TextPartly OCR
Some pages are OCR from a scan. OCR can misread letters and numbers.
Query with SQL
duckdb -csv -c "SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '7f5ec58d330e57c3a8782c042dcad2d66ddf715aa2141ecbe121905d5ca27839' ORDER BY p.page"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '7f5ec58d330e57c3a8782c042dcad2d66ddf715aa2141ecbe121905d5ca27839' ORDER BY p.page
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
Commercial Airplanes 737 Service Bulletin ALERT Number: 737-28A1201 Original Issue: February 19, 2007 Revision 1: May 28, 2009 ATA System: 2820 SUBJECT: FUEL - Engine Fuel Feed System - Fuel Pump Control Ground Fault Interrupter (GFI) Relay Installation Export of this technology is controlled under the United States Export Administration Regulations (EAR) (15 CFR 730-774). An export license may be required before it is used for development, production or use by foreign persons from specific countries. The controller of this data has the individual responsibility to abide by all export laws.
9E991ECCN:
BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET Copyright © 2007 The Boeing Company Unpublished Work - All Rights Reserved Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable subject matter. Boeing also claims copyright in this document as a compilation and/or collective work.
This document includes proprietary information owned by The Boeing Company and/or one or more third parties.
Treatment of the document and the information it contains is governed by contract with Boeing. For more information, contact The Boeing Company, P .O. Box 3707, Seattle, Washington 98124.
Boeing, the Boeing signature, the Boeing symbol, 707, 717, 727, 737, 747, 757, 767, 777, 787, Dreamliner, BBJ, DC-8, DC-9, DC-10, KC-10, KDC-10, MD-10, MD-11, MD-80, MD-88, MD-90, P-8A, Poseidon and the Boeing livery are all trademarks owned by The Boeing Company; and no trademark license is granted in connection with this document unless provided in writing by Boeing.
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 19, 2007 737-28A1201Revision 1: May 28, 2009 1 of 45
3.0
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 19, 2007 737-28A1201Revision 1: May 28, 2009 2 of 45 BOEING SERVICE BULLETIN 737-28A1201
ALERTALERT
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 ........................................ 1 9 B. Concurrent Requirements ...................................... 1 9 C. Reason ................................................ 1 9 D. Description .............................................. 2 0 E. Compliance .............................................. 2 1 F . Approval ............................................... 2 1 G. Manpower .............................................. 2 1 H. Weight and Balance Changes .................................... 2 2 I. Electrical Load Data ......................................... 2 2 J. References .............................................. 2 3
1. Existing Data: .......................................... 2 3
2. Data supplied with this Service Bulletin: ........................... 2 3
3. Installation Drawings Used in the Preparation of this Service Bulletin: ........... 2 3 K. Publications Affected ......................................... 2 3 L. Interchangeability and Intermixability of Parts ........................... 2 3
2. MATERIAL INFORMATION ........................................ 2 5 A. Material - Price and Availability ................................... 2 5 B. Industry Support Information .................................... 2 5 C. Parts Necessary For Each Airplane ................................. 2 5
1. Kits/Parts: ............................................ 2 5
2. Parts and Materials Supplied by the Operator: ........................ 2 5
3. Parts Modified and Reidentified: ................................ 2 5
4. Parts Removed and Not Replaced: .............................. 2 9 D. Parts Necessary to Change Spares ................................. 2 9 E. Special Tooling - Price and Availability ............................... 2 9 F . Special Tooling Necessary to do this Service Bulletin ....................... 2 9
3. ACCOMPLISHMENT INSTRUCTIONS .................................. 3 1 A. GENERAL INFORMATION ..................................... 3 1 B. WORK INSTRUCTIONS ....................................... 3 1 FIGURE 1: P91 POWER DISTRIBUTION PANEL CHANGE ....................... 4 2 FIGURE 2: P92 POWER DISTRIBUTION PANEL CHANGE ....................... 4 4
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 19, 2007 737-28A1201Revision 1: May 28, 2009 3 of 45 BOEING SERVICE BULLETIN 737-28A1201
ALERTALERT
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 19, 2007 737-28A1201Revision 1: May 28, 2009 4 of 45 BOEING SERVICE BULLETIN 737-28A1201
ALERTALERT
BLANK PAGE
Commercial Airplanes 737 Service Bulletin ALERT Revision Transmittal SheetNumber: 737-28A1201Original Issue: February 19, 2007 Revision 1: May 28, 2009 ATA System: 2820 SUBJECT: FUEL - Engine Fuel Feed System - Fuel Pump Control Ground Fault Interrupter (GFI) Relay 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 2007-NM-320-AD, is related to this service bulletin.
More work is required for airplanes that have done the initial release of this service bulletin. Operators must measure the electrical resistance between the GFI relays mounting flange and a point on the panel cross member of the P91 and P92 Panels. in accordance with Honeywell SB 1151932-24-61, Revision 5, dated Jan 22/2009 and Honeywell SB 1151934-24-62, Revision 5, dated Jan 22/2009. For more information see Paragraph 3.B, WORK INSTRUCTIONS, Group 1, Configuration 2, Part 2.
REASON FOR REVISION This revision is sent to tell operators that supplier service bulletins, Honeywell ASCa Inc. 1151932-24-61, Revision 5, dated Jan 22/2009 and 1151934-24-62, Revision 5, dated Jan 22/2009 were changed to add a resistance check between the GFI relays mounting flange and a point on the panel cross member of the P91 and P92 Panels. Operators that have done the initial release of this service bulletin must measure the electrical resistance between the GFI relays mounting flange and a point on the panel cross member of the P91 and P92 Panels in accordance with the latest version of these supplier service bulletins.
Two new configurations were added to Group 1. Configuration 1 is now all the airplanes that are applicable to this service bulletin that have not yet done this service bulletin. Configuration 2 is now all the applicable airplanes to this service bulletin that have done this service bulletin by the initial release.
These sections were changed:
1. SUMMARY Revised the SUMMARY , COMPLIANCE, to add NPRM 2007-NM-320-AD and to revise the compliance time to within 60 months of the date on revision 1 of this service bulletin.
Revised the SUMMARY , ACTION, to add a Part 1 and Part 2 Work Instructions.
2. PLANNING INFORMATION
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 19, 2007 737-28A1201Revision 1: May 28, 2009 5 of 45
Revised Paragraph 1.A., Effectivity to add new Configuration 1 and 2 to GROUP 1 in the group configuration table Revised Paragraph 1.C., Reason to add a list of changes for Revision 1 of this service bulletin Revised Paragraph 1.D., Description to add a paragraph to tell operators that more work is required for Configuration 2 airplanes, See Paragraph 3.B., Work Instructions, Part 2 Revised Paragraph 1.E., Compliance to add NPRM-NM-320-AD and to revise the compliance time to within 60 months of the date on revision 1 of this service bulletin.
3. ACCOMPLISHMENT INSTRUCTIONS Revised Paragraph 3.A., General Information Note 3 to change "as given in" to "in accordance with" Revised Paragraph 3.B., Work Instructions to add a new Part 1 for all Group1, Configuration 1 airplanes Revised Paragraph 3.B., Work Instructions to add a new Part 2 and a new step 1 to measure resistance between the GFI relays mounting flange and a point on the panel cross member of the P91 and P92 Panels, for Group 1, Configuration 2 airplanes.
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 February 19, 2007Original Issue:
May 28, 2009Revision 1:
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 19, 2007 737-28A1201Revision 1: May 28, 2009 6 of 45 BOEING SERVICE BULLETIN 737-28A1201
ALERTALERT
Commercial Airplanes 737 Service Bulletin ALERT SummaryNumber: 737-28A1201Original Issue: February 19, 2007 Revision 1: May 28, 2009 ATA System: 2820 SUBJECT: FUEL - Engine Fuel Feed System - Fuel Pump Control Ground Fault Interrupter (GFI) Relay 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 Honeywell Service Bulletins 1151932-24-61, Revision 5, dated Jan 22/2009 and 1151934-24-62, Revision 5, dated Jan 22/2009 are necessary to be accomplished prior to or concurrent with this service bulletin.
BACKGROUND This service bulletin gives the instructions to replace the power control relays for the fuel boost pump and override pumps. The relays are located in the P91 and P92 power distribution panels. The new relays include a ground fault interrupt (GFI) feature.The GFI feature will protect the fuel pumps from damage caused by electrical arcing.
Electrical arcing could create a possible source of ignition of flammable fuel vapors in the fuel tanks. Ignition of flammable fuel vapors could cause a fire or explosion which could put the airplane in an unsafe condition.
This change affects section 9 of the Maintenance Planning Data (MPD) Document. New Airworthiness Limitations (AWL) "28-AWL-20" will be added to section 9 of the MPD to include a functional check of the ground fault interrupt (GFI) relays for the fuel boost pumps and override pumps.
This service bulletin is the result of the safety assessments conducted by Boeing under SFAR 88, "Fuel Tank System Fault Tolerance Evaluation Requirements".
ACTION (PRR 38545-10S) PART 1 In the electrical/electronics compartment, get access to the P91 and P92 power distribution panels. Change the P91 and P92 power distribution panels as shown in the Honeywell Service Bulletins 1151932-24-61, Revision 5, dated Jan 22/2009 and 1151934-24-62, Revision 5, dated Jan 22/2009. Do an operational test of the GFI relays installed in the P91 and P92 panels.
PART 2
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 19, 2007 737-28A1201Revision 1: May 28, 2009 7 of 45
Measure the resistance in accordance with supplier service bulletin Honeywell ASCa Inc. 1151932-24-61, Revision 5, dated Jan 22/2009, and 1151934-24-62, Revision 5, dated Jan 22/2009.
EFFECTIVITY 737-600/700/700C/800/900 airplanes line numbers 1 - 1980, 1982 - 2092, 2094 - 2209. Refer to Paragraph
1.A.1., Airplanes for the list of affected airplanes.
COMPLIANCE Federal Aviation Administration (FAA) Notice of Proposed Rule Making 2007-NM-320-AD, is related to this service bulletin.
Boeing recommends that operators do this change within 60 months of the date on Revision 01 of this service bulletin.
INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the configuration changes given in this service bulletin.
MANPOWER Elapsed HoursTotal Task Hours
3.503.50
MATERIAL INFORMATION Operator Supplied Parts/Materials.
Refer to Paragraph 2.A., Material - Price and Availability.
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 19, 2007 737-28A1201Revision 1: May 28, 2009 8 of 45 BOEING SERVICE BULLETIN 737-28A1201
ALERTALERT
BOEING SERVICE BULLETIN 737-28A1201
ALERT ALERT CHANGE THE P91 AND P92
POWER DISTRIBUTION PANELS
ELECTRICAL AND
ELECTRONICS ELECTRONIC
COMPARTMENT
EQUIPMENT
SEE ACCESS DOOR, 117A 0000
ELECTRONIC EQUIPMENT ACCESS DOOR, 117A
ELECTRICAL AND ELECTRONICS COMPARMENT J65466 Original Issue: February 19, 2007 Revision 1: May 28, 2009 737-28A1201
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 9 of 45
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 19, 2007 737-28A1201Revision 1: May 28, 2009 10 of 45 BOEING SERVICE BULLETIN 737-28A1201
ALERTALERT
BLANK PAGE
Commercial Airplanes 737 Service Bulletin ALERT Number: 737-28A1201 Original Issue: February 19, 2007 Revision 1: May 28, 2009 ATA System: 2820 SUBJECT: FUEL - Engine Fuel Feed System - Fuel Pump Control Ground Fault Interrupter (GFI) Relay 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 Refer to Service Bulletin Index Document D6-19567 Part 3 for Airplane Variable Number, Line Number, and Serial Number data.
This service bulletin is for the airplanes shown below. An equivalent change is on subsequent production airplanes. Refer to PRR38545-10S for data about this change.
DESCRIPTIONCONFIGURATIONGROUP 737-600/700/700C/800/900 Airplanes Line Numbers 1 - 1980, 1982-2092, 2094-2209.
-1 All applicable airplanes that have not done this service bulletin.1 All applicable airplanes that have done the initial release of this service bulletin.
2 Airplane Models:
737-600, 737-700, 737-700C, 737-800, 737-900 GroupVariable Number 1YA001 - YA099 1YA101 - YA199
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 19, 2007 737-28A1201Revision 1: May 28, 2009 11 of 45
GroupVariable Number 1YA201 - YA211 1YA221 1YA231 - YA242 1YA251 - YA256 1YA271 - YA272 1YA291 1YA301 - YA302 1YA311 - YA314 1YA321 - YA323 1YA336 - YA345 1YA351 1YA356 - YA357 1YA366 - YA367 1YA371 - YA377 1YA501 - YA536 1YA541 - YA552 1YA571 - YA578 1YA601 - YA615 1YA621 - YA622 1YA626 - YA631 1YA635 - YA636 1YA641 - YA642 1YA645 - YA650 1YA656 - YA659 1YA666 - YA667 1YA671 - YA672 1YA681 - YA691 1YA701 - YA710 1YA721 - YA722 1YA731 - YA734 1YA751 - YA756 1YA801 - YA803 1YA809
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 19, 2007 737-28A1201Revision 1: May 28, 2009 12 of 45 BOEING SERVICE BULLETIN 737-28A1201