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Commercial Airplane Group 767 Service Bulletin Number: 767-57A0100 Date: August 21, 2006 Revision 1: June 19, 2008 ATA System: 5720 2811 SUBJECT: WINGS - Outer Wing - Change to Fasteners in Fuel Tank Walls - Application of Sealant Export of this technology is controlled under the United States Export Administration Regulations (EAR) (15 CFR 730-774). 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BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET Copyright © 2006 The Boeing Company Unpublished Work - All Rights Reserved Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable subject matter. Boeing also claims copyright in this document as a compilation and/or collective work.
This document includes proprietary information owned by The Boeing Company and/or one or more third parties.
Treatment of the document and the information it contains is governed by contract with Boeing. For more information, contact The Boeing Company, P .O. Box 3707, Seattle, Washington 98124.
Boeing, the Boeing signature, the Boeing symbol, 707, 717, 727, 737, 747, 757, 767, 777, 787, Dreamliner, BBJ, DC-8, DC-9, DC-10, MD-10, MD-11, MD-80, MD-88, MD-90, and the Boeing livery 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.
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
August 21, 2006 767-57A0100Revision 1: June 19, 2008 1 of 46
3.0
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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Table of Contents
Revision Transmittal Sheet5
Summary7
1. PLANNING INFORMATION ........................................ 1 1 A. Effectivity ............................................... 1 1
1. Airplanes ............................................ 1 1
2. Spares Affected ........................................ 1 7 B. Concurrent Requirements ...................................... 1 7 C. Reason ................................................ 1 7 D. Description .............................................. 1 8 E. Compliance .............................................. 1 9 F . Approval ............................................... 2 0 G. Manpower .............................................. 2 0 H. Weight and Balance Changes .................................... 2 1 I. Electrical Load Data ......................................... 2 2 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
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 4 E. Special Tooling - Price and Availability ............................... 2 4 F . Special Tooling Necessary to do this Service Bulletin ....................... 2 4
3. ACCOMPLISHMENT INSTRUCTIONS .................................. 2 5 A. GENERAL INFORMATION ..................................... 2 5 B. WORK INSTRUCTIONS ....................................... 2 5 FIGURE 1: SEAL OF THE FASTENERS [Group 1-2; Group 3, Configuration 1] ............. 2 9 FIGURE 2: UPPER WING SKIN - LEFT MAIN TANK - LOCATION OF THE FASTENERS [Group 1-2; Group 3, Configuration 1] ....................................... 3 1 FIGURE 3: UPPER WING SKIN - RIGHT MAIN TANK - LOCATION OF THE FASTENERS [Group 1-2;
Group 3, Configuration 1] ................................... 3 3 FIGURE 4: REAR SPAR - LEFT MAIN TANK AND SURGE TANK - LOCATION OF THE FASTENERS [Group 2] ............................................ 3 5 FIGURE 5: GROUP 2 - REAR SPAR - RIGHT MAIN TANK AND SURGE TANK - LOCATION OF THE FASTENERS [Group 2] .................................... 3 9 FIGURE 6: INSPECTION OF THE VORTEX GENERATORS - UPPER WING SKIN - LEFT WING [Group 3 ] ................................................ 4 3 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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FIGURE 7: INSPECTION OF THE VORTEX GENERATORS - UPPER WING SKIN - RIGHT WING [Group 3 ] ................................................ 4 5 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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Commercial Airplane Group 767 Service Bulletin Revision Transmittal SheetNumber: 767-57A0100Date: August 21, 2006 Revision 1: June 19, 2008 ATA System: 5720 2811 SUBJECT: WINGS - Outer Wing - Change to Fasteners in Fuel Tank Walls - Application of Sealant This revision includes all pages of the service bulletin.
COMPLIANCE INFORMATION RELATED TO THIS REVISION Federal Aviation Administration (FAA) Notice of Proposed Rule Making 2006-NM-293-AD, is related to this service bulletin.
No more work is necessary on airplanes changed as shown in the original issue of this service bulletin.
REASON FOR REVISION This revision is sent to to give instructions to do a General Visual Inspection of the vortex generators on certain airplanes. Before work is done, the vortex generators on certain airplanes must be inspected to determine if the vortex generators are installed with fasteners or adhesive alone. An operator reported that the vortex generators on some 767 airplanes are attached with adhesive alone. If fasteners are not used to install the vortex generators it is not necessary to apply sealant at these locations. A review of the engineering drawing for the upper wing inspar panel installation confirms that some airplanes in a certain line number range were delivered with vortex generators that are attached by adhesive alone.
These sections were changed:
1. Summary, Action, added actions for a General Visual inspection to determine if the vortex generators are attached with fasteners or adhesive alone.
2. Summary, Compliance, added a reference to Federal Aviation Administration (FAA) Notice of Proposed Rule Making 2006-NM-293-AD.
3. Summary, Manpower, added manpower for Group 3 airplanes.
4. Paragraph 1.A, Effectivity; added a new Group 3 and moved airplanes VA516-VA519, VB122-VB123, VE041, VE067-VE068, VE102-VE103, VE116-VE117, VK001-VK003, and VK031 from Group 1 to Group
3.
5. Paragraph 1.D., Description, added actions for a General Visual Inspection to determine if the vortex generators are attached with fasteners or adhesive alone.
6. Paragraph 1.D., added Maintenance Zones.
7. Paragraph 1.E., Compliance, added a reference to FAA Notice of Proposed Rule Making 2006-NM-293-AD.
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8. Paragraph 1.G., Manpower, added manpower for Group 3 airplanes.
9. Paragraph 1.H., Weight and Balance, added data for Group 3 airplanes.
10. Paragraph 3.B. Work Instructions, added steps for a General Visual Inspection to determine if the vortex generators are attached with fasteners or adhesive alone.
11. Paragraph 3., Accomplishment Instructions, added new Figures 6 and 7 to do a General Visual Inspection of the vortex generators on the wings.
The data given in Information Notice 767-57A0100 IN 01 is included in this revision.
Vertical lines are put on the left edge of each page, except in Paragraph 1.A., Effectivity Pages with no vertical lines have no important changes.
REVISION HISTORY August 21, 2006Original Issue:
June 19, 2008Revision 1:
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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Commercial Airplane Group 767 Service Bulletin SummaryNumber: 767-57A0100Date: August 21, 2006 Revision 1: June 19, 2008 ATA System: 5720 2811 SUBJECT: WINGS - Outer Wing - Change to Fasteners in Fuel Tank Walls - Application of Sealant
CONCURRENT REQUIREMENTS None.
BACKGROUND Accomplishment of the modifications within this service bulletin will help prevent possible ignition sources in the main fuel tanks, and the surge tanks caused by a lightning strike on certain wing surfaces. An ignition source in a fuel tank could result in a fire or an explosion.
A review by Boeing identified a certain fastener type in the fuel tank walls that have an insufficient bond to the structure. If energy from lightning strike goes through these fasteners, arcing can occur at the ends of the fasteners in the fuel tank. The ends of the fasteners in the fuel tank do not have sufficient electrical insulation to contain the energy from the arcs.
This Service Bulletin gives the instructions to seal the end of certain fasteners in the fuel tank walls. These changes make sure that the risk of an ignition source in the fuel tank from a lightning strike on the wing is kept to a minimum.
This service bulletin is the result of the safety assessments conducted by Boeing under SFAR 88, "Fuel Tank System Fault Tolerance Evaluation Requirements".
ACTION (PRR B13421-10) Group 1:
Prepare the main fuel tanks for entry. Get access to the left main tank. Seal the ends of the fasteners on the brackets that hold the vortex generators. Get access to the right main tank. Seal the ends of the fasteners on the brackets that hold the vortex generators. Close access to the main fuel tanks.
Group 2:
Prepare the main fuel tanks for entry. Get access to the left main tank. Seal the ends of the fasteners on the brackets that hold the vortex generators. Seal the ends of fasteners on certain stiffeners on the rear spar. Get access to the right main tank. Seal the ends of the fasteners on the brackets that hold the vortex generators.
Seal the ends of fasteners on certain stiffeners on the rear spar. Close access to the main fuel tanks.
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Group 3:
Get access to the outer surface of the upper wing panel on the left wing. Do a General Visual Inspection of the specified vortex generators on the upper wing panel of the left wing. Get access to the outer surface of the upper wing panel on the right wing. Do a General Visual Inspection of the specified vortex generators on the upper wing panel on the right wing. If the vortex generators are attached with adhesive alone, no more work is necessary.
If the vortex generators are attached with fasteners, do the following steps: Prepare the main fuel tanks for entry.
Get access to the left main tank. Seal the ends of the fasteners on the brackets that hold the vortex generators.
Get access to the right main tank. Seal the ends of the fasteners on the brackets that hold the vortex generators.
Close access to the main fuel tanks.
Service Bulletin 767-57A0102 has similar access requirements as this bulletin and can be incorporated at the same time or separately. Service Bulletin 767-57A0102 is separate from this bulletin because it makes improvements to existing design and does not have warranty remedies.
EFFECTIVITY 767 Airplanes. See Service Bulletin Paragraph 1.A.1 for effectivity.
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.
Boeing recommends that this service bulletin be incorporated within 5 years after the date on this service bulletin.
Federal Aviation Administration (FAA) Notice of Proposed Rule Making 2006-NM-293-AD, is related to this service bulletin.
INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are available for airplanes in warranty as of July 16, 2004. Please refer to Paragraph
2.B., Industry Support Information.
MANPOWER Elapsed HoursTotal Task HoursAirplanes
10.0029.25Group 1
38.81143.24Group 2
10.0529.75Group 3, Configuration 1
0.500.50Group 3, Configuration 2
MATERIAL INFORMATION Operator Supplied Parts/Materials.
Refer to Paragraph 2.A., Material - Price and Availability.
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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Commercial Airplane Group 767 Service Bulletin Number: 767-57A0100 Date: August 21, 2006 Revision 1: June 19, 2008 ATA System: 5720 2811 SUBJECT: WINGS - Outer Wing - Change to Fasteners in Fuel Tank Walls - Application of Sealant
1. PLANNING INFORMATION A. Effectivity
1. Airplanes This service bulletin is for the airplanes shown below. An equivalent change is on subsequent production airplanes. Refer to PRRB13421-10 for data about this change.
Refer to Service Bulletin Index Document D624T001 Part 3 for Airplane Variable Number, Line Number, and Serial Number data.
DESCRIPTIONCONFIGURATIONGROUP 767-200/300/300F airplanes-1 767-400ER airplanes-2 767-200/300 airplanes that have vortex fasteners installed with or without fasteners -3 Airplanes that have vortex generators installed with fasteners1 Airplanes that have vortex generators installed with adhesive alone2 Airplane Models:
767-200, 767-300, 767-300F , 767-400ER GroupVariable Number 1VA001 - VA020 1VA301 - VA315 1VA501 - VA515 3VA516 - VA519 1VA520 - VA530 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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GroupVariable Number 1VA701 - VA719 1VA801 - VA810 1VB001 - VB002 1VB051 - VB055 1VB101 - VB121 3VB122 - VB123 1VB124 - VB125 1VB201 - VB202 1VB251 - VB253 1VB281 - VB284 1VB301 - VB302 1VB321 - VB332 1VB371 - VB373 1VB401 1VB441 - VB444 1VE001 - VE003 1VE021 - VE023 3VE041 1VE042 - VE043 1VE061 - VE066 3VE067 - VE068 1VE069 1VE083 - VE086 1VE101 3VE102 - VE103 1VE104 3VE116 - VE117 1VE118 1VE121 - VE126 1VE141 - VE152 1VE171 - VE172 1VF001 - VF002 1VF041 - VF042 BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
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