ALERT ALERT Commercial Airplane Group 737 Service Bulletin ALERTALERT Number: 737-31A1325 Date: January 11, 2010 ATA System: 3100
SUBJECT: INDICATING / RECORDING SYSTEMS - Aural Warning System - Installation of the Cabin Altitude Warning System and Takeoff Configuration Warning System Lights
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Table of Contents Summary ...... 7 1. PLANNING INFORMATION ...... 11 A. Effectivity ...... 11 1. Airplanes ...... 11 2. Spares Affected ...... 59 B. Concurrent Requirements ...... 59 C. Reason ...... 59 D. Description ...... 59 E. Compliance...... 59 F. Approval ...... 60 G. Manpower ...... 60 H. Weight and Balance Changes ...... 61 I. Electrical Load Data ...... 61 J. References ...... 61 1. Existing Data: ...... 61 2. Data supplied with this Service Bulletin: ...... 61 3. Installation Drawings Used in the Preparation of this Service Bulletin: ...... 61 K. Publications Affected ...... 62 L. Interchangeability and Intermixability of Parts ...... 62 2. MATERIAL INFORMATION ...... 63 A. Material - Price and Availability...... 63 B. Industry Support Information ...... 65 C. Parts Necessary For Each Airplane ...... 66
1. Kits/Parts: ...... 66 2. Parts and Materials Supplied by the Operator: ...... 68 3. Parts Modified and Reidentified: ...... 68 4. Parts Removed and Not Replaced: ...... 73 D. Parts Necessary to Change Spares ...... 73 E. Special Tooling - Price and Availability...... 73 F. Special Tooling Necessary to do this Service Bulletin ...... 73 3. ACCOMPLISHMENT INSTRUCTIONS ...... 75 A. GENERAL INFORMATION ...... 75 B. WORK INSTRUCTIONS ...... 75 FIGURE 1: P2-2 CENTER INSTRUMENT PANEL REMOVAL ...... 83 FIGURE 2: MODIFICATION OF THE P2-2 CENTER INSTRUMENT PANEL...... 85 FIGURE 3: LIGHT ASSEMBLY INSTALLATION ...... 88 FIGURE 4: WIRE BUNDLE W066 WIRE ROUTING - GROUPS 1-29, 31-36, 38 AND 43 AIRPLANES 91 FIGURE 5: WIRE BUNDLE W066 WIRE ROUTING - GROUP 37 AIRPLANES ...... 92 FIGURE 6: WIRE BUNDLE W066 WIRE ROUTING - GROUPS 30, 39-42 AND 44-48 AIRPLANES . 93 FIGURE 7: WIRE BUNDLES W002 AND W066 WIRE ROUTING - GROUP 49 AIRPLANES . . . . . 94 FIGURE 8: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 14 AND 17 AIRPLANES ...... 96 FIGURE 9: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 1, 4, 24 AND 43 AIRPLANES . . . 98 FIGURE 10: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 15 AND 25 AIRPLANES . . . . . 100 FIGURE 11: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 6 AND 23 AIRPLANES ...... 102 FIGURE 12: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 7 AND 8 AIRPLANES ...... 104
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FIGURE 13: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 5 AND 9 AIRPLANES ...... 106 FIGURE 14: WIRE BUNDLE W066 WIRING CHANGE - GROUP 10 AIRPLANES ...... 108 FIGURE 15: WIRE BUNDLE W066 WIRING CHANGE - GROUP 16 AIRPLANES ...... 110 FIGURE 16: WIRE BUNDLE W066 WIRING CHANGE - GROUP 3 AIRPLANES ...... 112 FIGURE 17: WIRE BUNDLE W066 WIRING CHANGE - GROUP 18 AIRPLANES ...... 114 FIGURE 18: WIRE BUNDLE W066 WIRING CHANGE - GROUP 19 AIRPLANES ...... 116 FIGURE 19: WIRE BUNDLE W066 WIRING CHANGE - GROUP 20 AIRPLANES ...... 118 FIGURE 20: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 21 AND 22 AIRPLANES . . . . . 120 FIGURE 21: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 2 AND 13 AIRPLANES . . . . . 122 FIGURE 22: WIRE BUNDLE W066 WIRING CHANGE - GROUP 11 AIRPLANES ...... 124 FIGURE 23: WIRE BUNDLE W066 WIRING CHANGE - GROUP 26 AIRPLANES ...... 126 FIGURE 24: WIRE BUNDLE W066 WIRING CHANGE - GROUP 27 AIRPLANES ...... 128 FIGURE 25: WIRE BUNDLE W066 WIRING CHANGE - GROUP 28 AIRPLANES ...... 130 FIGURE 26: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 12 AND 29 AIRPLANES . . . . . 132 FIGURE 27: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 31 AND 32 AIRPLANES . . . . . 134 FIGURE 28: WIRE BUNDLE W066 WIRING CHANGE - GROUP 33 AIRPLANES ...... 136 FIGURE 29: WIRE BUNDLE W066 WIRING CHANGE - GROUP 34 AIRPLANES ...... 138 FIGURE 30: WIRE BUNDLE W066 WIRING CHANGE - GROUP 35 AIRPLANES ...... 140 FIGURE 31: WIRE BUNDLE W066 WIRING CHANGE - GROUP 36 AIRPLANES ...... 142 FIGURE 32: WIRE BUNDLE W066 WIRING CHANGE - GROUP 37 AIRPLANES ...... 144 FIGURE 33: WIRE BUNDLE W066 WIRING CHANGE - GROUP 38 AIRPLANES ...... 146 FIGURE 34: WIRE BUNDLE W066 WIRING CHANGE - GROUP 39 AIRPLANES ...... 148 FIGURE 35: WIRE BUNDLE W066 WIRING CHANGE - GROUP 40 AIRPLANES ...... 150 FIGURE 36: WIRE BUNDLE W066 WIRING CHANGE - GROUP 41 AIRPLANES ...... 152
FIGURE 37: WIRE BUNDLE W066 WIRING CHANGE - GROUP 42 AIRPLANES ...... 154 FIGURE 38: WIRE BUNDLE W066 WIRING CHANGE - GROUP 30 AIRPLANES ...... 156 FIGURE 39: WIRE BUNDLE W066 WIRING CHANGE - GROUP 44 AIRPLANES ...... 158 FIGURE 40: WIRE BUNDLE W066 WIRING CHANGE - GROUP 45 AIRPLANES ...... 160 FIGURE 41: WIRE BUNDLE W066 WIRING CHANGE - GROUP 46 AIRPLANES ...... 162 FIGURE 42: WIRE BUNDLE W066 WIRING CHANGE - GROUP 47 AIRPLANES ...... 164 FIGURE 43: WIRE BUNDLE W066 WIRING CHANGE - GROUP 48 AIRPLANES ...... 166 FIGURE 44: WIRE BUNDLE W066 WIRING CHANGE - GROUP 49 AIRPLANES ...... 168 FIGURE 45: WIRE BUNDLE W002 WIRE ROUTING - GROUPS 1-29, 31, 38 AND 43 AIRPLANES. 170 FIGURE 46: WIRE BUNDLE W002 WIRE ROUTING - GROUPS 30, 39-42 AND 44-48 AIRPLANES 171 FIGURE 47: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 1, 3, 5-10, 15-20, 23 AND 25 AIRPLANES ...... 172 FIGURE 48: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 2, 13 AND 21-22 AIRPLANES. . 174 FIGURE 49: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 11 AND 26-28 AIRPLANES . . . 176 FIGURE 50: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 12, 29, 31 AND 32 AIRPLANES . 178 FIGURE 51: WIRE BUNDLE W002 WIRING CHANGE - GROUP 33 AIRPLANES ...... 180 FIGURE 52: WIRE BUNDLE W002 WIRING CHANGE - GROUP 34 AIRPLANES ...... 182 FIGURE 53: WIRE BUNDLE W002 WIRING CHANGE - GROUP 35 AIRPLANES ...... 184 FIGURE 54: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 36 AND 37 AIRPLANES . . . . . 186 FIGURE 55: WIRE BUNDLE W002 WIRING CHANGE - GROUP 38 AIRPLANES ...... 188 FIGURE 56: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 4, 14 AND 43 AIRPLANES . . . 190 FIGURE 57: WIRE BUNDLE W002 WIRING CHANGE - GROUP 24 AIRPLANES ...... 192
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FIGURE 58: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 30 AND 39-42 AIRPLANES. . . . 194 FIGURE 59: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 44, 45, 46, 47 AND 48 AIRPLANES . 196 FIGURE 60: WIRE BUNDLE W002 WIRING CHANGE - GROUP 49 AIRPLANES ...... 198 FIGURE 61: WIRE BUNDLE W246 WIRE ROUTING ...... 200 FIGURE 62: WIRE BUNDLE W246 WIRING CHANGE - GROUPS 1, 3, 5, 8, 10, 11, 13, 15-21, 23, 26-31, 33-34, 36-39, 41-42, 44 AND 46-49 AIRPLANES ...... 203 FIGURE 63: WIRE BUNDLE W246 WIRING CHANGE - GROUPS 2, 6, 7, 9, 12, 22, 25, 32, 35, 40 AND 45 AIRPLANES ...... 205 FIGURE 64: WIRE BUNDLE W246 WIRING CHANGE - GROUPS 4 AND 14 AIRPLANES ...... 207 FIGURE 65: WIRE BUNDLE W246 WIRING CHANGE - GROUP 24 AIRPLANES ...... 209 FIGURE 66: WIRE BUNDLE W246 WIRING CHANGE - GROUP 43 AIRPLANES ...... 211 FIGURE 67: P2-2 CENTER INSTRUMENT PANEL INSTALLATION ...... 213
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Table of Contents January 11, 2010 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 6 of 214 ALERT ALERT Commercial Airplanes 737 Service Bulletin ALERTALERT Number: 737-31A1325 Summary Original Issue: January 11, 2010 ATA System: 3100
SUBJECT: INDICATING / RECORDING SYSTEMS - Aural Warning System - Installation of the Cabin Altitude Warning System and Takeoff Configuration Warning System Lights
THIS BULLETIN IS SENT TO THE OPERATORS OF RECORD OF THE AIRPLANES SHOWN IN PARAGRAPH 1.A., EFFECTIVITY. IF AN AIRPLANE HAS BEEN LEASED OR SOLD, SEND THIS SERVICE BULLETIN TO THE NEW OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS SERVICE BULLETIN TO THE NEW OWNER.
CONCURRENT REQUIREMENTS
None
BACKGROUND
This service bulletin gives instructions to install two warning level indicator lights on the P2-2 center instrument panel in the flight compartment. The installation of these lights will provide a visual indication to the flight crew to be used in conjuction with the existing aural warning horn for cabin altitude and takeoff configuration alerts. The visual warning lights are intended to provide additional notice to crews to prepare a correct takeoff configuration, respond to excessive cabin altitude and avoid confusion between the takeoff configuration and cabin altitude alerts. An unrecognized incorrect takeoff configuration or excessive cabin altitude could prevent a continued safe flight and landing.
As a part of a service bulletin validation program, this change was completed on airplane PW234 by Service Bulletin 737-31A1325 Validation Copy 1 and Installation Deviation Records 737-31A1325-001 through 737- 31A1325-006 before the initial release of this service bulletin. The change completed on airplane PW234 by Service Bulletin 737-31A1325 Validation Copy 1 and Installation Deviation Records 737-31A1325-001 through 737-31A1325-006 is equivalent to the initial release of this service bulletin. Airplane PW234 has the configuration of a Group 13 airplane.
Boeing Service Related Problem (SRP) 737-SRP-31-0042 is related to this service bulletin.
ACTION
Get access to the flight compartment. Remove the P2-2 center instrument panel to install two warning level indicator lights on the panel and change three wire bundles. Reinstall the modified P2-2 center instrument panel. Do a test of the warning level indicator lights.
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EFFECTIVITY
All 737-100/-200/-200C/-300/-400/-500 Airplanes. Refer to Paragraph 1.A.1 Airplanes, for the list of affected airplanes.
COMPLIANCE
The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to this service bulletin. The Airworthiness Directive will make the compliance tasks and times given in this service bulletin mandatory.
Boeing recommends that the change given in this service bulletin be done within 36 months after the date on this service bulletin.
INDUSTRY SUPPORT INFORMATION
Boeing warranty remedies are not available for the configuration changes given in this service bulletin.
MANPOWER
Airplanes Total Task Hours Elapsed Hours Groups 1-49 32.50 20.50
MATERIAL INFORMATION
Boeing Supplied Kits/Parts.
Refer to Paragraph 2.A., Material - Price and Availability.
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MODIFY P2-2 PANEL AND INSTALL LIGHT ASSEMBLIES P2-2 CENTER CHANGE WIRE INSTRUMENT PANEL BUNDLES W002 AND W066 P9 PANEL P6 LOAD CONTROL CENTER
CHANGE WIRE BUNDLE W246 1376079
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Original Issue: January 11, 2010 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 10 of 214 ALERT ALERT Commercial Airplanes 737 Service Bulletin ALERTALERT Number: 737-31A1325 Original Issue: January 11, 2010 ATA System: 3100
SUBJECT: INDICATING / RECORDING SYSTEMS - Aural Warning System - Installation of the Cabin Altitude Warning System and Takeoff Configuration Warning System Lights
THIS BULLETIN IS SENT TO THE OPERATORS OF RECORD OF THE AIRPLANES SHOWN IN PARAGRAPH 1.A., EFFECTIVITY. IF AN AIRPLANE HAS BEEN LEASED OR SOLD, SEND THIS SERVICE BULLETIN TO THE NEW OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS SERVICE BULLETIN TO THE NEW OWNER.
1. PLANNING INFORMATION
A. Effectivity
1. Airplanes
Refer to Service Bulletin Index Document D6-19567 Part 3 for Airplane Variable Number, Line
Number, and Serial Number data.
This service bulletin is for the airplanes shown below. Refer to PRR 35005-277RS for data about this change.
GROUP CONFIGURATION DESCRIPTION 1 - Wiring and P2 panel configuration differences 2 - Wiring and P2 panel configuration differences 3 - Wiring and P2 panel configuration differences 4 - Wiring and P2 panel configuration differences 5 - Wiring and P2 panel configuration differences 6 - Wiring and P2 panel configuration differences 7 - Wiring and P2 panel configuration differences 8 - Wiring and P2 panel configuration differences 9 - Wiring and P2 panel configuration differences 10 - Wiring and P2 panel configuration differences 11 - Wiring and P2 panel configuration differences 12 - Wiring and P2 panel configuration differences 13 - Wiring and P2 panel configuration differences
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GROUP CONFIGURATION DESCRIPTION 14 - Wiring and P2 panel configuration differences 15 - Wiring and P2 panel configuration differences 16 - Wiring and P2 panel configuration differences 17 - Wiring and P2 panel configuration differences 18 - Wiring and P2 panel configuration differences 19 - Wiring and P2 panel configuration differences 20 - Wiring and P2 panel configuration differences 21 - Wiring and P2 panel configuration differences 22 - Wiring and P2 panel configuration differences 23 - Wiring and P2 panel configuration differences 24 - Wiring and P2 panel configuration differences 25 - Wiring and P2 panel configuration differences 26 - Wiring and P2 panel configuration differences 27 - Wiring and P2 panel configuration differences 28 - Wiring and P2 panel configuration differences 29 - Wiring and P2 panel configuration differences 30 - Wiring and P2 panel configuration differences 31 - Wiring and P2 panel configuration differences 32 - Wiring and P2 panel configuration differences 33 - Wiring and P2 panel configuration differences
34 - Wiring and P2 panel configuration differences 35 - Wiring and P2 panel configuration differences 36 - Wiring and P2 panel configuration differences 37 - Wiring and P2 panel configuration differences 38 - Wiring and P2 panel configuration differences 39 - Wiring and P2 panel configuration differences 40 - Wiring and P2 panel configuration differences 41 - Wiring and P2 panel configuration differences 42 - Wiring and P2 panel configuration differences 43 - Wiring and P2 panel configuration differences 44 - Wiring and P2 panel configuration differences 45 - Wiring and P2 panel configuration differences 46 - Wiring and P2 panel configuration differences 47 - Wiring and P2 panel configuration differences 48 - Wiring and P2 panel configuration differences 49 - Wiring and P2 panel configuration differences
Airplane models:
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737-100 737-200 737-200C 737-300 737-400 737-500
IDENTIFICATION BY CUSTOMER, CUSTOMER CODE, GROUP AND VARIABLE NUMBER
A.P.S. TRADING SERV S.R.L (PSV) 1 PL019
AAR A/C ENG. SALES & LEASING (AFD) 7PQ116
ADC AIRLINES (ADN) 1 PJ118–PJ119 10 PK462 3 PN034
AEGEAN AIRLINES S.A. (CRM) 13 PW261 2 PS608 PW002 PW046 PW053 PW157 PW276 PW289 PW564
AERCAP B.V. (DEA) 2PT009
AERGO CAPITAL LIMITED (CLJ) 1PK802 10 PK528 30 PK901 PK903 PK909 PK912
PK915–PK916 PK922
AERO CONTRACTORS OF NIGERIA (NCC) 2 PQ194 PQ196 PT396 PT401 PT420–PT421 PT430–PT431 PT433 9PV031 PV041
AERO CONTROLS (AEO) 1PG629 11 PG312
AERO NORTH INTERNATIONAL (NIN) 2PT125
AEROFLOT - CARGO (CGB) 5 PP825–PP826
AEROFLOT-DON (DAU) 2 PT701–PT703 PW249 35 PT507–PT508 PT513–PT514
AEROFLOT-NORD (CJS) 2 PR044 PT021–PT022 PT027–PT028 PT050–PT051 PT054 PT056–PT057 PT147–PT148 PT182–PT184 PT295
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AEROGAL/GALAPAGOS AIRLINES (ERG) 1 PK715 PK827 PL171 10 PL624–PL625 19 PL102 PL110 2PQ226 23 PP946 3PN030 PN405 7PQ243
AEROLINEA PRINCIPAL (APW) 1 PK775
AEROLINEAS ARGENTINAS (ARG) 1 PG584–PG585 PH705–PH708 PH742 PK735–PK737 PK740 PK747 10 PK102–PK103 2 PT023 PT042 PT044–PT045 PT047 PT101–PT102 PT212 PT214 PT220 PT303–PT306 PT309 3 PN104 PN110–PN115 PN117 30 PK750–PK751 PK755 PK757 PK761 PK765 35 PT509–PT510
AEROLINEAS AUSTRAL CHILE S.A. (LUT) 1 PK745 PL405 PM141–PM142 3PN103
AEROSERVICE (SRI) 3 PL742–PL743
AEROSUCRE (SUS) 17 PY341 26 PY451 3 PY201
AEROSUR (REO) 1 PK594 PK713–PK714 PK716
AEROSVIT (UKA) 1 PK564 13 PQ284 PQ286 PW265 2 PP924 PT138 PW039 PW268 PW591–PW592 PW595–PW596 6 PT614–PT615
AEROTECNIC, LLC (TCQ) 1 PM054
AEROVISTA GULF EXPRESS (GXP) 3 PK861–PK863 PY621
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AIR ALGERIE (ALG) 1 PL722 PL724 PY051 PY053 10 PK633–PK634
AIR AUSTRAL (AUX) 2 PS621 PT215
AIR CANADA (ACN) 1 PK679–PK680
AIR CARRIER ACCESSORY SERVICE (RCY) 3 PN085
AIR CHINA (BEJ) 13 PS957 2 PQ345–PQ346 PQ361–PQ364 PQ373 PQ447 PQ971 PQ975 6PQ438
AIR CHINA INNER MONGOLIAN (IML) 13 PQ365–PQ366 2 PQ370 PQ372 PQ988 PQ990 PS614–PS617
AIR CHINA SOUTHWEST BRANCH (XIN) 2 PQ401–PQ406 PQ408–PQ410 PS811 5 PP632–PP633
AIR CHINA TIANJIN BRANCH (TJA) 13 PQ367 2 PQ368–PQ369 PQ371
AIR CORRIDOR (KRD) 1PK749 10 PK468
AIR DO (HIA) 2 PT871 PT874 PT877 PT879
AIR DOMINICANA (DMA) 6PP894
AIR GUINEE (GNE) 3 PN456 42 PY651
AIR HORIZONS (AHZ) 1PY004
AIR INDIA (IND) 3 PK237–PK240 PM001–PM006 PY631
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AIR INUIT (AIU) 28 PY243
AIR ITALY (RIT) 6 PP903 8 PP393
AIR MADAGASCAR (MAD) 2PQ297 PQ299 7 PP852
AIR MALAWI (AML) 2 PS602 PT397
AIR MEDITERRANEE (AMV) 16 PY301 4 PG028–PG029
AIR NAMIBIA (NAM) 35 PT503–PT504
AIR NEW ZEALAND (ANZ) 13 PS866–PS868 2 PQ997 PR041 PR062–PR066 PR077–PR080 PS873–PS874
AIR NIPPON (ANK) 2 PJ817 PT053 PT060 PT063–PT064
PT126 PT128–PT131 PT872–PT873 PT875–PT876 PT878 PT880–PT886
AIR NORTH YUKON'S AIRLINE (AND) 1 PK596 PK599 41 PY592
AIR ONE (ADH) 1 PK432 12 PV232–PV234 PV236–PV237 2 PQ228–PQ229 PR021–PR022 PV228 PV301 PW041 PW043 PW052 PW054 PW287 PW290 30 PK933 PK938
AIR PHILIPPINES (PHP) 1 PK099 PK541–PK542 3 PN021–PN022 PN025 PN029 PN031 PN038 PN417–PN418 4 PG001 PG039 PG052 PG054 PG061–PG062 PG066–PG067 PG070
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AIR SLOVAKIA (SLO) 29 PP866 PP868–PP869 30 PK936 7PP851
AIR TANZANIA (TNZ) 3 PN413
AIR ZIMBABWE (ZMB) 3 PN431–PN433
AIRASIA BERHAD (ASW) 13 PP516–PP517 2 PM385 PM388 PM390 PM397 PQ184 PQ332 PQ448 5 PP002 PP021 PP406–PP409 PP471
AIRBALTIC CORPORATION (BCB) 2 PR015–PR017 PR162 PR164 PS624 PT005 PT161–PT163 PT424–PT425 PT428–PT429 PU311 PU313
AIRCRAFT MAINTENANCE CORP. (AMF) 10 PK254
AIRFAST INDONESIA (PTF) 3 PN481
AIRLINE CAPITAL LEASING, INC. (VTI) 10 PJ009
AIRTRAN AIRWAYS (CQT) 10 PK697
AIRWORK NZ (ANX) 10 PY741 5 PP028 PP039–PP040 7PQ242
ALASKA AIRLINES (ASA) 13 PW231–PW238 2 PJ301–PJ302 PJ601–PJ615 PW116 PW239–PW247 PW250–PW252
ALOHA AIR CARGO (HLH) 18 PY721 26 PY131 34 PY463 41 PY593–PY594
ALTER BAIL AVIATION (ABH) 1PK215 10 PK359
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AMERICAN FALCON AIR (FAK) 1 PL026
AMERISTAR AIR CARGO (CGG) 1 PK560 PM051 11 PK221 17 PY345–PY346
APOLLO AVIATION GROUP LLC (APV) 5 PP419 PP421 6 PP905 7 PP981–PP982 9 PP234
ARIK AIR (AKD) 2PQ154 PQ161
ASIA AIRLINES (YDO) 1 PL020 PY005 26 PY135
ASIANA AIRLINES (AAR) 2 PT851–PT853 PV204–PV206 PV208 PV227 PW283 PW286
ASTRAEUS, LTD. (AUA) 2 PP929 PS605
ATA ATLANTICO TRANSPORTE AEREO (AUI) 1 PY361 10 PY322
ATLANT-SOYUZ (AYZ) 2 PP967 7 PP962 9 PP233 PP239
ATLANTIC AIRLINES (LNL) 1 PK673 PL008 10 PL622–PL623
ATLANTIC AIRLINES LTD (YDG) 7PQ119
ATLAS BLUE (ABT) 2PT581 7 PW631–PW636
AURELA (URE) 13 PQ307 7PQ233
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AURORA AVIATION (AGX) 13 PQ287 5PP420 6 PQ141–PQ142 8 PP199 PS666–PS667
AUTOMATIC LLC (AUM) 30 PK759–PK760 PK764
AVE.COM (PHX) 1 PG579 PK213 PK823 PK826 41 PM252 6PP892
AVIA ASSET MANAGEMENT (VMA) 2 PQ192 PQ237 PT434 PT438
AVIACSA AEROEXO (AEJ) 1 PK211 PK598 PK609 PK625–PK626 PM101–PM102 PM104–PM107 PM114–PM119 10 PK216–PK219 PM181 3 PN154–PN155 PN401–PN404 5 PP422–PP423 PP425
AVIATION CONSULTANTS (ACT) 37 PY001 4PG037
AVIOGENEX (AVG) 3 PN501
AVIOR (AWD) 1 PK549 PK591 PM052 PM058 3 PN133–PN134 PN137 PN139 PN144 PN147–PN148 PN153 PN159
AVOLAR (AOL) 9 PP231–PP232 PP679 PP682
AVSTAR (VSV) 10 PK355 19 PL111
AWAS (AWW) 2PT213 PT216 6 PP911–PP912
BABCOCK & BROWN A/C MANAGEMENT (BBB) 7PP848
BAHAMASAIR (BAH) 1PK672 10 PL501 PL506
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BASIC CAPITAL MANAGEMENT (BCM) 3PN455
BATAVIA AIR (BTV) 1 PJ107 PJ112 PK305 PK563 PK617 PK711–PK712 PK825 PL413 10 PK252 PK360 PK514–PK515 PK622 2 PJ554 PJ558 PP917 PP921 PS631 PW005 PW015 PW020 PW032 PW156 PW575 3 PK283–PK284 41 PK635 5 PP003–PP004 PP006 PP008 PP017–PP020
BAVARIA (BAV) 2 PP984
BAYU INDONESIA AIR (BAY) 1 PK561
BCI AIRCRAFT LEASING (BLI) 26 PY134 27 PY112 3 PN131 PN136 PN138 PN142–PN143 34 PY462 9 PP237–PP238
BELAVIA (ITU)
2PQ472 PT722 6 PT971–PT973
BELLVIEW AIRLINES (BEB) 1 PK203 PK612 PL028 3 PK872
BLUE AIR (BTR) 2 PQ160 PS618 PW831 6PW741 7PQ026
BLUE DART AVIATION (BDA) 1 PL451 PM281 3 PK231–PK232 PN521
BLUE PANORAMA AIRLINES (BPA) 2 PR025–PR026 PW284 PW518–PW519
BLUEBIRD CARGO (BLS) 2 PM383 PQ342–PQ344 PW001
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BMI BRITISH MIDLAND (BMA) 13 PP520 PQ291–PQ292 PS861 PS956 2 PQ431 PQ974 PQ992 PQ996 PR012 PR043 PS625 PS971 PT186–PT188 6 PQ433–PQ435 PQ454
BOA (BOV) 13 PQ304 2PS604
BOEING (TBC) 1PG215 4PG051
BOEING CAPITAL CORPORATION (ZMF) 2PQ792 5PP162
BOURAQ AIRLINES (PTB) 10 PK501 30 PK913 PK918–PK920 PK931
BRANSON AIR (PTY) LTD (BSL) 1 PL025 3PK874
BRIAN M. FREEMAN ENTERPRISES (BMF)
11 PG304
BRITISH AIRWAYS (BAB) 12 PW314–PW315 PW317–PW327 13 PQ283 PQ305 2 PM399 PT185 PT307–PT308 29 PW301–PW302 PW305–PW308 PW312 35 PT515–PT516 7 PP841–PP842
BRUSSELS AIRLINES (EBA) 2 PQ984 PQ989 PQ993 PS656 PS972 PW013 PW264 PW271 PW275 PW571–PW572
BULGARIA AIR (BLD) 12 PQ086–PQ087 2 PQ190 PQ262 PQ331 PT170 PT211 PT427 PT437 8PP503
BURAQ AIR (BQA) 1 PL723 11 PL725
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C.I.T. LEASING CORPORATION (TCI) 2PW502 PW562 7 PP836
CANADIAN NORTH (ANP) 11 PL415 PY152–PY154 PY422 27 PY441 3 PK681 PN132 PN492
CANJET (CNJ) 7PQ231
CAPITAL AIRCRAFT (CPT) 10 PK464
CAPITAL AIRWAYS LLC (CPY) 5 PP404
CARDIG AIR (CGD) 17 PY343 9 PP241–PP242
CARGO AIR (CGE) 5 PP410
CASBAH AG AVIATION DIVISION (BHV) 10 PL581
CAYMAN AIRWAYS (CAY) 13 PQ293 2 PQ347–PQ348 PQ481 28 PY244 30 PK753
CELTIC CAPITAL (IAQ) 3PN411
CENTRALWINGS (CLW) 2PW106 PW267
CHANCHANGI AIRLINES (CGI) 1 PL412 PL416–PL417 3 PN083–PN084 PN086
CHARTER AIR (FIH) 2 PS630 PS871
CHILEAN AIR FORCE (CHF) 12 PQ053 2PT996
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CHINA EASTERN AIRLINES (CEA) 2 PQ263 PQ411–PQ412 PQ414–PQ418 PQ977 PQ979 PQ981 PR141–PR143 PS622–PS623 PS628
CHINA EASTERN AIRLINES WUHAN (WUH) 2 PQ491–PQ492 PR081–PR082 PR131
CHINA POSTAL AIRLINES (YIH) 2 PM407–PM409 PQ295–PQ296 PQ471 PQ493 PW524
CHINA SOUTHERN AIRLINES (GUN) 2 PM412 PM541–PM544 PM547 PM549 PQ252–PQ255 PQ407 PQ479–PQ480 PR121–PR122 PS836–PS837 PS841–PS846 PT061–PT062
CHINA UNITED AIRLINES (CUL) 2 PS609–PS610 PS896–PS897 9 PP728–PP729
CHINA XINHUA AIRLINES (XIH) 2 PM546 PQ264 PR001 PS856 PW852–PW854 45 PQ804–PQ805
CHINA XINJIANG AIRLINES (XIJ) 2 PM545 PM548
CIRRUS ME S.A.L (CMU) 1 PM103
CIS AIR HOLDINGS (CIS) 1PG217
CITYLINE HUNGARY LTD. (CTZ) 1PY101
COMAIR LIMITED (CML) 1 PK734 PK738 PK744 PK748 2 PP915 PP923 PW111–PW112 PW115 PW118 PW215–PW216 22 PW556 29 PW303 PW310–PW311 30 PK754 PK758 7 PQ001 PQ003–PQ006 PQ008 PQ010
CONOCOPHILLIPS ALASKA, INC. (ATR) 3 PN452–PN453
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CONTINENTAL AIRLINES (CAL) 6 PT801–PT824 PT826–PT834 PT901–PT905 PT907–PT918 PT921 PT924 PT926 9 PP671–PP675 PP678 PP680–PP681 PP683 PP688–PP699 PP701 PP703–PP710 PP712–PP726 PP730 PP732–PP733
CONVIASA S.A. (VSS) 1 PL005 PL010 7PQ117
CORENDON AIRLINES (HVA) 2 PQ451 PW282 PW285
CP AIR (CPA) 2PW530
CSA (CSA) 2 PJ816 PT981–PT985 PV302 PW431–PW435 PW517 29 PW304 PW309 6 PT617–PT621
CSC TRANSPORT (CTC) 2PW007
DAIMLERCHRYSLER AVIATION (DCY) 5 PP119–PP120
DBA (DBA) 13 PP511 PP515 2 PS655
DELMUN AVIATION SERVICES (DLM) 26 PK318
DELTA AIR LINES (DAL) 3 PN149 PN161 PN415 9 PP240 PP243
DELTA CONNECTION (DTC) 1 PY272
DNIPROAVIA (DNE) 13 PP510 2 PR003 PT041 PT133–PT134 PW031
DODSON AVIATION (DOO) 1PJ032
DOLPHIN AIR (FDN) 28 PY241 42 PL151
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DONGHAI AIRLINES (JWC) 2 PM396 PM405 5 PP651–PP652
EARTH AIRLINES (ETL) 24 PG352
EASTOK AVIA (ETK) 2PW011 3 PN407–PN408 PN410 PN416 PN493 39 PK632 5PP034 PP440 9PV023
EDREES AVIATION (SME) 10 PL505
EG&G TECHNICAL SERVICES (EGN) 1 PJ205 PJ208–PJ210 PL763 3PJ207
EGYPTAIR (EGP) 2 PT561 PT563–PT565 4PG026
ESEN AIR LTD. (ESN) 26 PK317 PL729
ESTAFETA (EST) 1PY275 2 PQ224–PQ225 7PP833 PP846
ESTELAR (ESQ) 10 PL626
ESTONIAN AIR (ENA) 2 PQ994 PR045 PT136 PT716–PT717 PU312
EUROPE AIRPOST (EUE) 2 PP925 PQ421 PQ771–PQ772 PR096 PR163 PR166 PS607 PS641–PS644 23 PP947 7 PP832 PP951–PP952 8PP392
EUROPEAN AVIATION AIR CHARTER (EUL) 1 PK041 PK044 PK046 PK048–PK049 PY273 10 PN001 7PP965
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EUROPEAN CAPITAL HOLDINGS (ECC) 1 PK525 10 PK524 PY321 3 PJ006 PK641–PK642 37 PY003
EXECUTIVE JET AIRCRAFT COMPANY (EXF) 10 PL441
EXPORT RESTRICTED AIRPLANES (YWV) 1 PG219 PG224 PJ102 PK214 10 PG574 PJ002 11 PG218 PG305 PG308 PG310–PG311 PL758 13 PQ288–PQ289 14 PA002 27 PK391 3 PH731 PJ003 PY021–PY022 PY141–PY142 4 PG021 PG041 PG074
EXPRESSAIR (PTX) 3 PK304 PM022
FAA (FAA) 1 PL768
FACTS AIR (FAD) 1 PX701
FASCO AIRWAYS (EAO) 1PG228
FEDERATIVE REPUBLIC OF BRAZIL (BRZ) 49 PK068–PK069
FIRST AIR (BRS) 1 PK358 PL407 11 PY421 26 PY133 3 PY281 42 PY410
FLAIR AIRLINES (FLR) 2PW503 7PW662
FLANA (FLQ) 20 PY270
FLYGLOBESPAN.COM (FGS) 2 PS962–PS963
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FLYING CARPET (FYC) 10 PM064 3 PN140
FLYLAL CHARTERS (LCT) 2PQ189
FRESH AIR LTD. (FRR) 3 PN024 PN035
FUTURA (FUA) 2 PW047–PW048 PW101 PW266 PW561 5PP430 PP432 6PP899 9PV032
GA TELESIS, LLC (GTG) 1PK739
GARUDA INDONESIA (GIA) 13 PP508 PP514 PQ285 2 PM404 PQ487 PQ986–PQ987 PR061 PR068–PR072 PR091–PR092 PS653 PT681–PT685 PV271 PW067 PW119 PW443–PW450 PW461–PW467 PW525 PW712 PW851
GARY AIRCRAFT (GRH) 3 PL745
GE AVIATION MATERIALS (GML) 5PP001
GECAS (GEF) 1 PG651–PG652 PK026–PK027 10 PK256 PK466–PK467 11 PG220–PG221 2 PM398 PM410–PM411 PW009 PW012 PW018–PW019 PW021 7PP840 9 PP235–PP236
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GENERIC CUSTOMER/SUPPLIER (XXX) 1 PG375 PH743 PJ110–PJ111 PK029 PK274 PK286 PK801 PK803–PK804 PK821 PL004 PL009 PL012 PL014–PL016 PL023 PL793 10 PK253 PK495 PK503 PK519 PY611 11 PG307 PK112 PK144 PY411 19 PL107 PL112 2 PQ199 PT382–PT383 PT385 3 PJ005 PL740–PL741 30 PK934 4 PG024 PG055 PG057 PG069 PG071 41 PM253 5 PP031 PP046 PP431 PP436–PP438 6 PP936
GEORGIAN AIRWAYS (GEI) 2PT181 PW262 5 PP044 6PT611
GERMANIA (GER) 2 PQ152 PQ230 PQ234–PQ235 7 PP838 PP961 8 PP507
GLOBAL AIR (YCH) 1 PK548 PK595 PL013 11 PK145 3PJ004
GOL AIRLINES (GOT) 13 PQ303 2 PP922 PP988–PP990 PQ158 PQ162–PQ163 PQ191 PQ193 PQ195 PQ227 6 PQ143–PQ145 7PQ120
HAINAN AIRLINES (HNA) 12 PQ088–PQ091 2 PQ156–PQ157 PQ473–PQ475 PR005 PR010 PS611 PS613 PS976–PS978 PV203 PV356–PV357 PW086–PW088 PW093
HAMBURG INTERNATIONAL (HAU) 6 PP904
HOLA AIRLINES (HLB) 2PW006
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IAI (IAI) 1PG575 PK692
ICARO (IKA) 1PK742 PK771 34 PY461
IDM CAS (IDN) 1PK552
INDIAN AIR FORCE (IDF) 10 PH712–PH713 3 PM016–PM017
INTAL AIR (IRT) 1PY274 26 PK312 28 PY242
INTERAIR (ITI) 1PK546 PK610 11 PY046–PY047 19 PL108 PL113
INTERLINK AIRLINES (ILK) 1PK743 19 PL103 30 PK904 PK907
INTERNATIONAL AIR LEASES (IAL) 10 PL803
INTERNATIONAL AIR PARTS (IAO) 1PG580
ION TIRIAC AIR (ION) 13 PS862
IRAQI AIRWAYS (IRQ) 2PQ198
JAL INTERNATIONAL (JAL) 2 PW411–PW418
JANCO AIRCRAFT AND ENGINES (JNC) 1 PM282–PM283
JAPAN TRANSOCEAN AIR (SWL) 2 PW401–PW408 PW515–PW516 PW520–PW521 6 PW681–PW683
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JAT YUGOSLAV AIRLINES (JAT) 5 PP771–PP779 7PQ241 9 PV024
JATAYU AIR (JAJ) 1PJ117 10 PK257 PK511 30 PK937 4PG068
JET AIRWAYS (JPL) 2 PW421–PW424
JET LITE (JPQ) 13 PQ306 2 PW064 PW066 PW273
JET MIDWEST (JMI) 1 PK558 PM057 PM060 10 PM066
JET TIME (JME) 2 PM384 PM391 6 PP897 8 PP504
JET2.COM LTD (CEX)
12 PQ051–PQ052 PQ054–PQ055 PQ058–PQ059 6 PP908–PP909 PP913–PP914 7 PQ027 PQ030–PQ039
JET4YOU.COM (JFU) 2PW511 7PW661
JETAIRFLY (TLB) 2 PJ811 PT103 PW522
JETCONNECT LIMITED (JCL) 22 PW540 PW542–PW543 6 PQ013–PQ016 7PQ012
JETLEASE (JLI) 41 PY595
JETRAN INTERNATIONAL, LTD. (JTI) 1 PK593
JETSCAPE LEASING (IAN) 2PW008
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JETSTAR AIRCRAFT SALES (JTS) 11 PG306
JETSTAR PACIFIC AIRLINES (PAH) 12 PW316 2 PJ556 PJ559 PW102 PW272
JORDAN AVIATION (JOR) 2PQ187 PW528 6 PP896 PT671 7 PQ123–PQ124
JSC "AIRCOMPANY SCAT" (DVW) 2PT426 PT435
JSC STARLINE.KZ (MZK) 1 PL556 30 PK911
KARTHAGO AIRLINES (KAG) 2 PP926 PP928 PP930 PQ180 PR029 6PQ432
KARTIKA AIRLINES (KRK) 3 PK309–PK310
KD AVIA (JSK)
13 PQ302 2PP916 PS652 25 PP801 29 PP867 PP870 5 PP016 PP305 PP383 PP418 PP424 PP426 PP429 PP475 7 PP837 PP843–PP844 PQ232 8PP196
KENYA AIRWAYS (KEN) 2 PR031–PR034
KLM - ROYAL DUTCH AIRLINES (KLM) 2PW014 PW017 29 PP861 PP863–PP864 31 PP871–PP873 32 PP874–PP877 PW611–PW619 PW621–PW622
LAC (CQC) 27 PY113
LAM (LAM) 10 PL455–PL456 3 PN451 PN454
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LAN AIRLINES (LAN) 1 PJ104 PK431 30 PK914
LAPA ARGENTINA (LAZ) 1 PK051
LAS VEGAS SANDS, CORP. (LVS) 2PQ236 8 PP506
LIBYAN AIRLINES (LAA) 1 PK361
LINEAS AEREAS AZTECA (AZX) 2 PP983 PP986
LION AIR (MLI) 2 PW016 PW022–PW023 PW025 PW029 PW037–PW038 PW042 PW501 5 PP181–PP182
LITHUANIAN AIRLINES (LIJ) 2PT169 PT721
LJH AVIATION MANAGEMENT (WAT) 1 PL006
LLC GLOBUS (LLG) 2PW526
LOBAYE AIRWAYS (LBY) 3PN409
LOCALEASE (LLA) 3 PK282
LOCKHEED MARTIN (LMA) 12 PQ057
LOGISTIC AIR, INC. (LGA) 16 PY303–PY304
LORENA AIR (LRN) 2PQ951
LOT POLISH AIRLINES (LOT) 2 PQ978 PQ980 PS973 PT651–PT656 PV281–PV287 PW065
LUFTHANSA GERMAN AIRLINES (DLH) 12 PQ060–PQ085 PQ092 PS701–PS706 PT331–PT360
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LUXAIR (LUX) 6PT672
MACEDONIAN AIRLINES, MACEDONIA (MCC) 6 PT612–PT613
MACQUARIE AIR FINANCE (ZGT) 2PW504 5PP022
MAGNICHARTERS (MAM) 1 PL454 PL554 PL558 11 PK143 2PQ168 5PP405 7PQ028
MALAYSIA AIRLINES (MAS) 2 PJ551–PJ553 PJ555 PJ557 PJ560–PJ561 PW044 PW201–PW214 PW217–PW230 PW529
MANDALA AIRLINES (MND) 1 PL027 10 PK255 PN002 11 PL421 2PW004 PW010 3 PL744 41 PK636
MANGAL AIRLINES (MGG) 18 PL785
MARANATHA LEASING CORPORATION (MNT) 1 PK201–PK202 PL011 33 PG436
MAX AVIA (MXY) 1PK671 PK830 11 PK222 26 PK315 PL732
MERPATI NUSANTARA AIRLINES (PNM) 1 PK354 PK614–PK615 PK623 PK819 PL409 10 PK624 13 PQ281 2PW091 30 PK917 PK929–PK930 5 PP043 PP434–PP435 6PP898
MEXICO'S PRESIDENTIAL AIRCRAFT (MXG) 2 PP919 PQ155
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MIAMI AIR (MIB) 2 PV226 PV229
MIDAMERICAN AEROSPACE, LTD (MML) 1 PL557 10 PY231
MIRAGE AVIATION LTD (MLE) 7 PP991
MISTRAL AIR (MSX) 2 PQ222 PQ341 PS638
MNG AIRLINES (MHK) 2 PW512 PW514 PW593
NAT AVIATION U.S.A. (NTV) 1 PK551 PK557 PK732 10 PK258
NATIONAL CITY (NTJ) 10 PL471
NATIONWIDE AIRLINES (NWR) 1 PK357 PK741 10 PJ007–PJ008 PK871 3 PL631–PL632 PN107 PN109 30 PK906 PK928 PK932
NEW AXIS AIRWAYS (NXA) 13 PQ301 2PW033
NEWJET (NES) 1 PL172 PL562
NICON AIRWAYS LTD. (EAV) 1 PL453 3PN032
NIGERIA AIRWAYS (NIA) 18 PL788
NOK AIR (OWL) 2 PM553 PW045
NOLINOR AVIATION (NLO) 10 PY671–PY672
NORDESTE (NDT) 2 PP987
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NORTHERN AIR CARGO (NAC) 3 PN150–PN152
NORTHROP GRUMMAN CORPORATION (GRU) 1PG208
NORTHSTAR PRESIDIO MANAGEMENT (INH) 1 PK094–PK095
NORWEGIAN AIR SHUTTLE AS (NSB) 13 PP518–PP519 2 PM381 PM389 PM401–PM402 PP805–PP808 PP918 PP985 PQ791 PQ793 PQ983 PQ985 PR002 PR028 PR030 PR101 PR132 PR169 PS601 PS620 PS627 PS654 PS872 PS961
NOVA AIR (PDM) 1 PL007 PL406 3 PN412 PN414
OKAY AIRWAYS COMPANY LIMITED (OKY) 13 PQ290 2PT725 5PP631 PP634
OLYMPIC AIRLINES (OLY)
12 PV231 2 PQ298 PS657 PV201–PV202 PW063 PW068 PW072 PW291 PW711 PW713–PW717 PW771
OLYMPIC AIRWAY SERVICES (OLS) 2PW062
ORENBURG AIRLINES (ORG) 2 PT010 PT029 PT301–PT302 PW028 PW036
ORIX AVIATION SYSTEMS (OXA) 2PT127
OUR AIRLINE (NAU) 6PP902 7PP831
OZJET AIRLINES (OZJ) 1 PK045 PK050 PK052–PK053
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PACE AIRLINES (PIE) 1 PG203 PL001 10 PL502–PL503 3PN102 PN116 4PG075 7 PP835
PACIFIC PEARL AIRWAYS (PPA) 3PN146
PACIFIC SKY AVIATION INC. (SEF) 2PT219
PAI AVIATION, INC. (PSS) 1 PK043 25 PP802 3 PK233 PK235 30 PK752 PK756 5 PP161
PAKISTAN INT'L AIRLINES (PIA) 2 PS612 9 PP281–PP286
PAMIR AIRWAYS (PMY) 3PN135
PEGASUS AIRLINES (PGS)
2 PT137 PT724 PT854 PW030 PW263
PERUVIAN AIR FORCE (PRF) 10 PG251 PG253 12 PT517 24 PG351 3PN082
PHILIPPINE AIRLINES (PAL) 45 PQ803
PHUKET AIRLINES (PHK) 1 PG581–PG582 3PN037 PN039
PLATINUM AIRWAYS (PLW) 5 PP189
PLUNA (PLU) 10 PL201–PL203
PRECISIONAIR (PCR) 2 PM395
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Q AVIATION (QAV) 1 PK288 PK603–PK604 7PQ132
QANTAS (QAN) 22 PW531–PW539 PW541 PW544–PW550 PW557 7 PQ002 PQ007 PQ009 PQ011
QUIKJET (QKJ) 2 PQ221 PQ223
QWEST AIR PARTS (QWE) 33 PG438
REGIONALCARGO (RGC) 41 PY057
REPEX AIRLINES (REX) 3 PY102–PY103
REPUBLIC FINANCIAL CORPORATION (RFC) 1 PG225 PG502–PG503 PG622 PG704 14 PA011 33 PG433 47 PG199
REPUBLIC OF INDONESIA (IDO) 41 PL601–PL603
REPUBLIC OF KOREA AIR FORCE (KAF) 5PP221
REPUBLIC OF NIGER (NIR) 26 PY166
REPUBLIC OF VENEZUELA (VNZ) 11 PK070
REPUBLICAIR (RPB) 1 PL553 PL555
RICO (RLA) 11 PK120
ROSSIYA RUSSIAN AIRLINES (STG) 2 PT164–PT168
ROYAL AIR MAROC (RAM) 1 PK271–PK272 2 PT582–PT586
ROYAL KHMER AIRLINES (KHM) 3 PN163
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RUTACA AIRLINES (ZRU) 1 PK611 PK613 PM062 3 PK281
RUTAS AEREAS VENEZOLANAS S.A. (RTV) 1 PK822 PL402 PL414 3PN145 PN157
RYAN INTERNATIONAL AIRLINES (RYN) 1 PK543 PK606 2PQ197
RYM AIRLINES (RYM) 1 PL017–PL018
S7 AIRLINES (SBR) 2 PM556 PT381 PT388–PT389 PW051 PW094 35 PT501–PT502 PT505–PT506
SAFAIR (SFA) 1 PK731 PK746 PK824 PL061 30 PK974 37 PY002
SAFAIR OPERATIONS (SFZ) 1 PK820
SAFI AIRWAYS (FFI) 5 PP521–PP522
SAGA AIRLINES (SGV) 2 PV207 PV209
SAMA AIRLINES (AWM) 13 PP509 2 PM393–PM394 PQ982 PS606 PS651
SAS NORWAY (BRT) 2 PT002–PT004 PT006–PT008 PT011–PT015 PT024–PT025 PV351 PW573–PW574 PW576
SAT AIRLINES (SKH) 1 PL221 3PN158
SAUDI ARABIAN AIRLINES (SVA) 26 PK316 PL727–PL728 PL730–PL731 PL733 PY036
SEAGLE AIR (SGQ) 7 PP964
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SHAHEEN INTERNATIONAL (SHK) 1 PK602 PK608 PL003 PL551 PL561 3 PN036
SHANDONG AIRLINES (SHG) 2 PQ391–PQ395 PR006–PR009 PR013–PR014 PR161
SHANTOU AIRLINES (SHT) 2 PM415–PM417
SHENZHEN AIRLINES (SHZ) 2 PQ486 PQ972 PQ976 PQ995 PS629 PS691–PS692 PS851–PS852
SIERRA PACIFIC AIRLINES (SRP) 1PK627 10 PL621
SILVER AIR (SARL) (SVT) 26 PK313–PK314 PL726 PL734 29 PP865 6PP935
SILVER SKY (SLZ) 3 PN419
SKY AIRLINES (SYC)
12 PV235 13 PW281 PW293 PW296 2PW278
SKY EXPRESS (SXR) 12 PQ056 2 PQ258–PQ259 PT058 PT123–PT124 PT146 PT217–PT218 6PT616
SKY HOLDING COMPANY (PSH) 1 PL401 PL403 3 PN491
SKY KING (SKN) 1 PK352–PK353 PL002 10 PK351 PK696 3 PN156 PN162
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SKY SERVICE (SSV) 1 PK772 10 PK526–PK527 11 PK881 3 PL736 30 PK902 PK908 PK910 PK923 PK927 PK971 PK973 39 PK628–PK629 44 PK884
SKYNET ASIA AIRWAYS (SNU) 2 PM555 PW026 PW274 PW441–PW442 PW855–PW856
SLOK AIR (SRO) 1 PM108–PM113
SOUTH AFRICAN AIRWAYS (SAA) 19 PL104–PL106 2 PM413–PM414
SOUTHERN WINDS (SOW) 1 PK047 PK616
SOUTHWEST AIRLINES (SWA) 10 PM065 25 PP803–PP804 5 PP101–PP118 PP121–PP160 PP163–PP169 PP188
PP190–PP193 PP202–PP205 PP301–PP304 PP351 PP353 PP376–PP380 PP382 PP402–PP403 PP501–PP502 PP821–PP824 PP827 PS751–PS799 PS901–PS941 9 PP727 PP731 PU001–PU025
SPACE WORLD AIRLINE/SWA (WIN) 1 PL021–PL022
SRIWIJAYA AIR (SJA) 1 PJ114 PK777 13 PS863 2 PP927 PW034–PW035 PW061 3 PK302–PK303 PK307–PK308 PM021 PN023 PN026–PN027 PN040 PN042–PN043 41 PM254 6 PP910
STA SUPPLIES PTE. LTD. (SSP) 7 PQ040–PQ041
STAR (EQA) 41 PN512
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STAR AIR (SGY) 3 PN033
STAR UP S.A. (SRU) 1PJ115 30 PK921 46 PL611
STERLING AIR (STR) 2PT121 PT132
STEWART INDUSTRIES INT'L (SDT) 3 PN473 30 PK905 PK926 PK935 41 PM251
SUNDOWNER OKLAHOMA CITY LLC (SDO) 29 PW313
SWIFT AIR (SWF) 2 PM392 23 PP948 29 PP862 5PP352 7PP847
SWIFT AIR LLC (SFW) 2PW563
9 PV042–PV043
TAAG (ANGOLA AIRLINES) (ANG) 26 PK661 PY162 39 PK664 42 PK665–PK666
TAC (TGB) 1PY031
TACA INTERNATIONAL AIRLINES (TAC) 3 PL737 PN420
TAF LINHAS AEREAS (TFL) 1 PL404 10 PY323 17 PY342 3 PN160
TAILWIND AIRLINES (TWK) 2PW248
TAROM - ROMANIAN AIR TRANSPORT (TRM) 2 PQ931–PQ935
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TEEBAH AIRLINES (EBH) 1 PK601 PK605 3PN028
THAI AIRASIA (THA) 5 PP411–PP412 9 PP676–PP677 PP684 PP686–PP687
THAI AIRWAYS INTERNATIONAL (TII) 2PW594 40 PV296 PW161–PW162 PW164–PW171
THE MOURITZEN FAMILY TRUST (MRZ) 11 PY191
THE PEGASUS AVIATION COMPANY (PEG) 1 PK285
THOMSON AIRWAYS (BRI) 2 PR004 PR011 PR023–PR024 PR067 PR165 PS974–PS975 6 PQ436–PQ437
TITAN AIRWAYS (TIU) 2 PM387 PS636–PS637 8 PP505
TNT AIRWAYS (TNB)
2 PP845 5 PP384 PP413–PP414 PP433 PP472 PP474 8 PP391 9 PP702 PP711
TOR AIR (TOB) 2PW288
TRAFIC (TFI) 41 PY056
TRANS AIR CONGO (TSC) 10 PK562 30 PK763
TRANSAERO AIRLINES (TRX) 1 PK451 PK773 PK779 2 PP966 PT046 PT049 PT052 PT104–PT105 PT723 PW024 PW040 PW113–PW114 PW120 6PT923 PT925 7 PP963
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TRANSMILE AIR SERVICES (TML) 10 PY381 11 PY151 3 PN472 PN474
TRAVEL SERVICE (TSF) 2PT432 PT436
TRAVIRA AIR (TVR) 2PT135
TRIGANA AIR (TGN) 10 PL504
TRITON AVIATION SERVICES (TIA) 1 PJ101 PJ103 PK677 PL408 PL410–PL411 PL770 3 PN101 PN105–PN106 PN108
TUIFLY (HAP) 2PW513
TUNISAIR (TUN) 2 PT641–PT644
TURKISH AIRLINES (THY) 2 PM552 PM557 PM559–PM560 PM562–PM564 PW049–PW050
TURKMENISTAN AIRLINES (TUE) 2PQ265 45 PQ801–PQ802
UETAAM (MXA) 3 PN041
UKRAINE INTERNATIONAL AIRLINES (UKR) 13 PT059 2 PM382 PM551 PM554 PM561 PQ251 PQ991 PR042 PR181 PT043 PT048 PT055 PW701–PW702 35 PT511–PT512 6PW742
UNITED AIR LINES (UAL) 2 PQ151 PQ164–PQ167 PQ169–PQ179 PQ181–PQ183 PQ185–PQ186 PQ201–PQ202 PT384 PT386–PT387 PT390–PT395 PT398–PT399 PT402–PT419 PT422–PT423 6 PQ139–PQ140 PQ146–PQ150 7 PQ101–PQ115 PQ118 PQ121–PQ122 PQ125–PQ131 PQ133–PQ138
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UNIVERSAL ASSET MANAGEMENT (UAM) 1 PM056 PM059 10 PM061
UNKNOWN CUSTOMER (UNZ) 1 PK675 11 PK111 PK114 PK118–PK119
US AIR FORCE (USF) 1 PJ202 PJ206 PJ211 PJ213–PJ219
US AIRWAYS (USA) 1 PL081 PL560 15 PV009–PV010 PV012–PV020 21 PS669 5 PP005 PP007 PP014–PP015 PP024–PP027 PP029–PP030 PP032 PP036–PP038 PP047–PP054 PP183–PP187 PP194 PP401 PP417 PP428 PP439 PV001–PV008 6 PP891 PP893 PP895 PP901 PP931–PP934 7 PP834 8 PP195 PP197–PP198 PS668 9 PV021–PV022 PV025–PV030 PV033–PV040 PV044–PV055
UT FINANCE CORPORATION (ZZJ) 2PQ153
UTAIR (UTR) 6 PT825 PT919–PT920 PT922 PT927–PT929
VASP AIRLINES (VSP) 11 PG472 PK581 13 PP512
VIRGIN NIGERIA (VNA) 2 PR167–PR168 PR170–PR172
VISION AIR (VEG) 2 PS626 9 PP685
VIVA AEROBUS (VIV) 5 PP009–PP010 PP013 PP023 PP041 PP427 PP473
VOLVO AERO SERVICES (AGD) 5 PP381
VTB LEASING (VTB) 6PT930
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WAHA LEASING (OSI) 2PW527
WEBJET LINHAS AEREAS LTDA. (WJL) 2 PQ159 PQ188 PQ256–PQ257 PQ260–PQ261 PQ266–PQ267 PS603 6 PP906–PP907 7PP839
WELLS FARGO (FSB) 13 PP513
WEST DOVER LLC (WDR) 5PP415
WESTAIR CARGO AIRLINES (WCO) 26 PY037
WESTSTAR AVIATION (WSE) 18 PK565
WILMINGTON TRUST COMPANY (WBT) 5 PP035 PP042 PP045
WINGS OF LEBANON S.A.L. (WGL) 3 PN141
XIAMEN AIRLINES (XIA)
2 PT030–PT031
XSTRATA CANADA CORPORATION (NAD) 26 PY612
XTRA AIRWAYS (CIN) 10 PG279 2PW117 6PW761
YAMAL AIRLINES (YMA) 2 PU301
ZAMBIAN AIRWAYS (MBA) 10 PK220 19 PL109
ZASA (CZA) 26 PL735
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IDENTIFICATION BY VARIABLE NUMBER
Variable Group PA001–PA022 14 PA099 43 PA231–PA232 1 PC001–PC002 10 PC003–PC005 1 PG001–PG075 4 PG199 47 PG201 1 PG202 11 PG203–PG204 1 PG205 11 PG206 1 PG207 11 PG208 1 PG209 11 PG210 1 PG211–PG214 11 PG215 1
PG216 11 PG217 1 PG218 11 PG219 1 PG220–PG221 11 PG222–PG230 1 PG251–PG255 10 PG271–PG278 1 PG279 10 PG301–PG314 11 PG331–PG332 1 PG351–PG353 24 PG354–PG356 1 PG375 1 PG401–PG403 1 PG431–PG434 33 PG435 1 PG436 33 PG437 1
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Variable Group PG438 33 PG439–PG440 1 PG441 33 PG442 1 PG471–PG475 11 PG501–PG505 1 PG571–PG572 10 PG573 1 PG574 10 PG575–PG586 1 PG621–PG630 1 PG651–PG652 1 PG701–PG703 26 PG704 1 PG705 10 PH001 1 PH011–PH013 11 PH021–PH022 3 PH023 1 PH024 3
PH701–PH708 1 PH709–PH713 10 PH714–PH715 1 PH731–PH732 3 PH741–PH743 1 PJ001–PJ002 10 PJ003–PJ006 3 PJ007–PJ009 10 PJ031–PJ032 1 PJ071–PJ072 1 PJ101–PJ119 1 PJ201–PJ206 1 PJ207 3 PJ208–PJ219 1 PJ301–PJ302 2 PJ551–PJ561 2 PJ601–PJ615 2 PJ811 2 PJ816–PJ817 2
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Variable Group PK026–PK029 1 PK041–PK053 1 PK061–PK067 11 PK068–PK069 49 PK070 11 PK081–PK082 1 PK091–PK099 1 PK101–PK103 10 PK111–PK120 11 PK141–PK146 11 PK201–PK203 1 PK204 11 PK211–PK215 1 PK216–PK220 10 PK221–PK223 11 PK231–PK240 3 PK241 1 PK251–PK258 10 PK271–PK274 1 PK281–PK284 3
PK285–PK289 1 PK291 27 PK301–PK304 3 PK305–PK306 1 PK307–PK310 3 PK311–PK318 26 PK341 26 PK351 10 PK352–PK354 1 PK355 10 PK356–PK358 1 PK359–PK360 10 PK361 1 PK391 27 PK431–PK433 1 PK451–PK452 1 PK461–PK468 10 PK469 1 PK495 10
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Variable Group PK501–PK504 10 PK511–PK515 10 PK519 10 PK521 10 PK522 1 PK523–PK524 10 PK525 1 PK526–PK528 10 PK541–PK561 1 PK562 10 PK563–PK564 1 PK565 18 PK581 11 PK591–PK599 1 PK601–PK617 1 PK621 1 PK622 10 PK623 1 PK624 10 PK625–PK627 1
PK628–PK630 39 PK631 10 PK632 39 PK633–PK634 10 PK635–PK637 41 PK641–PK642 3 PK661 26 PK662–PK663 42 PK664 39 PK665–PK666 42 PK671–PK680 1 PK681 3 PK691–PK694 1 PK695–PK697 10 PK711–PK716 1 PK731–PK749 1 PK750–PK765 30 PK771–PK779 1 PK801–PK804 1
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Variable Group PK819–PK827 1 PK830 1 PK861–PK863 3 PK871 10 PK872–PK874 3 PK881–PK883 11 PK884 44 PK901–PK938 30 PK971–PK974 30 PL001–PL028 1 PL061 1 PL081 1 PL101–PL113 19 PL151 42 PL171–PL172 1 PL201–PL203 10 PL221 1 PL401–PL414 1 PL415 11 PL416–PL417 1
PL421 11 PL441 10 PL451–PL454 1 PL455–PL456 10 PL471 10 PL491 39 PL501–PL506 10 PL551–PL562 1 PL581 10 PL601–PL603 41 PL611 46 PL621–PL626 10 PL631–PL632 3 PL711 1 PL712 16 PL716 1 PL717 11 PL718–PL724 1 PL725 11
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Variable Group PL726–PL735 26 PL736–PL738 3 PL739 1 PL740–PL745 3 PL746–PL747 10 PL756 11 PL758 11 PL761–PL770 1 PL781–PL782 3 PL783–PL788 18 PL793 1 PL801–PL802 1 PL803 10 PM001–PM006 3 PM016–PM017 3 PM021–PM023 3 PM051–PM060 1 PM061 10 PM062 1 PM063–PM066 10
PM101–PM119 1 PM141–PM142 1 PM171 48 PM181 10 PM251–PM255 41 PM281–PM283 1 PM381–PM399 2 PM401–PM417 2 PM541–PM564 2 PN001–PN002 10 PN021–PN043 3 PN081–PN086 3 PN101–PN117 3 PN131–PN163 3 PN401–PN420 3 PN431–PN433 3 PN451–PN456 3 PN471–PN474 3 PN481 3
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Variable Group PN491–PN493 3 PN501–PN502 3 PN511–PN512 41 PN521 3 PP001–PP054 5 PP101–PP169 5 PP181–PP194 5 PP195–PP199 8 PP201–PP205 5 PP221 5 PP231–PP243 9 PP281–PP286 9 PP301–PP305 5 PP351–PP353 5 PP376–PP384 5 PP391–PP393 8 PP401–PP440 5 PP471–PP475 5 PP501–PP502 5 PP503–PP507 8
PP508–PP520 13 PP521–PP522 5 PP631–PP634 5 PP651–PP652 5 PP671–PP699 9 PP701–PP733 9 PP771–PP779 5 PP801–PP804 25 PP805–PP808 2 PP821–PP827 5 PP831–PP844 7 PP845 2 PP846–PP848 7 PP851–PP852 7 PP861–PP870 29 PP871–PP873 31 PP874–PP877 32 PP891–PP899 6 PP901–PP914 6
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Variable Group PP915–PP930 2 PP931–PP936 6 PP946–PP948 23 PP951–PP952 7 PP961–PP965 7 PP966–PP967 2 PP981–PP982 7 PP983–PP990 2 PP991 7 PP993 2 PQ001–PQ012 7 PQ013–PQ016 6 PQ026–PQ041 7 PQ051–PQ092 12 PQ101–PQ138 7 PQ139–PQ150 6 PQ151–PQ199 2 PQ201–PQ202 2 PQ221–PQ230 2 PQ231–PQ233 7
PQ234–PQ237 2 PQ241–PQ243 7 PQ251–PQ267 2 PQ281–PQ293 13 PQ294–PQ299 2 PQ301–PQ307 13 PQ331–PQ332 2 PQ341–PQ348 2 PQ361–PQ364 2 PQ365–PQ367 13 PQ368–PQ373 2 PQ391–PQ395 2 PQ401–PQ418 2 PQ421 2 PQ431 2 PQ432–PQ438 6 PQ447–PQ448 2 PQ451 2 PQ454 6
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Variable Group PQ471–PQ475 2 PQ479–PQ481 2 PQ486–PQ487 2 PQ491–PQ493 2 PQ771–PQ772 2 PQ791–PQ793 2 PQ801–PQ805 45 PQ931–PQ935 2 PQ951 2 PQ971–PQ997 2 PR001–PR017 2 PR021–PR034 2 PR041–PR045 2 PR061–PR072 2 PR077–PR082 2 PR091–PR092 2 PR096 2 PR101 2 PR121–PR122 2 PR131–PR132 2
PR141–PR143 2 PR161–PR172 2 PR181 2 PS601–PS631 2 PS636–PS638 2 PS641–PS644 2 PS651–PS657 2 PS666–PS668 8 PS669 21 PS691–PS692 2 PS701–PS706 12 PS751–PS799 5 PS811 2 PS836–PS837 2 PS841–PS846 2 PS851–PS852 2 PS856 2 PS861–PS863 13 PS866–PS868 13
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Variable Group PS871–PS874 2 PS896–PS897 2 PS901–PS941 5 PS956–PS957 13 PS961–PS963 2 PS971–PS978 2 PT001–PT015 2 PT021–PT031 2 PT041–PT058 2 PT059 13 PT060–PT064 2 PT101–PT105 2 PT121–PT138 2 PT146–PT148 2 PT161–PT170 2 PT181–PT188 2 PT211–PT220 2 PT295 2 PT301–PT309 2 PT331–PT360 12
PT381–PT399 2 PT401–PT438 2 PT501–PT516 35 PT517 12 PT561–PT565 2 PT581–PT586 2 PT611–PT621 6 PT641–PT644 2 PT651–PT656 2 PT671–PT672 6 PT681–PT685 2 PT701–PT703 2 PT716–PT717 2 PT721–PT725 2 PT801–PT834 6 PT851–PT854 2 PT871–PT886 2 PT901–PT930 6 PT971–PT973 6
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Variable Group PT981–PT985 2 PT996 2 PU001–PU025 9 PU301 2 PU311–PU313 2 PV001–PV008 5 PV009–PV010 15 PV011 25 PV012–PV020 15 PV021–PV055 9 PV201–PV209 2 PV226–PV229 2 PV231–PV237 12 PV271–PV272 2 PV281–PV287 2 PV296 40 PV301–PV302 2 PV351 2 PV356–PV357 2 PW001–PW054 2
PW061–PW068 2 PW072 2 PW086–PW088 2 PW091–PW094 2 PW101–PW102 2 PW106 2 PW111–PW120 2 PW156–PW157 2 PW161–PW171 40 PW201–PW230 2 PW231–PW238 13 PW239–PW252 2 PW261 13 PW262–PW264 2 PW265 13 PW266–PW268 2 PW271–PW276 2 PW278 2 PW281 13
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Variable Group PW282–PW292 2 PW293 13 PW296 13 PW301–PW313 29 PW314–PW327 12 PW401–PW408 2 PW411–PW418 2 PW421–PW424 2 PW431–PW435 2 PW441–PW450 2 PW461–PW467 2 PW501–PW504 2 PW511–PW522 2 PW524–PW530 2 PW531–PW550 22 PW556–PW557 22 PW561–PW564 2 PW571–PW576 2 PW591–PW596 2 PW611–PW622 32
PW631–PW637 7 PW661–PW662 7 PW681–PW683 6 PW701–PW702 2 PW711–PW717 2 PW741–PW742 6 PW761 6 PW771 2 PW831 2 PW851–PW856 2 PX071 10 PX701 1 PY001–PY003 37 PY004–PY005 1 PY006 36 PY007–PY008 1 PY021–PY022 3 PY031 1 PY036–PY037 26
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Variable Group PY046–PY048 11 PY051–PY053 1 PY056–PY057 41 PY101 1 PY102–PY103 3 PY111–PY113 27 PY131–PY135 26 PY141–PY143 3 PY151–PY154 11 PY156–PY157 26 PY161 11 PY162 26 PY166 26 PY191 11 PY201 3 PY221–PY222 1 PY231 10 PY241–PY244 28 PY270 20 PY271–PY275 1
PY281 3 PY286 11 PY301–PY304 16 PY321–PY323 10 PY341–PY346 17 PY361–PY362 1 PY381 10 PY401 38 PY409–PY410 42 PY411 11 PY421–PY422 11 PY441 27 PY451 26 PY461–PY463 34 PY591–PY595 41 PY611 10 PY612 26 PY621 3 PY631 3
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Variable Group PY651 42 PY671–PY672 10 PY721 18 PY741 10
2. Spares Affected
Examine your spares supply for the parts or components identified in Paragraph 2.C., Parts Necessary for Each Airplane. If any parts or components are found, refer to Paragraph 2.C. for the recommended use.
B. Concurrent Requirements
None.
C. Reason
This service bulletin gives instructions to install two warning level indicator lights on the P2-2 center instrument panel in the flight compartment. The installation of these lights will provide a visual indication to the flight crew to be used in conjuction with the existing aural warning horn for cabin altitude and takeoff configuration alerts. The visual warning lights are intended to provide additional notice to crews to prepare a correct takeoff configuration, respond to excessive cabin altitude and avoid confusion between the takeoff configuration and cabin altitude alerts. An unrecognized incorrect takeoff configuration or excessive cabin altitude could prevent a continued safe flight and landing.
As a part of a service bulletin validation program, this change was completed on airplane PW234 by Service Bulletin 737-31A1325 Validation Copy 1 and Installation Deviation Records 737-31A1325- 001 through 737-31A1325-006 before the initial release of this service bulletin. The change completed on airplane PW234 by Service Bulletin 737-31A1325 Validation Copy 1 and Installation Deviation Records 737-31A1325-001 through 737-31A1325-006 is equivalent to the initial release of this service bulletin. Airplane PW234 has the configuration of a Group 13 airplane.
Boeing Service Related Problem (SRP) 737-SRP-31-0042 is related to this service bulletin.
D. Description
Get access to the flight compartment. Remove the P2-2 center instrument panel to install two warning level indicator lights on the panel and change three wire bundles. Reinstall the modified P2-2 center instrument panel. Do a test of the warning level indicator lights.
E. Compliance
The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to this service bulletin. The Airworthiness Directive will make the compliance tasks and times given in this service bulletin mandatory.
Boeing recommends that the change given in this service bulletin be done within 36 months after the date on this service bulletin.
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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.
G. Manpower
The table below shows an estimate of the task-hours necessary to do this change 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.
Number of Task Persons Task-Hours Elapsed Hours
Open Access 1 2.25 2.25 Remove 1 4.50 4.50 Change 3 15.00 5.00 Replace 1 4.50 4.50 Close Access 1 2.25 2.25 Test 2 4.00 2.00 TOTAL FOR EACH AIRPLANE 32.50 20.50
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H. Weight and Balance Changes
Change in Weight Change in Moment Airplane (Pounds) (Pound-Inches) 737-100 + 0.8 + 175 737-200/200C + 0.8 + 145 737-300 + 0.8 + 110 737-400 + 0.8 + 55 737-500 + 0.8 + 155
I. Electrical Load Data
Not changed.
J. References
1. Existing Data:
a. 737-100/200 Aircraft Maintenance Manual (AMM) 24-22-0, 27-88-11, 31-26-0, 32-42-0, 32-43-0, 34-11-0, 71-09-100, 78-32-01
b. 737-300/400/500 Aircraft Maintenance Manual (AMM) 24-22-00, 27-88-00, 31-26-00, 32-42-00, 32-43-01, 34-11-00, 71-00-00, 78-31-00
c. 737 Wiring Diagram 737-100/200 WDM 21-33-01, 27-43-01, 33-18-03, 33-18-12, 33-18-18, 80-11-11
d. 737 Wiring Diagram 737-300/400/500 WDM 21-33-01, 27-43-01, 33-18-03, 33-18-12, 33-18-18, 80-11-11
e. Overhaul Manual (OHM) 31-10-01
f. Standard Wiring Practices Manual (SWPM) 20-00-13, 20-10-11, SWPM 20-10-12, 20-10-18, 20-30-11, 20-30-12, 20-60-09, 20-61-11, 20-61-19
2. Data supplied with this Service Bulletin:
None
3. Installation Drawings Used in the Preparation of this Service Bulletin:
None
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K. Publications Affected
1. Publications
Publication Chapter-Section 737 FAA Approved Airplane Flight Manual Section 2 737 Flight Crew Operations Manual 1.10, 1.20, 15.10, 15.20 737 Maintenance Manual 31-26-0 (737-100/200/200C), 31-26-00 (737-300/400/500) 737 Wiring Diagram 21-33-01, 27-43-01, 33-18-03, 33-18-12, 33-18-18, 80-11- 11 737 Illustrated Parts Catalog 31-10 (737-100/200/200C), 31-11 (737-300/400/500) 737 System Schematic Manual 21-30-05, 27-09-00, 31-26-00 Component Maintenance Manual 31-36
2. Damage Tolerance Based Structural Inspections:
Boeing has evaluated the repairs and/or changes in this service bulletin for effects on Fatigue Critical Structure (FCS) and for changes to Damage Tolerance Inspections (DTI) required in the Maintenance Program. This service bulletin does not affect FCS, therefore DTIs are not necessary.
L. Interchangeability and Intermixability of Parts
Refer to Paragraph 2.C., Parts Necessary For Each Airplane, for interchangeability and intermixability information.
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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.
Unit Price thru ROLT December 31, Kit Number Name Date QTY (Weeks) 2009 65C38791-1 Top Kit - Cabin Altitude 8/31/07 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 9/17/07 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 10/01/07 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 10/15/07 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 10/29/07 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 11/12/07 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 11/28/07 25 17 $2,738.00
Warning Indication 65C38791-1 Top Kit - Cabin Altitude 12/12/07 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 1/04/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 1/18/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 2/01/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 2/15/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 2/29/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 3/14/08 10 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 5/09/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 5/23/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 6/09/08 25 17 $2,738.00 Warning Indication
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Unit Price thru ROLT December 31, Kit Number Name Date QTY (Weeks) 2009 65C38791-1 Top Kit - Cabin Altitude 6/23/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 7/08/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 7/22/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 8/05/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 8/19/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 9/03/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 9/17/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 10/01/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 10/15/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 10/29/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 11/12/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 11/26/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 12/12/08 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 1/06/09 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 1/20/09 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 2/03/09 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 2/17/09 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 3/03/09 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 3/17/09 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 3/31/09 25 17 $2,738.00 Warning Indication 65C38791-1 Top Kit - Cabin Altitude 4/14/09 25 17 $2,738.00 Warning Indication
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B. Industry Support Information
Boeing warranty remedies are not available for the configuration changes given in this service bulletin.
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C. Parts Necessary For Each Airplane
1. Kits/Parts:
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 65C38791
New Part QTY Number -1 Name Notes 65C38791-1 - Top Kit - Cabin Altitude Warning Indication 61-74487-1 1 Wire Kit - Cabin Altitude Warning Indication 61-74488-1 1 Wire Kit - Cabin Altitude Warning Indication 65C38242-1 1 Kit - Cabin Altitude Warning Indication, P2-2 Modification
Kit 61-74487
New Part QTY Number -101 -1 Name Notes 61-74487-1 . - Wire Kit - Cabin Altitude Warning Indication 61-74487-101 - . Wire Bundle W066 Assembly 61-74487-101 . 1 Wire Bundle W066 Assembly - 1 . Wire, Identified as W066-8032-20, Length 6 Feet (a) (d)
- 1 . Wire, Identified as W066-8033-20, Length 6 Feet (a) (d) - 1 . Wire, Identified as W066-8034-22, Length 2 Feet (b) (d) - 1 . Wire, Identified as W066-8035-22, Length 2 Feet (b) (d) - 1 . Wire, Identified as W066-8036-22, Length 2 Feet (b) (d) - 1 . Wire, Identified as W066-8037-22, Length 2 Feet (b) (d) - 1 . Wire, Identified as W066-8038-24, Length 2 Feet (c) (d) - 1 . Wire, Identified as W066-8039-24, Length 2 Feet (c) (d) 61-74487-2001 . 1 Lacing Tape, White, Length 27 Feet 61-74487-2002 . 1 Lacing Tape, Red, Length 9 Feet 61-74487-2003 . 1 Lacing Tape, Yellow, Length 9 Feet 61-74487-10101 1 . Connector Identification Tape, Imprinted "D04258J" 61-74487-10102 1 . Connector Identification Tape, Imprinted "D04260J" 61-74487-10103 1 . Splice Identification Sleeve, Imprinted "SP4016" 61-74487-10104 1 . Splice Identification Sleeve, Imprinted "SP4018" BACC47CN1S 3 . Pin Contact (e) BACT12AC44 2 . Terminal Lug BACT12AC48 14 . Terminal Lug BACT12AC52 14 . Terminal Lug D-436-58 3 . Splice Sleeve
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Kit 61-74487 New Part QTY Number -101 -1 Name Notes (a) Make from BMS 13-48, Type 10, Class 1, AWG 20. (b) Make from BMS 13-48, Type 10, Class 1, AWG 22. (c) Make from BMS 13-48, Type 11, Class 1, AWG 24. (d) Refer to SWPM 20-00-13 for alternative wire types. (e) There are more parts than are necessary.
Kit 61-74488
New Part QTY Number -112 -111 -1 Name Notes 61-74488-1 . . - Wire Kit - Cabin Altitude Warning Indication 61-74488-111 . - 1 Wire Bundle W002 Assembly 61-74488-112 - . 1 Wire Bundle W246 Assembly - . 1 . Wire, Identified as W002-8051-20, Length 10 Feet (a) (b) - . 1 . Wire, Identified as W002-8052-22, Length 10 Feet (a) (c) - 1 . . Wire, Identified as W246-170-20, Length 5 Feet (a) (b) - 1 . . Wire, Identified as W246-171-20, Length 40 Feet (a) (b) - 1 . . Wire, Identified as W246-172-22, Length 10 Feet (a) (c) 61-74488-2001 . . 1 Lacing Tape, White, Length 100 Feet 61-74488-2003 . . 1 Expandable Sleeve - White, 0.250 Inch Inner Diameter, Length 10 Feet 61-74488-2007 . . 1 Lacing Tape, Red, Length 15 Feet 61-74488-2008 . . 1 Lacing Tape, Yellow, Length 30 Feet 61-74488-10101 . 1 . Connector Identification (I.D.) Tape - D04258P 61-74488-10102 . 1 . Connector I.D. Tape - D04260P 61-74488-10103 . 1 . Connector I.D. Tape - D04006P 61-74488-10201 1 . . Connector I.D. Tape - D04006J 61-74488-10202 1 . . Connector I.D. Tape - D00776 61-74488-10203 1 . . Splice I.D. Sleeve - SM3 61-74488-10204 1 . . Splice I.D. Sleeve - SP2218 61-74488-10205 1 . . Splice I.D. Sleeve - SM21 61-74488-10207 1 . . Splice I.D. Sleeve - SM23 61-74488-10212 1 . . Diode I.D. Sleeve - M2592 61-74488-10213 1 . . Thermofit Sleeve - 0.093 Inch Inner Diameter, Length 2 Inches 69-58806-4 1 . . Diode Assembly BACC47CN1S . 3 . Pin Contact (d) BACC47CP1S 3 3 . Socket Contact (d)
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Kit 61-74488 New Part QTY Number -112 -111 -1 Name Notes BACC47DR1 2 . . Socket Contact (d) D-436-37 4 . . Splice (d) D-436-38 2 . . Splice (d) (a) Make from BMS 13-48, Type 10, Class 1, AWG 20. (b) Make from BMS 13-48, Type 10, Class 1, AWG 22. (c) Refer to SWPM 20-00-13 for alternative wire types. (d) There are more parts than are necessary.
Kit 65C38242 QTY New Part Number -1 Name Notes 65C38242-1 - Kit - Cabin Altitude Warning Indication, P2-2 Modification 318-630-1001-452 1 Light Assembly, PRESS-TO-TEST Indicator 318-630-1001-460 1 Light Assembly, PRESS-TO-TEST Indicator
2. Parts and Materials Supplied by the Operator:
Part Number / Specification QTY Name Notes
61-74488-2004 1 Loctite 222, Thread Lock Compound 61-74488-2005 1 Adhesive Tape, Permacel P-421 or equivalent, 0.5 Inch Width 61-74488-2006 1 Adhesive Tape, Permacel P-440 or equivalent, 1.0 Inch Width (c) See the Qualified Products List at the end of the Boeing Material Specification (BMS) for supplier data.
3. Parts Modified and Reidentified:
The parts shown below are changed as shown in this service bulletin. The quantity (QTY) is the number of parts changed on each airplane.
Existing Part Number QTY Name New Part Number Notes 69-37305-1 1 P2-2 Center Instrument Module Assembly 69-37305-2001 (a) 69-37305-101 1 P2-2 Center Instrument Module Assembly 69-37305-2101 (a) 69-37305-104 1 P2-2 Center Instrument Module Assembly 69-37305-2104 (a) 69-37305-107 1 P2-2 Center Instrument Module Assembly 69-37305-2107 (a) 69-37305-11 1 P2-2 Center Instrument Module Assembly 69-37305-2011 (a) 69-37305-110 1 P2-2 Center Instrument Module Assembly 69-37305-2110 (a)
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Existing Part Number QTY Name New Part Number Notes 69-37305-111 1 P2-2 Center Instrument Module Assembly 69-37305-2111 (a) 69-37305-114 1 P2-2 Center Instrument Module Assembly 69-37305-2114 (a) 69-37305-120 1 P2-2 Center Instrument Module Assembly 69-37305-2120 (a) 69-37305-123 1 P2-2 Center Instrument Module Assembly 69-37305-2123 (a) 69-37305-126 1 P2-2 Center Instrument Module Assembly 69-37305-2126 (a) 69-37305-129 1 P2-2 Center Instrument Module Assembly 69-37305-2129 (a) 69-37305-135 1 P2-2 Center Instrument Module Assembly 69-37305-2135 (a) 69-37305-138 1 P2-2 Center Instrument Module Assembly 69-37305-2138 (a) 69-37305-14 1 P2-2 Center Instrument Module Assembly 69-37305-2014 (a) 69-37305-141 1 P2-2 Center Instrument Module Assembly 69-37305-2141 (a) 69-37305-144 1 P2-2 Center Instrument Module Assembly 69-37305-2144 (a) 69-37305-1452 1 P2-2 Center Instrument Module Assembly 69-37305-3452 (a) 69-37305-147 1 P2-2 Center Instrument Module Assembly 69-37305-2147 (a) 69-37305-148 1 P2-2 Center Instrument Module Assembly 69-37305-2148 (a) 69-37305-151 1 P2-2 Center Instrument Module Assembly 69-37305-2151 (a) 69-37305-155 1 P2-2 Center Instrument Module Assembly 69-37305-2155 (a) 69-37305-158 1 P2-2 Center Instrument Module Assembly 69-37305-2158 (a) 69-37305-163 1 P2-2 Center Instrument Module Assembly 69-37305-2163 (a) 69-37305-167 1 P2-2 Center Instrument Module Assembly 69-37305-2167 (a) 69-37305-1684 1 P2-2 Center Instrument Module Assembly 69-37305-3684 (a) 69-37305-1688 1 P2-2 Center Instrument Module Assembly 69-37305-3688 (a) 69-37305-170 1 P2-2 Center Instrument Module Assembly 69-37305-2170 (a) 69-37305-173 1 P2-2 Center Instrument Module Assembly 69-37305-2173 (a) 69-37305-180 1 P2-2 Center Instrument Module Assembly 69-37305-2180 (a) 69-37305-184 1 P2-2 Center Instrument Module Assembly 69-37305-2184 (a) 69-37305-188 1 P2-2 Center Instrument Module Assembly 69-37305-2188 (a) 69-37305-201 1 P2-2 Center Instrument Module Assembly 69-37305-2201 (a) 69-37305-205 1 P2-2 Center Instrument Module Assembly 69-37305-2205 (a) 69-37305-217 1 P2-2 Center Instrument Module Assembly 69-37305-2217 (a) 69-37305-22 1 P2-2 Center Instrument Module Assembly 69-37305-2022 (a) 69-37305-233 1 P2-2 Center Instrument Module Assembly 69-37305-2233 (a) 69-37305-240 1 P2-2 Center Instrument Module Assembly 69-37305-2240 (a) 69-37305-241 1 P2-2 Center Instrument Module Assembly 69-37305-2241 (a) 69-37305-245 1 P2-2 Center Instrument Module Assembly 69-37305-2245 (a) 69-37305-246 1 P2-2 Center Instrument Module Assembly 69-37305-2246 (a) 69-37305-247 1 P2-2 Center Instrument Module Assembly 69-37305-2247 (a) 69-37305-25 1 P2-2 Center Instrument Module Assembly 69-37305-2025 (a) 69-37305-266 1 P2-2 Center Instrument Module Assembly 69-37305-2266 (a)
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Existing Part Number QTY Name New Part Number Notes 69-37305-270 1 P2-2 Center Instrument Module Assembly 69-37305-2270 (a) 69-37305-271 1 P2-2 Center Instrument Module Assembly 69-37305-2271 (a) 69-37305-275 1 P2-2 Center Instrument Module Assembly 69-37305-2275 (a) 69-37305-279 1 P2-2 Center Instrument Module Assembly 69-37305-2279 (a) 69-37305-28 1 P2-2 Center Instrument Module Assembly 69-37305-2028 (a) 69-37305-283 1 P2-2 Center Instrument Module Assembly 69-37305-2283 (a) 69-37305-290 1 P2-2 Center Instrument Module Assembly 69-37305-2290 (a) 69-37305-293 1 P2-2 Center Instrument Module Assembly 69-37305-2293 (a) 69-37305-297 1 P2-2 Center Instrument Module Assembly 69-37305-2297 (a) 69-37305-301 1 P2-2 Center Instrument Module Assembly 69-37305-2301 (a) 69-37305-305 1 P2-2 Center Instrument Module Assembly 69-37305-2305 (a) 69-37305-309 1 P2-2 Center Instrument Module Assembly 69-37305-2309 (a) 69-37305-31 1 P2-2 Center Instrument Module Assembly 69-37305-2031 (a) 69-37305-310 1 P2-2 Center Instrument Module Assembly 69-37305-2310 (a) 69-37305-318 1 P2-2 Center Instrument Module Assembly 69-37305-2318 (a) 69-37305-323 1 P2-2 Center Instrument Module Assembly 69-37305-2323 (a) 69-37305-327 1 P2-2 Center Instrument Module Assembly 69-37305-2327 (a) 69-37305-331 1 P2-2 Center Instrument Module Assembly 69-37305-2331 (a) 69-37305-335 1 P2-2 Center Instrument Module Assembly 69-37305-2335 (a) 69-37305-339 1 P2-2 Center Instrument Module Assembly 69-37305-2339 (a) 69-37305-34 1 P2-2 Center Instrument Module Assembly 69-37305-2034 (a) 69-37305-343 1 P2-2 Center Instrument Module Assembly 69-37305-2343 (a) 69-37305-347 1 P2-2 Center Instrument Module Assembly 69-37305-2347 (a) 69-37305-35 1 P2-2 Center Instrument Module Assembly 69-37305-2035 (a) 69-37305-351 1 P2-2 Center Instrument Module Assembly 69-37305-2351 (a) 69-37305-355 1 P2-2 Center Instrument Module Assembly 69-37305-2355 (a) 69-37305-359 1 P2-2 Center Instrument Module Assembly 69-37305-2359 (a) 69-37305-36 1 P2-2 Center Instrument Module Assembly 69-37305-2036 (a) 69-37305-362 1 P2-2 Center Instrument Module Assembly 69-37305-2362 (a) 69-37305-363 1 P2-2 Center Instrument Module Assembly 69-37305-2363 (a) 69-37305-367 1 P2-2 Center Instrument Module Assembly 69-37305-2367 (a) 69-37305-37 1 P2-2 Center Instrument Module Assembly 69-37305-2037 (a) 69-37305-371 1 P2-2 Center Instrument Module Assembly 69-37305-2371 (a) 69-37305-375 1 P2-2 Center Instrument Module Assembly 69-37305-2375 (a) 69-37305-379 1 P2-2 Center Instrument Module Assembly 69-37305-2379 (a) 69-37305-38 1 P2-2 Center Instrument Module Assembly 69-37305-2038 (a) 69-37305-383 1 P2-2 Center Instrument Module Assembly 69-37305-2383 (a) 69-37305-387 1 P2-2 Center Instrument Module Assembly 69-37305-2387 (a)
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Existing Part Number QTY Name New Part Number Notes 69-37305-39 1 P2-2 Center Instrument Module Assembly 69-37305-2039 (a) 69-37305-390 1 P2-2 Center Instrument Module Assembly 69-37305-2390 (a) 69-37305-394 1 P2-2 Center Instrument Module Assembly 69-37305-2394 (a) 69-37305-398 1 P2-2 Center Instrument Module Assembly 69-37305-2398 (a) 69-37305-402 1 P2-2 Center Instrument Module Assembly 69-37305-2402 (a) 69-37305-406 1 P2-2 Center Instrument Module Assembly 69-37305-2406 (a) 69-37305-410 1 P2-2 Center Instrument Module Assembly 69-37305-2410 (a) 69-37305-414 1 P2-2 Center Instrument Module Assembly 69-37305-2414 (a) 69-37305-418 1 P2-2 Center Instrument Module Assembly 69-37305-2418 (a) 69-37305-422 1 P2-2 Center Instrument Module Assembly 69-37305-2422 (a) 69-37305-425 1 P2-2 Center Instrument Module Assembly 69-37305-2425 (a) 69-37305-433 1 P2-2 Center Instrument Module Assembly 69-37305-2433 (a) 69-37305-437 1 P2-2 Center Instrument Module Assembly 69-37305-2437 (a) 69-37305-448 1 P2-2 Center Instrument Module Assembly 69-37305-2448 (a) 69-37305-452 1 P2-2 Center Instrument Module Assembly 69-37305-2452 (a) 69-37305-456 1 P2-2 Center Instrument Module Assembly 69-37305-2456 (a) 69-37305-457 1 P2-2 Center Instrument Module Assembly 69-37305-2457 (a) 69-37305-461 1 P2-2 Center Instrument Module Assembly 69-37305-2461 (a) 69-37305-463 1 P2-2 Center Instrument Module Assembly 69-37305-2463 (a) 69-37305-467 1 P2-2 Center Instrument Module Assembly 69-37305-2467 (a) 69-37305-471 1 P2-2 Center Instrument Module Assembly 69-37305-2471 (a) 69-37305-475 1 P2-2 Center Instrument Module Assembly 69-37305-2475 (a) 69-37305-479 1 P2-2 Center Instrument Module Assembly 69-37305-2479 (a) 69-37305-483 1 P2-2 Center Instrument Module Assembly 69-37305-2483 (a) 69-37305-487 1 P2-2 Center Instrument Module Assembly 69-37305-2487 (a) 69-37305-491 1 P2-2 Center Instrument Module Assembly 69-37305-2491 (a) 69-37305-495 1 P2-2 Center Instrument Module Assembly 69-37305-2495 (a) 69-37305-5 1 P2-2 Center Instrument Module Assembly 69-37305-2005 (a) 69-37305-51 1 P2-2 Center Instrument Module Assembly 69-37305-2051 (a) 69-37305-55 1 P2-2 Center Instrument Module Assembly 69-37305-2055 (a) 69-37305-59 1 P2-2 Center Instrument Module Assembly 69-37305-2059 (a) 69-37305-60 1 P2-2 Center Instrument Module Assembly 69-37305-2060 (a) 69-37305-600 1 P2-2 Center Instrument Module Assembly 69-37305-2600 (a) 69-37305-603 1 P2-2 Center Instrument Module Assembly 69-37305-2603 (a) 69-37305-609 1 P2-2 Center Instrument Module Assembly 69-37305-2609 (a) 69-37305-61 1 P2-2 Center Instrument Module Assembly 69-37305-2061 (a) 69-37305-612 1 P2-2 Center Instrument Module Assembly 69-37305-2612 (a) 69-37305-615 1 P2-2 Center Instrument Module Assembly 69-37305-2615 (a)
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Existing Part Number QTY Name New Part Number Notes 69-37305-62 1 P2-2 Center Instrument Module Assembly 69-37305-2062 (a) 69-37305-623 1 P2-2 Center Instrument Module Assembly 69-37305-2623 (a) 69-37305-627 1 P2-2 Center Instrument Module Assembly 69-37305-2627 (a) 69-37305-63 1 P2-2 Center Instrument Module Assembly 69-37305-2063 (a) 69-37305-631 1 P2-2 Center Instrument Module Assembly 69-37305-2631 (a) 69-37305-634 1 P2-2 Center Instrument Module Assembly 69-37305-2634 (a) 69-37305-64 1 P2-2 Center Instrument Module Assembly 69-37305-2064 (a) 69-37305-642 1 P2-2 Center Instrument Module Assembly 69-37305-2642 (a) 69-37305-644 1 P2-2 Center Instrument Module Assembly 69-37305-2644 (a) 69-37305-648 1 P2-2 Center Instrument Module Assembly 69-37305-2648 (a) 69-37305-65 1 P2-2 Center Instrument Module Assembly 69-37305-2065 (a) 69-37305-659 1 P2-2 Center Instrument Module Assembly 69-37305-2659 (a) 69-37305-663 1 P2-2 Center Instrument Module Assembly 69-37305-2663 (a) 69-37305-667 1 P2-2 Center Instrument Module Assembly 69-37305-2667 (a) 69-37305-671 1 P2-2 Center Instrument Module Assembly 69-37305-2671 (a) 69-37305-675 1 P2-2 Center Instrument Module Assembly 69-37305-2675 (a) 69-37305-679 1 P2-2 Center Instrument Module Assembly 69-37305-2679 (a) 69-37305-68 1 P2-2 Center Instrument Module Assembly 69-37305-2068 (a) 69-37305-683 1 P2-2 Center Instrument Module Assembly 69-37305-2683 (a) 69-37305-684 1 P2-2 Center Instrument Module Assembly 69-37305-2684 (a) 69-37305-685 1 P2-2 Center Instrument Module Assembly 69-37305-2685 (a) 69-37305-686 1 P2-2 Center Instrument Module Assembly 69-37305-2686 (a) 69-37305-687 1 P2-2 Center Instrument Module Assembly 69-37305-2687 (a) 69-37305-688 1 P2-2 Center Instrument Module Assembly 69-37305-2688 (a) 69-37305-69 1 P2-2 Center Instrument Module Assembly 69-37305-2069 (a) 69-37305-694 1 P2-2 Center Instrument Module Assembly 69-37305-2694 (a) 69-37305-698 1 P2-2 Center Instrument Module Assembly 69-37305-2698 (a) 69-37305-699 1 P2-2 Center Instrument Module Assembly 69-37305-2699 (a) 69-37305-700 1 P2-2 Center Instrument Module Assembly 69-37305-2700 (a) 69-37305-701 1 P2-2 Center Instrument Module Assembly 69-37305-2701 (a) 69-37305-703 1 P2-2 Center Instrument Module Assembly 69-37305-2703 (a) 69-37305-707 1 P2-2 Center Instrument Module Assembly 69-37305-2707 (a) 69-37305-709 1 P2-2 Center Instrument Module Assembly 69-37305-2709 (a) 69-37305-72 1 P2-2 Center Instrument Module Assembly 69-37305-2072 (a) 69-37305-75 1 P2-2 Center Instrument Module Assembly 69-37305-2075 (a) 69-37305-78 1 P2-2 Center Instrument Module Assembly 69-37305-2078 (a) 69-37305-8 1 P2-2 Center Instrument Module Assembly 69-37305-2008 (a) 69-37305-81 1 P2-2 Center Instrument Module Assembly 69-37305-2081 (a)
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Existing Part Number QTY Name New Part Number Notes 69-37305-82 1 P2-2 Center Instrument Module Assembly 69-37305-2082 (a) 69-37305-87 1 P2-2 Center Instrument Module Assembly 69-37305-2087 (a) 69-37305-88 1 P2-2 Center Instrument Module Assembly 69-37305-2088 (a) 69-37305-91 1 P2-2 Center Instrument Module Assembly 69-37305-2091 (a) 69-37305-92 1 P2-2 Center Instrument Module Assembly 69-37305-2092 (a) 69-37305-95 1 P2-2 Center Instrument Module Assembly 69-37305-2095 (a) 69-37305-98 1 P2-2 Center Instrument Module Assembly 69-37305-2098 (a) (a) Make the change given in this service bulletin.
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.
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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. Refer to the Boeing Standard Wiring Practices Manuals 20-10-11 and 20-10-12 for the wire installation procedures.
4. 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.
5. These work instructions refer to procedures included on other Boeing documents. When the words "refer to" are used and the operator has an accepted alternative procedure, the accepted alternative procedure can be used. When the words "in accordance with" are included in the instruction, the procedure in the Boeing document
must be used.
B. WORK INSTRUCTIONS
1. Remove electrical power from the airplane. Refer to 737-100/200 AMM 24-22-0 or 737-300/400/ 500 AMM 24-22-00 as an accepted procedure.
2. Get access to the flight compartment.
3. Remove the P2-2 center instrument panel in accordance with Figure 1.
4. Modify the P2-2 center instrument panel in accordance with Figure 2.
5. Install the light assembly in accordance with Figure 3.
6. Change wire bundle W066:
a. Group 14, 17: In accordance with Figures 4 and 8.
b. Group 1, 4, 24, 43: In accordance with Figures 4 and 9.
c. Group 15, 25: In accordance with Figures 4 and 10.
d. Group 6, 23: In accordance with Figures 4 and 11.
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e. Group 7-8: In accordance with Figures 4 and 12.
f. Group 5, 9: In accordance with Figures 4 and 13.
g. Group 10: In accordance with Figures 4 and 14.
h. Group 16: In accordance with Figures 4 and 15.
i. Group 3: In accordance with Figures 4 and 16.
j. Group 18: In accordance with Figures 4 and 17.
k. Group 19: In accordance with Figures 4 and 18.
l. Group 20: In accordance with Figures 4 and 19.
m. Group 21-22: In accordance with Figures 4 and 20.
n. Group 2, 13: In accordance with Figures 4 and 21.
o. Group 11: In accordance with Figures 4 and 22.
p. Group 26: In accordance with Figures 4 and 23.
q. Group 27: In accordance with Figures 4 and 24.
r. Group 28: In accordance with Figures 4 and 25.
s. Group 12, 29: In accordance with Figures 4 and 26.
t. Group 31-32: In accordance with Figures 4 and 27.
u. Group 33: In accordance with Figures 4 and 28.
v. Group 34: In accordance with Figures 4 and 29.
w. Group 35: In accordance with Figures 4 and 30.
x. Group 36: In accordance with Figures 4 and 31.
y. Group 37: In accordance with Figures 5 and 32.
z. Group 38: In accordance with Figures 4 and 33.
aa. Group 39: In accordance with Figures 6 and 34.
ab. Group 40: In accordance with Figures 6 and 35.
ac. Group 41: In accordance with Figures 6 and 36.
ad. Group 42: In accordance with Figures 6 and 37.
ae. Group 30: In accordance with Figures 6 and 38.
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af. Group 44: In accordance with Figures 6 and 39.
ag. Group 45: In accordance with Figures 6 and 40.
ah. Group 46: In accordance with Figures 6 and 41.
ai. Group 47: In accordance with Figures 6 and 42.
aj. Group 48: In accordance with Figures 6 and 43.
ak. Group 49: In accordance with Figures 7 and 44.
7. Change wire bundle W002:
a. Group 1, 3, 5-10, 15-20, 23, 25: In accordance with Figures 45 and 47.
b. Group 2, 13, 21-23: In accordance with Figures 45 and 48.
c. Group 11, 26-28: In accordance with Figures 45 and 49.
d. Group 12, 29, 31-32: In accordance with Figures 45 and 50.
e. Group 33: In accordance with Figures 45 and 51.
f. Group 34: In accordance with Figures 45 and 52.
g. Group 35: In accordance with Figures 45 and 53.
h. Group 36-37: In accordance with Figures 45 and 54.
i. Group 38: In accordance with Figures 45 and 55.
j. Group 4, 14, 43: In accordance with Figures 45 and 56.
k. Group 24: In accordance with Figures 45 and 57.
l. Group 30, 39-42: In accordance with Figures 46 and 58.
m. Group 44-48: In accordance with Figures 46 and 59.
n. Group 49: In accordance with Figures 7 and 60.
8. Change wire bundle W246:
a. Group 1, 3, 5, 8, 10-11, 13, 15-21, 23, 26-31, 33-34, 36-39, 41-42, 44, 46-49: In accordance with Figures 61 and 62.
b. Group 2, 6-7, 9, 12, 22, 25, 32, 35, 40, 45: In accordance with Figures 61 and 63.
c. Group 4, 14: In accordance with Figures 61 and 64.
d. Group 24: In accordance with Figures 61 and 65.
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e. Group 43: In accordance with Figures 61 and 66.
9. Install the P2-2 center instrument panel in accordance with Figure 67.
10. Restore electrical power removed in Step 1. Refer to 737-100/200 AMM 24-22-0 or 737-300/400/ 500 AMM 24-22-00 as an accepted procedure.
11. Do the "Antiskid Indication Monitor Function Test". Refer to 737-100/200 AMM 32-42-0 or 737-300/400/500 AMM 32-42-00 as an accepted procedure.
12. Do the "Automatic Braking System Test". Refer to 737-100/200 AMM 32-43-0 or 737-300/400/ 500 AMM 32-43-01 as an accepted procedure.
13. Do the test of the leading edge flap and slat indicators. Refer to 737-100/200 AMM 27-88-11 or 737-300/400/500 AMM 27-88-00 as an accepted procedure.
14. Do a test of the reverser indicator lights. Refer to 737-100/200 AMM 78-32-01 or 737-300/400/ 500 AMM 78-31-00 as an accepted procedure.
15. Do a test of the takeoff warning system as follows:
Group 1, 3-4, 10-11, 14, 16-20, 24, 26-28, 30, 33-34, 36-39, 41-44, 46-49:
a. Make sure these circuit breakers are closed:
Panel/Location Circuit Breaker Name P6-2 or P6-3 C404 LANDING GEAR AIR/GND RELAY LIGHTS
P6-2 or P6-3 C451 AURAL WARN P6-2 C552 ENGINE PRESSURE RATIO WARNING
b. Do one of these steps:
(1) Make sure the flap control lever is outside of the takeoff range.
(2) Make sure the speedbrake handle is not in the down detent position
(3) Make sure the stabilizer is out of the green band range.
(4) Make sure the leading edge flaps are not extended.
(5) Make sure the parking brake is set.
c. For airplanes that have a engine pressure ratio (EPR) activated takeoff warning, do the following test.
In the electrical/electronics compartment, at the M528 engine accessory unit (EAU) on the E3-2 electronics shelf, press and hold the S1 Engine 1 or S2 Engine 2 engine pressure ratio (EPR) test switch on the front of the M528 EAU.
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NOTE: Airplanes that do not have the EPR activated takeoff warning, do not need this step completed.
d. Move the thrust levers to the takeoff position.
(1) Make sure you hear the warning horn.
(2) Make sure the "Red" TAKE OFF WARNING light on the P2-2 panel is on.
e. Move the thrust levers to the idle position.
(1) Make sure the warning horn stops.
(2) Make sure the "Red" TAKE OFF WARNING light on the P2-2 panel is off.
f. In the electrical/electronics compartment, at the M528 EAU on the E3-2 electronics shelf, release the S1 Engine 1 or S2 Engine 2 EPR test switch on the front of the M528 EAU.
NOTE: Airplanes that do not have the EPR activated takeoff warning, do not need this step completed.
(1) Make sure the warning horn stays off.
(2) Make sure the "Red" TAKE OFF WARNING light on the P2-2 panel stays off.
Group 2, 5-9, 12-13, 15, 21-23, 25, 29, 31-32, 35, 40, 45:
a. Make sure these circuit breakers are closed:
Panel/Location Circuit Breaker Name P6-2 or P6-3 C404 LANDING GEAR AIR/GND RELAY LIGHTS P6-2 C451 AURAL WARN
b. Do one of these steps:
(1) Make sure the flap control lever is outside of the takeoff range.
(2) Make sure the speedbrake handle is not in the down detent position
(3) Make sure the stabilizer is out of the green band range.
(4) Make sure the leading edge flaps are not extended.
(5) Make sure the parking brake is set.
c. Move the thrust levers to the takeoff position.
(1) Make sure you hear the warning horn.
(2) Make sure the "Red" TAKE OFF WARNING light on the P2-2 panel is on.
d. Move the thrust levers to the idle position.
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(1) Make sure the warning horn stops.
(2) Make sure the "Red" TAKE OFF WARNING light on the P2-2 panel is off.
16. Do a test of the Cabin Altitude Warning System as follows:
a. Open the forward access door.
b. Make sure these circuit breakers are closed:
Panel/Location Circuit Breaker Name P6-2 or P6-3 C451 AURAL WARN P6-2 or P6-3 C129 LAND LATCH & PRESS WARN
c. Do a test of the altitude warning horn.
(1) Remove the vent port screen.
(2) Connect the pitot static system tester (No. 4 Union and O-ring) to the vent port of the warning switch for the cabin altitude. Refer to 737-100/200 AMM 34-11-0 or 737-300/ 400/500 AMM 34-11-00 as an accepted procedure..
(3) Operate the system by slowly increasing the vacuum and monitor the altimeter.
(4) Make a record of the altitude at which you hear the warning horn.
(a) Make sure you hear the intermittent warning horn at an altitude between 9,000
and 11,000 feet.
(b) Make sure the "Red" CABIN ALTITUDE light on the P2-2 panel is on.
(5) Push the switch for the ALTITUDE HORN CUTOUT.
(a) Make sure the warning horn stops.
(b) Make sure the "Red" CABIN ALTITUDE light on the P2-2 panel remains on.
(6) Slowly lower the altitude shown to approximately 1,700 feet below the altitude at which you hear the horn.
(a) Make sure the "Red" CABIN ALTITUDE light on the P2-2 panel goes off.
(7) Increase the altitude.
(a) Make sure the horn is again heard between 9,000 and 11,000 feet.
(b) Make sure the "Red" CABIN ALTITUDE light on the P2-2 panel comes on.
(8) Decrease the altitude to the ground level.
d. Disconnect the pitot static system equipment.
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e. Install the vent port screen.
f. Close the forward access panel.
17. Do the Power Plant Operational Test as follows:
a. With the engine stopped:
(1) Make sure the amber LOW OIL PRESSURE light on the pilots center instrument panel, P2, is on.
(2) Make sure the amber OIL FILTER BYPASS light on the pilots center instrument panel, P2, is off.
b. Do the Power Plant Operation (Normal) procedure. Refer to 737-100/200 AMM 71-09-100 or 737-300/400/500 AMM 71-00-00 as an accepted procedure.
c. Operate each engine at the same power setting. Refer to 737-100/200 AMM 71-09-100 or 737-300/400/500 AMM 71-00-00 as an accepted procedure.
(1) Make sure the amber START VALVE OPEN light on the pilots center instrument panel, P2, goes off.
(2) Monitor the LOW OIL PRESSURE light and oil pressure indicator.
(a) The light must go off at or before the oil pressure is 15.25 psi.
(b) The LOW OIL PRESSURE light must stay off during the engine operation.
(3) Make sure the OIL FILTER BYPASS light stays off during the engine operation.
(4) Make sure the oil quantity indicator reads: For EIS airplanes: 94 - 100%. For non-EIS airplanes: 4.5 gallons for engine No. 1 or 4.75 gallons for engine No. 2 (on airplanes with indicators graduated from 0 to 4.5 U.S. gallons) or 17 liters for engine No. 1 or 18 liters for engine No. 2 (on airplanes with indicators graduated from 0 to 18 liters).
(5) Push and hold the ENG OIL QTY TEST switch on the pilots center instrument panel P2-2 (non-EIS airplanes only).
(a) The indicator pointer will start to move to zero.
(b) Release the ENG OIL QTY TEST switch.
1) The indicator pointer will go back to its initial value.
(6) Make sure the oil temperature indication for the two engines is approximately equal.
(7) Make sure the N1 indicators show approximately the same N1% when the N2 indicators show the same N2%.
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(8) Make sure that the EGT for the engine system in test is approximately the same as that for the other engine.
(9) Make sure the Fuel Flow indication for the two engines is approximately equal.
d. Stop the engines. Refer to 737-100/200 AMM 71-09-100 or 737-300/400/500 AMM 71-00-00 as an accepted procedure.
18. Put the airplane in a serviceable condition.
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FIGURE 1: P2-2 CENTER INSTRUMENT PANEL REMOVAL
FLIGHT COMPARTMENT 1 1
P2-2 CENTER INSTRUMENT PANEL P2-2 CENTER INSTRUMENT PANEL EIS CONFIGURATION NON-EIS CONFIGURATION 1366853
FIGURE 1: P2-2 CENTER INSTRUMENT PANEL REMOVAL Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 83 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
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.
STEP TASK NAME IDENTIFICATION QTY MORE DATA Remove/Keep P2-2 Panel 69-37305-( ) 1 Refer to OHM 31-10-01 as 1 an accepted procedure.
FIGURE 1: P2-2 CENTER INSTRUMENT PANEL REMOVAL Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 84 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 2: MODIFICATION OF THE P2-2 CENTER INSTRUMENT PANEL
SEE A
FLIGHT COMPARTMENT
0.55 1.94 0.45
1.70 1.60
0.44 2
1 STIFFENER
P2-2 CENTER INSTRUMENT PANEL EIS CONFIGURATION A 1367051
FIGURE 2: MODIFICATION OF THE P2-2 CENTER INSTRUMENT PANEL Original Issue: January 11, 2010 (SHEET 1 OF 3) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 85 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
1.05 1.05 1.94 0.95 0.94 0.95
1.70 2.30 1.60 2.20
0.44 0.94
1 1
2 2
P2-2 CENTER INSTRUMENT PANEL P2-2 CENTER INSTRUMENT PANEL PREFERRED NON-EIS CONFIGURATION OPTIONAL NON-EIS CONFIGURATION
A A 1367888
FIGURE 2: MODIFICATION OF THE P2-2 CENTER INSTRUMENT PANEL Original Issue: January 11, 2010 (SHEET 2 OF 3) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 86 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
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.
STEP TASK NAME IDENTIFICATION QTY MORE DATA Cut Hole - 1 (a) 1 NOTE: For NON-EIS airplanes, the two lights can be configured with one on top of the other no less than 1.70 inches from the panel top for visual purposes. Identify P2-2 Center 69-37305-( ) 1 (b) 2 Instrument Panel (a) Lights can be located to the left of location shown if the designated space is already in use for EIS and NON-EIS configurations. (b) Refer to Paragraph 2.C.3., Parts Modified and Reidentified.
FIGURE 2: MODIFICATION OF THE P2-2 CENTER INSTRUMENT PANEL Original Issue: January 11, 2010 (SHEET 3 OF 3) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 87 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 3: LIGHT ASSEMBLY INSTALLATION
SEE A
FLIGHT COMPARTMENT
1 2
P2-2 CENTER INSTRUMENT PANEL EIS CONFIGURATION A 1368247
FIGURE 3: LIGHT ASSEMBLY INSTALLATION Original Issue: January 11, 2010 (SHEET 1 OF 3) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 88 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
1 2
1 2
P2-2 CENTER INSTRUMENT PANEL P2-2 CENTER INSTRUMENT PANEL PREFERRED NON-EIS CONFIGURATION OPTIONAL NON-EIS CONFIGURATION
A A 1368348
FIGURE 3: LIGHT ASSEMBLY INSTALLATION Original Issue: January 11, 2010 (SHEET 2 OF 3) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 89 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
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.
STEP TASK NAME IDENTIFICATION QTY MORE DATA Install Light Assembly 318-630-1001-452 1 "CABIN ALTITUDE". Refer to 1 OHM 31-10-01 as an accepted procedure. Install Light Assembly 318-630-1001-460 1 "TAKEOFF CONFIG". Refer to 2 OHM 31-10-01 as an accepted procedure.
FIGURE 3: LIGHT ASSEMBLY INSTALLATION Original Issue: January 11, 2010 (SHEET 3 OF 3) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 90 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 4: WIRE BUNDLE W066 WIRE ROUTING - GROUPS 1-29, 31-36, 38 AND 43 AIRPLANES
L1316
L1304
W066
D4258J L360
L361
FWD 1368514
FIGURE 4: WIRE BUNDLE W066 WIRE ROUTING - GROUPS 1-29, 31-36, 38 AND 43 AIRPLANES January 11, 2010 (SHEET 1 OF 1) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 91 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 5: WIRE BUNDLE W066 WIRE ROUTING - GROUP 37 AIRPLANES
L1316 L1304
L381
W066
D4258J L360
FWD 1369399
FIGURE 5: WIRE BUNDLE W066 WIRE ROUTING - GROUP 37 AIRPLANES January 11, 2010 (SHEET 1 OF 1) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 92 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 6: WIRE BUNDLE W066 WIRE ROUTING - GROUPS 30, 39-42 AND 44-48 AIRPLANES
L1316 L1304
W066
D4260J L360
L361
FWD 1369323
FIGURE 6: WIRE BUNDLE W066 WIRE ROUTING - GROUPS 30, 39-42 AND 44-48 AIRPLANES January 11, 2010 (SHEET 1 OF 1) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 93 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 7: WIRE BUNDLES W002 AND W066 WIRE ROUTING - GROUP 49 AIRPLANES
W002
D4006P A
P2-2
PANEL
W002
DISC STA 178
FWD 1368896
FIGURE 7: WIRE BUNDLES W002 AND W066 WIRE ROUTING - GROUP 49 AIRPLANES January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 94 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
L1316
L1304
W066
SPLICE AREA L360
L361 A
FWD 1368898
FIGURE 7: WIRE BUNDLES W002 AND W066 WIRE ROUTING - GROUP 49 AIRPLANES January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 95 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 8: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 14 AND 17 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 10 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W066-8036-22 2 W002
R 4 W066-8037-22 2
2 4 R W066-8033-20 1 12 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-22 8 L361 LOW OIL PRESSURE ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING EXISTING WIRE 1369585
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 8: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 14 AND 17 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 96 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 8: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 14 AND 17 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 97 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 9: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 1, 4, 24 AND 43 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 10 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8032-20 1 12 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 8 L361 LOW OIL PRESSURE ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING EXISTING WIRE 1366707
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 9: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 1, 4, 24 AND 43 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 98 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 9: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 1, 4, 24 AND 43 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 99 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 10: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 15 AND 25 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 10 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8032-20 1 12 1 W066-8038-24 3 J D4258P L1316 TAKEOFF WARNING
LIGHT 8 3 W066-031-24 A 4 W066-016-24
2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3 A 4
2 A 1 W066-055-24 W066-153-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368310
REFERENCE: 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01, 737-300/400/500 WDM 33-18-03, 737-300/400/500 WDM 33-18-12.
FIGURE 10: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 15 AND 25 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 100 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 10: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 15 AND 25 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 101 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 11: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 6 AND 23 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 10 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 12 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-006-22 A 4 W066-016-20 W066-015-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3 A 4
2 A 1 W066-055-24 W066-153-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING EXISTING WIRE 1368373
REFERENCE: 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01, 737-300/400/500 WDM 33-18-03, 737-300/400/500 WDM 33-18-12.
FIGURE 11: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 6 AND 23 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 102 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 11: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 6 AND 23 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 103 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 12: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 7 AND 8 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 10 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 12 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-24 W066-006-24 A 4 W066-016-24 W066-005-24 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3 A 4
2 A 1 W066-055-24 W066-153-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368386
REFERENCE: 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01, 737-300/400/500 WDM 33-18-03, 737-300/400/500 WDM 33-18-12.
FIGURE 12: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 7 AND 8 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 104 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 12: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 7 AND 8 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 105 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 13: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 5 AND 9 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 10 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 12 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 A 4 W066-016-22
2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3 A 4
2 A 1 W066-055-24 W066-153-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368396
REFERENCE: 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01, 737-300/400/500 WDM 33-18-03, 737-300/400/500 WDM 33-18-12.
FIGURE 13: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 5 AND 9 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 106 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 13: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 5 AND 9 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 107 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 14: WIRE BUNDLE W066 WIRING CHANGE - GROUP 10 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 10 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 12 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-153-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368400
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 14: WIRE BUNDLE W066 WIRING CHANGE - GROUP 10 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 108 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 14: WIRE BUNDLE W066 WIRING CHANGE - GROUP 10 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 109 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 15: WIRE BUNDLE W066 WIRING CHANGE - GROUP 16 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 10 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 12 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-116-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368402
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 15: WIRE BUNDLE W066 WIRING CHANGE - GROUP 16 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 110 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 15: WIRE BUNDLE W066 WIRING CHANGE - GROUP 16 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 111 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 16: WIRE BUNDLE W066 WIRING CHANGE - GROUP 3 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 10 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 12 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-153-22 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368404
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 16: WIRE BUNDLE W066 WIRING CHANGE - GROUP 3 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 112 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 16: WIRE BUNDLE W066 WIRING CHANGE - GROUP 3 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 113 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 17: WIRE BUNDLE W066 WIRING CHANGE - GROUP 18 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 10 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 12 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-190-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368409
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 17: WIRE BUNDLE W066 WIRING CHANGE - GROUP 18 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 114 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 17: WIRE BUNDLE W066 WIRING CHANGE - GROUP 18 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 115 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 18: WIRE BUNDLE W066 WIRING CHANGE - GROUP 19 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 10 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 12 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-903-22 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368424
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 18: WIRE BUNDLE W066 WIRING CHANGE - GROUP 19 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 116 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 18: WIRE BUNDLE W066 WIRING CHANGE - GROUP 19 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 117 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 19: WIRE BUNDLE W066 WIRING CHANGE - GROUP 20 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 10 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 12 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-016-20 W066-025-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-043-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368430
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 19: WIRE BUNDLE W066 WIRING CHANGE - GROUP 20 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 118 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 19: WIRE BUNDLE W066 WIRING CHANGE - GROUP 20 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 119 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 20: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 21 AND 22 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 23 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 24 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-006-22 A 4 W066-016-20 W066-005-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-153-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368431
REFERENCE: 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01, 737-300/400/500 WDM 33-18-03, 737-300/400/500 WDM 33-18-12.
FIGURE 20: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 21 AND 22 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 120 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 20: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 21 AND 22 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 121 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 21: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 2 AND 13 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 23 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 24 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-24 W066-006-24 A 4 W066-016-24 W066-005-24 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-153-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368433
REFERENCE: 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01, 737-300/400/500 WDM 33-18-03, 737-300/400/500 WDM 33-18-12.
FIGURE 21: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 2 AND 13 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 122 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 21: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 2 AND 13 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 123 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 22: WIRE BUNDLE W066 WIRING CHANGE - GROUP 11 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 1 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 2 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 8 L361 LOW OIL PRESSURE ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368439
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 22: WIRE BUNDLE W066 WIRING CHANGE - GROUP 11 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 124 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 22: WIRE BUNDLE W066 WIRING CHANGE - GROUP 11 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 125 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 23: WIRE BUNDLE W066 WIRING CHANGE - GROUP 26 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 1 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 2 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-153-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368441
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 23: WIRE BUNDLE W066 WIRING CHANGE - GROUP 26 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 126 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 23: WIRE BUNDLE W066 WIRING CHANGE - GROUP 26 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 127 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 24: WIRE BUNDLE W066 WIRING CHANGE - GROUP 27 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 1 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 2 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-153-22 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368444
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 24: WIRE BUNDLE W066 WIRING CHANGE - GROUP 27 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 128 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 24: WIRE BUNDLE W066 WIRING CHANGE - GROUP 27 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 129 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 25: WIRE BUNDLE W066 WIRING CHANGE - GROUP 28 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 1 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 2 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-016-20 W066-025-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-043-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368445
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 25: WIRE BUNDLE W066 WIRING CHANGE - GROUP 28 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 130 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 25: WIRE BUNDLE W066 WIRING CHANGE - GROUP 28 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 131 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 26: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 12 AND 29 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 30 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 31 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-006-22 A 4 W066-016-20 W066-005-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-153-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368448
REFERENCE: 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01, 737-300/400/500 WDM 33-18-03, 737-300/400/500 WDM 33-18-12.
FIGURE 26: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 12 AND 29 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 132 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 26: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 12 AND 29 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 133 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 27: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 31 AND 32 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 30 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 31 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-24 W066-006-24 A 4 W066-016-24 W066-005-24 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-153-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368449
REFERENCE: 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01, 737-300/400/500 WDM 33-18-03, 737-300/400/500 WDM 33-18-12.
FIGURE 27: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 31 AND 32 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 134 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 27: WIRE BUNDLE W066 WIRING CHANGE - GROUPS 31 AND 32 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 135 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 28: WIRE BUNDLE W066 WIRING CHANGE - GROUP 33 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 16 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 20 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24
L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368507
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 28: WIRE BUNDLE W066 WIRING CHANGE - GROUP 33 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 136 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 28: WIRE BUNDLE W066 WIRING CHANGE - GROUP 33 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 137 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 29: WIRE BUNDLE W066 WIRING CHANGE - GROUP 34 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 33 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 34 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-036-22 A 4 W066-016-20 W066-020-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-054-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368509
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 29: WIRE BUNDLE W066 WIRING CHANGE - GROUP 34 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 138 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 29: WIRE BUNDLE W066 WIRING CHANGE - GROUP 34 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 139 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 30: WIRE BUNDLE W066 WIRING CHANGE - GROUP 35 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 5 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 12 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-006-22 A 4 W066-016-20 W066-005-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-153-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368573
REFERENCE: 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01, 737-300/400/500 WDM 33-18-03, 737-300/400/500 WDM 33-18-12.
FIGURE 30: WIRE BUNDLE W066 WIRING CHANGE - GROUP 35 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 140 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 30: WIRE BUNDLE W066 WIRING CHANGE - GROUP 35 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 141 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 31: WIRE BUNDLE W066 WIRING CHANGE - GROUP 36 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 10 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 31 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-116-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368581
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 31: WIRE BUNDLE W066 WIRING CHANGE - GROUP 36 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 142 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 31: WIRE BUNDLE W066 WIRING CHANGE - GROUP 36 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 143 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 32: WIRE BUNDLE W066 WIRING CHANGE - GROUP 37 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 10 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 31 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-153-24 L821 START VALVE OPEN 8 ENGINE-1 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368583
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-12.
FIGURE 32: WIRE BUNDLE W066 WIRING CHANGE - GROUP 37 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 144 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 32: WIRE BUNDLE W066 WIRING CHANGE - GROUP 37 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 145 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 33: WIRE BUNDLE W066 WIRING CHANGE - GROUP 38 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 28 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 31 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4258P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-153-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368584
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 33: WIRE BUNDLE W066 WIRING CHANGE - GROUP 38 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 146 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 33: WIRE BUNDLE W066 WIRING CHANGE - GROUP 38 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 147 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 34: WIRE BUNDLE W066 WIRING CHANGE - GROUP 39 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 30 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 31 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4260P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368586
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 34: WIRE BUNDLE W066 WIRING CHANGE - GROUP 39 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 148 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 34: WIRE BUNDLE W066 WIRING CHANGE - GROUP 39 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 149 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 35: WIRE BUNDLE W066 WIRING CHANGE - GROUP 40 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 30 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 31 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4260P LIGHT 8 3 W066-031-24 W066-006-24 A 4 W066-016-24 W066-005-24 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-153-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368587
REFERENCE: 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01, 737-300/400/500 WDM 33-18-03, 737-300/400/500 WDM 33-18-12.
FIGURE 35: WIRE BUNDLE W066 WIRING CHANGE - GROUP 40 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 150 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 35: WIRE BUNDLE W066 WIRING CHANGE - GROUP 40 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 151 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 36: WIRE BUNDLE W066 WIRING CHANGE - GROUP 41 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 30 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 31 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4260P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-153-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368588
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 36: WIRE BUNDLE W066 WIRING CHANGE - GROUP 41 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 152 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 36: WIRE BUNDLE W066 WIRING CHANGE - GROUP 41 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 153 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 37: WIRE BUNDLE W066 WIRING CHANGE - GROUP 42 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 30 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 31 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4260P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-190-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368590
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 37: WIRE BUNDLE W066 WIRING CHANGE - GROUP 42 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 154 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 37: WIRE BUNDLE W066 WIRING CHANGE - GROUP 42 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 155 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 38: WIRE BUNDLE W066 WIRING CHANGE - GROUP 30 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 30 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 31 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4260P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-190-22 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368591
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.737-100/200 WDM 80-11-01.
FIGURE 38: WIRE BUNDLE W066 WIRING CHANGE - GROUP 30 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 156 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 38: WIRE BUNDLE W066 WIRING CHANGE - GROUP 30 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 157 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 39: WIRE BUNDLE W066 WIRING CHANGE - GROUP 44 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 12 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 13 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4260P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 8 L361 LOW OIL PRESSURE ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368592
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 39: WIRE BUNDLE W066 WIRING CHANGE - GROUP 44 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 158 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 39: WIRE BUNDLE W066 WIRING CHANGE - GROUP 44 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 159 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 40: WIRE BUNDLE W066 WIRING CHANGE - GROUP 45 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 12 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8032-20 1 13 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4260P LIGHT 8 3 W066-814-24 A 4 W066-813-24
2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3 A 4
2 A 1 W066-055-24 W066-153-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368596
REFERENCE: 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01, 737-300/400/500 WDM 33-18-03, 737-300/400/500 WDM 33-18-12.
FIGURE 40: WIRE BUNDLE W066 WIRING CHANGE - GROUP 45 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 160 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 40: WIRE BUNDLE W066 WIRING CHANGE - GROUP 45 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 161 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 41: WIRE BUNDLE W066 WIRING CHANGE - GROUP 46 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 12 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 13 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4260P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-153-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368650
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 41: WIRE BUNDLE W066 WIRING CHANGE - GROUP 46 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 162 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 41: WIRE BUNDLE W066 WIRING CHANGE - GROUP 46 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 163 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 42: WIRE BUNDLE W066 WIRING CHANGE - GROUP 47 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 12 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 13 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4260P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-116-24 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368659
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03,
FIGURE 42: WIRE BUNDLE W066 WIRING CHANGE - GROUP 47 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 164 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 42: WIRE BUNDLE W066 WIRING CHANGE - GROUP 47 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 165 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 43: WIRE BUNDLE W066 WIRING CHANGE - GROUP 48 AIRPLANES
7 3 W066-8034-22 2 R 4 W066-8035-22 2 4 5 2 R W066-8032-20 1 12 1 W066-8039-24 3 6 L1304 CABIN ALTITUDE LIGHT 7 3 W002 W066-8036-22 2 R 4 W066-8037-22 2
2 4 R W066-8033-20 1 13 1 W066-8038-24 3 L1316 TAKEOFF WARNING J D4260P LIGHT 8 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-153-22 L361 LOW OIL PRESSURE 8 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368660
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 43: WIRE BUNDLE W066 WIRING CHANGE - GROUP 48 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 166 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 4 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, Class 2 Identify as shown. Cut to the 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74887-10101 1 Imprinted "D04258J". Refer to SWPM 20-10-11 as an accepted procedure. 6 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 7 Terminal Lug BACT12AC48 7 (a) 8 Terminal Lug BACT12AC48 or 3(a) (b) BACT12AC52 (a) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (b) Install the terminal lug with the best fit.
FIGURE 43: WIRE BUNDLE W066 WIRING CHANGE - GROUP 48 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 167 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 44: WIRE BUNDLE W066 WIRING CHANGE - GROUP 49 AIRPLANES
9 3 W066-8034-22 2 R 4 W066-8035-22 2 5 7 2 R W066-8032-20 1 4 SP4016 1 W066-8039-24 3 8 L1304 CABIN ALTITUDE LIGHT 9 3 W002 W066-8036-22 2 R 4 W066-8037-22 2 6 7 2 R W066-8033-20 1 4 SP4018 1 W066-8038-24 3 L1316 TAKEOFF WARNING LIGHT 10 3 W066-031-22 W066-032-22 A 4 W066-015-20 W066-016-20 2 A 1
L360 LOW OIL PRESSURE ENGINE-1 LIGHT
3
A 4
2 A 1 W066-055-24 W066-153-24 L361 LOW OIL PRESSURE 10 ENGINE-2 LIGHT
P2-2 PANEL
ADDED WIRE OR NEW ROUTING
EXISTING WIRE 1368663
REFERENCE: 737-100/200 WDM 21-33-01, 737-100/200 WDM 27-43-01,737-100/200 WDM 33-18-03, 737-100/200 WDM 33-18-12.
FIGURE 44: WIRE BUNDLE W066 WIRING CHANGE - GROUP 49 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 168 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 2 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 4 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Wire BMS 13-48, Type 10, 2 Identify as shown. Cut to the Class 1, AWG 24 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 4 Sleeve 61-74488-2003 - Refer to SWPM 20-10-18 as an accepted procedure. (a) 5 Splice Identification 61-74487-10103 1 Imprinted "SP4016". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. 6 Splice Identification 61-74487-10104 1 Imprinted "SP4018". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. 7 Splice Sleeve D-436-58 1 8 Terminal Lug BACT12AC44 1 Refer to SWPM 20-30-11 as an accepted procedure. 9 Terminal Lug BACT12AC48 7 (b) 10 Terminal Lug BACT12AC48 or 3(b) (c) BACT12AC52 (a) Cut to the necessary length. Install sleeve up to splices but do not cover splices. This sleeve is found in kit 61-74488-1. (b) Terminate with existing wire. Refer to SWPM 20-30-11 as an accepted procedure. (c) Install the terminal lug with the best fit.
FIGURE 44: WIRE BUNDLE W066 WIRING CHANGE - GROUP 49 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 169 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 45: WIRE BUNDLE W002 WIRE ROUTING - GROUPS 1-29, 31, 38 AND 43 AIRPLANES
W002
D4006P
D4258P
P2-2
PANEL
DISC STA 178
FWD 1368796
FIGURE 45: WIRE BUNDLE W002 WIRE ROUTING - GROUPS 1-29, 31, 38 AND 43 AIRPLANES January 11, 2010 (SHEET 1 OF 1) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 170 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 46: WIRE BUNDLE W002 WIRE ROUTING - GROUPS 30, 39-42 AND 44-48 AIRPLANES
W002
D4006P
D4260P
P2-2
PANEL
DISC STA 178
FWD 1369317
FIGURE 46: WIRE BUNDLE W002 WIRE ROUTING - GROUPS 30, 39-42 AND 44-48 AIRPLANES January 11, 2010 (SHEET 1 OF 1) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 171 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 47: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 1, 3, 5-10, 15-20, 23 AND 25 AIRPLANES
4 5 3 6 9 10 W002-8051-20 1 49 W066 W246 12 W002-8052-22 2 50 7 8 7 8 J D4258P P D4006J P2-2 PANEL
P2 CENTER INSTRUMENT PANEL
ADDED WIRE OR NEW ROUTING 1368670
REFERENCE: 737-100/200 WDM 21-33-01,737-100/200 WDM 27-43-01, 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01.
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Sleeve 61-74488-2003 1 Refer to SWPM 20-10-18 as an accepted procedure. 4 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74888-10101 1 Imprinted "D04258P". Refer to SWPM 20-10-11 as an accepted procedure. 6 Identification Tape 61-74888-10103 1 Imprinted "D04006P". Refer to SWPM 20-10-11 as an accepted procedure. 7 Adhesive Tape, 61-74488-2005 - Refer to SWPM 20-60-09 as an accepted 0.5 inch procedure. (a)
FIGURE 47: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 1, 3, 5-10, 15-20, 23 AND 25 AIR- PLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 172 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 8 Thread Lock 61-74488-2004 - Install as required. Refer to SWPM 20-60-09 Compound as an accepted procedure. (b) 9 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. (a) Wrap wires with tape at connector if backshell is existing (b) Apply thread lock compound to backshell threads if backshell is existing.
FIGURE 47: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 1, 3, 5-10, 15-20, 23 AND 25 AIR- PLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 173 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 48: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 2, 13 AND 21-22 AIRPLANES
4 5 3 6 9 23 W002-8051-20 1 49 W066 W246 24 W002-8052-22 2 50 7 8 7 8 J D4258P P D4006J P2-2 PANEL
P2 CENTER INSTRUMENT PANEL
ADDED WIRE OR NEW ROUTING 1368673
REFERENCE: 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01.
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Sleeve 61-74488-2003 1 Refer to SWPM 20-10-18 as an accepted procedure. 4 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74888-10101 1 Imprinted "D04258P". Refer to SWPM 20-10-11 as an accepted procedure. 6 Identification Tape 61-74888-10103 1 Imprinted "D04006P". Refer to SWPM 20-10-11 as an accepted procedure. 7 Adhesive Tape, 61-74488-2005 - Refer to SWPM 20-60-09 as an accepted 0.5 inch procedure. (a)
FIGURE 48: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 2, 13 AND 21-22 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 174 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 8 Thread Lock 61-74488-2004 - Install as required. Refer to SWPM 20-60-09 Compound as an accepted procedure. (b) 9 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. (a) Wrap wires with tape at connector if backshell is existing (b) Apply thread lock compound to backshell threads if backshell is existing.
FIGURE 48: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 2, 13 AND 21-22 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 175 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 49: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 11 AND 26-28 AIRPLANES
4 5 3 6 9 1 W002-8051-20 1 49 W066 W246 2 W002-8052-22 2 50 7 8 7 8 J D4258P P D4006J P2-2 PANEL
P2 CENTER INSTRUMENT PANEL
ADDED WIRE OR NEW ROUTING 1368674
REFERENCE: 737-100/200 WDM 21-33-01,737-100/200 WDM 27-43-01,
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Sleeve 61-74488-2003 1 Refer to SWPM 20-10-18 as an accepted procedure. 4 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74888-10101 1 Imprinted "D04258P". Refer to SWPM 20-10-11 as an accepted procedure. 6 Identification Tape 61-74888-10103 1 Imprinted "D04006P". Refer to SWPM 20-10-11 as an accepted procedure. 7 Adhesive Tape, 61-74488-2005 - Refer to SWPM 20-60-09 as an accepted 0.5 inch procedure. (a)
FIGURE 49: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 11 AND 26-28 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 176 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 8 Thread Lock 61-74488-2004 - Install as required. Refer to SWPM 20-60-09 Compound as an accepted procedure. (b) 9 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. (a) Wrap wires with tape at connector if backshell is existing (b) Apply thread lock compound to backshell threads if backshell is existing.
FIGURE 49: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 11 AND 26-28 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 177 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 50: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 12, 29, 31 AND 32 AIRPLANES
4 5 3 6 9 30 W002-8051-20 1 49 W066 W246 31 W002-8052-22 2 50 7 8 7 8 J D4258P P D4006J P2-2 PANEL
P2 CENTER INSTRUMENT PANEL
ADDED WIRE OR NEW ROUTING 1368675
REFERENCE: 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01.
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Sleeve 61-74488-2003 1 Refer to SWPM 20-10-18 as an accepted procedure. 4 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74888-10101 1 Imprinted "D04258P". Refer to SWPM 20-10-11 as an accepted procedure. 6 Identification Tape 61-74888-10103 1 Imprinted "D04006P". Refer to SWPM 20-10-11 as an accepted procedure. 7 Adhesive Tape, 61-74488-2005 - Refer to SWPM 20-60-09 as an accepted 0.5 inch procedure. (a)
FIGURE 50: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 12, 29, 31 AND 32 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 178 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 8 Thread Lock 61-74488-2004 - Install as required. Refer to SWPM 20-60-09 Compound as an accepted procedure. (b) 9 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. (a) Wrap wires with tape at connector if backshell is existing (b) Apply thread lock compound to backshell threads if backshell is existing.
FIGURE 50: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 12, 29, 31 AND 32 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 179 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 51: WIRE BUNDLE W002 WIRING CHANGE - GROUP 33 AIRPLANES
4 5 3 6 9 16 W002-8051-20 1 49 W066 W246 20 W002-8052-22 2 50 7 8 7 8 J D4258P P D4006J P2-2 PANEL
P2 CENTER INSTRUMENT PANEL
ADDED WIRE OR NEW ROUTING 1368676
REFERENCE: 737-100/200 WDM 21-33-01,737-100/200 WDM 27-43-01,
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Sleeve 61-74488-2003 1 Refer to SWPM 20-10-18 as an accepted procedure. 4 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74888-10101 1 Imprinted "D04258P". Refer to SWPM 20-10-11 as an accepted procedure. 6 Identification Tape 61-74888-10103 1 Imprinted "D04006P". Refer to SWPM 20-10-11 as an accepted procedure. 7 Adhesive Tape, 61-74488-2005 - Refer to SWPM 20-60-09 as an accepted 0.5 inch procedure. (a)
FIGURE 51: WIRE BUNDLE W002 WIRING CHANGE - GROUP 33 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 180 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 8 Thread Lock 61-74488-2004 - Install as required. Refer to SWPM 20-60-09 Compound as an accepted procedure. (b) 9 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. (a) Wrap wires with tape at connector if backshell is existing (b) Apply thread lock compound to backshell threads if backshell is existing.
FIGURE 51: WIRE BUNDLE W002 WIRING CHANGE - GROUP 33 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 181 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 52: WIRE BUNDLE W002 WIRING CHANGE - GROUP 34 AIRPLANES
4 5 3 6 9 33 W002-8051-20 1 49 W066 W246 34 W002-8052-22 2 50 7 8 7 8 J D4258P P D4006J P2-2 PANEL
P2 CENTER INSTRUMENT PANEL
ADDED WIRE OR NEW ROUTING 1368677
REFERENCE: 737-100/200 WDM 21-33-01,737-100/200 WDM 27-43-01,
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Sleeve 61-74488-2003 1 Refer to SWPM 20-10-18 as an accepted procedure. 4 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74888-10101 1 Imprinted "D04258P". Refer to SWPM 20-10-11 as an accepted procedure. 6 Identification Tape 61-74888-10103 1 Imprinted "D04006P". Refer to SWPM 20-10-11 as an accepted procedure. 7 Adhesive Tape, 61-74488-2005 - Refer to SWPM 20-60-09 as an accepted 0.5 inch procedure. (a)
FIGURE 52: WIRE BUNDLE W002 WIRING CHANGE - GROUP 34 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 182 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 8 Thread Lock 61-74488-2004 - Install as required. Refer to SWPM 20-60-09 Compound as an accepted procedure. (b) 9 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. (a) Wrap wires with tape at connector if backshell is existing (b) Apply thread lock compound to backshell threads if backshell is existing.
FIGURE 52: WIRE BUNDLE W002 WIRING CHANGE - GROUP 34 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 183 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 53: WIRE BUNDLE W002 WIRING CHANGE - GROUP 35 AIRPLANES
4 5 3 6 9 5 W002-8051-20 1 49 W066 W246 12 W002-8052-22 2 50 7 8 7 8 J D4258P P D4006J P2-2 PANEL
P2 CENTER INSTRUMENT PANEL
ADDED WIRE OR NEW ROUTING 1368679
REFERENCE: 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01.
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Sleeve 61-74488-2003 1 Refer to SWPM 20-10-18 as an accepted procedure. 4 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74888-10101 1 Imprinted "D04258P". Refer to SWPM 20-10-11 as an accepted procedure. 6 Identification Tape 61-74888-10103 1 Imprinted "D04006P". Refer to SWPM 20-10-11 as an accepted procedure. 7 Adhesive Tape, 61-74488-2005 - Refer to SWPM 20-60-09 as an accepted 0.5 inch procedure. (a)
FIGURE 53: WIRE BUNDLE W002 WIRING CHANGE - GROUP 35 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 184 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 8 Thread Lock 61-74488-2004 - Install as required. Refer to SWPM 20-60-09 Compound as an accepted procedure. (b) 9 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. (a) Wrap wires with tape at connector if backshell is existing (b) Apply thread lock compound to backshell threads if backshell is existing.
FIGURE 53: WIRE BUNDLE W002 WIRING CHANGE - GROUP 35 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 185 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 54: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 36 AND 37 AIRPLANES
4 5 3 6 9 10 W002-8051-20 1 49 W066 W246 31 W002-8052-22 1 50 7 8 7 8 J D4258P P D4006J P2-2 PANEL
P2 CENTER INSTRUMENT PANEL
ADDED WIRE OR NEW ROUTING 1368680
REFERENCE: 737-100/200 WDM 21-33-01,737-100/200 WDM 27-43-01,
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Sleeve 61-74488-2003 1 Refer to SWPM 20-10-18 as an accepted procedure. 4 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74888-10101 1 Imprinted "D04258P". Refer to SWPM 20-10-11 as an accepted procedure. 6 Identification Tape 61-74888-10103 1 Imprinted "D04006P". Refer to SWPM 20-10-11 as an accepted procedure. 7 Adhesive Tape, 61-74488-2005 - Refer to SWPM 20-60-09 as an accepted 0.5 inch procedure. (a)
FIGURE 54: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 36 AND 37 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 186 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 8 Thread Lock 61-74488-2004 - Install as required. Refer to SWPM 20-60-09 Compound as an accepted procedure. (b) 9 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. (a) Wrap wires with tape at connector if backshell is existing (b) Apply thread lock compound to backshell threads if backshell is existing.
FIGURE 54: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 36 AND 37 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 187 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 55: WIRE BUNDLE W002 WIRING CHANGE - GROUP 38 AIRPLANES
4 5 3 6 9 28 W002-8051-20 1 49 W066 W246 31 W002-8052-22 2 50 7 8 7 8 J D4258P P D4006J P2-2 PANEL
P2 CENTER INSTRUMENT PANEL
ADDED WIRE OR NEW ROUTING 1368681
REFERENCE: 737-100/200 WDM 21-33-01,737-100/200 WDM 27-43-01,
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Sleeve 61-74488-2003 1 Refer to SWPM 20-10-18 as an accepted procedure. 4 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74888-10101 1 Imprinted "D04258P". Refer to SWPM 20-10-11 as an accepted procedure. 6 Identification Tape 61-74888-10103 1 Imprinted "D04006P". Refer to SWPM 20-10-11 as an accepted procedure. 7 Adhesive Tape, 61-74488-2005 - Refer to SWPM 20-60-09 as an accepted 0.5 inch procedure. (a)
FIGURE 55: WIRE BUNDLE W002 WIRING CHANGE - GROUP 38 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 188 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 8 Thread Lock 61-74488-2004 - Install as required. Refer to SWPM 20-60-09 Compound as an accepted procedure. (b) 9 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. (a) Wrap wires with tape at connector if backshell is existing (b) Apply thread lock compound to backshell threads if backshell is existing.
FIGURE 55: WIRE BUNDLE W002 WIRING CHANGE - GROUP 38 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 189 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 56: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 4, 14 AND 43 AIRPLANES
4 5 3 6 9 10 W002-8051-20 1 54 W066 W246 12 W002-8052-22 2 55 7 8 7 8 J D4258P P D4006J P2-2 PANEL
P2 CENTER INSTRUMENT PANEL
ADDED WIRE OR NEW ROUTING 1368682
REFERENCE: 737-100/200 WDM 21-33-01,737-100/200 WDM 27-43-01,
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Sleeve 61-74488-2003 1 Refer to SWPM 20-10-18 as an accepted procedure. 4 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74888-10101 1 Imprinted "D04258P". Refer to SWPM 20-10-11 as an accepted procedure. 6 Identification Tape 61-74888-10103 1 Imprinted "D04006P". Refer to SWPM 20-10-11 as an accepted procedure. 7 Adhesive Tape, 61-74488-2005 - Refer to SWPM 20-60-09 as an accepted 0.5 inch procedure. (a)
FIGURE 56: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 4, 14 AND 43 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 190 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 8 Thread Lock 61-74488-2004 - Install as required. Refer to SWPM 20-60-09 Compound as an accepted procedure. (b) 9 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. (a) Wrap wires with tape at connector if backshell is existing (b) Apply thread lock compound to backshell threads if backshell is existing.
FIGURE 56: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 4, 14 AND 43 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 191 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 57: WIRE BUNDLE W002 WIRING CHANGE - GROUP 24 AIRPLANES
4 5 3 6 9 10 W002-8051-20 1 46 W066 W246 12 W002-8052-22 2 47 7 8 7 8 J D4258P P D4006J P2-2 PANEL
P2 CENTER INSTRUMENT PANEL
ADDED WIRE OR NEW ROUTING 1368683
REFERENCE: 737-100/200 WDM 21-33-01,737-100/200 WDM 27-43-01,
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Sleeve 61-74488-2003 1 Refer to SWPM 20-10-18 as an accepted procedure. 4 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74888-10101 1 Imprinted "D04258P". Refer to SWPM 20-10-11 as an accepted procedure. 6 Identification Tape 61-74888-10103 1 Imprinted "D04006P". Refer to SWPM 20-10-11 as an accepted procedure. 7 Adhesive Tape, 61-74488-2005 - Refer to SWPM 20-60-09 as an accepted 0.5 inch procedure. (a)
FIGURE 57: WIRE BUNDLE W002 WIRING CHANGE - GROUP 24 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 192 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 8 Thread Lock 61-74488-2004 - Install as required. Refer to SWPM 20-60-09 Compound as an accepted procedure. (b) 9 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. (a) Wrap wires with tape at connector if backshell is existing (b) Apply thread lock compound to backshell threads if backshell is existing.
FIGURE 57: WIRE BUNDLE W002 WIRING CHANGE - GROUP 24 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 193 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 58: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 30 AND 39-42 AIRPLANES
4 5 3 6 9 30 W002-8051-20 1 49 W066 W246 31 W002-8052-22 2 50 7 8 7 8 J D4260P P D4006J P2-2 PANEL
P2 CENTER INSTRUMENT PANEL
ADDED WIRE OR NEW ROUTING 1368685
REFERENCE: 737-100/200 WDM 21-33-01,737-100/200 WDM 27-43-01, 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01.
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Sleeve 61-74488-2003 1 Refer to SWPM 20-10-18 as an accepted procedure. 4 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74888-10101 1 Imprinted "D04258P". Refer to SWPM 20-10-11 as an accepted procedure. 6 Identification Tape 61-74888-10103 1 Imprinted "D04006P". Refer to SWPM 20-10-11 as an accepted procedure. 7 Adhesive Tape, 61-74488-2005 - Refer to SWPM 20-60-09 as an accepted 0.5 inch procedure. (a)
FIGURE 58: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 30 AND 39-42 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 194 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 8 Thread Lock 61-74488-2004 - Install as required. Refer to SWPM 20-60-09 Compound as an accepted procedure. (b) 9 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. (a) Wrap wires with tape at connector if backshell is existing (b) Apply thread lock compound to backshell threads if backshell is existing.
FIGURE 58: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 30 AND 39-42 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 195 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 59: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 44, 45, 46, 47 AND 48 AIRPLANES
4 5 3 6 9 12 W002-8051-20 1 49 W066 W246 13 W002-8052-22 2 50 7 8 7 8 J D4260P P D4006J P2-2 PANEL
P2 CENTER INSTRUMENT PANEL
ADDED WIRE OR NEW ROUTING 1368686
REFERENCE: 737-100/200 WDM 21-33-01,737-100/200 WDM 27-43-01, 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01.
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Sleeve 61-74488-2003 1 Refer to SWPM 20-10-18 as an accepted procedure. 4 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74888-10101 1 Imprinted "D04258P". Refer to SWPM 20-10-11 as an accepted procedure. 6 Identification Tape 61-74888-10103 1 Imprinted "D04006P". Refer to SWPM 20-10-11 as an accepted procedure. 7 Adhesive Tape, 61-74488-2005 - Refer to SWPM 20-60-09 as an accepted 0.5 inch procedure. (a)
FIGURE 59: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 44, 45, 46, 47 AND 48 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 196 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 8 Thread Lock 61-74488-2004 - Install as required. Refer to SWPM 20-60-09 Compound as an accepted procedure. (b) 9 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. (a) Wrap wires with tape at connector if backshell is existing (b) Apply thread lock compound to backshell threads if backshell is existing.
FIGURE 59: WIRE BUNDLE W002 WIRING CHANGE - GROUPS 44, 45, 46, 47 AND 48 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 197 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 60: WIRE BUNDLE W002 WIRING CHANGE - GROUP 49 AIRPLANES
3 4 5 SP4016 W002-8051-20 1 49 W066 W246 SP4018 W002-8052-22 2 50 6 7 P D4006J P2-2 PANEL
P2 CENTER INSTRUMENT PANEL
ADDED WIRE OR NEW ROUTING 1368689
REFERENCE: 737-100/200 WDM 21-33-01,737-100/200 WDM 27-43-01,
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, Class 1 Identify as shown. Cut to the 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, Class 1 Identify as shown. Cut to the 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Sleeve 61-74488-2003 1 Refer to SWPM 20-10-18 as an accepted procedure. (a) 4 Pin Contact BACC47CN1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 5 Identification Tape 61-74888-10103 1 Imprint with "D04006P". Refer to SWPM 20-10-11 as an accepted procedure. 7 Adhesive Tape, 61-74488-2005 - Refer to SWPM 20-60-09 as an 0.5 inch accepted procedure. (b) 8 Thread Lock 61-74488-2004 - Refer to SWPM 20-60-09 as an Compound accepted procedure. (c)
FIGURE 60: WIRE BUNDLE W002 WIRING CHANGE - GROUP 49 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 198 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA (a) Install sleeve up to splices but do not cover splices. (b) Wrap wires with tape at connector if backshell is existing (c) Apply thread lock compound for threads if backshell is existing.
FIGURE 60: WIRE BUNDLE W002 WIRING CHANGE - GROUP 49 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 199 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 61: WIRE BUNDLE W246 WIRE ROUTING
D4006J POSITION 10 P2-2 PANEL
W246
M315
DISC STA D940 178 SPLICE AREA A SM3 AND SM23
FWD 1373380
FIGURE 61: WIRE BUNDLE W246 WIRE ROUTING January 11, 2010 (SHEET 1 OF 3) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 200 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
STA A 188 W246
AP0600B D4094P/W246 POSITION 21
B FWD
STA STA INBD 259.5 277 W246 TO D4212J POSITION 4 B STA 277
C
FWD
INBD 1373914
FIGURE 61: WIRE BUNDLE W246 WIRE ROUTING January 11, 2010 (SHEET 2 OF 3) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 201 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
STA 192 D776 BL 0 AT WL 207.5
SPLICE AREA SM21
W246
C FWD 1375041
FIGURE 61: WIRE BUNDLE W246 WIRE ROUTING January 11, 2010 (SHEET 3 OF 3) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 202 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 62: WIRE BUNDLE W246 WIRING CHANGE - GROUPS 1, 3, 5, 8, 10, 11, 13, 15-21, 23, 26-31, 33- 34, 36-39, 41-42, 44 AND 46-49 AIRPLANES
DISC STA 268
3 4 5 6 12 W246-033-20 A W246-170-20 1 P D4212J D776 S128 CABIN PRES SW STA 192, WL 207, BL 0
10 11 13 SM21 W246-171-20 1 49
W002 8 9 10 12 W246-B-B W246-B-R SM23 W246-172-22 2 50 BLU M2592 RED 13 14 DISC D4006J P STA 268
11 W246-074-22
P D4212J DISC STA 254R
3 W246-049-22 SM3 W246-072-22 29 W044
7 15 D940 D4094P J M315 AURAL WARNING UNIT STA 195
ADDED WIRE OR NEW ROUTING DELETED WIRE OR FORMER ROUTING EXISTING WIRE 1368794
REFERENCE: 737-100/200 WDM 21-33-01,737-100/200 WDM 27-43-01, 737-300/400/500 WDM 21-33-01, 737-300/400/500 WDM 27-43-01.
FIGURE 62: WIRE BUNDLE W246 WIRING CHANGE - GROUPS 1, 3, 5, 8, 10, 11, 13, 15-21, 23, 26-31, 33-34, 36-39, 41-42, 44 AND 46-49 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 203 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 2 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Socket Contact BACC47DR1 1 Refer to SWPM 20-61-19 as an accepted procedure. 4 Identification Tape 61-74888-10202 1 Imprinted "D00776". Refer to SWPM 20-10-11 as an accepted procedure. 5 Adhesive Tape, 1.0 61-74488-2006 - Refer to SWPM 20-60-09 as an Inch accepted procedure. (a) 6 Thread Lock 61-74488-2004 - Refer to SWPM 20-60-09 as an Compound accepted procedure. (b) 7 Splice D-436-37 1 Refer to SWPM 20-30-12 as an accepted procedure. 8 Diode Assembly 69-58806-4 1 Refer to SWPM 20-30-12 as an accepted procedure.
9 Diode Identification 61-74488-10212 1 Imprinted "M2592". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. 10 Splice D-436-37 or D-436-38 2 Refer to SWPM 20-30-12 as an accepted procedure. (c) 11 Splice Identification 61-74488-10205 1 Imprinted "SM21". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. 12 Splice Identification 61-74488-10207 1 Imprinted "SM23". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. 13 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 14 Identification Tape 61-74888-10201 1 Imprinted "D04006J M/W STA 178". Refer to SWPM 20-10-11 as an accepted procedure. 15 Splice Identification 61-74488-10203 1 Imprinted "SM3". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. (a) Apply thread lock compound to backshell threads if backshell is existing. (b) Wrap wires with tape at connector if backshell is existing (c) Install the smallest splice that will fit.
FIGURE 62: WIRE BUNDLE W246 WIRING CHANGE - GROUPS 1, 3, 5, 8, 10, 11, 13, 15-21, 23, 26-31, 33-34, 36-39, 41-42, 44 AND 46-49 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 204 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 63: WIRE BUNDLE W246 WIRING CHANGE - GROUPS 2, 6, 7, 9, 12, 22, 25, 32, 35, 40 AND 45 AIRPLANES
DISC STA 268
3 4 5 6 12 W246-033-20 A W246-170-20 1 P D4212J D776 S128 CABIN PRES SW STA 192, WL 207, BL 0
10 11 13 SM21 W246-171-20 1 49
W002 8 9 10 12 W246-B-B W246-B-R SM23 W246-172-22 2 50 BLU M2592 RED 13 14 DISC D4006J P STA 268
11 W246-074-22
P D4212J DISC STA 254R
3 W246-049-22 SM3 W246-072-24 29 W044
7 15 D940 D4094P J M315 AURAL WARNING UNIT STA 195
ADDED WIRE OR NEW ROUTING DELETED WIRE OR FORMER ROUTING EXISTING WIRE 1368795
REFERENCE: 737-100/200 WDM 21-33-01,737-100/200 WDM 27-43-01,
FIGURE 63: WIRE BUNDLE W246 WIRING CHANGE - GROUPS 2, 6, 7, 9, 12, 22, 25, 32, 35, 40 AND 45 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 205 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 2 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Socket Contact BACC47DR1 1 Refer to SWPM 20-61-19 as an accepted procedure. 4 Identification Tape 61-74888-10202 1 Imprinted "D00776". Refer to SWPM 20-10-11 as an accepted procedure. 5 Adhesive Tape, 1.0 61-74488-2006 - Refer to SWPM 20-60-09 as an Inch accepted procedure. (a) 6 Thread Lock 61-74488-2004 - Refer to SWPM 20-60-09 as an Compound accepted procedure. (b) 7 Splice D-436-37 1 Refer to SWPM 20-30-12 as an accepted procedure. 8 Diode Assembly 69-58806-4 1 Refer to SWPM 20-30-12 as an accepted procedure.
9 Diode Identification 61-74488-10212 1 Imprinted "M2592". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. 10 Splice D-436-37 or D-436-38 2 Refer to SWPM 20-30-12 as an accepted procedure. (c) 11 Splice Identification 61-74488-10205 1 Imprinted "SM21". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. 12 Splice Identification 61-74488-10207 1 Imprinted "SM23". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. 13 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 14 Identification Tape 61-74888-10201 1 Imprinted "D04006J M/W STA 178". Refer to SWPM 20-10-11 as an accepted procedure. 15 Splice Identification 61-74488-10203 1 Imprinted "SM3". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. (a) Apply thread lock compound to backshell threads if backshell is existing. (b) Wrap wires with tape at connector if backshell is existing (c) Install the smallest splice that will fit.
FIGURE 63: WIRE BUNDLE W246 WIRING CHANGE - GROUPS 2, 6, 7, 9, 12, 22, 25, 32, 35, 40 AND 45 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 206 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 64: WIRE BUNDLE W246 WIRING CHANGE - GROUPS 4 AND 14 AIRPLANES
DISC STA 268
3 4 5 6 12 W246-033-20 A W246-170-20 1 P D4212J D776 S128 CABIN PRES SW STA 192, WL 207, BL 0
10 11 13 SM21 W246-171-20 1 54
W002 8 9 10 12 W246-B-B W246-B-R SM23 W246-172-22 2 55 BLU M2592 RED 13 14 DISC D4006J P STA 268
11 W246-074-22
P D4212J DISC STA 254R
3 W246-049-22 SM3 W246-072-22 29 W044
7 15 D940 D4094P J M315 AURAL WARNING UNIT STA 195
ADDED WIRE OR NEW ROUTING DELETED WIRE OR FORMER ROUTING EXISTING WIRE 1368806
REFERENCE: 737-100/200 WDM 21-33-01,737-100/200 WDM 27-43-01,
FIGURE 64: WIRE BUNDLE W246 WIRING CHANGE - GROUPS 4 AND 14 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 207 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 2 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Socket Contact BACC47DR1 1 Refer to SWPM 20-61-19 as an accepted procedure. 4 Identification Tape 61-74888-10202 1 Imprinted "D00776". Refer to SWPM 20-10-11 as an accepted procedure. 5 Adhesive Tape, 1.0 61-74488-2006 - Refer to SWPM 20-60-09 as an Inch accepted procedure. (a) 6 Thread Lock 61-74488-2004 - Refer to SWPM 20-60-09 as an Compound accepted procedure. (b) 7 Splice D-436-37 1 Refer to SWPM 20-30-12 as an accepted procedure. 8 Diode Assembly 69-58806-4 1 Refer to SWPM 20-30-12 as an accepted procedure.
9 Diode Identification 61-74488-10212 1 Imprinted "M2592". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. 10 Splice D-436-37 or D-436-38 2 Refer to SWPM 20-30-12 as an accepted procedure. (c) 11 Splice Identification 61-74488-10205 1 Imprinted "SM21". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. 12 Splice Identification 61-74488-10207 1 Imprinted "SM23". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. 13 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 14 Identification Tape 61-74888-10201 1 Imprinted "D04006J M/W STA 178". Refer to SWPM 20-10-11 as an accepted procedure. 15 Splice Identification 61-74488-10203 1 Imprinted "SM3". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. (a) Apply thread lock compound to backshell threads if backshell is existing. (b) Wrap wires with tape at connector if backshell is existing (c) Install the smallest splice that will fit.
FIGURE 64: WIRE BUNDLE W246 WIRING CHANGE - GROUPS 4 AND 14 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 208 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 65: WIRE BUNDLE W246 WIRING CHANGE - GROUP 24 AIRPLANES
DISC STA 268
3 4 5 6 12 W246-033-20 A W246-170-20 1 P D4212J D776 S128 CABIN PRES SW STA 192, WL 207, BL 0
10 11 13 SM21 W246-171-20 1 46
W002 8 9 10 12 W246-B-B W246-B-R SM23 W246-172-22 2 47 BLU M2592 RED 13 14 DISC D4006J P STA 268
11 W246-074-22
P D4212J DISC STA 254R
3 W246-049-22 SM3 W246-072-22 29 W044
7 15 D940 D4094P J M315 AURAL WARNING UNIT STA 195
ADDED WIRE OR NEW ROUTING DELETED WIRE OR FORMER ROUTING EXISTING WIRE 1368811
REFERENCE: 737-100/200 WDM 21-33-01,737-100/200 WDM 27-43-01,
FIGURE 65: WIRE BUNDLE W246 WIRING CHANGE - GROUP 24 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 209 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 2 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Socket Contact BACC47DR1 1 Refer to SWPM 20-61-19 as an accepted procedure. 4 Identification Tape 61-74888-10202 1 Imprinted "D00776". Refer to SWPM 20-10-11 as an accepted procedure. 5 Adhesive Tape, 1.0 61-74488-2006 - Refer to SWPM 20-60-09 as an Inch accepted procedure. (a) 6 Thread Lock 61-74488-2004 - Refer to SWPM 20-60-09 as an Compound accepted procedure. (b) 7 Splice D-436-37 1 Refer to SWPM 20-30-12 as an accepted procedure. 8 Diode Assembly 69-58806-4 1 Refer to SWPM 20-30-12 as an accepted procedure.
9 Diode Identification 61-74488-10212 1 Imprinted "M2592". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. 10 Splice D-436-37 or D-436-38 2 Refer to SWPM 20-30-12 as an accepted procedure. (c) 11 Splice Identification 61-74488-10205 1 Imprinted "SM21". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. 12 Splice Identification 61-74488-10207 1 Imprinted "SM23". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. 13 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 14 Identification Tape 61-74888-10201 1 Imprinted "D04006J M/W STA 178". Refer to SWPM 20-10-11 as an accepted procedure. 15 Splice Identification 61-74488-10203 1 Imprinted "SM3". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. (a) Apply thread lock compound to backshell threads if backshell is existing. (b) Wrap wires with tape at connector if backshell is existing (c) Install the smallest splice that will fit.
FIGURE 65: WIRE BUNDLE W246 WIRING CHANGE - GROUP 24 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 210 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 66: WIRE BUNDLE W246 WIRING CHANGE - GROUP 43 AIRPLANES
DISC STA 268
3 4 5 6 12 W246-033-20 A W246-170-20 1 P D4212J D776 S128 CABIN PRES SW STA 192, WL 207, BL 0
10 11 13 SM21 W246-171-20 1 54
W002 8 9 10 12 W246-B-B W246-B-R SM23 W246-172-22 2 55 BLU M2592 RED 13 14 DISC D4006J P STA 268
11 W246-074-22
P D4212J DISC STA 254R
3 W246-049-22 SP2218 W246-072-22 29 W044
7 15 D940 D4094P J M315 AURAL WARNING UNIT STA 195
ADDED WIRE OR NEW ROUTING DELETED WIRE OR FORMER ROUTING EXISTING WIRE 1368812
REFERENCE: 737-100/200 WDM 21-33-01,737-100/200 WDM 27-43-01,
FIGURE 66: WIRE BUNDLE W246 WIRING CHANGE - GROUP 43 AIRPLANES Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 211 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
The flag note numbers shown below agree with the numbers shown in the flag symbols in the figure.
FLAG NOTE NAME IDENTIFICATION QTY MORE DATA 1 Wire BMS 13-48, Type 10, 2 Identify as shown. Cut to the Class 1, AWG 20 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 2 Wire BMS 13-48, Type 10, 1 Identify as shown. Cut to the Class 1, AWG 22 necessary length. Lacing Tape 61-74488-2001 - Install as required. Refer to SWPM 20-10-11 as an accepted procedure. 3 Socket Contact BACC47DR1 1 Refer to SWPM 20-61-19 as an accepted procedure. 4 Identification Tape 61-74888-10202 1 Imprinted "D00776". Refer to SWPM 20-10-11 as an accepted procedure. 5 Adhesive Tape, 1.0 61-74488-2006 - Refer to SWPM 20-60-09 as an Inch accepted procedure. (a) 6 Thread Lock 61-74488-2004 - Refer to SWPM 20-60-09 as an Compound accepted procedure. (b) 7 Splice D-436-37 1 Refer to SWPM 20-30-12 as an accepted procedure. 8 Diode Assembly 69-58806-4 1 Refer to SWPM 20-30-12 as an accepted procedure.
9 Diode Identification 61-74488-10212 1 Imprinted "M2592". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. 10 Splice D-436-37 or D-436-38 2 Refer to SWPM 20-30-12 as an accepted procedure. (c) 11 Splice Identification 61-74488-10205 1 Imprinted "SM21". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. 12 Splice Identification 61-74488-10207 1 Imprinted "SM23". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. 13 Socket Contact BACC47CP1S 2 Refer to SWPM 20-61-11 as an accepted procedure. 14 Identification Tape 61-74888-10201 1 Imprinted "D04006J M/W STA 178". Refer to SWPM 20-10-11 as an accepted procedure. 15 Splice Identification 61-74488-10204 1 Imprinted "SM2218". Refer to SWPM Sleeve 20-10-11 as an accepted procedure. (a) Apply thread lock compound to backshell threads if backshell is existing. (b) Wrap wires with tape at connector if backshell is existing (c) Install the smallest splice that will fit.
FIGURE 66: WIRE BUNDLE W246 WIRING CHANGE - GROUP 43 AIRPLANES Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 212 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
FIGURE 67: P2-2 CENTER INSTRUMENT PANEL INSTALLATION
FLIGHT COMPARTMENT 1 1
P2-2 CENTER INSTRUMENT PANEL P2-2 CENTER INSTRUMENT PANEL EIS CONFIGURATION NON-EIS CONFIGURATION 1368169
FIGURE 67: P2-2 CENTER INSTRUMENT PANEL INSTALLATION Original Issue: January 11, 2010 (SHEET 1 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 213 of 214 BOEING SERVICE BULLETIN 737-31A1325 ALERT ALERT
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.
STEP TASK NAME IDENTIFICATION QTY MORE DATA Install P2-2 Panel 69-37305-( ) 1 Refer to OHM 31-10-01 as 1 an accepted procedure.
FIGURE 67: P2-2 CENTER INSTRUMENT PANEL INSTALLATION Original Issue: January 11, 2010 (SHEET 2 OF 2) 737-31A1325 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 214 of 214