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Commercial Airplanes 767 Service Bulletin ALERT Number: 767-53A0266 Original Issue: April 20, 2015 ATA System: 5380 SUBJECT: FUSELAGE - Aft Pressure Bulkhead - STA 1582 Aft Pressure Bulkhead Web Inspection Under Pressure Chord Splice Plate 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Unpublished Work.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 20, 2015 767-53A0266 1 of 41
5.0
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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BLANK PAGE
Table of Contents
Summary5
1. PLANNING INFORMATION9
A. Effectivity9
1. Airplanes9
2. Spares Affected17
B. Concurrent Requirements17
C. Reason17
D. Description17
E. Compliance18
F. Approval20
G. Manpower21
H. Weight and Balance Changes22
I. Electrical Load Data22
J. References22
1. Existing Data:22
2. Data Supplied with this Service Bulletin:23
3. Installation Drawings Used in the Preparation of this Service Bulletin:23
K. Publications Affected23
L. Interchangeability and Intermixability of Parts23
M. Software Accomplishment Summary24
2. MATERIAL INFORMATION25
A. Material - Price and Availability25
B. Industry Support Information25
C. Parts Necessary for Each Airplane25
1. Kits/Parts25
2. Parts and Materials Supplied by the Operator25
3. Parts Modified and Reidentified25
4. Parts Removed and Not Replaced25
D. Parts Necessary to Change Spares25
E. Special Tooling - Price and Availability25
F. Special Tooling Necessary to do this Service Bulletin26
3. ACCOMPLISHMENT INSTRUCTIONS27
A. GENERAL INFORMATION27
B. WORK INSTRUCTIONS28
FIGURE 1: AFT PRESSURE BULKHEAD WEB COMMON TO PRESSURE CHORD SPLICE PLATE - FASTENER REMOVAL AND WEB INSPECTION [Group 2, Configuration 1; Group 3] . . 32 FIGURE 2: AFT PRESSURE BULKHEAD WEB COMMON TO PRESSURE CHORD SPLICE PLATE - FASTENER REMOVAL AND WEB INSPECTION [Group 1; Group 2, Configuration 2; Group 4]
.34
FIGURE 3: AFT PRESSURE BULKHEAD - PRESSURE CHORD SPLICE PLATES - FASTENER
INSTALLATION [Group 2, Configuration 1; Group 3]36
FIGURE 4: AFT PRESSURE BULKHEAD - PRESSURE CHORD SPLICE PLATES - FASTENER
INSTALLATION [Group 1; Group 2, Configuration 2; Group 4]38
APPENDIX A: LOGIC DIAGRAM FOR PARAGRAPH 1.E. COMPLIANCE TABLE 1: AFT PRESSURE BULKHEAD WEB INSPECTIONS AT PRESSURE CHORD JOINT. [Group 2, Configuration 1;
Group 3-4]40
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APPENDIX B: LOGIC DIAGRAM FOR PARAGRAPH 1.E. COMPLIANCE TABLE 2: AFT PRESSURE BULKHEAD WEB INSPECTIONS AT PRESSURE CHORD JOINT. [Group 1; Group 2,
Configuration 2]41
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: April 20, 2015 767-53A0266 4 of 41 BOEING SERVICE BULLETIN 767-53A0266
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Commercial Airplanes 767 Service Bulletin ALERT SummaryNumber: 767-53A0266Original Issue: April 20, 2015 ATA System: 5380 SUBJECT: FUSELAGE - Aft Pressure Bulkhead - STA 1582 Aft Pressure Bulkhead Web Inspection Under Pressure Chord Splice Plate
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 Accomplishment of the inspection described in this service bulletin will enable detection and repair of cracks if they should occur, in the areas under splice plates at the Station (STA) 1582 aft pressure bulkhead web to pressure chord joint. If a crack is present in the aft pressure bulkhead web and not found and repaired, crack growth can result in possible rapid decompression and loss of structural integrity.
The aft pressure bulkhead web is attached to the pressure chords with a double row of fasteners and the pressure chord segments are spliced using pressure chord splice plates. At these splice plate locations, the aft pressure bulkhead web is hidden and cannot be inspected in accordance with existing 767 MPD Section 9 or Service Bulletin (SB) 767-53A0087 and do not provide sufficient crack detection probability of the aft pressure bulkhead web under splice plates.
Boeing Service Related Problem (SRP) 767-SRP-53-0470 is related to this service bulletin.
Boeing SB 767-53A0087 and 767-53A0139 are related to this service bulletin.
Boeing 767 MPD SSI 53-80-I01A is related to this service bulletin.
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 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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ReferenceAffectedPlanning Data 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 YesOperator Supplied Parts/Material Paragraph 2.F., Special Tooling Necessary to do this Service Bulletin NoSpecial Tooling Required ACTION Get access to the forward and aft sides of the aft pressure bulkhead at STA 1582. Locate the splice plates that splice pressure chords on the circumference of the forward side of the aft pressure bulkhead. Remove the aft row of fasteners from each splice plate and do an open hole High Frequency Eddy Current (HFEC) inspection for any crack in the aft pressure bulkhead web. If any crack is found, contact The Boeing Company for repair instructions and do the repair. If no crack is found, install new fasteners, close access to the area and repeat the inspection at the time specified in Paragraph 1.E., Compliance.
EFFECTIVITY All 767-200/-300/-300F/-400ER airplanes. Refer to Paragraph 1.A.1., Airplanes for the list of affected airplanes.
COMPLIANCE The Federal Aviation Administration (FAA) will possibly release an additional 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 is related to 767 MPD SSI 53-80-I01A, which is mandated by AD 2014-14-04. All other MPD inspections outside of the affected area are not affected and must continue.
Refer to Paragraph 1.E., Compliance.
INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the inspection and/or repair procedures given in this service bulletin.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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MANPOWER Elapsed Hours Total Task Hours Airplanes
12.6045.20Group 1, Configuration 1 Airplanes
13.3546.70Group 1, Configuration 2 Airplanes
12.6045.20Group 2, Configuration 1 Passenger Airplanes
8.6017.20Group 2, Configuration 1 Converted Freighters
13.3546.70Group 2, Configuration 2 Passenger Airplanes
9.3518.70Group 2, Configuration 2 Converted Freighters
12.6045.20Group 3 Passenger Airplanes
8.6017.20Group 3 Freighters and Converted Freighters
13.3546.70Group 4 Passenger Airplanes
9.3518.70Group 4 Freighters and Converted Freighters Refer to Paragraph 1.G., Manpower.
MATERIAL INFORMATION Operator Supplied Parts/Materials.
Refer to Paragraph 2.A., Material - Price and Availability.
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BOEING SERVICE BULLETIN 767-53A0266
ALERT ALERT
REMOVE ROW OF SIX AFT FASTENERS AND DO A HIGH FREQUENCY EDDY CURRENT INSPECTION FOR ANY CRACK.
IF ANY CRACK IS FOUND, CONTACT THE BOEING COMPANY FOR REPAIR INSTRUCTIONS AND DO THE REPAIR. IF NO CRACK IS FOUND, DO REPEAT INSPECTIONS.
BULKHEAD WEB
TYPICAL RADIAL
STIFFENER
SPLICE PLATE STA 1582
SKIN INBD
TYPICAL INSPECTION AREA NOTE:
SOME AFFECTED AIRPLANE CONFIGURATIONS HAVE SHORT
STIFFENERS AT THE AFT PRESSURE BULKHEAD TO PRESSURE CHORD JOINT. SHORT STIFFENERS ARE NOT SHOWN FOR CLARITY.
Original Issue: April 20, 2015 PROPRIETARY - Copyright © Unpublished Export Controlled ECCN: 9E991 - BOEING 767-53A0266 Work - See page 1 for details. 8 of 41
Commercial Airplanes 767 Service Bulletin ALERT Number: 767-53A0266 Original Issue: April 20, 2015 ATA System: 5380 SUBJECT: FUSELAGE - Aft Pressure Bulkhead - STA 1582 Aft Pressure Bulkhead Web Inspection Under Pressure Chord Splice Plate
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 Airplanes, in 4 Groups. The Variable Numbers and Group Information for the applicable airplanes are 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 1097.
Affected airplanes after Line Number 1097 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 from line number 1 to 175 with aft pressure bulkhead replaced in accordance with SB 767-53A0139, with four pressure chord splice plates.
-1 Airplanes from line number 176 to 423.-2 Airplanes with original production bulkhead installed with three pressure chord splice plates.
1 Airplanes with aft pressure bulkhead replaced in accordance with a Boeing Organization Design Authorization (ODA) approval via FAA Form 8100-9, with four pressure chord splice plates.
2 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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DESCRIPTIONCONFIGURATIONGROUP Airplanes from line number 424 to 926 installed with three pressure chord splice plates.
-3 Airplanes from line number 927 and on installed with four pressure chord splice plates.
-4 Airplane Models:
767-200, 767-300, 767-300F, 767-400ER 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 1VE061 - VE068 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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GroupVariable Number 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 2VK081 - VK099 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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GroupVariable Number 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 3VN174 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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