# Boeing Alert Service Bulletin 737-30A1063: Revision 1

- Rights: © The Boeing Company. Filed by the FAA in regulations.gov docket FAA-2012-0186; AD 2012-24-08 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
- Document: [Boeing Alert Service Bulletin 737-30A1063](https://openairdocs.org/service-documents/boeing/737-30a1063.md)
- Title as filed: U.S. DOT/FAA - Service Bulletin
- Pages: 172
- PDF: https://openairdocs.org/files/sha256/1d/81/1d81ef1c9bc24b64a1ba5ce86f808d124b21040c1723809c2ff353e036b7d4cf
- Page: https://openairdocs.org/service-documents/boeing/737-30a1063/file/1d81ef1c9bc2

## Text

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### Page 1

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Unpublished Work.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

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Table of Contents
Revision Transmittal Sheet ............................................ 5
Summary ...................................................... 7
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
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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
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ALERTALERT

### Page 5

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.
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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:
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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
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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 Air-
plane 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.
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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.
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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
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### Page 11

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
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### Page 12

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
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GroupVariable Number
1YA607 - YA615
1YA621 - YA622
1YA626
2YA627 - YA629
1YA630 - YA631
1YA635 - YA636
1YA641 - YA642
1YA645 - YA650
1YA656 - YA659
1YA666 - YA667
1YA671 - YA672
1YA681 - YA687
2YA688 - YA691
2YA701 - YA710
2YA721 - YA722
1YA731 - YA734
1YA751 - YA756
2YA801 - YA803
2YA809
2YA811 - YA814
1YA831 - YA835
2YA841 - YA862
2YA881 - YA882
2YA891 - YA892
2YA961 - YA978
1YB001 - YB006
1YB101 - YB132
2YB151 - YB153
2YB156 - YB158
1YB161 - YB164
1YB171 - YB172
2YB181 - YB184
1YB201 - YB208
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GroupVariable Number
1YB271
1YB276
1YB301 - YB310
1YB371 - YB392
1YB501 - YB502
1YB521 - YB526
1YB541 - YB544
1YB551
2YB561 - YB598
1YB601 - YB632
3YB633 - YB635
1YB651
1YB656
1YB671 - YB672
2YB851 - YB863
2YB871 - YB874
2YB881 - YB893
1YB901 - YB903
1YB911
1YB961 - YB973
3YB974
1YB986
3YB987 - YB995
6YB996
1YC001 - YC030
1YC051 - YC084
1YC091 - YC094
3YC095
1YC101 - YC104
1YC111 - YC113
1YC121
1YC126 - YC127
1YC136 - YC141
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GroupVariable Number
1YC146 - YC147
1YC151 - YC156
1YC166 - YC169
2YC170
1YC171
1YC176 - YC179
1YC186 - YC190
1YC201 - YC203
1YC206 - YC207
1YC301 - YC305
2YC321 - YC380
1YC381 - YC387
1YC391 - YC394
2YC396
2YC401 - YC407
1YC408 - YC417
1YC421 - YC422
1YC426 - YC428
1YC436 - YC439
2YC441
1YC442 - YC448
1YC451 - YC455
1YC459
1YC461 - YC467
1YC471 - YC499
1YC501 - YC526
2YC571 - YC583
2YC587 - YC589
2YC591 - YC593
2YC601 - YC655
2YC681 - YC696
1YC701 - YC715
1YC720 - YC725
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GroupVariable Number
1YC727 - YC730
2YC731 - YC741
1YC742 - YC752
1YC761 - YC770
1YC781 - YC793
2YC801 - YC892
1YC901 - YC907
1YC921 - YC922
1YC931 - YC932
2YC941 - YC951
2YC971 - YC978
2YC981 - YC983
1YD001 - YD007
1YD021 - YD025
1YD041 - YD057
1YD081 - YD084
1YD101 - YD110
6YD111
2YD121 - YD126
1YD151 - YD159
2YD171 - YD172
1YD201 - YD203
1YD206 - YD209
1YD216 - YD219
1YD251 - YD254
1YD256 - YD257
1YD261
1YD301 - YD334
1YD391
1YD401 - YD410
1YD412 - YD414
3YD415 - YD416
6YD417
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GroupVariable Number
1YD481 - YD485
2YD491 - YD499
2YD501 - YD512
1YD531 - YD535
2YD541 - YD547
2YD561 - YD564
2YD571 - YD572
2YD591 - YD595
2YD601 - YD612
2YD651 - YD655
1YE001 - YE020
1YE051
1YE101 - YE109
1YE151 - YE157
1YE171 - YE172
1YE201 - YE206
1YE301 - YE305
1YE321 - YE326
1YE371 - YE383
3YF001 - YF009
6YF010 - YF011
4YF021 - YF041
7YF042 - YF045
4YF046 - YF047
7YF048
4YF051 - YF060
7YF061 - YF062
3YF086
1YF106 - YF107
1YF111
3YF112 - YF114
3YF116 - YF117
3YF121 - YF124
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GroupVariable Number
6YF125 - YF126
1YF176 - YF177
3YF178
3YF191 - YF192
4YF201 - YF252
7YF253 - YF265
3YF401 - YF402
7YF431 - YF432
4YF441
7YF442
3YF451 - YF455
6YF456 - YF459
3YF501 - YF588
6YF589 - YF592
4YF701 - YF707
3YF801 - YF803
3YF831 - YF832
3YF836 - YF837
4YF901 - YF903
7YF904 - YF905
3YF921 - YF922
6YF923 - YF926
7YF951
1YG001 - YG044
1YG061 - YG064
1YG066 - YG089
1YG091 - YG099
1YG101 - YG103
1YG111 - YG114
1YG116 - YG119
3YG120 - YG125
6YG126
1YG201 - YG205
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GroupVariable Number
1YG211 - YG214
3YG221 - YG224
2YG251 - YG252
10YG501 - YG509
14YG510 - YG511
10YG601 - YG602
10YG701
10YG711
9YH001 - YH010
5YH011 - YH012
5YH031 - YH050
9YH051 - YH052
5YH053 - YH055
11YH071 - YH076
9YH101 - YH109
5YH110 - YH130
11YH131 - YH132
12YH201
8YH202
8YH206 - YH207
8YH301 - YH305
13YH306
8YH321 - YH322
1YJ001 - YJ008
3YJ009 - YJ010
1YJ011 - YJ013
1YJ021
1YJ471 - YJ480
2YJ501 - YJ517
2YJ531 - YJ562
4YJ563 - YJ579
2YJ591 - YJ596
4YJ597 - YJ599
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GroupVariable Number
1YJ631 - YJ632
2YJ671 - YJ682
1YJ683 - YJ685
2YJ686 - YJ694
1YJ801 - YJ867
1YJ871 - YJ873
3YJ874 - YJ880
1YJ901 - YJ904
1YJ908
3YJ909 - YJ910
2YJ911 - YJ929
1YJ931 - YJ937
1YJ941 - YJ947
2YJ948 - YJ949
1YJ950 - YJ952
2YJ953
1YJ954 - YJ956
6YJ961
1YJ976 - YJ977
1YK001 - YK007
1YK101 - YK104
1YK111 - YK112
1YK121 - YK122
1YK131 - YK132
3YK133
1YK136 - YK139
1YK141 - YK142
1YK146 - YK148
1YK151 - YK154
1YK161 - YK166
3YK167
1YK171
3YK176 - YK177
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GroupVariable Number
3YK186
3YK191
3YK196
4YK201 - YK202
1YK301 - YK309
3YK310 - YK314
1YK321 - YK337
3YK338 - YK340
1YK361 - YK373
3YK374 - YK378
1YK401 - YK406
1YK426 - YK427
2YK431 - YK450
2YK456 - YK460
4YK461 - YK466
7YK467
4YK471 - YK472
7YK473
2YK476
1YK480 - YK485
3YK486 - YK487
1YK495
3YK496 - YK498
2YK511 - YK516
4YK521 - YK530
1YK551 - YK565
3YK566 - YK570
1YK571
1YK576 - YK577
2YK580 - YK585
1YK601 - YK602
1YK606 - YK607
1YK611 - YK614
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GroupVariable Number
3YK615 - YK616
1YK621 - YK625
3YK626 - YK630
1YK631 - YK634
1YK641 - YK644
1YK651 - YK660
3YK661 - YK665
3YK671 - YK672
3YK676 - YK677
3YK681 - YK686
3YK691
2YK701 - YK711
4YK712 - YK713
2YK716 - YK719
2YK721 - YK741
2YK751 - YK758
4YK759 - YK770
4YK776 - YK778
4YK781 - YK782
1YK791 - YK792
1YK796 - YK797
1YK801 - YK884
3YK885 - YK899
1YK901 - YK910
3YK911 - YK912
1YK918
3YK919
1YK921 - YK925
3YK926 - YK927
1YK941 - YK951
3YK952 - YK957
6YK958
1YK961 - YK971
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GroupVariable Number
3YK972 - YK980
2YK981 - YK984
4YK985 - YK992
7YK993
2YL001 - YL005
1YL011
2YL012 - YL016
1YL021 - YL024
1YL051 - YL052
1YL056 - YL057
1YL061
2YL066 - YL069
1YL076 - YL077
2YL101 - YL113
4YL114 - YL134
12YL201 - YL207
8YL208 - YL220
13YL221 - YL223
1YL271 - YL272
1YL281 - YL282
3YL283 - YL284
1YL301 - YL303
2YL311 - YL312
7YL313 - YL314
2YL316 - YL318
4YL319 - YL320
3YL321
3YL351 - YL353
1YL371 - YL373
3YL374
3YL401
1YL421 - YL426
3YL427 - YL429
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GroupVariable Number
2YL431 - YL437
4YL438 - YL444
1YL461 - YL471
3YL472 - YL478
12YL501 - YL505
8YL506 - YL509
2YL531 - YL533
4YL534
3YL541 - YL544
2YL561
4YL562 - YL568
1YL591
3YL592 - YL595
6YL596 - YL597
1YL601 - YL606
3YL611 - YL612
3YL616 - YL617
3YL621
3YL626
3YL631 - YL634
6YL636 - YL637
4YL661 - YL664
4YL676 - YL681
4YL691
3YL701 - YL704
6YL705 - YL706
3YL731
3YL751 - YL752
3YL756
5YL761 - YL773
11YL774 - YL778
7YL796
4YL801 - YL805
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GroupVariable Number
3YL806 - YL811
2YL901 - YL903
4YL904 - YL910
4YL921 - YL930
1YL931 - YL932
3YL933 - YL938
6YL939 - YL940
3YL951 - YL964
6YL965 - YL967
1YM101 - YM103
1YM201 - YM236
3YM237 - YM242
2YM251 - YM299
2YM301 - YM363
4YM364 - YM393
7YM394 - YM396
2YM471
2YM481 - YM484
2YM501 - YM515
1YM521 - YM522
1YM541
2YM551 - YM553
1YM571 - YM572
1YM581 - YM582
2YM591 - YM593
4YM594 - YM599
2YM631 - YM634
1YM641 - YM648
3YM649 - YM652
1YM671 - YM672
3YM673 - YM674
3YM691 - YM697
6YM698
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GroupVariable Number
4YM701 - YM710
4YM761 - YM763
7YM764
2YN001 - YN016
2YN021 - YN023
4YN024
1YN061
2YN071 - YN079
4YN080 - YN082
1YN091 - YN092
1YN101 - YN112
1YN121
1YN201
3YN202
1YN211 - YN215
3YN216 - YN219
1YN231
3YN232 - YN235
4YN261
3YQ001 - YQ003
3YQ011 - YQ012
3YQ026
6YQ036 - YQ038
6YQ201
6YQ241
6YQ401 - YQ402
7YR001 - YR002
6YR051
2. Spares Affected
None.
B. Concurrent Requirements
None
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### Page 27

C. Reason
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.
Revision 1 is sent to update multiple figures, graphics and/or tables, to correct items encountered during
the validation. Figure 4 was changed to correct the graphic for the installation of the relays. Figures 8,
11 and 14 were updated to change the graphics and tables to include new terminal lug part numbers.
Figure 27 was changed to add a section of the routing of the W2212 wire bundle. Figures 16, 28 and
29 were changed to update the graphics and tables to revise the component module part numbers and
add decals.
D. Description
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.
Revision 1 - No more work is necessary on airplanes changed in accordance with the original issue of
this service bulletin.
The work in this service bulletin is done in the maintenance zone(s) given below.
Group 1:
Affected Maintenance Zones
ZoneModel
117, 118, 121, 122, 211, 212737-600, 737-700, 737-800,
737-900
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### Page 28

Group 2:
Affected Maintenance Zones
ZoneModel
117, 118, 121, 122, 211, 212737-700, 737-800, 737-900
Group 3-4, 6-7:
Affected Maintenance Zones
ZoneModel
117, 118, 121, 122, 211, 212737-700, 737-800
Group 5, 8, 11-13:
Affected Maintenance Zones
ZoneModel
117, 118, 121, 122, 211, 212737-800, 737-900ER
Group 9:
Affected Maintenance Zones
ZoneModel
117, 118, 121, 122, 211, 212737-900ER
Group 10, 14:
Affected Maintenance Zones
ZoneModel
117, 118, 121, 122, 211, 212737-700C
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 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.
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### Page 29

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 configuration changes 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 inspect the work
 Time to cure the materials
 Time to find the tools.
Group 1:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
0.750.751Open Access
0.500.501FIGURE 1
0.750.751FIGURE 2
1.001.001FIGURE 3, FIGURE 4
14.2528.502FIGURE 8, FIGURE 10
3.053.051FIGURE 16, FIGURE 17
3.106.202FIGURE 18, FIGURE 19
2.905.802FIGURE 26, FIGURE 27
3.607.202FIGURE 28, FIGURE 30
2.602.601FIGURE 31, FIGURE 32
2.805.602FIGURE 33, FIGURE 34
3.353.351FIGURE 35, FIGURE 36
2.002.001Test
0.750.751Close access
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### Page 30

Group 1:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
41.4068.05TOTAL FOR EACH AIRPLANE
Group 2:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
0.750.751Open Access
0.500.501FIGURE 1
0.750.751FIGURE 2
1.001.001FIGURE 3, FIGURE 4
13.9527.902FIGURE 11, FIGURE 13
3.053.051FIGURE 16, FIGURE 17
3.106.202FIGURE 18, FIGURE 19
2.905.802FIGURE 26, FIGURE 27
3.607.202FIGURE 29, FIGURE 30
2.602.601FIGURE 31, FIGURE 32
2.805.602FIGURE 33, FIGURE 34
3.353.351FIGURE 35, FIGURE 36
2.002.001Test
0.750.751Close access
41.1067.45TOTAL FOR EACH AIRPLANE
Group 3:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
0.750.751Open Access
0.500.501FIGURE 1
0.750.751FIGURE 2
0.300.301FIGURE 5, FIGURE 6
0.750.751FIGURE 7
14.2528.502FIGURE 8, FIGURE 9
3.053.051FIGURE 16, FIGURE 17
3.106.202FIGURE 18, FIGURE 19
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### Page 31

Group 3:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
2.905.802FIGURE 26, FIGURE 27
3.607.202FIGURE 28, FIGURE 30
2.602.601FIGURE 31, FIGURE 32
2.805.602FIGURE 33, FIGURE 34
3.353.351FIGURE 35, FIGURE 36
2.002.001Test
0.750.751Close access
41.4568.10TOTAL FOR EACH AIRPLANE
Group 4:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
0.750.751Open Access
0.500.501FIGURE 1
0.750.751FIGURE 2
0.300.301FIGURE 5, FIGURE 6
0.750.751FIGURE 7
13.9527.902FIGURE 11, FIGURE 12
3.053.051FIGURE 16, FIGURE 17
3.106.202FIGURE 18, FIGURE 19
2.905.802FIGURE 26, FIGURE 27
3.607.202FIGURE 29, FIGURE 30
2.602.601FIGURE 31, FIGURE 32
2.805.602FIGURE 33, FIGURE 34
3.353.351FIGURE 35, FIGURE 36
2.002.001Test
0.750.751Close access
41.1567.50TOTAL FOR EACH AIRPLANE
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### Page 32

Group 5:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
0.750.751Open Access
0.500.501FIGURE 1
0.750.751FIGURE 2
0.300.301FIGURE 5, FIGURE 6
0.750.751FIGURE 7
13.9527.902FIGURE 11, FIGURE 12
3.053.051FIGURE 16, FIGURE 17
3.106.202FIGURE 18, FIGURE 19
2.905.802FIGURE 26, FIGURE 27
2.602.601FIGURE 31, FIGURE 32
2.805.602FIGURE 33, FIGURE 34
3.153.151FIGURE 37, FIGURE 38
2.002.001Test
0.750.751Close access
37.3560.10TOTAL FOR EACH AIRPLANE
Group 6:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
0.750.751Open Access
0.500.501FIGURE 1
0.750.751FIGURE 2
0.750.751FIGURE 7
14.2528.502FIGURE 8, FIGURE 9
3.053.051FIGURE 16, FIGURE 17
3.106.202FIGURE 18, FIGURE 19
2.905.802FIGURE 26, FIGURE 27
3.607.202FIGURE 28, FIGURE 30
2.602.601FIGURE 31, FIGURE 32
2.805.602FIGURE 33, FIGURE 34
3.353.351FIGURE 35, FIGURE 36
2.002.001Test
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### Page 33

Group 6:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
0.750.751Close access
41.1567.80TOTAL FOR EACH AIRPLANE
Group 7:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
0.750.751Open Access
0.500.501FIGURE 1
0.750.751FIGURE 2
0.750.751FIGURE 7
13.9527.902FIGURE 11, FIGURE 12
3.053.051FIGURE 16, FIGURE 17
3.106.202FIGURE 18, FIGURE 19
2.905.802FIGURE 26, FIGURE 27
3.607.202FIGURE 29, FIGURE 30
2.602.601FIGURE 31, FIGURE 32
2.805.602FIGURE 33, FIGURE 34
3.353.351FIGURE 35, FIGURE 36
2.002.001Test
0.750.751Close access
40.8567.20TOTAL FOR EACH AIRPLANE
Group 8:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
0.750.751Open Access
0.500.501FIGURE 1
0.750.751FIGURE 2
0.300.301FIGURE 5, FIGURE 6
0.750.751FIGURE 7
14.2528.502FIGURE 8, FIGURE 9
3.053.051FIGURE 16, FIGURE 17
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### Page 34

Group 8:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
3.053.051FIGURE 18, FIGURE 19
3.106.202FIGURE 26, FIGURE 27
2.905.802FIGURE 29, FIGURE 30
2.602.601FIGURE 31, FIGURE 32
2.805.602FIGURE 33, FIGURE 34
3.153.151FIGURE 37, FIGURE 38
2.002.001Test
0.750.751Close access
44.3070.95TOTAL FOR EACH AIRPLANE
Group 9:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
0.750.751Open Access
0.500.501FIGURE 1
0.750.751FIGURE 2
1.001.001FIGURE 3, FIGURE 4
13.9527.902FIGURE 11, FIGURE 13
3.053.051FIGURE 16, FIGURE 17
3.106.202FIGURE 18, FIGURE 19
2.905.802FIGURE 26, FIGURE 27
2.602.601FIGURE 31, FIGURE 32
2.805.602FIGURE 33, FIGURE 34
3.153.151FIGURE 37, FIGURE 38
2.002.001Test
0.750.751Close access
37.3060.05TOTAL FOR EACH AIRPLANE
Group 10:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
0.750.751Open Access
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
34 of 172
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ALERTALERT

### Page 35

Group 10:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
0.500.501FIGURE 1
0.750.751FIGURE 2
1.001.001FIGURE 3, FIGURE 4
10.4520.902FIGURE 14, FIGURE 39
3.053.051FIGURE 16, FIGURE 17
3.106.202FIGURE 18, FIGURE 19
12.1024.202FIGURE 20, FIGURE 21,
FIGURE 22, FIGURE 23,
FIGURE 24, FIGURE 25
3.607.202FIGURE 29, FIGURE 30
2.602.601FIGURE 31, FIGURE 32
2.805.602FIGURE 33, FIGURE 34
3.353.351FIGURE 35, FIGURE 36
2.002.001Test
0.750.751Close access
46.8078.85TOTAL FOR EACH AIRPLANE
Group 11:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
0.750.751Open Access
0.500.501FIGURE 1
0.750.751FIGURE 2
0.750.751FIGURE 7
13.9527.902FIGURE 11, FIGURE 12
3.053.051FIGURE 16, FIGURE 17
3.106.202FIGURE 18, FIGURE 19
2.905.802FIGURE 26, FIGURE 27
2.602.601FIGURE 31, FIGURE 32
2.805.602FIGURE 33, FIGURE 34
3.153.151FIGURE 37, FIGURE 38
2.002.001Test
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
35 of 172
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ALERTALERT

### Page 36

Group 11:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
0.750.751Close access
37.0559.80TOTAL FOR EACH AIRPLANE
Group 12:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
0.750.751Open Access
0.500.501FIGURE 1
0.750.751FIGURE 2
1.001.001FIGURE 3, FIGURE 4
14.2528.502FIGURE 8, FIGURE 9
3.053.051FIGURE 16, FIGURE 17
3.106.202FIGURE 18, FIGURE 19
3.607.202FIGURE 28, FIGURE 30
2.602.601FIGURE 31, FIGURE 32
2.805.602FIGURE 33, FIGURE 34
3.153.151FIGURE 37, FIGURE 38
2.002.001Test
0.750.751Close access
38.3062.05TOTAL FOR EACH AIRPLANE
Group 13:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
0.750.751Open Access
0.500.501FIGURE 1
0.750.751FIGURE 2
0.750.751FIGURE 7
14.2528.502FIGURE 8, FIGURE 10
3.053.051FIGURE 16, FIGURE 17
3.106.202FIGURE 18, FIGURE 19
2.905.802FIGURE 26, FIGURE 27
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
36 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 37

Group 13:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
3.607.202FIGURE 28, FIGURE 30
2.602.601FIGURE 31, FIGURE 32
2.805.602FIGURE 33, FIGURE 34
3.153.151FIGURE 37, FIGURE 38
2.002.001Test
0.750.751Close access
40.9567.60TOTAL FOR EACH AIRPLANE
Group 14:
Elapsed Time
(Hours)
Task-HoursNumber Of PersonsTask
0.750.751Open Access
0.500.501FIGURE 1
0.750.751FIGURE 2
0.750.751FIGURE 7
10.4520.902FIGURE 14, FIGURE 15
3.053.051FIGURE 16, FIGURE 17
3.106.202FIGURE 18, FIGURE 19
12.1024.202FIGURE 20, FIGURE 21,
FIGURE 22, FIGURE 23,
FIGURE 24, FIGURE 25
3.607.202FIGURE 29, FIGURE 30
2.602.601FIGURE 31, FIGURE 32
2.805.602FIGURE 33, FIGURE 34
3.353.351FIGURE 35, FIGURE 36
2.002.001Test
0.750.751Close access
46.5578.60TOTAL FOR EACH AIRPLANE
H. Weight and Balance Changes
Change in Moment
(Pound-Inches)
Change in Weight
(Pounds)Airplane
+ 1,104.0+ 4.0737-600
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
37 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 38

Change in Moment
(Pound-Inches)
Change in Weight
(Pounds)Airplane
+ 888.0+ 4.0737-700
+ 416.0+ 4.0737-800
+ 168.0+ 4.0737-900
+ 168.0+ 4.0737-900ER
I. Electrical Load Data
Not changed.
J. References
1. Existing Data:
a. Engineering Change Memo PRR 38275-160S
b. BAE Systems Service Bulletin SB 233A3201-30-02
c. Component Maintenance Manual (CMM) 25-00-66
d. Federal Aviation Administration (FAA) Notice of Proposed Rule Making (NPRM)
2011-NM-268-AD
e. Standard Overhaul Practices Manual (SOPM) 20-50-05
f. Standard Wiring Practices Manual (SWPM) 20-00-08, 20-00-11, 20-10-11, 20-10-12, 20-10-14,
20-10-18, 20-10-19, 20-20-00, 20-20-10, 20-30-11, 20-30-12, 20-61-11, 20-74-11, 20-81-12,
20-81-22, 20-90-11, 20-90-15
g. 737-600/700/800/900 Aircraft Maintenance Manual (AMM) 24-22-00, 30-31-00, 30-41-41,
33-26-03
h. 737-600/700/800/900 Wiring Diagram Manual (WDM) 24-61-21, 24-61-23, 30-31-11, 30-31-12
2. Data Supplied with this Service Bulletin:
None.
3. Installation Drawings Used in the Preparation of this Service Bulletin:
TitleDrawing Number
BRACKET ASSY - P18 EQUIPMENT SUPPORT233A5513
P18 PANEL SHEET METAL DETAIL/ASSY233A5624
WIRE BUNDLE INSTL - E2-2 SHELF288A2022
WIRE BUNDLE INSTL - E3-1 SHELF288A2031
WIRE BUNDLE INSTL - P18 EE CIRCUIT BREAKER288A4155
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
38 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 39

TitleDrawing Number
WIRE BUNDLE INSTL - FWD AND OVERHEAD PANEL288A4156
WIRE BUNDLE INSTL - AFT AND OVERHEAD PANEL288A4157
These drawings were used to prepare this service bulletin. These drawings are not necessary to
make the specified changes, and are not supplied with this service bulletin. These drawings may
not be applicable to all airplane configurations or operators.
K. Publications Affected
1. Publications:
Chapter-SectionPublication
30-31, 30-41737 Maintenance Manual
24-51, 24-53, 24-61, 30-31, Equipment List737 Wiring Diagram Manual
11-31, 23-29, 24-41, 24-50, 25-20737 Illustrated Parts Catalog
Ch 3.10, Ch 3.20737 FCOM
24-51, 24-53, 24-61, 30-31737 System Schematic Manual
2. Damage Tolerance Based Structural Inspections:
Boeing has evaluated 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
Accomplishment of this service bulletin does not affect interchangeability or intermixability of parts.
M. Software Accomplishment Summary
Not 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
39 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 40

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
40 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT
BLANK PAGE

### Page 41

2.    MATERIAL INFORMATION
A. Material - Price and Availability
Boeing can supply the kits shown in Paragraph 2.C., Parts Necessary for Each Airplane. Operators
are encouraged to share schedule requirements with Boeing for incorporation of the service bulletin.
The kits are subject to the terms and conditions of the Boeing standard purchase order acknowledgment.
Prices are in United States Dollars. Terms: Net 30 days.
Reference this service bulletin and submit your purchase order by one of these methods:
1. Order on-line via ATA Spec 2000 or The Boeing PART Page
2. Fax to (206) 662-7145
Group 1:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
QTYDateNameKit Number
$7,461.002981906/18/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-81
$7,461.002982507/02/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-81
$7,461.00298607/17/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-81
$7,461.002982008/13/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-81
$7,461.002982008/27/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-81
$7,461.002982009/11/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-81
$7,461.002982009/25/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-81
$7,461.002982010/09/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-81
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
41 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 42

Group 1:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
QTYDateNameKit Number
$7,461.002982510/23/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-81
$7,461.002982511/06/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-81
$7,461.002982511/20/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-81
$7,461.002982512/06/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-81
$7,461.002983512/20/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-81
$7,461.002984501/14/13TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-81
$7,461.002984501/28/13TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-81
$7,461.002983202/11/13TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-81
Group 2:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
QTYDateNameKit Number
$6,679.002985006/04/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-91
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
42 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 43

Group 2:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
QTYDateNameKit Number
$6,679.002982006/18/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-91
$6,679.002982507/02/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-91
$6,679.00298507/17/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-91
$6,679.002982008/13/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-91
$6,679.002982008/27/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-91
$6,679.002982009/11/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-91
$6,679.002982009/25/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-91
$6,679.002982010/09/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-91
$6,679.002982010/23/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-91
$6,679.002982011/06/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-91
$6,679.002982011/20/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-91
$6,679.002982012/06/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-91
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
43 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 44

Group 2:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
QTYDateNameKit Number
$6,679.002981012/20/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-91
Group 3:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
QTYDateNameKit Number
$7,588.00298508/13/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-92
$7,588.00298508/27/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-92
$7,588.00298509/11/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-92
$7,588.00298509/25/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-92
$7,588.00298510/09/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-92
$7,588.00298510/23/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-92
$7,588.00298511/06/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-92
$7,588.00298511/20/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-92
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
44 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 45

Group 3:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
QTYDateNameKit Number
$7,588.00298512/06/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-92
$7,588.00298512/20/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-92
$7,588.00298501/14/13TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-92
$7,588.00298501/28/13TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-92
$7,588.002981802/11/13TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-92
$7,588.00298402/25/13TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-92
Group 4:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
QTYDateNameKit Number
$7,445.00298506/18/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-95
$7,445.00298508/13/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-95
$7,445.00298508/27/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-95
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
45 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 46

Group 4:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
QTYDateNameKit Number
$7,445.00298509/11/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-95
$7,445.00298509/25/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-95
$7,445.00298510/09/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-95
Group 5:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
QTYDateNameKit Number
$7,445.00298506/18/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-96
Group 6:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
NameNumber
$7,530.00298TOP KIT - PITOT TUBE AUTOMATION
REPLACEMENT
002A0006-97
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
46 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 47

Group 7:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
NameNumber
$6,664.00298TOP KIT - PITOT TUBE AUTOMATION
REPLACEMENT
002A0006-98
Group 8:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
NameNumber
$8,051.00298TOP KIT - PITOT TUBE AUTOMATION
REPLACEMENT
002A0006-99
Group 9:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
NameNumber
$6,819.00298TOP KIT - PITOT TUBE AUTOMATION
REPLACEMENT
002A0006-100
Group 10:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
QTYDateNameKit Number
$7,781.00298106/18/12TOP KIT - PITOT
TUBE AUTOMATION
REPLACEMENT
002A0006-101
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
47 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 48

Group 11:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
NameNumber
$6,782.00298TOP KIT - PITOT TUBE AUTOMATION
REPLACEMENT
002A0006-102
Group 12:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
NameNumber
$7,475.00298TOP KIT - PITOT TUBE AUTOMATION
REPLACEMENT
002A0006-103
Group 13:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
NameNumber
$7,388.00298TOP KIT - PITOT TUBE AUTOMATION
REPLACEMENT
002A0006-104
Group 14:
REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER
AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION
Unit Price as of
the Revision 01
date of this Ser-
vice Bulletin (US
Dollars)
ROLT as of the
Revision 01 date
of this Service
Bulletin (Calendar
Days)
NameNumber
$7,292.00298TOP KIT - PITOT TUBE AUTOMATION
REPLACEMENT
002A0006-105
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
48 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 49

B. Industry Support Information
Boeing warranty remedies are not available for the configuration changes given in this service bulletin.
C. Parts Necessary for Each Airplane
1. Kits/Parts
To get the kits/parts shown below, refer to Paragraph 2.A., Material - Price and Availability.
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. The Top Kit is divided into Figure kits for
each installation figure shown in the table below.
Figure Kit
1076432Top Kit
1--111002A0006-81
---111002A0006-91
-11--1002A0006-92
-11--1002A0006-95
-11--1002A0006-96
-1---1002A0006-97
-1---1002A0006-98
-11--1002A0006-99
---111002A0006-100
---111002A0006-101
-1---1002A0006-102
1--111002A0006-103
-1---1002A0006-104
-1---1002A0006-105
Figure Kit
392928251613Top Kit
--1-1-002A0006-81
-1--11002A0006-91
--1-1-002A0006-92
-1--1-002A0006-95
----1-002A0006-96
--1-1-002A0006-97
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
49 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 50

Figure Kit
392928251613Top Kit
-1--1-002A0006-98
-1--1-002A0006-99
----11002A0006-100
11-11-002A0006-101
----1-002A0006-102
--1-1-002A0006-103
--1-1-002A0006-104
-1-11-002A0006-105
Top Kit
002A0006-92002A0006-91002A0006-81Wire Kit
111280A3157-108
111280A3157-112
111280A3157-116
111280A3157-115
111280A3157-105
1-1280A3157-118
111280A3157-121
1-1280A3157-123
-1-280A3157-119
-1-280A3157-122
Top Kit
002A0006-97002A0006-96002A0006-95Wire Kit
111280A3157-108
111280A3157-112
111280A3157-116
1-1280A3157-115
111280A3157-105
1--280A3157-118
111280A3157-121
1--280A3157-123
-11280A3157-119
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
50 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 51

Top Kit
002A0006-97002A0006-96002A0006-95Wire Kit
-11280A3157-122
-1-280A3157-109
Top Kit
002A0006-
100002A0006-99002A0006-98Wire Kit
111280A3157-108
111280A3157-112
111280A3157-116
--1280A3157-115
111280A3157-105
-1-280A3157-118
111280A3157-121
-1-280A3157-123
1-1280A3157-119
1-1280A3157-122
11-280A3157-109
Top Kit
002A0006-
103
002A0006-
102
002A0006-
101Wire Kit
11-280A3157-108
111280A3157-112
111280A3157-116
--1280A3157-115
111280A3157-105
1--280A3157-118
111280A3157-121
1--280A3157-123
-1-280A3157-119
-11280A3157-122
11-280A3157-109
--1280A3157-106
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
51 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 52

Top Kit
002A0006-
103
002A0006-
102
002A0006-
101Wire Kit
--1280A3157-107
--1280A3157-113
--1280A3157-114
--1280A3157-117
--1280A3157-120
Top Kit
002A0006-
105
002A0006-
104Wire Kit
-1280A3157-108
11280A3157-112
11280A3157-116
1-280A3157-115
11280A3157-105
-1280A3157-118
11280A3157-121
-1280A3157-123
1-280A3157-122
-1280A3157-109
1-280A3157-106
1-280A3157-107
1-280A3157-113
1-280A3157-114
1-280A3157-117
1-280A3157-120
Group 1:
KIT 002A0006-81
Notes
Existing Part
NumberName
Figure
New Part Number
281610432
Qty
BRACKET ASSY -
P18 EQUIPMENT
...1..233A5513-4
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
52 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 53

Group 1:
KIT 002A0006-81
Notes
Existing Part
NumberName
Figure
New Part Number
281610432
Qty
OVERLAY MARK-
ER, P18-3
.....1233A5518-25
LACING TAPE.1....280A2001-1
CIRCUIT BREAK-
ER
.....2BACC18AD2
BONDING
JUMPER
...1..BACJ40K5A5A7
NUT...2..BACN10YR3CD
RELAY...1..BACR13CG2AB
SCREW, WASHER
HEAD
...2..BACS12FA3K11GR
SCREW..1...BACS12GU3K32
SCREW...1..BACS12GU3K8
DECAL2..2..BACT19J1
TAPE, ID.2...3BACT19J4
RELAY, 6PDT, 10
AMP
...1..F600-D4NC
WASHER...4..NAS1149D0316H
WASHER..1...NAS1149D0316J
INSERT....2.NAS1834C3-250
SPACERS FOR
BOLTS
..1...NAS43DD3-96FC
Group 2:
KIT 002A0006-91
Notes
Existing Part
NumberName
Figure
New Part Number
291613432
Qty
BRACKET ASSY -
P18 EQUIPMENT
...1..233A5513-4
OVERLAY MARK-
ER, P18-3
.....1233A5518-25
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
53 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 54

Group 2:
KIT 002A0006-91
Notes
Existing Part
NumberName
Figure
New Part Number
291613432
Qty
LACING TAPE.1....280A2001-1
CIRCUIT BREAK-
ER
.....2BACC18AD2
BONDING
JUMPER
...1..BACJ40K5A5A7
NUT...2..BACN10YR3CD
RELAY...1..BACR13CG2AB
SCREW, WASHER
HEAD
...2..BACS12FA3K11GR
SCREW..1...BACS12GU3K32
SCREW...1..BACS12GU3K8
DECAL2..2..BACT19J1
TAPE, ID.2...3BACT19J4
RELAY, 6PDT, 10
AMP
...1..F600-D4NC
WASHER...4..NAS1149D0316H
WASHER..1...NAS1149D0316J
INSERT....2.NAS1834C3-250
SPACERS FOR
BOLTS
..1...NAS43DD3-96FC
Group 3:
KIT 002A0006-92
Notes
Existing Part
NumberName
Figure
New Part Number
2816762
Qty
BRACKET - P18
EQUIPMENT SUP-
PORT
..1..233A5513-3
OVERLAY MARK-
ER, P18-3
....1233A5518-25
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
54 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 55

Group 3:
KIT 002A0006-92
Notes
Existing Part
NumberName
Figure
New Part Number
2816762
Qty
STANCHION AS-
SY
...1.233A5624-47
LACING TAPE.1...280A2001-1
CIRCUIT BREAK-
ER
....2BACC18AD2
BONDING
JUMPER
..1..BACJ40K5A5A12
NUT..2..BACN10YR3CD
RELAY..1..BACR13CG2AB
FAIRING SCREWS...1.BACS12FA3K5
FAIRING SCREWS..2..BACS12FA3K7GR
SCREW, WASHER
HEAD
...1.BACS12FA3K8
SCREW..1..BACS12GU3K8
DECAL2.2..BACT19J1
TAPE, ID.2..3BACT19J4
RELAY, 6PDT, 10
AMP
..1..F600-D4NC
WASHER..4..NAS1149D0316H
Group 4:
KIT 002A0006-95
Notes
Existing Part
NumberName
Figure
New Part Number
2916762
Qty
BRACKET - P18
EQUIPMENT SUP-
PORT
..1..233A5513-3
OVERLAY MARK-
ER, P18-3
....1233A5518-25
STANCHION AS-
SY
...1.233A5624-47
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
55 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 56

Group 4:
KIT 002A0006-95
Notes
Existing Part
NumberName
Figure
New Part Number
2916762
Qty
LACING TAPE.1...280A2001-1
CIRCUIT BREAK-
ER
....2BACC18AD2
BONDING
JUMPER
..1..BACJ40K5A5A12
NUT..2..BACN10YR3CD
RELAY..1..BACR13CG2AB
FAIRING SCREWS...1.BACS12FA3K5
FAIRING SCREWS..2..BACS12FA3K7GR
SCREW, WASHER
HEAD
...1.BACS12FA3K8
SCREW..1..BACS12GU3K8
DECAL2.2..BACT19J1
TAPE, ID.2..3BACT19J4
RELAY, 6PDT, 10
AMP
..1..F600-D4NC
WASHER..4..NAS1149D0316H
Group 5:
KIT 002A0006-96
Notes
Existing Part
NumberName
Figure
New Part Number
16762
Qty
BRACKET - P18
EQUIPMENT SUP-
PORT
.1..233A5513-3
OVERLAY MARK-
ER, P18-3
...1233A5518-25
STANCHION AS-
SY
..1.233A5624-47
LACING TAPE1...280A2001-1
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
56 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 57

Group 5:
KIT 002A0006-96
Notes
Existing Part
NumberName
Figure
New Part Number
16762
Qty
CIRCUIT BREAK-
ER
...2BACC18AD2
BONDING
JUMPER
.1..BACJ40K5A5A12
NUT.2..BACN10YR3CD
RELAY.1..BACR13CG2AB
FAIRING SCREWS..1.BACS12FA3K5
FAIRING SCREWS.2..BACS12FA3K7GR
SCREW, WASHER
HEAD
..1.BACS12FA3K8
SCREW.1..BACS12GU3K8
DECAL.2..BACT19J1
TAPE, ID2..3BACT19J4
RELAY, 6PDT, 10
AMP
.1..F600-D4NC
WASHER.4..NAS1149D0316H
Group 6:
KIT 002A0006-97
Notes
Existing Part
NumberName
Figure
New Part Number
281672
Qty
BRACKET - P18
EQUIPMENT SUP-
PORT
..1.233A5513-3
OVERLAY MARK-
ER, P18-3
...1233A5518-25
LACING TAPE.1..280A2001-1
CIRCUIT BREAK-
ER
...2BACC18AD2
BONDING
JUMPER
..1.BACJ40K5A5A12
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
57 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 58

Group 6:
KIT 002A0006-97
Notes
Existing Part
NumberName
Figure
New Part Number
281672
Qty
NUT..2.BACN10YR3CD
RELAY..1.BACR13CG2AB
FAIRING SCREWS..2.BACS12FA3K7GR
SCREW..1.BACS12GU3K8
DECAL2.2.BACT19J1
TAPE, ID.2.3BACT19J4
RELAY, 6PDT, 10
AMP
..1.F600-D4NC
WASHER..4.NAS1149D0316H
Group 7:
KIT 002A0006-98
Notes
Existing Part
NumberName
Figure
New Part Number
291672
Qty
BRACKET - P18
EQUIPMENT SUP-
PORT
..1.233A5513-3
OVERLAY MARK-
ER, P18-3
...1233A5518-25
LACING TAPE.1..280A2001-1
CIRCUIT BREAK-
ER
...2BACC18AD2
BONDING
JUMPER
..1.BACJ40K5A5A12
NUT..2.BACN10YR3CD
RELAY..1.BACR13CG2AB
FAIRING SCREWS..2.BACS12FA3K7GR
SCREW..1.BACS12GU3K8
DECAL2.2.BACT19J1
TAPE, ID.2.3BACT19J4
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
58 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 59

Group 7:
KIT 002A0006-98
Notes
Existing Part
NumberName
Figure
New Part Number
291672
Qty
RELAY, 6PDT, 10
AMP
..1.F600-D4NC
WASHER..4.NAS1149D0316H
Group 8:
KIT 002A0006-99
Notes
Existing Part
NumberName
Figure
New Part Number
2916762
Qty
BRACKET - P18
EQUIPMENT SUP-
PORT
..1..233A5513-3
OVERLAY MARK-
ER, P18-3
....1233A5518-25
STANCHION AS-
SY
...1.233A5624-47
LACING TAPE.1...280A2001-1
CIRCUIT BREAK-
ER
....2BACC18AD2
BONDING
JUMPER
..1..BACJ40K5A5A12
NUT..2..BACN10YR3CD
RELAY..1..BACR13CG2AB
FAIRING SCREWS...1.BACS12FA3K5
FAIRING SCREWS..2..BACS12FA3K7GR
SCREW, WASHER
HEAD
...1.BACS12FA3K8
SCREW..1..BACS12GU3K8
DECAL2.2..BACT19J1
TAPE, ID.2..3BACT19J4
RELAY, 6PDT, 10
AMP
..1..F600-D4NC
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
59 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

### Page 60

Group 8:
KIT 002A0006-99
Notes
Existing Part
NumberName
Figure
New Part Number
2916762
Qty
WASHER..4..NAS1149D0316H
Group 9:
KIT 002A0006-100
Notes
Existing Part
NumberName
Figure
New Part Number
1613432
Qty
BRACKET ASSY -
P18 EQUIPMENT
..1..233A5513-4
OVERLAY MARK-
ER, P18-3
....1233A5518-25
LACING TAPE1....280A2001-1
CIRCUIT BREAK-
ER
....2BACC18AD2
BONDING
JUMPER
..1..BACJ40K5A5A7
NUT..2..BACN10YR3CD
RELAY..1..BACR13CG2AB
SCREW, WASHER
HEAD
..2..BACS12FA3K11GR
SCREW.1...BACS12GU3K32
SCREW..1..BACS12GU3K8
DECAL..2..BACT19J1
TAPE, ID2...3BACT19J4
RELAY, 6PDT, 10
AMP
..1..F600-D4NC
WASHER..4..NAS1149D0316H
WASHER.1...NAS1149D0316J
INSERT...2.NAS1834C3-250
SPACERS FOR
BOLTS
.1...NAS43DD3-96FC
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
60 of 172
BOEING SERVICE BULLETIN 737-30A1063
ALERTALERT

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