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Commercial Airplanes 737 Service Bulletin
SPECIAL ATTENTION Number: 737-30-1058 Original Issue: July 27, 2006 Revision 3: July 07, 2010 ATA System: 3041 SUBJECT: ICE AND RAIN PROTECTION - Control Cabin Window Anti-Icing System - Coil Cord Assembly Replacement on the Number 2 Windows in the Flight Compartment Export of this technology is controlled under the United States Export Administration Regulations (EAR) (15 CFR 730-774). An export license may be required before it is used for development, production or use by foreign persons from specific countries. The controller of this data has the individual responsibility to abide by all export laws.
9E991ECCN:
BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET Copyright © 2006 The Boeing Company Unpublished Work - All Rights Reserved Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable subject matter. Boeing also claims copyright in this document as a compilation and/or collective work.
This document includes proprietary information owned by The Boeing Company and/or one or more third parties.
Treatment of the document and the information it contains is governed by contract with Boeing. For more information, contact The Boeing Company, P.O. Box 3707, Seattle, Washington 98124.
Boeing, the Boeing signature, the Boeing symbol, 707, 717, 727, 737, 747, 757, 767, 777, 787, Dreamliner, BBJ, DC-8, DC-9, DC-10, KC-10, KDC-10, MD-10, MD-11, MD-80, MD-88, MD-90, P-8A, Poseidon and the Boeing livery are all trademarks owned by The Boeing Company; and no trademark license is granted in connection with this document unless provided in writing by Boeing.
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Original Issue: July 27, 2006 737-30-1058Revision 3: July 07, 2010 1 of 36
2.0
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: July 27, 2006 737-30-1058Revision 3: July 07, 2010 2 of 36 BOEING SERVICE BULLETIN 737-30-1058
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Table of Contents
Revision Transmittal Sheet5
Summary7
1. PLANNING INFORMATION9
A. Effectivity9
1. Airplanes9
2. Spares Affected ........................................ 1 6 B. Concurrent Requirements ...................................... 1 6 C. Reason ................................................ 1 6 D. Description .............................................. 1 7 E. Compliance .............................................. 1 7 F. Approval ............................................... 1 7 G. Manpower .............................................. 1 8 H. Weight and Balance Changes .................................... 1 8 I. Electrical Load Data ......................................... 1 8 J. References .............................................. 1 8
1. Existing Data .......................................... 1 8
2. Data supplied with this Service Bulletin ............................ 1 8
3. Installation Drawings Used in the Preparation of this Service Bulletin ............ 1 8 K. Publications Affected ........................................ 1 9 L. Interchangeability and Intermixability of Parts ........................... 1 9
2. MATERIAL INFORMATION ........................................ 2 1 A. Material - Price and Availability ................................... 2 1 B. Industry Support Information .................................... 2 1 C. Parts Necessary For Each Airplane ................................. 2 1
1. Kits/Parts ............................................ 2 1
2. Parts and Materials Supplied by the Operator ........................ 2 2
3. Parts Modified and Reidentified ................................ 2 2
4. Parts Removed and Not Replaced .............................. 2 2 D. Parts Necessary to Change Spares ................................. 2 2 E. Special Tooling - Price and Availability ............................... 2 2 F. Special Tooling Necessary to do this Service Bulletin ....................... 2 3
3. ACCOMPLISHMENT INSTRUCTIONS .................................. 2 5 A. GENERAL INFORMATION ..................................... 2 5 B. WORK INSTRUCTIONS ....................................... 2 5 FIGURE 1: CAPTAIN'S SIDE - COIL CORD AND PANEL REMOVAL .................. 2 7 FIGURE 2: CAPTAIN'S SIDE - IDENTIFICATION TAPE INSTALLATION ................ 2 8 FIGURE 3: CAPTAIN'S SIDE - CONNECTOR KEYWAY INSPECTION ................. 2 9 FIGURE 4: CAPTAIN'S SIDE - RECLOCKING OF THE CONNECTOR KEYWAY ........... 3 0 FIGURE 5: CAPTAIN'S SIDE - COIL CORD AND PANEL INSTALLATION ............... 3 1 FIGURE 6: FIRST OFFICER'S SIDE - COIL CORD AND PANEL REMOVAL .............. 3 2 FIGURE 7: FIRST OFFICER'S SIDE - IDENTIFICATION TAPE INSTALLATION ............ 3 3 FIGURE 8: FIRST OFFICER'S SIDE - CONNECTOR KEYWAY INSPECTION ............. 3 4 FIGURE 9: FIRST OFFICER'S SIDE - RECLOCKING OF THE CONNECTOR KEYWAY ....... 3 5 FIGURE 10: FIRST OFFICER'S SIDE - COIL CORD AND PANEL INSTALLATION ........... 3 6
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Commercial Airplanes 737 Service Bulletin
SPECIAL ATTENTION Revision Transmittal SheetNumber: 737-30-1058Original Issue: July 27, 2006 Revision 3: July 07, 2010 ATA System: 3041 SUBJECT: ICE AND RAIN PROTECTION - Control Cabin Window Anti-Icing System - Coil Cord Assembly Replacement on the Number 2 Windows in the Flight Compartment This revision includes all pages of the service bulletin.
COMPLIANCE INFORMATION RELATED TO THIS REVISION Boeing recommends that the change given in this service bulletin be done within 48 months after the Revision 3 date of this service bulletin.
No more work is necessary on airplanes changed in accordance with the original issue, Revision 1, or Revision 2 of this service bulletin.
REASON FOR REVISION This revision is sent to notify operators that the Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive (AD) related to this service bulletin. The AD will make the compliance tasks and times given in this service bulletin mandatory.
These sections were changed:
1. On the Summary page, in the Compliance paragraph, a compliance time was added to accomplish this service bulletin.
2. In Paragraph 1.E., Compliance, added a compliance time to accomplish this service bulletin.
Vertical lines are put on the left edge of each page, except in Paragraph 1.A., Effectivity, to show the location of important changes.
Pages with no vertical lines have no important changes.
REVISION HISTORY July 27, 2006Original Issue:
June 18, 2007Revision 1:
February 13, 2009Revision 2:
July 07, 2010Revision 3:
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BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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Commercial Airplanes 737 Service Bulletin
SPECIAL ATTENTION SummaryNumber: 737-30-1058Original Issue: July 27, 2006 Revision 3: July 07, 2010 ATA System: 3041 SUBJECT: ICE AND RAIN PROTECTION - Control Cabin Window Anti-Icing System - Coil Cord Assembly Replacement on the Number 2 Windows in the Flight Compartment BOEING RECOMMENDS THAT EACH OPERATOR EXAMINE THIS SERVICE BULLETIN IMMEDIATELY.
CONCURRENT REQUIREMENTS None.
BACKGROUND Boeing received a report from an operator of arcing and smoke at the left number 2 window in the flight compartment. An investigation showed the cause of this problem to be mechanical damage at the connector backshell of the coil cord assembly. The new assembly will prevent mechanical damage which could cause a fire in the flight compartment.
This service bulletin gives instructions to install a new coil cord assembly on the captain’s and first officer’s sides of the number 2 windows in the flight compartment. This bulletin also gives instructions to inspect and reclock the connector keyways if necessary.
Boeing Service Related Problem (SRP) 737-SRP-56-0017 is related to this service bulletin.
ACTION (PRR 38275-97) Get access to the flight compartment. Do an inspection of the connector keyway’s orientation on both sides of the coil cord located on the captain’s and first officer’s number 2 windows.
Reclock the connector keyway if necessary and replace the coil cord assembly.
Do the Window Heat Control Unit (WHCU) Test.
EFFECTIVITY 737-600, -700, -700C, -800, -900 Airplanes. See Service Bulletin Paragraph 1.A.1., Airplanes, for the list of affected airplanes.
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COMPLIANCE The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to this service bulletin. The Airworthiness Directive will make the compliance tasks and times given in this service bulletin mandatory.
Boeing recommends that the change given in this service bulletin be done within 48 months after the Revision 3 date of this service bulletin.
INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are available for airplanes in warranty as of August 8, 2005. Please refer to Paragraph
2.B., Industry Support Information.
MANPOWER Elapsed HoursTotal Task HoursAirplanes
3.255.50Group 1
MATERIAL INFORMATION Boeing Supplied Kits/Parts.
Refer to Paragraph 2.A., Material - Price and Availability.
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Commercial Airplanes 737 Service Bulletin
SPECIAL ATTENTION Number: 737-30-1058 Original Issue: July 27, 2006 Revision 3: July 07, 2010 ATA System: 3041 SUBJECT: ICE AND RAIN PROTECTION - Control Cabin Window Anti-Icing System - Coil Cord Assembly Replacement on the Number 2 Windows in the Flight Compartment BOEING RECOMMENDS THAT EACH OPERATOR EXAMINE THIS SERVICE BULLETIN IMMEDIATELY.
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. An equivalent change is on subsequent production airplanes. Refer to PRR38275-97 for data about this change.
DESCRIPTIONCONFIGURATIONGROUP Airplanes with one 90 degree and one straight connector backshell installed on window number 2.
-1 Airplane Models:
737-600, 737-700, 737-700C, 737-800, 737-900 GroupVariable Number 1YA001 - YA099 1YA101 - YA199 1YA201 - YA211 1YA221 1YA231 - YA242 1YA251 - YA256 1YA271 - YA272
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GroupVariable Number 1YA291 1YA301 - YA302 1YA311 - YA314 1YA321 - YA323 1YA336 - YA345 1YA351 1YA356 - YA357 1YA366 - YA367 1YA371 - YA377 1YA501 - YA536 1YA541 - YA552 1YA571 - YA578 1YA601 - YA615 1YA621 - YA622 1YA626 - YA631 1YA635 - YA636 1YA641 - YA642 1YA645 - YA650 1YA656 - YA659 1YA666 - YA667 1YA671 - YA672 1YA681 - YA691 1YA701 - YA710 1YA721 - YA722 1YA731 - YA734 1YA751 - YA756 1YA801 - YA803 1YA809 1YA811 - YA814 1YA831 - YA835 1YA841 - YA862 1YA881 - YA882 1YA891 - YA892
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GroupVariable Number 1YA961 - YA977 1YB001 - YB006 1YB101 - YB132 1YB151 - YB153 1YB156 - YB158 1YB161 - YB164 1YB171 - YB172 1YB181 - YB184 1YB201 - YB208 1YB271 1YB276 1YB301 - YB310 1YB371 - YB390 1YB501 - YB502 1YB521 - YB526 1YB541 - YB544 1YB551 1YB561 - YB579 1YB581 - YB596 1YB601 - YB632 1YB651 1YB656 1YB851 - YB863 1YB871 - YB874 1YB881 - YB890 1YB901 - YB903 1YB911 1YB961 - YB964 1YC001 - YC030 1YC051 - YC083 1YC091 - YC094 1YC101 - YC104 1YC111 - YC113
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GroupVariable Number 1YC121 1YC126 - YC127 1YC136 - YC141 1YC146 - YC147 1YC151 - YC156 1YC166 - YC171 1YC176 - YC178 1YC186 - YC189 1YC201 - YC203 1YC206 - YC207 1YC301 - YC305 1YC321 - YC387 1YC391 - YC394 1YC396 1YC401 - YC417 1YC421 - YC422 1YC426 - YC428 1YC436 - YC437 1YC441 - YC448 1YC451 - YC455 1YC459 1YC461 - YC467 1YC471 - YC499 1YC501 - YC526 1YC571 - YC583 1YC587 - YC589 1YC591 - YC593 1YC601 - YC655 1YC681 - YC696 1YC701 - YC715 1YC720 - YC725 1YC727 - YC742 1YC751 - YC752
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