# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL 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



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 24 

### TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - IMPROVE ELECTRICAL INSTALLATION IN WING SHROUD BOX. MODIFICATION No.: 13381S22755 This page transmits Revision No.01 of Service Bulletin No.A300-24-6102 ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue. REASON The equivalent of this Service Bulletin has been validated on A300-600ST aircraft MSN 001. Revision 01 issued to include minor improvements after validation on Aircraft. CHANGES SUMMARY MODIFICATIONS Minor editorial or document structure change N REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Minor editorial or document structure change N GENERAL EVALUATION Minor editorial or document structure change N MATERIAL PRICE INFORMATION Minor editorial or document structure change N EFFECTIVITY Minor editorial or document structure change N CONCURRENT REQUIREMENTS Minor editorial or document structure change N REFERENCES / REPERCUSSIONS Minor editorial or document structure change N NATURE OF THE WORK Minor editorial or document structure change N MANPOWER Minor editorial or document structure change N APPENDICES Minor editorial or document structure change N Fig. A-FSUAA Minor editorial or document structure change N Fig. A-FSUAA Sheet 01 Minor editorial or document structure change N PLANNING INFORMATION EFFECTIVITY Minor editorial or document structure change N DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 1 5

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# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Configuration definition Minor editorial or document structure change N CONF 001 Minor editorial or document structure change N Minor editorial or document structure change N Material Effectivity Minor editorial or document structure change N CONCURRENT REQUIREMENTS Minor editorial or document structure change N REASON Minor editorial or document structure change N History Minor editorial or document structure change N Objective/Action Minor editorial or document structure change N Advantages Minor editorial or document structure change N Operational/Maintenance Consequences Minor editorial or document structure change N DESCRIPTION Minor editorial or document structure change N COMPLIANCE Minor editorial or document structure change N Classification Minor editorial or document structure change N Accomplishment Timescale Minor editorial or document structure change N Minor editorial or document structure change N APPROVAL Minor editorial or document structure change N Minor editorial or document structure change N MANPOWER Minor editorial or document structure change N WEIGHT AND BALANCE Minor editorial or document structure change N ELECTRICAL LOAD DATA Minor editorial or document structure change N Minor editorial or document structure change N REFERENCES Minor editorial or document structure change N PUBLICATION AFFECTED Minor editorial or document structure change N INTERCHANGEABILITY/MIXABILITY Minor editorial or document structure change N SPARES Minor editorial or document structure change N MATERIAL INFORMATION MATERIAL - PRICE AND AVAILABILITY Minor editorial or document structure change N Procurement Addresses Minor editorial or document structure change N Price and Availability Minor editorial or document structure change N INDUSTRY SUPPORT INFORMATION Minor editorial or document structure change N LIST OF COMPONENTS Minor editorial or document structure change N LIST OF MATERIALS - OPERATOR SUPPLIED Minor editorial or document structure change N Consumable Materials Minor editorial or document structure change N Consumable CMLA01 Minor editorial or document structure change N Components Minor editorial or document structure change N Component COMPA01 Minor editorial or document structure change N Equipment Minor editorial or document structure change N PARTS TO BE RE-IDENTIFIED BY OPERATOR Minor editorial or document structure change N TOOLING Minor editorial or document structure change N DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 2 5

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# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL SHEET ACCOMPLISHMENT INSTRUCTIONS TASK 246102- 831-801-001-Modification Minor editorial or document structure change N Task associated data - 001 Minor editorial or document structure change N Subtask 246102-910-001-001 Minor editorial or document structure change N Subtask 246102-839-001-001 Minor editorial or document structure change N Subtask 246102-941-001-001 Minor editorial or document structure change N Subtask 246102-831-001-001 Minor editorial or document structure change N Subtask 246102-710-002-001 Minor editorial or document structure change N Subtask 246102-942-001-001 Minor editorial or document structure change N Fig. A-FBAAA Minor editorial or document structure change N Fig. A-FBAAA Sheet 01 Minor editorial or document structure change N Fig. A-FBBAA Minor editorial or document structure change N Fig. A-FBBAA Sheet 01 Minor editorial or document structure change N Fig. A-FBBAA Sheet 02 Minor editorial or document structure change N Fig. A-FBBAA Sheet 03 Minor editorial or document structure change N Fig. A-FBBAA Sheet 04 Minor editorial or document structure change N Fig. A-FBBAA Sheet 05 Minor editorial or document structure change N Fig. A-FBBAA Sheet 06 Minor editorial or document structure change N Fig. A-FBBAA Sheet 07 Minor editorial or document structure change N FILLING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document. Replace the complete document. Put this Revision Transmittal Sheet in front of the Service Bulletin. HISTORY OF PREVIOUS REVISIONS No previous revision REVISION SEQUENCE ORIGINAL: Aug 13/09 REVISION No. : 01 - Sep 24/10

DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 3 5

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# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 4 5

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# @A300-600 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. 

# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 24 

### TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - IMPROVE ELECTRICAL INSTALLATION IN WING SHROUD BOX. **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR 13381S22755 MINOR None NOTE: 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. REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES During accomplishment of Service Bulletin No. A300-24-6094, it has been noted that the fuel pump electrical power supply harness passing through the hydraulic reservoir panel (Lower Left Hand side) could be damaged in case of chafing and then potentially lead to short circuit, resulting in intermittent operation or loss of the inner tank fuel pump function. This Service Bulletin introduces Teflon bushing at the level of the hydraulic reservoir panel (Lower Left Hand side) to improve the inner tank fuel pump electrical power supply harness protection against chafing and possible damages. Accomplishment of this Service Bulletin will prevent possible fuel pump electrical power supply harness damages in case of chafing at the level of the hydraulic reservoir panel (Lower Left Hand side). Should both pumps become lost in one inner tank then the pumps should be switched-off and the related fuel should be considered as unusable for the rest of the flight. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 1 5

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# @A300-600 SERVICE BULLETIN SUMMARY EVALUATION TABLE COST SAVING NO ETOPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPA01 1 See SB Bush EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

66U AAL AAW ABD AHK AMU CES CSN DLH F2I FDX G8E IRA IRM JAL KAC KAL LAA MNB MON MSR MXU OHY QTR SUD TAR THA TMA UPS UZB NOTE: The equivalent of this Service Bulletin has been validated on A300-600ST aircraft MSN 001. NOTE: This modification is applicable by Service Bulletin only. NOTE: A booklet including photographs taken during the validation of this Service Bulletin is available on AirbusWorld - Maintenance and Engineering - Service Bulletin Information. CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO OBRM NO MANPOWER Task 246102-831-801-001: Modification TOTAL MANHOURS 12.50 DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 2 5

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# @A300-600 SERVICE BULLETIN SUMMARY Task 246102-831-801-001: Modification ELAPSED TIME (HOURS) 7.50 APPENDICES None

DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 3 5

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# @A300-600 SERVICE BULLETIN SUMMARY

**CONF ALL

49QA−A 43QA−A

HYDRAULIC PANEL FR47 FR50

2P 1P



## A Z571 

### A

BE REPLACED BUSHES TO

D_SB_246102_5_SUAA_01_01 Figure A-FSUAA - Sheet 01
DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 4 5

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# @A300-600 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



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 24 

### TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - IMPROVE ELECTRICAL INSTALLATION IN WING SHROUD BOX. MODIFICATION No.: 13381S22755 This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence 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 in part to third parties and shall not be duplicated in any manner (except for the purposes 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. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY NOTE: The equivalent of this Service Bulletin has been validated on A300-600ST aircraft MSN 001. NOTE: This modification is applicable by Service Bulletin only. NOTE: A booklet including photographs taken during the validation of this Service Bulletin is available on AirbusWorld - Maintenance and Engineering - Service Bulletin Information. (1) Models B4-601 B4-603 B4-605R B4-620 B4-622 B4-622R C4-605R/FC4-620 F4-605R F4-622R (2) Effectivity by MSN 0284 0294 0301 0307 0312 0317 0321 0336 0344 0348 0351 0354 0358 0361 0365 0368 0380 0388 0398 0401 0405 0408 0411 0414 0417 0423 0459-0466 0469-0470 0474 0477 0479 0505-0518 0521 0525 0529-0530 0532 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 DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 1 5

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# @A300-600 SERVICE BULLETIN
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 0845-0878 (3) 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 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. OPERATOR MSN 66U 0762 AAL 0423 0459 0460 0461 0463 0466 0469 0470 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 AHK 0855 0856 0857 0858 0859 0860 0870 0871 AMU 0677 0743 CES 0521 0525 0532 0707 0725 0732 0741 0746 0754 0763 CSN 0733 0734 0739 0750 0756 DLH 0380 0401 0405 0623 0701 0773 F2I 0284 0294 0301 0307 0312 0317 0321 0336 0348 0351 0408 0618 FDX 0358 0361 0365 0388 0417 0477 0479 0530 0536 0543 0555 0559 0572 0575 0579 0581 0611 0613 0625 0630 0633 0657 0659 0664 0668 0688 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 0873 0874 0875 0876 0877 0878 G8E 0462 0465 IRA 0632 0696 0723 0727 IRM 0411 0414 0546 0553 0608 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 0731 LAA 0601 0616 MNB 0758 MON 0540 0556 0604 0605 MSR 0561 0607 MXU 0767 0788 OHY 0584 0603 0744 0747 0749 0764 QTR 0554 0560 0614 SUD 0666 0775 TAR 0505 0558 0563 THA 0368 0398 0464 0518 0566 0569 0577 0628 0629 0635 0681 0705 0782 0784 0785 0786 0787 TMA 0872 DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 2 5

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# @A300-600 SERVICE BULLETIN

OPERATOR MSN 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 0845 0846 0847 0848 0849 0850 0851 0852 0853 0854 0861 0862 0863 0864 0865 0866 0867 0868 0869 UZB 0717 0722 (4) Configuration by MSN MSN CONFIGURATION 0284 0294 0301 0307 0312 0317 0321 0336 0344 0348 0351 0354 0358 0361 0365 0368 0380 0388 0398 0401 0405 0408 0411 0414 0417 0423 0459 0460 0461 0462 0463 0464 0465 0466 0469 0470 0474 0477 0479 0505 0506 0507 0508 0509 0510 0511 0512 0513 0514 0515 0516 0517 0518 0521 0525 0529 0530 0532 0536 0540 0543 0546 0553 0554 0555 0556 0557 0558 0559 0560 0561 0563 0566 0569 0572 0575 0577 0579 0581 0582 0584 0601 0602 0603 0604 0605 0606 0607 0608 0609 0610 0611 0612 0613 0614 0615 0616 0617 0618 0619 0621 0623 0625 0626 0627 0628 0629 0630 0631 0632 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 0722 0723 0724 0725 0726 0727 0728 0729 0730 0731 0732 0733 0734 0735 0736 0737 0738 0739 0740 0741 0742 0743 0744 0745 0746 0747 0748 0749 0750 0752 0753 0754 0755 0756 0757 0758 0759 0760 0761 0762 0763 0764 0766 0767 0768 0769 0770 0771 0772 0773 0774 0775 0777 0778 0779 0780 0781 0782 0783 0784 0785 0786 0787 0788 0789 0790 0791 0792 0793 0794 0797 0799 0800 0801 0802 0803 0804 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 0836 0837 0838 0839 0840 0841 0845 0846 0847 0848 0849 0850 0851 0852 0853 0854 0855 0856 0857 0858 0859 0860 0861 0862 0863 0864 0865 0866 0867 0868 0869 0870 0871 0872 0873 0874 0875 0876 0877 0878 001

(5) Configuration definition **CONF 001 Config. 01 is valid for all the aircraft given in the effectivity of this Service Bulletin as a standard configuration. (6) Material Effectivity MATERIAL QTY PER A/C SEE NOTES Component COMPA01 1 Consumable CMLA01 1

DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 3 5

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# @A300-600 SERVICE BULLETIN
B. CONCURRENT REQUIREMENTS None C. REASON (1) History During accomplishment of Service Bulletin No. A300-24-6094, it has been noted that the fuel pump electrical power supply harness passing through the hydraulic reservoir panel (Lower Left Hand side) could be damaged in case of chafing and then potentially lead to short circuit, resulting in intermittent operation or loss of the inner tank fuel pump function. (2) Objective/Action This Service Bulletin introduces Teflon bushing at the level of the hydraulic reservoir panel (Lower Left Hand side) to improve the inner tank fuel pump electrical power supply harness protection against chafing and possible damages. (3) Advantages Accomplishment of this Service Bulletin will prevent possible fuel pump electrical power supply harness damages in case of chafing at the level of the hydraulic reservoir panel (Lower Left Hand side). (4) Operational/Maintenance ConsequencesShould both pumps become lost in one inner tank then the pumps should be switchedoff and the related fuel should be considered as unusable for the rest of the flight. D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 246102-831-801-001: Modification (1) Replace the bushes in the hydraulic reservoir panel at LH side. E. COMPLIANCE (1) Classification MANDATORY (2) Accomplishment Timescale Accomplishment of this Service Bulletin is expected to be rendered mandatory by the issue of an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA). The accomplishment timescale, which has not yet been defined, will be given in the AD.

DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 4 5

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# @A300-600 SERVICE BULLETIN
F. APPROVAL 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, and 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. MANPOWER The manpower estimates given in this Service Bulletin are based on the 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 operator’s 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, sealants, etc., and general administration work are also not included. Task 246102-831-801-001: Modification Get Access 1.00 On Aircraft Replace the bushes in the hydraulic reservoir panel at LH side. 10.00 Tests 0.50 Close-Up 1.00 TOTAL MANHOURS 12.50 ELAPSED TIME (HOURS) 7.50 H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-41-53 06-41-57 24-00-00 28-21-12 52-10-00 52-30-00 52-52-00 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-55-00 Structural Repair Manual (SRM) 51-40-21 K. PUBLICATION AFFECTED None L. INTERCHANGEABILITY/MIXABILITY Not Applicable DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 5 5

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# @A300-600 SERVICE BULLETIN
M. SPARES None

DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 6 5

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# @A300-600 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Customers with aircraft shown in the effectivity of this Service Bulletin should send a purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is : Component COMPA01 AIRBUS SPARES SUPPORT AND SERVICES Weg beim Jaeger 150 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 No AIRBUS kit will be provided. Parts required to accomplish this Service Bulletin are to be purchased by a Spares Purchase Order. B. INDUSTRY SUPPORT INFORMATION AIRBUS will not provide industry support for accomplishment of this Service Bulletin. C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Two Part Paste Adhesive 08-078 As required Isopropyl Alcohol 11-010 As required (2) Components Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 2 A0041094120000 2 Bush

DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 7 5

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# @A300-600 SERVICE BULLETIN (3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 8 5

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# @A300-600 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 246102-831-801-001 - Modification WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS : - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC. AS NECESSARY ON WIRING AND COMPONENTS, - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IF THERE IS CONTAMINATION, ESPM 20-55-00 Task Associated Data Manpower TOTAL MANHOURS 12.50 ELAPSED TIME (HOURS) 7.50 A. GENERAL (1) Subtask 246102-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Consumable Material List (CML) Structural Repair Manual (SRM) 51-40-21 (a) For the specification of the material numbers (Mat. No.), Refer to Consumable Material List (CML). (b) Remove/install the fasteners (Refer to SRM 51-40-21). (2) Subtask 246102-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC
DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 9 5

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# @A300-600 SERVICE BULLETIN Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 246102-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 24-00-00, Page Block 301 52-10-00, Page Block 001 52-30-00, Page Block 001 52-52-00, Page Block 001 (a) Make sure that the aircraft is grounded (Refer to AMM 24-00-00 Page Block 301). (b) Put the access platforms in position. (c) Open the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (d) On the lower surface of the LH wing, remove panels as necessary (Refer to AMM 06-41-57, Page Block 001). (e) Open the cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (f) Open fixed interior door (Refer to AMM 52-52-00, Page Block 001, AMM 06-41-53, Page Block 001). (g) Depending on aircraft configuration : 1 Open, safety and tag the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 101VU FUEL/L INNER TK/PUMP2/SUPPLY 1QA GEN1/A20 101VU FUEL/L INNER TK/PUMP1/SUPPLY 7QA GEN2/A20 128VU FUEL/L INNER TK/PUMP2/CTL 59QA 802/P84 128VU FUEL/L INNER TK/PUMP1/CTL 69QA 802/P82

DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 10 5

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# @A300-600 SERVICE BULLETIN

2 Or open, safety and tag the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 101VU FUEL/L INNER TK/PUMP2/SUPPLY 1QA ESS1/B01 101VU FUEL/L INNER TK/PUMP1/SUPPLY 7QA GEN2/A23 132VU FUEL/L INNER TK/PUMP2/CTL 59QA 323/M61 132VU FUEL/L INNER TK/PUMP1/CTL 69QA 322/N60
C. PROCEDURE (1) Subtask 246102-831-001-001 - Replace the bushes in the hydraulic reservoir panel at LH side. Manpower Resources Manhours 10.00 Minimum number of person 1 Subtask elapsed time 10.00 Skills NON SPECIFIC Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 A0041094120000 2 Bush Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Two Part Paste Adhesive 08-078 As required Isopropyl Alcohol 11-010 As required References Fig. A-FBAAA For access, Removal/Installation of the Inserts and Disconnection/Connection of the Plug 43QA-A and 49QA-A Sheet 01

Fig. A-FBBAA Replacement of the Bushes Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 Sheet 07
DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 11 5

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# @A300-600 SERVICE BULLETIN (a) Disconnect the cable harnesses 43QA-A and 49QA-A. Refer to Fig. A-FBAAA Sheet 01 Refer to Fig. A-FBBAA Sheet 01 1 Move the wiring between the pressure seal 35VP and the fuel pump 43QA (route 1P).
a For access to 43QA-A and the wiring, remove and retain all the inserts of the fairing. b Disconnect the plug 43QA-A.
c Move the wiring from the outer fuselage to the hydraulic panel. NOTE: To help the movement of the wiring through the hole, it is possible to remove and retain all the necessary clamps. 2 Move the wiring between the pressure seal 31VP and the fuel pump 49QA (route 2P).
a For access to 49QA-A and the wiring, remove and retain all the inserts of the fairing. b Disconnect the plug 49QA-A.
c Move the wiring from the outer fuselage to the hydraulic panel. NOTE: To help the movement of the wiring through the hole, it is possible to remove and retain all the necessary clamps. (b) Remove the aluminium bushes in the hydraulic reservoir panel at LH side. Refer to Fig. A-FBBAA Sheet 01, Fig. A-FBBAA Sheet 02 and Fig. A-FBBAA Sheet 03 1 Remove : 2 Bush Item (1) Discard NOTE: Remove the aluminium bushes as carefully as possible to prevent damage on the honeycomb section. (c) Lightly break the edge of the hole with sand paper after the removal of the bushes. (d) Install the new teflon bushes in the hydraulic reservoir panel at LH side. Refer to Fig. A-FBBAA Sheet 01, Fig. A-FBBAA Sheet 04, Fig. A-FBBAA Sheet 05, Fig. A-FBBAA Sheet 06 and Fig. A-FBBAA Sheet 07 1 Do a cleaning of the areas to bond using Isopropyl Alcohol 11-010 As required DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 12 5

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# @A300-600 SERVICE BULLETIN

. 2 Put the teflon bushes Item 2 in position. 3 Adjust the teflon bushes Item 2 as shown on Fig. A-FBBAA Sheet 04 Section C-C and D-D, to obtain a gap of 1 mm (0.04 inch) with the honeycomb section. 4 Install : 2 Bush A0041094120000 Item 2 NOTE: Install the teflon bushes Item 2 using Two Part Paste Adhesive 08-078 As required (e) Connect the cable harnesses 43QA-A and 49QA-A. Refer to Fig. A-FBAAA Sheet 01 Refer to Fig. A-FBBAA Sheet 01 1 Re-install the wiring between the pressure seal 35VP and the fuel pump 43QA (route 1P). NOTE: The clamps of the wiring and the inserts of the fairing were retained at removal.
a Move the wiring from the hydraulic panel to the outer fuselage. b Connect the plug 43QA-A.
c Install all the inserts of the fairing. NOTE: The clamps of the wiring and the inserts of the fairing were retained at removal. 2 Re-install the wiring between the pressure seal 31VP and the fuel pump 49QA (route 2P).
a Move the wiring from the hydraulic panel to the outer fuselage. NOTE: If removed, install the clamps. b Connect the plug 49QA-A.
c Install all the inserts of the fairing. NOTE: The clamps of the wiring and the inserts of the fairing were retained at removal.

DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 13 5

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# @A300-600 SERVICE BULLETIN
D. TEST (1) Subtask 246102-710-002-001 - Operational Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 28-21-12, Page Block 501 (a) Do the operational test of the inner tanks booster pump (Refer to AMM 28-21-12 Page Block 501). E. CLOSE-UP (1) Subtask 246102-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 06-41-57, Page Block 001 52-10-00, Page Block 001 52-30-00, Page Block 001 52-52-00, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Depending on aircraft configuration : 1 Remove safety clips and tags and close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 101VU FUEL/L INNER TK/PUMP2/SUPPLY 1QA GEN1/A20 101VU FUEL/L INNER TK/PUMP1/SUPPLY 7QA GEN2/A20 128VU FUEL/L INNER TK/PUMP2/CTL 59QA 802/P84 128VU FUEL/L INNER TK/PUMP1/CTL 69QA 802/P82
2 Or remove safety clips and tags and close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 101VU FUEL/L INNER TK/PUMP2/SUPPLY 1QA ESS1/B01 101VU FUEL/L INNER TK/PUMP1/SUPPLY 7QA GEN2/A23 DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 14 5

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# @A300-600 SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE NOTES 132VU FUEL/L INNER TK/PUMP2/CTL 59QA 323/M61 132VU FUEL/L INNER TK/PUMP1/CTL 69QA 322/N60 (c) Close fixed interior door (Refer to AMM 52-52-00, Page Block 001, AMM 06-41-53, Page Block 001). (d) On the lower surface of the LH wing , install panels as necessary (Refer to AMM 06-41-57, Page Block 001). (e) Close the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (f) Close the cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (g) Restore the systems and the aircraft to normal operating condition. (h) Remove the access platforms.

DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 15 5

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# @A300-600 SERVICE BULLETIN

**CONF ALL

VIEW LOOKING UP RIB1 FUEL PUMP DATUM REAR SPAR DATUM

RIB2

REAR FAIRING BOOSTER PUMP MOUNTING FLANGE FORWARD FAIRING LH SIDE SHOWN INSERTS OF THE FAIRING TO BE REMOVED

CONNECTORS 43QA−A OR 49QA−A TO BE DISCONNECTED D_SB_246102_5_BAAA_01_01 

### A



## A **FWD**



## B **B**
**B**

REMOVALPULL

USE TOOL No205859 TURN PULL DRAIN

Figure A-FBAAA - Sheet 01 For access, Removal/Installation of the Inserts and Disconnection/Connection of the Plug 43QA-A and 49QA-A DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 16 5

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# @A300-600 SERVICE BULLETIN

**CONF ALL

49QA−A 43QA−A

HYDRAULIC PANEL FR47 FR50

TO FAIRING UNDER WING (OUTER FUSELAGE) TO METALLIC CONDUITS OUTER FUSELAGE

CLAMPS TO BE REMOVED IF NECESSARY

CLAMPS TO BE REMOVED IF NECESSARY TO 35VP
2P 1P TO 31VP



## A

**B C**  Z571 

### A

D_SB_246102_5_BBAA_01_01 Figure A-FBBAA - Sheet 01 Replacement of the Bushes DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 17 5

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# @A300-600 SERVICE BULLETIN

**CONF ALL



## BEFORE

**B B**  **A A**  RIB1

FR47

FR48

FR49

TOP VIEW **F W**  **D** 

## B

D_SB_246102_5_BBAA_02_01 Figure A-FBBAA - Sheet 02 Replacement of the Bushes DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 18 5

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# @A300-600 SERVICE BULLETIN

**CONF ALL

TO REMOVE THE BUSHES ITEM . DRILL CAREFULLY FROM THE UNDER WING THROUGH THE BUSHES, TO PREVENT DAMAGE ON THE HONEYCOMB SECTION **NOTE:** 

## A **A**

**B B**  (1)

(1) (1)

D_SB_246102_5_BBAA_03_01 Figure A-FBBAA - Sheet 03 Replacement of the Bushes DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 19 5

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# @A300-600 SERVICE BULLETIN

**CONF ALL



## AFTER

RIB1

FR47

FR48

FR49

TOP VIEW **F W**  **D** 

## C **C C**  **D D** 

D_SB_246102_5_BBAA_04_01 Figure A-FBBAA - Sheet 04 Replacement of the Bushes DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 20 5

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# @A300-600 SERVICE BULLETIN

**CONF ALL

DO A BONDING OF THE BUSHES WITH MAT. No. 08−078 ADJUST IF NECESSARY THE BUSH ITEM TO OBTAIN A GAP OF 1 mm (0.04 in) WITH THE HONEYCOMB DO A CLEANING OF THE AREAS WITH MAT. No. 11−010. **NOTE:** 2 01 02 03 02 03 01 2 01

02 03 

## C **C**

**D D**  **D**

**E** 2

D_SB_246102_5_BBAA_05_01 Figure A-FBBAA - Sheet 05 Replacement of the Bushes DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 21 5

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# @A300-600 SERVICE BULLETIN

**CONF ALL

ADJUST IF NECESSARY THE BUSH ITEM TO OBTAIN A GAP OF 1 mm (0.04 in) 1 mm (0.04 in)

**NOTE:** 01 WITH THE HONEYCOMB SECTION. 2 01

**F W**  **D** 

## D 2

D_SB_246102_5_BBAA_06_00 Figure A-FBBAA - Sheet 06 Replacement of the Bushes DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 22 5

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# @A300-600 SERVICE BULLETIN

**CONF ALL

ADJUST IF NECESSARY THE BUSH ITEM TO OBTAIN A GAP OF 1 mm (0.04 in) 1 mm (0.04 in)

**NOTE:** 01 WITH THE HONEYCOMB SECTION. 2 01 2

**F W**  **D** 

## E

D_SB_246102_5_BBAA_07_00 Figure A-FBBAA - Sheet 07 Replacement of the Bushes DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 23 5

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# @A300-600 SERVICE BULLETIN REPORTING SHEET 

### TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - IMPROVE ELECTRICAL INSTALLATION IN WING SHROUD BOX. MODIFICATION No.: 13381S22755 Please complete the appropriate item (A or B): A - SB WILL BE embodied YES/NO (if NO please comment) If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiment:

B - SB HAS BEEN embodied on aircraft: Operator comments:
From Airline: Name/Title: Signature: Date: If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next normal revision or prior to SB embodiment, please indicate required service(s): Either: Modification Operational Impact (MOI), if available YES/NO Or : Intermediate revision YES/NO Important Information: This SB will only be incorporated in your maintenance and operational documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in - Updating of maintenance documentation to show pre and post SB data. - Updating of maintenance and operational documentation to show post SB data after embodiment. If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include them in the manual revisions. Refer to SIL 00-037 for detailed information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 93 28 06 e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, SB lists via letters or fax are also accepted.

DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 1 5

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# @A300-600 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4 3 2 1 - Quality rating of the Accomplishment Instructions 4 3 2 1 - Quality rating of the Illustrations 4 3 2 1 - Is this SB easy to understand ? Y / N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: Date: Name/Title: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.

DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102 REVISION No.: 01 - Sep 24/10 Page: 1 5

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