@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

MANDATORY MANDATORY MANDATORY

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

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Configuration definition Minor editorial or document structure change N

CONF 001 Minor editorial or document structure change N

Material Effectivity Minor editorial or document structure change N

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

APPROVAL Minor editorial or document structure change N

Minor editorial or document structure change N

MANPOWER Minor editorial or document structure change N

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

REFERENCES Minor editorial or document structure change N

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

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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

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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

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SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is not approved for modification of the aircraft.

MANDATORY MANDATORY MANDATORY

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

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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

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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

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SERVICE BULLETIN

SUMMARY

**CONF ALL

43QA−A 49QA−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

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

MANDATORY MANDATORY MANDATORY

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

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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

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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

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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 Consequences

Should 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

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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

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M. SPARES

None

DATE: Aug 13/09 SERVICE BULLETIN No.: A300-24-6102

REVISION No.: 01 - Sep 24/10 Page: 6

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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

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(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

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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

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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

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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

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(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

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.

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

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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

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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

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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

FWD A

B

B

B

REMOVAL

PULL

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

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**CONF ALL

43QA−A 49QA−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

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**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

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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

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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

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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:

01 2

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

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**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

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**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

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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

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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

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