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Commercial Airplanes 767 Service Bulletin
SPECIAL ATTENTION Number: 767-25-0428 Original Issue: August 23, 2007 Revision 3: October 21, 2010 ATA System: 2566 SUBJECT: EQUIPMENT/FURNISHINGS - Door Mounted Escape System - Escape Slide Deployment System - Type A Entry/Service Door Escape Slide Deployment Bar Separation Link Assembly Change 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BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET Copyright © 2007 The Boeing Company Unpublished Work - All Rights Reserved Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable subject matter.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, KC-10, KDC-10, MD-10, MD-11, MD-80, MD-88, MD-90, P-8A, Poseidon 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BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 23, 2007 767-25-0428Revision 3: October 21, 2010 1 of 66
2.0
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 23, 2007 767-25-0428Revision 3: October 21, 2010 2 of 66 BOEING SERVICE BULLETIN 767-25-0428
BLANK PAGE
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 8 D. Description .............................................. 1 9 E. Compliance .............................................. 1 9 F. Approval ............................................... 2 0 G. Manpower .............................................. 2 0 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
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 5
3. Parts Modified and Reidentified: ............................... 2 5
4. Parts Removed and Not Replaced: .............................. 2 5 D. Parts Necessary to Change Spares ................................. 2 5 E. Special Tooling - Price and Availability ............................... 2 6 F. Special Tooling Necessary to do this Service Bulletin ....................... 2 6
3. ACCOMPLISHMENT INSTRUCTIONS .................................. 2 7 A. GENERAL INFORMATION ..................................... 2 7 B. WORK INSTRUCTIONS ....................................... 2 7 FIGURE 1: ENTRY/SERVICE DOOR BUSTLE REMOVAL [Group 1, 3] ................. 2 9 FIGURE 2: ENTRY/SERVICE DOOR BUSTLE REMOVAL [Group 2, 4] ................. 3 2 FIGURE 3: SEPARATION LINK ASSEMBLY REMOVAL [Group 1, 3] .................. 3 5 FIGURE 4: SEPARATION LINK ASSEMBLY REMOVAL [Group 2, 4] .................. 3 8 FIGURE 5: SEPARATION LINK ASSEMBLY INSTALLATION [Group 1, 3] ............... 4 1 FIGURE 6: SEPARATION LINK ASSEMBLY INSTALLATION [Group 2, 4] ............... 4 6 FIGURE 7: DEPLOYMENT BAR ASSEMBLY PART MARKING [Group 1] ............... 5 1 FIGURE 8: DEPLOYMENT BAR ASSEMBLY PART MARKING [Group 2] ............... 5 3 FIGURE 9: DEPLOYMENT BAR ASSEMBLY PART MARKING [Group 3] ............... 5 5 FIGURE 10: DEPLOYMENT BAR ASSEMBLY PART MARKING [Group 4] ............... 5 7 FIGURE 11: ENTRY/SERVICE DOOR BUSTLE INSTALLATION [Group 1, 3] .............. 5 9
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Original Issue: August 23, 2007 767-25-0428Revision 3: October 21, 2010 3 of 66 BOEING SERVICE BULLETIN 767-25-0428
FIGURE 12: ENTRY/SERVICE DOOR BUSTLE INSTALLATION [Group 2, 4] .............. 6 3
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Original Issue: August 23, 2007 767-25-0428Revision 3: October 21, 2010 4 of 66 BOEING SERVICE BULLETIN 767-25-0428
Commercial Airplanes 767 Service Bulletin
SPECIAL ATTENTION Revision Transmittal SheetNumber: 767-25-0428Original Issue: August 23, 2007 Revision 3: October 21, 2010 ATA System: 2566 SUBJECT: EQUIPMENT/FURNISHINGS - Door Mounted Escape System - Escape Slide Deployment System - Type A Entry/Service Door Escape Slide Deployment Bar Separation Link Assembly Change This revision includes all pages of the service bulletin.
COMPLIANCE INFORMATION RELATED TO THIS REVISION Federal Aviation Administration (FAA) Airworthiness Directive 2009-04-12, is related to this service bulletin.
No more work is necessary on airplanes changed in accordance with the original issue, Revision 1, or Revision 2 of this service bulletin.
REASON FOR REVISION This revision is sent to add new Step 5 in FIGURE 11 and FIGURE 12. New Step 5 gives instructions to remove the entry/service door ground lock installed in FIGURE 1 and FIGURE 2.
These sections were changed:
1. In Summary-Manpower and Paragraph 1.G., Manpower; changed manpower estimates.
2. In Figure 11; added new Step 5 for Group 1 and Group 3 airplanes.
3. In Figure 12; added new Step 5 for Group 2 and Group 4 airplanes.
The data given in Information Notice 767-25-0428 IN 03 is included in this revision.
Vertical lines are put on the left edge of each page, except in Paragraph 1.A., Effectivity, to show the location of important changes.
Pages with no vertical lines have no important changes.
REVISION HISTORY August 23, 2007Original Issue:
May 08, 2008Revision 1:
February 04, 2010Revision 2:
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Original Issue: August 23, 2007 767-25-0428Revision 3: October 21, 2010 5 of 66
October 21, 2010Revision 3:
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Original Issue: August 23, 2007 767-25-0428Revision 3: October 21, 2010 6 of 66 BOEING SERVICE BULLETIN 767-25-0428
Commercial Airplanes 767 Service Bulletin
SPECIAL ATTENTION SummaryNumber: 767-25-0428Original Issue: August 23, 2007 Revision 3: October 21, 2010 ATA System: 2566 SUBJECT: EQUIPMENT/FURNISHINGS - Door Mounted Escape System - Escape Slide Deployment System - Type A Entry/Service Door Escape Slide Deployment Bar Separation Link Assembly Change BOEING RECOMMENDS THAT EACH OPERATOR EXAMINE THIS SERVICE BULLETIN IMMEDIATELY.
CONCURRENT REQUIREMENTS None.
BACKGROUND This service bulletin will prevent the partial opening of the entry/service doors during emergency escape slide deployment. If the entry/service doors do not fully open the exit may not be available for emergency evacuation use.
Boeing has received five reports since 1993 of partial entry/service door opening during escape slide deployment testing. Boeing has also received one report of partial entry/service door opening during an actual airplane emergency evacuation.
These events were the result of the separation link assembly on the slide deployment bar not properly rotating to release the deployment cable. It was found that the snap rings attaching the separation links to the deployment bar were missing. Loss of a snap ring will result in movement of the separation link assembly past the stop screws. Movement of the separation link assembly past the stop screws will prevent full rotation of the separation link assembly and normal release of the deployment cable. If the deployment cables do not release from the separation link assemblies on the deployment bar, the un-released deployment cables will prevent full opening of the entry/service door. Service Letter 767-SL-25-101-A was issued to instruct operators to inspect the separation link assemblies for missing or damaged snap links.
This service bulletin installs separation link assemblies secured with a nut and washer instead of a snap ring.
The installation of a separation link assembly secured with a nut and washer will prevent movement of the separation link assembly past the stop screws and make sure the service/entry doors open fully in an emergency evacuation.
Boeing Service Related Problem (SRP) 767-SRP-25-0258 is related to this service bulletin.
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Original Issue: August 23, 2007 767-25-0428Revision 3: October 21, 2010 7 of 66
ACTION (PRR B12901-81S) — Remove bustle — Remove existing separation link assembly — Install new separation link assembly — Install bustle
EFFECTIVITY 767-200/-300/-400ER Airplanes. Refer to Paragraph 1.A., Effectivity, for the list of affected airplanes.
COMPLIANCE Federal Aviation Administration (FAA) Airworthiness Directive AD 2009-04-12 is related to this service bulletin.
Boeing recommends that the change given in this service bulletin be done within 4 years after the original issue date of this service bulletin.
INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the configuration changes given in this service bulletin.
MANPOWER Group 1:
Elapsed HoursTotal Task Hours
4.854.85 Group 2:
Elapsed HoursTotal Task Hours
6.106.10 Group 3:
Elapsed HoursTotal Task Hours
4.854.85 Group 4:
Elapsed HoursTotal Task Hours
6.106.10
MATERIAL INFORMATION Boeing Supplied Kits/Parts.
Refer to Paragraph 2.A., Material - Price and Availability.
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Original Issue: August 23, 2007 767-25-0428Revision 3: October 21, 2010 8 of 66 BOEING SERVICE BULLETIN 767-25-0428
BOEING SERVICE BULLETIN 767-25-0428 GROUP 1, 3 GROUP 2, 4 AFT
SERVICE AFT
DOOR SERVICE DOOR
FORWARD
SERVICE DOOR • AFT MID AFT
ENTRY SERVICE ENTRY
DOOR DOOR DOOR
FORWARD MID
FORWARD SERVICE ENTRY DOOR
ENTRY DOOR DOOR FORWARD
SEE D ENTRY DOOR (4 LOCATIONS) SEE A (6 LOCATIONS)
DEPLOYMENT BAR
- REMOVE BUSTLE
- REMOVE EXISTING
SEPARATION LINK
- INSTALL NEW
SEPARATION LINK UP
- INSTALL BUSTLE INBD < 1362153 Original Issue: August 23, 2007 Revision 3: October 21, 2010 767-25-0428
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 9 of 66
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 23, 2007 767-25-0428Revision 3: October 21, 2010 10 of 66 BOEING SERVICE BULLETIN 767-25-0428
BLANK PAGE
Commercial Airplanes 767 Service Bulletin
SPECIAL ATTENTION Number: 767-25-0428 Original Issue: August 23, 2007 Revision 3: October 21, 2010 ATA System: 2566 SUBJECT: EQUIPMENT/FURNISHINGS - Door Mounted Escape System - Escape Slide Deployment System - Type A Entry/Service Door Escape Slide Deployment Bar Separation Link Assembly Change BOEING RECOMMENDS THAT EACH OPERATOR EXAMINE THIS SERVICE BULLETIN IMMEDIATELY.
1. PLANNING INFORMATION A. Effectivity
1. Airplanes Refer to Service Bulletin Index Document D624T001 Part 3 for Airplane Variable Number, Line Number, and Serial Number data.
This service bulletin is for the airplanes shown below. An equivalent change is on subsequent production airplanes. Refer to PRR B12901-81S for data about this change.
DESCRIPTIONCONFIGURATIONGROUP 767 Airplanes with four Type A entry/service doors and have the 416T2184-2 deployment bar assembly.
-1 767 Airplanes with six Type A entry/service doors and have the 416T2184-2 deployment bar assembly.
-2 767 Airplanes with four Type A entry/service doors and have the 416T2184-3 deployment bar assembly.
-3 767 Airplanes with six Type A entry/service doors and have the 416T2184-3 deployment bar assembly.
-4 Airplane Models:
767-200, 767-300, 767-400ER
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Original Issue: August 23, 2007 767-25-0428Revision 3: October 21, 2010 11 of 66
GroupVariable Number 1VA002 - VA020 1VA301 - VA315 1VA501 - VA510 1VA512 - VA530 1VA701 - VA719 1VA801 - VA810 1VB001 - VB002 1VB051 - VB055 1VB101 - VB125 1VB201 - VB202 1VB251 - VB253 1VB281 - VB284 1VB301 - VB302 1VB321 - VB332 1VB371 - VB373 1VB401 3VB441 - VB444 1VE001 - VE003 1VE021 - VE023 1VE041 - VE043 1VE061 - VE069 1VE083 - VE086 1VE101 - VE104 1VE116 - VE118 1VE121 - VE126 1VE141 - VE150 3VE151 - VE152 1VE171 - VE172 1VF001 - VF002 1VF041 - VF042 1VF051 1VF061 - VF062
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Original Issue: August 23, 2007 767-25-0428Revision 3: October 21, 2010 12 of 66 BOEING SERVICE BULLETIN 767-25-0428