# Boeing Alert Service Bulletin 747-53A2605: Revision 3 - Rights: © The Boeing Company. Filed by the FAA in regulations.gov docket FAA-2014-0289; AD 2014-22-11 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. - Document: [Boeing Alert Service Bulletin 747-53A2605](https://openairdocs.org/service-documents/boeing/747-53a2605.md) - Title as filed: U.S. DOT/FAA - SB-747-53A2605-03 - Pages: 203 - PDF: https://openairdocs.org/files/sha256/14/60/1460b1db8f3bbff4681adb54282cc866e36df68023947ce317c2c3303178d559 - Page: https://openairdocs.org/service-documents/boeing/747-53a2605/file/1460b1db8f3b ## Text Some pages are OCR from a scan. OCR can misread letters and numbers. Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 Commercial Airplanes 747 Service Bulletin ALERT Number: 747-53A2605 Original Issue: October 08, 2009 Revision 3: July 10, 2013 ATA System: 5312 SUBJECT: FUSELAGE - Center Section - Tension Ties and Frames - Modification and Inspection 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 © 2009 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 Unpublished Work.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: October 08, 2009 747-53A2605Revision 3: July 10, 2013 1 of 203 4.0 ### Page 2 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 2 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT BLANK PAGE ### Page 3 Table of Contents Revision Transmittal Sheet ............................................ 5 Summary ...................................................... 7 1. PLANNING INFORMATION ........................................ 1 1 A. Effectivity ............................................... 1 1 1. Airplanes ............................................ 1 1 2. Spares Affected ........................................ 2 2 B. Concurrent Requirements ...................................... 2 2 C. Reason ................................................ 2 3 D. Description .............................................. 2 3 E. Compliance .............................................. 2 5 F. Approval ............................................... 3 0 G. Manpower .............................................. 3 1 H. Weight and Balance Changes .................................... 4 1 I. Electrical Load Data ......................................... 4 2 J. References .............................................. 4 2 1. Existing Data: ......................................... 4 2 2. Data Supplied with this Service Bulletin: ........................... 4 2 3. Installation Drawings Used in the Preparation of this Service Bulletin: ........... 4 9 K. Publications Affected ........................................ 4 9 L. Interchangeability and Intermixability of Parts ........................... 5 0 M. Software Accomplishment Summary ................................ 5 0 2. MATERIAL INFORMATION ........................................ 5 1 A. Material - Price and Availability ................................... 5 1 B. Industry Support Information .................................... 5 2 C. Parts Necessary for Each Airplane ................................. 5 2 1. Kits/Parts: ........................................... 5 2 2. Parts and Materials Supplied by the Operator: ....................... 1 6 2 3. Parts Modified and Reidentified: ............................... 1 6 3 4. Parts Removed and Not Replaced: ............................. 1 6 3 D. Parts Necessary to Change Spares ................................ 1 6 3 E. Special Tooling - Price and Availability .............................. 1 6 3 F. Special Tooling Necessary to do this Service Bulletin ...................... 1 6 4 3. ACCOMPLISHMENT INSTRUCTIONS ................................. 1 6 5 A. GENERAL INFORMATION .................................... 1 6 5 B. WORK INSTRUCTIONS ...................................... 1 6 6 FIGURE 1: SURFACE HFEC INSPECTION OF TENSION TIE CENTER SECTIONS (STA 760 - STA 940) [Group 1-3, 13-14] ....................................... 1 7 7 FIGURE 2: SURFACE HFEC INSPECTION OF TENSION TIE CENTER SECTIONS (STA 800 - STA 940) [Group 4, 9] .......................................... 1 7 9 FIGURE 3: SURFACE HFEC INSPECTION OF TENSION TIE CENTER SECTIONS (STA 800 - STA 880, STA 920, AND STA 940) [Group 5, 16] ........................... 1 8 1 FIGURE 4: SURFACE HFEC INSPECTION OF TENSION TIE CENTER SECTIONS (STA 840 - STA 940) [Group 6] ............................................ 1 8 3 FIGURE 5: SURFACE HFEC INSPECTION OF TENSION TIE CENTER SECTIONS (STA 840 - STA 880, STA 920, AND STA 940) [Group 7] ............................. 1 8 5 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 3 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 4 FIGURE 6: SURFACE HFEC INSPECTION OF TENSION TIE CENTER SECTIONS (STA 780 - STA 880, STA 920, AND STA 940) [Group 8, 11-12, 15] ....................... 1 8 7 FIGURE 7: SURFACE HFEC INSPECTION OF TENSION TIE CENTER SECTIONS (STA 720 - STA 940) [Group 10] ........................................... 1 8 9 FIGURE 8: EDDY CURRENT INSPECTIONS OF ALL AREAS OF TENSION TIES - LEFT SIDE [Group 1-16] .............................................. 1 9 2 FIGURE 9: EDDY CURRENT INSPECTIONS OF ALL AREAS OF TENSION TIES - RIGHT SIDE [Group 1-16] .............................................. 1 9 7 APPENDIX A: TENSION TIE DISCONNECTION METHODS ....................... 2 0 2 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 4 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 5 Commercial Airplanes 747 Service Bulletin ALERT Revision Transmittal SheetNumber: 747-53A2605Original Issue: October 08, 2009 Revision 3: July 10, 2013 ATA System: 5312 SUBJECT: FUSELAGE - Center Section - Tension Ties and Frames - Modification and Inspection This revision includes all pages of the service bulletin. COMPLIANCE INFORMATION RELATED TO THIS REVISION More work is necessary on airplanes modified in accordance with the original issue, Revision 1, or Revision 2 of this service bulletin. Airplanes previously modified in accordance with this service bulletin will require surface high frequency eddy current (HFEC) inspection for cracks in the forward and aft tension tie channels around fasteners in unmodified areas where fastener holes were not zero-timed during modification. Refer to paragraph 1.E., Compliance for the compliance time of this additional inspection. However, no additional modification is necessary. Federal Aviation Administration (FAA) Airworthiness Directive AD 2012-13-08 is related to this service bulletin. Airplanes RG001-RG009, RG091-RG091, RG095-RG095, RG101-RG104, RG121-RG126, RG141-RG142, RG161-RG164, RG171-RG174, RG191-RG193, RG211-RG213, RG221-RG222, RH111-RH112, RH121-RH122 were added to the service bulletin effectivity as Group 17. Airplanes RH101 and RH102 were added to the service bulletin effectivity as Group 18. REASON FOR REVISION This revision is sent to add the requirement to do surface high frequency eddy current (HFEC) inspection where fastener holes are not zero-timed during modification on Group 1-16 airplanes. Revision 3 also adds instructions for post-modification inspection of the entire tension tie for Group 1-16 airplanes, and adds effectivity and modification instructions for 747SP (Group 17-18) airplanes. These sections were changed: 1. In the Summary: Updated the Background and Action sections to reflect new inspection requirements. Also, updated Compliance section with current Airworthiness Directive (AD) information. 2. In Paragraph 1.A., Effectivity: Added 747SP airplanes as Group 17 and Group 18. Also, revised the Group/Configuration table to specify configurations for airplanes that have and have not already had the tension tie and frame modification accomplished. 3. In Paragraph 1.C., Reason: Added reason for Revision 3. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 5 of 203 ### Page 6 4. In Paragraph 1.D., Description: Updated the description of service bulletin actions and added "more work" statement related to Revision 3. 5. In Paragraph 1.E., Compliance: Updated Airworthiness Directive information. Revised compliance Table 1 to apply only to initial inspection and modification. Added new compliance Tables 2, 3, and 4 for Post-Modification inspections. Added new compliance Table 5 for additional (more work) inspection requirements on airplanes that had the tension tie and frame modification accomplished in accordance with a previous revision of this service bulletin. Added new compliance Tables 6 and 7 for Group 17 and 18 airplanes. 6. In Paragraph 1.F., Approval: Updated Alternative Method of Compliance (AMOC) statements for AD 2004-07-22 R1, 84-19-01, and 94-13-06. Added new AMOC statements for AD 2012-13-08 (which superseded AD 2006-01-07). 7. In Paragraph 1.G., Manpower: Added task hour estimates for tension tie center section inspections and post-modification inspections. 8. In Paragraph 1.J.2., Data Supplied with this Service Bulletin: Added drawings required for post-modification inspections of Group 1-16 airplanes and added drawings required for modification of Group 17-18 airplanes. Also added KPL data previously not listed. 9. In Paragraph 3.A., General Information: Added note 15. 10. In Paragraph 3.B., Work Instructions: Added PART 3 to give instructions for new post-modification inspection requirements, and added PART 4 to give instructions for inspection of the unmodified tension tie center sections. PART 4 is a "more work" requirement for airplanes that had the tension tie and frame modification accomplished in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. Also in the Work Instructions, added PART 5 and PART 6 for modification of Group 17-18 airplanes. 11. In Figures 1 - 7: These new figures have been added to give inspection instructions for the unmodified tension tie center sections on Group 1-16 airplanes. 12. In Figures 8 and 9: These new figure have been added to give post-modification inspection instructions not previously included in the service bulletin for Group 1-16 airplanes. 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 October 08, 2009Original Issue: May 27, 2010Revision 1: December 09, 2011Revision 2: July 10, 2013Revision 3: Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 6 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 7 Commercial Airplanes 747 Service Bulletin ALERT SummaryNumber: 747-53A2605Original Issue: October 08, 2009 Revision 3: July 10, 2013 ATA System: 5312 SUBJECT: FUSELAGE - Center Section - Tension Ties and Frames - Modification and Inspection 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 This service bulletin gives instructions for modification of upper deck tension ties and adjacent frame structure on non stretched upper deck (Non-SUD) airplanes. The tension ties have been determined to be structure that is susceptible to Widespread Fatigue Damage (WFD). WFD can cause tension ties to become severed or disconnected from the frames. Severed or disconnected Tension Ties and/or Frames at multiple locations could result in rapid in-flight decompression. For more information about WFD, refer to Boeing Service Letter 747-SL-53-088. Service Bulletin 747-53A2502 recommends initial and repeat inspections of Non-SUD airplane tension ties from body station (STA) 760 to STA 940 (STA 1040 to STA 1140 for 747SP). Service Bulletin 747-53A2502 was issued to address multiple reports of cracks found in tension ties and adjacent frame structure. Group 1-16: Accomplishment of the modification in this service bulletin terminates the repeat inspection requirement of Service Bulletin 747-53A2502. Group 17-18: Accomplishment of the modification in this service bulletin does not terminate the repeat inspection requirement of Service Bulletin 747-53A2502, but a new inspection threshold is provided. Boeing Service Related Problem (SRP) 747-SRP-53-0200 and 747-SRP-53-0438 are related to this service bulletin. As a part of a service bulletin validation program, this modification and inspection was completed on airplane RD041 by Service Bulletin 747-53A2605, Original Issue. The modification and inspection completed on airplane RD041 by Service Bulletin 747-53A2605, Original Issue is equivalent to the Revision 2 of this service bulletin. Airplane RD041 has the configuration of a Group 5 airplane. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 7 of 203 ### Page 8 Subsequent to the release of Revision 2 of this service bulletin, Boeing has determined that additional inspections are required in the center sections of the tension ties where the tension tie channels are not replaced and where fastener holes are not zero-timed during modification. 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., ComplianceYesAD Related Paragraph 1.H., Weight and Balance ChangesYesWeight and Balance Change Paragraph 1.I., Electrical Load DataNoElectrical Load Changed Paragraph 1.K., Publications AffectedYesPublications Affected Paragraph 1.K., Publications AffectedNoAirplane Flight Operations Affected (Flight Crew Operations Manual and/or FAA Approved Air- plane Flight Manual) Paragraph 2.C.1., Kits/PartsYesKits/Parts Required Paragraph 2.C.2., Parts and Materials Supplied by the Operator YesOperator Supplied Material Paragraph 2.F., Special Tooling Necessary to do this Service Bulletin YesSpecial Tooling Required ACTION (PRR 85901-68RS) Get access to the Frame to Tension Tie joints in Section 42. At each station, disconnect and remove a section of the tension tie between the frame and approximate Buttock Line (BL) 36. For each frame, remove a specified section of the frame above and below the tension tie attach point. After the existing frame and tension tie structure has been removed and discarded, install new frame and tension tie structure. Do the modification on both sides of the airplane. Group 1-16: Do surface high frequency eddy current (HFEC) inspection of the tension ties at fastener locations where the holes were not zero-timed during modification. If cracks are found, contact Boeing for repair instructions and do the repair. Group 1-16: After modification, do initial and repeat detailed, high frequency eddy current (HFEC), and low frequency eddy current (LFEC) inspections of the tension ties at the compliance time specified in paragraph 1.E., Compliance. If cracks are found, contact Boeing for repair instructions and do the repair. Group 17-18: After modification, do initial and repeat detailed and HFEC inspections for cracks in all tension ties, adjacent frame structure, and adjacent structure that attaches to the tension ties. If cracks are found, contact Boeing for repair instructions and do the repair. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 8 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 9 EFFECTIVITY 747-100, 747-100B, 747-200B, 747-200C, 747-200F, 747-400F, 747SR, and 747SP airplanes. Refer to Paragraph 1.A.1., Airplanes, for the list of affected airplanes. COMPLIANCE Federal Aviation Administration (FAA) Airworthiness Directives AD 84-19-01, AD 94-13-06, AD 2004-07-22 R1, and AD 2012-13-08 are related to this service bulletin. Refer to paragraph 1.E, Compliance. INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the modification and inspections given in this service bulletin. MANPOWER Refer to paragraph 1.G., Manpower. MATERIAL INFORMATION Boeing Supplied Kits/Parts. Refer to Paragraph 2.A., Material - Price and Availability. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 9 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 10 (OCR) BOEING SERVICE BULLETIN 747-53A2605 ALERT ALERT STA STA 940 720 FRAME (TYPICAL) TENSION TIE (TYPICAL) STA 720 MODIFY /INSPECT TENSION TIES AND FRAMES NOTE: TENSION TIES ON 747SP AIRPLANES ARE FROM STA 1040 TO STA 1140 FWD STA 940 1732168 Original Issue: October 08, 2009 Revision 3: July 10, 2013 PROPRIETARY - Copyright © Unpublished Export Controlled ECCN: 9E991 - BOEING 747-53A2605 Work - See page 1 for details. 10 of 203 ### Page 11 Commercial Airplanes 747 Service Bulletin ALERT Number: 747-53A2605 Original Issue: October 08, 2009 Revision 3: July 10, 2013 ATA System: 5312 SUBJECT: FUSELAGE - Center Section - Tension Ties and Frames - Modification and Inspection 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 for the airplanes shown below. Refer to PRR 85901-68RS for data about this change. Refer to Service Bulletin Index Document D6-30300 Part 3 for Airplane Variable Number, Line Number, and Serial Number data. DESCRIPTIONCONFIGURATIONGROUP 747-100 and -200B airplanes with tension ties from STA 760 to STA 940, and a combination of tension ties at STA 760 and STA 940 that is unique. The Group 1 tension tie modification is similar to Group 2, except at STA 760. The Group 1 tension tie modification similar to Group 13, except at STA 940. This group requires 142U0102-233 tension tie modification kit. -1 Group 1 airplanes not modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 1 Group 1 airplanes that were modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 2 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 11 of 203 ### Page 12 DESCRIPTIONCONFIGURATIONGROUP 747-100 airplanes with tension ties from STA 760 to STA 940, and a combination of tension ties at STA 760 and STA 940 that is unique. The Group 2 tension tie modification is similar to Group 1, except at STA 760. The Group 2 tension tie modification similar to Group 14, except at STA 940. This group requires 142U0102-233 tension tie modification kit. -2 Group 2 airplanes not modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 1 Group 2 airplanes that were modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 2 -100 and -200B airplanes with tension ties from STA 760 to STA 940, and a unique tension tie configuration at STA 760. -3 Group 3 airplanes not modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 1 Group 3 airplanes that were modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 2 747-100, -100B, -200B and SR airplanes with tension ties from STA 800 to STA 940, and a unique combination of tension ties at STA 900, 920, and 940. -4 Group 4 airplanes not modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 1 Group 4 airplanes that were modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 2 747-200B and SR airplanes with tension ties from STA 800 to STA 940, and a unique frame configuration. -5 Group 5 airplanes not modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 1 Group 5 airplanes that were modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 2 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 12 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 13 DESCRIPTIONCONFIGURATIONGROUP 747-100, -100B, -200B and SR airplanes with tension ties from STA 840 to STA 940 that have a unique configuration. -6 Group 6 airplanes not modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 1 Group 6 airplanes that were modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 2 747-200B and SR airplanes with tension ties from STA 840 to STA 940 that have a unique configuration. -7 Group 7 airplanes not modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 1 Group 7 airplanes that were modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 2 747-200F airplanes. These airplanes have tension ties from STA 780 to STA 940, and have a unique configuration at STA 940. -8 Group 8 airplanes not modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 1 Group 8 airplanes that were modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 2 747-200C airplanes. These airplanes have tension ties from STA 800 to STA 940, and have a unique configuration at STA 900. -9 Group 9 airplanes not modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 1 Group 9 airplanes that were modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 2 747-400F airplanes. These airplanes have tension ties from STA 720 to STA 940. -10 Group 10 airplanes not modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 1 Group 10 airplanes that were modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 2 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 13 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 14 DESCRIPTIONCONFIGURATIONGROUP 747-100 airplanes with tension ties from STA 780 to STA 940, and a unique combination of tension ties at STA 900, 920, and 940. This group requires 142U0102-233 tension tie modification kit. -11 Group 11 airplanes not modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 1 Group 11 airplanes that were modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 2 747-100 airplanes with tension ties from STA 780 to STA 940, and a unique combination of tension ties at STA 900, 920, and 940. -12 Group 12 airplanes not modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 1 Group 12 airplanes that were modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 2 747-100 airplanes with tension ties from STA 760 to STA 940, and a combination of tension ties at STA 760 and STA 940 that is unique. The Group 13 tension tie modification is similar to Group 14, except at STA 760. The Group 13 tension tie modification similar to Group 1, except at STA 940. This group requires 142U0102-232 tension tie modification kit. -13 Group 13 airplanes not modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 1 Group 13 airplanes that were modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 2 747-100 airplanes with tension ties from STA 760 to STA 940, and a combination of tension ties at STA 760 and STA 940 that is unique. The Group 14 tension tie modification is similar to Group 13, except at STA 760. The Group 14 tension tie modification similar to Group 2, except at STA 940. This group requires 142U0102-232 tension tie modification kit. -14 Group 14 airplanes not modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 1 Group 14 airplanes that were modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 2 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 14 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 15 DESCRIPTIONCONFIGURATIONGROUP 747-100 airplanes with tension ties from STA 840 to STA 940 that have a unique configuration. This group requires 142U0102-232 tension tie modification kit. -15 Group 15 airplanes not modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 1 Group 15 airplanes that were modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 2 747-200C airplanes with tension ties from STA 800 to STA 940, and a unique frame configuration. -16 Group 16 airplanes not modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 1 Group 16 airplanes that were modified in accordance with the Original Issue, Revision 1, or Revision 2 of this service bulletin. 2 747SP airplanes that have tension ties from STA 1040 to STA 1140.-17 747SP airplanes that have tension ties from STA 1060 to STA 1140.-18 Airplane Models: 747-100, 747-100B, 747-200B, 747-200C, 747-200F, 747-400F, 747SP, 747SR GroupVariable Number 13RA001 - RA025 11RA026 1RA027 - RA028 11RA029 1RA030 - RA032 11RA033 1RA034 15RA101 - RA103 14RA104 - RA110 11RA111 - RA112 2RA113 - RA115 11RA161 - RA162 12RA163 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 15 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 16 GroupVariable Number 3RA164 14RA201 - RA203 1RA216 3RA217 1RA245 4RA246 13RA251 - RA254 1RA255 3RA256 - RA266 13RA301 - RA303 1RA304 - RA306 3RA307 - RA313 4RA314 - RA317 6RA318 13RA351 - RA355 1RA356 - RA360 1RA369 - RA371 3RA372 - RA373 14RA401 - RA403 2RA404 - RA412 3RA413 4RA414 - RA418 1RA501 - RA502 13RA521 - RA523 12RA524 3RA525 - RA528 1RA532 - RA534 3RA535 - RA543 4RA544 - RA548 13RA551 - RA552 1RA559 - RA560 3RA561 1RA581 - RA582 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 16 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 17 GroupVariable Number 3RA585 1RA601 - RA602 1RA631 11RA632 1RA633 12RA634 - RA635 1RA651 - RA652 1RA671 - RA674 3RA675 - RA677 1RA701 3RA702 1RA721 - RA722 3RA723 - RA724 4RA725 - RA731 1RA741 - RA743 3RA744 - RA745 4RA749 - RA750 1RA761 - RA762 1RA781 4RA782 - RA783 5RA784 15RA901 - RA902 14RA903 - RA904 2RA905 - RA909 11RA910 - RA916 4RB001 - RB016 15RB041 14RB042 15RB043 2RB044 3RB071 - RB075 1RB101 - RB102 6RB411 - RB413 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 17 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 18 GroupVariable Number 4RB421 4RB601 - RB603 5RB604 - RB605 4RB606 5RB607 6RB681 - RB695 7RB696 6RB697 6RB711 4RB721 - RB723 4RB741 - RB748 4RD001 - RD004 4RD021 - RD022 5RD041 4RD042 5RD043 - RD044 4RD045 - RD054 5RD055 4RD056 - RD059 4RD071 - RD072 4RD081 7RD082 - RD083 6RD091 - RD092 4RD101 - RD104 4RD121 6RD122 - RD127 6RD131 - RD141 7RD142 6RD143 7RD144 6RD166 - RD167 4RD171 - RD172 6RD181 - RD183 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 18 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 19 GroupVariable Number 6RD201 - RD204 6RD221 - RD224 7RD225 6RD226 7RD227 6RD231 - RD232 7RD233 - RD235 6RD241 - RD243 4RD251 - RD262 6RD271 - RD272 6RD291 - RD292 7RD301 - RD302 6RD311 6RD351 - RD357 7RD358 7RD361 - RD366 7RD411 - RD412 6RD413 - RD414 6RD421 - RD426 4RD431 - RD435 7RD441 - RD442 6RD451 - RD456 7RD461 6RD471 - RD475 6RD513 - RD519 6RD531 - RD533 5RD551 6RD561 4RD571 7RD581 - RD583 6RD591 - RD593 4RD621 5RD622 - RD623 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 19 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 20 GroupVariable Number 7RD641 - RD643 6RD644 - RD645 7RD646 6RD647 - RD649 6RD651 - RD659 6RD661 4RD671 6RD681 - RD682 7RD691 6RD692 6RD701 - RD702 6RD741 - RD742 6RD751 7RD752 6RD753 - RD755 6RD761 6RD771 - RD775 6RD781 - RD783 6RD791 - RD792 6RE001 17RG001 - RG009 17RG091 17RG095 17RG101 - RG104 17RG121 - RG126 17RG141 - RG142 17RG161 - RG164 17RG171 - RG174 17RG191 - RG193 17RG211 - RG213 17RG221 - RG222 18RH101 - RH102 17RH111 - RH112 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 20 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 21 GroupVariable Number 17RH121 - RH122 9RJ131 - RJ133 9RJ151 - RJ152 16RJ301 - RJ303 16RJ321 - RJ322 16RJ331 - RJ333 10RL401 - RL403 10RL411 - RL436 10RL451 - RL456 10RL461 - RL462 10RL471 - RL481 10RL491 - RL492 10RL501 - RL502 10RL511 - RL516 10RL521 - RL522 10RL531 - RL534 10RL551 10RL561 - RL568 10RL571 - RL572 10RL576 - RL577 10RL579 10RL581 - RL586 10RL651 - RL655 10RL671 - RL675 10RL681 - RL684 10RL751 - RL752 10RM851 - RM859 10RM861 - RM863 10RM871 - RM899 10RM901 - RM906 10RM911 8RR001 - RR005 8RR021 - RR025 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 21 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 22 GroupVariable Number 8RR031 8RR201 - RR206 8RR221 - RR226 8RR261 - RR267 8RR301 - RR310 8RR331 - RR332 8RR336 8RR341 - RR345 8RR361 - RR362 8RR421 - RR422 8RR431 - RR432 8RR441 - RR442 8RR451 8RR501 - RR504 8RR521 - RR522 8RR526 8RR531 8RR551 - RR556 8RR561 8RR566 10RR701 10RR721 - RR724 10RR746 - RR748 10RR851 - RR856 10RR861 - RR862 10RR951 - RR952 2. Spares Affected None. B. Concurrent Requirements None. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 22 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 23 C. Reason This service bulletin gives instructions for modification of upper deck tension ties and adjacent frame structure on non stretched upper deck (Non-SUD) airplanes. The tension ties have been determined to be structure that is susceptible to Widespread Fatigue Damage (WFD). WFD can cause tension ties to become severed or disconnected from the frames. Severed or disconnected Tension Ties and/or Frames at multiple locations could result in rapid in-flight decompression. For more information about WFD, refer to Boeing Service Letter 747-SL-53-088. Service Bulletin 747-53A2502 recommends initial and repeat inspections of Non-SUD airplane tension ties from body station (STA) 760 to STA 940 (STA 1040 to STA 1140 for 747SP). Service Bulletin 747-53A2502 was issued to address multiple reports of cracks found in tension ties and adjacent frame structure. Group 1-16: Accomplishment of the modification in this service bulletin terminates the repeat inspection requirement of Service Bulletin 747-53A2502. Group 17-18: Accomplishment of the modification in this service bulletin does not terminate the repeat inspection requirement of Service Bulletin 747-53A2502, but a new inspection threshold is provided. As a part of a service bulletin validation program, this modification and inspection was completed on airplane RD041 by Service Bulletin 747-53A2605, Original Issue. The modification and inspection completed on airplane RD041 by Service Bulletin 747-53A2605, Original Issue is equivalent to the Revision 2 of this service bulletin. Airplane RD041 has the configuration of a Group 5 airplane. Boeing Service Related Problem (SRP) 747-SRP-53-0200 and 747-SRP-53-0438 are related to this service bulletin. Revision 1 was sent to add more airplanes to the service bulletin effectivity and add Appendix A to give information on methods for disconnecting tension ties. Revision 2 was sent to tell operators that new retrofit drawings have been added for airplanes with barrier net fittings installed under the shear ties located at frame station (STA) 860. Subsequent to the release of Revision 2 of this service bulletin, Boeing has determined that additional inspections are required in the center sections of the tension ties where the tension tie channels are not replaced and where fastener holes are not zero-timed during modification. Revision 3 is sent to add the requirement to do surface high frequency eddy current (HFEC) inspection where fastener holes are not zero-timed during modification on Group 1-16 airplanes. Revision 3 also adds instructions for post-modification inspection of the entire tension tie for Group 1-16 airplanes, and adds effectivity and modification instructions for 747SP (Group 17-18) airplanes. D. Description Get access to the Frame to Tension Tie joints in Section 42. At each station, disconnect and remove a section of the tension tie between the frame and approximate Buttock Line (BL) 36. For each frame, remove a specified section of the frame above and below the tension tie attach point. After the existing frame and tension tie structure has been removed and discarded, install new frame and tension tie structure. Do the modification on both sides of the airplane. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 23 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 24 Group 1-16: Do surface high frequency eddy current (HFEC) inspection of the tension ties at fastener locations where the holes were not zero-timed during modification. If cracks are found, contact Boeing for repair instructions and do the repair. Group 1-16: After modification, do initial and repeat detailed, high frequency eddy current (HFEC), and low frequency eddy current (LFEC) inspections of the tension ties at the compliance time specified in paragraph 1.E., Compliance. If cracks are found, contact Boeing for repair instructions and do the repair. Group 17-18: After modification, do initial and repeat detailed and HFEC inspections for cracks in all tension ties, adjacent frame structure, and adjacent structure that attaches to the tension ties. If cracks are found, contact Boeing for repair instructions and do the repair. Revision 1 - No more work is necessary on airplanes changed in accordance with the original issue of this service bulletin. Revision 2 - No more work is necessary on airplanes changed in accordance with the original issue or Revision 1 of this service bulletin. Revision 3 - More work is necessary on airplanes modified in accordance with the original issue, Revision 1, or Revision 2 of this service bulletin. Airplanes previously modified in accordance with this service bulletin will require surface high frequency eddy current (HFEC) inspection for cracks in the forward and aft tension tie channels around fasteners in unmodified areas where fastener holes were not zero-timed during modification. Refer to paragraph 1.E., Compliance for the compliance time of this additional inspection. However, no additional modification is necessary. The work in this service bulletin is done in the maintenance zone(s) given below. Group 1, 3: Affected Maintenance Zones ZoneModel 233, 234, 243, 244747-100, 747-200B Group 2, 11-15: Affected Maintenance Zones ZoneModel 233, 234, 243, 244747-100 Group 4, 6: Affected Maintenance Zones ZoneModel 233, 234, 243, 244747-100, 747-100B, 747-200B, 747SR Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 24 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 25 Group 5, 7: Affected Maintenance Zones ZoneModel 233, 234, 243, 244747-200B, 747SR Group 8: Affected Maintenance Zones ZoneModel 233, 234, 243, 244747-200F Group 9, 16: Affected Maintenance Zones ZoneModel 233, 234, 243, 244747-200C Group 10: Affected Maintenance Zones ZoneModel 233, 234, 243, 244747-400F Group 17-18: Affected Maintenance Zones ZoneModel 243, 244747SP E. Compliance Federal Aviation Administration (FAA) Airworthiness Directives AD 84-19-01, AD 94-13-06, AD 2004-07-22 R1, and AD 2012-13-08 are related to this service bulletin. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 25 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 26 Group 1-16, Configuration 1: Table 1: Tension Tie and Frame - Inspection and Modification Repeat Interval (Not to Exceed) Compliance Time (Whichever Occurs Later) ActionCondition -Within 3,000 flight cycles af- ter August 14, 2012 (the effec- tive date of AD 2012-13-08). Before 30,000 total flight cy- cles. Do tension tie and frame modifica- tion in accordance with Paragraph 3.B., Work Instructions, PART 1. (a) All airplanes. AND -Within 3,000 flight cycles af- ter the Revision 3 date of this service bulletin. Concurrently with modifica- tion in accor- dance with Paragraph 3.B., Work Instruc- tions, PART 1. Do surface high frequency eddy current (HFEC) inspections for cracks in the tension tie center sections in accordance with Paragraph 3.B., Work Instruc- tions, PART 4. (b) -Before further flight.Contact Boeing for repair instruc- tions, and do the repair. Any crack found. -At the times specified in Para- graph 1.E., Compliance, Tables 2, 3 and 4, as applicable. Do post-modification inspections in accordance with Paragraph 1.E., Compliance, Tables 2, 3 and 4, as applicable. No crack found. (a) Due to the post-modification inspection requirements, Boeing does not recommend tension tie modification prior to 15,000 total flight cycles. (b) Boeing recommends accomplishment of the HFEC inspection before beginning the modification in case cracks are found in the center section and repairs are necessary that may affect the modification. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 26 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 27 Group 5, 7-8, 10-12, 15: Table 2: Post-Modification Detailed Inspection of Unmodified Areas of the Tension Ties Repeat Interval (Not to Exceed) Compliance TimeActionCondition -Within 6,000 flight cycles after modification in accordance with Paragraph 3.B., Work Instructions, PART 1. Do a detailed inspection for cracks in the unmodi- fied areas of the tension ties in accordance with Paragraph 3.B., Work In- structions, PART 2. Modification has been done in accordance with Para- graph 3.B., Work Instruc- tions, PART 1 of this ser- vice bulletin. 3,000 flight cycles.-Repeat the detailed in- spection for cracks in the unmodified areas of the tension ties in accor- dance with Paragraph 3.B., Work Instructions, PART 2. No crack found during in- spection in accordance with Paragraph 3.B., Work Instructions, PART 2. -Before further flight.Contact Boeing for repair instructions, and do the repair. Any crack found during in- spection in accordance with Paragraph 3.B., Work Instructions, PART 2. AND 3,000 flight cycles.-Repeat the detailed in- spection for cracks in the unmodified areas of the tension ties in accor- dance with Paragraph 3.B., Work Instructions, PART 2. Group 1-4, 6, 9, 13-14, 16: Table 3: Post-Modification Detailed Inspection of Unmodified Areas of the Tension Ties Repeat Interval (Not to Exceed) Compliance TimeActionCondition -Within 6,000 flight cycles after modification in accordance with Paragraph 3.B., Work Instructions, PART 1. Do a detailed inspection for cracks in the unmodi- fied areas of the tension ties in accordance with Paragraph 3.B., Work In- structions, PART 2. Modification has been done in accordance with Para- graph 3.B., Work Instruc- tions, PART 1 of this ser- vice bulletin. 4,000 flight cycles.-Repeat the detailed in- spection for cracks in the unmodified areas of the tension ties in accor- dance with Paragraph 3.B., Work Instructions, PART 2. No crack found during in- spection in accordance with Paragraph 3.B., Work Instructions, PART 2. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 27 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 28 Group 1-4, 6, 9, 13-14, 16: Table 3: Post-Modification Detailed Inspection of Unmodified Areas of the Tension Ties Repeat Interval (Not to Exceed) Compliance TimeActionCondition -Before further flight.Contact Boeing for repair instructions, and do the repair. Any crack found during in- spection in accordance with Paragraph 3.B., Work Instructions, PART 2. AND 4,000 flight cycles.-Repeat the detailed in- spection for cracks in the unmodified areas of the tension ties in accor- dance with Paragraph 3.B., Work Instructions, PART 2. Group 1-16: Table 4: Post-Modification Inspections of the Tension Ties in all Areas (Modified and Unmodified areas) Repeat Interval (Not to Exceed) Compliance TimeActionCondition -Within 20,000 flight cycles after modification in accordance with Paragraph 3.B., Work Instructions, PART 1. Do eddy current inspec- tions for cracks in all ar- eas of the tension ties in accordance with Para- graph 3.B., Work Instruc- tions, PART 3. Modification has been done in accordance with Para- graph 3.B., Work Instruc- tions, PART 1 of this ser- vice bulletin. 3,000 flight cycles.-Repeat the eddy current inspections for cracks in all areas of the tension ties in accordance with Paragraph 3.B., Work In- structions, PART 3. No crack found during in- spection in accordance with Paragraph 3.B., Work Instructions, PART 3. -Before further flight.Contact Boeing for repair instructions, and do the repair. Any crack found during in- spection in accordance with Paragraph 3.B., Work Instructions, PART 3. AND 3,000 flight cycles.-Repeat the eddy current inspections for cracks in all areas of the tension ties in accordance with Paragraph 3.B., Work In- structions, PART 3. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 28 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 29 Group 1-16, Configuration 2: Table 5: Surface HFEC Inspection of Unmodified Tension Tie Center Sections (More Work) Compliance Time (Whichever Occurs Later)ActionCondition Within 1,000 flight cycles after the Revision 3 date of this service bulletin. Within 3,000 flight cycles after accomplishment of the modification in accor- dance with Paragraph 3.B., Work Instructions, PART 1. Do a surface HFEC inspection for cracks in unmodified center sec- tions of the tension tie channels in accordance with Paragraph 3.B., Work Instructions, PART 4. All airplanes. -Before further flight.Contact Boeing for repair instruc- tions, and do the repair. Any crack found. --No further action is required until you begin inspections in accor- dance with Paragraph 1.E., Com- pliance, Tables 2, 3, and 4, as applicable. No crack found. Group 17: Table 6: Modification and Post-Modification Inspection of Tension Ties and Frame Segments Repeat Interval (Not to Exceed) Compliance Time (Whichever Occurs Later) ActionCondition -Within 3,000 flight cycles after August 14, 2012 (the effective date of AD 2012- 13-08). Before 30,000 total flight cycles. At each station location from STA 1040 to STA 1140, remove and replace existing tension tie and frame structure with new structure which is the same as the original pro- duction parts in accor- dance with Paragraph 3.B., Work Instructions, PART 5. All airplanes. 4,000 flight cy- cles. -Within 20,000 flight cycles after the tension tie and frame struc- ture was re- placed in accor- dance with Para- graph 3.B., Work Instructions, PART 5. Do inspections of the re- placed tension tie and frame structure in accor- dance with Service Bulletin 747-53A2502. Tension tie and frame structure has been re- moved and replaced with new parts in accor- dance with Paragraph 3.B., Work Instructions, PART 5. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 29 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 30 Group 18: Table 7: Modification and Post-Modification Inspection of Tension Ties and Frame Segments Repeat Interval (Not to Exceed) Compliance Time (Whichever Occurs Later) ActionCondition -Within 3,000 flight cycles after August 14, 2012 (the effective date of AD 2012- 13-08). Before 30,000 total flight cycles. At each station location from STA 1060 to STA 1140, remove and replace existing tension tie and frame structure with new structure which is the same as the original pro- duction parts in accor- dance with Paragraph 3.B., Work Instructions, PART 6. All airplanes. 4,000 flight cy- cles. -Within 20,000 flight cycles after the tension tie and frame struc- ture was re- placed in accor- dance with Para- graph 3.B., Work Instructions, PART 6. Do inspections of the re- placed tension tie and frame structure in accor- dance with Service Bulletin 747-53A2502. Tension tie and frame structure has been re- moved and replaced with new parts in accor- dance with Paragraph 3.B., Work Instructions, PART 6. F. Approval This service bulletin was examined by the Federal Aviation Administration (FAA). The changes specified in this service bulletin comply with the applicable regulations and are FAA approved, as well as European Aviation Safety Agency (EASA)/Joint Aviation Authorities (JAA) approved for all EASA/JAA approved airplanes listed in the service bulletin effectivity. This service bulletin and its approval were based on the airplane in its original Boeing delivery configuration or as modified by other approved Boeing changes. If an airplane has a non-Boeing modification or repair that affects a component or system also affected by this service bulletin, the operator is responsible for obtaining appropriate regulatory agency approval before incorporating this service bulletin. This SB has been approved by the FAA. In addition, the Manager of the Seattle Aircraft Certification Office (ACO) approves the accomplishment of the modification, post modification inspection and corrective action with the corresponding compliance times specified in Table 1, under paragraph 1.E., "Compliance," of SB 747-53A2605, Revision 3, as an AMOC to the inspections and corrective action required by paragraphs (h) and (i) of AD 2004-07-22 R1, for the inspection of Structural Significant Item (SSI) F-19A of the Supplemental Structural Inspection Document (SSID) D6-35022, Revision G. This AMOC only applies to the areas inspected by this service bulletin. When this SB specifies contacting Boeing for repair instructions and post modification inspections, the repair instructions and post modification inspections must be approved by the FAA in accordance with paragraph (I) of the AD. All provisions of AD 2004-07-22 R1 that are not specifically referenced in this paragraph remain fully applicable and must be complied with accordingly. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 30 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 31 Group 1-16: In addition, the Manager of the Seattle ACO approves the accomplishment of the inspections, modification, post-modification inspections, and related corrective actions with corresponding compliance times specified in Tables 1, 2, 3, 4, and 5 (as applicable) under paragraph 1.E., "Compliance," of Service Bulletin 747-53A2605, Revision 3 as an AMOC to the inspections, investigative actions, modification, post-modification, and repair actions with corresponding compliance times required by paragraphs (g), (h), (i), (j)(1), (k), and (l) of AD 2012-13-08. When this service bulletin specifies contacting Boeing for repair instructions, the repair instructions must be approved by the FAA in accordance with paragraph (n) of the AD. All provisions of AD 2012-13-08 that are not specifically referenced in this paragraph remain fully applicable and must be complied with accordingly. Group 17-18: In addition, the Manager of the Seattle ACO approves the accomplishment of the modification and post-modification inspections with corresponding compliance times specified in Table 6 or 7 (as applicable) under paragraph 1.E., "Compliance," of Service Bulletin 747-53A2605, Revision 3 as an AMOC to the inspections, investigative actions, corrective actions, modification, and post-modification actions with corresponding compliance times required by paragraphs (g) and (j)(2) of AD 2012-13-08. When this service bulletin specifies contacting Boeing for repair instructions, the repair instructions must be approved by the FAA in accordance with paragraph (n) of the AD. All provisions of AD 2012-13-08 that are not specifically referenced in this paragraph remain fully applicable and must be complied with accordingly. In addition, the Manager of the Seattle ACO approves the accomplishment of the modification, inspections and repair with the corresponding compliance times specified in Tables 1, 2, 3, 4, and 5 under paragraph 1.E., "Compliance," of Service Bulletin 747-53A2605, Revision 3 as an AMOC to the inspections, repair and modification with the corresponding compliance times required by paragraphs A. and B. of AD 84-19-01. When this service bulletin specifies contacting Boeing for repair instructions, the repair instructions must be approved by the FAA in accordance with paragraph C. of the AD. All provisions of AD 84-19-01 that are not specifically referenced in this paragraph, including but not limited to repeat inspections in accordance with paragraphs A. and B. until the modification in accordance with Service Bulletin 747-53A2605, Revision 3 is installed, remain fully applicable and must be complied with accordingly. In addition, the Manager of the Seattle ACO approves the accomplishment of the modification, inspections and repair with the corresponding compliance times specified in Tables 1, 2, 3, 4, and 5 under paragraph 1.E., "Compliance," of Service Bulletin 747-53A2605, Revision 3 as an AMOC to the inspections, repair and modification with the corresponding compliance times required by paragraphs (a) and (b) of AD 94-13-06. When this service bulletin specifies contacting Boeing for repair instructions, the repair instructions must be approved by the FAA in accordance with paragraph (c) of the AD. All provisions of AD 94-13-06 that are not specifically referenced in this paragraph, including but not limited to repeat inspections in accordance with paragraphs (a) and (b) until the modification in accordance with Service Bulletin 747-53A2605, Revision 3 is installed, remain fully applicable and must be complied with accordingly. G. Manpower The table below shows an estimate of the task hours necessary to do the modification for each airplane. This estimate is for direct labor only, done by an experienced crew. Adjust the estimate with operator task hour data if necessary. The estimate does not include lost time. These are some examples of lost time: — Time to adjust to the workplace — Time to schedule the work Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 31 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 32 — Time to inspect the work — Time to cure the materials — Time to make the parts — Time to find the tools. Elapsed HoursTask HoursNumber of PersonsTask 6.0024.004Access 7.5030.004Restoration 13.5054.00TOTAL FOR EACH AIRPLANE Group 1-5, 8-9, 11-16: Shear Panel Removal/Installation Elapsed HoursTask HoursNumber of PersonsTask 5.0010.002Remove 5.0010.002Install 10.0020.00TOTAL FOR EACH AIRPLANE Group 6-7: Shear Panel Removal/Installation Elapsed HoursTask HoursNumber of PersonsTask 5.0010.002Remove 5.0010.002Install 10.0020.00TOTAL FOR EACH AIRPLANE Group 10: Shear Panel Removal/Installation Elapsed HoursTask HoursNumber of PersonsTask 5.0010.002Remove 5.0010.002Install 10.0020.00TOTAL FOR EACH AIRPLANE Group 10: STA 720 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 3.5014.004Remove 3.5014.004Install 7.0028.00TOTAL FOR EACH AIRPLANE Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 32 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 33 Group 10: STA 740 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 3.5014.004Remove 3.5014.004Install 7.0028.00TOTAL FOR EACH AIRPLANE Group 1, 13: STA 760 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 3.7515.004Remove 3.7515.004Install 7.5030.00TOTAL FOR EACH AIRPLANE Group 2-3, 14: STA 760 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 3.2513.004Remove 3.2513.004Install 6.5026.00TOTAL FOR EACH AIRPLANE Group 10: STA 760 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 3.0012.004Remove 3.0012.004Install 6.0024.00TOTAL FOR EACH AIRPLANE Group 1-2, 8, 11, 13-15: STA 780 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 3.5014.004Remove 3.5014.004Install 7.0028.00TOTAL FOR EACH AIRPLANE Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 33 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 34 Group 3, 12: STA 780 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 3.2513.004Remove 3.2513.004Install 6.5026.00TOTAL FOR EACH AIRPLANE Group 10: STA 780 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 2.5010.004Remove 2.5010.004Install 5.0020.00TOTAL FOR EACH AIRPLANE Group 1-5, 8-9, 11-16: STA 800 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 3.2513.004Remove 3.2513.004Install 6.5026.00TOTAL FOR EACH AIRPLANE Group 10: STA 800 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 2.5010.004Remove 2.5010.004Install 5.0020.00TOTAL FOR EACH AIRPLANE Group 1-5, 9, 11-16: STA 820 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 13.0052.004Remove 13.0052.004Install 26.00104.00TOTAL FOR EACH AIRPLANE Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 34 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 35 Group 8, 10: STA 820 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 13.7555.004Remove 13.7555.004Install 27.50110.00TOTAL FOR EACH AIRPLANE Group 1-5, 9-16: STA 840 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 12.0048.004Remove 12.0048.004Install 24.0096.00TOTAL FOR EACH AIRPLANE Group 6-7: STA 840 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 11.7547.004Remove 11.7547.004Install 23.5094.00TOTAL FOR EACH AIRPLANE Group 8: STA 840 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 13.0052.004Remove 13.0052.004Install 26.00104.00TOTAL FOR EACH AIRPLANE Group 1-5, 8, 11-15: STA 860 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 13.7555.004Remove 13.7555.004Install 27.50110.00TOTAL FOR EACH AIRPLANE Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 35 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 36 Group 6-7: STA 860 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 13.0052.004Remove 13.0052.004Install 26.00104.00TOTAL FOR EACH AIRPLANE Group 9, 16: STA 860 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 13.5054.004Remove 13.5054.004Install 27.00108.00TOTAL FOR EACH AIRPLANE Group 10: STA 860 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 12.7551.004Remove 12.7551.004Install 25.50102.00TOTAL FOR EACH AIRPLANE Group 1-9, 11-16: STA 880 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 14.0056.002Remove 14.0056.002Install 28.00112.00TOTAL FOR EACH AIRPLANE Group 10: STA 880 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 12.5050.004Remove 12.5050.004Install 25.00100.00TOTAL FOR EACH AIRPLANE Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 36 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 37 Group 1-4, 6, 13-14: STA 900 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 13.0052.004Remove 13.0052.004Install 26.00104.00TOTAL FOR EACH AIRPLANE Group 5, 7, 16: STA 900 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 12.2549.004Remove 12.2549.004Install 24.5098.00TOTAL FOR EACH AIRPLANE Group 8: STA 900 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 12.7551.004Remove 12.7551.004Install 25.50102.00TOTAL FOR EACH AIRPLANE Group 9-10: STA 900 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 12.0048.004Remove 12.0048.004Install 24.0096.00TOTAL FOR EACH AIRPLANE Group 11-12, 15: STA 900 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 13.0052.004Remove 13.0052.004Install 26.00104.00TOTAL FOR EACH AIRPLANE Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 37 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 38 STA 920 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 12.5050.004Remove 12.5050.004Install 25.00100.00TOTAL FOR EACH AIRPLANE Group 1-2, 11: STA 940 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 14.2557.004Remove 14.2557.004Install 28.50114.00TOTAL FOR EACH AIRPLANE Group 3-4, 6, 12: STA 940 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 14.5058.004Remove 14.5058.004Install 29.00116.00TOTAL FOR EACH AIRPLANE Group 5, 7, 9, 16: STA 940 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 16.0064.004Remove 16.0064.004Install 32.00128.00TOTAL FOR EACH AIRPLANE Group 8: STA 940 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 14.0056.004Remove 14.0056.004Install 28.00112.00TOTAL FOR EACH AIRPLANE Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 38 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 39 Group 10: STA 940 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 16.2565.004Remove 16.2565.004Install 32.50130.00TOTAL FOR EACH AIRPLANE Group 13-15: STA 940 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 13.0052.004Remove 13.0052.004Install 26.00104.00TOTAL FOR EACH AIRPLANE Group 17: STA 1040 - STA 1140 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 32.25129.004Remove 64.50258.004Install 96.75387.00TOTAL FOR EACH AIRPLANE Group 18: STA 1060 - STA 1140 Tension Tie and Frame Modification Elapsed HoursTask HoursNumber of PersonsTask 27.00108.004Remove 54.00216.004Install 81.00324.00TOTAL FOR EACH AIRPLANE Group 1-3, 13-14: Surface HFEC Inspection of Tension Tie Center Sections Elapsed HoursTask HoursNumber of PersonsTask 25.00100.004FIGURE 1 25.00100.00TOTAL FOR EACH AIRPLANE Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 39 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 40 Group 4, 9: Surface HFEC Inspection of Tension Tie Center Sections Elapsed HoursTask HoursNumber of PersonsTask 20.0080.004FIGURE 2 20.0080.00TOTAL FOR EACH AIRPLANE Group 5, 16: Surface HFEC Inspection of Tension Tie Center Sections Elapsed HoursTask HoursNumber of PersonsTask 17.5070.004FIGURE 3 17.5070.00TOTAL FOR EACH AIRPLANE Group 6: Surface HFEC Inspection of Tension Tie Center Sections Elapsed HoursTask HoursNumber of PersonsTask 15.0060.004FIGURE 4 15.0060.00TOTAL FOR EACH AIRPLANE Group 7: Surface HFEC Inspection of Tension Tie Center Sections Elapsed HoursTask HoursNumber of PersonsTask 12.5050.004FIGURE 5 12.5050.00TOTAL FOR EACH AIRPLANE Group 8, 11-12, 15: Surface HFEC Inspection of Tension Tie Center Sections Elapsed HoursTask HoursNumber of PersonsTask 20.0080.004FIGURE 6 20.0080.00TOTAL FOR EACH AIRPLANE Group 10: Surface HFEC Inspection of Tension Tie Center Sections Elapsed HoursTask HoursNumber of PersonsTask 30.00120.004FIGURE 7 30.00120.00TOTAL FOR EACH AIRPLANE Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 40 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 41 Group 1-16: Post-Modification Inspections of All Areas of the Tension Ties Elapsed HoursTask HoursNumber of PersonsTask 9.00 (a)18.00 (a)2FIGURE 8 9.00 (a)18.00 (a)2FIGURE 9 (a)(a)TOTAL FOR EACH TENSION TIE (a) Estimates given are for each tension tie location. Multiply the estimates by the number of tension ties to determine the total estimate for the airplane. H. Weight and Balance Changes Group 1-2, 13-14: Change in Moment (Pound-Inches) Change in Weight (Pounds)Airplane +247016.2+286.2747-100, 747-200B Group 3: Change in Moment (Pound-Inches) Change in Weight (Pounds)Airplane +241382.6+280.2747-100, 747-200B Group 4-5, 9, 16: Change in Moment (Pound-Inches) Change in Weight (Pounds)Airplane +213354.9+243.8747-100, 747-100B, 747-200B, 747SR, 747-200C Group 6-7: Change in Moment (Pound-Inches) Change in Weight (Pounds)Airplane +172879.8+193.9747-100, 747-100B, 747-200B, 747SR Group 8, 12: Change in Moment (Pound-Inches) Change in Weight (Pounds)Airplane +227550.8+262.0747-100, 747-200F Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 41 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 42 Group 10: Change in Moment (Pound-Inches) Change in Weight (Pounds)Airplane +273811.8+322.6747-400F Group 11, 15: Change in Moment (Pound-Inches) Change in Weight (Pounds)Airplane +233184.4+268.0747-100 Group 17-18: None. I. Electrical Load Data Not changed. J. References 1. Existing Data: a. Engineering Change Memo PRR 85901-68RS b. Boeing Service Bulletin 747-53A2502, 747-53A2605 c. Boeing Service Letter 747-SL-51-048, 747-SL-53-088 d. Boeing Service Related Problem (SRP) 747-SRP-53-0200, 747-SRP-53-0438 e. Federal Aviation Administration (FAA) Airworthiness Directive (AD) 2004-07-22 R1, 2012-13-08, 84-19-01, 94-13-06 f. Standard Overhaul Practices Manual (SOPM) 20-41-01, 20-41-05, 20-43-03 g. 747 Non-Destructive Testing (NDT) Manual Part 6, 51-00-00, Part 6, 51-00-26 h. 747-100/200/300 Aircraft Maintenance Manual (AMM) 24-22-00, 25-21-04, 25-22-01, 25-25-01 i. 747-100/200/300 Structural Repair Manual (SRM) 51-10-01, 51-30-09 j. 747-400 Aircraft Maintenance Manual (AMM) 24-22-00, 25-21-04, 25-22-01, 25-25-01 k. 747-400F Structural Repair Manual (SRM) 51-10-02, 51-40-09 2. Data Supplied with this Service Bulletin: a. Drawings: Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 42 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 43 ADCNDCN/REVSheetTitleDrawing No -A1TOP KIT - FRAME AND TENSION TIE MODIFICATION, STA 720 - STA 940 142U0100 --10 --11 -A12 -A13 --14 --15 --2 --3 --4 --5 -A6 --7 -A8 -A9 -AKPLTOP KIT - FRAME AND TENSION TIE MODIFICATION 142U0100-1001 -AKPLTOP KIT - FRAME AND TENSION TIE MODIFICATION 142U0100-1002 -AKPLTOP KIT - FRAME AND TENSION TIE MODIFICATION 142U0100-1003 -BKPLTOP KIT - FRAME AND TENSION TIE MODIFICATION 142U0100-1004 -BKPLTOP KIT - FRAME AND TENSION TIE MODIFICATION 142U0100-1005 -AKPLTOP KIT - FRAME AND TENSION TIE MODIFICATION 142U0100-1006 -BKPLTOP KIT - FRAME AND TENSION TIE MODIFICATION 142U0100-1007 -CKPLTOP KIT - FRAME AND TENSION TIE MODIFICATION 142U0100-1008 -BKPLTOP KIT - FRAME AND TENSION TIE MODIFICATION 142U0100-1009 -BKPLTOP KIT - FRAME AND TENSION TIE MODIFICATION 142U0100-1010 -BKPLTOP KIT - FRAME AND TENSION TIE MODIFICATION 142U0100-1011 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 43 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 44 ADCNDCN/REVSheetTitleDrawing No -BKPLTOP KIT - FRAME AND TENSION TIE MODIFICATION 142U0100-1012 -AKPLTOP KIT - FRAME AND TENSION TIE MODIFICATION 142U0100-1013 -AKPLTOP KIT - FRAME AND TENSION TIE MODIFICATION 142U0100-2001 -AKPLTOP KIT - FRAME AND TENSION TIE MODIFICATION 142U0100-2002 --1KIT - FRAME MODIFICATION, STA 820 - STA 940 142U0101 --10 --11 --12 --13 --14 --15 -A16 --17 -A18 --19 --2 --20 --21 --22 --23 --24 --3 --4 -A5 -A6 --7 -A8 --9 -CPSDLKIT - FRAME MODIFICATION, STA 820 - STA 940 142U0101#DL -AKPLKIT - FRAME MODIFICATION142U0101-101 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 44 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 45 ADCNDCN/REVSheetTitleDrawing No -AKPLKIT - FRAME MODIFICATION142U0101-102 -AKPLKIT - FRAME MODIFICATION142U0101-103 -AKPLKIT - FRAME MODIFICATION142U0101-104 -AKPLKIT - FRAME MODIFICATION142U0101-105 -AKPLKIT - FRAME MODIFICATION142U0101-106 -AKPLKIT - FRAME MODIFICATION142U0101-107 -AKPLKIT - FRAME MODIFICATION142U0101-108 -AKPLKIT - FRAME MODIFICATION142U0101-109 -AKPLKIT - FRAME MODIFICATION142U0101-110 -AKPLKIT - FRAME MODIFICATION142U0101-111 -AKPLKIT - FRAME MODIFICATION142U0101-112 -AKPLKIT - FRAME MODIFICATION142U0101-113 -AKPLKIT - FRAME MODIFICATION142U0101-114 -AKPLKIT - FRAME MODIFICATION142U0101-115 -AKPLKIT - FRAME MODIFICATION142U0101-116 -AKPLKIT - FRAME MODIFICATION142U0101-117 -AKPLKIT - FRAME MODIFICATION142U0101-119 -AKPLKIT - FRAME MODIFICATION142U0101-120 -AKPLKIT - FRAME MODIFICATION142U0101-121 -AKPLKIT - FRAME MODIFICATION142U0101-123 -AKPLKIT - FRAME MODIFICATION142U0101-124 -AKPLKIT - FRAME MODIFICATION142U0101-125 -AKPLKIT - FRAME MODIFICATION142U0101-126 -AKPLKIT - FRAME MODIFICATION142U0101-127 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 45 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 46 ADCNDCN/REVSheetTitleDrawing No -A1KIT - TENSION TIE MODIFICATION, STA 720 - STA 940 142U0102 -A10 -A11 -A12 -A13 -A14 -B15 -B16 -A17 -A18 -A19 -A2 -A20 -A21 -A22 -A23 -A24 -A25 -A26 -A27 -A28 -A29 -A3 -A30 -A31 -A32 -A33 --34 --35 --36 --37 -A4 -A5 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 46 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 47 ADCNDCN/REVSheetTitleDrawing No 6- A -A7 -A8 -A9 -APSDLKIT - TENSION TIE MODIFICATION, STA 720 - STA 940 142U0102#DL -BKPLKIT - TENSION TIE MODIFICATION142U0102-201 -BKPLKIT - TENSION TIE MODIFICATION142U0102-202 -BKPLKIT - TENSION TIE MODIFICATION142U0102-203 -BKPLKIT - TENSION TIE MODIFICATION142U0102-204 -BKPLKIT - TENSION TIE MODIFICATION142U0102-205 -BKPLKIT - TENSION TIE MODIFICATION142U0102-206 -BKPLKIT - TENSION TIE MODIFICATION142U0102-207 -BKPLKIT - TENSION TIE MODIFICATION142U0102-208 -BKPLKIT - TENSION TIE MODIFICATION142U0102-209 -BKPLKIT - TENSION TIE MODIFICATION142U0102-210 -BKPLKIT - TENSION TIE MODIFICATION142U0102-211 -BKPLKIT - TENSION TIE MODIFICATION142U0102-212 -BKPLKIT - TENSION TIE MODIFICATION142U0102-213 -BKPLKIT - TENSION TIE MODIFICATION142U0102-214 -BKPLKIT - TENSION TIE MODIFICATION142U0102-215 -BKPLKIT - TENSION TIE MODIFICATION142U0102-216 -BKPLKIT - TENSION TIE MODIFICATION142U0102-217 -BKPLKIT - TENSION TIE MODIFICATION142U0102-218 -BKPLKIT - TENSION TIE MODIFICATION142U0102-219 -BKPLKIT - TENSION TIE MODIFICATION142U0102-220 -BKPLKIT - TENSION TIE MODIFICATION142U0102-221 -BKPLKIT - TENSION TIE MODIFICATION142U0102-222 -BKPLKIT - TENSION TIE MODIFICATION142U0102-223 -BKPLKIT - TENSION TIE MODIFICATION142U0102-224 -BKPLKIT - TENSION TIE MODIFICATION142U0102-225 -BKPLKIT - TENSION TIE MODIFICATION142U0102-226 -BKPLKIT - TENSION TIE MODIFICATION142U0102-227 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 47 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 48 ADCNDCN/REVSheetTitleDrawing No -BKPLKIT - TENSION TIE MODIFICATION142U0102-228 -BKPLKIT - TENSION TIE MODIFICATION142U0102-229 -BKPLKIT - TENSION TIE MODIFICATION142U0102-230 -BKPLKIT - TENSION TIE MODIFICATION142U0102-231 -BKPLKIT - TENSION TIE MODIFICATION142U0102-232 -BKPLKIT - TENSION TIE MODIFICATION142U0102-233 -AKPLKIT - TENSION TIE MODIFICATION142U0102-234 -AKPLKIT - TENSION TIE MODIFICATION142U0102-235 -AKPLKIT - TENSION TIE MODIFICATION142U0102-301 -AKPLKIT - TENSION TIE MODIFICATION142U0102-302 -AKPLKIT - TENSION TIE MODIFICATION142U0102-303 --1TENSION TIE - INSPECTION624U0077 --2 -F4FRAME INSTL - STA 104065B01745 -B6 -A7 -YPL --PSDL -H1FRAME INSTL - STA 106065B01746 -E4 -C6 -A7 --8 -AAPL --PSDL -G1FRAME INSTL - STA 108065B01747 -E4 -C6 -A7 --8 -YPL --PSDL Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 48 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 49 ADCNDCN/REVSheetTitleDrawing No -E4FRAME INSTL - STA 110065B01748 -B6 -A7 -YPL --PSDL -D4FRAME INSTL - STA 112065B01749 -C7 -A8 -YPL --PSDL -C10TENSION TIE INSTL - AFT OF UPPER DECK FLOOR 65B09631 -E9 -AGPL --PSDL -C2BULKHEAD INSTL - MID SPAR BODY - STA 1140 65B18703 -B3 -A4 -APL --PSDL 3. Installation Drawings Used in the Preparation of this Service Bulletin: None. K. Publications Affected 1. Publications Chapter-SectionPublication 53-11747-100/200/300 Structural Repair Manual 53-20747-400F Structural Repair Manual 2. Damage Tolerance Based Structural Inspections: Boeing has evaluated the repairs and/or changes in this service bulletin for effects on Fatigue Critical Structure (FCS) and for changes to Damage Tolerance Inspections (DTI) required in the Maintenance Program. This service bulletin affects FCS. DTI requirements for the structure affected are contained in Paragraph 1.E., Compliance of this service bulletin. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 49 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 50 L. Interchangeability and Intermixability of Parts Accomplishment of this service bulletin does not affect interchangeability or intermixability of parts. M. Software Accomplishment Summary Not affected. Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 50 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 51 2. MATERIAL INFORMATION A. Material - Price and Availability Boeing can supply the kits shown in Paragraph 2.C., Parts Necessary for Each Airplane. Operators are encouraged to share schedule requirements with Boeing for incorporation of the service bulletin. The kits are subject to the terms and conditions of the Boeing standard purchase order acknowledgment. Prices are in United States Dollars. Terms: Net 30 days. Reference this service bulletin and submit your purchase order by one of these methods: 1. Order on-line via ATA Spec 2000 or The Boeing PART Page 2. Fax to (206) 662-7145 REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION Price as of the Revi- sion 02 date of this Service Bulletin (US Dollars) ROLT as of the Revi- sion 02 date of this Service Bulletin (Calendar Days) QTYDateNameKit Number 635,004.0039918/26/09TOP KIT - TENSION TIE AND FRAME MODIFICATION 142U0100-1001 634,277.00399-(a)TOP KIT - TENSION TIE AND FRAME MODIFICATION 142U0100-1002 655,323.0039918/28/09TOP KIT - TENSION TIE AND FRAME MODIFICATION 142U0100-1003 623,027.0039918/31/09TOP KIT - TENSION TIE AND FRAME MODIFICATION 142U0100-1004 623,719.0039919/03/09TOP KIT - TENSION TIE AND FRAME MODIFICATION 142U0100-1005 535,131.0039919/04/09TOP KIT - TENSION TIE AND FRAME MODIFICATION 142U0100-1006 535,823.0039919/08/09TOP KIT - TENSION TIE AND FRAME MODIFICATION 142U0100-1007 645,067.0039919/10/09TOP KIT - TENSION TIE AND FRAME MODIFICATION 142U0100-1008 623,537.00399-(a)TOP KIT - TENSION TIE AND FRAME MODIFICATION 142U0100-1009 658,423.00399-(a)TOP KIT - TENSION TIE AND FRAME MODIFICATION 142U0100-1010 618,575.0039919/11/09TOP KIT - TENSION TIE AND FRAME MODIFICATION 142U0100-1011 639,219.00399-(a)TOP KIT - TENSION TIE AND FRAME MODIFICATION 142U0100-1012 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 51 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 52 REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION Price as of the Revi- sion 02 date of this Service Bulletin (US Dollars) ROLT as of the Revi- sion 02 date of this Service Bulletin (Calendar Days) QTYDateNameKit Number 623,268.00(a)-(a)TOP KIT - FRAME AND TEN- SION TIE MODIFICATION 142U0100-1013 18,657.00399-(a)TOP KIT - TENSION TIE AND FRAME MODIFICATION 142U0100-2001 21,288.00399-(a)TOP KIT - TENSION TIE AND FRAME MODIFICATION 142U0100-2002 (a) Contact Boeing Spares for kit availability. NOTE: Due to the limited number of kits available and the long ROLT, Boeing recommends that operators submit purchase orders 18 months in advance of performing the modification. B. Industry Support Information Boeing warranty remedies are not available for the inspection or modification procedures given in this service bulletin. C. Parts Necessary for Each Airplane 1. Kits/Parts: NOTE: The top kits shown in the table that follows and the items shown in Paragraph 2.C.2., Parts and Materials Supplied by the Operator, are necessary for each airplane. To get the kits/parts shown below, refer to Paragraph 2.A., Material - Price and Availability. Top KitGroup(s) 142U0100-1001 and 142U0100-20021 142U0100-1002 and 142U0100-20022 142U0100-10033 142U0100-10044 142U0100-10055 142U0100-10066 142U0100-10077 142U0100-10088 142U0100-10099 142U0100-101010 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 52 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 53 Top KitGroup(s) 142U0100-1011 and 142U0100-200211 142U0100-101212 142U0100-1001 and 142U0100-200113 142U0100-1002 and 142U0100-200114 142U0100-1011 and 142U0100-200115 142U0100-101316 (a)17-18 (a) Only operator supplied parts are needed for Group 17-18. Group 1, 13: Kit 142U0100 NotesExisting Part NumberNameQTYNew Part Number -1001 KIT - FRAME MODIFICA- TION, STA 820 1142U0101-101 KIT - FRAME MODIFICA- TION, STA 840 1142U0101-104 KIT - FRAME MODIFICA- TION, STA 860 1142U0101-107 KIT - FRAME MODIFICA- TION, STA 880 1142U0101-111 KIT - FRAME MODIFICA- TION, STA 900 1142U0101-113 KIT - FRAME MODIFICA- TION, STA 920 1142U0101-117 KIT - FRAME MODIFICA- TION, STA 940 1142U0101-121 KIT - TENSION TIE MODI- FICATION, STA 760 1142U0102-203 KIT - TENSION TIE MODI- FICATION, STA 780 1142U0102-207 KIT - TENSION TIE MODI- FICATION, STA 800 1142U0102-210 KIT - TENSION TIE MODI- FICATION, STA 820 1142U0102-212 KIT - TENSION TIE MODI- FICATION, STA 840 1142U0102-214 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 53 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 54 Group 1, 13: Kit 142U0100 NotesExisting Part NumberNameQTYNew Part Number -1001 KIT - TENSION TIE MODI- FICATION, STA 860 1142U0102-217 KIT - TENSION TIE MODI- FICATION, STA 880 1142U0102-220 KIT - TENSION TIE MODI- FICATION, STA 900 1142U0102-222 KIT - TENSION TIE MODI- FICATION, STA 920 1142U0102-225 KIT - SHEAR PANEL INSTL - TENSION TIE MODIFICA- TION 1142U0102-301 Group 2, 14: Kit 142U0100 NotesExisting Part NumberNameQTYNew Part Number -1002 KIT - FRAME MODIFICA- TION, STA 820 1142U0101-101 KIT - FRAME MODIFICA- TION, STA 840 1142U0101-104 KIT - FRAME MODIFICA- TION, STA 860 1142U0101-107 KIT - FRAME MODIFICA- TION, STA 880 1142U0101-111 KIT - FRAME MODIFICA- TION, STA 900 1142U0101-113 KIT - FRAME MODIFICA- TION, STA 920 1142U0101-117 KIT - FRAME MODIFICA- TION, STA 940 1142U0101-121 KIT - TENSION TIE MODIFI- CATION, STA 760 1142U0102-204 KIT - TENSION TIE MODIFI- CATION, STA 780 1142U0102-207 KIT - TENSION TIE MODIFI- CATION, STA 800 1142U0102-210 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 54 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 55 Group 2, 14: Kit 142U0100 NotesExisting Part NumberNameQTYNew Part Number -1002 KIT - TENSION TIE MODIFI- CATION, STA 820 1142U0102-212 KIT - TENSION TIE MODIFI- CATION, STA 840 1142U0102-214 KIT - TENSION TIE MODIFI- CATION, STA 860 1142U0102-217 KIT - TENSION TIE MODIFI- CATION, STA 880 1142U0102-220 KIT - TENSION TIE MODIFI- CATION, STA 900 1142U0102-222 KIT - TENSION TIE MODIFI- CATION, STA 920 1142U0102-225 KIT - SHEAR PANEL INSTL - TENSION TIE MODIFICA- TION 1142U0102-301 Group 3: Kit 142U0100 NotesExisting Part NumberNameQTYNew Part Number -1003 KIT - FRAME MODIFICA- TION, STA 820 1142U0101-101 KIT - FRAME MODIFICA- TION, STA 840 1142U0101-104 KIT - FRAME MODIFICA- TION, STA 860 1142U0101-107 KIT - FRAME MODIFICA- TION, STA 880 1142U0101-111 KIT - FRAME MODIFICA- TION, STA 900 1142U0101-113 KIT - FRAME MODIFICA- TION, STA 920 1142U0101-117 KIT - FRAME MODIFICA- TION, STA 940 1142U0101-121 KIT - TENSION TIE MODIFI- CATION, STA 760 1142U0102-205 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 55 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 56 Group 3: Kit 142U0100 NotesExisting Part NumberNameQTYNew Part Number -1003 KIT - TENSION TIE MODIFI- CATION, STA 780 1142U0102-208 KIT - TENSION TIE MODIFI- CATION, STA 800 1142U0102-210 KIT - TENSION TIE MODIFI- CATION, STA 820 1142U0102-212 KIT - TENSION TIE MODIFI- CATION, STA 840 1142U0102-214 KIT - TENSION TIE MODIFI- CATION, STA 860 1142U0102-217 KIT - TENSION TIE MODIFI- CATION, STA 880 1142U0102-220 KIT - TENSION TIE MODIFI- CATION, STA 900 1142U0102-222 KIT - TENSION TIE MODIFI- CATION, STA 920 1142U0102-225 KIT - TENSION TIE MODIFI- CATION, STA 940 1142U0102-229 KIT - SHEAR PANEL INSTL - TENSION TIE MODIFICA- TION 1142U0102-301 Group 4: Kit 142U0100 NotesExisting Part NumberNameQTYNew Part Number -1004 KIT - FRAME MODIFICA- TION, STA 820 1142U0101-101 KIT - FRAME MODIFICA- TION, STA 840 1142U0101-104 KIT - FRAME MODIFICA- TION, STA 860 1142U0101-107 KIT - FRAME MODIFICA- TION, STA 880 1142U0101-111 KIT - FRAME MODIFICA- TION, STA 900 1142U0101-113 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 56 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 57 Group 4: Kit 142U0100 NotesExisting Part NumberNameQTYNew Part Number -1004 KIT - FRAME MODIFICA- TION, STA 920 1142U0101-117 KIT - FRAME MODIFICA- TION, STA 940 1142U0101-121 KIT - TENSION TIE MODI- FICATION, STA 800 1142U0102-210 KIT - TENSION TIE MODI- FICATION, STA 820 1142U0102-212 KIT - TENSION TIE MODI- FICATION, STA 840 1142U0102-214 KIT - TENSION TIE MODI- FICATION, STA 860 1142U0102-217 KIT - TENSION TIE MODI- FICATION, STA 880 1142U0102-220 KIT - TENSION TIE MODI- FICATION, STA 900 1142U0102-222 KIT - TENSION TIE MODI- FICATION, STA 920 1142U0102-225 KIT - TENSION TIE MODI- FICATION, STA 940 1142U0102-229 KIT - SHEAR PANEL INSTL - TENSION TIE MODIFICA- TION 1142U0102-301 Group 5: Kit 142U0100 NotesExisting Part NumberNameQTYNew Part Number -1005 KIT - FRAME MODIFICA- TION, STA 820 1142U0101-101 KIT - FRAME MODIFICA- TION, STA 840 1142U0101-104 KIT - FRAME MODIFICA- TION, STA 860 1142U0101-107 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 57 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 58 Group 5: Kit 142U0100 NotesExisting Part NumberNameQTYNew Part Number -1005 KIT - FRAME MODIFICA- TION, STA 880 1142U0101-111 KIT - FRAME MODIFICA- TION, STA 900 1142U0101-125 KIT - FRAME MODIFICA- TION, STA 920 1142U0101-126 KIT - FRAME MODIFICA- TION, STA 940 1142U0101-127 KIT - TENSION TIE MODI- FICATION, STA 800 1142U0102-210 KIT - TENSION TIE MODI- FICATION, STA 820 1142U0102-212 KIT - TENSION TIE MODI- FICATION, STA 840 1142U0102-214 KIT - TENSION TIE MODI- FICATION, STA 860 1142U0102-217 KIT - TENSION TIE MODI- FICATION, STA 880 1142U0102-220 KIT - TENSION TIE MODI- FICATION, STA 920 1142U0102-226 KIT - TENSION TIE MODI- FICATION, STA 940 1142U0102-230 KIT - TENSION TIE MODI- FICATION, STA 900 1142U0102-235 KIT - SHEAR PANEL INSTL - TENSION TIE MODIFICA- TION 1142U0102-301 Group 6: Kit 142U0100 NotesExisting Part NumberNameQTYNew Part Number -1006 KIT - FRAME MODIFICA- TION, STA 840 1142U0101-104 KIT - FRAME MODIFICA- TION, STA 860 1142U0101-107 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 58 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 59 Group 6: Kit 142U0100 NotesExisting Part NumberNameQTYNew Part Number -1006 KIT - FRAME MODIFICA- TION, STA 880 1142U0101-111 KIT - FRAME MODIFICA- TION, STA 900 1142U0101-113 KIT - FRAME MODIFICA- TION, STA 920 1142U0101-117 KIT - FRAME MODIFICA- TION, STA 940 1142U0101-121 KIT - TENSION TIE MODIFI- CATION, STA 840 1142U0102-215 KIT - TENSION TIE MODIFI- CATION, STA 860 1142U0102-218 KIT - TENSION TIE MODIFI- CATION, STA 880 1142U0102-220 KIT - TENSION TIE MODIFI- CATION, STA 900 1142U0102-222 KIT - TENSION TIE MODIFI- CATION, STA 920 1142U0102-225 KIT - TENSION TIE MODIFI- CATION, STA 940 1142U0102-229 KIT - SHEAR PANEL INSTL - TENSION TIE MODIFICA- TION 1142U0102-302 Group 7: Kit 142U0100 NotesExisting Part NumberNameQTYNew Part Number -1007 KIT - FRAME MODIFICA- TION, STA 840 1142U0101-104 KIT - FRAME MODIFICA- TION, STA 860 1142U0101-107 KIT - FRAME MODIFICA- TION, STA 880 1142U0101-111 KIT - FRAME MODIFICA- TION, STA 900 1142U0101-125 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 59 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT ### Page 60 Group 7: Kit 142U0100 NotesExisting Part NumberNameQTYNew Part Number -1007 KIT - FRAME MODIFICA- TION, STA 920 1142U0101-126 KIT - FRAME MODIFICA- TION, STA 940 1142U0101-127 KIT - TENSION TIE MODI- FICATION, STA 840 1142U0102-215 KIT - TENSION TIE MODI- FICATION, STA 860 1142U0102-218 KIT - TENSION TIE MODI- FICATION, STA 880 1142U0102-220 KIT - TENSION TIE MODI- FICATION, STA 920 1142U0102-226 KIT - TENSION TIE MODI- FICATION, STA 940 1142U0102-230 KIT - TENSION TIE MODI- FICATION, STA 900 1142U0102-235 KIT - SHEAR PANEL INSTL - TENSION TIE MODIFICA- TION 1142U0102-302 Group 8: Kit 142U0100 NotesExisting Part NumberNameQTYNew Part Number -1008 KIT - FRAME MODIFICA- TION, STA 820 1142U0101-102 KIT - FRAME MODIFICA- TION, STA 840 1142U0101-105 KIT - FRAME MODIFICA- TION, STA 860 1142U0101-108 KIT - FRAME MODIFICA- TION, STA 880 1142U0101-111 KIT - FRAME MODIFICA- TION, STA 900 1142U0101-114 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: October 08, 2009 747-53A2605Revision 3: July 10, 2013 60 of 203 BOEING SERVICE BULLETIN 747-53A2605 ALERTALERT The text continues at https://openairdocs.org/service-documents/boeing/747-53a2605/file/1460b1db8f3b.md?from=61 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.