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Commercial Airplanes 737 Service Bulletin ALERT Number: 737-30A1064 Original Issue: May 04, 2017 Revision 2: June 26, 2020 ATA System: 3031 SUBJECT: ICE AND RAIN PROTECTION - Pitot Static Tubes, Temperature Probe, and Alpha Vane Anti-Icing System - Change P5 and P18-3 Panels to Activate Automated Probe Heat System 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 © 2017 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Unpublished Work.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, KC-46, KDC-10, MD-10, MD-11, MD-80, MD-88, MD-90, P-8, 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.
Original Issue: May 04, 2017 737-30A1064Revision 2: June 26, 2020 1 of 84
5.0
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: May 04, 2017 737-30A1064Revision 2: June 26, 2020 2 of 84 BOEING SERVICE BULLETIN 737-30A1064
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Table of Contents
Revision Transmittal Sheet5
Summary9
1. PLANNING INFORMATION13
A. Effectivity13
1. Airplanes13
2. Spares Aff ected20
B. Concurrent Requirements20
C. Reason20
D. Description21
E. Compliance23
F. Approval24
G. Manpower24
H. Weight and Balance Changes27
I. Electrical Load Data27
J. References27
1. Existing Data:27
2. Data Supplied with this Ser vice Bulletin:27
3. Installation Drawings Used in the Prepar ation of this Ser vice Bulletin:27
K. Publications Affected27
L. Interchangeability and Inter mixability of P arts28
M. Software Accomplishment Summar y28
2. MATERIAL INFORMATION29
A. Material - Pr ice and Availability29
B. Industry Suppor t Information29
C. Parts Necessary for Each Air plane29
1. Kits/Parts29
2. Parts and Mater ials Supplied by the Operator29
3. Parts Modified and Reidentified29
4. Parts Removed and Not Replaced29
D. Parts Necessary to Change Spares30
E. Special Tooling - Pr ice and Availability30
F. Special Tooling Necessary to do this Ser vice Bulletin30
3. ACCOMPLISHMENT INSTRUCTIONS31
A. GENERAL INFORMATION31
B. WORK INSTRUCTIONS32
FIGURE 1: FLIGHT COMPARTMENT - P5-9 WINDOW AND PITOT HEAT MODULE - REPLACEMENT
[Group 1, 6]71
FIGURE 2: FLIGHT COMPARTMENT - P5-9 WINDOW AND PITOT HEAT MODULE - REPLACEMENT
[Group 2-4]73
FIGURE 3: FLIGHT COMPARTMENT - P18-3 CIRCUIT BREAKER PANEL - CHANGE [Group 1, 6] . 75 FIGURE 4: FLIGHT COMPARTMENT - P18-3 CIRCUIT BREAKER PANEL - CHANGE [Group 2] . . . 77 FIGURE 5: FLIGHT COMPARTMENT - P18-3 CIRCUIT BREAKER PANEL - CHANGE [Group 3] . . . 79 FIGURE 6: FLIGHT COMPARTMENT - P18-3 CIRCUIT BREAKER PANEL - CHANGE [Group 4] . . . 81 FIGURE 7: FLIGHT COMPARTMENT - P18-3 CIRCUIT BREAKER PANEL - CHANGE [Group 1-4, 6] . 83 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: May 04, 2017 737-30A1064Revision 2: June 26, 2020 3 of 84 BOEING SERVICE BULLETIN 737-30A1064
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Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: May 04, 2017 737-30A1064Revision 2: June 26, 2020 4 of 84 BOEING SERVICE BULLETIN 737-30A1064
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Commercial Airplanes 737 Service Bulletin ALERT Revision Transmittal SheetNumber: 737-30A1064Original Issue: May 04, 2017 Revision 2: June 26, 2020 ATA System: 3031 SUBJECT: ICE AND RAIN PROTECTION - Pitot Static Tubes, Temperature Probe, and Alpha Vane Anti-Icing System - Change P5 and P18-3 Panels to Activate Automated Probe Heat System This revision includes all pages of the service bulletin.
COMPLIANCE INFORMATION RELATED TO THIS REVISION Federal Aviation Administration (FAA) Airworthiness Directive (AD) 2019-09-01 is related to this service bulletin.
Airplanes PK625-PK627 were added to new Group 6 of this service bulletin effectivity.
Effects of this revision on airplanes on which Revision 1 were previously done:
None.
REASON FOR REVISION This revision is sent to add airplanes inadvertently omitted to the effectivity of this service bulletin, PK625-PK627.
These airplanes are in the effectivity of the concurrent requirement service bulletins.
The data given in Information Notice (IN) 737-30A1064 IN 01 is included in this revision.
The data given in Alternative Method of Compliance Notice (AMOC) 737-30A1064 AMOC 01 is included in this revision.
These sections were changed:
1. Summary, ACTION, added Group 6 information.
2. Summary, COMPLIANCE, added FAA AD and changed to reference statements.
3. Paragraph 1.A.1., Airplanes, added airplanes to Group 6.
4. Paragraph 1.B., Concurrent Requirements, added Group 6 information.
5. Paragraph 1.C., Reason:
a. Added revision statement.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: May 04, 2017 737-30A1064Revision 2: June 26, 2020 5 of 84
b. Added Information Notice (IN) statement.
c. Added Alternative Method of Compliance (AMOC) statement.
6. Paragraph 1.D., Description:
a. Added Group 6 information.
b. Added effects of this Revision.
c. Added Group 6 Maintenance Zones information.
7. Paragraph 1.E., Compliance:
a. Added FAA AD and compliance statements.
b. Added Group 6 compliance table.
8. Paragraph 1.F. Approval, added AMOC statement.
9. Paragraph 1.G. Manpower, added Group 6 manpower.
10. Paragraph 1.J.1., Existing Data:
a. Added FAA AD reference.
b. Changed Aircraft Maintenance Manual (AMM) reference.
11. Paragraph 1.K., Publications Affected, added and removed references.
12. Paragraph 2.C.2, Parts and Materials Supplied by the Operator, added Group 6 information.
13. Paragraph 3.B., Work Instructions:
a. Added Group 6 work instructions.
b. Added notes for TAT test feature.
c. Added FIGURE 7 instructions.
14. FIGURE 1:
a. Added Group 6 applicability.
b. Step table, footnote (a), changed Aircraft Maintenance Manual (AMM) reference.
15. FIGURE 3, added Group 6 applicability.
16. Added FIGURE 7.
Vertical lines are put on the left edge of each page, except in Paragraph 1.A., Effectivity and format changes, to show the location of all content changes.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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Pages with no vertical lines have no changes.
REVISION HISTORY May 04, 2017Original Issue:
October 18, 2017Revision 1:
June 26, 2020Revision 2:
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: May 04, 2017 737-30A1064Revision 2: June 26, 2020 8 of 84 BOEING SERVICE BULLETIN 737-30A1064
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Commercial Airplanes 737 Service Bulletin ALERT SummaryNumber: 737-30A1064Original Issue: May 04, 2017 Revision 2: June 26, 2020 ATA System: 3031 SUBJECT: ICE AND RAIN PROTECTION - Pitot Static Tubes, Temperature Probe, and Alpha Vane Anti-Icing System - Change P5 and P18-3 Panels to Activate Automated Probe Heat System
THIS DOCUMENT 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 DOCUMENT TO THE NEW OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS DOCUMENT TO THE NEW OWNER.
CONCURRENT REQUIREMENTS Refer to Paragraph 1.B., Concurrent Requirements.
BACKGROUND Boeing has received reports from operators that the pitot heat switch is not always set to ON. The work given in this service bulletin changes the anti-icing system to automatically supply power to heat the air data sensors.
The anti-icing system will come on (AUTO) automatically after engine start if the crew does not activate the system. If this service bulletin is not done, 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 Fleet Team Digest (FTD) 737 FTD 30-8001 is related to this service bulletin.
Boeing Service Related Problem (SRP) 737-SRP-30-0050 (previously 737-SRP-30-0032) is related to this service bulletin.
As a part of a service bulletin remote certification program, this change was completed on airplane PR009 by Service Bulletin 737-30A1064 RC 1 before the Original Issue of this service bulletin. The change completed on airplane PR009 by Service Bulletin 737-30A1064 RC 1 is equivalent to the Original Issue of this service bulletin.
Airplane PR009 has the configuration of a Group 3 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 Paragraph 1.E., ComplianceYesAD Related Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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ReferenceAffectedPlanning Data Paragraph 1.H., Weight and Balance ChangesNoWeight 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/PartsNoKits/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 35005-295RS) Group 1, 6:
1. Access the flight compartment.
2. Replace the P5-9 Window and Pitot Heat Module.
3. Remove INOP markers and collars on the P18-3 circuit breaker panel.
4. Do Pitot Static and Temperature Probe Anti-Icing System Test.
5. Do Control Cabin Window Anti-Icing System Test.
6. Do repetitive Pitot Static and Temperature Probe Anti-Icing System Test at the times specified in Paragraph 1.E., Compliance.
Group 2-4:
1. Access the flight compartment.
2. Replace the P5-9 Window and Pitot Heat Module.
3. Remove INOP markers and collars on the P18-3 circuit breaker panel.
4. Do Pitot-Static Tubes, Temperature Probe and Alpha Vane Anti-Icing System Test.
5. Do Operational Test - Control Cabin Window Anti-Icing System.
6. Do repetitive Pitot-Static Tubes, Temperature Probe and Alpha Vane Anti-Icing System Test at the times specified in Paragraph 1.E., Compliance.
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Group 5:
Boeing endorses the Federal Aviation Administration (FAA) rules related to Limit of Validity (LOV) and recommends immediate and permanent removal from service of any airplane upon reaching the LOV, whether or not it is operated under FAA jurisdiction. As such, Boeing no longer provides maintenance instructions for airplanes that have accumulated flight cycles beyond the LOV. Airplanes in Group 5 (line numbers 1-291) have accumulated flight cycles beyond the LOV of the maintenance program. Title 14, Code of Federal Regulations (14 CFR)
121.1115 and 129.115 prohibit operation of an airplane beyond its LOV.
Accomplishment of this service bulletin changes the flight deck and/or operations of the airplane. Refer to Paragraph 1.K., Publications Affected, for affected publications.
EFFECTIVITY 737-100/-200/-200C/-300/-400/-500 Airplane(s). Refer to Paragraph 1.A., Effectivity for the list of affected airplane(s).
COMPLIANCE Federal Aviation Administration (FAA) Airworthiness Directive (AD) 2019-09-01 is related to this service bulletin.
The effective date of AD 2019-09-01 is June 26, 2019.
Refer to Paragraph 1.E., Compliance.
INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the configuration changes given in this service bulletin.
MANPOWER Refer to Paragraph 1.G., Manpower.
MATERIAL INFORMATION Operator Supplied Parts/Materials.
Refer to Paragraph 2.A., Material - Price and Availability Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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Original Issue: May 04, 2017 737-30A1064Revision 2: June 26, 2020 12 of 84 BOEING SERVICE BULLETIN 737-30A1064