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 = 'd040bf682d1ed47cae6437e743ef159aedc0854037c7304498180d9bb75f395f' 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 = 'd040bf682d1ed47cae6437e743ef159aedc0854037c7304498180d9bb75f395f' 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 707 Service Bulletin ALERT Number: A3542 Original Issue: February 12, 2016 ATA System: 5232 SUBJECT: DOORS - Main Cargo Door - Cam Support Assembly Inspection and Replacement 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 © 2016 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Unpublished Work.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: February 12, 2016 A3542 1 of 67
4.0
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 12, 2016 A3542 2 of 67 BOEING SERVICE BULLETIN A3542
ALERTALERT
BLANK PAGE
Table of Contents
S u m m a r y5
1. PLANNING INFORMATION9
A . E f f e c t i v i t y9
1. Airplanes9
2 . S p a r e s A f f e c t e d ........................................ 1 1 B. Concurrent Requirements ...................................... 1 1 C. Reason ................................................ 1 1 D. Description .............................................. 1 2 E. Compliance .............................................. 1 2 F . A p p r o v a l ............................................... 1 3 G. Manpower .............................................. 1 4 H. Weight and Balance Changes .................................... 1 4 I. Electrical Load Data ......................................... 1 5 J . R e f e r e n c e s .............................................. 1 5
1. Existing Data: ......................................... 1 5
2. Data Supplied with this Service Bulletin: ........................... 1 5
3. Installation Drawings Used in the Preparation of this Service Bulletin: ........... 1 5 K. Publications Affected ........................................ 1 5 L. Interchangeability and Intermixability of Parts ........................... 1 5 M. Software Accomplishment Summary ................................ 1 5
2. MATERIAL INFORMATION ........................................ 1 7 A. Material - Price and Availability ................................... 1 7 B. Industry Support Information .................................... 1 7 C. Parts Necessary for Each Airplane ................................. 1 7 1 . K i t s / P a r t s ............................................ 1 7
2. Parts and Materials Supplied by the Operator ........................ 2 1
3. Parts Modified and Reidentified ................................ 2 1
4. Parts Removed and Not Replaced .............................. 2 1 D. Parts Necessary to Change Spares ................................. 2 1 E. Special Tooling - Price and Availability ............................... 2 1 F. Special Tooling Necessary to do this Service Bulletin ....................... 2 2
3. ACCOMPLISHMENT INSTRUCTIONS .................................. 2 3 A. GENERAL INFORMATION ..................................... 2 3 B. WORK INSTRUCTIONS ....................................... 2 4 FIGURE 1: CAM SUPPORT ASSEMBLY AT STA 487.10 AND 500 - REPLACEMENT ........ 2 6 FIGURE 2: CAM SUPPORT ASSEMBLY AT STA 520, 540, 560, 580 - REPLACEMENT ....... 3 8 FIGURE 3: CAM SUPPORT ASSEMBLY AT STA 600 AND 612.9 - REPLACEMENT ......... 5 0 APPENDIX A: LOGIC DIAGRAM FOR PARAGRAPH 1.E., COMPLIANCE: TABLE 1: MAIN CARGO DOOR CAM SUPPORT ASSEMBLY - INSPECTION ........................ 6 2 APPENDIX B: ADDITIONAL ACCESS .................................... 6 4 APPENDIX C: PART DEMAND INTENT ................................... 6 7 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 12, 2016 A3542 3 of 67 BOEING SERVICE BULLETIN A3542
ALERTALERT
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 12, 2016 A3542 4 of 67 BOEING SERVICE BULLETIN A3542
ALERTALERT
BLANK PAGE
Commercial Airplanes 707 Service Bulletin ALERT SummaryNumber: A3542Original Issue: February 12, 2016 ATA System: 5232 SUBJECT: DOORS - Main Cargo Door - Cam Support Assembly Inspection and Replacement
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 None.
BACKGROUND Boeing analysis of the main cargo door cam support assembly part numbers 69-23588-5 and 69-23588-6 indicated that the existing maintenance program for the support assemblies is not adequate to reliably detect cracks before two adjacent cam support assemblies could fail, which would reduce the structural integrity of the door. The main cargo door is on the upper left side of the forward fuselage between body stations 480 and 620.
The door is hinged on its upper edge and opens outward to a canopy or a fully open position. The main cargo door has eight cam support assemblies along the bottom of the door that support the latch cams. The door latch cams engage with latch pins on the fuselage and hold the door closed. The main cargo door cam support assemblies are subject to ground loads, flight loads, and cabin pressure loads. If the work in this service bulletin is not done, undetected cracks at adjacent support assembly part numbers 69-23588-5 and 69-23588-6, or replacement part numbers 69-23588-9 and 69-23588-10, could result in reduced structural integrity of the main cargo door and consequent rapid decompression of the 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., Compliance and Paragraph
1.F., Approval YesAD Related Paragraph 1.H., Weight and Balance ChangesNoWeight and Balance Change Paragraph 1.I., Electrical Load DataNoElectrical Load Changed Paragraph 1.K., Publications AffectedYesPublications Affected Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 12, 2016 A3542 5 of 67
ReferenceAffectedPlanning Data Paragraph 1.K., Publications AffectedNoAirplane Flight Operations Affected (Flight Crew Operations Manual and/or FAA Approved Airplane Flight Manual) Paragraph 2.C.1., Kits/PartsYesKits/Parts Required Paragraph 2.C.2., Parts and Materials Supplied by the Operator YesOperator Supplied Parts/Material Paragraph 2.F., Special Tooling Necessary to do this Service Bulletin NoSpecial Tooling Required ACTION
1. Do an Ultrasonic Inspection of the grease fitting lug area of affected main cargo door cam support assemblies for any crack.
NOTE: 69-23588-5 and 69-23588-6 are affected part numbers. 69-23588-9 and 69-23588-10 are also affected part numbers if installed.
a. If no crack is found, repeat the Ultrasonic Inspection of the grease fitting lug area of the main cargo door cam support assembly at all locations where an affected part number is installed for any crack at the repeat interval given in Paragraph 1.E., Compliance.
NOTE: 69-23588-5 and 69-23588-6 are affected part numbers. 69-23588-9 and 69-23588-10 are also affected part numbers if installed.
b. If any crack is found, replace the cam support assembly pair at the affected location and repeat the Ultrasonic Inspection of the grease fitting lug area of the main cargo door cam support assembly at all locations where an affected part number is installed for any crack at the repeat interval given in Paragraph 1.E., Compliance.
NOTE: 69-23588-5 and 69-23588-6 are affected part numbers. 69-23588-9 and 69-23588-10 are also affected part numbers if installed.
EFFECTIVITY 707-300B, 707-300C Airplane(s). Refer to Paragraph 1.A.1., Airplanes, for the list of affected airplanes.
COMPLIANCE Refer to Paragraph 1.E., Compliance.
INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the inspection and repair procedures given in this service bulletin.
MANPOWER Refer to Paragraph 1.G., Manpower.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 12, 2016 A3542 6 of 67 BOEING SERVICE BULLETIN A3542
ALERTALERT
MATERIAL INFORMATION Boeing Supplied Kits/Parts.
Refer to Paragraph 2.A., Material - Price and Availability.
Operators are encouraged to complete the survey provided in APPENDIX C of this service bulletin to help Boeing predict the quantity and timing of the Boeing Supplied Kits/Parts.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 12, 2016 A3542 7 of 67 BOEING SERVICE BULLETIN A3542
ALERTALERT
BOEING SERVICE BULLETIN A3542
ALERT ALERT D
DO AN INSPECTION OF THE
CAM SUPPORT ASSEMBLIES
FOR ANY CRACK 2461257 Original Issue: February 12, 2016 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished A3542 Work - See page 1 for details. 8 of 67
Commercial Airplanes 707 Service Bulletin ALERT Number: A3542 Original Issue: February 12, 2016 ATA System: 5232 SUBJECT: DOORS - Main Cargo Door - Cam Support Assembly Inspection and Replacement
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
DESCRIPTIONCONFIGURATIONGROUP 707-300B, 707-300C airplanes with main deck cargo door cam support assemblies, part numbers 69-23588-5 and 69-23588-6, or 69-23588-9 and 69-23588-10, installed.
-1 Airplane Models:
707-300B, 707-300C GroupVariable Number 105602 - 05605 107001 - 07017 107041 - 07059 107071 - 07081 107101 - 07109 107181 107191 107201 - 07215 107251 - 07271 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 12, 2016 A3542 9 of 67
GroupVariable Number 107401 - 07407 107451 - 07458 107501 - 07504 107601 - 07626 107661 - 07662 107681 - 07684 107701 - 07702 107801 - 07821 107901 - 07907 108001 - 08008 108021 108051 - 08056 108071 - 08073 108077 108101 - 08103 108121 - 08129 108141 - 08144 108151 - 08153 108171 - 08173 108191 - 08192 108201 - 08204 108209 108221 - 08224 108241 - 08244 108251 108261 108271 108301 - 08320 108324 - 08330 108333 108401 - 08407 108410 108451 - 08452 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 12, 2016 A3542 10 of 67 BOEING SERVICE BULLETIN A3542
ALERTALERT
GroupVariable Number 108471 - 08475 108501 - 08502 108551 - 08553 108581 - 08582 109002 - 09004 109101 - 09107 109161 - 09167 109202 109223 109227 109231 - 09232 109251 109288 - 09290 109411 109421 109438 109441
2. Spares Affected None.
B. Concurrent Requirements None.
C. Reason Boeing analysis of the main cargo door cam support assembly part numbers 69-23588-5 and 69-23588-6 indicated that the existing maintenance program for the support assemblies is not adequate to reliably detect cracks before two adjacent cam support assemblies could fail, which would reduce the structural integrity of the door. The main cargo door is on the upper left side of the forward fuselage between body stations 480 and 620. The door is hinged on its upper edge and opens outward to a canopy or a fully open position. The main cargo door has eight cam support assemblies along the bottom of the door that support the latch cams. The door latch cams engage with latch pins on the fuselage and hold the door closed. The main cargo door cam support assemblies are subject to ground loads, flight loads, and cabin pressure loads. If the work in this service bulletin is not done, undetected cracks at adjacent support assembly part numbers 69-23588-5 and 69-23588-6, or replacement part numbers 69-23588-9 and 69-23588-10, could result in reduced structural integrity of the main cargo door and consequent rapid decompression of the airplane.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 12, 2016 A3542 11 of 67 BOEING SERVICE BULLETIN A3542
ALERTALERT
D. Description
1. Do an Ultrasonic Inspection of the grease fitting lug area of affected main cargo door cam support assemblies for any crack NOTE: 69-23588-5 and 69-23588-6 are affected part numbers. 69-23588-9 and 69-23588-10 are also affected part numbers if installed.
a. If no crack is found, repeat the Ultrasonic Inspection of the grease fitting lug area of the main cargo door cam support assembly at all locations where an affected part number is installed for any crack at the repeat interval given in Paragraph 1.E., Compliance.
NOTE: 69-23588-5 and 69-23588-6 are affected part numbers. 69-23588-9 and 69-23588-10 are also affected part numbers if installed.
b. If any crack is found, replace the cam support assembly pair at the affected location and repeat the Ultrasonic Inspection of the grease fitting lug area of the main cargo door cam support assembly at all locations where an affected part number is installed for any crack at the repeat interval given in Paragraph 1.E., Compliance.
NOTE: 69-23588-5 and 69-23588-6 are affected part numbers. 69-23588-9 and 69-23588-10 are also affected part numbers if installed.
The work in this service bulletin is done in the maintenance zone(s) given below.
Affected Maintenance Zones ZoneModel 2-49707-300B, 707-300C 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.
Do the required actions in accordance with Paragraph 3. Accomplishment Instructions.
A logic diagram showing compliance tasks and compliance times is included as an aid in APPENDIX A.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: February 12, 2016 A3542 12 of 67 BOEING SERVICE BULLETIN A3542