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Commercial Airplanes 767 Service Bulletin ALERT Number: 767-53A0268 Original Issue: April 01, 2015 ATA System: 5363 SUBJECT: FUSELAGE - Section 48 - STA 1582 Aft Pressure Bulkhead Web Inspection at Web to Pressure Chord Joint 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Unpublished Work.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: April 01, 2015 767-53A0268 1 of 35
3.0
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: April 01, 2015 767-53A0268 2 of 35 BOEING SERVICE BULLETIN 767-53A0268
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Table of Contents
Summary5
1. PLANNING INFORMATION9
A. Effectivity9
1. Airplanes9
2. Spares Affected ........................................ 1 6 B. Concurrent Requirements ...................................... 1 6 C. Reason ................................................ 1 6 D. Description .............................................. 1 7 E. Compliance .............................................. 1 7 F. Approval ............................................... 2 0 G. Manpower .............................................. 2 1 H. Weight and Balance Changes .................................... 2 1 I. Electrical Load Data ......................................... 2 1 J. References .............................................. 2 2
1. Existing Data: ......................................... 2 2
2. Data Supplied with this Service Bulletin: ........................... 2 2
3. Installation Drawings Used in the Preparation of this Service Bulletin: ........... 2 2 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. Kits/Parts ............................................ 2 3
2. Parts and Materials Supplied by the Operator ........................ 2 3
3. Parts Modified and Reidentified ................................ 2 3
4. Parts Removed and Not Replaced .............................. 2 3 D. Parts Necessary to Change Spares ................................. 2 3 E. Special Tooling - Price and Availability ............................... 2 3 F. Special Tooling Necessary to do this Service Bulletin ....................... 2 3
3. ACCOMPLISHMENT INSTRUCTIONS .................................. 2 5 A. GENERAL INFORMATION ..................................... 2 5 B. WORK INSTRUCTIONS ....................................... 2 6 FIGURE 1: HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION OF THE AFT PRESSURE BULKHEAD WEB ....................................... 2 8 APPENDIX A: LOGIC DIAGRAM FOR PARAGRAPH 1.E. COMPLIANCE TABLE 1: INSPECTION FOR ANY CRACK AT STA 1582 AFT PRESSURE BULKHEAD [Group 2, Configuration 1] ..... 3 0 APPENDIX B: LOGIC DIAGRAM FOR PARAGRAPH 1.E. COMPLIANCE TABLE 2: INSPECTION FOR ANY CRACK AT STA 1582 AFT PRESSURE BULKHEAD [Group 3, Configuration 1] ..... 3 2 APPENDIX C: LOGIC DIAGRAM FOR PARAGRAPH 1.E. COMPLIANCE TABLE 3: INSPECTION FOR ANY CRACK AT STA 1582 AFT PRESSURE BULKHEAD [Group 1; Group 2-3, Configuration 2] .................................................. 3 4 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: April 01, 2015 767-53A0268 3 of 35 BOEING SERVICE BULLETIN 767-53A0268
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Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: April 01, 2015 767-53A0268 4 of 35 BOEING SERVICE BULLETIN 767-53A0268
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Commercial Airplanes 767 Service Bulletin ALERT SummaryNumber: 767-53A0268Original Issue: April 01, 2015 ATA System: 5363 SUBJECT: FUSELAGE - Section 48 - STA 1582 Aft Pressure Bulkhead Web Inspection at Web to Pressure Chord Joint
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 Widespread Fatigue Damage (WFD) analysis of the 767, as required by 14 CFR 26.21(b), has resulted in the conclusion that existing MPD Section 9, Airworthiness Limitation Item (ALI) inspection program is not sufficient to preclude the occurrence of WFD in the aft pressure bulkhead to pressure chord joint as the airplane ages.
The aft pressure bulkhead web to pressure chord joint has multiple adjacent identical details which have the potential for Multi-Site Damage (MSD) and the potential for WFD. 14 CFR 26.21 requires evaluation of such designs for the potential for WFD and implementation of the appropriate service actions to ensure that WFD is precluded before the Limit of Validity (LOV). Boeing has not received any reports of cracks in the bulkhead web to pressure chord joint. Accomplishment of the inspection described in this service bulletin will enable detection and repair of cracks if they should occur, at the STA 1582 Aft Pressure Bulkhead Web to Pressure Chord joint.
If Widespread Fatigue cracking is not found and repaired, the cracks can rapidly link up and can result in possible rapid decompression and loss of structural integrity.
The aft pressure bulkhead web to pressure chord joint affected by this service bulletin has been determined to be structure that is susceptible to WFD.
Boeing Service Related Problem (SRP) 767-SRP-53-0469 is related to this service bulletin.
Boeing 767 MPD 622T001-9 Section 9, SSI 53-80-l01A is related to this service bulletin.
Boeing Service Bulletin 767-53A0087 is related to this service bulletin.
Boeing Service Bulletin 767-53A0139 is related to this service bulletin.
This table is provided to operators for planning purposes only. Refer to the applicable sections for more information.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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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 AffectedNoPublications 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/PartsNoKits/Parts Required Paragraph 2.C.2., Parts and Materials Supplied by the Operator NoOperator Supplied Parts/Material Paragraph 2.F., Special Tooling Necessary to do this Service Bulletin NoSpecial Tooling Required ACTION Get access to the forward side of the aft pressure bulkhead at STA 1582. Remove the aft galley and the main water tank(s) in the lower lobe. Do a Surface High Frequency Eddy Current (HFEC) inspection of all visible locations of the aft pressure bulkhead web at the aft/inboard row of fasteners common to the aft pressure bulkhead web and pressure chord around the entire circumference of the pressure chord for any crack. If any crack is found, contact Boeing to get instructions for the repair for this service bulletin, and do the work instructed by Boeing. If no crack is found, repeat the inspection.
EFFECTIVITY All 767-200 and 767-300 Airplanes. Refer to Paragraph 1.A.1., Airplanes, for the list of affected airplane(s).
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.
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.
Federal Aviation Administration (FAA) Airworthiness Directive AD 2012-09-08 is related to this service bulletin.
The effective date of AD 2012-09-08 is June 18, 2012.
Federal Aviation Administration (FAA) Airworthiness Directive AD 2014-14-04 is related to this service bulletin.
The effective date of AD 2014-14-04 is September 5, 2014.
This service bulletin affects SSI 53-80-I01A of 767 MPD 622T001-9 Section 9, which is mandated by AD 2014-14-04. All other MPD inspections outside the of the affected area are not affected and must continue.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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Refer to Paragraph 1.E., Compliance.
INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the inspection given in this service bulletin.
MANPOWER Elapsed HoursTotal Task HoursAirplanes
17.2555.00Group 1, 2 and 3 Airplanes with one water tank removal required
17.7557.00Group 1, 2 and 3 Airplanes with two water tank removals required Refer to Paragraph 1.G., Manpower.
MATERIAL INFORMATION None.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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BOEING SERVICE BULLETIN 767-53A0268
ALERT ALERT
• BULKHEAD WEB
POSSIBLE
WEB CRACK
TYPICAL
INSPECTION
AREA - RIVETS STA 1582
TYPICAL RADIAL
STIFFENER INNER CHORD
PRESSURE RING
PRESSURE CHORD INBD
FAILSAFE FRAME CHORD
FWD TYPICAL INSPECTION AREA FWD NOTE:
SOME AFFECTED AIRPLANE CONFIGURATIONS
HAVE SHORT STIFFENERS AT THE AFT PRESSURE BULKHEAD TO PRESSURE CHORD JOINT.
SHORT STIFFENERS ARE NOT SHOWN FOR CLARITY.
DO A HIGH FREQUENCY EDDY CURRENT INSPECTION
OF THE WEB AT THE INDICATED FASTENERS
COMMON TO THE AFT PRESSURE BULKHEAD WEB
AND PRESSURE CHORD AROUND THE ENTIRE CIRCUMFERENCE OF THE PRESSURE CHORD. IF ANY CRACK IS FOUND, CONTACT BOEING TO GET 2377532
INSTRUCTIONS FOR THIS SERVICE BULLETIN AND DO THE WORK INSTRUCTED BY BOEING.
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Commercial Airplanes 767 Service Bulletin ALERT Number: 767-53A0268 Original Issue: April 01, 2015 ATA System: 5363 SUBJECT: FUSELAGE - Section 48 - STA 1582 Aft Pressure Bulkhead Web Inspection at Web to Pressure Chord Joint
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 applicable to all 767-200 and 767-300 Airplanes in 3 Group(s). The Variable Numbers and Group Information for the applicable airplanes is given below.
Refer to Service Bulletin Index D624T001 Part 3 for Airplane Variable Number, Line Number, and Serial Number data.
NOTE: The Variable Number table below includes all affected airplanes up to Line Number 1068.
Affected airplanes after Line Number 1068 will be added to the service bulletin's MyBoeingFleet.com (MBF) "get effectivity" result when they are added to the MBF Fleet Profile Page.
DESCRIPTIONCONFIGURATIONGROUP Airplanes Line Numbers 1-175 with replaced aft pressure bulkhead in accordance with SB 767-53A0139.
-1 Airplanes Line Numbers 176-423.-2 Airplanes with original production aft pressure bulkhead installed.1 Airplanes with aft pressure bulkhead replaced in accordance with a Boeing Organization Design Authorization (ODA) approval via FAA Form 8100-9.
2 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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DESCRIPTIONCONFIGURATIONGROUP Airplanes Line Numbers 424 and on (767-200/300 only).-3 Airplanes with original production aft pressure bulkhead installed.1 Airplanes with aft pressure bulkhead replaced in accordance with a Boeing Organization Designation Authorization (ODA) approval via FAA Form 8100-9.
2 Airplane Models:
767-200, 767-300 GroupVariable Number 1VA001 - VA020 1VA301 - VA315 1VA501 - VA526 2VA527 - VA530 1VA701 - VA712 2VA713 - VA719 1VA801 - VA810 1VB001 - VB002 1VB051 - VB055 1VB101 - VB125 1VB201 - VB202 1VB251 - VB253 1VB281 - VB284 1VB301 - VB302 1VB321 - VB324 2VB325 - VB332 1VB371 - VB373 1VB401 3VB441 - VB444 1VE001 - VE002 2VE003 1VE021 - VE023 1VE041 - VE043 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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GroupVariable Number 1VE061 - VE068 2VE069 1VE083 - VE084 2VE085 - VE086 1VE101 - VE103 2VE104 1VE116 - VE117 2VE118 1VE121 - VE123 2VE124 - VE126 1VE141 - VE142 2VE143 - VE151 3VE152 2VE171 - VE172 2VF001 - VF002 2VF041 - VF042 2VF051 2VF061 - VF062 2VF071 - VF072 2VF091 - VF093 2VF101 - VF102 2VF161 3VF162 3VF171 - VF172 3VF180 - VF184 3VF251 1VK001 - VK004 2VK005 - VK011 3VK012 - VK016 2VK021 - VK022 1VK031 - VK037 2VK038 - VK053 3VK054 - VK056 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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GroupVariable Number 2VK081 - VK099 3VK100 - VK113 2VK131 - VK133 2VK141 - VK142 3VK143 - VK148 3VK161 - VK164 3VK171 3VK181 3VK186 1VL001 2VL002 - VL006 1VL011 3VL701 - VL703 3VL751 - VL755 3VL806 - VL807 3VL871 - VL873 3VL891 - VL900 3VL911 - VL914 3VL931 - VL932 3VL941 2VN001 - VN019 3VN020 - VN041 2VN051 - VN062 3VN063 - VN064 2VN081 - VN092 3VN093 - VN099 2VN111 - VN124 3VN125 - VN127 2VN130 - VN132 3VN133 - VN137 2VN151 - VN158 2VN163 - VN168 2VN171 - VN173 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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