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 = '86d9e3d6cf0e2dfe4aabf353a1e2da0784d09a3e9901aacbcc37ee4e92a3b1ab' 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 = '86d9e3d6cf0e2dfe4aabf353a1e2da0784d09a3e9901aacbcc37ee4e92a3b1ab' 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 767 Service Bulletin ALERT Number: 767-53A0267 Original Issue: August 13, 2015 Revision 1: August 04, 2016 ATA System: 5380 SUBJECT: FUSELAGE - Aft Pressure Bulkhead - Replacement of Station 1582 Aft Pressure Bulkhead 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 © 2015 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Unpublished Work.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: August 13, 2015 767-53A0267Revision 1: August 04, 2016 1 of 206
2.0
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 13, 2015 767-53A0267Revision 1: August 04, 2016 2 of 206 BOEING SERVICE BULLETIN 767-53A0267
ALERTALERT
BLANK PAGE
Table of Contents
Revision Transmittal Sheet5
S u m m a r y7
1. PLANNING INFORMATION ........................................ 1 1 A . E f f e c t i v i t y ............................................... 1 1
1. Airplanes ............................................ 1 1 2 . S p a r e s A f f e c t e d ........................................ 1 3 B. Concurrent Requirements ...................................... 1 3 C. Reason ................................................ 1 4 D. Description .............................................. 1 4 E. Compliance .............................................. 1 5 F . A p p r o v a l ............................................... 1 5 G. Manpower .............................................. 1 6 H. Weight and Balance Changes .................................... 1 8 I. Electrical Load Data ......................................... 1 8 J . R e f e r e n c e s .............................................. 1 8
1. Existing Data: ......................................... 1 8
2. Data Supplied with this Service Bulletin: ........................... 1 8
3. Installation Drawings Used in the Preparation of this Service Bulletin: ........... 2 1 K. Publications Affected ........................................ 2 2 L. Interchangeability and Intermixability of Parts ........................... 2 2 M. Software Accomplishment Summary ................................ 2 2
2. MATERIAL INFORMATION ........................................ 2 3 A. Material - Price and Availability ................................... 2 3 B. Industry Support Information .................................... 2 3 C. Parts Necessary for Each Airplane ................................. 2 3 1 . K i t s / P a r t s ............................................ 2 3
2. Parts and Materials Supplied by the Operator ........................ 3 4
3. Parts Modified and Reidentified ................................ 3 5
4. Parts Removed and Not Replaced .............................. 3 5 D. Parts Necessary to Change Spares ................................. 3 5 E. Special Tooling - Price and Availability ............................... 3 5 F. Special Tooling Necessary to do this Service Bulletin ....................... 3 8
3. ACCOMPLISHMENT INSTRUCTIONS .................................. 3 9 A. GENERAL INFORMATION ..................................... 3 9 B. WORK INSTRUCTIONS ....................................... 4 0 FIGURE 1: AFT PRESSURE BULKHEAD ASSEMBLY PREPARATION ................ 5 5 FIGURE 2: AFT PRESSURE BULKHEAD ASSEMBLY PREPARATION ................ 6 0 FIGURE 3: REMOVAL OF AUXILIARY PITOT SYSTEM TUBES AND SEALS ............. 6 2 FIGURE 4: REMOVAL OF PRESSURE SEALS .............................. 6 6 FIGURE 5: APU FUEL LINE BULKHEAD FITTING REMOVAL ..................... 6 9 FIGURE 6: APU FUEL LINE BULKHEAD FITTING INSTALLATION ................... 7 2 FIGURE 7: AFT SECTION 48 (TAIL CONE) FASTENER REMOVAL .................. 7 5 FIGURE 8: STA 1809.5 CENTER BULKHEAD REMOVAL ........................ 7 8 FIGURE 9: FORWARD SECTION 48 PARTS REMOVAL ........................ 8 5 F I G U R E 1 0 : A F T P R E S S U R E B U L K H E A D P R E S S U R E R I N G F A S T E N E R R E M O V A L ......... 8 7 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 13, 2015 767-53A0267Revision 1: August 04, 2016 3 of 206 BOEING SERVICE BULLETIN 767-53A0267
ALERTALERT
FIGURE 11: AFT PRESSURE BULKHEAD ATTACHMENT TO THE PRESSURE RING AT STA 1582 . 89 FIGURE 12: FORWARD SECTION 48 INSTALLATION .......................... 9 1 FIGURE 13: LEFT STA 1809.5 CENTER BULKHEAD INSTALLATION ................. 1 1 0 FIGURE 14: RIGHT STA 1809.5 CENTER BULKHEAD INSTALLATION ................ 1 2 2 FIGURE 15: AFT SECTION 48 (TAIL CONE) INSTALLATION ...................... 1 3 4 FIGURE 16: PRESSURE SEAL INSTALLATION ............................. 1 3 9 FIGURE 17: INSTALLATION OF AUXILIARY PITOT SYSTEM TUBES AND PRESSURE SEALS . . 142 FIGURE 18: MAKE AND INSTALL STA 1809.5 BULKHEAD STABILIZATION TOOLS ......... 1 4 6 FIGURE 19: REMOVE STA 1809.5 BULKHEAD STABILIZATION TOOLS ............... 1 5 6 FIGURE 20: STA 1582 FLOOR BEAM DETACHMENT .......................... 1 5 8 FIGURE 21: STA 1582 FLOOR BEAM SUPPORT ............................ 1 6 2 FIGURE 22: STA 1582 FLOOR BEAM ATTACHMENT .......................... 1 6 5 FIGURE 23: LEFT SIDE HORIZONTAL STABILIZER FAIRING SKIN REMOVAL ........... 1 7 0 FIGURE 24: LEFT SIDE HORIZONTAL STABILIZER FAIRING SKIN INSTALLATION ......... 1 7 3 FIGURE 25: RIGHT SIDE HORIZONTAL STABILIZER FAIRING SKIN REMOVAL ........... 1 7 7 FIGURE 26: RIGHT SIDE HORIZONTAL STABILIZER FAIRING SKIN INSTALLATION ........ 1 8 0 FIGURE 27: PREPARATION OF THE VERTICAL FIN .......................... 1 8 3 FIGURE 28: INSTALLATION OF THE VERTICAL FIN .......................... 1 9 0 APPENDIX A: APU WIRING TEST PROCEDURE ............................. 1 9 9 APPENDIX B: ALIGNMENT PINS ...................................... 2 0 4 APPENDIX C: LOGIC DIAGRAM FOR PARAGRAPH 1.E. COMPLIANCE: TABLE 1: REPLACEMENT OF THE STA 1582 AFT PRESSURE BULKHEAD .......................... 2 0 5 APPENDIX D: PART DEMAND INTENT ................................... 2 0 6 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 13, 2015 767-53A0267Revision 1: August 04, 2016 4 of 206 BOEING SERVICE BULLETIN 767-53A0267
ALERTALERT
Commercial Airplanes 767 Service Bulletin ALERT Revision Transmittal SheetNumber: 767-53A0267Original Issue: August 13, 2015 Revision 1: August 04, 2016 ATA System: 5380 SUBJECT: FUSELAGE - Aft Pressure Bulkhead - Replacement of Station 1582 Aft Pressure Bulkhead This revision includes all pages of the service bulletin.
COMPLIANCE INFORMATION RELATED TO THIS REVISION None.
REASON FOR REVISION Revision 1 is sent to replace kit number 015T1812-2 with 015T1907-1, and add five airplanes to the effectivity that were inadvertently omitted at initial release.
These sections were changed:
1. 1.A. Effectivity, added airplane Variable Numbers VN018, VN092, VN191, VN371, and VN537.
2. 1.K.1 Publications Affected - Publications, included additional publications that are affected by this service bulletin.
3. 2.A. Material - Price and Availability, updated kit number and Re-Order Lead Time (ROLT) information.
4. 2.C.1 Kits/Parts, replaced kit 015T1812-2 with kit number 015T1907-1.
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.
Pages with no vertical lines have no changes.
REVISION HISTORY August 13, 2015Original Issue:
August 04, 2016Revision 1:
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 13, 2015 767-53A0267Revision 1: August 04, 2016 5 of 206
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 13, 2015 767-53A0267Revision 1: August 04, 2016 6 of 206 BOEING SERVICE BULLETIN 767-53A0267
ALERTALERT
BLANK PAGE
Commercial Airplanes 767 Service Bulletin ALERT SummaryNumber: 767-53A0267Original Issue: August 13, 2015 Revision 1: August 04, 2016 ATA System: 5380 SUBJECT: FUSELAGE - Aft Pressure Bulkhead - Replacement of Station 1582 Aft Pressure Bulkhead
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 This service bulletin gives instruction for the replacement of the Station (STA) 1582 aft pressure bulkhead due to Widespread Fatigue Damage (WFD). The WFD analysis of the 767, as required by 14 CFR 26.21(b), has resulted in the conclusion that the existing MPD Section 9, Airworthiness Limitation Item (ALI) inspection program is not sufficient to preclude the occurrence of WFD in the aft pressure bulkhead before the Limit of Validity (LOV) as the airplane ages. If widespread fatigue cracking at aft pressure bulkhead radial web lap splices is not found and repaired, the cracks can rapidly link up and become large, and can result in possible rapid decompression and loss of structural integrity.
Boeing has not received any reports of cracks in the aft pressure bulkhead web on line number 176 through
423.
The Aft Pressure Bulkhead has been determined to be structure that is susceptible to Widespread Fatigue Damage (WFD).
Federal Aviation Administration (FAA) AD 2012-09-08 was released to mandate replacement of the initial configuration aft pressure bulkhead which was installed on line number 1 through 175 per service bulletin 767-53A0139. Design changes were made to improve the durability of the bulkhead in production at line number 176, and again at line number 424. However, the configuration of aft pressure bulkheads installed on line number 176 through 423, have the same web gage of 0.032 inch as the initial configuration aft pressure bulkhead and does not provide adequate strength to preclude WFD before the Limit of Validity (LOV).
Boeing Service Related Problem (SRP) 767-SRP-53-0469 is related to this service bulletin.
Accomplishment of the aft pressure bulkhead replacement given in this service bulletin will end the inspections at aft pressure bulkhead web for indications of "oil cans" and previous "oil can" repairs currently required by Boeing Service Bulletin 767-53A0105 and AD 2004-14-19.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 13, 2015 767-53A0267Revision 1: August 04, 2016 7 of 206
Accomplishment of the aft pressure bulkhead replacement given in this service bulletin will end the repeat inspections at aft pressure bulkhead web lap splices currently required by Boeing Service Bulletin 767-53A0147 and AD 2009-06-19.
Accomplishment of the aft pressure bulkhead replacement given in this service bulletin will also end the repeat inspections of web at pressure chord joint currently required by Boeing Service Bulletin 767-53A0087 and AD 2004-05-16.
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 ChangesYesWeight and Balance Change Paragraph 1.I., Electrical Load DataNoElectrical Load Changed Paragraph 1.K., Publications AffectedYesPublications Affected 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 YesSpecial Tooling Required ACTION Remove equipment for access to the forward and aft sides of the STA 1582 aft pressure bulkhead. Remove the vertical fin, the tail cone (with the APU installed), the left and right STA 1809.5 center bulkhead, and the horizontal stabilizer. Disconnect and remove the forward portion of Section 48 (with the aft pressure bulkhead attached) from Section 46 at STA 1582. Remove the aft pressure bulkhead from Section 48 and install a new aft pressure bulkhead in accordance with this service bulletin. Attach the modified forward part of Section 48 to Section 46 at STA 1582. Reinstall the horizontal stabilizer and reassemble the STA 1809.5 bulkhead. Reinstall the tail cone and the vertical fin. Install the equipment that was removed for access to the aft pressure bulkhead. Test disturbed systems in accordance with this service bulletin.
EFFECTIVITY 767-200 and 767-300 Airplanes. 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.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 13, 2015 767-53A0267Revision 1: August 04, 2016 8 of 206 BOEING SERVICE BULLETIN 767-53A0267
ALERTALERT
Federal Aviation Administration (FAA) Airworthiness Directive AD 2004-14-19 is related to this service bulletin.
The effective date of AD 2004-14-19 is August 20, 2004.
Federal Aviation Administration (FAA) Airworthiness Directive AD 2009-06-19 is related to this service bulletin.
The effective date of AD 2009-06-19 is April 28, 2009.
Federal Aviation Administration (FAA) Airworthiness Directive AD 2004-05-16 is related to this service bulletin.
The effective date of AD 2004-05-16 is April 13, 2004.
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 Boeing Supplied Kits/Parts.
Refer to Paragraph 2.A., Material - Price and Availability.
Operators are encouraged to complete the survey provided in APPENDIX D 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: August 13, 2015 767-53A0267Revision 1: August 04, 2016 9 of 206 BOEING SERVICE BULLETIN 767-53A0267
ALERTALERT
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 13, 2015 767-53A0267Revision 1: August 04, 2016 10 of 206 BOEING SERVICE BULLETIN 767-53A0267
ALERTALERT
BLANK PAGE
Commercial Airplanes 767 Service Bulletin ALERT Number: 767-53A0267 Original Issue: August 13, 2015 Revision 1: August 04, 2016 ATA System: 5380 SUBJECT: FUSELAGE - Aft Pressure Bulkhead - Replacement of Station 1582 Aft Pressure Bulkhead
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 D624T001 Part 3 for Airplane Variable Number, Line Number, and Serial Number data.
This service bulletin is applicable to 767-200 and -300 Airplanes, line numbers 176 - 423 in 3 Groups. The Variable Numbers and Group Information for the applicable airplanes are given below.
DESCRIPTIONCONFIGURATIONGROUP Airplane Line numbers 176-401 with Non-Dual bottle fire extinguisher-1 Airplane Line numbers 186-416 with APC Dual Bottle fire extinguisher-2 Airplane Line numbers 202-423 which have dedicated Static pressure inputs -3 Airplane Models:
767-200, 767-300 GroupVariable Number 1VA527 - VA530 1VA713 - VA719 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 13, 2015 767-53A0267Revision 1: August 04, 2016 11 of 206
GroupVariable Number 1VB325 2VB326 1VB327 - VB332 1VE003 1VE069 1VE085 - VE086 1VE104 1VE118 1VE124 - VE126 1VE143 - VE151 1VE171 - VE172 3VF001 - VF002 3VF041 - VF042 3VF051 3VF061 - VF062 3VF071 - VF072 3VF091 - VF093 3VF101 - VF102 2VF161 2VK005 - VK011 2VK021 - VK022 2VK038 - VK053 1VK081 - VK099 1VK131 - VK133 1VK141 - VK142 2VL002 - VL006 3VN001 - VN019 3VN051 - VN062 3VN081 - VN092 3VN111 - VN124 3VN130 - VN132 3VN151 - VN158 3VN163 - VN168 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 13, 2015 767-53A0267Revision 1: August 04, 2016 12 of 206 BOEING SERVICE BULLETIN 767-53A0267