# @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: ELECTRICAL POWER -INSPECTION OF SHUT-OFF VALVE BONDING LEAD MODIFICATION No.: None This page transmits Revision No.01 of Service Bulletin No.A300-24-6108 ADDITIONAL WORK **CONF ALL ADDITIONAL WORK is required by this revision for aircraft inspected by the original issue of this Service Bulletin. The ADDITIONAL WORK for this Service Bulletin is issued to ensure that the correct bonding leads (one on RH and one on LH) are inspected. At original issue, the description of the bonding leads (two on RH and two on LH) to be inspected was misleading and some operators could have inspected other bonding leads than the one to be checked. REASON Revision 01 issued to clarify the bonding leads (RH and LH) to be inspected, to replace PN E0088-10-80 by PN E0088-10-80NN (as per Standards Manual evolution) and to update the effectivity. CHANGES The main changes of revision 01 are: - To modify figure A-FBAAA to correctthe bonding lead to be inspected. - To modify the Inspection Report (figure A-FRAAA) in accordance with the correct bonding leads (RH and LH) to be inspected. - To modify the COMPA01: . Bonding lead PN E0088-10-80 replaced by PN E0088-10-80NN in accordance with Standards Manual. . Bonding leads quantity changed from 4 to 2. . Nuts (PN NSA5050-3) quantity changed from 8 to 4.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 1 5

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# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL SHEET - To add a NOTE to align the clamps. - To update the effectivity. SUMMARY REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES REASON UPDATED R EFFECTIVITY OPERATOR LIST UPDATED R MANPOWER MANPOWER UPDATED R APPENDICES APPENDICES UPDATED R PLANNING INFORMATION EFFECTIVITY EFFECTIVITY RELATED INFORMATION UPDATED R Configuration definition CONF 001 CONFIGURATION DEFINITION UPDATED R Material Effectivity MATERIAL EFFECTIVITY UPDATED MATERIAL SET QUANTITY UPDATED MATERIAL SET UPDATED R
REASON History HISTORY UPDATED R Objective/Action OBJECTIVE/ACTION UPDATED R COMPLIANCE Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED CONFIGURATION UPDATED R APPROVAL APPROVAL UPDATED R MANPOWER MANPOWER UPDATED R REFERENCES REFERENCED DOCUMENTATION UPDATED R MATERIAL INFORMATION MATERIAL - PRICE AND AVAILABILITY Procurement Addresses PROCUREMENT ADDRESSES UPDATED MATERIAL SET UPDATED R Price and Availability PRICE AND AVAILABILITY UPDATED R LIST OF MATERIALS - OPERATOR SUPPLIED Consumable Materials CONSUMABLE MATERIALS UPDATED R Consumable CMLA01 CONSUMABLE MATERIAL SET ADDED N Components Component COMPA01 PART MATERIAL SET UPDATED QUANTITY UPDATED PART NUMBER UPDATED R
ACCOMPLISHMENT INSTRUCTIONS TASK 246108- 832-801-001-Inspection Subtask 246108-910-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED R

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 2 5

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# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
Subtask 246108-832-001-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED PART NUMBER UPDATED CONSUMABLE UPDATED FIGURE REFERENCE UPDATED NOTE UPDATED MATERIAL LIST UPDATED REFERENCES UPDATED R

Subtask 246108-832-002-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED PART NUMBER UPDATED CONSUMABLE UPDATED FIGURE REFERENCE UPDATED NOTE UPDATED MATERIAL LIST UPDATED REFERENCES UPDATED R

TASK 246108- 832-802-001-Inspection - ADDITIONAL WORK TASK SOLUTION ADDED N Task associated data - 001 TASK ASSOCIATED DATA ADDED N Subtask 246108-910-002-001 SUBTASK SOLUTION ADDED N Subtask 246108-839-002-001 SUBTASK SOLUTION ADDED N Subtask 246108-941-002-001 SUBTASK SOLUTION ADDED N Subtask 246108-865-003-001 SUBTASK SOLUTION ADDED N Subtask 246108-010-003-001 SUBTASK SOLUTION ADDED N Subtask 246108-010-004-001 SUBTASK SOLUTION ADDED N Subtask 246108-832-003-001 SUBTASK SOLUTION ADDED N Subtask 246108-832-004-001 SUBTASK SOLUTION ADDED N Subtask 246108-865-004-001 SUBTASK SOLUTION ADDED N Subtask 246108-700-002-001 SUBTASK SOLUTION ADDED N Subtask 246108-410-003-001 SUBTASK SOLUTION ADDED N Subtask 246108-410-004-001 SUBTASK SOLUTION ADDED N Subtask 246108-942-003-001 SUBTASK SOLUTION ADDED N Fig. A-FBAAA Fig. A-FBAAA Sheet 01 SHEET UPDATED R Fig. A-FFAAA FIGURE SOLUTION ADDED N Fig. A-FFAAA Sheet 01 SHEET ADDED N Fig. A-FBCAA FIGURE SOLUTION ADDED N Fig. A-FBCAA Sheet 01 SHEET ADDED N Fig. A-FFBAA FIGURE SOLUTION ADDED N Fig. A-FFBAA Sheet 01 SHEET ADDED N Fig. A-FBB FIGURE DELETED FOR APPLICABLE MSN D Appendix 01 - Inspection Report Fig. A-FRAAA FIGURE SOLUTION ADDED N Fig. A-FRAAA Sheet 01 SHEET ADDED N Fig. A-FAA FIGURE DELETED FOR APPLICABLE MSN D

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 3 5

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# @A300-600 SERVICE BULLETIN REVISION TRANSMITTAL SHEET Appendix 03 - Inspection Report (Additional Work) APPENDIX CONTENT APPENDIX CONTENT ADDED N Fig. A-FRBAA FIGURE SOLUTION ADDED N Fig. A-FRBAA Sheet 01 SHEET ADDED N Appendix 04 - Gantt Chart (Additional Work) APPENDIX CONTENT APPENDIX CONTENT ADDED N Fig. A-FADAA FIGURE SOLUTION ADDED N Fig. A-FADAA Sheet 01 SHEET ADDED 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: Jul 09/10 REVISION No. : 01 - Mar 26/13

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 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: ELECTRICAL POWER -INSPECTION OF SHUT-OFF VALVE BONDING LEAD **CONF ALL MODIFICATIONS None REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES During maintenance an operator has reported an inoperative GREEN hydraulic Fire Shut-Off Valve (FSOV). Troubleshooting evidenced some damages : - A wire located between Engine 2 hydraulic FSOV and wing rear spar (zones 575/675) has been found cut - A bonding lead (E0088-10-80NN) located between Rib 7A and Rib 8 below Hydraulic Pressure Lines has been found cut. Investigations on different aircraft have shown that some aircraft are fitted with bonding leads of (120mm (4.72in) length instead of 80mm (3.15in)). This overlength can lead to contact and chafing between the harness and the bonding lead, which can lead to the findings. It can also entail damages in case of lightning strike. This Inspection Service Bulletin requires inspection and repair (when necessary) of the : - Wires located between Engines hydraulic FSOV and wing rear spar (zones 575/675) - Two bonding leads (RH and LH) (E0088-10-80NN) located between Rib 7A and Rib 8 below Hydraulic Pressure Lines. Accomplishment of this Inspection Service Bulletin will avoid such a case of inoperative hydraulic FSOV due to wiring damaged by a bonding lead and restore the aircraft system reliability.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 1 5

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# @A300-600 SERVICE BULLETIN SUMMARY GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO COST SAVING NO ETOPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO NOTE (1): Service Bulletin must be accomplished. 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 Bonding leads, Nuts. EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

14S 34Z 77T ABD ABR AHK BCS CES F2I FDX G8E I2L IRA IRM KAC KAL MNB MON MSR MXU OHY QTR RLB SUD TAR THA TMA UPS URS UZB CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO OBRM NO MANPOWER Task 246108-832-801-001: Inspection TOTAL MANHOURS 8.00 DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 2 5

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# @A300-600 SERVICE BULLETIN SUMMARY Task 246108-832-801-001: Inspection ELAPSED TIME (HOURS) 4.50 Task 246108-832-802-001: Inspection - ADDITIONAL WORK TOTAL MANHOURS 8.00 ELAPSED TIME (HOURS) 4.50 APPENDICES Appendix 01 - Inspection Report Appendix 02 - Gantt Chart Appendix 03 - Inspection Report (Additional Work) Appendix 04 - Gantt Chart (Additional Work)

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 3 5

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# @A300-600 SERVICE BULLETIN SUMMARY

**CONF ALL

AREA TO BE INSPECTED 

### A

Z575 (Z675)

RIB5 RIB8

REAR SPAR


## A
LH SIDE SHOWN RH SIDE SYMMETRICAL

D_SB_246108_5_SAAA_01_01 RIB7A

Figure A-FSAAA - Sheet 01

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 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: ELECTRICAL POWER -INSPECTION OF SHUT-OFF VALVE BONDING LEAD MODIFICATION No.: None 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 (1) Models 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 0321 0336 0344 0348 0351 0358 0361 0365 0380 0388 0401 0405 0408 0411 0414 0417 0462 0464-0465 0477 0479 0505-0506 0509 0514 0516 0518 0521 0525 0529-0530 0532 0536 0540 0543 0546 0553-0561 0563 0566 0569 0572 0575 0577 0579 0581-0582 0584 0602-0605 0607-0611 0613-0614 0617-0618 0621 0623 0625-0633 0635 0637 0641 0643 0657 0659 0662 0664 0666 0668 0670 0673 0677 0679 0681 0683 0685 0688 0692 0694 0696 0699 0701 0703 0705 0707 0709 0711 0713 0715 0717 0719 0721-0746 0748-0750 0752-0764 0766-0775 0777-0794 0797 0799-0841 0845-0878

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 1 5

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# @A300-600 SERVICE BULLETIN (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 14S 0609 34Z 0685 0692 0731 77T 0838 ABD 0529 0557 ABR 0683 0770 AHK 0855 0856 0857 0858 0859 0860 0870 0871 BCS 0602 0617 0621 0637 0641 0670 0679 0703 0711 0724 0729 0730 0737 0740 0753 0783 CES 0521 0525 0532 0707 0725 0732 0741 0746 0754 0763 F2I 0284 0294 0301 0307 0312 0321 0336 0348 0351 0518 0610 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 0506 0509 0514 0516 I2L 0677 0743 IRA 0632 0696 0723 0727 IRM 0380 0401 0405 0408 0411 0414 0546 0553 0608 0618 0623 0701 0750 0762 0773 KAC 0344 0673 0694 0699 0719 0721 KAL 0582 0627 0631 0662 MNB 0734 0739 0755 0756 0758 MON 0540 0556 0604 0605 MSR 0561 0607 MXU 0767 0788 0797 0836 0837 OHY 0584 0603 0744 0749 0764 QTR 0554 0560 0614 RLB 0626 0643 SUD 0666 0775 TAR 0505 0558 0563 THA 0464 0566 0569 0577 0628 0629 0635 0681 0705 0782 0784 0785 0786 0787 TMA 0872 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 URS 0733
DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 2 5

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# @A300-600 SERVICE BULLETIN

OPERATOR MSN UZB 0717 0722 (4) Configuration by MSN MSN CONFIGURATION 0284 0294 0301 0307 0312 0321 0336 0344 0348 0351 0358 0361 0365 0380 0388 0401 0405 0408 0411 0414 0417 0462 0464 0465 0477 0479 0505 0506 0509 0514 0516 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 0602 0603 0604 0605 0607 0608 0609 0610 0611 0613 0614 0617 0618 0621 0623 0625 0626 0627 0628 0629 0630 0631 0632 0633 0635 0637 0641 0643 0657 0659 0662 0664 0666 0668 0670 0673 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 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. 001 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 B. CONCURRENT REQUIREMENTS None C. REASON (1) History During maintenance an operator has reported an inoperative GREEN hydraulic Fire Shut-Off Valve (FSOV). DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 3 5

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# @A300-600 SERVICE BULLETIN Troubleshooting evidenced some damages : - A wire located between Engine 2 hydraulic FSOV and wing rear spar (zones 575/675) has been found cut - A bonding lead (E0088-10-80NN) located between Rib 7A and Rib 8 below Hydraulic Pressure Lines has been found cut. Investigations on different aircraft have shown that some aircraft are fitted with bonding leads of (120mm (4.72in) length instead of 80mm (3.15in)). This overlength can lead to contact and chafing between the harness and the bonding lead, which can lead to the findings. It can also entail damages in case of lightning strike. (2) Objective/Action This Inspection Service Bulletin requires inspection and repair (when necessary) of the : - Wires located between Engines hydraulic FSOV and wing rear spar (zones 575/675) - Two bonding leads (RH and LH) (E0088-10-80NN) located between Rib 7A and Rib 8 below Hydraulic Pressure Lines. (3) Advantages Accomplishment of this Inspection Service Bulletin will avoid such a case of inoperative hydraulic FSOV due to wiring damaged by a bonding lead and restore the aircraft system reliability. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 246108-832-801-001: Inspection (1) Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on Wing Rear Spar (RH side). (2) Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on Wing Rear Spar (LH side). Task 246108-832-802-001: Inspection - ADDITIONAL WORK (1) Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on Wing Rear Spar (RH side). (2) Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on Wing Rear Spar (LH side).
DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 4 5

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# @A300-600 SERVICE BULLETIN
E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the thresholds given in Table 1 but reference should be made to the AD for confirmation of the mandated accomplishment timescale. Table 1, Config. 001: Detailed inspection of the FSOV bonding leads and of the wires located on wing rear spar (zones 575-675) COMPLIANCE TIME (Whichever occurs later) CONDITION ACTION THRESHOLD GRACE PERIOD REPETITIVE INTERVAL Aircraft on which original issue of this ISB has not been accomplished Inspect in accordance with SUBTASK 246108-832-001 001 Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on Wing Rear Spar (RH side). and SUBTASK 246108-832-002 001 Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on Wing Rear Spar (LH side). Within 4,500 Flight Hours (FH) or 30 months after the reception of the Service Bulletin at original issue whichever occurs first. None None

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 5 5

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# @A300-600 SERVICE BULLETIN
Table 1, Config. 001: Detailed inspection of the FSOV bonding leads and of the wires located on wing rear spar (zones 575-675) COMPLIANCE TIME (Whichever occurs later) CONDITION ACTION THRESHOLD GRACE PERIOD REPETITIVE INTERVAL Aircraft on which original issue of this ISB has been accomplished Inspect in accordance with SUBTASK 246108-832-003 001 Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on Wing Rear Spar (RH side). and SUBTASK 246108-832-004 001 Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on Wing Rear Spar (LH side). Within 4,500 Flight Hours (FH) or 30 months after the reception of the Service Bulletin at Revision No. 01 whichever occurs first. None None

F. APPROVAL Approved under EASA Design Organization 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 246108-832-801-001: Inspection Get Access 2.00 On Aircraft Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on Wing Rear Spar (RH side). 1.50

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 6 5

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# @A300-600 SERVICE BULLETIN
Task 246108-832-801-001: Inspection Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on Wing Rear Spar (LH side). 1.50
Tests 1.00 Close-Up 2.00 TOTAL MANHOURS 8.00 ELAPSED TIME (HOURS) 4.50 NOTE: For an explanation of the manhours and elapsed time, refer to the Gantt Chart given in Appendix 02 - Gantt Chart . Task 246108-832-802-001: Inspection - ADDITIONAL WORK Get Access 2.00 On Aircraft Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on Wing Rear Spar (RH side). 1.50 Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on Wing Rear Spar (LH side). 1.50
Tests 1.00 Close-Up 2.00 TOTAL MANHOURS 8.00 ELAPSED TIME (HOURS) 4.50 NOTE: For an explanation of the manhours and elapsed time, refer to the Gantt Chart given in Appendix 04 - Gantt Chart (Additional Work)

. H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-21-00 06-41-57 20-21-12 20-28-11 24-00-00 24-50-20 29-10-00 52-10-00 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-51-20 20-53-21 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-40-20 51-40-30 K. PUBLICATION AFFECTED None
DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 7 5

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# @A300-600 SERVICE BULLETIN
L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 8 5

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# @A300-600 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses AIRBUS Material, Logistics and Suppliers do not stock standard hardware as competitive multiple suppliers ensure access to minimum prices. AIRBUS recommends Customers with aircraft shown in the effectivity of this Service Bulletin to send a purchase order to B/E Aerospace. The address is: Component COMPA01 B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com Internet: http://www.beconsumables.com or, alternatively any other source on the open market. (2) Price and Availability No AIRBUS Kit will be provided. Operator supplied standard hardware parts required to accomplish this Service Bulletin are to be supplied from the Operator’s stock. B. INDUSTRY SUPPORT INFORMATION AIRBUS will not provide industry support for accomplishment of this Service Bulletin. C. LIST OF COMPONENTS No Kit

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 9 5

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# @A300-600 SERVICE BULLETIN
D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Fuel Tank Sealant Polysulfid 09-002 As required (2) Components Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 2 NSA5050-3 4 NUT (1) 3 E0088-10-80NN 2 LEAD (1) NOTE: 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, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. NOTE (1): The quantity depends on the result of the inspection. (3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 10 5

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# @A300-600 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 246108-832-801-001 - Inspection WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. WARNING: MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 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. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data Zone 575 675 Access Panel 575CB 575DB 575FB 675CB 675DB 675FB Manpower TOTAL MANHOURS 8.00 ELAPSED TIME (HOURS) 4.50 A. GENERAL (1) Subtask 246108-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 11 5

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# @A300-600 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 20-21-12, Page Block 001 20-28-11, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-51-20 Structural Repair Manual (SRM) 51-40-20 51-40-30 (a) For the specification of materials (Mat. No.) given in this Service Bulletin refer to Consumable Materials List (CML). (b) For the identification of zones, (Refer to AMM 06-21-00, Page Block 001). (c) For the removal and installation of fasteners, (Refer to SRM 51-40-20). (d) For alternative and substitute fasteners, (Refer to SRM 51-40-30). (e) Do the electrical bonding, (Refer to AMM 20-28-11, Page Block 001 and to ESPM 20-51-20). (f) To torque tighten the standard thread fasteners, (Refer to AMM 20-21-12, Page Block 001). (2) Subtask 246108-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 246108-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301 52-10-00, Page Block 001 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) Put access platform(s) in position. (c) Open the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001).

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 12 5

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# @A300-600 SERVICE BULLETIN (2) Subtask 246108-865-001-001 - C/B Opening Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 24-50-20, Page Block 001 (a) If the wire(s) must be repaired, open, safety tag these circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 120VU ELEC/PUMPS/WARN 4GE (1) 120VU ENG 1,2/FIRE VALVES 103GK (1) NOTE (1): Refer to AMM 24-50-20, Page Block 001 for the C/B location. (3) Subtask 246108-010-001-001 - Open for Access on RH Side Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 (a) Open the access panels 675DB and/or 675CB and/or 675FB (Refer to AMM 06-41-57, Page Block 001). (4) Subtask 246108-010-002-001 - Open for Access on LH Side Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 (a) Open the access panels 575DB and/or 575CB and/or 575FB (Refer to AMM 06-41-57, Page Block 001). C. PROCEDURE (1) Subtask 246108-832-001-001 - Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on Wing Rear Spar (RH side). Work Zones and Access Panels Zone Access/Work location 675 Access Panel 675DB, Panel 675CB, Panel 675FB Work location from Rib 7A to Rib 8

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 13 5

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# @A300-600 SERVICE BULLETIN
Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills ELECTRICAL Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 NSA5050-3 2 NUT (1) 3 E0088-10-80NN 1 LEAD (1) NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. NOTE (1): The quantity depends on the result of the inspection. Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Fuel Tank Sealant Polysulfid 09-002 As required
References Elec. Std. Practices Manual (ESPM) 20-53-21 Fig. A-FBAAA Area to be inspected Sheet 01 Fig. A-FFAAA Flow Chart Sheet 01 (a) For the inspection area, Refer to Fig. A-FBAAA (b) Do a detailed inspection of the length of the bonding lead, Refer to Fig. A-FFAAA 1 Depending on the inspection result :
a Remove : 1 lead-Bonding Item (3) attached with : 2 Bolt Item (1) Retain 2 Nut Item (2) Discard

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 14 5

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# @A300-600 SERVICE BULLETIN
b Install : 1 Lead-Bonding E0088-10-80NN Item 3 with : 2 Bolt Item (1) Retained at removal and with : 2 Nut NSA5050-3 Item 2 NOTE: Do the alignment of the two clamps, and seal them with: Fuel Tank Sealant Polysulfid 09-002 As required (c) Do a detailed inspection of the wires, Refer to Fig. A-FFAAA

. 1 If there is no contact and no chafing, no further action is required. 2 If there is chafing, repair the wire(s) (Refer to ESPM 20-53-21). (d) For the inspection report, Refer to Appendix 01 - Inspection Report . (2) Subtask 246108-832-002-001 - Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on Wing Rear Spar (LH side). Work Zones and Access Panels Zone Access/Work location 575 Access Panel 575DB, Panel 575CB, Panel 575FB Work location from Rib 7A to Rib 8 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills ELECTRICAL Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 NSA5050-3 2 NUT (1) 3 E0088-10-80NN 1 LEAD (1) NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. NOTE (1): The quantity depends on the result of the inspection. DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 15 5

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# @A300-600 SERVICE BULLETIN
Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Fuel Tank Sealant Polysulfid 09-002 As required
References Elec. Std. Practices Manual (ESPM) 20-53-21 Fig. A-FBAAA Area to be inspected Sheet 01 Fig. A-FFAAA Flow Chart Sheet 01 (a) For the inspection area, Refer to Fig. A-FBAAA (b) Do a detailed inspection of the length of the bonding lead, Refer to Fig. A-FFAAA 1 Depending on the inspection result :
a Remove : 1 lead-Bonding Item (3) attached with : 2 Bolt Item (1) Retain 2 Nut Item (2) Discard b Install : 1 Lead-Bonding E0088-10-80NN Item 3 with : 2 Bolt Item (1) Retained at removal and with : 2 Nut NSA5050-3 Item 2 NOTE: Do the alignment of the two clamps, and seal them with: Fuel Tank Sealant Polysulfid 09-002 As required (c) Do a detailed inspection of the wires, Refer to Fig. A-FFAAA

. 1 If there is no contact and no chafing, no further action is required. 2 If there is chafing, repair the wire(s) (Refer to ESPM 20-53-21).

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 16 5

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# @A300-600 SERVICE BULLETIN (d) For the inspection report, Refer to Appendix 01 - Inspection Report . D. TEST (1) Subtask 246108-865-002-001 - C/B Closing Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 24-50-20, Page Block 001 (a) If a wire has been repaired, remove the safety clips and tags and close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 120VU ELEC/PUMPS/WARN 4GE (1) 120VU ENG 1,2/FIRE VALVES 103GK (1) NOTE (1): Refer to AMM 24-50-20, Page Block 001 for the C/B location. (2) Subtask 246108-700-001-001 - Testing Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 20-28-11, Page Block 001 29-10-00, Page Block 501 (a) If a bonding lead has been replaced, do the check of the electrical bonding (Refer to AMM 20-28-11, Page Block 001). NOTE: For the maximum Permissible Resistance Values, (Refer to the Table AMM 20-28-11, Page Block 001). (b) If a wire has been repaired, do a functional test of fire valves (Refer to AMM 29-10-00, Page Block 501). E. CLOSE-UP (1) Subtask 246108-410-001-001 - Close the access panels on RH Side Work Zones and Access Panels Zone Access/Work location 675 Manpower Resources Skills NON SPECIFIC

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 17 5

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# @A300-600 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the access panels 675DB and/or 675CB and/or 675FB (Refer to AMM 06-41-57, Page Block 001). (2) Subtask 246108-410-002-001 - Close the access panels on LH Side Work Zones and Access Panels Zone Access/Work location 575 Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the access panels 575DB and/or 575CB and/or 575FB (Refer to AMM 06-41-57, Page Block 001). (3) Subtask 246108-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 52-10-00, Page Block 001 (a) Close the passenger/crew door 831 (Refer to AMM 52-10-00, Page Block 001). (b) Remove the access platform(s). (c) Restore the system and the aircraft to the normal operating condition.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 18 5

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# @A300-600 SERVICE BULLETIN Task 246108-832-802-001 - Inspection - ADDITIONAL WORK WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. WARNING: MAKE SURE THAT THE SAFETY DEVICES AND THE WARNING NOTICES ARE IN POSITION BEFORE YOU START A TASK ON OR NEAR: - THE FLIGHT CONTROLS - THE FLIGHT CONTROL SURFACES - THE LANDING GEAR AND THE RELATED DOORS - COMPONENTS THAT MOVE. MOVEMENT OF COMPONENTS CAN KILL OR INJURE PERSONS. 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. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data Zone 575 675 Access Panel 575CB 575DB 575FB 675CB 675DB 675FB Manpower TOTAL MANHOURS 8.00 ELAPSED TIME (HOURS) 4.50 A. GENERAL (1) Subtask 246108-910-002-001 - Standard Practices Manpower Resources Skills NON SPECIFIC

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 19 5

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# @A300-600 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 06-21-00, Page Block 001 20-21-12, Page Block 001 20-28-11, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-51-20 Structural Repair Manual (SRM) 51-40-20 51-40-30 (a) For the specification of materials (Mat. No.) given in this Service Bulletin refer to Consumable Materials List (CML). (b) For the identification of zones, refer to AMM 06-21-00, Page Block 001. (c) Remove and install fasteners in accordance with SRM 51-40-20. (d) Obtain alternative and substitute fasteners data, in accordance with SRM 51-40-30. (e) For the electrical bonding, refer to ESPM 20-51-20 and AMM 20-28-11, Page Block 001. (f) To torque tighten the standard thread fasteners, refer to AMM 20-21-12, Page Block 001. (2) Subtask 246108-839-002-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 246108-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301 52-10-00, Page Block 001 (a) Make sure that the aircraft is electrically grounded, refer to AMM 24-00-00, Page Block 301. (b) Put access platform(s) in position. (c) Open the passenger/crew door 831, refer to AMM 52-10-00, Page Block 001.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 20 5

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# @A300-600 SERVICE BULLETIN (2) Subtask 246108-865-003-001 - C/B Opening Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 24-50-20, Page Block 001 (a) If the wire(s) must be repaired, open, safety/lock and tag these circuit breakers: PANEL DESIGNATION FIN LOCATION SEE NOTES 120VU ELEC/PUMPS/WARN 4GE (1) 120VU ENG 1,2/FIRE VALVES 103GK (1) NOTE (1): Refer to AMM 24-50-20, Page Block 001 for the C/B location. (3) Subtask 246108-010-003-001 - Open for Access on RH Side Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 (a) Open the access panels 675DB and/or 675CB and/or 675FB, refer to AMM 06-41-57, Page Block 001. (4) Subtask 246108-010-004-001 - Open for Access on LH Side Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 (a) Open the access panels 575DB and/or 575CB and/or 575FB, refer to AMM 06-41-57, Page Block 001. C. PROCEDURE (1) Subtask 246108-832-003-001 - Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on Wing Rear Spar (RH side). Work Zones and Access Panels Zone Access/Work location 675 Access Panel 675CB, Panel 675DB, Panel 675FB Work location from Rib 7A to Rib 8

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 21 5

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# @A300-600 SERVICE BULLETIN
Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills ELECTRICAL Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 NSA5050-3 2 NUT (1) 3 E0088-10-80NN 1 LEAD (1) NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. NOTE (1): The quantity depends on the result of the inspection. Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Fuel Tank Sealant Polysulfid 09-002 As required
References Elec. Std. Practices Manual (ESPM) 20-53-21 Fig. A-FBCAA Area to be inspected (Additional Work) Sheet 01 Fig. A-FFBAA Flow Chart (Additional Work) Sheet 01 (a) For the inspection area, refer to Fig. A-FBCAA (b) Do a detailed inspection of the length of the bonding lead, refer to Fig. A-FFBAA 1 Depending on the inspection result:
a Remove: 1 lead-Bonding Item (3) attached with: 2 Bolt Item (1) Retain 2 Nut Item (2) Discard

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 22 5

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# @A300-600 SERVICE BULLETIN
b Install: 1 Lead-Bonding E0088-10-80NN Item 3 with: 2 Bolt Item (1) Retained at removal and with: 2 Nut NSA5050-3 Item 2 NOTE: Do the alignment of the two clamps, and seal them with: Fuel Tank Sealant Polysulfid 09-002 As required (c) Do a detailed inspection of the wires, refer to Fig. A-FFBAA

. 1 If there is no contact and no chafing, no further action is required. 2 If there is chafing, repair the wire(s), refer to ESPM 20-53-21. (d) For the inspection report, refer to Appendix 03 - Inspection Report (Additional Work)

. (2) Subtask 246108-832-004-001 - Do a Detailed Inspection of the FSOV Bonding Lead and of the Wires Located on Wing Rear Spar (LH side). Work Zones and Access Panels Zone Access/Work location 575 Access Panel 575DB, Panel 575CB, Panel 575FB Work location from Rib 7A to Rib 8 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills ELECTRICAL Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 NSA5050-3 2 NUT (1) 3 E0088-10-80NN 1 LEAD (1) NOTE: The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel.
DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 23 5

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# @A300-600 SERVICE BULLETIN
NOTE (1): The quantity depends on the result of the inspection. Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Fuel Tank Sealant Polysulfid 09-002 As required
References Elec. Std. Practices Manual (ESPM) 20-53-21 Fig. A-FBCAA Area to be inspected (Additional Work) Sheet 01 Fig. A-FFBAA Flow Chart (Additional Work) Sheet 01 (a) For the inspection area, refer to Fig. A-FBCAA (b) Do a detailed inspection of the length of the bonding lead, refer to Fig. A-FFBAA 1 Depending on the inspection result:
a Remove: 1 lead-Bonding Item (3) attached with: 2 Bolt Item (1) Retain 2 Nut Item (2) Discard b Install: 1 Lead-Bonding E0088-10-80NN Item 3 with: 2 Bolt Item (1) Retained at removal and with: 2 Nut NSA5050-3 Item 2 NOTE: Do the alignment of the two clamps, and seal them with: Fuel Tank Sealant Polysulfid 09-002 As required (c) Do a detailed inspection of the wires, refer to Fig. A-FFBAA

. 1 If there is no contact and no chafing, no further action is required.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 24 5

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# @A300-600 SERVICE BULLETIN

2 If there is chafing, repair the wire(s), refer to ESPM 20-53-21. (d) For the inspection report, refer to Appendix 03 - Inspection Report (Additional Work)

. D. TEST (1) Subtask 246108-865-004-001 - C/B Closing Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 24-50-20, Page Block 001 (a) If a wire has been repaired, remove the safety clips and/or tags and close/unlock the following circuit breakers: PANEL DESIGNATION FIN LOCATION SEE NOTES 120VU ELEC/PUMPS/WARN 4GE (1) 120VU ENG 1,2/FIRE VALVES 103GK (1) NOTE (1): Refer to AMM 24-50-20, Page Block 001 for the C/B location. (2) Subtask 246108-700-002-001 - Testing Manpower Resources Skills ELECTRICAL References Aircraft Maintenance Manual (AMM) 20-28-11, Page Block 001 29-10-00, Page Block 501 (a) If a bonding lead has been replaced, do the check of the electrical bonding, refer to AMM 20-28-11, Page Block 001. NOTE: For the maximum Permissible Resistance Values, refer to the Table AMM 20-28-11, Page Block 001. (b) If a wire has been repaired, do a functional test of fire valves, refer to AMM 29-10-00, Page Block 501. E. CLOSE-UP (1) Subtask 246108-410-003-001 - Close the access panels on RH Side Work Zones and Access Panels Zone Access/Work location 675

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 25 5

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# @A300-600 SERVICE BULLETIN
Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the access panels 675DB and/or 675CB and/or 675FB, refer to AMM 06-41-57, Page Block 001. (2) Subtask 246108-410-004-001 - Close the access panels on LH Side Work Zones and Access Panels Zone Access/Work location 575 Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-57, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the access panels 575DB and/or 575CB and/or 575FB, refer to AMM 06-41-57, Page Block 001. (3) Subtask 246108-942-003-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 52-10-00, Page Block 001 (a) Close the passenger/crew door 831, refer to AMM 52-10-00, Page Block 001. (b) Remove the access platform(s). (c) Restore the systems and the aircraft to normal operating condition.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 26 5

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# @A300-600 SERVICE BULLETIN

**CONF ALL Z575 (Z675)

LH SIDE SHOWN RH SIDE SYMMETRICAL RIB8

RIB5

WIRES TO BE RIB7A

AREA TO BE INSPECTED **NOTE:** BONDING LEAD TO BE

ELECTRICAL BONDING REAR SPAR

INSPECTED (1)

(2) 2 (3) 3 

### A

**B**



## A

**B C**  **C**

BONDING LEAD TO BE INSPECTED (2) 2 (1)

INSPECTED

D_SB_246108_5_BAAA_01_06 Figure A-FBAAA - Sheet 01 Area to be inspected
DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 27 5

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# @A300-600 SERVICE BULLETIN

**CONF ALL

QUESTION ACTION FINDING AT THE THRESHOLD GIVEN IN THE PLANNING INFORMATION PARAGRAPH E.(2).

BONDING LEAD (RH AND LH) IS NO YES DO A DETAILED INSPECTION OF THE LENGTH OF THE BONDING LEAD (RH AND LH) DO A DETAILED INSPECTION OF THE FSOV BONDING LEAD (RH AND LH) AND OF THE WIRES (RH AND LH) LOCATED ON WING REAR SPAR

REPLACE THE BONDING LEAD (RH AND LH)

CONTACT/CHAFING NO YES
REPAIR THE WIRE(S) (RH AND LH) LENGTH OF THE

80 mm (3.15 in)

WITH THE LENGTH = 80 mm (3.15 in)

DO A DETAILED INSPECTION OF THE WIRES (RH AND LH)

SEND TO AIRBUS THE INSPECTION

REPORT REFER TO APPENDIX 1

NO FURTHER ACTION REFER TO ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH INSPECTION (SUBTASK 246108−832−001−001 AND 246108−832−002−001)

PARAGRAPH INSPECTION (SUBTASK 246108−832−001−001 AND 246108−832−002−001) REFER TO ACCOMPLISHMENT INSTRUCTIONS

D_SB_246108_5_FAAA_01_01 Figure A-FFAAA - Sheet 01 Flow Chart
DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 28 5

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# @A300-600 SERVICE BULLETIN

**CONF ALL Z575 (Z675)

LH SIDE SHOWN RH SIDE SYMMETRICAL RIB8

RIB5

WIRES TO BE RIB7A

AREA TO BE INSPECTED **NOTE:** BONDING LEAD TO BE

ELECTRICAL BONDING REAR SPAR

INSPECTED (1)

(2) 2 (3) 3 

### A

**B**



## A

**B C**  **C**

BONDING LEAD TO BE INSPECTED (2) 2 (1)

INSPECTED

D_SB_246108_5_BCAA_01_01 Figure A-FBCAA - Sheet 01 Area to be inspected (Additional Work)
DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 29 5

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# @A300-600 SERVICE BULLETIN

**CONF ALL

QUESTION ACTION FINDING AT THE THRESHOLD GIVEN IN THE PLANNING INFORMATION PARAGRAPH E.(2).

BONDING LEAD (RH AND LH) IS NO YES DO A DETAILED INSPECTION OF THE LENGTH OF THE BONDING LEAD (RH AND LH) DO A DETAILED INSPECTION OF THE FSOV BONDING LEAD (RH AND LH) AND OF THE WIRES (RH AND LH) LOCATED ON WING REAR SPAR

REPLACE THE BONDING LEAD (RH AND LH)

CONTACT/CHAFING NO YES
REPAIR THE WIRE(S) (RH AND LH) LENGTH OF THE

80 mm (3.15 in)

WITH THE LENGTH = 80 mm (3.15 in)

DO A DETAILED INSPECTION OF THE WIRES (RH AND LH)

SEND TO AIRBUS THE INSPECTION

REPORT REFER TO APPENDIX 3

NO FURTHER ACTION REFER TO ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH INSPECTION (SUBTASK 246108−832−003−001 AND 246108−832−004−001)

PARAGRAPH INSPECTION (SUBTASK 246108−832−003−001 AND 246108−832−004−001) REFER TO ACCOMPLISHMENT INSTRUCTIONS

D_SB_246108_5_FBAA_01_01 Figure A-FFBAA - Sheet 01 Flow Chart (Additional Work)
DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 30 5

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# @A300-600 SERVICE BULLETIN Appendix 01 - Inspection Report **CONF ALL The results of the inspection, including no findings, replacement or action to be done, must be forwarded to AIRBUS department SEEA6, on the attached inspection report sheet.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 1 5

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# @A300-600 SERVICE BULLETIN Appendix 01 - Inspection Report

**CONF ALL **INSPECTION REPORT** SERVICE BULLETIN No. : A/C MSN : FLIGHT CYCLES : FLIGHT HOURS : A300−24−6108

DATE OF INSPECTION : RETURN TO : AIRBUS CUSTOMER SERVICES ENGINEERING − SEEA6 ELECTRICAL INSTALLATION & ELECTRICAL

INSPECTION METHOD : DETAILED INSPECTION STANDARD ITEMS 1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE FAX +33 (0)5 61 93 44 25

LENGTH 80 mm (3.15 in) BONDING LEAD

CONTACT/CHAFING YES NO

BONDING LEAD
WIRE(S) REPAIRED REPLACED WIRE(S)

YES NO YES NO N/A

YES NO N/A N/A

N/A **LH SIDE**

LENGTH 80 mm (3.15 in) BONDING LEAD

CONTACT/CHAFING YES NO

BONDING LEAD
WIRE(S) REPAIRED REPLACED WIRE(S)

YES NO YES NO N/A

YES NO N/A N/A

N/A **RH SIDE**

D_SB_246108_5_RAAA_01_00 Figure A-FRAAA - Sheet 01 Inspection Report
DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 2 5

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# @A300-600 SERVICE BULLETIN Appendix 02 - Gantt Chart **CONF ALL (1) For detail concerning the elapsed time assumption of the modification, refer to the Gantt chart shown in the next page :

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 1 5

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# @A300-600 SERVICE BULLETIN Appendix 02 - Gantt Chart

**CONF ALL
**ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A300−24−6108**

ELAPSED TIME (HOURS)

**NOTE:** THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. MH ET PER

MH: ET: PER: MANHOURS ELAPSED TIME NUMBER OF PERSONS

TOTAL MANHOURS (MH) ELAPSED TIME (ET) 8.00 4.50 STEPS

0 1 2.00. 1.00 2 GET ACCESS

1.50 1.50 1

CLOSE−UP 2.00 1.00 2 OF THE SHUT−OFF VALVE DO A DETAILED INSPECTION BONDING LEAD AND WIRE

TEST 1.00 1.00 1

2345 (LH SIDE)

1.50 1.50 1 OF THE SHUT−OFF VALVE DO A DETAILED INSPECTION BONDING LEAD AND WIRE (RH SIDE)

D_SB_246108_5_ABAA_01_02 Figure A-FABAA - Sheet 01 Gantt Chart
DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 2 5

Printed in FRANCE ©AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN Appendix 03 - Inspection Report (Additional Work) **CONF ALL (1) The results of the inspection, including no findings, replacement or action to be done, must be forwarded to AIRBUS department SEEA6, on the attached inspection report sheet.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 1 5

Printed in FRANCE ©AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN Appendix 03 - Inspection Report (Additional Work)

**CONF ALL **INSPECTION REPORT** SERVICE BULLETIN No. : A/C MSN : FLIGHT CYCLES : FLIGHT HOURS : A300−24−6108

DATE OF INSPECTION : RETURN TO : AIRBUS CUSTOMER SERVICES ENGINEERING − SEEA6 ELECTRICAL INSTALLATION & ELECTRICAL

INSPECTION METHOD : DETAILED INSPECTION STANDARD ITEMS 1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE FAX +33 (0)5 61 93 44 25

LENGTH 80 mm (3.15 in) BONDING LEAD

CONTACT/CHAFING YES NO

BONDING LEAD
WIRE(S) REPAIRED REPLACED WIRE(S)

YES NO YES NO N/A

YES NO N/A N/A

N/A **LH SIDE**

LENGTH 80 mm (3.15 in) BONDING LEAD

CONTACT/CHAFING YES NO

BONDING LEAD
WIRE(S) REPAIRED REPLACED WIRE(S)

YES NO YES NO N/A

YES NO N/A N/A

N/A **RH SIDE**

D_SB_246108_5_RBAA_01_00 Figure A-FRBAA - Sheet 01 Inspection Report (Additional Work)
DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 2 5

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# @A300-600 SERVICE BULLETIN Appendix 04 - Gantt Chart (Additional Work) **CONF ALL (1) The following Gantt Chart is only a proposal. Operators may determine that another way to do the work is more suitable for them.

DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 1 5

Printed in FRANCE ©AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN Appendix 04 - Gantt Chart (Additional Work)

**CONF ALL

**ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A300−24−6108**

MH ET/S

TOTAL MANHOURS SB ELAPSED TIME 8.00 4.50 STEPS

2.00 1.00

5 0 1.50 1.50

1.50 1.50

2.00 1.00

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. 01
02 **NOTE:**

PER

2

1

1

2 1.00 1.00 1

: : SB ELAPSED TIME (HOURS) 1 2 3 4

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS ARE NOT REFLECTED IN THIS GANTT CHART. GET ACCESS

CLOSE−UP OF THE SHUT−OFF VALVE DO A DETAILED INSPECTION BONDING LEAD AND WIRE

TEST (LH SIDE)

OF THE SHUT−OFF VALVE DO A DETAILED INSPECTION BONDING LEAD AND WIRE (RH SIDE)

D_SB_246108_5_ADAA_01_00 Figure A-FADAA - Sheet 01 Gantt Chart (Additional Work)
DATE: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 2 5

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# @A300-600 SERVICE BULLETIN REPORTING SHEET 

### TITLE: ELECTRICAL POWER -INSPECTION OF SHUT-OFF VALVE BONDING LEAD MODIFICATION No.: None 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: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 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 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - 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: Jul 09/10 SERVICE BULLETIN No.: A300-24-6108 REVISION No.: 01 - Mar 26/13 Page: 1 5

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