 40-79, 88 Airplanes.**



### MAIN EQUIPMENT CENTER P37 PANEL

A A FWD

FWD UPJ81862



### (SHEET 1 OF 2)

### FIGURE 143: P37 Panel - Relay Installation, Groups 40-79, 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 314 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 40-79, 88: The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY numbers shown below are the number of parts necessary for each airplane. Use parts from Top Kit 015T1775- 3 (Group 40-79 airplanes). **STEP TASK NAME IDENTIFICATION QTY MORE DATA** 1 Install Relay BACR13CD2 1 -- 2 Install Relay TDH-1852-1402 1 -- 

### A-AK10692K10690



### FWD UP 1 2J81861



### (SHEET 2 OF 2)

### FIGURE 144: P36 to P37 Panel - Wiring Changes W/B0590, Groups 47-48, 50, 53, 59-60, 66, 74-75, 77- **78 Airplanes.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 315 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 144: P36 to P37 Panel - Wiring Changes W/B0590, Groups 47-48, 50, 53, 59-60, 66, 74-75, 77-78 Airplanes.** 

This Figure applies to Group 47-48, 50, 53, 59-60, 66, 74-75, 77-78: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-108. Reference Figure 152 for wire bundle routing information. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact BACC47CN1S 1 SWPM 20-61-11 3 Identification Tape 289T1144-10803 1 SWPM 20-10-11 4 Identification Tape 289T1144-10804 1 SWPM 20-10-11 5 Wire 289T1144-108W 1 SWPM 20-10-11 6 Lacing Tape 289T1144-10802 1 SWPM 20-10-11 ELECTRICAL EQPT PANEL 4 RIGHT MISC. W590- AE0209 AE0224

P37 021-24 W184 D4856P 13 J 19 D5052P W198 J 2 1

LEFT MISC. ELECTRICAL EQPT PANEL 3 P36
REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 5 6

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60607



### (SHEET 1 OF 1)

### FIGURE 145: P36 to P37 Panel - Wiring Changes W/B0590, Groups 61-63 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 316 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 145: P36 to P37 Panel - Wiring Changes W/B0590, Groups 61-63 Airplanes.**

This Figure applies to Group 61-63: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-108. Reference Figure 152 for wire bundle routing information. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact BACC47CN1S 1 SWPM 20-61-11 3 Identification Tape 289T1144-10803 1 SWPM 20-10-11 4 Identification Tape 289T1144-10804 1 SWPM 20-10-11 5 Wire 289T1144-108W 1 SWPM 20-10-11 6 Lacing Tape 289T1144-10802 1 SWPM 20-10-11 ELECTRICAL EQPT PANEL P36 4 FRIGHT MISC. W590- AE0209 AE0224

P37 021-24 W184 D4856P 2 J D5052P W198 J 2 1

LEFT MISC. ELECTRICAL EQPT PANEL 3 19

REFERENCE: 767 WIRE DIAGRAMS 28-22-12, 28-42-12 5 6

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60609



### (SHEET 1 OF 1)

### FIGURE 146: P36 to P37 Panel - Wiring Changes W/B0590, Groups 40-41, 43-46, 51, 57-58, 64-65, 69- **73 Airplanes.** May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 317 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 146: P36 to P37 Panel - Wiring Changes W/B0590, Groups 40-41, 43-46, 51, 57-58, 64-65, 69-73 Airplanes.** 

This Figure applies to Group 40-41, 43-46, 51, 57-58, 64-65, 69-73: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-108. Reference Figure 152 for wire bundle routing information. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact BACC47CN1S 1 SWPM 20-61-11 3 Identification Tape 289T1144-10803 1 SWPM 20-10-11 4 Identification Tape 289T1144-10804 1 SWPM 20-10-11 5 Wire 289T1144-108W 1 SWPM 20-10-11 6 Lacing Tape 289T1144-10802 1 SWPM 20-10-11 ELECTRICAL EQPT PANEL 4 RIGHT MISC. W590- AE0209 AE0224

P37 021-24 W184 D4856P 13 J 12 D5052P W198 J 2 1

LEFT MISC. ELECTRICAL EQPT PANEL 3 P36 REFERENCE: 767 WIRE DIAGRAMS 28-42-12 5 6D60611 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 147: P36 to P37 Panel - Wiring Changes W/B0590, Groups 52, 56 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 318 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 147: P36 to P37 Panel - Wiring Changes W/B0590, Groups 52, 56 Airplanes.**

This Figure applies to Group 52, 56: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-108. Reference Figure 152 for wire bundle routing information. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact BACC47CN1S 1 SWPM 20-61-11 3 Identification Tape 289T1144-10803 1 SWPM 20-10-11 4 Identification Tape 289T1144-10804 1 SWPM 20-10-11 5 Wire 289T1144-108W 1 SWPM 20-10-11 6 Lacing Tape 289T1144-10802 1 SWPM 20-10-11 ELECTRICAL EQPT PANEL P36 4 FRIGHT MISC. W590- AE0209 AE0224

P37 021-24 W184 D4856P 13 J D5052P W198 J 2 1

LEFT MISC. ELECTRICAL EQPT PANEL 3 13

REFERENCE: 767 WIRE DIAGRAMS 28-42-12 5 6D60612 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 148: P36 to P37 Panel - Wiring Changes W/B0942, Groups 42, 49, 54, 67-68, 76, 79 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 319 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 148: P36 to P37 Panel - Wiring Changes W/B0942, Groups 42, 49, 54, 67-68, 76, 79 Airplanes.**

This Figure applies to Group 42, 49, 54, 67-68, 76, 79: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-109. Reference Figure 152 for wire bundle routing information. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 2 SWPM 20-61-11 2 Identification Tape 289T1144-10904 1 SWPM 20-10-11 3 Identification Tape 289T1144-10905 1 SWPM 20-10-11 4 Wire 289T1144-109W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10901 1 SWPM 20-10-11 ELECTRICAL EQPT PANEL P36 3 RIGHT MISC. W942- AE0209 AE0218

P37 011-24 W176 D4906P 5 J D6658P W1118 J 1 1

LEFT MISC. ELECTRICAL EQPT PANEL 2 13

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60615



### (SHEET 1 OF 1)

### FIGURE 149: P36 to P37 Panel - Wiring Changes W/B0942, Group 55 Airplane. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 320 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 149: P36 to P37 Panel - Wiring Changes W/B0942, Group 55 Airplane.**

This Figure applies to Group 55: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-109. Reference Figure 152 for wire bundle routing information. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 1 SWPM 20-61-11 2 Contact BACC47CN1S 1 SWPM 20-61-11 3 Identification Tape 289T1144-10904 1 SWPM 20-10-11 4 Identification Tape 289T1144-10906 1 SWPM 20-10-11 5 Wire 289T1144-109W 1 SWPM 20-10-11 6 Lacing Tape 289T1144-10901 1 SWPM 20-10-11 ELECTRICAL EQPT PANEL P36 4 RIGHT MISC. W942- AE0209 AE0218

P37 011-24 W176 D4906P 5 J D7352P W188 J 2 1

LEFT MISC. ELECTRICAL EQPT PANEL 3 15

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 5 6

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTINGD60617



### (SHEET 1 OF 1)

### FIGURE 150: P37 Panel - Wiring Changes W/B1118, Groups 49, 54, 79, 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 321 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 150: P37 Panel - Wiring Changes W/B1118, Groups 49, 54, 79, 88 Airplanes.**

This Figure applies to Group 49, 54, 79, 88: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-110. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact - Burndy M39029/11-145 1 SWPM 20-90-11 See note (a) 2 Contact BACC47CN1S 1 SWPM 20-61-11 3 Identification Tape 289T1144-11003 1 SWPM 20-10-11 4 Wire 289T1144-110W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-11001 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 1 14A-24 W1118- 13 D6658P W942 YC12 2
3 AE0218
J W192

P37 RIGHT MISCELLANEOUS ELECTRICAL PANEL TB212

REFERENCE 767 WIRE DIAGRAM 28-22-12 4 5D60620 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 151: P37 Panel - Wiring Changes W/B1118, Groups 42, 67-68, 76 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 322 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 151: P37 Panel - Wiring Changes W/B1118, Groups 42, 67-68, 76 Airplanes.**

This Figure applies to Group 42, 67-68, 76: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-110. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact - Burndy M39029/11-145 1 SWPM 20-90-11 See note (a) 2 Contact BACC47CN1S 1 SWPM 20-61-11 3 Identification Tape 289T1144-11003 1 SWPM 20-10-11 4 Wire 289T1144-110W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-11001 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144-201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. 2
3 W942 W192

P37

J AE0218
D6658P 13
RIGHT MISCELLANEOUS ELECTRICAL PANEL 1 W1118- YA7 TB212 14A-24

REFERENCE 767 WIRE DIAGRAM 28-22-12 4 5D60674 ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING



### (SHEET 1 OF 1)

### FIGURE 152: Wiring Bundle Routing, P36 to P37 Panel, Groups 40-79 and 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 323 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 152: Wiring Bundle Routing, P36 to P37 Panel, Groups 40-79 and 88 Airplanes.**

P36 P37

P33

FWD 2 1J81855



### (SHEET 1 OF 3)

### FIGURE 152: Wiring Bundle Routing, P36 to P37 Panel, Groups 40-79 and 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 324 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 40-79, 88: P36 P37

P33 ALTERNATE WIRE ROUTING

FWD 2 11556148



### (SHEET 2 OF 3)

### FIGURE 152: Wiring Bundle Routing, P36 to P37 Panel, Groups 40-79 and 88 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 325 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY numbers shown below are the number of parts necessary for each airplane. Use lacing tape supplied as required for wire bundle installation. **STEP TASK NAME IDENTIFICATION QTY MORE DATA**

1 Install Wire Bundle -- -- Gain access to the P36 and P37 Panel. Install the new wiring between the P36 and P37 panels using the existing wire bundle routing for W/B 590 or W/B 942 (use alternate wire routing when applicable). Refer to SWPM 20-10-11, 20-10-12 for wire installation procedures. 2 Install Lacing Tape 289T1144-( ) -- --

**(SHEET 3 OF 3)**

### FIGURE 153: P36 Panel - Wiring Changes W/B0175, Group 80-81 and 89 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 326 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 153: P36 Panel - Wiring Changes W/B0175, Group 80-81 and 89 Airplanes.**

This Figure applies to Group 80-81, 89: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from Kit 015T1775-4. Connect the cap and stored wires shown in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary.

**FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact - Burndy M39029/11-145 1 SWPM 20-90-11. If contact is already installed, installation may not be necessary. P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY D11631 

# W176

83U-24 AE0209 YC10 TB216 4

K10691 L/H HOLD RELAY D11629 YA20 J D4992P 42

TB218 3 85U-24 1 W184-768-24

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING REFERENCE 767 WIRE DIAGRAM 28-22-12D60675



### (SHEET 1 OF 1)

### FIGURE 154: P36 Panel - Relay Installation, Group 80-81 and 89 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 327 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 154: P36 Panel - Relay Installation, Group 80-81 and 89 Airplanes.**

P36 PANEL 

### MAIN EQUIPMENT CENTER

1 4

SEE A FWD FWDD60676



### (SHEET 1 OF 2)

### FIGURE 154: P36 Panel - Relay Installation, Group 80-81 and 89 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 328 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 80-81, 89: The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY numbers shown below are the number of parts necessary for each airplane. Use parts supplied in Top Kit 015T1775-4. **STEP TASK NAME IDENTIFICATION QTY MORE DATA** 1 Open Door -- 1 -- 2 Install Relay BACR13CD2 1 Install relay in Position 200. For mounting hardware information, refer to SWPM 20-81-22 as an accepted procedure. 3 Install Relay TDH-1852-1402 1 Install relay in Position 269. For mounting hardware information refer to SWPM 20-81-22 as an accepted procedure. 4 Close Door -- 1 -- LOWER RELAY PANEL FWD 3 2



### AD60677



### (SHEET 2 OF 2)

### FIGURE 155: P37 Panel - Wiring Changes W/B0192 and W/B1118, Group 80 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 329 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 155: P37 Panel - Wiring Changes W/B0192 and W/B1118, Group 80 Airplanes.**

This Figure applies to Group 80: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from Kit 015T1775-4. Connect cap and stored wires on the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary.

**FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact - Burndy M39029/11-145 1 SWPM 20-90-11. If contact is already installed, installation may not be necessary. D6658P

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10692 R/H TIME DELAY D31186 

# W192

79H-24 AE0218 YA12 TB212 4

K10690 L/H HOLD RELAY D31184 YC12 J 13

TB212 3 79G-24 1 W1118-14A-24

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING REFERENCE 767 WIRE DIAGRAM 28-22-12D60678



### (SHEET 1 OF 1)

### FIGURE 156: P37 Panel - Wiring Changes W/B0192 and W/B0188, Group 81 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 330 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 156: P37 Panel - Wiring Changes W/B0192 and W/B0188, Group 81 Airplanes.**

This Figure applies to Group 81: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from Kit 015T1775-4. Connect cap and stored wires on the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary.

**FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact - Burndy M39029/11-145 1 SWPM 20-90-11. If contact is already installed, installation may not be necessary. D7352P 15

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10692 R/H TIME DELAY D31186 

# W192

79H-24 AE0218 YA12 TB212 4

K10690 L/H HOLD RELAY D31184 YC12 J TB212 3 79G-24 1 W188-14A-24

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING REFERENCE 767 WIRE DIAGRAM 28-22-121561742



### (SHEET 1 OF 1)

### FIGURE 157: P37 Panel - Relay Installation, Group 80-81 and 89 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 331 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 157: P37 Panel - Relay Installation, Group 80-81 and 89 Airplanes.**



### MAIN EQUIPMENT CENTER P37 PANEL

FWD

1 FWD UP

4 SEE AD60679



### (SHEET 1 OF 3)

### FIGURE 157: P37 Panel - Relay Installation, Group 80-81 and 89 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 332 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 80-81, 89: UPPER RELAY PANEL FWD 3 2



### AD60681



### (SHEET 2 OF 3)

### FIGURE 157: P37 Panel - Relay Installation, Group 80-81 and 89 Airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 333 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY numbers shown below are the number of parts necessary for each airplane. Use parts supplied in Top Kit 015T1775-4. **STEP TASK NAME IDENTIFICATION QTY MORE DATA** 1 Open Door -- 1 -- 2 Install Relay BACR13CD2 1 Install relay in Position 30. For mounting hardware information refer to SWPM 20-81-22 as an accepted procedure. 3 Install Relay TDH-1852-1402 1 Install relay in Position 39. For mounting hardware information refer to SWPM 20-81-22 as an accepted procedure. 4 Close Door -- 1 --

**(SHEET 3 OF 3)**

### FIGURE 158: P37 Panel - Wiring Changes W/B0188, Groups 82-87 airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 334 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 158: P37 Panel - Wiring Changes W/B0188, Groups 82-87 airplanes.**

This Figure applies to Group 82-87: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-104. Route new wiring in the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact M39029/11-145 3 SWPM 20-90-11 See note (a) 2 Contact BACC47CN1S 2 SWPM 20-81-12 3 Contact BACC47CP1S 1 SWPM 20-90-11 4 Identification Tape 289T1144-10402 1 SWPM 20-10-11 5 Identification Tape 289T1144-10403 1 SWPM 20-10-11 6 Identification Tape 289T1144-10405 1 SWPM 20-10-11 YC4

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL AE0218

W192 TB304

TB274 J 22 D5330P

J 3 D5506P

J 5 D5372P 

# W188 074-22

075-22

073-24 1 074-22

075-22

073-24

2

2

3 6 4

5 Z26

REFERENCE: 767 WIRE DIAGRAMS 28-42-12 7 8



### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING1310271



### (SHEET 1 OF 2)

### FIGURE 158: P37 Panel - Wiring Changes W/B0188, Groups 82-87 airplanes. May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 335 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

7 Wire 289T1144-104W 1 SWPM 20-10-11 8 Lacing Tape 289T1144-10401 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA** 

**(SHEET 2 OF 2)**

### FIGURE 159: P37 Panel - Wiring Changes W/B0176 Group 88 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 336 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 159: P37 Panel - Wiring Changes W/B0176 Group 88**

40 D5658P

P36 LEFT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10693 L/H TIME DELAY

W184 D11631 

# W176

83U-24 02F-24 J 4

J D5658P W0942 TB216

YA10

YC10 TB216 4

W184

5

7 7

K10691 L/H HOLD RELAY D11629 TB216 Z14 TB218 YC5

7

TB218 J D4672P 18

YA20 85W-24 02H-22

K2089 LEFT JETTISON RLY K329 OVRD PUMP CONT RLY L FUEL X1 D12156 C1 75W-22 53E-24 75W-22 02H-22

53E-24 YA5 TB218 02F-24

2

2 5 3

B1 7 83V-24

3 85U-24 83Y-24 85V-24

85J-24

53C-22 W184 53C-22 TB218 XD3 7

2 6

4 12 13 11

10 9 8 3 (10 LOCATIONS) 1

1 (4 LOCATIONS)

(4 LOCATIONS) AE0223 14 151561744



### (SHEET 1 OF 2)

### FIGURE 159: P37 Panel - Wiring Changes W/B0176 Group 88 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 337 of 339 

### BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 88: REFERENCE: 767 Wiring Diagrams 767 WDM 28-22-12, 28-42-12 The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-102. Route new wiring in the P36 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47ER1 8 SWPM 20-81-19 2 Contact BACC47DJ1 2 SWPM 20-81-12 3 Contact M39029/11-145 10 SWPM 20-90-11 See note (a) 4 Terminal Lug BACT12AR222 1 SWPM 20-30-11 5 Relay Socket BACS16AH1 1 SWPM 20-81-22 6 Relay Socket BACS16AG1 1 SWPM 20-81-22 7 Pin BACC47CN1S 3 SWPM 20-61-11 8 Identification Tape 289T1144-10202 1 SWPM 20-10-11 9 Identification Tape 289T1144-10203 1 SWPM 20-10-11 10 Identification Tape 289T1144-10204 1 SWPM 20-10-11 11 Identification Tape 289T1144-10209 1 SWPM 20-10-11 12 Identification Tape 289T1144-10210 1 SWPM 20-10-11 13 Identification Tape 289T1144-10211 1 SWPM 20-10-11 14 Wire 289T1144-102W 1 SWPM 20-10-11 15 Lacing Tape 289T1144-10201 1 SWPM 20-10-11 (a) New Burndy terminal blocks BACM15C3C and BACM15C3B are supplied in kit 289T1144- 201, if required. Refer to SWPM 20-90-11 as an acceptable procedure for installation instructions.989752 

### ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING

**(SHEET 2 OF 2)**

### FIGURE 160: P36 to P37 Panel - Wiring Changes W/B0942, Groups 88 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 338 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 160: P36 to P37 Panel - Wiring Changes W/B0942, Groups 88**

This Figure applies to Group 88: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from wire kit 289T1144-109. Reference Figure 152 for wire bundle routing information. Use lacing tape as necessary. **FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact BACC47CP1S 2 SWPM 20-61-11 2 Identification Tape 289T1144-10904 1 SWPM 20-10-11 3 Identification Tape 289T1144-10905 1 SWPM 20-10-11 4 Wire 289T1144-109W 1 SWPM 20-10-11 5 Lacing Tape 289T1144-10901 1 SWPM 20-10-11 40 D5658P ELECTRICAL EQPT PANEL P36 3 RIGHT MISC. W942- AE0209 AE0218

P37 011-24 W176 J D6658P W1118 J 1 1

LEFT MISC. ELECTRICAL EQPT PANEL 2 13

REFERENCE: 767 WIRE DIAGRAMS 28-22-12 4 5

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING1561746



### (SHEET 1 OF 1)

### FIGURE 161: P37 Panel - Wiring Changes W/B0192 and W/B198, Group 89 May 03, 2006 Revision 2: February 12, 2009 767-28A0083 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 

### 339 of 339 

### BOEING SERVICE BULLETIN 767-28A0083 **FIGURE 161: P37 Panel - Wiring Changes W/B0192 and W/B198, Group 89**

This Figure applies to Group 89: The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure. **NOTE:** Use the parts from Kit 015T1775-4. Connect cap and stored wires on the P37 panel following the existing wire bundle routing, refer to SWPM 20-10-11. Use lacing tape as necessary.

**FLAG NOTE NAME IDENTIFICATION QTY MORE DATA**  1 Contact - Burndy M39029/11-145 1 SWPM 20-90-11. If contact is already installed, installation may not be necessary. D5052P W198-02A-24 8

P37 RIGHT MISCELLANEOUS ELECTRICAL EQUIPMENT PANEL K10692 R/H TIME DELAY D31186 

# W192

79H-24 AE0224 YA12 TB212 4

K10690 L/H HOLD RELAY D31184 YC12 J TB212 3 79G-24 1

ADDED WIRE OR NEW ROUTING EXISTING WIRE DELETED WIRE OR FORMER ROUTING REFERENCE 767 WIRE DIAGRAM 28-22-121561747



### (SHEET 1 OF 1)