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Commercial Airplanes 767 Service Bulletin ALERT Number: 767-53A0263 Original Issue: January 12, 2015 ATA System: 5300 SUBJECT: FUSELAGE - Section 43 - Inspection of Skin and Splice Fittings at Stringer 29, Body Station 786 Ring Chord 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Unpublished Work.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: January 12, 2015 767-53A0263 1 of 30
4.0
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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Table of Contents
Summary5
1. PLANNING INFORMATION9
A. Effectivity9
1. Airplanes9
2. Spares Affected ........................................ 1 5 B. Concurrent Requirements ...................................... 1 5 C. Reason ................................................ 1 5 D. Description .............................................. 1 6 E. Compliance .............................................. 1 6 F. Approval ............................................... 1 7 G. Manpower .............................................. 1 7 H. Weight and Balance Changes .................................... 1 8 I. Electrical Load Data ......................................... 1 8 J. References .............................................. 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: ........... 1 8 K. Publications Affected ........................................ 1 8 L. Interchangeability and Intermixability of Parts ........................... 1 9 M. Software Accomplishment Summary ................................ 1 9
2. MATERIAL INFORMATION ........................................ 2 1 A. Material - Price and Availability ................................... 2 1 B. Industry Support Information .................................... 2 1 C. Parts Necessary for Each Airplane ................................. 2 1
1. Kits/Parts ............................................ 2 1
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 1
3. ACCOMPLISHMENT INSTRUCTIONS .................................. 2 3 A. GENERAL INFORMATION ..................................... 2 3 B. WORK INSTRUCTIONS ....................................... 2 5 FIGURE 1: LEFT SIDE OF FUSELAGE – EXTERNAL INSPECTION AT THE UPPER AND LOWER SPLICE FITTINGS ............................................ 2 7 FIGURE 2: RIGHT SIDE OF FUSELAGE – EXTERNAL INSPECTION AT THE UPPER AND LOWER SPLICE FITTINGS ....................................... 2 9 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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Commercial Airplanes 767 Service Bulletin ALERT SummaryNumber: 767-53A0263Original Issue: January 12, 2015 ATA System: 5300 SUBJECT: FUSELAGE - Section 43 - Inspection of Skin and Splice Fittings at Stringer 29, Body Station 786 Ring Chord
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 While replacing a cracked underwing longeron fitting per service bulletin 767-57A0126, a crack indication was found in the STA 786 ring chord at the tension bolt hole common to the wing front spar lower chord and the internal bathtub fittings. There were two similar reports of these findings from two separate operators. The airplanes in these reports had 14,367 and 18,354 flight cycles and had 90,389 and 96,826 flight hours, respectively.
The current Maintenance Planning Document (MPD) inspections are not sufficient to detect any possible fuselage skin crack in the area adjacent to the ring chord at STA 786 before the crack extends to a critical length. The fuselage skin in this area is hidden between the splice fittings on the external side of the fuselage and the bathtub fittings on the internal side. This service bulletin specifies an external ultrasonic inspection of the skin hidden by the upper and lower splice fittings on both sides of the fuselage to detect any fatigue crack in the fuselage skin. It also specifies an external detailed inspection of the splice fittings and the adjacent visible fuselage skin and structure for any crack, corrosion or other damage. If the service bulletin action is not accomplished, then cracks in the fuselage skin in this hidden area could go undetected, potentially leading to a loss of a primary load path between the fuselage and the wing box. The loss of the primary load path could adversely affect the structural integrity of the airplane.
To date, there have been no reports of any fuselage skin cracks in the area that is inspected by this service bulletin.
Boeing Service Related Problem (SRP) 767-53-0461 is related to this service bulletin.
Boeing Fleet Team Digest (FTD) 767 FTD 53-14001 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.
Original Issue: January 12, 2015 767-53A0263 5 of 30
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 Remove the wing-to-body access panels on the left and right sides of the airplane to open access to the splice fittings on the fuselage adjacent and forward of the STA 786 ring chord. Do an initial external ultrasonic and detailed inspection of the area on both sides of the fuselage. Do repeat inspections if no damage is found. If damage is found, contact Boeing to get instructions for the repair for this service bulletin and do the work instructed by Boeing, before further flight. Do the inspections in accordance with paragraph 1.E., Compliance.
EFFECTIVITY 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 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.
INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the inspection given in this service bulletin.
MANPOWER Elapsed HoursTotal Task HoursAirplanes
4.608.60All Airplanes Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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BOEING SERVICE BULLETIN 767-53A0263
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MATERIAL INFORMATION None.
UPPER SPLICE
FITTING S-29
• LOWER SPLICE
FITTING INBD
DO AN INITIAL ULTRASONIC AND DETAILED INSPECTION OF THE FUSELAGE SKIN AT THE SPLICE FITTINGS. DO A REPEAT INSPECTION IF NO DAMAGE IS FOUND. IF DAMAGE IS FOUND, DO THE REPAIR BEFORE FURTHER FLIGHT. 2365367 Original Issue: January 12, 2015 Export Controlled ECCN: 9E991 - BOEING 767-53A0263 PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 7 of 30
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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Commercial Airplanes 767 Service Bulletin ALERT Number: 767-53A0263 Original Issue: January 12, 2015 ATA System: 5300 SUBJECT: FUSELAGE - Section 43 - Inspection of Skin and Splice Fittings at Stringer 29, Body Station 786 Ring Chord
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/-300/-300F/-400ER airplanes, line numbers 1-9999 in one (1) Group. 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 1093.
Affected airplanes after Line Number 1093 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 All 767 Airplanes, line numbers 1-9999-1 Airplane Models:
767-200, 767-300, 767-300F, 767-400ER GroupVariable Number 1VA001 - VA020 1VA301 - VA315 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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GroupVariable Number 1VA501 - VA530 1VA701 - VA719 1VA801 - VA810 1VB001 - VB002 1VB051 - VB055 1VB101 - VB125 1VB201 - VB202 1VB251 - VB253 1VB281 - VB284 1VB301 - VB302 1VB321 - VB332 1VB371 - VB373 1VB401 1VB441 - VB444 1VE001 - VE003 1VE021 - VE023 1VE041 - VE043 1VE061 - VE069 1VE083 - VE086 1VE101 - VE104 1VE116 - VE118 1VE121 - VE126 1VE141 - VE152 1VE171 - VE172 1VF001 - VF002 1VF041 - VF042 1VF051 1VF061 - VF062 1VF071 - VF072 1VF091 - VF093 1VF101 - VF102 1VF161 - VF162 1VF171 - VF172 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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GroupVariable Number 1VF180 - VF184 1VF251 1VK001 - VK016 1VK021 - VK022 1VK031 - VK056 1VK081 - VK113 1VK131 - VK133 1VK141 - VK148 1VK161 - VK164 1VK171 1VK181 1VK186 1VL001 - VL006 1VL011 1VL701 - VL703 1VL751 - VL755 1VL806 - VL807 1VL871 - VL873 1VL891 - VL900 1VL911 - VL914 1VL931 - VL932 1VL941 1VN001 - VN041 1VN051 - VN064 1VN081 - VN099 1VN111 - VN127 1VN130 - VN137 1VN151 - VN158 1VN163 - VN168 1VN171 - VN174 1VN191 - VN198 1VN211 - VN212 1VN221 - VN225 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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GroupVariable Number 1VN231 - VN234 1VN241 - VN243 1VN251 - VN276 1VN291 - VN293 1VN301 - VN314 1VN371 - VN372 1VN376 1VN381 - VN388 1VN421 - VN427 1VN436 1VN471 - VN472 1VN491 - VN513 1VN531 - VN532 1VN536 - VN537 1VN541 - VN542 1VN546 - VN547 1VN551 1VN556 - VN557 1VN561 - VN562 1VN631 - VN638 1VN651 - VN658 1VN671 - VN672 1VN676 1VN681 - VN691 1VN731 - VN732 1VN751 - VN753 1VN791 - VN792 1VN811 - VN813 1VN921 - VN922 1VN931 - VN936 1VN951 - VN953 1VN966 - VN972 1VQ001 - VQ021 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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