# Airbus Mandatory Service Bulletin A300-28-6064 Copy: Revision 03 ("U.S. DOT/FAA - Service Bulletin - A300-28-6064 R03"), 262 pages: PDF https://openairdocs.org/files/sha256/3c/20/3c20dad35602fa177386e851292d2e3a303df55a3bc2aab47958d98f467355f8; text https://openairdocs.org/service-documents/airbus/a300-28-6064/file/3c20dad35602.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2011-0264; AD 2011-21-14 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. ## Details - Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md) - Type: Service bulletin (Mandatory Service Bulletin) - Number: A300-28-6064 - Latest revision known: A300-28-6064, Revision 05, dated September 27, 2010 (OpenAirDocs) - Page: https://openairdocs.org/service-documents/airbus/a300-28-6064 ## ADs that cite it (3) (OpenAirDocs) Newest first, with the revision each names, as OpenAirDocs read it from the AD's text. - [AD 2011-21-14](https://openairdocs.org/ad/2011-21-14.md), effective Nov 23, 2011: Revisions 01, 02, 03, 04 and 05 - [AD 2008-03-04](https://openairdocs.org/ad/2008-03-04.md), effective Mar 6, 2008: Revision 01 - [AD 2007-20-04](https://openairdocs.org/ad/2007-20-04.md), effective Nov 7, 2007: No revision named Also cited in [3 proposed ADs](https://openairdocs.org/service-documents/airbus/a300-28-6064/proposed.md). ## Text (262 pages) Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2011-0264; AD 2011-21-14 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. 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 A300-600A300-600 SERVICE BULLETIN REVISION TRANSMITT AL SHEET AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 MANDATORY MANDATORY MANDATORY MANDATORY ATA SYSTEM : 28 TITLE : FUEL - GENERAL - MODIFY THE EQUIPMENT IN THE FUEL TANKS FOR ADDITIONAL ELECTRICAL BONDING MODIFICATION No. : 12495H5555 This page transmits Revision No. 03 of Service Bulletin No. A300-28-6064 ADDITIONAL WORK Additional work is required by this revision for aircraft modified by any previous issue. REASON Revision No. 03 issued to include improvements further to discrepancies found during accomplishment. CHANGES SUMMARY : - EFFECTIVITY . Operators 09V and 98W have been deleted. Operator MXU has been added. - MANPOWER . Additional work has been added. PLANNING INFORMA TION : - EFFECTIVITY . 1.A. Effectivity has been updated. Kits B11 and B19 have been raised in issue. Config. 08 note added. Additional work notes have been added. - DESCRIPTION . 1.D.(7) Additional work has been added. - Accomplishment Timescale . 1.E.(2)(d) Additional work has been added. DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 1 of 4 Printed in France © AIRBUS 2008 All rights reserved ### Page 2 A300-600A300-600 SERVICE BULLETIN REVISION TRANSMITT AL SHEET - MANPOWER . 1.G. Additional work has been added. Kits B11 and B19 have been raised in issue. - REFERENCES . 1.J. Service Bulletin A300-28-6089. MA TERIAL INFORMA TION : - MA TERIAL - PRICE AND AVAILABILITY . 2.A. Kit B11 and B19 have been raised in issue. - LIST OF COMPONENTS . 2.C. Kit B11 has been raised in issue. Item 60 has been replace with Item 70. . 2.C. Kit B19 has been raised in issue. . 2.D.(2) Additional work has been added. ACCOMPLISHMENT INSTRUCTIONS : - Preparation . 3.A.(1)(j) Additional work has been added. - MODIFICA TION . 3.B.(1)(a) Note has been updated. . 3.B.(5)(a) T ext corrected. Kits B11 and B19 have been raised in issue. . 3.B.(9)(b)2 Item (4) has been corrected to Item (11). . 3.B.(16) Kit B11 has been raised in issue. . 3.B.(16)(a) Kit B11 has been raised in issue. . 3.B.(16)(a)6 Item 60 has been replaced with Item 70 . 3.B.(16)(a)7 Item 60 has been replaced with Item 70. . 3.B.(16)(c) Kit B11 has been raised in issue. . 3.B.(16)(d) Kit B11 has been raised in issue. . 3.B.(23) Kit B19 has been raised in issue. . 3.B.(23)(a)1 Item 70 has been replaced with Item 71. . 3.B.(23)(a)3 Item 70 has been replaced with Item 71. DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 2 Printed in France © AIRBUS 2008 All rights reserved ### Page 3 A300-600A300-600 SERVICE BULLETIN REVISION TRANSMITT AL SHEET . - TESTS . 3.C.(5) Additional work has been added. - CLOSE-UP . 3.D.(3) Additional work has been added. - Figure 6 . Figure 6, Sheet 2 : Detail 25, 2 points added. - Figure 7 . Figure 7, Sheet 1 : Item 25, 6 points become 8 points. - Figure 10 . Figure 10, Sheet 4 updated. - Figure 30 . Sheet 1 Item 70 has been replaced with Item 71. - Figure 31 . Sheet 2 washer has been added. - Figure 42 . Item 60 has been replaced with Item 70. - Figure 50 . Figure added for additional work. - Figure 51 . Figure added for additional work. - Figure 52 . Figure added for additional work. FILING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document. Replace the complete document. Put this Revision T ransmittal Sheet in front of the Service Bulletin. DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 3 Printed in France © AIRBUS 2008 All rights reserved ### Page 4 A300-600A300-600 SERVICE BULLETIN REVISION TRANSMITT AL SHEET HISTORY OF PREVIOUS REVISIONS Revision No. 01 was issued to: - incorporate the comments of an airline request, - update the effectivity , - apply refuel/defuel valve modification on the LH wing for all aircraft. Other minor changes to the new Service Bulletin format were added. This Service Bulletin has been revised following operator queries on figure references, item numbers, bolt lengths and effectivity applicability . Revision No. 02 was issued to include improvements further to discrepancies found during accomplishment. REVISION SEQUENCE ORIGINAL : Jul 28/05 REVISION No. : 01 - Apr 03/07 REVISION No. : 02 - Mar 10/08 REVISION No. : 03 - Dec 15/08 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 4 Printed in France © AIRBUS 2008 All rights reserved ### Page 5 A300-600A300-600 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 This summary is for information only and is not approved for modification of the aircraft MANDATORY MANDATORY MANDATORY MANDATORY ATA SYSTEM : 28 TITLE : FUEL - GENERAL - MODIFY THE EQUIPMENT IN THE FUEL TANKS FOR ADDITIONAL ELECTRICAL BONDING MODIFICATION No. : 12495H5555 REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES As part of the Fuel Safety Assessment program, AIRBUS has carried out investigations of the electrical bonding in the aircraft fuel tanks. As a result of these investigations this Service Bulletin has been issued for additional electrical bonding of the equipment in the fuel tanks. This modification consists of installing additional bonding leads and electrical bonding points in the wings fuel tanks and center tank. The accomplishment of this Service Bulletin provides improved electrical bonding to ensure continuous electrical bonding protection of all the equipment in the fuel tanks for the design life goal of the aircraft. It is Mandatory to accomplish this modification before the 31st December 2010. This Service Bulletin has been validated on A300-600 aircraft MSN 0569. EVALUA TION T ABLE COMPLIANCE Mandatory CANCELS INSPECTION SB No POTENTIAL AD Ye s A/C OPERA TION AFFECTED No RELIABILITY AFFECTED No P AX COMFORT AFFECTED No COST SAVING No ETOPS AFFECTED No STRUCTURAL LIFE EXTN No VENDOR SB INVOL VED No DEFUEL/VENTILA TION Ye s KIT PRICE (USD) Refer to SB MODIFICA TION CLASSIFICA TION MAJOR None MINOR 12495H5555 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 1 of 4 Printed in France © AIRBUS 2008 All rights reserved ### Page 6 A300-600A300-600 SERVICE BULLETIN SUMMARY As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability , operational characteristics, affecting the airworthiness of the product. All other changes are Major changes. EFFECTIVITY This Service Bulletin is applicable to these operators: AAL AAW ABD AMU CES CSN DLH EGN F2I FDX GXY IRA JAL KAC KAL LAA MON MSR MXU OAL OHY QTR SUD T AR THA UPS CONCURRENT REQUIREMENTS None REFERENCES/REPERCUSSIONS TFU : None OEB : None AOT : None SIL : 28-072 LIFE LIMIT : None LINE MAINTENANCE AFFECTED : No OTHERS : None NATURE OF THE WORK AIRCRAFT : Y es EQUIPMENT : No HARD : No SOFT : No OBRM : No MANPOWER Center T ank, Kit 286064A01R05 TOTAL MANHOURS 114.5 ELAPSED TIME (HOURS) 73.0 Center T ank, Kit 286064A02R02 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 2 Printed in France © AIRBUS 2008 All rights reserved ### Page 7 A300-600A300-600 SERVICE BULLETIN SUMMARY TOTAL MANHOURS 114.5 ELAPSED TIME (HOURS) 73.0 Center T ank, Kit 286064A03R00 TOTAL MANHOURS 104.5 ELAPSED TIME (HOURS) 63.0 LH and RH Wing Fuel T anks - Config. 08 (Post Mod. 12226 Aircraft only) TOTAL MANHOURS 20 ELAPSED TIME (HOURS) 10.0 LH and RH Wing Fuel T anks - All other Aircraft TOTAL MANHOURS 226.0* ELAPSED TIME (HOURS) 114.5 NOTE(*) Subject to aircraft configuration. Refer to para. 1.G. MANPOWER in the Service Bulletin for the breakdown of the wings manhours. The manhours are given by rib bay and aircraft configuration. ADDITIONAL WORK (Introduced by Rev 01) TOTAL MANHOURS 2.0 ELAPSED TIME (HOURS) 2.0 ADDITIONAL WORK TOTAL MANHOURS 62.5 ELAPSED TIME (HOURS) 31.0 MATERIAL INFORMATION AIRCRAFT DA T A Center T ank - Kit 286064A01R05 thru Kit 286064A03R00: Bonding leads, clamps, rivets, bolts, nuts and washers. Wings Fuel T anks Equipment - Kit 286064B01R05 thru Kit 286064B28R01: DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 3 Printed in France © AIRBUS 2008 All rights reserved ### Page 8 A300-600A300-600 SERVICE BULLETIN SUMMARY Bonding leads, clamps, bolts, nuts, washers and drain attachment plates. NOTE : Kit 286064B24 has not been used. ADDITIONAL WORK (Introduced by Rev 01) Wings Fuel T anks Equipment - Kit 286064B39R00: Bonding leads, nuts and screws. APPENDICES None DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 4 Printed in France © AIRBUS 2008 All rights reserved ### Page 9 A300-600A300-600 SERVICE BULLETIN AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 MANDATORY MANDATORY MANDATORY MANDATORY ATA SYSTEM : 28 TITLE : FUEL - GENERAL - MODIFY THE EQUIPMENT IN THE FUEL TANKS FOR ADDITIONAL ELECTRICAL BONDING MODIFICATION No. : 12495H5555 This document contains AIRBUS PROPRIET ARY INFORMA TION and shall at all times remain the property of AIRBUS; no intellectual property right or license is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or part to third parties and shall not be duplicated in any manner (except for the purpose of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. P LANNING INFORMATION A. E FFECTIVITY (1) Models B4-601 B4-603 B4-605R B4-620 B4-622 B4-622R C4-605R/F C4-620 F4-605R F4-622R (2) Aircraft (a) Effectivity by MSN This Service Bulletin is applicable to aircraft MSN: 0252 0284 0294 0301 0307 0312 0317 0321 0336 0341 0344 0348 0351 0354 0358 0361 0365 0368 0380 0384 0388 0395 0398 0401 0405 0408 0411 0414 0417 0423 0459-0466 0469-0471 0474 0477 0479 0505-0518 0521 0525 0529 0530 0532 0533 0536 0540 0543 0546 0553-0561 0563 0566 0569 0572 0575 0577 0579 0581 0582 0584 0601-0619 0621 0623 0625-0633 0635 0637 0639 0641 0643 0645 0657 0659 0662 0664 0666 0668 0670 0673 0675 0677 0679 0681 0683 0685 0688 0692 0694 0696 0699 0701 0703 0705 0707 0709 0711 0713 0715 0717 0719 0721-0750 0752-0764 0766-0775 0777-0794 0797 0799-0841 (b) Effectivity by Operator The Operator/MSN relationship is provided for information only and is correct at the time of issue in accordance with the information available to AIRBUS. Any future DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 1 of 251 Printed in France © AIRBUS 2008 All rights reserved ### Page 10 A300-600A300-600 SERVICE BULLETIN changes resulting from transfer of an aircraft from one operator to another will not be reflected in this list unless the Service Bulletin is revised for another reason. OPERA TOR MSN AAL 0423 0459 0460 0461 0462 0463 0465 0466 0469 0470 0471 0474 0506 0507 0508 0509 0510 0511 0512 0513 0514 0515 0516 0517 0606 0610 0612 0615 0619 0626 0639 0643 0645 0675 AAW 0354 ABD 0529 0557 0755 0758 AMU 0677 0743 CES 0521 0525 0532 0707 0725 0732 0741 0746 0754 0763 CSN 0733 0734 0739 0750 0756 0762 DLH 0380 0401 0405 0408 0411 0414 0546 0553 0608 0618 0623 0701 0773 EGN 0555 0625 F2I 0284 0294 0301 0307 0312 0317 0321 0336 0341 0348 0351 FDX 0358 0361 0365 0388 0417 0477 0479 0530 0536 0543 0559 0572 0575 0579 0581 0611 0613 0630 0633 0657 0659 0668 0709 0713 0715 0726 0728 0735 0736 0738 0742 0745 0748 0752 0757 0759 0760 0761 0766 0768 0769 0771 0772 0774 0777 0778 0779 0780 0781 0789 0790 0791 0792 0793 0794 0799 0800 0801 0802 0803 0804 GXY 0533 IRA 0632 0696 0723 0727 JAL 0602 0617 0621 0637 0641 0670 0679 0683 0703 0711 0724 0729 0730 0737 0740 0753 0770 0783 0797 0836 0837 0838 KAC 0344 0673 0694 0699 0719 0721 KAL 0582 0609 0627 0631 0662 0685 0692 0717 0722 0731 LAA 0601 0616 MON 0540 0556 0604 0605 MSR 0561 0607 MXU 0767 0788 OAL 0603 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 2 Printed in France © AIRBUS 2008 All rights reserved ### Page 11 A300-600A300-600 SERVICE BULLETIN OPERA TOR MSN OHY 0584 0744 0747 0749 0764 QTR 0554 0560 0614 0664 0688 SUD 0252 0666 0775 T AR 0505 0558 0563 THA 0368 0384 0395 0398 0464 0518 0566 0569 0577 0628 0629 0635 0681 0705 0782 0784 0785 0786 0787 UPS 0805 0806 0807 0808 0809 0810 0811 0812 0813 0814 0815 0816 0817 0818 0819 0820 0821 0822 0823 0824 0825 0826 0827 0828 0829 0830 0831 0832 0833 0834 0835 0839 0840 0841 (c) Effectivity by MSN and Kit/Configuration The Kits and configurations applicable to these MSNs are given at the end of this list 0423 0459-0466 0469-0471 0474 0506-0518 0529 0533 0536 0540 0555-0557 0559 0561 0566 0569 0572 0575 0577 0579 0581-0582 0584 0603-0610 0612 0615 0619 0625-0629 0631-0632 0635 0639 0643 0645 0657 0659 0662 0666 0673 0675 0677 0681 0685 0692 0694 0701 0705 0717 0722-0723 0725 KIT No. QTY PER A/C CONFIGURA TION 286064A01R05 1 01 NOTE(01) Kit 286064A01R05 concerns the modification of the electrical bonding in the center tank and is valid for aircraft on which Mod. No. 8692S20032 (FUEL - SECTION - INTRODUCE MOULDED P ARTS ON A300/600) is not embodied. NOTE(02) Additional work is required by this revision for aircraft modified by Revision 00 or 01 or 02. NOTE(03) Config. 01 is valid for aircraft on which Mod. No. 04801H5078 (FUEL - INST ALL TRIM T ANK SYSTEM) is embodied. The Kits and configurations applicable to these MSNs are given at the end of this list 0477 0479 0505 0521 0525 0530 0532 0543 0546 0553-0554 0558 0560 0563 0601-0602 0611 0613-0614 0616-0618 0621 0623 0630 0633 0637 0641 0664 0668 0670 0679 0683 0688 0696 0699 0703 0707 0709 0711 0713 0715 0719 0721 0724 KIT No. QTY PER A/C CONFIGURA TION DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 3 Printed in France © AIRBUS 2008 All rights reserved ### Page 12 A300-600A300-600 SERVICE BULLETIN 286064A01R05 1 01 286064A03R00 1 01 NOTE(01) Kit 286064A01R05 concerns the modification of the electrical bonding in the center tank and is valid for aircraft on which Mod. No. 8692S20032 (FUEL - SECTION - INTRODUCE MOULDED P ARTS ON A300/600) is not embodied. NOTE(02) Additional work is required by this revision for aircraft modified by Revision 00 or 01 or 02. NOTE(03) Config. 01 is valid for aircraft on which Mod. No. 04801H5078 (FUEL - INST ALL TRIM T ANK SYSTEM) is embodied. NOTE(04) Kit 286064A03R00 concerns the modification of the electrical bonding in the center tank and is valid for aircraft on which Mod. No. 12315S22009 (FUEL - FUEL PUMP SYSTEM - ADD BONDING LEAD ON RH AND LH CENTER T ANK BOOSTER PUMP CANISTERS) is not embodied and for aircraft on which Mod. No. 12314H5524 (FUEL - FUEL PUMP SYSTEM - INST ALL MODIFIED CENTER T ANK BOOSTER PUMP CANISTERS) or Mod. No. 13041H5657 (FUEL - FUEL PUMP SYSTEM - INST ALL MODIFIED CENTER T ANK BOOSTER PUMP CANISTERS) are not embodied or Service Bulletin No. A300-28-6069 or A300-28-6089 are not accomplished. The Kits and configurations applicable to these MSNs are given at the end of this list 0252 0284 0294 0301 0307 0312 0317 0321 0336 0341 0344 0348 0351 0354 0358 0361 0365 0368 0380 0384 0388 0395 0398 0401 0405 0408 0411 0414 0417 KIT No. QTY PER A/C CONFIGURA TION 286064A01R05 1 02 286064A03R00 1 02 NOTE(01) Kit 286064A01R05 concerns the modification of the electrical bonding in the center tank and is valid for aircraft on which Mod. No. 8692S20032 (FUEL - SECTION - INTRODUCE MOULDED P ARTS ON A300/600) is not embodied. NOTE(02) Additional work is required by this revision for aircraft modified by Revision 00 or 01 or 02. NOTE(03) Config. 02 is valid for aircraft on which Mod. No. 04801H5078 (FUEL - INST ALL TRIM T ANK SYSTEM) is not embodied. NOTE(04) Kit 286064A03R00 concerns the modification of the electrical bonding in the center tank and is valid for aircraft on which Mod. No. 12315S22009 (FUEL - FUEL PUMP SYSTEM - ADD BONDING LEAD ON RH AND DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 4 Printed in France © AIRBUS 2008 All rights reserved ### Page 13 A300-600A300-600 SERVICE BULLETIN LH CENTER T ANK BOOSTER PUMP CANISTERS) is not embodied and for aircraft on which Mod. No. 12314H5524 (FUEL - FUEL PUMP SYSTEM - INST ALL MODIFIED CENTER T ANK BOOSTER PUMP CANISTERS) or Mod. No. 13041H5657 (FUEL - FUEL PUMP SYSTEM - INST ALL MODIFIED CENTER T ANK BOOSTER PUMP CANISTERS) are not embodied or Service Bulletin No. A300-28-6069 or A300-28-6089 are not accomplished. The Kits and configurations applicable to these MSNs are given at the end of this list 0726-0750 0752-0764 0766-0775 0777-0794 0797 0799-0841 KIT No. QTY PER A/C CONFIGURA TION 286064A02R02 1 None NOTE(01) Kit 286064A02R02 concerns the modification of the electrical bonding in the center tank and is valid for aircraft on which Mod. No. 8692S20032 (FUEL - SECTION - INTRODUCE MOULDED P ARTS ON A300/600) is embodied. NOTE(02) Additional work is required by this revision for aircraft modified by Revision 00 or 01 or 02. The Kits and configurations applicable to these MSNs are given at the end of this list 0252 0284 0294 0301 0307 0312 0317 0321 0336 0341 0344 0348 0351 0354 0358 0361 0365 0368 0380 0384 0388 0395 0398 0401 0405 0408 0411 0414 0417 0423 0459-0466 0469-0471 0474 0477 0479 0505-0518 0521 0525 0529-0530 0532-0533 0536 0540 0543 0546 0553-0561 0563 0566 0569 0572 0575 0577 0579 0581-0582 0584 0601-0619 0621 0623 0625-0633 0635 0637 0639 0641 0643 0645 0657 0659 0662 0664 0666 0668 0670 0673 0675 0677 0679 0681 0683 0685 0688 0692 0694 0696 0699 0701 0703 0705 0707 0709 0711 0713 0715 0717 0719 0721-0750 0752-0764 0766-0775 0777-0794 0797 0799-0804 KIT No. QTY PER A/C CONFIGURA TION DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 5 Printed in France © AIRBUS 2008 All rights reserved ### Page 14 A300-600A300-600 SERVICE BULLETIN 286064B01R05 2 None 286064B02R02 4 01 286064B02R02 12 02 286064B03R03 2 None 286064B04R03 2 None 286064B05R01 2 None 286064B06R03 2 None 286064B07R01 1 None 286064B08R03 2 None DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 6 Printed in France © AIRBUS 2008 All rights reserved ### Page 15 A300-600A300-600 SERVICE BULLETIN KIT No. QTY PER A/C CONFIGURA TION 286064B09R04 2 None 286064B10R01 2 None 286064B11R05 2 None 286064B12R01 2 None 286064B13R03 2 None 286064B14R02 2 None 286064B15R04 2 None 286064B16R03 2 None 286064B17R01 2 None 286064B18R04 2 None 286064B19R02 2 None 286064B21R01 2 04 286064B22R05 2 03 286064B23R01 2 06 286064B25R01 2 07 286064B26R01 12 02 286064B27R01 1 02 286064B28R01 1 02 286064B39R00 (ADDITIONAL WORK only) 10 5 NOTE : Config. 01 - Post SB A300-57-6070 (Mod. 11055). Config. 02 - Pre SB A300-57-6070 (Mod. 11055). Config. 03 - Post Mod. 08680 and Post SB A300-28-6028 (Mod. 08679) aircraft. Config. 04 - Post Mod. 06128 aircraft. Config. 06 - Pre Mod. 06708 aircraft. Config. 07 - Pre Mod. 04607 aircraft. Kit 286064B39R00 is only applicable to Additional Work described in Rev 01 of this Service Bulletin. The Kits and configurations applicable to these MSNs are given at the end of this list DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 7 Printed in France © AIRBUS 2008 All rights reserved ### Page 16 A300-600A300-600 SERVICE BULLETIN 0805-0811 KIT No. QTY PER A/C CONFIGURA TION 286064B20R06 2 08 NOTE : Config. 08 - Post Mod. 12226 aircraft. NOTE : Mod. No. 12365H5540 (FUEL - GENERAL - REVISE ELECTRICAL BONDING OF EQUIPMENT IN INNER WING FUEL T ANKS) is embodied on MSN 0812 and subsequent. (3) Spares None B. C ONCURRENT REQUIREMENTS None C. R EASON (1) History As part of the Fuel Safety Assessment program, AIRBUS has carried out investigations of the electrical bonding in the aircraft fuel tanks. This Service Bulletin has been validated on A300-600 aircraft MSN 0569. (2) Objective/Action As a result of these investigations this Service Bulletin has been issued for additional electrical bonding of the equipment in the fuel tanks. This modification consists of installing additional bonding leads and electrical bonding points in the wings fuel tanks and center tank. (3) Advantages The accomplishment of this Service Bulletin provides extra electrical bonding to ensure continuous electrical bonding protection of all the equipment in the fuel tanks for the design life goal of the aircraft. (4) Operational/Maintenance Consequences None D. D ESCRIPTION T o accomplish this Service Bulletin it is necessary to: (1) Center T ank - Kit 286064A01R05, Kit 286064A02R02 and Kit 286064A03R00 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 8 Printed in France © AIRBUS 2008 All rights reserved ### Page 17 A300-600A300-600 SERVICE BULLETIN (a) Defuel and vent the center fuel tanks. (b) Get access to the center fuel tanks. (c) Check the bonding points in the center tank. (2) Center T ank Kit 286064A01R05 (a) Modify or install the bonding points. (3) Center T ank Kit 286064A02R02 (a) Modify or install the bonding points. (4) Center T ank Kit 286064A03R00 (a) Install the bonding points. (5) LH and RH Wing Fuel T anks - Kit 286064B01R05 thru Kit 286064B28R01 NOTE : Kit 286064B24 has not been used. (a) Defuel and vent the wings fuel tanks. (b) Fully extend the slats. (c) Get access to the applicable equipment in the wings fuel tanks (rib bay 1-2 thru to rib bay 27-28, LH and RH wing) for all Configs except Config. 08. For Config. 08 rib bays 1-2 only . (d) Install additional bonding leads and electrical bonding points. (e) Do electrical bonding resistant tests of the new electrical bonding points. (f) Re-fuel the wings fuel tanks. (g) Check the wings fuel tanks for leaks. (h) Close-up. (6) ADDITIONAL WORK (Introduced by Rev 01) (a) Refuel/Defuel Valve LH Wing - Kit 286064B39R00 1 Defuel and vent the LH wing fuel tank. 2 Get access to rib bay 13 to 14. 3 Bond the refuel/defuel valve. (7) ADDITIONAL WORK (a) Preparation DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 9 Printed in France © AIRBUS 2008 All rights reserved ### Page 18 A300-600A300-600 SERVICE BULLETIN (b) Check the bonding points in the center tank. (c) T est (d) Close-up E. C OMPLIANCE (1) Classification Mandatory (2) Accomplishment Timescale (a) It is mandatory to accomplish this Service Bulletin before 31st December 2010. (b) Accomplishment of this Service Bulletin has been rendered mandatory by the issue of an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA). The AD must be used as the reference document for the mandatory accomplishment timescale. (c) ADDITIONAL WORK (Introduced by Rev 01) 1 It is mandatory to accomplish the additional work before 31st December 2010. (d) ADDITIONAL WORK 1 It is mandatory to accomplish the additional work before 31st December 2010. F. A PPROVAL Approved under EASA Design Organisation Approval No. EASA 21J.031. If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin. G. M ANPOWER The manpower estimates given in this Service Bulletin are based on direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit operators circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying times for paints and sealants, etc. and general administration are also not included. Center T ank Kit 286064A01R05 Get access 30.0 Check of the bonding points 40.0 Modification/install the bonding points 13.0 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 10 Printed in France © AIRBUS 2008 All rights reserved ### Page 19 A300-600A300-600 SERVICE BULLETIN T est 1.5 Close-up 30.0 TOTAL MANHOURS 114.5 ELAPSED TIME (HOURS) 73.0 Center T ank Kit 286064A02R02 Get access 30.0 Check of the bonding points 40.0 Modification/install the bonding points 13.0 T est 1.5 Close-up 30.0 TOTAL MANHOURS 114.5 ELAPSED TIME (HOURS) 73.0 Center T ank Kit 286064A03R00 Get access 30.0 Check of the bonding points 40.0 Install the bonding points 3.0 T est 1.5 Close-up 30.0 TOTAL MANHOURS 104.5 ELAPSED TIME (HOURS) 63.0 LH and RH Wing Fuel T anks. The hours for the following kits are for both wings. Rib Bay 1-2, Config. 08 Aircraft Only Kit 286064B20R06 Modification 20.0 TOTAL MANHOURS 20.0 ELAPSED TIME (HOURS) 10.0 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 11 Printed in France © AIRBUS 2008 All rights reserved ### Page 20 A300-600A300-600 SERVICE BULLETIN NOTE : After the completion of the work in the wings fuel tanks, operators should allow two hours for fuel leak tests. Rib Bay 1-2, Kit 286064B01R05 All Aircraft Get access 1.0 Modification 21.0 Close up 1.0 TOTAL MANHOURS 23.0 ELAPSED TIME (HOURS) 11.5 Rib Bay 1-2, Kit 286064B22R05 Config. 03 Aircraft Modification 6.0 TOTAL MANHOURS 6.0 ELAPSED TIME (HOURS) 3.0 Rib Bay 1-2, Kit 286064B23R01 Config. 06 Aircraft Modification 2.0 TOTAL MANHOURS 2.0 ELAPSED TIME (HOURS) 1.0 Rib Bay 2-3, Kit 286064B01R05 All Aircraft Modification 6.0 TOTAL MANHOURS 6.0 ELAPSED TIME (HOURS) 3.0 Rib Bay 2-3, Kit 286064B21R01 Config. 04 Aircraft Modification 6.0 TOTAL MANHOURS 6.0 ELAPSED TIME (HOURS) 3.0 Rib Bay 5-6, Kit 286064B03R03 All Aircraft Get access 1.0 Modification 4.0 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 12 Printed in France © AIRBUS 2008 All rights reserved ### Page 21 A300-600A300-600 SERVICE BULLETIN Close up 1.0 TOTAL MANHOURS 6.0 ELAPSED TIME (HOURS) 3.0 Rib Bay 5-6, Kit 286064B02R02 or Kit 286064B26R01 Config. 02 Aircraft Modification 4.0 TOTAL MANHOURS 4.0 ELAPSED TIME (HOURS) 2.0 Rib Bay 8-9, Kit 286064B04R03 All Aircraft Get access 1.0 Modification 6.0 Close up 1.0 TOTAL MANHOURS 8.0 ELAPSED TIME (HOURS) 4.0 Rib Bay 8-9, Kit 286064B02R02 or Kit 286064B26R01 Config. 02 Aircraft Modification 4.0 TOTAL MANHOURS 4.0 ELAPSED TIME (HOURS) 2.0 Rib Bay 9-10, Kit 286064B05R01 All Aircraft Get access 1.0 Modification 6.0 Close up 1.0 TOTAL MANHOURS 8.0 ELAPSED TIME (HOURS) 4.0 Rib Bay 9-10, Kit 286064B02R02 or Kit 286064B26R01 Config. 02 Aircraft Modification 4.0 TOTAL MANHOURS 4.0 ELAPSED TIME (HOURS) 2.0 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 13 Printed in France © AIRBUS 2008 All rights reserved ### Page 22 A300-600A300-600 SERVICE BULLETIN Rib Bay 10-11, Kit 286064B06R03 All Aircraft Get access 1.0 Modification 4.0 Close up 1.0 TOTAL MANHOURS 6.0 ELAPSED TIME (HOURS) 3.0 Rib Bay 10-11, Kit 286064B02R02 or Kit 286064B26R01 Config. 02 Aircraft Modification 4.0 TOTAL MANHOURS 4.0 ELAPSED TIME (HOURS) 2.0 Rib Bay 11-12, Kit 286064B07R01 All Aircraft Get access 1.0 Modification 2.0 Close up 1.0 TOTAL MANHOURS 4.0 ELAPSED TIME (HOURS) 4.0 Rib Bay 12-13, Kit 286064B08R03 All Aircraft Get access 1.0 Modification 4.0 Close up 1.0 TOTAL MANHOURS 6.0 ELAPSED TIME (HOURS) 3.0 Rib Bay 12-13, Kit 286064B02R02 or Kit 286064B26R01 Config. 02 Aircraft Modification 4.0 TOTAL MANHOURS 4.0 ELAPSED TIME (HOURS) 2.0 Rib Bay 13-14, and Kit 286064B09R04 All Aircraft DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 14 Printed in France © AIRBUS 2008 All rights reserved ### Page 23 A300-600A300-600 SERVICE BULLETIN Get access 1.0 Modification 6.0 Close up 1.0 TOTAL MANHOURS 8.0 ELAPSED TIME (HOURS) 4.0 Rib Bay 14-15, Kit 286064B10R01 All Aircraft Get access 1.0 Modification 14.0 Close up 1.0 TOTAL MANHOURS 16.0 ELAPSED TIME (HOURS) 8.0 Rib Bay 14-15, Kit 286064B02R02 or Kit 286064B26R01 Config. 02 Aircraft Modification 4.0 TOTAL MANHOURS 4.0 ELAPSED TIME (HOURS) 2.0 Rib Bay 14-15, Kit 286064B25R01 Config. 07 Aircraft Modification 2.0 TOTAL MANHOURS 2.0 ELAPSED TIME (HOURS) 1.0 Rib Bay 15-16, Kit 286064B11R05 All Aircraft Get access 1.0 Modification 8.0 Close up 1.0 TOTAL MANHOURS 10.0 ELAPSED TIME (HOURS) 5.0 Rib Bay 15-16, Kit 286064B02R02 or Kit 286064B26R01 Config. 02 Aircraft Modification 4.0 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 15 Printed in France © AIRBUS 2008 All rights reserved ### Page 24 A300-600A300-600 SERVICE BULLETIN TOTAL MANHOURS 4.0 ELAPSED TIME (HOURS) 2.0 Rib Bay 16-17, Kit 286064B12R01 All Aircraft Get access 1.0 Modification 2.0 Close up 1.0 TOTAL MANHOURS 4.0 ELAPSED TIME (HOURS) 2.0 Rib Bay 17-18, Kit 286064B25R01 Config. 07 Aircraft Get access 1.0 Modification 1.0 Close up 1.0 TOTAL MANHOURS 3.0 ELAPSED TIME (HOURS) 1.5 Rib Bay 18-19, Kit 286064B13R03 All Aircraft Get access 1.0 Modification 4.0 Close up 1.0 TOTAL MANHOURS 6.0 ELAPSED TIME (HOURS) 3.0 Rib Bay 18-19, Kit 286064B02R02 or Kit 286064B26R01 Config. 01 and Config. 02 Modification 4.0 TOTAL MANHOURS 4.0 ELAPSED TIME (HOURS) 2.0 Rib Bay 20-21, Kit 286064B14R02 All Aircraft Get access 1.0 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 16 Printed in France © AIRBUS 2008 All rights reserved ### Page 25 A300-600A300-600 SERVICE BULLETIN Modification 4.0 Close up 1.0 TOTAL MANHOURS 6.0 ELAPSED TIME (HOURS) 3.0 Rib Bay 20-21, Kit 286064B02R02 or Kit 286064B26R01 Config. 02 Aircraft Modification 4.0 TOTAL MANHOURS 4.0 ELAPSED TIME (HOURS) 2.0 Rib Bay 21-22, Kit 286064B15R04 All Aircraft Get access 1.0 Modification 4.0 Close up 1.0 TOTAL MANHOURS 6.0 ELAPSED TIME (HOURS) 3.0 Rib Bay 21-22 Kit 286064B02R02 or Kit 286064B26R01 Config. 01 and Config. 02 Modification 4.0 TOTAL MANHOURS 4.0 ELAPSED TIME (HOURS) 2.0 Rib Bay 24-25, Kit 286064B16R03 All Aircraft Get access 1.0 Modification 4.0 Close up 1.0 TOTAL MANHOURS 6.0 ELAPSED TIME (HOURS) 3.0 Rib Bay 24-25, Kit 286064B02R02 or Kit 286064B26R01 Config. 01 and Config. 02 Modification 4.0 TOTAL MANHOURS 4.0 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 17 Printed in France © AIRBUS 2008 All rights reserved ### Page 26 A300-600A300-600 SERVICE BULLETIN ELAPSED TIME (HOURS) 2.0 Rib Bay 25-26, Kit 286064B19R02 All Aircraft Get access 1.0 Modification 1.0 Close up 1.0 TOTAL MANHOURS 3.0 ELAPSED TIME (HOURS) 1.5 Rib Bay 26-27, Kit 286064B17R01 All Aircraft Get access 1.0 Modification 5.0 Close up 1.0 TOTAL MANHOURS 7.0 ELAPSED TIME (HOURS) 3.5 Rib Bay 26-27, Kit 286064B27R01 or Kit 286064B28R01 Config. 02 Aircraft Modification 5.0 TOTAL MANHOURS 5.0 ELAPSED TIME (HOURS) 2.5 Rib Bay 27-28, Kit 286064B18R04 All Aircraft Get access 1.0 Modification 8.0 Close up 1.0 TOTAL MANHOURS 10.0 ELAPSED TIME (HOURS) 5.0 Rib Bay 27-28, Kit 286064B02R02 or Kit 286064B26R01 Config. 01 and Config. 02 Modification 4.0 TOTAL MANHOURS 4.0 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 18 Printed in France © AIRBUS 2008 All rights reserved ### Page 27 A300-600A300-600 SERVICE BULLETIN ELAPSED TIME (HOURS) 2.0 NOTE : The overall manhours for the wings fuel tanks can vary between 162 total manhours, elapsed time 83 manhours and 226 total manhours, 113 elapsed time manhours, depending on the aircraft configuration. NOTE : After the completion of the work in the wings fuel tanks, operators should allow two hours for fuel leak tests. ADDITIONAL WORK (Introduced by Rev 01) Rib Bay 13-14, Kit 286064B39R00 All Aircraft Get access 0.5 Modification 1.0 Close up 0.5 TOTAL MANHOURS 2.0 ELAPSED TIME (HOURS) 2.0 ADDITIONAL WORK Get access 30.0 Check of the bonding points 1.0 T est 1.5 Close-up 30.0 TOTAL MANHOURS 62.5 ELAPSED TIME (HOURS) 31.0 H. W EIGHT AND BALANCE Not changed I. E LECTRICAL LOAD DATA Not changed J. R EFERENCES Aircraft Maintenance Manual (AMM) : 06-41-57 20-28-11 24-00-00 24-31-11 24-41-00 27-80-00 28-00-00 28-10-00 28-11-00 28-11-22 28-11-29 28-25-00 28-25-21 33-13-00 33-14-00 57-20-43 57-23-11 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 19 Printed in France © AIRBUS 2008 All rights reserved ### Page 28 A300-600A300-600 SERVICE BULLETIN Elec. Std. Practices Manual (ESPM) : 20-51-10 20-55-00 Service Information Letter (SIL) : 28-072 Structural Repair Manual (SRM) : 51-40-20 51-40-30 51-40-44 51-43-00 51-75-10 51-76-10 51-76-20 Consumable Materials List (CML) Service Bulletin (SB) : A300-28-6028 A300-28-6069 A300-28-6089 A300-57-6026 A300-57-6070 K. P UBLICATIONS AFFECTED Aircraft Maintenance Manual (AMM) : 28-11-21 28-12-15 28-21-13 28-21-21 28-25-15 28-25-21 28-42-23 28-42-24 28-42-35 28-42-36 28-42-44 28-42-45 28-43-21 28-46-21 28-46-22 57-20-43 Illustrated Parts Catalogue (IPC) : 28-11-05 28-11-11 28-11-12 28-21-13 28-21-21 28-25-03 28-25-05 28-25-12 28-26-03 28-42-44 28-43-05 57-20-43 L. I NTERCHANGEABILITY/MIXABILITY None DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 20 Printed in France © AIRBUS 2008 All rights reserved ### Page 29 A300-600A300-600 SERVICE BULLETIN 2. M ATERIAL INFORMATION A. M ATERIAL - PRICE AND AVAILABILITY (1) Material Operators with aircraft shown in the effectivity of this Service Bulletin should submit a purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is: AIRBUS Spares Support and Services Weg beim Jaeger 150 P .O. Box 630262 D-22335 HAMBURG GERMANY For ordering by internet: http://spares.airbus.com For ordering by fax: +49 40 50 76 25 90 (2) Price and Availability Kit 286064A01R05 Cost : 60 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064A02R02 Cost : 70 US dollars Availability : 90 calendar days from receipt of order The sales terms (costs and availability) are estimated in relation to economic conditions at the issue date of the Service Bulletin. Kit 286064A03R00 Cost : 90 US dollars Availability : 90 calendar days from receipt of order The sales terms (costs and availability) are estimated in relation to economic conditions at the issue date of the Service Bulletin. Kit 286064B01R05 Cost : 150 US dollars Availability : 90 calendar days from receipt of order DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 21 Printed in France © AIRBUS 2008 All rights reserved ### Page 30 A300-600A300-600 SERVICE BULLETIN The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B02R02 Cost : 30 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B03R03 Cost : 60 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B04R03 Cost : 80 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B05R01 Cost : 50 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B06R03 Cost : 230 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B07R01 Cost : 10 US dollars Availability : 90 calendar days from receipt of order DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 22 Printed in France © AIRBUS 2008 All rights reserved ### Page 31 A300-600A300-600 SERVICE BULLETIN The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B08R03 Cost : 130 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B09R04 Cost : 20 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B10R01 Cost : 520 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B11R05 Cost : 110 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B12R01 Cost : 20 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B13R03 Cost : 180 US dollars Availability : 90 calendar days from receipt of order DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 23 Printed in France © AIRBUS 2008 All rights reserved ### Page 32 A300-600A300-600 SERVICE BULLETIN The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B14R02 Cost : 150 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B15R04 Cost : 140 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B16R03 Cost : 71.90 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B17R01 Cost : 140 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B18R04 Cost : 120 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B19R02 Cost : 30 US dollars Availability : 90 calendar days from receipt of order DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 24 Printed in France © AIRBUS 2008 All rights reserved ### Page 33 A300-600A300-600 SERVICE BULLETIN The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B20R06 Cost : 120 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B21R01 Cost : 130 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B22R05 Cost : 10 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B23R01 Cost : 13 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B25R01 Cost : 120 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B26R01 Cost : 30 US dollars Availability : 90 calendar days from receipt of order DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 25 Printed in France © AIRBUS 2008 All rights reserved ### Page 34 A300-600A300-600 SERVICE BULLETIN The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B27R01 Cost : 150 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. Kit 286064B28R01 Cost : 150 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. NOTE : The kits availability given above is the standard lead time from the date of your purchase order. If you require the Kits before this time, please include your retrofit planning schedule with your order so that we can try to comply with your requirements. ADDITIONAL WORK (Introduced by Rev 01) Kit 286064B39R00 Cost : 20 US dollars Availability : 90 calendar days from receipt of order The sales terms (Cost and Availability) are estimated in relation to economic conditions at the issue date of this Service Bulletin. NOTE : The kits availability given above is the standard lead time from the date of your purchase order. If you require the Kits before this time, please include your retrofit planning schedule with your order so that we can try to comply with your requirements. B. I NDUSTRY SUPPORT INFORMATION None DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 26 Printed in France © AIRBUS 2008 All rights reserved ### Page 35 A300-600A300-600 SERVICE BULLETIN C. L IST OF COMPONENTS Kit 286064A01R05 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 2 NAS1303-3 2 Bolt 3 NAS1149F0332P 2 Washer 4 NAS1726-4E 2 Nut 5 NAS1726-3E 14 Nut 7 E0088-10-125 1 Lead 8 NSA5519-2B 3 Clamp 13 AN735D40 8 Clamp 14 NAS1801-3-8 8 Screw 15 E0088-10-80 7 Lead 16 E0088-10-160 3 Lead 17 NAS1303-2 2 Bolt NOTE : Refer to the AIRBUS Standards Manual (SM) if you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin. The SM will give you the correct part number to part number relationship. Kit 286064A02R02 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 2 NAS1303-3 2 Bolt 3 NAS1149F0332P 1 Washer 4 NAS1726-4E 1 Nut 5 NAS1726-3E 18 Nut 7 E0088-10-125 1 Lead 8 NSA5519-2B 3 Clamp 9 NSA5050-4 1 Nut 13 AN735D40 8 Clamp 14 NAS1801-3-8 8 Screw 15 E0088-10-80 7 Lead 16 E0088-10-160 3 Lead 17 NAS1303-2 1 Bolt NOTE : Refer to the AIRBUS Standards Manual (SM) if you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin. The SM will give you the correct part number to part number relationship. Kit 286064A03R00 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 2 NAS1303-3 2 Bolt 3 NAS1149F0332P 2 Washer 5 NAS1726-3E 2 Nut 10 E0088-10-200 2 Lead DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 27 Printed in France © AIRBUS 2008 All rights reserved ### Page 36 A300-600A300-600 SERVICE BULLETIN ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 11 ASNA2050DCJ3215 4 Rivet 12 A9242127720000 2 Angle Kit 286064B01R05 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 4 NSA5472-4K7 4 Nut 14 E0088-41-160 1 Lead 15 AN742D6 1 Clamp 16 NSA5474-3K7 11 Nut 17 NSA5020-3-3 3 Bolt 20 NSA5474-4K7 7 Nut 25 H19200C4 1 Nut 27 NSA5041VBV3-4 1 Bolt 28 AN960C10L 1 Washer 34 NSA5041VBV3-10 2 Bolt 35 NSA5519-2B 4 Clamp 37 NAS1303-2 4 Bolt 38 E0088-10-100 2 Lead 39 E0088-41-100 2 Lead 45 NSA5022-4-21 4 Screw 46 NAS1304-3 4 Bolt 49 NSA5472-5K7 5 Nut 52 A2824028520000 3 Washer 53 AN960PD416 3 Washer 74 AN960KD10L 2 Washer 77 NSA5041VBV3-8 1 Bolt Kit 286064B02R02 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 4 NSA5472-4K7 4 Nut 9 A5715206420000 1 Plate 13 NAS1252-416L 1 Washer Kit 286064B03R03 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 2 NSA5020-3-6 1 Bolt 4 NSA5472-4K7 2 Nut 5 AN960C416L 1 Washer 6 NSA5041VBV4-2 1 Bolt 16 NSA5474-3K7 1 Nut 70 NSA5020-3-2 1 Bolt DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 28 Printed in France © AIRBUS 2008 All rights reserved ### Page 37 A300-600A300-600 SERVICE BULLETIN Kit 286064B04R03 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 4 NSA5472-4K7 2 Nut 5 AN960C416L 1 Washer 16 NSA5474-3K7 1 Nut 17 NSA5020-3-3 1 Bolt 25 H19200C4 1 Nut 30 NSA5041VBV4-3 1 Bolt 88 AN960KD10 1 Washer Kit 286064B05R01 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 1 E0088-40-100 1 Lead 3 NSA5041VBV4-11 1 Bolt 4 NSA5472-4K7 2 Nut 5 AN960C416L 1 Washer 7 NSA5041VBV3-5 1 Bolt 14 E0088-41-160 1 Lead 15 AN742D6 1 Clamp 16 NSA5474-3K7 3 Nut 17 NSA5020-3-3 1 Bolt 19 ABS0114-4-18 1 Bolt 20 NSA5474-4K7 1 Nut 31 NAS1303-10 1 Bolt Kit 286064B06R03 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 1 E0088-40-100 1 Lead 4 NSA5472-4K7 3 Nut 5 AN960C416L 1 Washer 16 NSA5474-3K7 1 Nut 18 NSA5472-3K7 1 Nut 28 AN960C10L 1 Washer 32 NSA5041VBV4-9 1 Bolt 33 NSA5041VBV3-3 1 Bolt 40 ABS0114-4-16 1 Bolt 70 NSA5020-3-2 1 Bolt Kit 286064B07R01 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 16 NSA5474-3K7 2 Nut 20 NSA5474-4K7 1 Nut 39 E0088-41-100 1 Lead 50 AN742D8 1 Clamp 51 NAS1100-3-7 1 Screw DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 29 Printed in France © AIRBUS 2008 All rights reserved ### Page 38 A300-600A300-600 SERVICE BULLETIN ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 55 NAS1304-11 1 Bolt 56 NAS1303-7 1 Bolt 58 NAS1304-14 1 Bolt Kit 286064B08R03 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 4 NSA5472-4K7 3 Nut 5 AN960C416L 1 Washer 16 NSA5474-3K7 2 Nut 28 AN960C10L 1 Washer 32 NSA5041VBV4-9 1 Bolt 41 NSA5041VBV3-2 1 Bolt 42 NAS1303-1 1 Bolt 44 ABS0114-4-15 1 Bolt 89 E0088-40-190 1 Lead Kit 286064B09R04 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 16 NSA5474-3K7 4 Nut 17 NSA5020-3-3 1 Bolt 20 NSA5474-4K7 2 Nut 25 H19200C4 1 Nut 51 NAS1100-3-7 2 Screw 59 E0088-41-304 2 Lead 70 NSA5020-3-2 1 Bolt 90 NSA5020-3-5 1 Bolt Kit 286064B10R01 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 1 E0088-40-100 1 Lead 4 NSA5472-4K7 2 Nut 5 AN960C416L 1 Washer 7 NSA5041VBV3-5 1 Bolt 14 E0088-41-160 1 Lead 15 AN742D6 1 Clamp 16 NSA5474-3K7 8 Nut 17 NSA5020-3-3 1 Bolt 18 NSA5472-3K7 2 Nut 20 NSA5474-4K7 3 Nut 26 NSA5041VBV3-7 1 Bolt 35 NSA5519-2B 4 Clamp 37 NAS1303-2 4 Bolt 38 E0088-10-100 2 Lead 39 E0088-41-100 2 Lead DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 30 Printed in France © AIRBUS 2008 All rights reserved ### Page 39 A300-600A300-600 SERVICE BULLETIN ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 45 NSA5022-4-21 4 Screw 54 NSA5041VBV4-7 1 Bolt 57 ABS0114-4-14 1 Bolt 69 NSA5041VBV3-6 2 Bolt Kit 286064B11R05 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 1 E0088-40-100 1 Lead 4 NSA5472-4K7 5 Nut 5 AN960C416L 1 Washer 14 E0088-41-160 1 Lead 15 AN742D6 1 Clamp 16 NSA5474-3K7 1 Nut 17 NSA5020-3-3 1 Bolt 18 NSA5472-3K7 2 Nut 20 NSA5474-4K7 3 Nut 28 AN960C10L 1 Washer 29 NSA5041VBV4-8 1 Bolt 33 NSA5041VBV3-3 1 Bolt 46 NAS1304-3 2 Bolt 49 NSA5472-5K7 2 Nut 52 A2824028520000 2 Washer 53 AN960PD416 1 Washer 70 NSA5020-3-2 1 Bolt 85 ABS0114-4-13 1 Bolt Kit 286064B12R01 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 16 NSA5474-3K7 2 Nut 70 NSA5020-3-2 1 Bolt 71 NSA5020-3-4 1 Bolt Kit 286064B13R03 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 1 E0088-40-100 1 Lead 4 NSA5472-4K7 3 Nut 5 AN960C416L 1 Washer 16 NSA5474-3K7 1 Nut 18 NSA5472-3K7 1 Nut 28 AN960C10L 1 Washer 29 NSA5041VBV4-8 1 Bolt 33 NSA5041VBV3-3 1 Bolt 42 NAS1303-1 1 Bolt 61 ABS0114-4-12 1 Bolt DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 31 Printed in France © AIRBUS 2008 All rights reserved ### Page 40 A300-600A300-600 SERVICE BULLETIN Kit 286064B14R02 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 1 E0088-40-100 1 Lead 4 NSA5472-4K7 3 Nut 5 AN960C416L 1 Washer 12 NSA5041VBV4-5 1 Bolt 16 NSA5474-3K7 1 Nut 25 H19200C4 1 Nut 54 NSA5041VBV4-7 1 Bolt 63 ABS0114-4-10 1 Bolt 69 NSA5041VBV3-6 1 Bolt Kit 286064B15R04 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 1 E0088-40-100 1 Lead 4 NSA5472-4K7 1 Nut 5 AN960C416L 1 Washer 12 NSA5041VBV4-5 1 Bolt 16 NSA5474-3K7 2 Nut 28 AN960C10L 1 Washer 41 NSA5041VBV3-2 1 Bolt 42 NAS1303-1 1 Bolt 64 NSA5475-4K7 2 Nut 86 ABS0114-4-9 1 Bolt Kit 286064B16R03 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 1 E0088-40-100 1 Lead 5 AN960C416L 1 Washer 7 NSA5041VBV3-5 1 Bolt 16 NSA5474-3K7 2 Nut 27 NSA5041VBV3-4 1 Bolt 28 AN960C10L 1 Washer 62 NSA5041VBV4-6 1 Bolt 64 NSA5475-4K7 2 Nut 87 DHS1085-4 1 Washer 91 ABS0114-4-6 1 Bolt Kit 286064B17R01 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 1 E0088-40-100 1 Lead 4 NSA5472-4K7 2 Nut 5 AN960C416L 1 Washer 12 NSA5041VBV4-5 1 Bolt 16 NSA5474-3K7 8 Nut DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 32 Printed in France © AIRBUS 2008 All rights reserved ### Page 41 A300-600A300-600 SERVICE BULLETIN ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 18 NSA5472-3K7 1 Nut 20 NSA5474-4K7 1 Nut 28 AN960C10L 1 Washer 67 ABS0114-4-5 1 Bolt 72 ABS0114-3-6 1 Bolt Kit 286064B18R04 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 1 E0088-40-100 1 Lead 5 AN960C416L 1 Washer 7 NSA5041VBV3-5 3 Bolt 16 NSA5474-3K7 3 Nut 20 NSA5474-4K7 1 Nut 30 NAS1304-4 2 Bolt 64 NSA5475-4K7 2 Nut 65 DHS783-63-18 1 Washer 78 NSA5041VBV4-4 1 Bolt 79 ABS0114-4-4 1 Bolt 87 DHS1085-4 1 Washer Kit 286064B19R02 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 16 NSA5474-3K7 1 Nut 17 NSA5020-3-3 1 Bolt 71 NSA5020-3-4 1 Bolt Kit 286064B20R06 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 14 E0088-41-160 1 Lead 15 AN742D6 1 Clamp 16 NSA5474-3K7 15 Nut 17 NSA5020-3-3 3 Bolt 20 NSA5474-4K7 5 Nut 25 H19200C4 1 Nut 27 NSA5041VBV3-4 1 Bolt 28 AN960C10L 1 Washer 34 NSA5041VBV3-10 2 Bolt 35 NSA5519-2B 4 Clamp 37 NAS1303-2 8 Bolt 38 E0088-10-100 2 Lead 39 E0088-41-100 2 Lead 45 NSA5022-4-21 4 Screw 46 NAS1304-3 2 Bolt 52 A2824028520000 1 Washer DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 33 Printed in France © AIRBUS 2008 All rights reserved ### Page 42 A300-600A300-600 SERVICE BULLETIN ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 53 AN960PD416 2 Washer 74 AN960KD10L 2 Washer 77 NSA5041VBV3-8 1 Bolt Kit 286064B21R01 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 16 NSA5474-3K7 2 Nut 17 NSA5020-3-3 1 Bolt 77 NSA5041VBV3-8 1 Bolt Kit 286064B22R05 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 16 NSA5474-3K7 7 Nut 23 NAS1303-8 1 Bolt 37 NAS1303-2 4 Bolt 82 NSA5480PN3-5 2 Bolt Kit 286064B23R01 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 16 NSA5474-3K7 1 Nut 17 NSA5020-3-3 1 Bolt 38 E0088-10-100 1 Lead 83 NSA5519-4B 1 Clamp Kit 286064B25R01 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 16 NSA5474-3K7 2 Nut 20 NSA5474-4K7 2 Nut 62 NSA5041VBV4-6 1 Bolt 66 NAS1153-12 1 Screw 68 NSA5041VBV4-14 1 Bolt 69 NSA5041VBV3-6 1 Bolt Kit 286064B26R01 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 4 NSA5472-4K7 4 Nut 10 A5715206420100 1 Plate 13 NAS1252-416L 1 Washer DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 34 Printed in France © AIRBUS 2008 All rights reserved ### Page 43 A300-600A300-600 SERVICE BULLETIN Kit 286064B27R01 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 4 NSA5472-4K7 5 Nut 9 A5715206420000 1 Plate 12 NSA5041VBV4-5 4 Bolt 13 NAS1252-416L 1 Washer Kit 286064B28R01 ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 4 NSA5472-4K7 5 Nut 10 A5715206420100 1 Plate 12 NSA5041VBV4-5 4 Bolt 13 NAS1252-416L 1 Washer Kit 286064B39R00 (ADDITIONAL WORK Introduced by Rev 01) ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP 16 NSA5474-3K7 2 Nut 20 NSA5474-4K7 2 Nut 51 NAS1100-3-7 2 Screw 59 E0088-41-304 2 Lead NOTE : Refer to the AIRBUS Standards Manual (SM) if you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin. The SM will give you the correct part number to part number relationship. D. L IST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials DESCRIPTION REFERENCE TO CML QTY PER A/C INST/DISP MA T No. Sealant Mat. No. 09-001 As required Sealant Mat. No. 09-002 As required Low Density Fuel T ank Sealant Mat. No. 09-002D As required Corrosion Inhibiting Brush Consistency Mat. No. 09-013B As required Corrosion Inhibiting Fillet Consistency Mat. No. 09-016B As required Sealant Mat. No. 09-018 As required Corrosion Inhibiting Sealant Sprayable Mat. No. 09-025 As required Sealant Mat. No. 09-530 As required Cleaning agent Mat. No. 11-026 As required Alodine Mat. No. 13-002 As required Primer Mat. No. 16-001C As required DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 35 Printed in France © AIRBUS 2008 All rights reserved ### Page 44 A300-600A300-600 SERVICE BULLETIN DESCRIPTION REFERENCE TO CML QTY PER A/C INST/DISP MA T No. Varnish Mat. No. 16-021 As required NOTE : T o accomplish this Service Bulletin it is necessary to use the expendable parts listed in the AMM 28-25-21 P . Block 401. (2) Components Center T ank ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP EN6115V5-15 1 Screw EN6115V5-16 1 Screw NSA5041VP4-11 2 Screw NSA5041-3-9 1 Screw NSA5061-3 1 Washer NSA5061-4 5 Washer NSA5112-03 1 Washer NSA5112-04 3 Washer NSA5050-3 48 Nut NSA5050-4 21 Nut NSA5050-5 2 Nut NSA5050-6 4 Nut NSA5075-6 2 Nut NSA5182-4 2 Nut NSA5182-3 2 Nut NAS1726-3E 1 Nut NAS1726-4E 7 Nut ASNA2529-4 2 Nut ASNA2529-5 2 Nut ASNA2029-3 2 Nut NSA5355-4CA 1 Nut ASNA2050DXJ4828 2 Rivet ASNA2050DCJ3215 54 Rivet ASNA2050DCJ4020 2 Rivet Additional Work ITEM NEW P ART No. QTY UM KEYWORD ITEM OLD P ART No. INT INST DISP NSA5061-3 1 Washer NSA5112-04 1 Washer E. P ARTS TO BE RE-IDENTIFIED BY THE OPERATOR None F. T OOLING - PRICE AND AVAILABILITY None DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 36 Printed in France © AIRBUS 2008 All rights reserved ### Page 45 A300-600A300-600 SERVICE BULLETIN G. S PECIAL TOOLS None DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 37 Printed in France © AIRBUS 2008 All rights reserved ### Page 46 A300-600A300-600 SERVICE BULLETIN This Page Intentionally Left Blank DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 38 Printed in France © AIRBUS 2008 All rights reserved ### Page 47 A300-600A300-600 SERVICE BULLETIN 3. A CCOMPLISHMENT INSTRUCTIONS A. G ENERAL WARNING : MAKE SURE THA T YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. WARNING : MAKE SURE THA T ALL THE FLIGHT CONTROLS GROUND SAFETY LOCKS AND NOTICES ARE IN POSITION BEFORE YOU ST ART THIS MODIFICA TION. WARNING : BEFORE YOU DO ANY WORK ON THE FUEL SYSTEM OBEY THE SAFETY PRECAUTIONS (REFER TO AMM 28-00-00 P AGE BLOCK 301). WARNING : DO NOT DO ANY WORK IN THE FUEL T ANKS UNTIL THE VAPOR CONCENTRA TION IS BELOW 20% OF THE LOWER EXPLOSION LIMIT (LEL). WARNING : OBEY THE MANUFACTURER’S SAFETY INSTRUCTIONS WHEN YOU USE SEALANTS, VARNISH AND CLEANING AGENTS IN THE FUEL T ANKS. CAUTION : ALWAYS OBEY THE PRECAUTIONS THA T FOLLOW TO KEEP ELECTRICAL WIRING IN A SA TISFACTORY CONDITION (ELECTRICALL Y AND MECHANICALL Y SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REP AIRS OR MODIFICA TIONS, ALWA YS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE, TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTH, ETC; AS NECESSARY ON WIRING AND COMPONENTS. - REGULARL Y REMOVE ALL MET AL SHAVINGS, UNWANTED MA TERIAL AND OTHER CONT AMINA TION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONT AMINA TION AND DAMAGE TO THE ELECTRICAL WIRING INST ALLA TION. IN CASE OF CONT AMINA TION REFER TO ESPM 20-55-00, CLEANING. (1) Preparation (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page block 301). WARNING : MAKE SURE THA T PERSONNEL AND EQUIPMENT ARE CLEAR OF THE TRAVEL RANGES OF THE SLA TS/FLAPS. (b) Fully extend the slats (Refer to AMM 27-80-00, Page block 301). (c) Open the Main Landing Gear (MLG) doors (Refer to AMM 32-12-11, Page block 301). (d) Put access platforms in position as necessary. (e) Defuel and ventilate the center fuel tanks and the wing fuel tanks (Refer to AMM 28-10-00, Page block 301 and AMM 28-25-00, Page block 301). (f) Remove additional wing manhole covers as necessary (Refer to AMM 28-11-22, Page block 401). DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 39 Printed in France © AIRBUS 2008 All rights reserved ### Page 48 A300-600A300-600 SERVICE BULLETIN NOTE : The center tank manhole covers, 147AZ and 148AZ, are removed during the ventilation process. (g) Make sure that the circuit breakers of all systems that you will work on are open, in safety and tagged and warning notices are in position. (h) For Slat T rack Canisters and Screwjack Canisters it is necessary to remove the inboard heat shields (as applicable) to allow the removal/installation of the applicable canister-flange nut (Refer to AMM 57-20-43, Page block 401). (i) For some T rack Cans/Jack Cans it may be difficult to get access to the modification areas due to the small work area. If necessary these T rack Cans/Jack Cans can be temporarily removed to allow access for bonding preparation. For the removal/installation of T rack Cans/Jack Cans, refer to AMM 57-20-43, Page block 401. (j) ADDITIONAL WORK 1 De-energize the aircraft electrical circuits (Refer to AMM 24-41-00, Page block 301). 2 Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page block 301). 3 Put the access platforms in position. 4 Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PWR. 5 Make sure that there is (are) warning notice(s) on the external power receptacle(s) to tell persons not to connect an external power source. 6 Make sure that the EMER EXIT L T pushbutton switch on the panel 26VU is on the DISARM position. 7 In the flight compartment, on the overhead panel 51VU, release the BA T pushbutton switch. 8 Display a warning notice on the overhead panel 51VU to tell persons not to operate the batteries. 9 Display a warning notice on refuel/defuel panel 110VU to tell persons not to operate the NORMAL BA TTERY switch. 10 Display a warning notice in the cockpit to tell persons not to start the Auxiliary Power Unit (APU). 11 Display a warning notice in the cockpit to tell persons not to start ENG 1, 2. 12 Battery disconnection : - For the job set-up, refer to the removal/installation of the batteries (Refer to AMM 24-31-11, Page block 401). DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 40 Printed in France © AIRBUS 2008 All rights reserved ### Page 49 A300-600A300-600 SERVICE BULLETIN - T urn the knurled nut a quarter turn. - Disconnect the connectors. - Put blanking caps on the disconnected electrical connectors. 13 Open, safety and tag these circuit breakers : Depending on aircraft configuration P ANEL DESIGNA TION FIN LOCA TION 22VU FUEL/TK LO L VL AND CAL/L OUTR & R INR & CTR R 1QJ 208/B26 22VU FUEL/TK LO L VL AND CAL/R OUTR & L INR & CTR L 2QJ 208/B27 132VU FUEL/FUELING HI L VL 6QJ 321/P57 132VU FUEL/FUELING OVERFLOW AND CAL 5QJ 321/P58 132VU FUEL/FUELING/CTL & REFUEL VAL VE 1QU 321/P56 132VU FUEL/FQI/SUPPL Y AND IND 1QT 321/P59 132VU FUEL/FQI/CHAN SUPPL Y 1 3QT 321/P60 132VU FUEL/FQI/CHAN SUPPL Y 2 4QT 321/P61 or P ANEL DESIGNA TION FIN LOCA TION 22VU FUEL/TK LO L VL AND CAL/L OUTR & R INR & CTR R 1QJ 208/B26 22VU FUEL/TK LO L VL AND CAL/R OUTR & L INR & CTR L 2QJ 208/B27 128VU FUEL/FUELING HI L VL 6QJ 805/L87 128VU FUEL/FUELING OVERFLOW AND CAL 5QJ 805/L86 128VU FUEL/FUELING/CTL & REFUEL VAL VE 1QU 805/L88 128VU FUEL/FQI/SUPPL Y AND IND 1QT 805/L83 128VU FUEL/FQI/CHAN SUPPL Y 1 3QT 805/L84 128VU FUEL/FQI/CHAN SUPPL Y 2 4QT 805/L85 14 Open the Main Landing Gear (MLG) doors (Refer to AMM 32-12-11, Page block 301). 15 Defuel and ventilate the center fuel tank and the wing fuel tanks (Refer to AMM 28-10-00, Page block 301 and AMM 28-25-00, Page block 301). 16 Remove additional wing manhole covers as necessary (Refer to AMM 28-11-22, Page block 401). 17 Open the access doors 147AZ and 148AZ (Refer to AMM 28-11-29, Page block 401). (2) Standard Practices DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 41 Printed in France © AIRBUS 2008 All rights reserved ### Page 50 A300-600A300-600 SERVICE BULLETIN (a) For access to the slat track canisters and screw-jack canisters (LH and RH wings), refer to AMM 57-20-43, Page block 401. (b) For wing access panels/doors, refer to AMM 06-41-57, Page block 001. (c) For the removal and installation of fasteners, refer to SRM 51-40-20. (d) Cut rivets to the applicable length. (e) For fastener hole and drill information, refer to SRM 51-40-44. (f) For alternative fasteners, refer to SRM 51-40-30. (g) For applicable torque values of fasteners, refer to SRM 51-43-00. (h) For general sealant repair, refer to SRM 51-76-10. (i) For the repair of integral tank sealing, refer to SRM 51-76-20. (j) For the repair of paint coatings, refer to SRM 51-75-10. (k) For the specification of material numbers (Mat.No.), refer to the CML. (l) Clean the modification areas with cleaning agent (Mat. No. 11-026)as necessary . (m) For the installation of the new bonding leads and new bonding positions in the wings fuel tanks and the center fuel, refer to AMM 20-28-11, Page block 001 for: - the preparation of the bonding positions. - the installation of bonding leads, clamps and the installation of bolts as bonding bolts. - the electrical-bonding resistance checks of the bonding positions. - the application of protective coating to bonding items. B. M ODIFICATION (1) Kit 286064A01R05, Kit 286064A02R02 and Kit 286064A03R00 (a) Check the bonding points in the center tank. NOTE : In Fuel Center T ank, the modification consists in : - Checking the bonding points identified as potentially non conform, Refer to Figure 1, Sheet 1. For each point identified check the presence of blue coat : - If blue coat present, no further action. - If no blue coat then : Measure the electrical resistance between part and the structure, (Refer to AMM 20-28-11, Page block 001). DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 42 Printed in France © AIRBUS 2008 All rights reserved ### Page 51 A300-600A300-600 SERVICE BULLETIN - If the ohmic resistance <10mhm, apply the blue coat. - If the ohmic resistance >10mhm, do the bonding, (Refer to AMM 20-28-11, Page block 001). 1 Check the bonding points Items 1 thru 5 at FR44. Refer to Figure 1, Sheet 1 (General location) Refer to Figure 2, Sheets 1 thru 6 (Detailed location) Refer to Figure 3, Sheet 1 (Result table) 2 Check the bonding points Items 6 thru 24 at FR47. Refer to Figure 1, Sheet 1 (General location) Refer to Figure 4, Sheets 1 thru 17 (Detailed location) Refer to Figure 5, Sheet 1 (Result table) 3 Check the bonding points Items 25 thru 29 on the rib 1 (LH side). Refer to Figure 1, Sheet 1 (General location) Refer to Figure 6, Sheets 1 thru 3 (Detailed location) Refer to Figure 7, Sheet 1 (Result table) 4 Check the bonding points Items 30 thru 44 on the intrados panel. Refer to Figure 1, Sheet 1 (General location) Refer to Figure 8, Sheets 1 thru 10 (Detailed location) Refer to Figure 9, Sheet 1 (Result table) 5 Check the bonding points Items 45 thru 51 on the rib 1 (RH side). Refer to Figure 1, Sheet 1 (General location) Refer to Figure 10, Sheets 1 thru 6 (Detailed location) Refer to Figure 11, Sheet 1 (Result table) 6 Check the bonding points Items 52 thru 78 on the extrados panel. Refer to Figure 1, Sheet 1 (General location) Refer to Figure 12, Sheets 1 thru 8 (Detailed location) Refer to Figure 13, Sheet 1 (Result table) (2) Kit 286064A01R05 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 43 Printed in France © AIRBUS 2008 All rights reserved ### Page 52 A300-600A300-600 SERVICE BULLETIN (a) Modify or install the bonding points. 1 Modify the refueling pipes on LH side between FR44 and FR47, valid for aircraft on which Mod. No. 04801H5078 (FUEL - INST ALL TRIM T ANK SYSTEM) is embodied. Refer to Figure 14 Sheets 1 thru 3 a Remove : 1 screw Item (285) Retain 1 washer Item (3) Retain Disengage the bonding lead item (281) without complete removal. - On the sleeve item (268), do a stripping to the dimensions given in the Figure 14 Sheet 3 - Install on the sleeve item (268) : 1 Bonding Lead E0088-10-80 Item 15 1 Nut NAS1726-3E Item 5 1 Clamp AN735D40 Item 13 1 Screw NAS1801-3-8 Item 14 b Install the bonding leads item (281) and 15 with : 1 Screw Item (285) 1 Washer Item (3) NOTE : Items (3) and (285) were retained at removal. c For aircraft on which modification No. 06549 (FUEL - TRIM T ANK SYSTEM - EMBODY ANTI-MODIFICA TION TO ALLOW CHANGE FROM "WET" TO "DRY") is not embodied, do a stripping on the sleeve item (268) to the dimensions given in the Figure 14 Sheet 3 detail E. - Install on the sleeve item (268) : 1 Bonding Lead E0088-10-80 Item 15 1 Nut NAS1726-3E Item 5 1 Clamp AN735D40 Item 13 1 Screw NAS1801-3-8 Item 14 - Remove : 1 Screw Item (220) Retain 1 Nut Item (4) Discard - Install the bonding lead Item 15 with : 1 Screw Item (220) 1 Nut NAS1726-4E Item 4 NOTE : Item (220) was retained at removal. DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 44 Printed in France © AIRBUS 2008 All rights reserved ### Page 53 A300-600A300-600 SERVICE BULLETIN 2 Modify the tube item (283) from TTS pipes, valid for aircraft on which Mod. No. 04801H5078 (FUEL - INST ALL TRIM T ANK SYSTEM) is embodied. Refer to Figure 15 Sheets 1 thru 3 a Remove : Refer to Figure 15 Sheets 2 and 3 1 Screw Item (285) Retain 1 Washer Item (3) Retain Disengage the bonding lead item (284) without complete removal. b On the sleeve item (268), do a stripping to the dimensions given in the Figure 15 Sheet 3 c Install on the sleeve item (268) : 1 Bonding Lead E0088-10-80 Item 15 1 Nut NAS1726-3E Item 5 1 Clamp AN735D40 Item 13 1 Screw NAS1801-3-8 Item 14 d Install the bonding leads item (284) and 15 with : 1 Screw Item (285) 1 Washer Item (3) NOTE : Items (3) and (285) were retained at removal. 3 Modify the sleeves item (268). Refer to Figure 15 Sheets 1, 4 thru 6 a Remove : Refer to Figure 15 Sheet 4 1 Screw Item (2) Retain 1 Washer Item (3) Retain 1 Screw Item (269) Retain 1 Nut Item (4) Discard - Disengage the bonding lead item (16). b On the sleeves item (268), do strippings to the dimensions given in the Figure 15 Sheet 6. c On the tee pipe, do strippings to the dimensions given in the Figure 15 Sheet 6. d Install on the sleeves item (268) : Refer to Figure 15 Sheet 6 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 45 Printed in France © AIRBUS 2008 All rights reserved ### Page 54 A300-600A300-600 SERVICE BULLETIN 2 Bonding Lead E0088-10-160 Item 16 2 Clamp AN735D40 Item 13 2 Nut NAS1726-3E Item 5 2 Screw NAS1801-3-8 Item 14 e Put the bonding leads Item (16) and Item 16 in position on the tee pipe. Refer to Figure 15 Sheet 5 f Install : 1 Screw Item (2) 1 Washer Item (3) 1 Screw Item (269) 1 Nut NAS1726-4E Item 4 NOTE : Items (2), (3) and (269) were retained at removal. 4 Modify the sleeves item (268) from TTS pipes, valid for aircraft on which Mod. No. 04801H5078 (FUEL - INST ALL TRIM T ANK SYSTEM) is embodied. Refer to Figure 15 Sheets 7 and 8 a On the sleeves item (268), do strippings to the dimensions given in the Figure 15 Sheet 8. b Install on the sleeves item (268) : Refer to Figure 15 Sheet 8 3 Bonding Lead E0088-10-80 Item 15 3 Clamp AN735D40 Item 13 3 Nut NAS1726-3E Item 5 3 Screw NAS1801-3-8 Item 14 c Remove from the tee pipe : Refer to Figure 15 Sheet 8 2 Screw Item (569) Retain 2 Nut Item (5) Discard d Put the bonding leads Item 15 in position on the tee pipe. Refer to Figure 15 Sheets 7 and 8 e Install on the tee pipe : Refer to Figure 15 Sheet 8 2 Screw Item (569) 2 Nut NAS1726-3E Item 5 NOTE : Item (569) was retained at removal. DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 46 Printed in France © AIRBUS 2008 All rights reserved ### Page 55 A300-600A300-600 SERVICE BULLETIN 5 Modify the feed pipes, valid for aircraft on which Mod. No. 04801H5078 (FUEL - INST ALL TRIM T ANK SYSTEM) is embodied. Refer to Figure 16 Sheets 1 thru 3 a Remove from LH side : 1 Screw Item (285) Retain 1 Washer Item (413) Retain b On the tube item (333), do a stripping to the dimensions given in the Figure 16 Sheet 2. c Install : 1 Bonding Lead E0088-10-80 Item 15 1 Clamp NSA5519-2B Item 8 1 Bolt NAS1303-3 Item 2 1 Nut NAS1726-3E Item 5 1 Screw Item (285) 1 Washer Item (413) NOTE : Items (285) and (413) were retained at removal. d Remove from RH side : 1 Screw Item (285) Retain 1 Washer Item (413) Retain 1 Nut Item (5) Discard Disengage the bonding lead without complete removal. e On the tube item (334), do a stripping to the dimensions given in the Figure 16 Sheet 3. f Install : 1 Bonding Lead E0088-10-160 Item 16 1 Clamp NSA5519-2B Item 8 1 Bolt NAS1303-3 Item 2 1 Nut NAS1726-3E Item 5 Put the bonding leads Item in position with : 1 Screw Item (285) 1 Washer Item (413) 1 Nut NAS1726-3E Item 5 NOTE : Items (285) and (413) were retained at removal. 6 Modify the feed pipe, valid for aircraft on which Mod. No. 04801H5078 (FUEL - INST ALL TRIM T ANK SYSTEM) is not embodied. Refer to Figure 16 Sheets 1 and 3 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 47 Printed in France © AIRBUS 2008 All rights reserved ### Page 56 A300-600A300-600 SERVICE BULLETIN a Remove from RH side : 1 Screw Item (285) Retain 1 Washer Item (413) Retain 1 Nut Item (5) Discard Disengage the bonding lead without complete removal. b On the tube item (334), do a stripping to the dimensions given in the Figure 16 Sheet 3. c Install : 1 Bonding Lead E0088-10-160 Item 16 1 Clamp NSA5519-2B Item 8 1 Bolt NAS1303-3 Item 2 1 Nut NAS1726-3E Item 5 Put the bonding leads Item in position with : 1 Screw Item (285) 1 Washer Item (413) 1 Nut NAS1726-3E Item 5 NOTE : Items (285) and (413) were retained at removal. 7 Install new bonding lead on the cross feed pipe between FR46 and FR47 Refer to Figure 17 Sheets 1 and 2 a Remove : 1 Screw Item (2) Retain 1 Washer Item (3) Retain - Disengage the bonding lead without complete removal. b On the tube, do a stripping to the dimensions given in the Figure 17 Sheet 2. c Install : 1 Nut NAS1726-3E Item 5 2 Bolt NAS1303-2 Item 17 2 Washer NAS1149F0332P Item 3 1 Bonding Lead E0088-10-125 Item 7 1 Clamp NSA5519-2B Item 8 - Install the bonding leads with : 1 Screw Item (2) 1 Washer Item (3) NOTE : Items (2) and (3) were retained at removal. DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 48 Printed in France © AIRBUS 2008 All rights reserved ### Page 57 A300-600A300-600 SERVICE BULLETIN (3) Kit 286064A02R02 (a) Modify or install the bonding points. 1 Modify the refueling pipes on LH side between FR44 and FR47. Refer to Figure 18 Sheets 1 thru 3 a Remove : 1 Screw Item (285) Retain 1 Washer Item (3) Retain Disengage the bonding lead item (281) without complete removal. - On the sleeve item (268), do a stripping to the dimensions given in the Figure 18, Sheet 3 - Install on the sleeve item (268) : 1 Bonding Lead E0088-10-80 Item 15 1 Nut NAS1726-3E Item 5 1 Clamp AN735D40 Item 13 1 Screw NAS1801-3-8 Item 14 b Install the bonding leads item (281) and 15 with : 1 Screw Item (285) 1 Washer Item (3) NOTE : Items (3) and (285) were retained at removal. c For aircraft on which modification No. 06549 (FUEL - TRIM T ANK SYSTEM - EMBODY ANTI-MODIFICA TION TO ALLOW CHANGE FROM "WET" TO "DRY") is not embodied, do a stripping on the sleeve item (268) to the dimensions given in the Figure 18, Sheet 3 detail E. - Install on the sleeve item (268) : 1 Bonding Lead E0088-10-80 Item 15 1 Nut NAS1726-3E Item 5 1 Clamp AN735D40 Item 13 1 Screw NAS1801-3-8 Item 14 - Remove : 1 Screw Item (220) Retain 1 Nut Item (4) Discard - Install the bonding lead Item 15 with : 1 Screw Item (220) 1 Nut NAS1726-4E Item 4 NOTE : Item (220) was retained at removal. 2 Modify the tube item (283) from TTS pipes. DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 49 Printed in France © AIRBUS 2008 All rights reserved ### Page 58 A300-600A300-600 SERVICE BULLETIN Refer to Figure 19 Sheets 1 thru 3 a Remove : Refer to Figure 19 Sheets 2 and 3 1 Screw Item (1) Retain 1 Nut Item (5) Discard Disengage the bonding lead item (284) without complete removal. b On the sleeve item (268), do a stripping to the dimensions given in the Figure 19, Sheet 3 c Install on the sleeve item (268) : 1 Bonding Lead E0088-10-80 Item 15 1 Nut NAS1726-3E Item 5 1 Clamp AN735D40 Item 13 1 Screw NAS1801-3-8 Item 14 d Install the bonding leads item (284) and 15 with : 1 Screw Item (1) 1 Nut NAS1726-3E Item 5 NOTE : Item (1) was retained at removal. 3 Modify the sleeves item (268). Refer to Figure 19 Sheets 1, 4 thru 6 a Remove : Refer to Figure 19 Sheet 4 1 Screw Item (1) Retain 1 Nut Item (5) Discard 1 Screw Item (255) Retain 1 Nut Item (9) Discard - Disengage the bonding lead item (249). b On the sleeves item (268), do strippings to the dimensions given in the Figure 19, Sheet 6. c On the tee pipe, do strippings to the dimensions given in the Figure 19, Sheets 4 and 6. d Install on the sleeves item (268) : Refer to Figure 19 Sheet 6 2 Bonding Lead E0088-10-160 Item 16 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 50 Printed in France © AIRBUS 2008 All rights reserved ### Page 59 A300-600A300-600 SERVICE BULLETIN 2 Clamp AN735D40 Item 13 2 Nut NAS1726-3E Item 5 2 Screw NAS1801-3-8 Item 14 e Put the bonding leads Item (249) and Item 16 in position on the tee pipe. Refer to Figure 19 Sheet 5 f Install : 1 Screw Item (1) 1 Nut NAS1726-3E Item 5 1 Screw Item (255) 1 Nut NSA5050-4 Item 9 NOTE : Items (1) and (255) were retained at removal. 4 Modify the sleeves item (268) from TTS pipes : Refer to Figure 19 Sheets 7 and 8 a On the sleeves item (268), do strippings to the dimensions given in the Figure 19, Sheet 8. b Install on the sleeves item (268) : Refer to Figure 19 Sheet 8 3 Bonding Lead E0088-10-80 Item 15 3 Clamp AN735D40 Item 13 3 Nut NAS1726-3E Item 5 3 Screw NAS1801-3-8 Item 14 c Remove from the tee pipe : Refer to Figure 19 Sheet 8 2 Screw Item (569) Retain 2 Nut Item (5) Discard d Put the bonding leads Item 15 in position on the tee pipe. Refer to Figure 19 Sheets 7 and 8 e Install on the tee pipe : Refer to Figure 19 Sheet 8 2 Screw Item (569) 2 Nut NAS1726-3E Item 5 NOTE : Items (569) were retained at removal. 5 Modify the feed pipes. Refer to Figure 20 Sheets 1 thru 3 DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 51 Printed in France © AIRBUS 2008 All rights reserved ### Page 60 A300-600A300-600 SERVICE BULLETIN a Remove from LH side : 1 Screw Item (1) Retain 1 Nut Item (5) Discard b On the tube item (333), do a stripping to the dimensions given in the Figure 20, Sheet 2. c Install : 1 Bonding Lead E0088-10-80 Item 15 1 Clamp NSA5519-2B Item 8 1 Bolt NAS1303-3 Item 2 2 Nut NAS1726-3E Item 5 1 Screw Item (1) NOTE : Item (1) was retained at removal. d Remove from RH side : 1 Screw Item (1) Retain 1 Nut Item (5) Discard Disengage the bonding lead without complete removal. e On the tube item (334), do a stripping to the dimensions given in the Figure 20, Sheet 3. f Install : 1 Bonding Lead E0088-10-160 Item 16 1 Clamp NSA5519-2B Item 8 1 Bolt NAS1303-3 Item 2 1 Nut NAS1726-3E Item 5 Put the bonding leads in position with : 1 Screw Item (1) 1 Nut NAS1726-3E Item 5 NOTE : Item (1) was retained at removal. 6 Install new bonding lead on the cross feed pipe between FR46 and FR47 Refer to Figure 21 Sheets 1 and 2 a Remove : 1 Screw Item (1) Retain 1 Nut Item (5) Discard - Disengage the bonding lead without complete removal. b On the tube, do a stripping to the dimensions given in the Figure 21, Sheet 2. DA TE : Jul 28/05 SERVICE BULLETIN No. : A300-28-6064 REVISION No. : 03 - Dec 15/08 Page : 52 Printed in France © AIRBUS 2008 All rights reserved The text continues at https://openairdocs.org/service-documents/airbus/a300-28-6064/file/3c20dad35602.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.