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Commercial Airplanes 737 Service Bulletin ALERT Number: 737-30A1063 Original Issue: November 16, 2011 Revision 1: July 10, 2012 ATA System: 3000 SUBJECT: ICE AND RAIN PROTECTION - PITOT AND STATIC - Air Data Probe Anti-Icing System
- Air Data Probe Heat Automation Installation Export of this technology is controlled under the United States Export Administration Regulations (EAR) (15 CFR 300-774). 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 © 2011 Boeing.
Unpublished Work. All Rights Reserved.
Treatment of this document and its content is governed by contract with Boeing. Rights to use this document are licensed on a per aircraft basis and such rights may not be transferable. For more information, contact The Boeing Company.
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 Boeing liveries 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. BOEING is a trademark of Boeing Management Company.
Original Issue: November 16, 2011 737-30A1063Revision 1: July 10, 2012 1 of 172
5.0
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 16, 2011 737-30A1063Revision 1: July 10, 2012 2 of 172 BOEING SERVICE BULLETIN 737-30A1063
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BLANK PAGE
Table of Contents
Revision Transmittal Sheet5
Summary7
1. PLANNING INFORMATION ........................................ 1 1 A. Effectivity ............................................... 1 1
1. Airplanes ............................................ 1 1
2. Spares Affected ........................................ 2 6 B. Concurrent Requirements ...................................... 2 6 C. Reason ................................................ 2 7 D. Description .............................................. 2 7 E. Compliance .............................................. 2 8 F. Approval ............................................... 2 9 G. Manpower .............................................. 2 9 H. Weight and Balance Changes .................................... 3 7 I. Electrical Load Data ......................................... 3 8 J. References .............................................. 3 8
1. Existing Data: ......................................... 3 8
2. Data Supplied with this Service Bulletin: ........................... 3 8
3. Installation Drawings Used in the Preparation of this Service Bulletin: ........... 3 8 K. Publications Affected ........................................ 3 9 L. Interchangeability and Intermixability of Parts ........................... 3 9 M. Software Accomplishment Summary ................................ 3 9
2. MATERIAL INFORMATION ........................................ 4 1 A. Material - Price and Availability ................................... 4 1 B. Industry Support Information .................................... 4 9 C. Parts Necessary for Each Airplane ................................. 4 9
1. Kits/Parts ............................................ 4 9
2. Parts and Materials Supplied by the Operator ........................ 7 3
3. Parts Modified and Reidentified ................................ 7 3
4. Parts Removed and Not Replaced .............................. 7 4 D. Parts Necessary to Change Spares ................................. 7 4 E. Special Tooling - Price and Availability ............................... 7 4 F. Special Tooling Necessary to do this Service Bulletin ....................... 7 5
3. ACCOMPLISHMENT INSTRUCTIONS .................................. 7 7 A. GENERAL INFORMATION ..................................... 7 7 B. WORK INSTRUCTIONS ....................................... 7 8 FIGURE 1: REPLACEMENT OF THE P5-9 WINDOW/PITOT HEAT MODULE ............. 8 1 FIGURE 2: INSTALLATION OF THE CIRCUIT BREAKERS INSIDE P18 PANEL ........... 8 3 FIGURE 3: INSTALLATION OF THE INSERTS ON THE P18 PANEL [Group 1-2, 9-10, 12] ...... 8 5 FIGURE 4: INSTALLATION OF THE BRACKET, RELAYS ON THE P18 PANEL [Group 1-2, 9-10, 12] . 87 FIGURE 5: REMOVAL OF THE STANCHION INSIDE THE P18 PANEL [Group 3-5, 8] ........ 9 1 FIGURE 6: INSTALLATION OF THE STANCHION INSIDE THE P18 PANEL [Group 3-5, 8] ..... 9 3 FIGURE 7: INSTALLATION OF THE BRACKET, RELAYS IN THE P18 PANEL [Group 3-8, 11, 13-14] . 95 FIGURE 8: CHANGE WIRE BUNDLES, W0018 AND W0020 [Group 1, 3, 6, 8, 12-13] ........ 1 0 0 FIGURE 9: ROUTE THE WIRE BUNDLES, W0018 AND W0020 [Group 3, 6, 8, 13] ......... 1 0 4 FIGURE 10: ROUTE THE WIRE BUNDLES, W0018 AND W0020 [Group 1, 12] ............ 1 0 6 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 16, 2011 737-30A1063Revision 1: July 10, 2012 3 of 172 BOEING SERVICE BULLETIN 737-30A1063
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FIGURE 11: CHANGE THE WIRE BUNDLES, W0018 AND W0020 [Group 2, 4-5, 7, 9, 11] ...... 1 0 9 FIGURE 12: ROUTE THE WIRE BUNDLES, W0018 AND W0020 [Group 4-5, 7, 11] .......... 1 1 3 FIGURE 13: ROUTE THE WIRE BUNDLES, W0018 AND W0020 [Group 2, 9] ............. 1 1 5 FIGURE 14: CHANGE THE WIRE BUNDLES, W0018 AND W0020 [Group 10, 14] .......... 1 1 8 FIGURE 15: ROUTE THE WIRE BUNDLES, W0018 AND W0020 [Group 14] ............. 1 2 2 FIGURE 16: CHANGE THE WIRE BUNDLE, W0220, INSIDE E2-2 ................... 1 2 4 FIGURE 17: ROUTE THE WIRE BUNDLE, W0220, INSIDE E2-2 .................... 1 2 5 FIGURE 18: CHANGE THE WIRE BUNDLES, W0311 AND W0313, INSIDE E3-1 ........... 1 2 6 FIGURE 19: ROUTE THE WIRE BUNDLES, W0311 AND W0313, INSIDE E3-1 ............ 1 2 8 FIGURE 20: CHANGE THE WIRE BUNDLE, W2112 [Group 10, 14] ................... 1 2 9 FIGURE 21: CHANGE THE WIRE BUNDLE, W2114 [Group 10, 14] ................... 1 3 0 FIGURE 22: CHANGE THE WIRE BUNDLE, W5158 [Group 10, 14] ................... 1 3 2 FIGURE 23: CHANGE THE WIRE BUNDLE, W5510 [Group 10, 14] ................... 1 3 3 FIGURE 24: CHANGE THE WIRE BUNDLE, W2212 [Group 10, 14] ................... 1 3 4 FIGURE 25: ROUTE THE WIRE BUNDLES, W2112, W2114, W2212, W5158, W5510 [Group 10, 14] . 136 FIGURE 26: CHANGE THE WIRE BUNDLE, W2212 [Group 1-9, 11, 13] ................ 1 4 1 FIGURE 27: ROUTE THE WIRE BUNDLE, W2212 [Group 1-9, 11, 13] ................. 1 4 3 FIGURE 28: CHANGE THE WIRE BUNDLE, W2218 [Group 1, 3, 6, 8, 12-13] ............. 1 4 5 FIGURE 29: CHANGE THE WIRE BUNDLE, W2218 [Group 2, 4-5, 7, 9-11, 14] ............ 1 4 7 FIGURE 30: ROUTE THE WIRE BUNDLE, W2218 ............................ 1 4 9 FIGURE 31: CHANGE THE WIRE BUNDLE, W5310 ........................... 1 5 3 FIGURE 32: ROUTE THE WIRE BUNDLE, W5310, FROM E2-2 TO E3-1 ............... 1 5 4 FIGURE 33: CHANGE THE WIRE BUNDLE, W2237 ........................... 1 5 5 FIGURE 34: ROUTE THE WIRE BUNDLE, W2237 ............................ 1 5 6 FIGURE 35: CHANGE THE WIRE BUNDLE, W3381 [Group 1-4, 6-7, 10, 14] .............. 1 5 8 FIGURE 36: ROUTE THE WIRE BUNDLE, W3381 [Group 1-4, 6-7, 10, 14] .............. 1 5 9 FIGURE 37: CHANGE THE WIRE BUNDLE, W6134 [Group 5, 8-9, 11, 13] ............... 1 6 4 FIGURE 38: ROUTE THE WIRE BUNDLE, W6134 [Group 5, 8-9, 11, 13] ................ 1 6 5 FIGURE 39: ROUTE THE WIRE BUNDLES, W0018 AND W0020 [Group 10] ............. 1 7 0 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 16, 2011 737-30A1063Revision 1: July 10, 2012 4 of 172 BOEING SERVICE BULLETIN 737-30A1063
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Commercial Airplanes 737 Service Bulletin ALERT Revision Transmittal SheetNumber: 737-30A1063Original Issue: November 16, 2011 Revision 1: July 10, 2012 ATA System: 3000 SUBJECT: ICE AND RAIN PROTECTION - PITOT AND STATIC - Air Data Probe Anti-Icing System
- Air Data Probe Heat Automation Installation This revision includes all pages of the service bulletin.
COMPLIANCE INFORMATION RELATED TO THIS REVISION Federal Aviation Administration (FAA) Notice of Proposed Rule Making NPRM 2011-NM-268-AD, is related to this service bulletin.
No more work is necessary on the airplane(s) changed in accordance with the original issue of this service bulletin.
REASON FOR REVISION This revision is sent to incorporate the changes from a validation with an operator. The changes are also applied to different groups of airplanes throughout the service bulletin.
These sections were changed:
1. The Summary, Compliance section and the Paragraph 1.E., Compliance is updated to include the reference to "Federal Aviation Administration (FAA) Notice of Proposed Rule Making NPRM 2011-NM-268-AD, is related to this service bulletin."
2. Section 1.J. References is updated to include the reference h. Federal Aviation Administration (FAA) Notice of Proposed Rule Making NPRM 2011-NM-268-AD.
3. Section 1.K. Publications Affected, updated the table to add and delete references to the Airplane Maintenance Manual (AMM), Wire Diagram Manual (WDM), Structural Repair Manual (SRM), and the System Schematic Manual (SSM).
4. Section 2.A. is updated to include new kit availability dates, quantities, ROLT and unit price updates.
5. Section 2.C.1. Material, Parts Necessary For Each Airplane, the top kits have been updated to remove the 280A3157-101, 280A3157-102, 280A3157-103, 280A3157-104, 280A3157-111 and the 280A3157-110 wire kits and add the 280A3157-118, 280A3157-119, 280A3157-120, 280A3157-121, 280A3157-122, and the 280A3157-123 wire kits respectively.
6. In Figure 4, the graphics were changed to show the correct installation of the relays.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 16, 2011 737-30A1063Revision 1: July 10, 2012 5 of 172
7. In Figure 8, the graphics and table were changed to revise the flag note numbers to add two new terminal lug part numbers.
8. In Figure 11, the graphics and table were changed to revise the flag note numbers to add two new terminal lug part numbers.
9. In Figure 14, the graphics and table were changed to revise the flag note numbers to add two new terminal lug part numbers.
10. In Figure 16, the graphics and table were changed to revise the flag note numbers to add a component module and new identification (ID) tapes.
11. In Figure 27, the graphic was changed to add the missing wire bundle routing.
12. In Figure 28, the graphics and table were changed to revise the flag note numbers to delete a terminal module and ID sleeves and add a component module and decals.
13. In Figure 29, the graphics and table were changed to revise the flag note numbers to delete a terminal module and ID sleeves and add a component module and decals.
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 November 16, 2011Original Issue:
July 10, 2012Revision 1:
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 16, 2011 737-30A1063Revision 1: July 10, 2012 6 of 172 BOEING SERVICE BULLETIN 737-30A1063
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Commercial Airplanes 737 Service Bulletin ALERT SummaryNumber: 737-30A1063Original Issue: November 16, 2011 Revision 1: July 10, 2012 ATA System: 3000 SUBJECT: ICE AND RAIN PROTECTION - PITOT AND STATIC - Air Data Probe Anti-Icing System
- Air Data Probe Heat Automation Installation
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 Refer to Paragraph 1.B., Concurrent Requirements.
BACKGROUND This service bulletin provides the instructions and the kits to change the anti-icing system for the angle of attack sensor, the total air temperature, and the pitot probes. The changes to the system will let the anti-icing system automatically supply power to heat the probes. The anti-icing system will automatically come on (AUTO) after engine start if the crew does not activate the system. If this service bulletin is not accomplished, the air data sensors could be unheated which could let ice form on the sensors, and cause erroneous air data. Unreliable air data can lead to loss of crew situational awareness which could cause failure to maintain safe flight and landing of the airplane.
Boeing has received reports that the Pilot Heat switch is not always set to ON.
Fleet Team Digest, 737NG-FTD-30-08002, is related to this service bulletin.
Boeing Service Related Problem, (SRP) 737NG-SRP-30-0032, is related to this service bulletin.
As a part of a service bulletin validation program, this change was completed on airplane YD591 by Service Bulletin 737-30A1063 Original Issue before the release of Revision 1 of this service bulletin. The change completed on airplane YD591 by Service Bulletin 737-30A1063 Original Issue is equivalent to the release of Revision 1 of this service bulletin. Airplane YD591 has the configuration of a Group 2 airplane.
This table is provided to operators for planning purposes only. Refer to the applicable sections for more information.
ReferenceAffectedPlanning Data Paragraph 1.A.2., Spares AffectedNOSpares Affected Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 16, 2011 737-30A1063Revision 1: July 10, 2012 7 of 172
ReferenceAffectedPlanning Data Paragraph 1.E., ComplianceYESAD Related Paragraph 1.H., Weight and Balance ChangesYESWeight and Balance Change Paragraph 1.I., Electrical Load DataNOElectrical Load Changed Paragraph 1.K., Publications AffectedYESPublications Affected Paragraph 1.K., Publications AffectedYESAirplane Flight Operations Affected (Flight Crew Operations Manual and/or FAA Approved Airplane Flight Manual) Paragraph 2.C.1., Kits/PartsYESKits/Parts Required Paragraph 2.C.2., Parts and Materials Supplied by the Operator YESOperator Supplied Material Paragraph 2.F., Special Tooling Necessary to do this Service Bulletin NOSpecial Tooling Required ACTION (PRR 38275-160S) Get access to the flight compartment at the P5 overhead panel. Change wires and replace the P5-9 window/pitot heat module. At the P18 circuit breaker panel, replace two circuit breakers, install relay supports, relays, decals and change the wiring.
Get access to the electrical/electronics compartment. At the E2-2 electronics shelf, change wiring. At the E3-1 electronics shelf, change the wiring.
Do an operational test of the anti-icing system for the air data probes.
EFFECTIVITY 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 24 months after the Revision 1 date of this service bulletin.
Federal Aviation Administration (FAA) Notice of Proposed Rule Making NPRM 2011-NM-268-AD, is related to this service bulletin.
INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the configuration changes given in this service bulletin.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 16, 2011 737-30A1063Revision 1: July 10, 2012 8 of 172 BOEING SERVICE BULLETIN 737-30A1063
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MANPOWER Elapsed HoursTotal Task HoursAirplanes
41.4068.05Each Airplane in Group 1
41.1067.45Each Airplane in Group 2
41.4568.10Each Airplane in Group 3
41.1567.50Each Airplane in Group 4
37.3560.10Each Airplane in Group 5
41.1567.80Each Airplane in Group 6
40.8567.20Each Airplane in Group 7
44.3070.95Each Airplane in Group 8
37.3060.05Each Airplane in Group 9
46.8078.85Each Airplane in Group 10
37.0559.80Each Airplane in Group 11
38.3062.05Each Airplane in Group 12
40.9567.60Each Airplane in Group 13
46.5578.60Each Airplane in Group 14
MATERIAL INFORMATION Boeing Supplied Kits/Parts.
Refer to Paragraph 2.A., Material - Price and Availability.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 16, 2011 737-30A1063Revision 1: July 10, 2012 9 of 172 BOEING SERVICE BULLETIN 737-30A1063
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BOEING SERVICE BULLETIN 737-30A1063
ALERT ALERT
CHANGE WIRING W5310 E3-1 ELECTRONICS E2-2 ELECTRONICS CHANGE WIRING SHELF: CHANGE WIRING W0311, W0313 , WIRING W0220 SHELF: CHANGE W2237 P5 OVERHEAD PANEL:
CHANGE P5-9 MODULE.
CHANGE WIRING W2112, W2218, W2114 J46 JUNCTION BOX:
CHANGE WIRING W2218
CHANGE WIRING W6134, W3381
CHANGE WIRING W2218, W5158, W5510
CHANGE WIRING W0018, W0020 P18 CIRCUIT BREAKER PANEL:
CHANGE CIRCUIT BREAKERS CHANGE WIRING W0018, WO020 J22 JUNCTION BOX:
CHANGE WIRING W5158, W5510 2039246 Original Issue: November 16, 2011 Revision 1: July 10, 2012 PROPRIETARY - Copyright © Unpublished Export Controlled ECCN: 9E991 - BOEING 737-30A1063 Work - See page 1 for details. 10 of 172
Commercial Airplanes 737 Service Bulletin ALERT Number: 737-30A1063 Original Issue: November 16, 2011 Revision 1: July 10, 2012 ATA System: 3000 SUBJECT: ICE AND RAIN PROTECTION - PITOT AND STATIC - Air Data Probe Anti-Icing System
- Air Data Probe Heat Automation Installation
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 This service bulletin is for the airplanes shown below. An equivalent change is on subsequent production airplanes. Refer to PRR 38275-160S for data about this change.
Refer to Service Bulletin Index Document D6-19567 Part 3 for Airplane Variable Number, Line Number, and Serial Number data.
DESCRIPTIONCONFIGURATIONGROUP Airplanes with different wiring configuration.-1 Airplanes with different wiring configuration.-2 Airplanes with different wiring configuration.-3 Airplanes with different wiring configuration.-4 Airplanes with different wiring configuration.-5 Airplanes with different wiring configuration.-6 Airplanes with different wiring configuration.-7 Airplanes with different wiring configuration.-8 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 16, 2011 737-30A1063Revision 1: July 10, 2012 11 of 172
DESCRIPTIONCONFIGURATIONGROUP Airplanes with different wiring configuration.-9 Airplanes with different wiring configuration.-10 Airplanes with different wiring configuration.-11 Airplanes with different wiring configuration.-12 Airplanes with different wiring configuration.-13 Airplanes with different wiring configuration.-14 Airplane Models:
737-600, 737-700, 737-700C, 737-800, 737-900, 737-900ER GroupVariable Number 2YA001 - YA099 2YA101 - YA199 1YA201 - YA211 1YA221 1YA231 - YA242 2YA251 - YA256 2YA271 - YA272 1YA291 1YA301 - YA302 1YA311 - YA314 1YA321 - YA323 1YA336 - YA345 1YA351 1YA356 - YA357 1YA366 - YA367 1YA371 - YA377 2YA501 - YA536 1YA541 - YA552 1YA571 - YA578 2YA601 - YA606 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: November 16, 2011 737-30A1063Revision 1: July 10, 2012 12 of 172 BOEING SERVICE BULLETIN 737-30A1063