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Commercial Airplanes 707 Service Bulletin ALERT Number: A3543 Original Issue: September 15, 2016 ATA System: 5304 SUBJECT: FUSELAGE - Aft Fuselage Section - STA 1440 Aft Pressure Bulkhead Web Inspection for Oil Canning 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Unpublished Work.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: September 15, 2016 A3543 1 of 52
3.0
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: September 15, 2016 A3543 2 of 52 BOEING SERVICE BULLETIN A3543
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Table of Contents
Summary5
1. PLANNING INFORMATION9
A. Effectivity9
1. Airplanes9
2. Spares Affected13
B. Concurrent Requirements13
C. Reason13
D. Description14
E. Compliance14
F. Approval18
G. Manpower18
H. Weight and Balance Changes18
I. Electrical Load Data18
J. References19
1. Existing Data:19
2. Data Supplied with this Service Bulletin:19
3. Installation Drawings Used in the Preparation of this Service Bulletin:19
K. Publications Affected19
L. Interchangeability and Intermixability of Parts19
M. Software Accomplishment Summary19
2. MATERIAL INFORMATION21
A. Material - Price and Availability21
B. Industry Support Information21
C. Parts Necessary for Each Airplane21
1. Kits/Parts21
2. Parts and Materials Supplied by the Operator21
3. Parts Modified and Reidentified21
4. Parts Removed and Not Replaced21
D. Parts Necessary to Change Spares21
E. Special Tooling - Price and Availability21
F. Special Tooling Necessary to do this Service Bulletin21
3. ACCOMPLISHMENT INSTRUCTIONS23
A. GENERAL INFORMATION23
B. WORK INSTRUCTIONS24
FIGURE 1: STA 1440 AFT PRESSURE BULKHEAD WEB - DETAILED INSPECTION28
FIGURE 2: STA 1440 AFT PRESSURE BULKHEAD WEB - OIL CANNING ZONE DETERMINATION AND
DETAILED INSPECTION31
FIGURE 3: STA 1440 AFT PRESSURE BULKHEAD WEB - DETAILED INSPECTION AND EDDY CURRENT
INSPECTION38
FIGURE 4: STA 1440 AFT PRESSURE BULKHEAD WEB - Y-CHORD - DETAILED INSPECTION AND
EDDY CURRENT INSPECTION42
FIGURE 5: STA 1440 AFT PRESSURE BULKHEAD WEB - HIGH FREQUENCY EDDY CURRENT (HFEC)
INSPECTION47
APPENDIX A: TABLE 1: STA 1440 AFT PRESSURE BULKHEAD WEB INSPECTION FOR OIL CANNING
.49
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: September 15, 2016 A3543 3 of 52 BOEING SERVICE BULLETIN A3543
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Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: September 15, 2016 A3543 4 of 52 BOEING SERVICE BULLETIN A3543
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Commercial Airplanes 707 Service Bulletin ALERT SummaryNumber: A3543Original Issue: September 15, 2016 ATA System: 5304 SUBJECT: FUSELAGE - Aft Fuselage Section - STA 1440 Aft Pressure Bulkhead Web Inspection for Oil Canning
THIS DOCUMENT 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 DOCUMENT TO THE NEW OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS DOCUMENT TO THE NEW OWNER.
CONCURRENT REQUIREMENTS None.
BACKGROUND This service bulletin gives instructions to inspect for any oil canning and any crack on the STA 1440 aft pressure bulkhead web. If the work given in this service bulletin is not accomplished, a fatigue crack caused by oil canning may go undetected. An undetected fatigue crack in the aft pressure bulkhead web could grow in length and may result in reduced structural integrity of the web and lead to rapid decompression of the airplane.
Accomplishment of the inspections in this service bulletin will enable early detection of any web fatigue crack at oil canning locations.
Oil canning is defined as a locally buckled forward area of the aft pressure bulkhead web between the radial stiffeners and the circumferential tear straps which can pop outward when the fuselage is pressurized causing a stress reversal cycle during each flight that may lead to fatigue cracking of the aft pressure bulkhead web.
Boeing Service Related Problem 707-SRP-53-0445 is related to this service bulletin.
Boeing Fleet Team Digest 707 FTD 53-16001 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.
Original Issue: September 15, 2016 A3543 5 of 52
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 NoOperator Supplied Parts/Material Paragraph 2.F., Special Tooling Necessary to do this Service Bulletin NoSpecial Tooling Required ACTION Get access to the aft side of the STA 1440 aft pressure bulkhead web and do a detailed inspection for any oil canning. If no oil canning is found do repeat inspections for any oil canning. If any oil canning is found, determine if the oil canning is within Zone 1 limits, do a detailed inspection for any damage or any irregularity and do an eddy current inspection for any crack from the forward or aft side of the STA 1440 aft pressure bulkhead web.
If any oil canning is found within Zone 1 limits and no crack is found, then do one of the following options. Option 1 do repeat inspections and then contact The Boeing Company for repair instructions and do the repair. Option 2 contact The Boeing Company for repair instructions and do the repair.
If any oil canning is found with any damage or any irregularity, contact The Boeing Company for repair instructions and do the repair.
If any oil canning is found within Zone 2 limits or if any crack is found, contact The Boeing Company for repair instructions and do the repair.
EFFECTIVITY 707-100 LONG BODY, 707-100B LONG BODY, 707-100B SHORT BODY, 707-200, 707-300, 707-300B, 707-300C, 707-400, 720, 720B 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.
Refer to Paragraph 1.E., Compliance for compliance information.
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 Refer to Paragraph 1.G., Manpower.
MATERIAL INFORMATION None.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: September 15, 2016 A3543 7 of 52 BOEING SERVICE BULLETIN A3543
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BOEING SERVICE BULLETIN A3543
ALERT ALERT , RADIAL STIFFENER
CIRCUMFERENTIAL
TEAR STRAPS
WEB LAP
SPLICES
Y CHORD
AFT PRESSURE
BULKHEAD WEB
VIEW LOOKING FORWARD GET ACCESS TO THE AFT SIDE OF THE STA 1440 AFT PRESSURE BULKHEAD WEB AND DO A DETAILED INSPECTION FOR ANY OIL CANNING. IF NO OIL CANNING IS FOUND DO REPEAT INSPECTIONS FOR ANY OIL CANNING. IF ANY OIL CANNING IS FOUND, DETERMINE IF THE OIL CANNING IS WITHIN ZONE 1 LIMITS, DO A
DETAILED INSPECTION FOR ANY DAMAGE OR ANY IRREGULARITY AND DO AN EDDY CURRENT INSPECTION FOR ANY CRACK FROM THE FORWARD OR AFT SIDE OF THE STA 1440 AFT PRESSURE BULKHEAD WEB.
IF ANY OIL CANNING IS FOUND WITHIN ZONE 1 LIMITS AND NO CRACK IS FOUND, THEN DO ONE OF THE FOLLOWING OPTIONS. OPTION 1: DO REPEAT INSPECTIONS AND THEN CONTACT THE BOEING COMPANY FOR REPAIR INSTRUCTIONS AND DO THE REPAIR. OPTION 2: CONTACT THE BOEING COMPANY FOR REPAIR INSTRUCTIONS AND DO THE REPAIR.
IF ANY OIL CANNING IS FOUND WITH ANY DAMAGE OR ANY IRREGULARITY, CONTACT THE BOEING COMPANY FOR REPAIR INSTRUCTIONS AND DO THE REPAIR.
IF ANY OIL CANNING IS FOUND WITHIN ZONE 2 LIMITS OR IF ANY CRACK IS FOUND, CONTACT THE BOEING COMPANY FOR REPAIR INSTRUCTIONS AND DO THE REPAIR.
Original Issue: September 15, 2016 PROPRIETARY - Copyright © Unpublished Export Controlled ECCN: 9E991 - BOEING A3543 Work - See page 1 for details. 8 of 52
Commercial Airplanes 707 Service Bulletin ALERT Number: A3543 Original Issue: September 15, 2016 ATA System: 5304 SUBJECT: FUSELAGE - Aft Fuselage Section - STA 1440 Aft Pressure Bulkhead Web Inspection for Oil Canning
THIS DOCUMENT 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 DOCUMENT TO THE NEW OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS DOCUMENT TO THE NEW OWNER.
1. PLANNING INFORMATION A. Effectivity
1. Airplanes This service bulletin is applicable to 707/720 airplanes, line numbers 1 thru 941 in 1 Group. The Variable Numbers and Group Information for the applicable airplanes is given below.
Refer to Service Bulletin Index D6-1647 Part 3 for Airplane Variable Number, Line Number, and Serial Number data.
DESCRIPTIONCONFIGURATIONGROUP 707-100 LONG BODY, 707-100B LONG BODY, 707-100B SHORT BODY, 707-200, 707-300, 707-300B, 707-300C, 707-400, 720, 720B airplanes.
-1 Airplane Models:
707-100 LONG BODY, 707-100B LONG BODY, 707-100B SHORT BODY, 707-200, 707-300, 707-300B, 707-300C, 707-400, 720, 720B GroupVariable Number 1B0001 - B0029 1B0101 - B0125 1B0201 - B0203 1B0301 - B0306 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: September 15, 2016 A3543 9 of 52
GroupVariable Number 1B0401 - B0402 1B0501 - B0515 1B2001 - B2008 1B2091 - B2092 1B2101 - B2116 1B2191 - B2194 1B2199 1B2201 - B2227 1B2401 - B2403 1B2501 - B2502 1B2551 - B2553 1B2601 - B2608 100001 - 00002 100004 - 00006 100101 100103 - 00113 100115 - 00153 100201 - 00205 100301 - 00305 100401 - 00449 100471 - 00475 100501 - 00513 100601 100701 - 00703 102001 - 02020 102101 - 02121 102201 - 02207 102301 - 02303 102401 - 02418 104001 - 04005 104020 - 04022 104101 - 04106 104201 - 04218 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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GroupVariable Number 104271 - 04272 104301 - 04303 105001 - 05060 105101 - 05138 105201 - 05208 105301 - 05312 105401 105601 - 05605 105631 - 05635 105701 - 05703 105801 - 05802 105821 - 05827 105831 - 05833 105851 - 05854 105891 - 05892 105921 - 05923 105941 - 05942 105961 - 05970 106001 - 06002 106101 106401 - 06404 106451 106461 107001 - 07017 107041 - 07059 107071 - 07081 107101 - 07109 107181 107191 107201 - 07215 107251 - 07271 107401 - 07407 107451 - 07458 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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GroupVariable Number 107501 - 07504 107601 - 07626 107661 - 07662 107681 - 07684 107701 - 07702 107801 - 07821 107901 - 07907 108001 - 08008 108021 108051 - 08056 108071 - 08077 108101 - 08104 108121 - 08129 108141 - 08144 108151 - 08153 108171 - 08173 108191 - 08192 108201 - 08210 108221 - 08224 108241 - 08244 108251 108261 108271 108301 - 08320 108324 - 08330 108333 108401 - 08410 108451 - 08452 108471 - 08475 108501 - 08502 108551 - 08553 108581 - 08582 109001 - 09006 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: September 15, 2016 A3543 12 of 52 BOEING SERVICE BULLETIN A3543