May 03, 2006

Revision 2: February 12, 2009 767-28A0083

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 1 of 339

Commercial

Airplane

Group 767

Service Bulletin

Number: 767-28A0083

Date: May 03, 2006

Revision 2: February 12, 2009

ATA System: 2822 2842

SUBJECT: FUEL SYSTEM - Engine Fuel Feed System - Fuel Pump Inlet Protection - Auxiliary 

Fuel Tank Pump Automatic Shut Off Installation

BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET

Copyright © 2006 The Boeing Company

Unpublished Work - All Rights Reserved

Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable 

subject matter. Boeing also claims copyright in this document as a compilation and/or collective work.

This document includes proprietary information owned by The Boeing Company and/or one or more third 

parties. Treatment of the document and the information it contains is governed by contract with Boeing. For 

more information, contact The Boeing Company, P.O. Box 3707, Seattle, Washington 98124.

Boeing, 707, 717, 727, 737, 747, 757, 767, 777, BBJ, BOEING BUSINESS JET, DC-8, DC-9, DC-10, MD-10, 

MD-11, MD-80, MD-90, the Boeing logo and the Boeing livery are among the trademarks owned by Boeing or 

its subsidiaries. No intellectual property license (express or implied) is granted in connection with this document 

or otherwise.
 BLANK PAGE

May 03, 2006

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BOEING SERVICE BULLETIN 767-28A0083

BLANK PAGE
 Table of Contents

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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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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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Airplanes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 168

FIGURE 55: P37 Panel - Wiring Changes W/B0198, Groups 2-3, 10 82-83 Airplanes. . . . . . . . . . 169

FIGURE 56: P37 Panel - Wiring Changes W/B0198, Group 4, 84 Airplanes. . . . . . . . . . . . . . . 170

FIGURE 57: P37 Panel - Wiring Changes W/B0198, Group 7, 86 Airplanes. . . . . . . . . . . . . . . 171

FIGURE 58: P37 Panel - Wiring Changes W/B0198, Groups 11, 21 Airplanes.. . . . . . . . . . . . . 172

FIGURE 59: P37 Panel - Wiring Changes W/B0198, Groups 12, 15, 23, 26 Airplanes.. . . . . . . . . 173

FIGURE 60: P37 Panel - Wiring Changes W/B0198, Groups 13, 24, 27 Airplanes.. . . . . . . . . . . 174

FIGURE 61: P37 Panel - Wiring Changes W/B0198, Groups 18, 20, 32-34 Airplanes. . . . . . . . . . 175

FIGURE 62: P37 Panel - Wiring Changes W/B0198, Group 22 Airplanes. . . . . . . . . . . . . . . . 176

FIGURE 63: P37 Panel - Wiring Changes W/B0198, Group 29-30 Airplanes. . . . . . . . . . . . . . 177

FIGURE 64: P37 Panel - Wiring Changes W/B0198, Group 31 Airplanes. . . . . . . . . . . . . . . . 178

FIGURE 65: P37 Panel - Wiring Changes W/B0198, Group 35 Airplanes. . . . . . . . . . . . . . . . 179

FIGURE 66: P37 Panel - Wiring Changes W/B0198, Group 37 Airplanes. . . . . . . . . . . . . . . . 180

FIGURE 67: P37 Panel - Relay Installation, Groups 1-39, 82-87 Airplanes. . . . . . . . . . . . . . . 181

FIGURE 68: P37 Panel - Wiring Changes W/B0198, Group 38 Airplanes. . . . . . . . . . . . . . . . 183

FIGURE 69: P33 to P36 Panel - Wiring Changes W/B0264, Groups 1-6, 8-15, 17-24, 26-31, 33-35, 37-39,

82-85, 87 Airplanes.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 184

FIGURE 70: P33 to P36 Panel - Wiring Changes W/B0264, Groups 7, 16, 86 Airplanes. . . . . . . . 185

FIGURE 71: P33 to P36 Panel - Wiring Changes W/B0264, Groups 25, 32 Airplanes. . . . . . . . . . 186

FIGURE 72: P33 to P36 Panel - Wiring Changes W/B0264, Group 36 Airplanes. . . . . . . . . . . . 187

FIGURE 73: P36 to P37 Panel - Wiring Changes W/B0590, Groups 1-6, 8-10, 14, 16-20, 25, 28-30, 32-34,

36, 82-85, 87 Airplanes.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 188

FIGURE 74: P36 to P37 Panel - Wiring Changes W/B0590, Group 31 Airplanes. . . . . . . . . . . . 189

FIGURE 75: P36 to P37 Panel - Wiring Changes W/B0590, Group 35 Airplanes. . . . . . . . . . . . 190

FIGURE 76: P36 to P37 Panel - Wiring Changes W/B0590, Groups 7, 11, 21-22, 86 Airplanes. . . . . 191

FIGURE 77: P36 to P37 Panel - Wiring Changes W/B0590, Groups 12-13, 15, 23-24, 26-27, 38 Airplanes.

192

FIGURE 78: P36 to P37 Panel - Wiring Changes W/B0942, Groups 37, 39 Airplanes. . . . . . . . . . 193

FIGURE 79: P37 Panel - Wiring Changes W/B1118, Group 39 Airplanes. . . . . . . . . . . . . . . . 194

FIGURE 80: P37 Panel - Wiring Changes W/B1118, Group 37 Airplanes. . . . . . . . . . . . . . . . 195

FIGURE 81: Wire Bundle Routing, P36 to P37 Panel, Groups 1-39, 82-87 Airplanes. . . . . . . . . . 196

FIGURE 82: P36 Panel - Bracket Installation, Group 40-79, 88 Airplanes. . . . . . . . . . . . . . . . 199

FIGURE 83: P37 Panel - Bracket Installation, Groups 40-79, 88 Airplanes.. . . . . . . . . . . . . . . 203

FIGURE 84: P36 Panel - Wiring Changes W/B0176, Group 40 Airplanes. . . . . . . . . . . . . . . . 206

FIGURE 85: P36 Panel - Wiring Changes W/B0176, Groups 42, 67-68 Airplanes. . . . . . . . . . . . 208

FIGURE 86: P36 Panel - Wiring Change W/B0176, Group 76 Airplanes. . . . . . . . . . . . . . . . . 210

FIGURE 87: P36 Panel - Wiring Changes W/B0176, Group 55 Airplanes. . . . . . . . . . . . . . . . 212

FIGURE 88: P36 Panel - Wiring Changes W/B0176, Group 49 Airplanes. . . . . . . . . . . . . . . . 214

FIGURE 89: P36 Panel - Wiring Changes W/B0176, Groups 54, 79 Airplanes.. . . . . . . . . . . . . 216

FIGURE 90: P36 Panel - Wiring Changes W/B0176, Group 66 Airplanes. . . . . . . . . . . . . . . . 218

FIGURE 91: P36 Panel - Wiring Changes W/B0176, Groups 44, 72, 74 Airplanes.. . . . . . . . . . . 220

FIGURE 92: P36 Panel - Wiring Changes W/B0176, Group 62 Airplanes. . . . . . . . . . . . . . . . 222

FIGURE 93: P36 Panel - Wiring Changes W/B0176, Groups 41, 43, 64 Airplanes.. . . . . . . . . . . 224

FIGURE 94: P36 Panel - Wiring Changes W/B0176, Group 69 Airplanes. . . . . . . . . . . . . . . . 226

FIGURE 95: P36 Panel - Wiring Changes W/B0176, Group 61 Airplanes. . . . . . . . . . . . . . . . 228

FIGURE 96: P36 Panel - Wiring Changes W/B0176, Group 70 Airplanes. . . . . . . . . . . . . . . . 230
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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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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
 Table of Contents

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BOEING SERVICE BULLETIN 767-28A0083

BLANK PAGE
Original Issue: May 03, 2006

Revision 2: February 12, 2009 767-28A0083

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 9 of 339

Commercial

Airplanes 767

Service Bulletin

Number: 767-28A0083 Revision Transmittal Sheet

Original Issue: May 03, 2006

Revision 2: February 12, 2009

ATA System: 2822 2842

SUBJECT: FUEL SYSTEM - Engine Fuel Feed System - Fuel Pump Inlet Protection - Auxiliary 

Fuel Tank Pump Automatic Shut Off Installation

This Revision includes all pages of the service bulletin.

COMPLIANCE INFORMATION RELATED TO THIS REVISION

Federal Aviation Administration (FAA) Notice of Proposed Rule Making 2006-NM-283-AD, is related to this 

service bulletin.

No more work is necessary on airplanes changed as shown in Revision 1 or initial release of this service bulletin.

No airplanes were added to the service bulletin effectivity.

REASON FOR REVISION

This revision is sent to address the comments received from operators since the release of Revision 1 of the 

service bulletin.

The effectivity group assignments were changed to show the correct wiring configuration for the affected 

airplanes.

The following sections of the service bulletin are changed:

— The Summary illustration, revised to show the wire bundle routing more accurately and show an alternate 

wire routing configuration.

— Summary - BackGround, Planning Information - Reason and Compliance Section, revised AD reference to 

remove AD 94-11-05. The AD 94-11-05 is superseded by AD 2001-15-08.

— Group and Configuration tables in Section 1.A, Description Section 1.D, Man-power tables Section 1.G, 

Weight and Balance Section H, Accomplishment Instructions Section 3, added new Groups 88 and 89 

airplanes.

Airplanes Affected Old Airplane Groups Airplane Groups

VL891-VL900 49 88 (new)

VR087 80 89 (new)

VR106 80 89 (new)

VR901 81 80 (existing)

VT521-VT522 80 81 (existing)
 

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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
May 03, 2006

Revision 2: February 12, 2009 767-28A0083

BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 11 of 339

Commercial

Airplane

Group 767

Service Bulletin

Number: 767-28A0083 Summary

Date: May 03, 2006

Revision 2: February 12, 2009

ATA System: 2822 2842

SUBJECT: FUEL SYSTEM - Engine Fuel Feed System - Fuel Pump Inlet Protection - Auxiliary 

Fuel Tank Pump Automatic Shut Off Installation

CONCURRENT REQUIREMENTS

None.

BACKGROUND

This service bulletin is the result of the safety assessments conducted by Boeing under SFAR 88, "Fuel Tank 

System Fault Tolerance Evaluation Requirements".

Initial results from the Fuel System Safety Analysis show that fuel pumps that run dry could cause an overheat 

condition external of the pump explosion resistance area that is open to the pump inlet. An overheat condition 

in this area could possibly cause an unwanted ignition source for the fuel vapors in the fuel tank. Ignition of 

flammable fuel vapors could cause a fire or explosion which could put the airplane in an unsafe condition. 

Installation of the automatic shut off system adds fuel pump inlet protection against sparks caused by friction 

overheat damage in the fuel tanks.

This service bulletin gives the instructions and a kit of parts to install an automatic shut off system for the center 

wing tank override boost pumps. Installation of the automatic system will prevent a potential ignition source in 

the tank by making sure the pumps do not run for an extended period of time when the fuel level is below pump 

inlet or the pump has failed.

Currently the flight crew turns off the pumps when a pump low pressure message is displayed on EICAS. The 

automatic shut off system installed by this service bulletin will make sure that the pumps will not run for more 

than 15 seconds with continuous low fuel pressure if the flight crew does not respond to the EICAS message 

sooner. The flight crew remains in primary control, with this automatic shut off system as a backup, to turn the 

pumps off after continuous low pressure indication.

This change affects Section 9 of the Maintenance Planning Data (MPD) Document. New Airworthiness 

Limitations (AWL) "28-AWL-20" will be added to Section 9 of the MPD to include a functional check of the center 

tank fuel boost pump automatic shut off system. This change also affects Section 1 and 3.1 of the FAA 

Approved Airplane Flight Manual.

Federal Aviation Administration (FAA) Airworthiness Directive 2001-15-08 is related to this service bulletin.
 

May 03, 2006

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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.

WB264 CHANGE THE PANEL WIRING.

WB590

WB942

ROUTING

FWD

497138
 

May 03, 2006

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BOEING SERVICE BULLETIN 767-28A0083

BLANK PAGE
May 03, 2006

Revision 2: February 12, 2009 767-28A0083

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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.
 

May 03, 2006

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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
 

May 03, 2006

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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
 

May 03, 2006

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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
 

May 03, 2006

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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
 

May 03, 2006

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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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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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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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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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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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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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— 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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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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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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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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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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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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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 

-4 -3 -2 Number Notes

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 

-104 -103 -102 -101 -3 -2 Number Notes

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 

-104 -103 -102 -101 -3 -2 Number Notes
 

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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 

-108 -107 -106 -105 -3 -2 Number Notes

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 

-104 -103 -102 -101 -3 -2 Number Notes
 

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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 

-201 -110 -109 -3 -2 Number Notes

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 

-108 -107 -106 -105 -3 -2 Number Notes
 

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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 

-201 -110 -109 -3 -2 Number Notes
 

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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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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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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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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.
 

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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.
 

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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.
 

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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.
 

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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.
 

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(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

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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

CONFIGURATION

D59766

(SHEET 1 OF 4)
 FIGURE 1: P36 Panel - Bracket Installation, Groups 1-39 and 82-87 Airplanes

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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

UP

D59769

(SHEET 2 OF 4)
 FIGURE 1: P36 Panel - Bracket Installation, Groups 1-39 and 82-87 Airplanes

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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

UP

1561718

(SHEET 3 OF 4)
 FIGURE 1: P36 Panel - Bracket Installation, Groups 1-39 and 82-87 Airplanes

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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

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FIGURE 2: P37 Panel - Bracket Installation, Groups 1-39 and 82-87 Airplanes

MAIN EQUIPMENT CENTER

A

A

P37 PANEL

FWD

1

FWD

UP

4

D59771

(SHEET 1 OF 3)
 FIGURE 2: P37 Panel - Bracket Installation, Groups 1-39 and 82-87 Airplanes

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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

3

D59774

(SHEET 2 OF 3)
 FIGURE 2: P37 Panel - Bracket Installation, Groups 1-39 and 82-87 Airplanes

May 03, 2006

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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

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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

W264 16A-22

J

23

D4042P

1 2

4 5

D59786

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

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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

85W-24 02H-22 18

W184 XB12

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 12

D59791

(SHEET 1 OF 2)
 FIGURE 4: P36 Panel - Wiring changes W/B0176, Groups 1-2, 5, 82, 85 Airplanes.

May 03, 2006

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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

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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

85W-24 02H-22 18

W184 XB12

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 12

D59801

(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

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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

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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

85W-24 02H-22 18

W184 XC12

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

11 12

D59811

(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

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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

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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

85W-24 02H-22 18

W184 XB12

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 12

D59816

(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

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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

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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

85W-24 02H-22 18

W184 XB12

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

11 12

D59827

(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

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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

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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

85W-24 02H-22 18

W184 XB12

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 ROUTING

D59848

(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

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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

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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

85W-24 02H-22 18

W184 XC12

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

12

D59856

(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

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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

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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

85W-24 02H-22 18

W184 XB12

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

11 12

D59858

(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

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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

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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

85W-24 02H-22 18

W184 XB12

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

11 12

D59861

(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

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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

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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

85W-24 02H-22 18

W184 XB12

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

11 12

D59866

(SHEET 1 OF 2)
 FIGURE 13: P36 Panel - Wiring Changes W/B0176, Groups 23-24 Airplanes.

May 03, 2006

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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

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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

85W-24 02H-22 18

W184 XB12

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 12

D59878

(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

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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

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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

85W-24 02H-22 18

W184 XB12

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

AE0209

D59882

(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

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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

85W-24 02H-22 18

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

8 10

7

02F-24

5

J

D4906P

4

J

D5658P

W0942

TB216

YA10

6

02F-24

6

11

9

(8 LOCATIONS) 2

1

1

(4 LOCATIONS)

(4 LOCATIONS)

AE0223

AE0209

12 13

D59888

(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

85W-24 02H-22 18

W184 XB12

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 12

D59900

(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

85W-24 02H-22 18

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

8 10

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

AE0209

D59907

(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

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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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D59910

(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

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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

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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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D59923

(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

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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

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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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D59927

(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

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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

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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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D59951

(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 airplanes

May 03, 2006

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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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D59956

(SHEET 1 OF 2)
 FIGURE 23: P36 Panel - Wiring Changes W/B0184, Groups 9, 11-15, 18-19, 21-24, 26-31, 33-34 airplanes

May 03, 2006

Revision 2: February 12, 2009 767-28A0083

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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

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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 ROUTING

D59977

(SHEET 1 OF 2)
 FIGURE 24: P36 Panel - Wiring Changes W/B0184, Groups 10, 20 Airplanes.

May 03, 2006

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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

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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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D59990

(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

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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

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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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D59994

(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

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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

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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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D59999

(SHEET 1 OF 2)
 FIGURE 27: P36 Panel - Wiring Changes W/B0184, Groups 25, 32 Airplanes.

May 03, 2006

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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.

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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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D60001

(SHEET 1 OF 2)
 FIGURE 28: P36 Panel - Wiring Changes W/B0184, Group 35 Airplanes.

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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.

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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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D60004

(SHEET 1 OF 2)
 FIGURE 29: P36 Panel - Wiring Changes W/B0184, Group36 Airplanes.

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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.

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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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D60013

(SHEET 1 OF 2)
 FIGURE 30: P36 Panel - Wiring Changes W/B0184, Group 37 Airplanes.

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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.

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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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D60014

(SHEET 1 OF 2)
 FIGURE 31: P36 Panel - Wiring Changes W/B0184, Group 38 Airplanes.

May 03, 2006

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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.

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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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D60022

(SHEET 1 OF 2)
 FIGURE 32: P36 Panel - Wiring Changes W/B0184, Group 39 Airplanes.

May 03, 2006

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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

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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

FWD

D60051

(SHEET 1 OF 2)
 FIGURE 33: P36 Panel - Relay Installation, Groups 1-39, 82-87 Airplanes

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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 --K10693 K10691

UP

FWD

A-A

1

2

D60052

(SHEET 2 OF 2)
 FIGURE 34: P37 Panel - Wiring Changes W/B0188, Group 1 Airplanes.

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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 ROUTING

D60055

(SHEET 1 OF 2)
 FIGURE 34: P37 Panel - Wiring Changes W/B0188, Group 1 Airplanes.

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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.

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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 ROUTING

D60057

(SHEET 1 OF 2)
 FIGURE 35: P37 Panel - Wiring Changes W/B0188, Groups 2-5, 7-9, 16, 82-87 Airplanes.

May 03, 2006

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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

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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 ROUTING

D60061

(SHEET 1 OF 2)
 FIGURE 36: P37 Panel - Wiring Changes W/B0188, Group 6 Airplanes.

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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.

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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 8

D60151

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

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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

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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 8

D60154

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

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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 8

D60157

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

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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)

10 11

D60187

(SHEET 1 OF 2)
 FIGURE 40: P37 Panel - Wiring Changes W/B0192, Group 1 Airplanes.

May 03, 2006

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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

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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)

10 11

D60191

(SHEET 1 OF 2)
 FIGURE 41: P37 Panel - Wiring Changes W/B0192, Groups 2-3, 82-83 Airplanes.

May 03, 2006

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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

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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 11

D60193

(SHEET 1 OF 2)
 FIGURE 42: P37 Panel - Wiring Changes W/B0192, Group 4, 84 Airplanes.

May 03, 2006

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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

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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)

10 11

D60194

(SHEET 1 OF 2)
 FIGURE 43: P37 Panel - Wiring Changes W/B0192, Groups 5, 8-9, 16, 85, 87 Airplanes

May 03, 2006

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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

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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)

10 11

D60197

(SHEET 1 OF 2)
 FIGURE 44: P37 Panel - Wiring Changes W/B0192, Group 6 Airplanes.

May 03, 2006

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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

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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)

10 11

D60202

(SHEET 1 OF 2)
 FIGURE 45: P37 Panel - Wiring Changes W/B0192, Group 7, 86 Airplanes.

May 03, 2006

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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

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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)

10 11

D60224

(SHEET 1 OF 2)
 FIGURE 46: P37 Panel - Wiring Changes W/B0192, Group 10 Airplanes.

May 03, 2006

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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

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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)

10 11

D60228

(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

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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

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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

79X-24 004-24 12

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)

10 11

D60236

(SHEET 1 OF 2)
 FIGURE 48: P37 Panel - Wiring Changes W/B0192, Groups 13, 22, 24, 27, 29-31 Airplanes.

May 03, 2006

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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

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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)

10 11

D60239

(SHEET 1 OF 2)
 FIGURE 49: P37 Panel - Wiring Changes W/B0192, Groups 18, 20, 32-34 Airplanes.

May 03, 2006

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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

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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)

10 11

D60242

(SHEET 1 OF 2)
 FIGURE 50: P37 Panel - Wiring Changes W/B0192, Group 35 Airplanes.

May 03, 2006

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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

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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)

10 11

D60244

(SHEET 1 OF 2)
 FIGURE 51: P37 Panel - Wiring Changes W/B0192, Group 37 Airplanes.

May 03, 2006

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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

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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

79X-24 004-24 12

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)

10 11

D60246

(SHEET 1 OF 2)
 FIGURE 52: P37 Panel - Wiring Changes W/B0192, Group 38 Airplanes.

May 03, 2006

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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

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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

79X-24 004-24 12

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)

10 11

D60247

(SHEET 1 OF 2)
 FIGURE 53: P37 Panel - Wiring Changes W/B0192, Group 39 Airplanes.

May 03, 2006

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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

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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 5

D60250

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

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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 5

D60255

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.

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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 5

D60258

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.

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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

02A-24 YA9

2

X2

4

TB212

W198

W192

REFERENCE: 767 WIRE DIAGRAMS 28-22-12

6 7

D60263

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.

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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

23 W192

REFERENCE: 767 WIRE DIAGRAMS 28-22-12

6 7

D60268

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.

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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

02A-24 YA7

2

X2

TB212

W198

W192

REFERENCE: 767 WIRE DIAGRAMS 28-22-12

4 5

D60270

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.

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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

W590 W192

1 2

REFERENCE: 767 WIRE DIAGRAMS 28-22-12

4 5

D60272

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.

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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

02A-24 YA7

2

X2

TB212

W198

W192

REFERENCE: 767 WIRE DIAGRAMS 28-22-12

4 5

D60276

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.

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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

6 W198- 02A-24

2

D5052P

YA7

J

W192

P37

TB212

RIGHT MISCELLANEOUS ELECTRICAL PANEL

5

6

REFERENCE: 767 WIRE DIAGRAMS 28-22-12

D60350

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

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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

02A-24 YA7

REFERENCE: 767 WIRE DIAGRAMS 28-22-12

4

5

D60353

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

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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

W590 W192

REFERENCE: 767 WIRE DIAGRAMS 28-22-12

4

5

D60355

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.

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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 5

D60356

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

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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 5

D60357

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

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FIGURE 67: P37 Panel - Relay Installation, Groups 1-39, 82-87 Airplanes.

MAIN EQUIPMENT CENTER

P37 PANEL

A

A

FWD

FWD

UP

D60360

(SHEET 1 OF 2)
 FIGURE 67: P37 Panel - Relay Installation, Groups 1-39, 82-87 Airplanes.

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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-A

K10692

K10690

FWD

UP

1

2

D60361

(SHEET 2 OF 2)
 FIGURE 68: P37 Panel - Wiring Changes W/B0198, Group 38 Airplanes.

May 03, 2006

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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

19 W198- 02A-24

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 ROUTING

D60358

(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.

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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

W184 16A-22

D8026P

41

J

23

D4042P

W146

J

1 1

LEFT MISC.

ELECTRICAL EQPT PANEL

2

P36

REFERENCE: 767 WIRE DIAGRAMS 28-42-12

4 5

D60362

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

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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

W184 16A-22

D8026P

54

J

23

D4042P

W146

J

1 1

LEFT MISC.

ELECTRICAL EQPT PANEL

2

REFERENCE: 767 WIRE DIAGRAMS 28-42-12

4 5

D60363

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.

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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

W184 16A-22

D8026P

40

J

23

D4042P

W146

J

1 1

LEFT MISC.

ELECTRICAL EQPT PANEL

2

P36

REFERENCE: 767 WIRE DIAGRAMS 28-42-12

4 5

D60365

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.

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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

W184 16A-22

D8026P

34

J

23

D4042P

W146

J

1 1

LEFT MISC.

ELECTRICAL EQPT PANEL

2

REFERENCE: 767 WIRE DIAGRAMS 28-42-12

4 5

D60366

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.

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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

W184 021-24

D4856P

13

J

12

D5052P

W198

J

1 2

LEFT MISC.

ELECTRICAL EQPT PANEL

3

P36

5

6

REFERENCE: 767 WIRE DIAGRAMS 28-42-12

D60380

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.

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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

W184 021-24

D4856P

13

J D5052P

W198

J

1 2

LEFT MISC.

ELECTRICAL EQPT PANEL

3

13

5

6

REFERENCE: 767 WIRE DIAGRAMS 28-42-12

D60383

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.

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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

W184 021-24

D4856P

2

J

19

D5052P

W146

J

1 2

LEFT MISC.

ELECTRICAL EQPT PANEL

3

P36

REFERENCE: 767 WIRE DIAGRAMS 28-42-12

5

6

D60393

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.

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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

W184 021-24

D4856P

13

J

6

D5052P

W198

J

1 2

LEFT MISC.

ELECTRICAL EQPT PANEL

4

3

REFERENCE: 767 WIRE DIAGRAMS 28-42-12

6

7

D60401

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 Airplanes.

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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

W184 021-24

D4856P

13

J

19

D5052P

W198

J

1 2

LEFT MISC.

ELECTRICAL EQPT PANEL

3

REFERENCE: 767 WIRE DIAGRAMS 28-42-12

5

6

D60403

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.

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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

W176 011-24

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 ROUTING

D60437

(SHEET 1 OF 1)
 FIGURE 79: P37 Panel - Wiring Changes W/B1118, Group 39 Airplanes

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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

13 W1118- 14A-24

D6658P

W942 YC12

2

3

AE0218

J

W192

P37 RIGHT MISCELLANEOUS ELECTRICAL PANEL

TB212

REFERENCE: 767 WIRE DIAGRAMS 28-22-12

4

5

D60457

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.

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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

5

D60468

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.

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FIGURE 81: Wire Bundle Routing, P36 to P37 Panel, Groups 1-39, 82-87 Airplanes.

P36

P37

P33

FWD

1 3

2 3

D60470

(SHEET 1 OF 3)
 FIGURE 81: Wire Bundle Routing, P36 to P37 Panel, Groups 1-39, 82-87 Airplanes.

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

P36

P37

P33

ALTERNATE

WIRE ROUTING

CONFIGURATION

FWD

1 3

2 3

1561302

(SHEET 2 OF 3)
 FIGURE 81: Wire Bundle Routing, P36 to P37 Panel, Groups 1-39, 82-87 Airplanes.

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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.

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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

CONFIGURATION

J82159

(SHEET 1 OF 4)
 FIGURE 82: P36 Panel - Bracket Installation, Group 40-79, 88 Airplanes.

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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

UP

J82158

(SHEET 2 OF 4)
 FIGURE 82: P36 Panel - Bracket Installation, Group 40-79, 88 Airplanes.

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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

UP

1561717

(SHEET 3 OF 4)
 FIGURE 82: P36 Panel - Bracket Installation, Group 40-79, 88 Airplanes.

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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.

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FIGURE 83: P37 Panel - Bracket Installation, Groups 40-79, 88 Airplanes.

MAIN EQUIPMENT CENTER

A

A

P37 PANEL

FWD

1

FWD

UP

4

J82157

(SHEET 1 OF 3)
 FIGURE 83: P37 Panel - Bracket Installation, Groups 40-79, 88 Airplanes.

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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

3

J82156

(SHEET 2 OF 3)
 FIGURE 83: P37 Panel - Bracket Installation, Groups 40-79, 88 Airplanes.

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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.

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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

85W-24 02H-22 18

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

W184 53C-22

6

3

02F-24

J

4

D5658P TB216 02F-24

YA10

TB218

XB12 6

9

W184

W184

2 (11 LOCATIONS)

1

1

(4 LOCATIONS)

(4 LOCATIONS)

11

10

AE0223

AE0209

D59731

(SHEET 1 OF 2)
 FIGURE 84: P36 Panel - Wiring Changes W/B0176, Group 40 Airplanes.

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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

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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

53C-22 W184

TB218

XD3

7

2

6

4

12

13

11

10

9

8

(10 LOCATIONS) 3

1

1

(4 LOCATIONS)

(4 LOCATIONS)

AE0223

AE0209

14 15

D59736

(SHEET 1 OF 2)
 FIGURE 85: P36 Panel - Wiring Changes W/B0176, Groups 42, 67-68 Airplanes.

May 03, 2006

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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

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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

53C-22 W184

TB218

XD3

7

2

6

4

12

13

11

10

9

8

(10 LOCATIONS) 3

1

1

(4 LOCATIONS)

(4 LOCATIONS)

AE0223

AE0209

14 15

D59738

(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

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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

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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

53C-22 W184

TB218

XD3

7

2

6

4

12

13

11

10

9

8

(10 LOCATIONS) 3

1

1

(4 LOCATIONS)

(4 LOCATIONS)

14 15

AE0223

AE0209

D59740

(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

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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

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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

53C-22 W184

TB218

XD3

7

2

6

4

12

13

11

10

9

8

(10 LOCATIONS) 3

1

1

(4 LOCATIONS)

(4 LOCATIONS)

AE0223

AE0209

14 15

D59741

(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

53C-22 W184

TB218

XD3

7

2

6

4

12

13

11

10

9

8

(10 LOCATIONS) 3

1

1

(4 LOCATIONS)

(4 LOCATIONS)

14 15

AE0223

AE0209

D59742

(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

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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

85W-24 02H-22 18

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

W184 53C-22

6

3

02F-24

J

4

D5658P TB216 02F-24

YA10

TB218

XB12 6

9

W184

W184

2 (11 LOCATIONS)

1

1

(4 LOCATIONS)

(4 LOCATIONS)

11 12

AE0223

AE0209

D59744

(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

53C-22 W184

TB218

XD3

7

2

6

4

12

11

10

9

8

3 (11 LOCATIONS)

1

1

(4 LOCATIONS)

(4 LOCATIONS)

13 14

AE0223

AE0209

D59747

(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

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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

53C-22 W184

TB218

XD3

7

2

6

4

12

11

10

9

8

3 (11 LOCATIONS)

1

1

(4 LOCATIONS)

(4 LOCATIONS)

13 14

AE0223

AE0209

D59750

(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

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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

53C-22 W184

TB218

XD3

7

2

6

4

12

11

10

9

8

3 (11 LOCATIONS)

1

1

(4 LOCATIONS)

(4 LOCATIONS)

13 14

AE0223

AE0209

D59751

(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

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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

53C-22 W184

TB218

XD3

7

2

6

4

12

11

10

9

8

3 (11 LOCATIONS)

1

1

(4 LOCATIONS)

(4 LOCATIONS)

13 14

AE0223

AE0209

D59754

(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

53C-22 W184

TB218

XD3

7

2

6

4

12

11

10

9

8

3 (11 LOCATIONS)

1

1

(4 LOCATIONS)

(4 LOCATIONS)

13 14

AE0223

AE0209

D59756

(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

53C-22 W184

TB218

XD3

7

2

6

4

12

11

10

9

8

3 (11 LOCATIONS)

1

1

(4 LOCATIONS)

(4 LOCATIONS)

13 14

AE0223

AE0209

D59759

(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

53C-22 W184

TB218

XD3

7

2

6

4

12

11

10

9

8

3 (11 LOCATIONS)

1

1

(4 LOCATIONS)

(4 LOCATIONS)

13 14

AE0223

AE0209

D59763

(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

53C-22 W184

TB218

XD3

7

2

6

4

12

11

10

9

8

3 (11 LOCATIONS)

1

1

(4 LOCATIONS)

(4 LOCATIONS)

AE0223

AE0209

13 14

D59988

(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

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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

53C-22 W184

TB218

XD3

7

2

6

4

12

11

10

9

8

3 (11 LOCATIONS)

1

1

(4 LOCATIONS)

(4 LOCATIONS)

TB218

AE0223

AE0209

13 14

D59991

(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

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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

53C-22 W184

TB218

XD3

7

2

6

4

12

11

10

9

8

3 (11 LOCATIONS)

1

1

(4 LOCATIONS)

(4 LOCATIONS)

AE0223

AE0209

13 14

D59993

(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

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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

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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

53C-22 W184

TB218

XD3

7

2

6

4

12

11

10

9

8

3 (11 LOCATIONS)

1

1

(4 LOCATIONS)

(4 LOCATIONS)

AE0223

AE0209

13 14

D59995

(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

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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

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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

53C-22 W184

TB218

XD3

7

2

6

4

12

11

10

9

8

3 (11 LOCATIONS)

1

1

(4 LOCATIONS)

(4 LOCATIONS)

AE0223

AE0209

13 14

D59996

(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

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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

53C-22 W184

TB218

XD3

7

2

6

4

12

11

10

9

8

3 (11 LOCATIONS)

1

1

(4 LOCATIONS)

(4 LOCATIONS)

13 14

AE0223

AE0209

D59998

(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

53C-22 W184

TB218

XD3

7

2

6

4

12

11

10

9

8

3 (11 LOCATIONS)

1

1

(4 LOCATIONS)

(4 LOCATIONS)

AE0223

AE0209

13 14

D60028

(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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D60029

(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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D60266

(SHEET 1 OF 2)
 FIGURE 106: P36 Panel - Wiring Changes W/B0184, Groups 62-63 Airplanes.

May 03, 2006

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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

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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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D60318

(SHEET 1 OF 2)
 FIGURE 107: P36 Panel - Wiring Changes W/B0184, Group 56 Airplanes.

May 03, 2006

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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

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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 10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D60319

(SHEET 1 OF 2)
 FIGURE 108: P36 Panel - Wiring Changes W/B0184, Groups 44, 72-75 Airplanes.

May 03, 2006

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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

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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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D60320

(SHEET 1 OF 2)
 FIGURE 109: P36 Panel - Wiring Changes W/B0184, Groups 65, 69 Airplanes.

May 03, 2006

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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

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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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D60321

(SHEET 1 OF 2)
 FIGURE 110: P36 Panel - Wiring Changes W/B0184, Groups 52-53, 78 Airplanes.

May 03, 2006

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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

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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

10 11

ADDED WIRE OR NEW ROUTING

EXISTING WIRE

DELETED WIRE OR FORMER ROUTING

D60322

(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

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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

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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

10 11

D60323

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

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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

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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

10 11

D60324

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

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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

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BOEING SERVICE BULLETIN 767-28A0083

FIGURE 114: P36 Panel - Relay Installation, Groups 40-79, 88 Airplanes.

P36 PANEL

MAIN EQUIPMENT CENTER

A

A

FWD

FWD

J82100

(SHEET 1 OF 2)
 FIGURE 114: P36 Panel - Relay Installation, Groups 40-79, 88 Airplanes.

May 03, 2006

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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 --K10693 K10691

UP

FWD

A-A

1

2

J82099

(SHEET 2 OF 2)
 FIGURE 115: P37 Panel - Wiring Changes W/B0188, Group 55 Airplanes.

May 03, 2006

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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 9

D60325

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.

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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 Airplanes.

May 03, 2006

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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 8

D60538

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 Airplanes.

May 03, 2006

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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

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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 8

D60540

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

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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

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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 8

D60543

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

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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

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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 8

D60547

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

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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 8

D60550

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

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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

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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 13

D60553

(SHEET 1 OF 2)
 FIGURE 121: P37 Panel - Wiring Changes W/B0192, Group 61 Airplanes.

May 03, 2006

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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

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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 13

D60642

(SHEET 1 OF 2)
 FIGURE 122: P37 Panel - Wiring Changes W/B0192, Group 62 Airplanes.

May 03, 2006

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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, Airplanes.

May 03, 2006

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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 13

D60557

(SHEET 1 OF 2)
 FIGURE 123: P37 Panel - Wiring Changes W/B0192, Groups 41, 43-45, 57, 59, 64, 69-70, 72, 74, Airplanes.

May 03, 2006

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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

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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 13

D60558

(SHEET 1 OF 2)
 FIGURE 124: P37 Panel - Wiring Changes W/B0192, Groups 42, 67-68, 76 Airplanes.

May 03, 2006

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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

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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 11

D60562

(SHEET 1 OF 2)
 FIGURE 125: P37 Panel - Wiring Changes W/B0192, Groups 40, 66 Airplanes.

May 03, 2006

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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

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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 13

D60564

(SHEET 1 OF 2)
 FIGURE 126: P37 Panel - Wiring Changes W/B0192, Group 55 Airplanes.

May 03, 2006

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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

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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 13

D60566

(SHEET 1 OF 2)
 FIGURE 127: P37 Panel - Wiring Changes W/B0192, Group 56 Airplanes.

May 03, 2006

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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

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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 13

D60568

(SHEET 1 OF 2)
 FIGURE 128: P37 Panel - Wiring Changes W/B0192, Group 54 Airplanes.

May 03, 2006

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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

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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 13

D60571

(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

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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

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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 13

D60572

(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

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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

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BOEING SERVICE BULLETIN 767-28A0083

FIGURE 131: P37 Panel - Wiring Changes W/B0192, Groups 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 13

D60573

(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

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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

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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 13

D60574

(SHEET 1 OF 2)
 FIGURE 132: P37 Panel - Wiring Changes W/B0192, Group 63 Airplanes.

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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

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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

02A-24 YA11

188-24 X1

TB82

W198

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

4 5

D60578

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

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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 5

D60582

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

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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

19 W198- 02A-24

1

D5052P

YC11

J

W192

P37

TB212

RIGHT MISCELLANEOUS ELECTRICAL PANEL

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

4 5

D60586

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

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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

02A-24 YA7

188-24 X1

TB82

W198

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

4 5

D60589

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

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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

02A-24 YA7

188-24 X1

TB82

W198

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

4 5

D60592

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

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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

12 W198- 02A-24

1

D5052P

YA7

J

W192

P37

TB212

RIGHT MISCELLANEOUS ELECTRICAL PANEL

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

4 5

D60594

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

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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

19 W198- 02A-24

1

D5052P

YA7

J

W192

P37

TB212

RIGHT MISCELLANEOUS ELECTRICAL PANEL

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

4 5

D60596

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

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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

12 W198- 02A-24

1

D5052P

YC12

J

W192

P37

TB212

RIGHT MISCELLANEOUS ELECTRICAL PANEL

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

4 5

D60599

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

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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

19 W198- 02A-24

1

D5052P

YC12

J

W192

P37

TB212

RIGHT MISCELLANEOUS ELECTRICAL PANEL

REFERENCE: 767 WIRE DIAGRAMS 28-22-12

4 5

D60601

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

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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

13 W198- 02A-24

1

D5052P

YC12

J

W192

P37

TB212

RIGHT MISCELLANEOUS ELECTRICAL PANEL

REFERENCE: 767 WIRE DIAGRAMS 28-22-12

4 5

D60604

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

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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

UP

J81862

(SHEET 1 OF 2)
 FIGURE 143: P37 Panel - Relay Installation, Groups 40-79, 88 Airplanes.

May 03, 2006

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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-A

K10692

K10690

FWD

UP

1

2

J81861

(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

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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

W184 021-24

D4856P

13

J

19

D5052P

W198

J

1 2

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 ROUTING

D60607

(SHEET 1 OF 1)
 FIGURE 145: P36 to P37 Panel - Wiring Changes W/B0590, Groups 61-63 Airplanes.

May 03, 2006

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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

W184 021-24

D4856P

2

J D5052P

W198

J

1 2

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 ROUTING

D60609

(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

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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

W184 021-24

D4856P

13

J

12

D5052P

W198

J

1 2

LEFT MISC.

ELECTRICAL EQPT PANEL

3

P36

REFERENCE: 767 WIRE DIAGRAMS 28-42-12

5

6

D60611

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

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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

W184 021-24

D4856P

13

J D5052P

W198

J

1 2

LEFT MISC.

ELECTRICAL EQPT PANEL

3

13

REFERENCE: 767 WIRE DIAGRAMS 28-42-12

5

6

D60612

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.

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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

W176 011-24

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 ROUTING

D60615

(SHEET 1 OF 1)
 FIGURE 149: P36 to P37 Panel - Wiring Changes W/B0942, Group 55 Airplane.

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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

W176 011-24

D4906P

5

J D7352P

W188

J

1 2

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 ROUTING

D60617

(SHEET 1 OF 1)
 FIGURE 150: P37 Panel - Wiring Changes W/B1118, Groups 49, 54, 79, 88 Airplanes.

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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

13 W1118- 14A-24

D6658P

W942 YC12

2

3

AE0218

J

W192

P37 RIGHT MISCELLANEOUS ELECTRICAL PANEL

TB212

REFERENCE 767 WIRE DIAGRAM 28-22-12

4

5

D60620

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.

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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

5

D60674

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.

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FIGURE 152: Wiring Bundle Routing, P36 to P37 Panel, Groups 40-79 and 88 Airplanes.

P36

P37

P33

FWD

1 2

J81855

(SHEET 1 OF 3)
 FIGURE 152: Wiring Bundle Routing, P36 to P37 Panel, Groups 40-79 and 88 Airplanes.

May 03, 2006

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This Figure applies to Group 40-79, 88: 

P36

P37

P33

ALTERNATE

WIRE ROUTING

FWD

1 2

1556148

(SHEET 2 OF 3)
 FIGURE 152: Wiring Bundle Routing, P36 to P37 Panel, Groups 40-79 and 88 Airplanes.

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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.

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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 28-22-12

D60675

(SHEET 1 OF 1)
 FIGURE 154: P36 Panel - Relay Installation, Group 80-81 and 89 Airplanes.

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FIGURE 154: P36 Panel - Relay Installation, Group 80-81 and 89 Airplanes.

P36 PANEL

MAIN EQUIPMENT CENTER

1 4

SEE A

FWD

FWD

D60676

(SHEET 1 OF 2)
 FIGURE 154: P36 Panel - Relay Installation, Group 80-81 and 89 Airplanes.

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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

A

D60677

(SHEET 2 OF 2)
 FIGURE 155: P37 Panel - Wiring Changes W/B0192 and W/B1118, Group 80 Airplanes.

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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 28-22-12

D60678

(SHEET 1 OF 1)
 FIGURE 156: P37 Panel - Wiring Changes W/B0192 and W/B0188, Group 81 Airplanes.

May 03, 2006

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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 28-22-12

1561742

(SHEET 1 OF 1)
 FIGURE 157: P37 Panel - Relay Installation, Group 80-81 and 89 Airplanes.

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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 A

D60679

(SHEET 1 OF 3)
 FIGURE 157: P37 Panel - Relay Installation, Group 80-81 and 89 Airplanes.

May 03, 2006

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BOEING SERVICE BULLETIN 767-28A0083

This Figure applies to Group 80-81, 89: 

UPPER RELAY PANEL

FWD

2 3

A

D60681

(SHEET 2 OF 3)
 FIGURE 157: P37 Panel - Relay Installation, Group 80-81 and 89 Airplanes.

May 03, 2006

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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

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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 ROUTING

1310271

(SHEET 1 OF 2)
 FIGURE 158: P37 Panel - Wiring Changes W/B0188, Groups 82-87 airplanes.

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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

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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

53C-22 W184

TB218

XD3

7

2

6

4

12

13

11

10

9

8

(10 LOCATIONS) 3

1

1

(4 LOCATIONS)

(4 LOCATIONS)

AE0223

14 15

1561744

(SHEET 1 OF 2)
 FIGURE 159: P37 Panel - Wiring Changes W/B0176 Group 88

May 03, 2006

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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

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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

W176 011-24

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 ROUTING

1561746

(SHEET 1 OF 1)
 FIGURE 161: P37 Panel - Wiring Changes W/B0192 and W/B198, Group 89

May 03, 2006

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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 28-22-12

1561747

(SHEET 1 OF 1)