@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.

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 28

TITLE: FUEL SYSTEM - INTRODUCE GROUND FAULT INTERRUPTER (GFI)

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 13382H5685

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

The European Aviation Safety Agency (EASA) has requested that Ground Fault Interrupters (GFI) are

installed into the electrical supply circuits of A300-600/600R and A310-200/300 fuel pumps where inlets

become uncovered during normal operation.

This is in response to SFAR88 - Fuel Tank Safety.

This Service Bulletin introduces Ground Fault Interrupters (GFI) and related bases into the electrical

supply circuits of the A300-600/600R aircraft, inner center and trim (where fitted) tank pumps. These

GFIs have the same ’footprint’ as the existing relay/micro-contactors and physically replace them on the

electrical panel.

The new GFI sockets are fool-proofed to prevent incorrectly installing normal relay/micro-contactors.

These GFIs will replace the existing 3-phase relay/micro-contactors. The function of the GFI is to

electrically isolate the pump if a ground fault condition occurs downstream of the GFI. The GFI gives

additional earth leakage protection to the downstream circuit.

Accomplishment of this Service Bulletin will not change the characteristics of the aircraft.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 1

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

SUMMARY

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD NO 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

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 286104A01R00 1 13,310.00 GFI, contacts

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 286104A02R00 1 17,680.00 GFI, contacts

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 286104A02R00 1 17,680.00 GFI, contacts

**CONF 004

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 286104A02R00 1 17,680.00 GFI, contacts

EFFECTIVITY

**CONF ALL

This Service Bulletin is applicable to this (these) operator(s) :

34Z 77T 83V AAL ABD AHK AIB AMU BCS CES F2I FDX G8E

GBG IRA IRM JAL KAC KAL MNB MON MSR MXU OHY QTR RUN

SUD TAR THA TMA UPS URS UZB

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 2

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

SUMMARY

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

**CONF 001

Task 286104-831-895-001: MODIFICATION

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

**CONF 002

Task 286104-831-895-001: MODIFICATION

TOTAL MANHOURS 5.50

ELAPSED TIME (HOURS) 5.50

**CONF 003

Task 286104-831-895-001: MODIFICATION

TOTAL MANHOURS 5.50

ELAPSED TIME (HOURS) 5.50

**CONF 004

Task 286104-831-895-001: MODIFICATION

TOTAL MANHOURS 5.50

ELAPSED TIME (HOURS) 5.50

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 3

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

SUMMARY

APPENDICES

**CONF ALL

None

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 4

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

SUMMARY

**CONF ALL

AND THE WIRING IN 107VU

MODIFICATION OF THE EQUIPMENT

FR20

FR1 Z120

D_SB_286104_5_SAAA_01_01

Figure A-FSAAA - Sheet 01

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 5

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 6

7

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: 28

TITLE: FUEL SYSTEM - INTRODUCE GROUND FAULT INTERRUPTER (GFI)

MODIFICATION No.: 13382H5685

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 0317 0321 0336 0344 0348 0351 0358 0361 0365 0380

0388 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 0602-0615 0617-0618 0621 0623

0625-0633 0635 0637 0639 0641 0643 0645 0657 0659 0662 0664 0666 0668 0670

0673 0675 0677 0679 0681 0683 0685 0688 0692 0694 0696 0699 0701 0703 0705

0707 0709 0711 0713 0715 0717 0719 0721-0750 0752-0764 0766-0775 0777-0794

0797 0799-0841 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.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 1

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

OPERATOR MSN

34Z 0685

77T 0838

83V 0423 0459 0460 0463 0466 0470 0474 0510 0511 0512 0615 0639

0675

AAL 0517 0612

ABD 0529 0557

AHK 0855 0856 0857 0858 0859 0860 0870 0871

AIB 0507 0508 0515

AMU 0677

BCS 0621 0637 0641 0670 0679 0711 0724 0729 0740

CES 0521 0525 0532 0707 0725 0732 0741 0746 0754 0763

F2I 0284 0294 0301 0307 0312 0317 0321 0336 0348 0351 0461 0518

0606 0610 0645 0753 0770

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 0469 0506 0509 0513 0514 0516

GBG 0626 0643

IRA 0632 0696 0723 0727

IRM 0380 0401 0405 0408 0411 0414 0546 0553 0608 0618 0623 0701

0750 0762 0773

JAL 0602 0617 0683 0703 0730 0737 0783

KAC 0344 0673 0694 0699 0719 0721

KAL 0582 0609 0627 0631 0662 0692 0731

MNB 0734 0739 0755 0756 0758

MON 0540 0556 0604 0605

MSR 0561 0607

MXU 0767 0788 0797 0836 0837

OHY 0584 0603 0744 0747 0749 0764

QTR 0554 0560 0614

RUN 0743

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

UZB 0717 0722

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 2

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0284 0294 0301 0307 0312 0317 0321 0336 0344 0348 0351

0358 0361 0365 0388 0417

001

0380 0401 0405 0408 0411 0414 002

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 0529 0530 0532 0536

0540 0543 0554 0555 0556 0558 0559 0560 0563 0566 0569

0572 0575 0577 0579 0581 0582 0584 0602 0603 0604 0605

0606 0608 0609 0610 0611 0612 0613 0614 0615 0617 0621

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

004

0525 0557 0561 0607 003 004

0546 0553 0618 0623 003

(5) Configuration definition

**CONF 001

Configuration 001 is valid on aircraft on which:

- Mod. No. 06213S7013 is not embodied.

- Mod. No. 04801S5725 is not embodied.

- Mod. No. 10778D20832 (or Service Bulletin No. A300-31-6051) is not embodied.

**CONF 002

Configuration 002 is valid on aircraft on which:

- Mod. No. 06213S7013 is not embodied.

- Mod. No. 04801S5725 is embodied.

- Mod. No. 10778D20832 (or Service Bulletin No. A300-31-6051) is not embodied.

**CONF 003

Configuration 003 is valid on aircraft on which:

- Mod. No. 06213S7013 is embodied.

- Mod. No. 04801S5725 is embodied.

- Mod. No. 10778D20832 (or Service Bulletin No. A300-31-6051) is not embodied.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 3

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 004

Configuration 004 is valid on aircraft on which:

- Mod. No. 06213S7013 is embodied.

- Mod. No. 04801S5725 is embodied.

- Mod. No. 10778D20832 (or Service Bulletin No. A300-31-6051) is embodied.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Kit 286104A01R00 1

**CONF 002 thru 004

MATERIAL QTY PER A/C SEE NOTES

Kit 286104A02R00 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

The European Aviation Safety Agency (EASA) has requested that Ground Fault

Interrupters (GFI) are installed into the electrical supply circuits of A300-600/600R and

A310-200/300 fuel pumps where inlets become uncovered during normal operation.

This is in response to SFAR88 - Fuel Tank Safety.

(2) Objective/Action

This Service Bulletin introduces Ground Fault Interrupters (GFI) and related bases into

the electrical supply circuits of the A300-600/600R aircraft, inner center and trim (where

fitted) tank pumps. These GFIs have the same ’footprint’ as the existing relay/microcontactors and physically replace them on the electrical panel.

The new GFI sockets are fool-proofed to prevent incorrectly installing normal relay/microcontactors.

(3) Advantages

These GFIs will replace the existing 3-phase relay/micro-contactors. The function of the

GFI is to electrically isolate the pump if a ground fault condition occurs downstream of

the GFI. The GFI gives additional earth leakage protection to the downstream circuit.

Accomplishment of this Service Bulletin will not change the characteristics of the aircraft.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 4

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 286104-831-895-001: MODIFICATION

(1) Modification of the Equipment and the Wiring in the LH Relay Box 107VU.

**CONF 002

Task 286104-831-895-001: MODIFICATION

(1) Modification of the Equipment and the Wiring in the LH Relay Box 107VU.

**CONF 003

Task 286104-831-895-001: MODIFICATION

(1) Modification of the Equipment and the Wiring in the LH Relay Box 107VU.

**CONF 004

Task 286104-831-895-001: MODIFICATION

(1) Modification of the Equipment and the Wiring in the LH Relay Box 107VU.

**CONF ALL

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. The accomplishment timescale, which has not yet been

defined, will be given in the AD.

F. APPROVAL

The technical content of this document is approved under the authority of Design

Organisation Approval No. EASA.21J.031.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 5

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

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.

**CONF 001

Task 286104-831-895-001: MODIFICATION

Get Access 0.50

On Aircraft

Modification of the Equipment and the Wiring in the LH

Relay Box 107VU.

3.50

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

**CONF 002

Task 286104-831-895-001: MODIFICATION

Get Access 0.50

On Aircraft

Modification of the Equipment and the Wiring in the LH

Relay Box 107VU.

4.00

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 5.50

ELAPSED TIME (HOURS) 5.50

**CONF 003

Task 286104-831-895-001: MODIFICATION

Get Access 0.50

On Aircraft

Modification of the Equipment and the Wiring in the LH

Relay Box 107VU.

4.00

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 5.50

ELAPSED TIME (HOURS) 5.50

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 6

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 004

Task 286104-831-895-001: MODIFICATION

Get Access 0.50

On Aircraft

Modification of the Equipment and the Wiring in the LH

Relay Box 107VU.

4.00

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 5.50

ELAPSED TIME (HOURS) 5.50

**CONF ALL

H. WEIGHT AND BALANCE

The weight and balance estimates given in this Service Bulletin are based on the

Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of

MEW and operator’s items, refer to Weight and Balance Manual (WBM) Chapter 1-00-07.

**CONF 001

Manufacturers Empty Weight -0.354 KG (-0.7804 LB)

Effect on Balance -3.399 KGM (-24.585 LB.FT )

**CONF 002 thru 004

Manufacturers Empty Weight -0.472 KG (-1.0405 LB)

Effect on Balance -4.533 KGM (-32.787 LB.FT )

**CONF ALL

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-00 06-41-52

12-11-28 20-21-12 24-00-00

24-50-20 24-50-40 28-21-12

28-21-36 52-30-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-33-00 20-46-50 20-52-21

20-55-00

Service Bulletin (SB) A300-31-6051

Standards Manual (SM)

Weight and Balance Manual (WBM) Chapter 1-00-07

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 7

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-00 06-41-52

12-11-28 20-21-12 24-00-00

24-50-10 24-50-20 24-50-40

28-21-12 28-21-36 28-27-00

52-30-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-33-00 20-46-50 20-52-21

20-55-00

Service Bulletin (SB) A300-31-6051

Standards Manual (SM)

Weight and Balance Manual (WBM) Chapter 1-00-07

**CONF 003

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-00 06-41-52

12-11-28 20-21-12 24-00-00

24-50-10 24-50-20 24-50-40

28-21-12 28-21-36 28-27-00

52-30-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-33-00 20-46-50 20-52-21

20-55-00

Service Bulletin (SB) A300-31-6051

Standards Manual (SM)

Weight and Balance Manual (WBM) Chapter 1-00-07

**CONF 004

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-00 06-41-52

12-11-28 20-21-12 24-00-00

24-50-10 24-50-20 24-50-40

28-21-12 28-21-36 28-27-00

52-30-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-33-00 20-46-50 20-52-21

20-55-00

Service Bulletin (SB) A300-31-6051

Standards Manual (SM)

Weight and Balance Manual (WBM) Chapter 1-00-07

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Schematic Manual (ASM) 28-21-00

Aircraft Wiring List (AWL)

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 8

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Aircraft Wiring Manual (AWM) 28-21-03 28-21-04 28-21-05

28-21-06 28-21-09 28-21-10

28-27-01 28-27-02 31-55-45

Illustrated Parts Catalog (IPC) 28-21-08

L. INTERCHANGEABILITY/MIXABILITY

**CONF 001

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Base NSA932844AA E0673D0S 03 YES with

Conditions

(1)

Relay NSA932843AA01 ABS1629-28A0 03 YES with

Conditions

(1)

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

NOTE (1): Not interchangeable, but one way interchangeable with the following

conditions. On embodiment existing socket and relay will be removed and

replaced with the new "error-proofed" socket and GFI. Post mod only a GFI

and associated socket can be fitted.

**CONF 002

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Base NSA932844AA E0673D0S 03 YES with

Conditions

(1)

Relay NSA932843AA01 ABS1629-28A0 03 YES with

Conditions

(1)

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

NOTE (1): Not interchangeable, but one way interchangeable with the following

conditions. On embodiment existing socket and relay will be removed and

replaced with the new "error-proofed" socket and GFI. Post mod only a GFI

and associated socket can be fitted.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 9

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 003

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Base NSA932844AA E0673D0S 03 YES with

Conditions

(1)

Relay NSA932843AA01 ABS1629-28A0 03 YES with

Conditions

(1)

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

NOTE (1): Not interchangeable, but one way interchangeable with the following

conditions. On embodiment existing socket and relay will be removed and

replaced with the new "error-proofed" socket and GFI. Post mod only a GFI

and associated socket can be fitted.

**CONF 004

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Base NSA932844AA E0673D0S 03 YES with

Conditions

(1)

Relay NSA932843AA01 ABS1629-28A0 03 YES with

Conditions

(1)

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

NOTE (1): Not interchangeable, but one way interchangeable with the following

conditions. On embodiment existing socket and relay will be removed and

replaced with the new "error-proofed" socket and GFI. Post mod only a GFI

and associated socket can be fitted.

**CONF ALL

M. SPARES

None

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 10

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 286104A01R00

Kit 286104A02R00

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:

(2) Price and Availability

Kit 286104A01R00

Cost 13,310.00 USD

Availability 120 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements. The sales terms (costs

and availability) are estimated in relation to economic conditions at the issue date of the

Service Bulletin.

Kit 286104A02R00

Cost 17,680.00 USD

Availability 120 calendar days from receipt of order

The Kit availability given above is the standard lead time from the date of your purchase

order. If you require Kits before this time, please include a retrofit planning schedule with

your order so that we can try to comply with your requirements. The sales terms (costs

and availability) are estimated in relation to economic conditions at the issue date of the

Service Bulletin.

B. INDUSTRY SUPPORT INFORMATION

This Service Bulletin is chargeable without any price reduction.

C. LIST OF COMPONENTS

Kit 286104A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

1 ABS1629-28A0 6 GFI (1) NSA932843AA01 03

2 E0673D0S 6 BASE (2) NSA932844AA 03

3 NAS1101-04-7 18 SCREW

4 ASNA2397-3L 18 WASHER

5 MS21042-04 18 NUT

EN3155-017F1216 36 CONTACT

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 11

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

EN3155-017F1620 30 CONTACT

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

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.

Kit 286104A02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

1 ABS1629-28A0 8 GFI (1) NSA932843AA01 03

2 E0673D0S 8 BASE (2) NSA932844AA 03

3 NAS1101-04-7 24 SCREW

4 ASNA2397-3L 24 WASHER

5 MS21042-04 24 NUT

EN3155-017F1216 48 CONTACT

EN3155-017F1620 38 CONTACT

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

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.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 12

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 286104-831-895-001 - MODIFICATION

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING: BEFORE POWER IS SUPPLIED TO THE AIRCRAFT MAKE SURE THAT

THE ELECTRICAL CIRCUITS UPON WHICH WORK IS IN PROGRESS ARE

ISOLATED.

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, REFER TO ESPM 20-55-00.

Task Associated Data

**CONF 001

Zone

120 121

Modified FIN

35QA 35QAA 36QA 36QAA 41QA 41QAA 42QA 42QAA 109QA 109QAA 110QA

110QAA

Manpower

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

**CONF 002

Zone

121

Modified FIN

35QA 35QAA 36QA 36QAA 41QA 41QAA 42QA 42QAA 109QA 109QAA 110QA

110QAA 9QN 9QNA 10QN 10QNA

Manpower

TOTAL MANHOURS 5.50

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 13

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ELAPSED TIME (HOURS) 5.50

**CONF 003

Zone

121

Modified FIN

35QA 35QAA 36QA 36QAA 41QA 41QAA 42QA 42QAA 109QA 109QAA 110QA

110QAA 9QN 9QNA 10QN 10QNA

Manpower

TOTAL MANHOURS 5.50

ELAPSED TIME (HOURS) 5.50

**CONF 004

Zone

121

Modified FIN

35QA 35QAA 36QA 36QAA 41QA 41QAA 42QA 42QAA 109QA 109QAA 110QA

110QAA 9QN 9QNA 10QN 10QNA

Manpower

TOTAL MANHOURS 5.50

ELAPSED TIME (HOURS) 5.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 286104-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001

06-41-00, Page Block 001

20-21-12, Page Block 001

Elec. Std. Practices Manual (ESPM) 20-33-00

20-46-50

20-52-21

(a) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

(b) For the identification of access panels (Refer to AMM 06-41-00, Page Block 001).

(c) To torque tighten the electrical component fasteners (Refer to AMM 20-21-12, Page

Block 001).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 14

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(d) Do a continuity test of the new and modified wires (Refer to ESPM 20-52-21).

(e) For the installation of the relays (Refer to ESPM 20-46-50).

(f) For the general wiring installation (Refer to ESPM 20-33-00).

(2) Subtask 286104-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 002

(1) Subtask 286104-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001

06-41-00, Page Block 001

20-21-12, Page Block 001

Elec. Std. Practices Manual (ESPM) 20-33-00

20-46-50

20-52-21

(a) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

(b) For the identification of access panels (Refer to AMM 06-41-00, Page Block 001).

(c) To torque tighten the electrical component fasteners (Refer to AMM 20-21-12, Page

Block 001).

(d) Do a continuity test of the new and modified wires (Refer to ESPM 20-52-21).

(e) For the installation of the relays (Refer to ESPM 20-46-50).

(f) For the general wiring installation (Refer to ESPM 20-33-00).

(2) Subtask 286104-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 15

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 003

(1) Subtask 286104-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001

06-41-00, Page Block 001

20-21-12, Page Block 001

Elec. Std. Practices Manual (ESPM) 20-33-00

20-46-50

20-52-21

(a) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

(b) For the identification of access panels (Refer to AMM 06-41-00, Page Block 001).

(c) To torque tighten the electrical component fasteners (Refer to AMM 20-21-12, Page

Block 001).

(d) Do a continuity test of the new and modified wires (Refer to ESPM 20-52-21).

(e) For the installation of the relays (Refer to ESPM 20-46-50).

(f) For the general wiring installation (Refer to ESPM 20-33-00).

(2) Subtask 286104-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF 004

(1) Subtask 286104-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001

06-41-00, Page Block 001

20-21-12, Page Block 001

Elec. Std. Practices Manual (ESPM) 20-33-00

20-46-50

20-52-21

(a) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 16

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(b) For the identification of access panels (Refer to AMM 06-41-00, Page Block 001).

(c) To torque tighten the electrical component fasteners (Refer to AMM 20-21-12, Page

Block 001).

(d) Do a continuity test of the new and modified wires (Refer to ESPM 20-52-21).

(e) For the installation of the relays (Refer to ESPM 20-46-50).

(f) For the general wiring installation (Refer to ESPM 20-33-00).

(2) Subtask 286104-839-401-001 - ADMINISTRATIVE

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 286104-941-001-001 - Job Set-up

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

24-00-00, Page Block 301

24-50-20, Page Block 001

24-50-40, Page Block 001

52-30-00, Page Block 001

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) Put the access platform(s) in position at the level of door 831.

(c) Open the FWD Cargo-compartment door 831 (Refer to AMM 52-30-00, Page Block

001 and AMM 06-41-52, Page Block 001).

(d) Open the door 132AZ (Refer to AMM 06-41-52, Page Block 001).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 17

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(e) Open, safety/lock and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

101VU FUEL/L INNER TK/PUMP

2/SUPPLY

1QA (1)

101VU FUEL/R INNER TK/PUMP

1/SUPPLY

2QA (1)

101VU FUEL/L INNER TK/PUMP

1/SUPPLY

7QA (1)

101VU FUEL/R INNER TK/PUMP

2/SUPPLY

8QA (1)

101VU FUEL/CTR

TK/L/PUMP/SUPPLY

99QA (1)

101VU FUEL/CTR

TK/R/PUMP/SUPPLY

100QA (1)

128VU FUEL/L INR TK/PUMP

2/WARN

11QA (1)

128VU FUEL/R INR TK/PUMP

1/WARN

12QA (1)

128VU FUEL/L INR TK/PUMP

1/WARN

17QA (1)

128VU FUEL/R INR TK/PUMP

2/WARN

18QA (1)

128VU FUEL/L INR TK/PUMP 2/CTL 59QA (1)

128VU FUEL/R INR TK/PUMP 1/CTL 60QA (1)

128VU FUEL/CTR TK/L/PUMP/CTL 63QA (1)

128VU FUEL/CTR TK/R/PUMP/CTL 64QA (1)

128VU FUEL/L INR TK/PUMP 1/CTL 69QA (1)

128VU FUEL/R INR TK/PUMP 2/CTL 70QA (1)

128VU FUEL/CTR

TK/L/PUMP/WARN

101QA (1)

128VU FUEL/CTR

TK/R/PUMP/WARN

102QA (1)

or

PANEL DESIGNATION FIN LOCATION SEE

NOTES

101VU FUEL/L INNER TK/PUMP

2/SUPPLY

1QA (1)

101VU FUEL/R INNER TK/PUMP

1/SUPPLY

2QA (1)

101VU FUEL/L INNER TK/PUMP

1/SUPPLY

7QA (1)

101VU FUEL/R INNER TK/PUMP

2/SUPPLY

8QA (1)

101VU FUEL/CTR

TK/L/PUMP/SUPPLY

99QA (1)

101VU FUEL/CTR

TK/R/PUMP/SUPPLY

100QA (1)

132VU FUEL/L INR TK/PUMP

2/WARN

11QA (1)

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 18

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE

NOTES

132VU FUEL/R INR TK/PUMP

1/WARN

12QA (1)

132VU FUEL/L INR TK/PUMP

1/WARN

17QA (1)

132VU FUEL/R INR TK/PUMP

2/WARN

18QA (1)

132VU FUEL/L INR TK/PUMP 2/CTL 59QA (1)

132VU FUEL/R INR TK/PUMP 1/CTL 60QA (1)

132VU FUEL/CTR TK/L/PUMP/CTL 63QA (1)

132VU FUEL/CTR TK/R/PUMP/CTL 64QA (1)

132VU FUEL/L INR TK/PUMP 1/CTL 69QA (1)

132VU FUEL/R INR TK/PUMP 2/CTL 70QA (1)

132VU FUEL/CTR

TK/L/PUMP/WARN

101QA (1)

132VU FUEL/CTR

TK/R/PUMP/WARN

102QA (1)

NOTE (1): For the location of the circuit breakers, refer to AMM 24-50-20,

Page Block 001 and AMM 24-50-40, Page Block 001.

**CONF 002

(1) Subtask 286104-941-001-003 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

24-00-00, Page Block 301

24-50-10, Page Block 001

24-50-10, Page Block 001

24-50-20, Page Block 001

24-50-40, Page Block 001

52-30-00, Page Block 001

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) Put the access platform(s) in position at the level of door 831.

(c) Open the FWD Cargo-compartment door 831 (Refer to AMM 52-30-00, Page Block

001 and AMM 06-41-52, Page Block 001).

(d) Open the door 132AZ (Refer to AMM 06-41-52, Page Block 001).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 19

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(e) Open, safety/lock and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/CTL

3QN (1)

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/WARN

5QN (1)

101VU FUEL/L INNER TK/PUMP

2/SUPPLY

1QA (1)

101VU FUEL/R INNER TK/PUMP

1/SUPPLY

2QA (1)

101VU FUEL/L INNER TK/PUMP

1/SUPPLY

7QA (1)

101VU FUEL/R INNER TK/PUMP

2/SUPPLY

8QA (1)

101VU FUEL/CTR

TK/L/PUMP/SUPPLY

99QA (1)

101VU FUEL/CTR

TK/R/PUMP/SUPPLY

100QA (1)

101VU FUEL/TRIM TANK/PUMP

1/SUPPLY

1QN (1)

101VU FUEL/TRIM TK/PUMP

2/SUPPLY

2QN (1)

128VU FUEL/TRIM TK/XFR PUMP

2/CTL

4QN (1)

128VU FUEL/TRIM TK/XFR PUMP

2/WARN

6QN (1)

128VU FUEL/L INR TK/PUMP

2/WARN

11QA (1)

128VU FUEL/R INR TK/PUMP

1/WARN

12QA (1)

128VU FUEL/L INR TK/PUMP

1/WARN

17QA (1)

128VU FUEL/R INR TK/PUMP

2/WARN

18QA (1)

128VU FUEL/L INR TK/PUMP 2/CTL 59QA (1)

128VU FUEL/R INR TK/PUMP 1/CTL 60QA (1)

128VU FUEL/CTR TK/L/PUMP/CTL 63QA (1)

128VU FUEL/CTR TK/R/PUMP/CTL 64QA (1)

128VU FUEL/L INR TK/PUMP 1/CTL 69QA (1)

128VU FUEL/R INR TK/PUMP 2/CTL 70QA (1)

128VU FUEL/CTR

TK/L/PUMP/WARN

101QA (1)

128VU FUEL/CTR

TK/R/PUMP/WARN

102QA (1)

or

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 20

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE

NOTES

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/CTL

3QN (1)

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/WARN

5QN (1)

101VU FUEL/L INNER TK/PUMP

2/SUPPLY

1QA (1)

101VU FUEL/R INNER TK/PUMP

1/SUPPLY

2QA (1)

101VU FUEL/L INNER TK/PUMP

1/SUPPLY

7QA (1)

101VU FUEL/R INNER TK/PUMP

2/SUPPLY

8QA (1)

101VU FUEL/CTR

TK/L/PUMP/SUPPLY

99QA (1)

101VU FUEL/CTR

TK/R/PUMP/SUPPLY

100QA (1)

101VU FUEL/TRIM TANK/PUMP

1/SUPPLY

1QN (1)

101VU FUEL/TRIM TK/PUMP

2/SUPPLY

2QN (1)

132VU FUEL/TRIM TK/XFR PUMP

2/CTL

4QN (1)

132VU FUEL/TRIM TK/XFR PUMP

2/WARN

6QN (1)

132VU FUEL/L INR TK/PUMP

2/WARN

11QA (1)

132VU FUEL/R INR TK/PUMP

1/WARN

12QA (1)

132VU FUEL/L INR TK/PUMP

1/WARN

17QA (1)

132VU FUEL/R INR TK/PUMP

2/WARN

18QA (1)

132VU FUEL/L INR TK/PUMP 2/CTL 59QA (1)

132VU FUEL/R INR TK/PUMP 1/CTL 60QA (1)

132VU FUEL/CTR TK/L/PUMP/CTL 63QA (1)

132VU FUEL/CTR TK/R/PUMP/CTL 64QA (1)

132VU FUEL/L INR TK/PUMP 1/CTL 69QA (1)

132VU FUEL/R INR TK/PUMP 2/CTL 70QA (1)

132VU FUEL/CTR

TK/L/PUMP/WARN

101QA (1)

132VU FUEL/CTR

TK/R/PUMP/WARN

102QA (1)

NOTE (1): For the location of the circuit breakers, refer to AMM 24-50-10,

Page Block 001, AMM 24-50-20, Page Block 001 and AMM

24-50-40, Page Block 001.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 21

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 003

(1) Subtask 286104-941-001-003 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

24-00-00, Page Block 301

24-50-10, Page Block 001

24-50-10, Page Block 001

24-50-20, Page Block 001

24-50-40, Page Block 001

52-30-00, Page Block 001

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) Put the access platform(s) in position at the level of door 831.

(c) Open the FWD Cargo-compartment door 831 (Refer to AMM 52-30-00, Page Block

001 and AMM 06-41-52, Page Block 001).

(d) Open the door 132AZ (Refer to AMM 06-41-52, Page Block 001).

(e) Open, safety/lock and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/CTL

3QN (1)

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/WARN

5QN (1)

101VU FUEL/L INNER TK/PUMP

2/SUPPLY

1QA (1)

101VU FUEL/R INNER TK/PUMP

1/SUPPLY

2QA (1)

101VU FUEL/L INNER TK/PUMP

1/SUPPLY

7QA (1)

101VU FUEL/R INNER TK/PUMP

2/SUPPLY

8QA (1)

101VU FUEL/CTR

TK/L/PUMP/SUPPLY

99QA (1)

101VU FUEL/CTR

TK/R/PUMP/SUPPLY

100QA (1)

101VU FUEL/TRIM TANK/PUMP

1/SUPPLY

1QN (1)

101VU FUEL/TRIM TK/PUMP

2/SUPPLY

2QN (1)

128VU FUEL/TRIM TK/XFR PUMP

2/CTL

4QN (1)

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 22

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE

NOTES

128VU FUEL/TRIM TK/XFR PUMP

2/WARN

6QN (1)

128VU FUEL/L INR TK/PUMP

2/WARN

11QA (1)

128VU FUEL/R INR TK/PUMP

1/WARN

12QA (1)

128VU FUEL/L INR TK/PUMP

1/WARN

17QA (1)

128VU FUEL/R INR TK/PUMP

2/WARN

18QA (1)

128VU FUEL/L INR TK/PUMP 2/CTL 59QA (1)

128VU FUEL/R INR TK/PUMP 1/CTL 60QA (1)

128VU FUEL/CTR TK/L/PUMP/CTL 63QA (1)

128VU FUEL/CTR TK/R/PUMP/CTL 64QA (1)

128VU FUEL/L INR TK/PUMP 1/CTL 69QA (1)

128VU FUEL/R INR TK/PUMP 2/CTL 70QA (1)

128VU FUEL/CTR

TK/L/PUMP/WARN

101QA (1)

128VU FUEL/CTR

TK/R/PUMP/WARN

102QA (1)

or

PANEL DESIGNATION FIN LOCATION SEE

NOTES

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/CTL

3QN (1)

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/WARN

5QN (1)

101VU FUEL/L INNER TK/PUMP

2/SUPPLY

1QA (1)

101VU FUEL/R INNER TK/PUMP

1/SUPPLY

2QA (1)

101VU FUEL/L INNER TK/PUMP

1/SUPPLY

7QA (1)

101VU FUEL/R INNER TK/PUMP

2/SUPPLY

8QA (1)

101VU FUEL/CTR

TK/L/PUMP/SUPPLY

99QA (1)

101VU FUEL/CTR

TK/R/PUMP/SUPPLY

100QA (1)

101VU FUEL/TRIM TANK/PUMP

1/SUPPLY

1QN (1)

101VU FUEL/TRIM TK/PUMP

2/SUPPLY

2QN (1)

132VU FUEL/TRIM TK/XFR PUMP

2/CTL

4QN (1)

132VU FUEL/TRIM TK/XFR PUMP

2/WARN

6QN (1)

132VU FUEL/L INR TK/PUMP

2/WARN

11QA (1)

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 23

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE

NOTES

132VU FUEL/R INR TK/PUMP

1/WARN

12QA (1)

132VU FUEL/L INR TK/PUMP

1/WARN

17QA (1)

132VU FUEL/R INR TK/PUMP

2/WARN

18QA (1)

132VU FUEL/L INR TK/PUMP 2/CTL 59QA (1)

132VU FUEL/R INR TK/PUMP 1/CTL 60QA (1)

132VU FUEL/CTR TK/L/PUMP/CTL 63QA (1)

132VU FUEL/CTR TK/R/PUMP/CTL 64QA (1)

132VU FUEL/L INR TK/PUMP 1/CTL 69QA (1)

132VU FUEL/R INR TK/PUMP 2/CTL 70QA (1)

132VU FUEL/CTR

TK/L/PUMP/WARN

101QA (1)

132VU FUEL/CTR

TK/R/PUMP/WARN

102QA (1)

NOTE (1): For the location of the circuit breakers, refer to AMM 24-50-10,

Page Block 001, AMM 24-50-20, Page Block 001 and AMM

24-50-40, Page Block 001.

**CONF 004

(1) Subtask 286104-941-001-003 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

24-00-00, Page Block 301

24-50-10, Page Block 001

24-50-10, Page Block 001

24-50-20, Page Block 001

24-50-40, Page Block 001

52-30-00, Page Block 001

(a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page

Block 301).

(b) Put the access platform(s) in position at the level of door 831.

(c) Open the FWD Cargo-compartment door 831 (Refer to AMM 52-30-00, Page Block

001 and AMM 06-41-52, Page Block 001).

(d) Open the door 132AZ (Refer to AMM 06-41-52, Page Block 001).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 24

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(e) Open, safety/lock and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/CTL

3QN (1)

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/WARN

5QN (1)

101VU FUEL/L INNER TK/PUMP

2/SUPPLY

1QA (1)

101VU FUEL/R INNER TK/PUMP

1/SUPPLY

2QA (1)

101VU FUEL/L INNER TK/PUMP

1/SUPPLY

7QA (1)

101VU FUEL/R INNER TK/PUMP

2/SUPPLY

8QA (1)

101VU FUEL/CTR

TK/L/PUMP/SUPPLY

99QA (1)

101VU FUEL/CTR

TK/R/PUMP/SUPPLY

100QA (1)

101VU FUEL/TRIM TANK/PUMP

1/SUPPLY

1QN (1)

101VU FUEL/TRIM TK/PUMP

2/SUPPLY

2QN (1)

128VU FUEL/TRIM TK/XFR PUMP

2/CTL

4QN (1)

128VU FUEL/TRIM TK/XFR PUMP

2/WARN

6QN (1)

128VU FUEL/L INR TK/PUMP

2/WARN

11QA (1)

128VU FUEL/R INR TK/PUMP

1/WARN

12QA (1)

128VU FUEL/L INR TK/PUMP

1/WARN

17QA (1)

128VU FUEL/R INR TK/PUMP

2/WARN

18QA (1)

128VU FUEL/L INR TK/PUMP 2/CTL 59QA (1)

128VU FUEL/R INR TK/PUMP 1/CTL 60QA (1)

128VU FUEL/CTR TK/L/PUMP/CTL 63QA (1)

128VU FUEL/CTR TK/R/PUMP/CTL 64QA (1)

128VU FUEL/L INR TK/PUMP 1/CTL 69QA (1)

128VU FUEL/R INR TK/PUMP 2/CTL 70QA (1)

128VU FUEL/CTR

TK/L/PUMP/WARN

101QA (1)

128VU FUEL/CTR

TK/R/PUMP/WARN

102QA (1)

or

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 25

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE

NOTES

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/CTL

3QN (1)

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/WARN

5QN (1)

101VU FUEL/L INNER TK/PUMP

2/SUPPLY

1QA (1)

101VU FUEL/R INNER TK/PUMP

1/SUPPLY

2QA (1)

101VU FUEL/L INNER TK/PUMP

1/SUPPLY

7QA (1)

101VU FUEL/R INNER TK/PUMP

2/SUPPLY

8QA (1)

101VU FUEL/CTR

TK/L/PUMP/SUPPLY

99QA (1)

101VU FUEL/CTR

TK/R/PUMP/SUPPLY

100QA (1)

101VU FUEL/TRIM TANK/PUMP

1/SUPPLY

1QN (1)

101VU FUEL/TRIM TK/PUMP

2/SUPPLY

2QN (1)

132VU FUEL/TRIM TK/XFR PUMP

2/CTL

4QN (1)

132VU FUEL/TRIM TK/XFR PUMP

2/WARN

6QN (1)

132VU FUEL/L INR TK/PUMP

2/WARN

11QA (1)

132VU FUEL/R INR TK/PUMP

1/WARN

12QA (1)

132VU FUEL/L INR TK/PUMP

1/WARN

17QA (1)

132VU FUEL/R INR TK/PUMP

2/WARN

18QA (1)

132VU FUEL/L INR TK/PUMP 2/CTL 59QA (1)

132VU FUEL/R INR TK/PUMP 1/CTL 60QA (1)

132VU FUEL/CTR TK/L/PUMP/CTL 63QA (1)

132VU FUEL/CTR TK/R/PUMP/CTL 64QA (1)

132VU FUEL/L INR TK/PUMP 1/CTL 69QA (1)

132VU FUEL/R INR TK/PUMP 2/CTL 70QA (1)

132VU FUEL/CTR

TK/L/PUMP/WARN

101QA (1)

132VU FUEL/CTR

TK/R/PUMP/WARN

102QA (1)

NOTE (1): For the location of the circuit breakers, refer to AMM 24-50-10,

Page Block 001, AMM 24-50-20, Page Block 001 and AMM

24-50-40, Page Block 001.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 26

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 286104-831-001-001 - Modification of the Equipment and the Wiring in the

LH Relay Box 107VU.

Work Zones and Access Panels

Zone Access/Work location

120 Work location Electrical panel 107VU

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills ELECTRICAL

Material necessary to do the job

Kit 286104A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS1629-28A0 6 GFI

2 E0673D0S 6 BASE

3 NAS1101-04-7 18 SCREW

4 ASNA2397-3L 18 WASHER

5 MS21042-04 18 NUT

EN3155-017F1216 36 CONTACT

EN3155-017F1620 30 CONTACT

References

Fig. A-FBAAA

Location of the Modification

Sheet 01

Fig. A-FBBAA

Modification of the Equipment in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHAAA

Hook-up Chart of the Modification of the

Wiring of the Relay 35QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHBAB

Hook-up Chart of the Modification of the

Wiring of the Relay 36QA in the LH

Relay Box 107VU.

Sheet 01

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 27

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

References

Fig. A-FHCAA

Hook-up Chart of the Modification of the

Wiring of the Relay 41QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHDAA

Hook-up Chart of the Modification of the

Wiring of the Relay 42QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHEAA

Hook-up Chart of the Modification of the

Wiring of the Relay 109QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHFAA

Hook-up Chart of the Modification of the

Wiring of the Relay 110QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FWAAA

Modification of the Wiring of the Relay

35QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWBAB

Modification of the Wiring of the Relay

36QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWCAA

Modification of the Wiring of the Relay

41QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWDAA

Modification of the Wiring of the Relay

42QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWEAA

Modification of the Wiring of the Relay

109QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWFAA

Modification of the Wiring of the Relay

110QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

(a) Remove the relay 35QA (Refer to Fig. A-FBBAA Sheet 01):

FIN 35QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 35QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 28

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

3 Nut Item (5) Discard

(b) Install the relay GFI 35QA:

1 Install (Refer to Fig. A-FBBAA Sheet 01):

FIN 35QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWAAA Sheet 01 and Fig. A-FWAAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHAAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAA Sheet 01):

FIN 35QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

(c) Remove the relay 36QA (Refer to Fig. A-FBBAA Sheet 01):

FIN 36QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 36QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 29

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(d) Install the relay GFI 36QA:

1 Install (Refer to Fig. A-FBBAA Sheet 01):

FIN 36QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWBAB Sheet 01 and Fig. A-FWBAB Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHBAB Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAA Sheet 01):

FIN 36QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

(e) Remove the relay 41QA (Refer to Fig. A-FBBAA Sheet 01):

FIN 41QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 41QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 30

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(f) Install the relay GFI 41QA:

1 Install (Refer to Fig. A-FBBAA Sheet 01):

FIN 41QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWCAA Sheet 01 and Fig. A-FWCAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHCAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAA Sheet 01):

FIN 41QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

(g) Remove the relay 42QA (Refer to Fig. A-FBBAA Sheet 01):

FIN 42QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 42QAA

1 Base NSA932844AA Item (2) Discard

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 31

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(h) Install the relay GFI 42QA:

1 Install (Refer to Fig. A-FBBAA Sheet 01):

FIN 42QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWDAA Sheet 01 and Fig. A-FWDAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHDAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAA Sheet 01):

FIN 42QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

(i) Remove the relay 109QA (Refer to Fig. A-FBBAA Sheet 01):

FIN 109QA

1 Relay NSA932843AA01 Item (1) Discard

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 32

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

FIN 109QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(j) Install the relay GFI 109QA:

1 Install (Refer to Fig. A-FBBAA Sheet 01):

FIN 109QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWEAA Sheet 01 and Fig. A-FWEAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHEAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAA Sheet 01):

FIN 109QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 33

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(k) Remove the relay 110QA (Refer to Fig. A-FBBAA Sheet 01):

FIN 110QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 110QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(l) Install the relay GFI 110QA:

1 Install (Refer to Fig. A-FBBAA Sheet 01):

FIN 110QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWFAA Sheet 01 and Fig. A-FWFAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHFAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAA Sheet 01):

FIN 110QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 34

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002

(1) Subtask 286104-831-001-002 - Modification of the Equipment and the Wiring in the

LH Relay Box 107VU.

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 286104A02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS1629-28A0 8 GFI

2 E0673D0S 8 BASE

3 NAS1101-04-7 24 SCREW

4 ASNA2397-3L 24 WASHER

5 MS21042-04 24 NUT

EN3155-017F1216 48 CONTACT

EN3155-017F1620 38 CONTACT

References

Fig. A-FBAAB

Location of the Modification

Sheet 01

Fig. A-FBBAB

Modification of the Equipment in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHAAA

Hook-up Chart of the Modification of the

Wiring of the Relay 35QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHBAB

Hook-up Chart of the Modification of the

Wiring of the Relay 36QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHCAA

Hook-up Chart of the Modification of the

Wiring of the Relay 41QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHDAA

Hook-up Chart of the Modification of the

Wiring of the Relay 42QA in the LH

Relay Box 107VU.

Sheet 01

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 35

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

References

Fig. A-FHEAA

Hook-up Chart of the Modification of the

Wiring of the Relay 109QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHFAA

Hook-up Chart of the Modification of the

Wiring of the Relay 110QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FWAAA

Modification of the Wiring of the Relay

35QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWBAB

Modification of the Wiring of the Relay

36QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWCAA

Modification of the Wiring of the Relay

41QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWDAA

Modification of the Wiring of the Relay

42QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWEAA

Modification of the Wiring of the Relay

109QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWFAA

Modification of the Wiring of the Relay

110QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWGAB

Modification of the Wiring of the Relay

9QN in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWHAB

Modification of the Wiring of the Relay

10QN in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FHGAB

Hook-up Chart of the Modification of the

Wiring of the Relay 9QN in the LH Relay

Box 107VU.

Sheet 01

Fig. A-FHHAB

Hook-up Chart of the Modification of the

Wiring of the Relay 10QN in the LH

Relay Box 107VU.

Sheet 01

(a) Remove the relay 35QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 35QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 35QAA

1 Base NSA932844AA Item (2) Discard

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 36

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(b) Install the relay GFI 35QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 35QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWAAA Sheet 01 and Fig. A-FWAAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHAAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 35QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

(c) Remove the relay 36QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 36QA

1 Relay NSA932843AA01 Item (1) Discard

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 37

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

FIN 36QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(d) Install the relay GFI 36QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 36QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWBAB Sheet 01 and Fig. A-FWBAB Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHBAB Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 36QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 38

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(e) Remove the relay 41QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 41QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 41QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(f) Install the relay GFI 41QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 41QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWCAA Sheet 01 and Fig. A-FWCAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHCAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 41QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 39

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(g) Remove the relay 42QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 42QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 42QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(h) Install the relay GFI 42QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 42QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWDAA Sheet 01 and Fig. A-FWDAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHDAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 42QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 40

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(i) Remove the relay 109QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 109QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 109QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(j) Install the relay GFI 109QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 109QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWEAA Sheet 01 and Fig. A-FWEAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHEAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 109QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 41

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(k) Remove the relay 110QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 110QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 110QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(l) Install the relay GFI 110QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 110QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWFAA Sheet 01 and Fig. A-FWFAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHFAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 110QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 42

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(m) Remove the relay 9QN (Refer to Fig. A-FBBAB Sheet 01):

FIN 9QN

1 Relay NSA932843AA01 Item (1) Discard

FIN 9QNA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(n) Install the relay GFI 9QN:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 9QNA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWGAB Sheet 01 and Fig. A-FWGAB Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FHGAB Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

4 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 9QN

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 43

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(o) Remove the relay 10QN (Refer to Fig. A-FBBAB Sheet 01):

FIN 10QN

1 Relay NSA932843AA01 Item (1) Discard

FIN 10QNA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(p) Install the relay GFI 10QN:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 10QNA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWHAB Sheet 01 and Fig. A-FWHAB Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FHHAB Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

4 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 10QN

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 44

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 003

(1) Subtask 286104-831-001-003 - Modification of the Equipment and the Wiring in the

LH Relay Box 107VU.

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 286104A02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS1629-28A0 8 GFI

2 E0673D0S 8 BASE

3 NAS1101-04-7 24 SCREW

4 ASNA2397-3L 24 WASHER

5 MS21042-04 24 NUT

EN3155-017F1216 48 CONTACT

EN3155-017F1620 38 CONTACT

References

Fig. A-FBAAB

Location of the Modification

Sheet 01

Fig. A-FBBAB

Modification of the Equipment in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHAAA

Hook-up Chart of the Modification of the

Wiring of the Relay 35QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHBAA

Hook-up Chart of the Modification of the

Wiring of the Relay 36QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHCAA

Hook-up Chart of the Modification of the

Wiring of the Relay 41QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHDAA

Hook-up Chart of the Modification of the

Wiring of the Relay 42QA in the LH

Relay Box 107VU.

Sheet 01

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 45

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

References

Fig. A-FHEAB

Hook-up Chart of the Modification of the

Wiring of the Relay 109QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHFAA

Hook-up Chart of the Modification of the

Wiring of the Relay 110QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FWAAA

Modification of the Wiring of the Relay

35QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWBAA

Modification of the Wiring of the Relay

36QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWCAA

Modification of the Wiring of the Relay

41QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWDAA

Modification of the Wiring of the Relay

42QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWEAB

Modification of the Wiring of the Relay

109QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWFAA

Modification of the Wiring of the Relay

110QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FHGAB

Hook-up Chart of the Modification of the

Wiring of the Relay 9QN in the LH Relay

Box 107VU.

Sheet 01

Fig. A-FHHAB

Hook-up Chart of the Modification of the

Wiring of the Relay 10QN in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FWGAB

Modification of the Wiring of the Relay

9QN in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWHAB

Modification of the Wiring of the Relay

10QN in the LH Relay Box 107VU.

Sheet 01

Sheet 02

(a) Remove the relay 35QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 35QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 35QAA

1 Base NSA932844AA Item (2) Discard

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 46

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(b) Install the relay GFI 35QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 35QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWAAA Sheet 01 and Fig. A-FWAAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHAAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 35QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

(c) Remove the relay 36QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 36QA

1 Relay NSA932843AA01 Item (1) Discard

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 47

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

FIN 36QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(d) Install the relay GFI 36QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 36QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWBAA Sheet 01 and Fig. A-FWBAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHBAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 36QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 48

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(e) Remove the relay 41QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 41QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 41QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(f) Install the relay GFI 41QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 41QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWCAA Sheet 01 and Fig. A-FWCAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHCAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 41QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 49

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(g) Remove the relay 42QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 42QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 42QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(h) Install the relay GFI 42QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 42QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWDAA Sheet 01 and Fig. A-FWDAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHDAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 42QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 50

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(i) Remove the relay 109QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 109QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 109QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(j) Install the relay GFI 109QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 109QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWEAB Sheet 01 and Fig. A-FWEAB Sheet 02and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHEAB Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 109QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 51

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(k) Remove the relay 110QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 110QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 110QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(l) Install the relay GFI 110QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 110QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWFAA Sheet 01 and Fig. A-FWFAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHFAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 110QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 52

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(m) Remove the relay 9QN (Refer to Fig. A-FBBAB Sheet 01):

FIN 9QN

1 Relay NSA932843AA01 Item (1) Discard

FIN 9QNA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(n) Install the relay GFI 9QN:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 9QNA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWGAB Sheet 01 and Fig. A-FWGAB Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FHGAB Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

4 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 9QN

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 53

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(o) Remove the relay 10QN (Refer to Fig. A-FBBAB Sheet 01):

FIN 10QN

1 Relay NSA932843AA01 Item (1) Discard

FIN 10QNA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(p) Install the relay GFI 10QN:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 10QNA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWHAB Sheet 01 and Fig. A-FWHAB Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FHHAB Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

4 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 10QN

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 54

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 004

(1) Subtask 286104-831-001-004 - Modification of the Equipment and the Wiring in the

LH Relay Box 107VU.

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 286104A02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS1629-28A0 8 GFI

2 E0673D0S 8 BASE

3 NAS1101-04-7 24 SCREW

4 ASNA2397-3L 24 WASHER

5 MS21042-04 24 NUT

EN3155-017F1216 48 CONTACT

EN3155-017F1620 38 CONTACT

References

Fig. A-FBAAB

Location of the Modification

Sheet 01

Fig. A-FBBAB

Modification of the Equipment in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHAAA

Hook-up Chart of the Modification of the

Wiring of the Relay 35QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHBAA

Hook-up Chart of the Modification of the

Wiring of the Relay 36QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHCAA

Hook-up Chart of the Modification of the

Wiring of the Relay 41QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHDAA

Hook-up Chart of the Modification of the

Wiring of the Relay 42QA in the LH

Relay Box 107VU.

Sheet 01

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 55

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

References

Fig. A-FHEAB

Hook-up Chart of the Modification of the

Wiring of the Relay 109QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHFAA

Hook-up Chart of the Modification of the

Wiring of the Relay 110QA in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FHGAA

Hook-up Chart of the Modification of the

Wiring of the Relay 9QN in the LH Relay

Box 107VU.

Sheet 01

Fig. A-FHHAA

Hook-up Chart of the Modification of the

Wiring of the Relay 10QN in the LH

Relay Box 107VU.

Sheet 01

Fig. A-FWAAA

Modification of the Wiring of the Relay

35QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWBAA

Modification of the Wiring of the Relay

36QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWCAA

Modification of the Wiring of the Relay

41QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWDAA

Modification of the Wiring of the Relay

42QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWEAB

Modification of the Wiring of the Relay

109QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWFAA

Modification of the Wiring of the Relay

110QA in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWGAA

Modification of the Wiring of the Relay

9QN in the LH Relay Box 107VU.

Sheet 01

Sheet 02

Fig. A-FWHAA

Modification of the Wiring of the Relay

10QN in the LH Relay Box 107VU.

Sheet 01

Sheet 02

(a) Remove the relay 35QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 35QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 35QAA

1 Base NSA932844AA Item (2) Discard

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 56

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(b) Install the relay GFI 35QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 35QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWAAA Sheet 01 and Fig. A-FWAAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHAAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 35QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

(c) Remove the relay 36QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 36QA

1 Relay NSA932843AA01 Item (1) Discard

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 57

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

FIN 36QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(d) Install the relay GFI 36QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 36QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWBAA Sheet 01 and Fig. A-FWBAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHBAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 36QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 58

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(e) Remove the relay 41QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 41QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 41QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(f) Install the relay GFI 41QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 41QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWCAA Sheet 01 and Fig. A-FWCAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHCAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 41QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 59

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(g) Remove the relay 42QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 42QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 42QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(h) Install the relay GFI 42QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 42QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWDAA Sheet 01 and Fig. A-FWDAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHDAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 42QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 60

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(i) Remove the relay 109QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 109QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 109QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(j) Install the relay GFI 109QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 109QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWEAB Sheet 01 and Fig. A-FWEAB Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHEAB Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 109QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 61

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(k) Remove the relay 110QA (Refer to Fig. A-FBBAB Sheet 01):

FIN 110QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 110QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(l) Install the relay GFI 110QA:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 110QAA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWFAA Sheet 01 and Fig. A-FWFAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 22 (Refer to Fig. A-FHFAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

5 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 110QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 62

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(m) Remove the relay 9QN (Refer to Fig. A-FBBAB Sheet 01):

FIN 9QN

1 Relay NSA932843AA01 Item (1) Discard

FIN 9QNA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(n) Install the relay GFI 9QN:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 9QNA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWGAA Sheet 01 and Fig. A-FWGAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FHGAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

4 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 9QN

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 63

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(o) Remove the relay 10QN (Refer to Fig. A-FBBAB Sheet 01):

FIN 10QN

1 Relay NSA932843AA01 Item (1) Discard

FIN 10QNA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

(p) Install the relay GFI 10QN:

1 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 10QNA

1 Base E0673D0S Item 2

Attach with:

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWHAA Sheet 01 and Fig. A-FWHAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FHHAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

4 Contact EN3155-017F1620

3 Install (Refer to Fig. A-FBBAB Sheet 01):

FIN 10QN

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws to a torque value comprised between

0.023 m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 64

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 286104-840-401-001 - Preparation for Test Procedure

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 12-11-28, Page Block 301

Fig. A-UBAAA

Ground Fault Interrupter - Tripped/Not

Tripped

Sheet 01

(a) Refer to Fig. A-UBAAA Sheet 01

1 Inspect the GFI 35QA, 36QA, 41QA, 42QA, 109QA, and 110QA and make

sure that it is in the reset (non-tripped) state (metal shaft is not seen on the

trip/reset plunger).

2 If the GFI 35QA, 36QA, 41QA, 42QA, 109QA, and 110QA is tripped (metal

shaft is seen on the trip/reset plunger) then reset by depressing the trip/reset

plunger until it latches in.

3 Make sure that the left and right inner tanks and the center tank contains a

minimum of 500 Kg (1,102 lb) of fuel. If necessary, refuel the tanks (Refer to

AMM 12-11-28, Page Block 301).

(2) Subtask 286104-700-001-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-50-20, Page Block 001

24-50-40, Page Block 001

28-21-12, Page Block 501

28-21-36, Page Block 401

(a) Remove the safety clip(s) and/or tag(s) and close/unlock these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

101VU FUEL/L INNER TK/PUMP

2/SUPPLY

1QA (1)

101VU FUEL/R INNER TK/PUMP

1/SUPPLY

2QA (1)

101VU FUEL/L INNER TK/PUMP

1/SUPPLY

7QA (1)

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 65

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE

NOTES

101VU FUEL/R INNER TK/PUMP

2/SUPPLY

8QA (1)

101VU FUEL/CTR

TK/L/PUMP/SUPPLY

99QA (1)

101VU FUEL/CTR

TK/R/PUMP/SUPPLY

100QA (1)

128VU FUEL/L INR TK/PUMP

2/WARN

11QA (1)

128VU FUEL/R INR TK/PUMP

1/WARN

12QA (1)

128VU FUEL/L INR TK/PUMP

1/WARN

17QA (1)

128VU FUEL/R INR TK/PUMP

2/WARN

18QA (1)

128VU FUEL/L INR TK/PUMP 2/CTL 59QA (1)

128VU FUEL/R INR TK/PUMP 1/CTL 60QA (1)

128VU FUEL/CTR TK/L/PUMP/CTL 63QA (1)

128VU FUEL/CTR TK/R/PUMP/CTL 64QA (1)

128VU FUEL/L INR TK/PUMP 1/CTL 69QA (1)

128VU FUEL/R INR TK/PUMP 2/CTL 70QA (1)

128VU FUEL/CTR

TK/L/PUMP/WARN

101QA (1)

128VU FUEL/CTR

TK/R/PUMP/WARN

102QA (1)

or

PANEL DESIGNATION FIN LOCATION SEE

NOTES

101VU FUEL/L INNER TK/PUMP

2/SUPPLY

1QA (1)

101VU FUEL/R INNER TK/PUMP

1/SUPPLY

2QA (1)

101VU FUEL/L INNER TK/PUMP

1/SUPPLY

7QA (1)

101VU FUEL/R INNER TK/PUMP

2/SUPPLY

8QA (1)

101VU FUEL/CTR

TK/L/PUMP/SUPPLY

99QA (1)

101VU FUEL/CTR

TK/R/PUMP/SUPPLY

100QA (1)

132VU FUEL/L INR TK/PUMP

2/WARN

11QA (1)

132VU FUEL/R INR TK/PUMP

1/WARN

12QA (1)

132VU FUEL/L INR TK/PUMP

1/WARN

17QA (1)

132VU FUEL/R INR TK/PUMP

2/WARN

18QA (1)

132VU FUEL/L INR TK/PUMP 2/CTL 59QA (1)

132VU FUEL/R INR TK/PUMP 1/CTL 60QA (1)

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 66

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE

NOTES

132VU FUEL/CTR TK/L/PUMP/CTL 63QA (1)

132VU FUEL/CTR TK/R/PUMP/CTL 64QA (1)

132VU FUEL/L INR TK/PUMP 1/CTL 69QA (1)

132VU FUEL/R INR TK/PUMP 2/CTL 70QA (1)

132VU FUEL/CTR

TK/L/PUMP/WARN

101QA (1)

132VU FUEL/CTR

TK/R/PUMP/WARN

102QA (1)

NOTE (1): For the location of the circuit breakers, refer to AMM 24-50-20,

Page Block 001 and AMM 24-50-40, Page Block 001.

(b) Do the operational test of the Inner Tanks Booster Pumps (Refer to AMM 28-21-12,

Page Block 501).

(c) Do the test procedure as specified after the installation of the center tank booster

pumps (81QA, 82QA) (Refer to AMM 28-21-36, Page Block 401).

(3) Subtask 286104-710-401-001 - Operational Test

Work Zones and Access Panels

Zone Access/Work location

121 Work location 107VU 35-QA

107VU 36-QA

107VU 41-QA

107VU 42-QA

107VU 109-QA

107VU 110-QA

Manpower Resources

Skills ELECTRICAL

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

L Inner Tank Pump 2 pushbutton switch

(P/BSW) (19QA) comes on.

- L Inner Tank Pump 2 Selected OFF.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 2 P/BSW (19 QA).

- L Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 2 P/BSW (19QA).

- L Inner Tank Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the L Inner Tank Pump 2 P/BSW

(19QA) comes on.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 2 P/BSW (19QA).

- L Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 67

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the L

Inner Tank Pump 2 GFI (35QA).

- L Inner Tank Pump 2 stops.

On Panel 107VU:

- the trip/RESET button on GFI (35QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the L Inner Tank Pump 2

P/BSW (19QA) comes on.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 2 P/BSW (19QA).

On Panel 430VU:

- the FAULT legend lamp on the L Inner Tank Pump 2

P/BSW (19QA) goes off.

- OFF legend lamp on the L Inner Tank Pump 2 P/BSW

(19QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the L Inner Tank Pump

2 GFI (35QA) until it latches in.

- L Inner Tank Pump 2 GFI (35QA) reset.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 2 P/BSW (19QA).

- L Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 2 P/BSW (19QA).

- L Inner Tank Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the L Inner Tank Pump 2 P/BSW

(19QA) comes on.

Table 1 - Operational Test Procedure - 35QA L Inner Tank Pump 2

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

R Inner Tank Pump 1 pushbutton switch

(P/BSW) (20QA) comes on.

- R Inner Tank Pump 1 Selected OFF.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the R Inner Tank Pump 1 P/BSW

(20QA) comes on.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 68

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the R

Inner Tank Pump 1 GFI (36QA).

- R Inner Tank Pump 1 stops.

On Panel 107VU:

- the trip/RESET button on GFI (36QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the R Inner Tank Pump 1

P/BSW (20QA) comes on.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 1 P/BSW (20QA).

On Panel 430VU:

- the FAULT legend lamp on the R Inner Tank Pump 1

P/BSW (20QA) goes off.

- OFF legend lamp on the R Inner Tank Pump 1 P/BSW

(20QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the R Inner Tank Pump

1 GFI (36QA) until it latches in.

- R Inner Tank Pump 1 GFI (36QA) reset.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the R Inner Tank Pump 1 P/BSW

(20QA) comes on.

Table 2 - Operational Test Procedure - 36QA R Inner Tank Pump 1

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

L Inner Tank Pump 1 pushbutton switch

(P/BSW) (25QA) comes on.

- L Inner Tank Pump 1 Selected OFF.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the L Inner Tank Pump 1 P/BSW

(25QA) comes on.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 69

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the L

Inner Tank Pump 1 GFI (41QA).

- L Inner Tank Pump 1 stops.

On Panel 107VU:

- the trip/RESET button on GFI (41QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the L Inner Tank Pump 1

P/BSW (25QA) comes on.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 1 P/BSW (25QA).

On Panel 430VU:

- the FAULT legend lamp on the L Inner Tank Pump 1

P/BSW (25QA) goes off.

- OFF legend lamp on the L Inner Tank Pump 1 P/BSW

(25QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the L Inner Tank Pump

1 GFI (41QA) until it latches in.

- L Inner Tank Pump 1 GFI (41QA) reset.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the L Inner Tank Pump 1 P/BSW

(25QA) comes on.

Table 3 - Operational Test Procedure - 41QA L Inner Tank Pump 1

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

R Inner Tank Pump 2 pushbutton switch

(P/BSW) (26QA) comes on.

- R Inner Tank Pump 2 Selected OFF.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the R Inner Tank Pump 2 P/BSW

(26QA) comes on.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 70

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the R

Inner Tank Pump 2 GFI (42QA).

- R Inner Tank Pump 2 stops.

On Panel 107VU:

- the trip/RESET button on GFI (42QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the R Inner Tank Pump 2

P/BSW (26QA) comes on.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 2 P/BSW (26QA).

On Panel 430VU:

- the FAULT legend lamp on the R Inner Tank Pump 2

P/BSW (26QA) goes off.

- OFF legend lamp on the R Inner Tank Pump 2 P/BSW

(26QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the R Inner Tank Pump

2 GFI (42QA) until it latches in.

- R Inner Tank Pump 2 GFI (42QA) reset.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the R Inner Tank Pump 2 P/BSW

(26QA) comes on.

Table 4 - Operational Test Procedure - 42QA R Inner Tank Pump 2

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

L Center Tank Pump pushbutton switch

(P/BSW) (93QA) comes on.

- L Center Tank Pump Selected OFF.

On Panel 430VU:

- Press (Select in) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump stops.

On Panel 430VU:

- OFF legend lamp on the L Center Tank Pump P/BSW

(93QA) comes on.

On Panel 430VU:

- Press (Select in) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 71

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the L

Center Tank Pump GFI (109QA).

- L Center Tank Pump stops.

On Panel 107VU:

- the trip/RESET button on GFI (109QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the L Center Tank Pump

P/BSW (93QA) comes on.

On Panel 430VU:

- Press (Release out) the L Center Tank

Pump P/BSW (93QA).

On Panel 430VU:

- the FAULT legend lamp on the L Center Tank Pump

P/BSW (93QA) goes off.

- OFF legend lamp on the L Center Tank Pump P/BSW

(93QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the L Center Tank

Pump GFI (109QA) until it latches in.

- L Center Tank Pump GFI (109QA) reset.

On Panel 430VU:

- Press (Select in) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump stops.

On Panel 430VU:

- OFF legend lamp on the L Center Tank Pump P/BSW

(93QA) comes on.

Table 5 - Operational Test Procedure - 109QA L Center Tank Pump

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

R Center Tank Pump pushbutton switch

(P/BSW) (94QA) comes on.

- R Center Tank Pump Selected OFF.

On Panel 430VU:

- Press (Select in) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump stops.

On Panel 430VU:

- OFF legend lamp on the R Center Tank Pump P/BSW

(94QA) comes on.

On Panel 430VU:

- Press (Select in) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 72

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the R

Center Tank Pump GFI (110QA).

- R Center Tank Pump stops.

On Panel 107VU:

- the trip/RESET button on GFI (110QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the R Center Tank Pump

P/BSW (94QA) comes on.

On Panel 430VU:

- Press (Release out) the R Center Tank

Pump P/BSW (94QA).

On Panel 430VU:

- the FAULT legend lamp on the R Center Tank Pump

P/BSW (94QA) goes off.

- OFF legend lamp on the R Center Tank Pump P/BSW

(94QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the R Center Tank

Pump GFI (110QA) until it latches in.

- R Center Tank Pump GFI (110QA) reset.

On Panel 430VU:

- Press (Select in) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump stops.

On Panel 430VU:

- OFF legend lamp on the R Center Tank Pump P/BSW

(94QA) comes on.

Table 6 - Operational Test Procedure - 110QA R Center Tank Pump

**CONF 002

(1) Subtask 286104-840-401-002 - Preparation for Test Procedure

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 12-11-28, Page Block 301

Fig. A-UBAAA

Ground Fault Interrupter - Tripped/Not

Tripped

Sheet 01

(a) Refer to Fig. A-UBAAA Sheet 01

1 Inspect the GFI 35QA, 36QA, 41QA, 42QA, 109QA, 110QA, 9QN and 10QN

and make sure that it is in the reset (non-tripped) state (metal shaft is not

seen on the trip/reset plunger).

2 If the GFI 35QA, 36QA, 41QA, 42QA, 109QA, 110QA, 9QN and 10QN is

tripped (metal shaft is seen on the trip/reset plunger) then reset by depressing

the trip/reset plunger until it latches in.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 73

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

3 Make sure that the left and right inner tanks and the center tank contains a

minimum of 500 Kg (1,102 lb) of fuel. If necessary, refuel the tanks (Refer to

AMM 12-11-28, Page Block 301).

(2) Subtask 286104-700-001-003 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-50-10, Page Block 001

24-50-20, Page Block 001

24-50-40, Page Block 001

28-21-12, Page Block 501

28-21-36, Page Block 401

28-27-00, Page Block 501

(a) Remove the safety clip(s) and/or tag(s) and close/unlock these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/CTL

3QN (1)

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/WARN

5QN (1)

101VU FUEL/L INNER TK/PUMP

2/SUPPLY

1QA (1)

101VU FUEL/R INNER TK/PUMP

1/SUPPLY

2QA (1)

101VU FUEL/L INNER TK/PUMP

1/SUPPLY

7QA (1)

101VU FUEL/R INNER TK/PUMP

2/SUPPLY

8QA (1)

101VU FUEL/CTR

TK/L/PUMP/SUPPLY

99QA (1)

101VU FUEL/CTR

TK/R/PUMP/SUPPLY

100QA (1)

101VU FUEL/TRIM TANK/PUMP

1/SUPPLY

1QN (1)

101VU FUEL/TRIM TK/PUMP

2/SUPPLY

2QN (1)

128VU FUEL/TRIM TK/XFR PUMP

2/CTL

4QN (1)

128VU FUEL/TRIM TK/XFR PUMP

2/WARN

6QN (1)

128VU FUEL/L INR TK/PUMP

2/WARN

11QA (1)

128VU FUEL/R INR TK/PUMP

1/WARN

12QA (1)

128VU FUEL/L INR TK/PUMP

1/WARN

17QA (1)

128VU FUEL/R INR TK/PUMP

2/WARN

18QA (1)

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 74

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE

NOTES

128VU FUEL/L INR TK/PUMP 2/CTL 59QA (1)

128VU FUEL/R INR TK/PUMP 1/CTL 60QA (1)

128VU FUEL/CTR TK/L/PUMP/CTL 63QA (1)

128VU FUEL/CTR TK/R/PUMP/CTL 64QA (1)

128VU FUEL/L INR TK/PUMP 1/CTL 69QA (1)

128VU FUEL/R INR TK/PUMP 2/CTL 70QA (1)

128VU FUEL/CTR

TK/L/PUMP/WARN

101QA (1)

128VU FUEL/CTR

TK/R/PUMP/WARN

102QA (1)

or

PANEL DESIGNATION FIN LOCATION SEE

NOTES

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/CTL

3QN (1)

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/WARN

5QN (1)

101VU FUEL/L INNER TK/PUMP

2/SUPPLY

1QA (1)

101VU FUEL/R INNER TK/PUMP

1/SUPPLY

2QA (1)

101VU FUEL/L INNER TK/PUMP

1/SUPPLY

7QA (1)

101VU FUEL/R INNER TK/PUMP

2/SUPPLY

8QA (1)

101VU FUEL/CTR

TK/L/PUMP/SUPPLY

99QA (1)

101VU FUEL/CTR

TK/R/PUMP/SUPPLY

100QA (1)

101VU FUEL/TRIM TANK/PUMP

1/SUPPLY

1QN (1)

101VU FUEL/TRIM TK/PUMP

2/SUPPLY

2QN (1)

132VU FUEL/TRIM TK/XFR PUMP

2/CTL

4QN (1)

132VU FUEL/TRIM TK/XFR PUMP

2/WARN

6QN (1)

132VU FUEL/L INR TK/PUMP

2/WARN

11QA (1)

132VU FUEL/R INR TK/PUMP

1/WARN

12QA (1)

132VU FUEL/L INR TK/PUMP

1/WARN

17QA (1)

132VU FUEL/R INR TK/PUMP

2/WARN

18QA (1)

132VU FUEL/L INR TK/PUMP 2/CTL 59QA (1)

132VU FUEL/R INR TK/PUMP 1/CTL 60QA (1)

132VU FUEL/CTR TK/L/PUMP/CTL 63QA (1)

132VU FUEL/CTR TK/R/PUMP/CTL 64QA (1)

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 75

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE

NOTES

132VU FUEL/L INR TK/PUMP 1/CTL 69QA (1)

132VU FUEL/R INR TK/PUMP 2/CTL 70QA (1)

132VU FUEL/CTR

TK/L/PUMP/WARN

101QA (1)

132VU FUEL/CTR

TK/R/PUMP/WARN

102QA (1)

NOTE (1): For the location of the circuit breakers, refer to AMM 24-50-10,

Page Block 001, AMM 24-50-20, Page Block 001 and AMM

24-50-40, Page Block 001.

(b) Do the operational test of the Inner Tanks Booster Pumps (Refer to AMM 28-21-12,

Page Block 501).

(c) Do the test procedure as specified after the installation of the center tank booster

pumps (81QA, 82QA) (Refer to AMM 28-21-36, Page Block 401).

(d) Do the operational test of the Trim Tank Pumps (Refer to AMM 28-27-00, Page

Block 501).

(3) Subtask 286104-710-401-002 - Operational Test

Work Zones and Access Panels

Zone Access/Work location

121 Work location 107VU 35-QA

107VU 36-QA

107VU 41-QA

107VU 42-QA

107VU 109-QA

107VU 110-QA

107VU 9-QN

107VU 10-QN

Manpower Resources

Skills ELECTRICAL

WARNING: ACCIDENTAL REARWARD FUEL TRANSFER CAN MOVE THE C OF

G AFT OF SAFE LIMIT. MAKE SURE TRIM TANK VALVES ARE SHUT.

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

L Inner Tank Pump 2 pushbutton switch

(P/BSW) (19QA) comes on.

- L Inner Tank Pump 2 Selected OFF.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 2 P/BSW (19 QA).

- L Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 76

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 2 P/BSW (19QA).

- L Inner Tank Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the L Inner Tank Pump 2 P/BSW

(19QA) comes on.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 2 P/BSW (19QA).

- L Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 107VU:

- Press the test button on top of the L

Inner Tank Pump 2 GFI (35QA).

- L Inner Tank Pump 2 stops.

On Panel 107VU:

- the trip/RESET button on GFI (35QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the L Inner Tank Pump 2

P/BSW (19QA) comes on.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 2 P/BSW (19QA).

On Panel 430VU:

- the FAULT legend lamp on the L Inner Tank Pump 2

P/BSW (19QA) goes off.

- OFF legend lamp on the L Inner Tank Pump 2 P/BSW

(19QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the L Inner Tank Pump

2 GFI (35QA) until it latches in.

- L Inner Tank Pump 2 GFI (35QA) reset.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 2 P/BSW (19QA).

- L Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 2 P/BSW (19QA).

- L Inner Tank Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the L Inner Tank Pump 2 P/BSW

(19QA) comes on.

Table 1 - Operational Test Procedure - 35QA L Inner Tank Pump 2

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

R Inner Tank Pump 1 pushbutton switch

(P/BSW) (20QA) comes on.

- R Inner Tank Pump 1 Selected OFF.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the R Inner Tank Pump 1 P/BSW

(20QA) comes on.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 77

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 107VU:

- Press the test button on top of the R

Inner Tank Pump 1 GFI (36QA).

- R Inner Tank Pump 1 stops.

On Panel 107VU:

- the trip/RESET button on GFI (36QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the R Inner Tank Pump 1

P/BSW (20QA) comes on.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 1 P/BSW (20QA).

On Panel 430VU:

- the FAULT legend lamp on the R Inner Tank Pump 1

P/BSW (20QA) goes off.

- OFF legend lamp on the R Inner Tank Pump 1 P/BSW

(20QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the R Inner Tank Pump

1 GFI (36QA) until it latches in.

- R Inner Tank Pump 1 GFI (36QA) reset.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the R Inner Tank Pump 1 P/BSW

(20QA) comes on.

Table 2 - Operational Test Procedure - 36QA R Inner Tank Pump 1

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

L Inner Tank Pump 1 pushbutton switch

(P/BSW) (25QA) comes on.

- L Inner Tank Pump 1 Selected OFF.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the L Inner Tank Pump 1 P/BSW

(25QA) comes on.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 78

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the L

Inner Tank Pump 1 GFI (41QA).

- L Inner Tank Pump 1 stops.

On Panel 107VU:

- the trip/RESET button on GFI (41QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the L Inner Tank Pump 1

P/BSW (25QA) comes on.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 1 P/BSW (25QA).

On Panel 430VU:

- the FAULT legend lamp on the L Inner Tank Pump 1

P/BSW (25QA) goes off.

- OFF legend lamp on the L Inner Tank Pump 1 P/BSW

(25QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the L Inner Tank Pump

1 GFI (41QA) until it latches in.

- L Inner Tank Pump 1 GFI (41QA) reset.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the L Inner Tank Pump 1 P/BSW

(25QA) comes on.

Table 3 - Operational Test Procedure - 41QA L Inner Tank Pump 1

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

R Inner Tank Pump 2 pushbutton switch

(P/BSW) (26QA) comes on.

- R Inner Tank Pump 2 Selected OFF.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the R Inner Tank Pump 2 P/BSW

(26QA) comes on.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 79

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the R

Inner Tank Pump 2 GFI (42QA).

- R Inner Tank Pump 2 stops.

On Panel 107VU:

- the trip/RESET button on GFI (42QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the R Inner Tank Pump 2

P/BSW (26QA) comes on.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 2 P/BSW (26QA).

On Panel 430VU:

- the FAULT legend lamp on the R Inner Tank Pump 2

P/BSW (26QA) goes off.

- OFF legend lamp on the R Inner Tank Pump 2 P/BSW

(26QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the R Inner Tank Pump

2 GFI (42QA) until it latches in.

- R Inner Tank Pump 2 GFI (42QA) reset.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the R Inner Tank Pump 2 P/BSW

(26QA) comes on.

Table 4 - Operational Test Procedure - 42QA R Inner Tank Pump 2

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

L Center Tank Pump pushbutton switch

(P/BSW) (93QA) comes on.

- L Center Tank Pump Selected OFF.

On Panel 430VU:

- Press (Select in) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump stops.

On Panel 430VU:

- OFF legend lamp on the L Center Tank Pump P/BSW

(93QA) comes on.

On Panel 430VU:

- Press (Select in) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 80

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the L

Center Tank Pump GFI (109QA).

- L Center Tank Pump stops.

On Panel 107VU:

- the trip/RESET button on GFI (109QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the L Center Tank Pump

P/BSW (93QA) comes on.

On Panel 430VU:

- Press (Release out) the L Center Tank

Pump P/BSW (93QA).

On Panel 430VU:

- the FAULT legend lamp on the L Center Tank Pump

P/BSW (93QA) goes off.

- OFF legend lamp on the L Center Tank Pump P/BSW

(93QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the L Center Tank

Pump GFI (109QA) until it latches in.

- L Center Tank Pump GFI (109QA) reset.

On Panel 430VU:

- Press (Select in) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump stops.

On Panel 430VU:

- OFF legend lamp on the L Center Tank Pump P/BSW

(93QA) comes on.

Table 5 - Operational Test Procedure - 109QA L Center Tank Pump

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

R Center Tank Pump pushbutton switch

(P/BSW) (94QA) comes on.

- R Center Tank Pump Selected OFF.

On Panel 430VU:

- Press (Select in) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump stops.

On Panel 430VU:

- OFF legend lamp on the R Center Tank Pump P/BSW

(94QA) comes on.

On Panel 430VU:

- Press (Select in) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 81

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the R

Center Tank Pump GFI (110QA).

- R Center Tank Pump stops.

On Panel 107VU:

- the trip/RESET button on GFI (110QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the R Center Tank Pump

P/BSW (94QA) comes on.

On Panel 430VU:

- Press (Release out) the R Center Tank

Pump P/BSW (94QA).

On Panel 430VU:

- the FAULT legend lamp on the R Center Tank Pump

P/BSW (94QA) goes off.

- OFF legend lamp on the R Center Tank Pump P/BSW

(94QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the R Center Tank

Pump GFI (110QA) until it latches in.

- R Center Tank Pump GFI (110QA) reset.

On Panel 430VU:

- Press (Select in) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump stops.

On Panel 430VU:

- OFF legend lamp on the R Center Tank Pump P/BSW

(94QA) comes on.

Table 6 - Operational Test Procedure - 110QA R Center Tank Pump

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

FUEL/TRIM TK Pump 1 pushbutton

switch (P/BSW) (7QN) comes on.

- FUEL/TRIM TK Pump 1 Selected OFF.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

- FUEL/TRIM TK Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

- FUEL/TRIM TK Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the FUEL/TRIM TK Pump 1 P/BSW

(7QN) comes on.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

- FUEL/TRIM TK Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 82

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the

FUEL/TRIM TK Pump 1 GFI (9QN).

- FUEL/TRIM TK Pump 1 stops.

On Panel 107VU:

- the trip/RESET button on GFI (9QN) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the FUEL/TRIM TK Pump 1

P/BSW (7QN) comes on.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

On Panel 430VU:

- the FAULT legend lamp on the FUEL/TRIM TK Pump 1

P/BSW (7QN) goes off.

- OFF legend lamp on the FUEL/TRIM TK Pump 1 P/BSW

(7QN) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the FUEL/TRIM TK

Pump 1 GFI (9QN) until it latches in.

- FUEL/TRIM TK Pump 1 GFI (9QN) reset.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

- FUEL/TRIM TK Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

- FUEL/TRIM TK Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the FUEL/TRIM TK Pump 1 P/BSW

(7QN) comes on.

Table 7 - Operational Test Procedure - 9QN Transfer Control Pump 1

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

FUEL/TRIM TK Pump 2 pushbutton

switch (P/BSW) (8QN) comes on.

- FUEL/TRIM TK Pump 2 Selected OFF.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

- FUEL/TRIM TK Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

- FUEL/TRIM TK Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the FUEL/TRIM TK Pump 2 P/BSW

(8QN) comes on.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

- FUEL/TRIM TK Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 83

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the

FUEL/TRIM TK Pump 2 GFI (10QN).

- FUEL/TRIM TK Pump 2 stops.

On Panel 107VU:

- the trip/RESET button on GFI (10QN) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the FUEL/TRIM TK Pump 2

P/BSW (8QN) comes on.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

On Panel 430VU:

- the FAULT legend lamp on the FUEL/TRIM TK Pump 2

P/BSW (8QN) goes off.

- OFF legend lamp on the FUEL/TRIM TK Pump 2 P/BSW

(8QN) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the FUEL/TRIM TK

Pump 2 GFI (10QN) until it latches in.

- FUEL/TRIM TK Pump 2 GFI (10QN) reset.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

- FUEL/TRIM TK Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

- FUEL/TRIM TK Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the FUEL/TRIM TK Pump 2 P/BSW

(8QN) comes on.

Table 8 - Operational Test Procedure - 10QN Transfer Control Pump 2

**CONF 003

(1) Subtask 286104-840-401-002 - Preparation for Test Procedure

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 12-11-28, Page Block 301

Fig. A-UBAAA

Ground Fault Interrupter - Tripped/Not

Tripped

Sheet 01

(a) Refer to Fig. A-UBAAA Sheet 01

1 Inspect the GFI 35QA, 36QA, 41QA, 42QA, 109QA, 110QA, 9QN and 10QN

and make sure that it is in the reset (non-tripped) state (metal shaft is not

seen on the trip/reset plunger).

2 If the GFI 35QA, 36QA, 41QA, 42QA, 109QA, 110QA, 9QN and 10QN is

tripped (metal shaft is seen on the trip/reset plunger) then reset by depressing

the trip/reset plunger until it latches in.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 84

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

3 Make sure that the left and right inner tanks and the center tank contains a

minimum of 500 Kg (1,102 lb) of fuel. If necessary, refuel the tanks (Refer to

AMM 12-11-28, Page Block 301).

(2) Subtask 286104-700-001-003 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-50-10, Page Block 001

24-50-20, Page Block 001

24-50-40, Page Block 001

28-21-12, Page Block 501

28-21-36, Page Block 401

28-27-00, Page Block 501

(a) Remove the safety clip(s) and/or tag(s) and close/unlock these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/CTL

3QN (1)

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/WARN

5QN (1)

101VU FUEL/L INNER TK/PUMP

2/SUPPLY

1QA (1)

101VU FUEL/R INNER TK/PUMP

1/SUPPLY

2QA (1)

101VU FUEL/L INNER TK/PUMP

1/SUPPLY

7QA (1)

101VU FUEL/R INNER TK/PUMP

2/SUPPLY

8QA (1)

101VU FUEL/CTR

TK/L/PUMP/SUPPLY

99QA (1)

101VU FUEL/CTR

TK/R/PUMP/SUPPLY

100QA (1)

101VU FUEL/TRIM TANK/PUMP

1/SUPPLY

1QN (1)

101VU FUEL/TRIM TK/PUMP

2/SUPPLY

2QN (1)

128VU FUEL/TRIM TK/XFR PUMP

2/CTL

4QN (1)

128VU FUEL/TRIM TK/XFR PUMP

2/WARN

6QN (1)

128VU FUEL/L INR TK/PUMP

2/WARN

11QA (1)

128VU FUEL/R INR TK/PUMP

1/WARN

12QA (1)

128VU FUEL/L INR TK/PUMP

1/WARN

17QA (1)

128VU FUEL/R INR TK/PUMP

2/WARN

18QA (1)

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 85

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE

NOTES

128VU FUEL/L INR TK/PUMP 2/CTL 59QA (1)

128VU FUEL/R INR TK/PUMP 1/CTL 60QA (1)

128VU FUEL/CTR TK/L/PUMP/CTL 63QA (1)

128VU FUEL/CTR TK/R/PUMP/CTL 64QA (1)

128VU FUEL/L INR TK/PUMP 1/CTL 69QA (1)

128VU FUEL/R INR TK/PUMP 2/CTL 70QA (1)

128VU FUEL/CTR

TK/L/PUMP/WARN

101QA (1)

128VU FUEL/CTR

TK/R/PUMP/WARN

102QA (1)

or

PANEL DESIGNATION FIN LOCATION SEE

NOTES

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/CTL

3QN (1)

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/WARN

5QN (1)

101VU FUEL/L INNER TK/PUMP

2/SUPPLY

1QA (1)

101VU FUEL/R INNER TK/PUMP

1/SUPPLY

2QA (1)

101VU FUEL/L INNER TK/PUMP

1/SUPPLY

7QA (1)

101VU FUEL/R INNER TK/PUMP

2/SUPPLY

8QA (1)

101VU FUEL/CTR

TK/L/PUMP/SUPPLY

99QA (1)

101VU FUEL/CTR

TK/R/PUMP/SUPPLY

100QA (1)

101VU FUEL/TRIM TANK/PUMP

1/SUPPLY

1QN (1)

101VU FUEL/TRIM TK/PUMP

2/SUPPLY

2QN (1)

132VU FUEL/TRIM TK/XFR PUMP

2/CTL

4QN (1)

132VU FUEL/TRIM TK/XFR PUMP

2/WARN

6QN (1)

132VU FUEL/L INR TK/PUMP

2/WARN

11QA (1)

132VU FUEL/R INR TK/PUMP

1/WARN

12QA (1)

132VU FUEL/L INR TK/PUMP

1/WARN

17QA (1)

132VU FUEL/R INR TK/PUMP

2/WARN

18QA (1)

132VU FUEL/L INR TK/PUMP 2/CTL 59QA (1)

132VU FUEL/R INR TK/PUMP 1/CTL 60QA (1)

132VU FUEL/CTR TK/L/PUMP/CTL 63QA (1)

132VU FUEL/CTR TK/R/PUMP/CTL 64QA (1)

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 86

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE

NOTES

132VU FUEL/L INR TK/PUMP 1/CTL 69QA (1)

132VU FUEL/R INR TK/PUMP 2/CTL 70QA (1)

132VU FUEL/CTR

TK/L/PUMP/WARN

101QA (1)

132VU FUEL/CTR

TK/R/PUMP/WARN

102QA (1)

NOTE (1): For the location of the circuit breakers, refer to AMM 24-50-10,

Page Block 001, AMM 24-50-20, Page Block 001 and AMM

24-50-40, Page Block 001.

(b) Do the operational test of the Inner Tanks Booster Pumps (Refer to AMM 28-21-12,

Page Block 501).

(c) Do the test procedure as specified after the installation of the center tank booster

pumps (81QA, 82QA) (Refer to AMM 28-21-36, Page Block 401).

(d) Do the operational test of the Trim Tank Pumps (Refer to AMM 28-27-00, Page

Block 501).

(3) Subtask 286104-710-401-002 - Operational Test

Work Zones and Access Panels

Zone Access/Work location

121 Work location 107VU 35-QA

107VU 36-QA

107VU 41-QA

107VU 42-QA

107VU 109-QA

107VU 110-QA

107VU 9-QN

107VU 10-QN

Manpower Resources

Skills ELECTRICAL

WARNING: ACCIDENTAL REARWARD FUEL TRANSFER CAN MOVE THE C OF

G AFT OF SAFE LIMIT. MAKE SURE TRIM TANK VALVES ARE SHUT.

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

L Inner Tank Pump 2 pushbutton switch

(P/BSW) (19QA) comes on.

- L Inner Tank Pump 2 Selected OFF.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 2 P/BSW (19 QA).

- L Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 87

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 2 P/BSW (19QA).

- L Inner Tank Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the L Inner Tank Pump 2 P/BSW

(19QA) comes on.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 2 P/BSW (19QA).

- L Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 107VU:

- Press the test button on top of the L

Inner Tank Pump 2 GFI (35QA).

- L Inner Tank Pump 2 stops.

On Panel 107VU:

- the trip/RESET button on GFI (35QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the L Inner Tank Pump 2

P/BSW (19QA) comes on.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 2 P/BSW (19QA).

On Panel 430VU:

- the FAULT legend lamp on the L Inner Tank Pump 2

P/BSW (19QA) goes off.

- OFF legend lamp on the L Inner Tank Pump 2 P/BSW

(19QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the L Inner Tank Pump

2 GFI (35QA) until it latches in.

- L Inner Tank Pump 2 GFI (35QA) reset.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 2 P/BSW (19QA).

- L Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 2 P/BSW (19QA).

- L Inner Tank Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the L Inner Tank Pump 2 P/BSW

(19QA) comes on.

Table 1 - Operational Test Procedure - 35QA L Inner Tank Pump 2

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

R Inner Tank Pump 1 pushbutton switch

(P/BSW) (20QA) comes on.

- R Inner Tank Pump 1 Selected OFF.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the R Inner Tank Pump 1 P/BSW

(20QA) comes on.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 88

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 107VU:

- Press the test button on top of the R

Inner Tank Pump 1 GFI (36QA).

- R Inner Tank Pump 1 stops.

On Panel 107VU:

- the trip/RESET button on GFI (36QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the R Inner Tank Pump 1

P/BSW (20QA) comes on.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 1 P/BSW (20QA).

On Panel 430VU:

- the FAULT legend lamp on the R Inner Tank Pump 1

P/BSW (20QA) goes off.

- OFF legend lamp on the R Inner Tank Pump 1 P/BSW

(20QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the R Inner Tank Pump

1 GFI (36QA) until it latches in.

- R Inner Tank Pump 1 GFI (36QA) reset.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the R Inner Tank Pump 1 P/BSW

(20QA) comes on.

Table 2 - Operational Test Procedure - 36QA R Inner Tank Pump 1

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

L Inner Tank Pump 1 pushbutton switch

(P/BSW) (25QA) comes on.

- L Inner Tank Pump 1 Selected OFF.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the L Inner Tank Pump 1 P/BSW

(25QA) comes on.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 89

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the L

Inner Tank Pump 1 GFI (41QA).

- L Inner Tank Pump 1 stops.

On Panel 107VU:

- the trip/RESET button on GFI (41QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the L Inner Tank Pump 1

P/BSW (25QA) comes on.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 1 P/BSW (25QA).

On Panel 430VU:

- the FAULT legend lamp on the L Inner Tank Pump 1

P/BSW (25QA) goes off.

- OFF legend lamp on the L Inner Tank Pump 1 P/BSW

(25QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the L Inner Tank Pump

1 GFI (41QA) until it latches in.

- L Inner Tank Pump 1 GFI (41QA) reset.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the L Inner Tank Pump 1 P/BSW

(25QA) comes on.

Table 3 - Operational Test Procedure - 41QA L Inner Tank Pump 1

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

R Inner Tank Pump 2 pushbutton switch

(P/BSW) (26QA) comes on.

- R Inner Tank Pump 2 Selected OFF.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the R Inner Tank Pump 2 P/BSW

(26QA) comes on.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 90

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the R

Inner Tank Pump 2 GFI (42QA).

- R Inner Tank Pump 2 stops.

On Panel 107VU:

- the trip/RESET button on GFI (42QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the R Inner Tank Pump 2

P/BSW (26QA) comes on.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 2 P/BSW (26QA).

On Panel 430VU:

- the FAULT legend lamp on the R Inner Tank Pump 2

P/BSW (26QA) goes off.

- OFF legend lamp on the R Inner Tank Pump 2 P/BSW

(26QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the R Inner Tank Pump

2 GFI (42QA) until it latches in.

- R Inner Tank Pump 2 GFI (42QA) reset.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the R Inner Tank Pump 2 P/BSW

(26QA) comes on.

Table 4 - Operational Test Procedure - 42QA R Inner Tank Pump 2

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

L Center Tank Pump pushbutton switch

(P/BSW) (93QA) comes on.

- L Center Tank Pump Selected OFF.

On Panel 430VU:

- Press (Select in) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump stops.

On Panel 430VU:

- OFF legend lamp on the L Center Tank Pump P/BSW

(93QA) comes on.

On Panel 430VU:

- Press (Select in) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 91

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the L

Center Tank Pump GFI (109QA).

- L Center Tank Pump stops.

On Panel 107VU:

- the trip/RESET button on GFI (109QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the L Center Tank Pump

P/BSW (93QA) comes on.

On Panel 430VU:

- Press (Release out) the L Center Tank

Pump P/BSW (93QA).

On Panel 430VU:

- the FAULT legend lamp on the L Center Tank Pump

P/BSW (93QA) goes off.

- OFF legend lamp on the L Center Tank Pump P/BSW

(93QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the L Center Tank

Pump GFI (109QA) until it latches in.

- L Center Tank Pump GFI (109QA) reset.

On Panel 430VU:

- Press (Select in) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump stops.

On Panel 430VU:

- OFF legend lamp on the L Center Tank Pump P/BSW

(93QA) comes on.

Table 5 - Operational Test Procedure - 109QA L Center Tank Pump

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

R Center Tank Pump pushbutton switch

(P/BSW) (94QA) comes on.

- R Center Tank Pump Selected OFF.

On Panel 430VU:

- Press (Select in) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump stops.

On Panel 430VU:

- OFF legend lamp on the R Center Tank Pump P/BSW

(94QA) comes on.

On Panel 430VU:

- Press (Select in) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 92

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the R

Center Tank Pump GFI (110QA).

- R Center Tank Pump stops.

On Panel 107VU:

- the trip/RESET button on GFI (110QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the R Center Tank Pump

P/BSW (94QA) comes on.

On Panel 430VU:

- Press (Release out) the R Center Tank

Pump P/BSW (94QA).

On Panel 430VU:

- the FAULT legend lamp on the R Center Tank Pump

P/BSW (94QA) goes off.

- OFF legend lamp on the R Center Tank Pump P/BSW

(94QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the R Center Tank

Pump GFI (110QA) until it latches in.

- R Center Tank Pump GFI (110QA) reset.

On Panel 430VU:

- Press (Select in) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump stops.

On Panel 430VU:

- OFF legend lamp on the R Center Tank Pump P/BSW

(94QA) comes on.

Table 6 - Operational Test Procedure - 110QA R Center Tank Pump

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

FUEL/TRIM TK Pump 1 pushbutton

switch (P/BSW) (7QN) comes on.

- FUEL/TRIM TK Pump 1 Selected OFF.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

- FUEL/TRIM TK Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

- FUEL/TRIM TK Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the FUEL/TRIM TK Pump 1 P/BSW

(7QN) comes on.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

- FUEL/TRIM TK Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 93

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the

FUEL/TRIM TK Pump 1 GFI (9QN).

- FUEL/TRIM TK Pump 1 stops.

On Panel 107VU:

- the trip/RESET button on GFI (9QN) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the FUEL/TRIM TK Pump 1

P/BSW (7QN) comes on.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

On Panel 430VU:

- the FAULT legend lamp on the FUEL/TRIM TK Pump 1

P/BSW (7QN) goes off.

- OFF legend lamp on the FUEL/TRIM TK Pump 1 P/BSW

(7QN) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the FUEL/TRIM TK

Pump 1 GFI (9QN) until it latches in.

- FUEL/TRIM TK Pump 1 GFI (9QN) reset.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

- FUEL/TRIM TK Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

- FUEL/TRIM TK Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the FUEL/TRIM TK Pump 1 P/BSW

(7QN) comes on.

Table 7 - Operational Test Procedure - 9QN Transfer Control Pump 1

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

FUEL/TRIM TK Pump 2 pushbutton

switch (P/BSW) (8QN) comes on.

- FUEL/TRIM TK Pump 2 Selected OFF.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

- FUEL/TRIM TK Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

- FUEL/TRIM TK Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the FUEL/TRIM TK Pump 2 P/BSW

(8QN) comes on.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

- FUEL/TRIM TK Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 94

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the

FUEL/TRIM TK Pump 2 GFI (10QN).

- FUEL/TRIM TK Pump 2 stops.

On Panel 107VU:

- the trip/RESET button on GFI (10QN) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the FUEL/TRIM TK Pump 2

P/BSW (8QN) comes on.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

On Panel 430VU:

- the FAULT legend lamp on the FUEL/TRIM TK Pump 2

P/BSW (8QN) goes off.

- OFF legend lamp on the FUEL/TRIM TK Pump 2 P/BSW

(8QN) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the FUEL/TRIM TK

Pump 2 GFI (10QN) until it latches in.

- FUEL/TRIM TK Pump 2 GFI (10QN) reset.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

- FUEL/TRIM TK Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

- FUEL/TRIM TK Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the FUEL/TRIM TK Pump 2 P/BSW

(8QN) comes on.

Table 8 - Operational Test Procedure - 10QN Transfer Control Pump 2

**CONF 004

(1) Subtask 286104-840-401-002 - Preparation for Test Procedure

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) 12-11-28, Page Block 301

Fig. A-UBAAA

Ground Fault Interrupter - Tripped/Not

Tripped

Sheet 01

(a) Refer to Fig. A-UBAAA Sheet 01

1 Inspect the GFI 35QA, 36QA, 41QA, 42QA, 109QA, 110QA, 9QN and 10QN

and make sure that it is in the reset (non-tripped) state (metal shaft is not

seen on the trip/reset plunger).

2 If the GFI 35QA, 36QA, 41QA, 42QA, 109QA, 110QA, 9QN and 10QN is

tripped (metal shaft is seen on the trip/reset plunger) then reset by depressing

the trip/reset plunger until it latches in.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 95

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

3 Make sure that the left and right inner tanks and the center tank contains a

minimum of 500 Kg (1,102 lb) of fuel. If necessary, refuel the tanks (Refer to

AMM 12-11-28, Page Block 301).

(2) Subtask 286104-700-001-003 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 24-50-10, Page Block 001

24-50-20, Page Block 001

24-50-40, Page Block 001

28-21-12, Page Block 501

28-21-36, Page Block 401

28-27-00, Page Block 501

(a) Remove the safety clip(s) and/or tag(s) and close/unlock these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/CTL

3QN (1)

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/WARN

5QN (1)

101VU FUEL/L INNER TK/PUMP

2/SUPPLY

1QA (1)

101VU FUEL/R INNER TK/PUMP

1/SUPPLY

2QA (1)

101VU FUEL/L INNER TK/PUMP

1/SUPPLY

7QA (1)

101VU FUEL/R INNER TK/PUMP

2/SUPPLY

8QA (1)

101VU FUEL/CTR

TK/L/PUMP/SUPPLY

99QA (1)

101VU FUEL/CTR

TK/R/PUMP/SUPPLY

100QA (1)

101VU FUEL/TRIM TANK/PUMP

1/SUPPLY

1QN (1)

101VU FUEL/TRIM TK/PUMP

2/SUPPLY

2QN (1)

128VU FUEL/TRIM TK/XFR PUMP

2/CTL

4QN (1)

128VU FUEL/TRIM TK/XFR PUMP

2/WARN

6QN (1)

128VU FUEL/L INR TK/PUMP

2/WARN

11QA (1)

128VU FUEL/R INR TK/PUMP

1/WARN

12QA (1)

128VU FUEL/L INR TK/PUMP

1/WARN

17QA (1)

128VU FUEL/R INR TK/PUMP

2/WARN

18QA (1)

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 96

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE

NOTES

128VU FUEL/L INR TK/PUMP 2/CTL 59QA (1)

128VU FUEL/R INR TK/PUMP 1/CTL 60QA (1)

128VU FUEL/CTR TK/L/PUMP/CTL 63QA (1)

128VU FUEL/CTR TK/R/PUMP/CTL 64QA (1)

128VU FUEL/L INR TK/PUMP 1/CTL 69QA (1)

128VU FUEL/R INR TK/PUMP 2/CTL 70QA (1)

128VU FUEL/CTR

TK/L/PUMP/WARN

101QA (1)

128VU FUEL/CTR

TK/R/PUMP/WARN

102QA (1)

or

PANEL DESIGNATION FIN LOCATION SEE

NOTES

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/CTL

3QN (1)

22VU FUEL/TRIM TK/FWD

XFR/PUMP 1/WARN

5QN (1)

101VU FUEL/L INNER TK/PUMP

2/SUPPLY

1QA (1)

101VU FUEL/R INNER TK/PUMP

1/SUPPLY

2QA (1)

101VU FUEL/L INNER TK/PUMP

1/SUPPLY

7QA (1)

101VU FUEL/R INNER TK/PUMP

2/SUPPLY

8QA (1)

101VU FUEL/CTR

TK/L/PUMP/SUPPLY

99QA (1)

101VU FUEL/CTR

TK/R/PUMP/SUPPLY

100QA (1)

101VU FUEL/TRIM TANK/PUMP

1/SUPPLY

1QN (1)

101VU FUEL/TRIM TK/PUMP

2/SUPPLY

2QN (1)

132VU FUEL/TRIM TK/XFR PUMP

2/CTL

4QN (1)

132VU FUEL/TRIM TK/XFR PUMP

2/WARN

6QN (1)

132VU FUEL/L INR TK/PUMP

2/WARN

11QA (1)

132VU FUEL/R INR TK/PUMP

1/WARN

12QA (1)

132VU FUEL/L INR TK/PUMP

1/WARN

17QA (1)

132VU FUEL/R INR TK/PUMP

2/WARN

18QA (1)

132VU FUEL/L INR TK/PUMP 2/CTL 59QA (1)

132VU FUEL/R INR TK/PUMP 1/CTL 60QA (1)

132VU FUEL/CTR TK/L/PUMP/CTL 63QA (1)

132VU FUEL/CTR TK/R/PUMP/CTL 64QA (1)

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 97

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE

NOTES

132VU FUEL/L INR TK/PUMP 1/CTL 69QA (1)

132VU FUEL/R INR TK/PUMP 2/CTL 70QA (1)

132VU FUEL/CTR

TK/L/PUMP/WARN

101QA (1)

132VU FUEL/CTR

TK/R/PUMP/WARN

102QA (1)

NOTE (1): For the location of the circuit breakers, refer to AMM 24-50-10,

Page Block 001, AMM 24-50-20, Page Block 001 and AMM

24-50-40, Page Block 001.

(b) Do the operational test of the Inner Tanks Booster Pumps (Refer to AMM 28-21-12,

Page Block 501).

(c) Do the test procedure as specified after the installation of the center tank booster

pumps (81QA, 82QA) (Refer to AMM 28-21-36, Page Block 401).

(d) Do the operational test of the Trim Tank Pumps (Refer to AMM 28-27-00, Page

Block 501).

(3) Subtask 286104-710-401-002 - Operational Test

Work Zones and Access Panels

Zone Access/Work location

121 Work location 107VU 35-QA

107VU 36-QA

107VU 41-QA

107VU 42-QA

107VU 109-QA

107VU 110-QA

107VU 9-QN

107VU 10-QN

Manpower Resources

Skills ELECTRICAL

WARNING: ACCIDENTAL REARWARD FUEL TRANSFER CAN MOVE THE C OF

G AFT OF SAFE LIMIT. MAKE SURE TRIM TANK VALVES ARE SHUT.

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

L Inner Tank Pump 2 pushbutton switch

(P/BSW) (19QA) comes on.

- L Inner Tank Pump 2 Selected OFF.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 2 P/BSW (19 QA).

- L Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 98

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 2 P/BSW (19QA).

- L Inner Tank Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the L Inner Tank Pump 2 P/BSW

(19QA) comes on.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 2 P/BSW (19QA).

- L Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 107VU:

- Press the test button on top of the L

Inner Tank Pump 2 GFI (35QA).

- L Inner Tank Pump 2 stops.

On Panel 107VU:

- the trip/RESET button on GFI (35QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the L Inner Tank Pump 2

P/BSW (19QA) comes on.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 2 P/BSW (19QA).

On Panel 430VU:

- the FAULT legend lamp on the L Inner Tank Pump 2

P/BSW (19QA) goes off.

- OFF legend lamp on the L Inner Tank Pump 2 P/BSW

(19QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the L Inner Tank Pump

2 GFI (35QA) until it latches in.

- L Inner Tank Pump 2 GFI (35QA) reset.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 2 P/BSW (19QA).

- L Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 2 P/BSW (19QA).

- L Inner Tank Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the L Inner Tank Pump 2 P/BSW

(19QA) comes on.

Table 1 - Operational Test Procedure - 35QA L Inner Tank Pump 2

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

R Inner Tank Pump 1 pushbutton switch

(P/BSW) (20QA) comes on.

- R Inner Tank Pump 1 Selected OFF.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the R Inner Tank Pump 1 P/BSW

(20QA) comes on.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 99

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 107VU:

- Press the test button on top of the R

Inner Tank Pump 1 GFI (36QA).

- R Inner Tank Pump 1 stops.

On Panel 107VU:

- the trip/RESET button on GFI (36QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the R Inner Tank Pump 1

P/BSW (20QA) comes on.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 1 P/BSW (20QA).

On Panel 430VU:

- the FAULT legend lamp on the R Inner Tank Pump 1

P/BSW (20QA) goes off.

- OFF legend lamp on the R Inner Tank Pump 1 P/BSW

(20QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the R Inner Tank Pump

1 GFI (36QA) until it latches in.

- R Inner Tank Pump 1 GFI (36QA) reset.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 1 P/BSW (20QA).

- R Inner Tank Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the R Inner Tank Pump 1 P/BSW

(20QA) comes on.

Table 2 - Operational Test Procedure - 36QA R Inner Tank Pump 1

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

L Inner Tank Pump 1 pushbutton switch

(P/BSW) (25QA) comes on.

- L Inner Tank Pump 1 Selected OFF.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the L Inner Tank Pump 1 P/BSW

(25QA) comes on.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 100

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the L

Inner Tank Pump 1 GFI (41QA).

- L Inner Tank Pump 1 stops.

On Panel 107VU:

- the trip/RESET button on GFI (41QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the L Inner Tank Pump 1

P/BSW (25QA) comes on.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 1 P/BSW (25QA).

On Panel 430VU:

- the FAULT legend lamp on the L Inner Tank Pump 1

P/BSW (25QA) goes off.

- OFF legend lamp on the L Inner Tank Pump 1 P/BSW

(25QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the L Inner Tank Pump

1 GFI (41QA) until it latches in.

- L Inner Tank Pump 1 GFI (41QA) reset.

On Panel 430VU:

- Press (Select in) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Inner Tank

Pump 1 P/BSW (25QA).

- L Inner Tank Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the L Inner Tank Pump 1 P/BSW

(25QA) comes on.

Table 3 - Operational Test Procedure - 41QA L Inner Tank Pump 1

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

R Inner Tank Pump 2 pushbutton switch

(P/BSW) (26QA) comes on.

- R Inner Tank Pump 2 Selected OFF.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the R Inner Tank Pump 2 P/BSW

(26QA) comes on.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 101

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the R

Inner Tank Pump 2 GFI (42QA).

- R Inner Tank Pump 2 stops.

On Panel 107VU:

- the trip/RESET button on GFI (42QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the R Inner Tank Pump 2

P/BSW (26QA) comes on.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 2 P/BSW (26QA).

On Panel 430VU:

- the FAULT legend lamp on the R Inner Tank Pump 2

P/BSW (26QA) goes off.

- OFF legend lamp on the R Inner Tank Pump 2 P/BSW

(26QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the R Inner Tank Pump

2 GFI (42QA) until it latches in.

- R Inner Tank Pump 2 GFI (42QA) reset.

On Panel 430VU:

- Press (Select in) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Inner Tank

Pump 2 P/BSW (26QA).

- R Inner Tank Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the R Inner Tank Pump 2 P/BSW

(26QA) comes on.

Table 4 - Operational Test Procedure - 42QA R Inner Tank Pump 2

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

L Center Tank Pump pushbutton switch

(P/BSW) (93QA) comes on.

- L Center Tank Pump Selected OFF.

On Panel 430VU:

- Press (Select in) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump stops.

On Panel 430VU:

- OFF legend lamp on the L Center Tank Pump P/BSW

(93QA) comes on.

On Panel 430VU:

- Press (Select in) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 102

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the L

Center Tank Pump GFI (109QA).

- L Center Tank Pump stops.

On Panel 107VU:

- the trip/RESET button on GFI (109QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the L Center Tank Pump

P/BSW (93QA) comes on.

On Panel 430VU:

- Press (Release out) the L Center Tank

Pump P/BSW (93QA).

On Panel 430VU:

- the FAULT legend lamp on the L Center Tank Pump

P/BSW (93QA) goes off.

- OFF legend lamp on the L Center Tank Pump P/BSW

(93QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the L Center Tank

Pump GFI (109QA) until it latches in.

- L Center Tank Pump GFI (109QA) reset.

On Panel 430VU:

- Press (Select in) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the L Center Tank

Pump P/BSW (93QA).

- L Center Tank Pump stops.

On Panel 430VU:

- OFF legend lamp on the L Center Tank Pump P/BSW

(93QA) comes on.

Table 5 - Operational Test Procedure - 109QA L Center Tank Pump

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

R Center Tank Pump pushbutton switch

(P/BSW) (94QA) comes on.

- R Center Tank Pump Selected OFF.

On Panel 430VU:

- Press (Select in) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump stops.

On Panel 430VU:

- OFF legend lamp on the R Center Tank Pump P/BSW

(94QA) comes on.

On Panel 430VU:

- Press (Select in) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 103

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the R

Center Tank Pump GFI (110QA).

- R Center Tank Pump stops.

On Panel 107VU:

- the trip/RESET button on GFI (110QA) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the R Center Tank Pump

P/BSW (94QA) comes on.

On Panel 430VU:

- Press (Release out) the R Center Tank

Pump P/BSW (94QA).

On Panel 430VU:

- the FAULT legend lamp on the R Center Tank Pump

P/BSW (94QA) goes off.

- OFF legend lamp on the R Center Tank Pump P/BSW

(94QA) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the R Center Tank

Pump GFI (110QA) until it latches in.

- R Center Tank Pump GFI (110QA) reset.

On Panel 430VU:

- Press (Select in) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the R Center Tank

Pump P/BSW (94QA).

- R Center Tank Pump stops.

On Panel 430VU:

- OFF legend lamp on the R Center Tank Pump P/BSW

(94QA) comes on.

Table 6 - Operational Test Procedure - 110QA R Center Tank Pump

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

FUEL/TRIM TK Pump 1 pushbutton

switch (P/BSW) (7QN) comes on.

- FUEL/TRIM TK Pump 1 Selected OFF.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

- FUEL/TRIM TK Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

- FUEL/TRIM TK Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the FUEL/TRIM TK Pump 1 P/BSW

(7QN) comes on.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

- FUEL/TRIM TK Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 104

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the

FUEL/TRIM TK Pump 1 GFI (9QN).

- FUEL/TRIM TK Pump 1 stops.

On Panel 107VU:

- the trip/RESET button on GFI (9QN) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the FUEL/TRIM TK Pump 1

P/BSW (7QN) comes on.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

On Panel 430VU:

- the FAULT legend lamp on the FUEL/TRIM TK Pump 1

P/BSW (7QN) goes off.

- OFF legend lamp on the FUEL/TRIM TK Pump 1 P/BSW

(7QN) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the FUEL/TRIM TK

Pump 1 GFI (9QN) until it latches in.

- FUEL/TRIM TK Pump 1 GFI (9QN) reset.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

- FUEL/TRIM TK Pump 1 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 1 P/BSW (7QN).

- FUEL/TRIM TK Pump 1 stops.

On Panel 430VU:

- OFF legend lamp on the FUEL/TRIM TK Pump 1 P/BSW

(7QN) comes on.

Table 7 - Operational Test Procedure - 9QN Transfer Control Pump 1

ACTION RESULT

On Panel 430VU:

- Check that the OFF legend lamp on the

FUEL/TRIM TK Pump 2 pushbutton

switch (P/BSW) (8QN) comes on.

- FUEL/TRIM TK Pump 2 Selected OFF.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

- FUEL/TRIM TK Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

- FUEL/TRIM TK Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the FUEL/TRIM TK Pump 2 P/BSW

(8QN) comes on.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

- FUEL/TRIM TK Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 105

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

ACTION RESULT

On Panel 107VU:

- Press the test button on top of the

FUEL/TRIM TK Pump 2 GFI (10QN).

- FUEL/TRIM TK Pump 2 stops.

On Panel 107VU:

- the trip/RESET button on GFI (10QN) extends revealing

the metallic shaft.

On Panel 430VU:

- the FAULT legend lamp on the FUEL/TRIM TK Pump 2

P/BSW (8QN) comes on.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

On Panel 430VU:

- the FAULT legend lamp on the FUEL/TRIM TK Pump 2

P/BSW (8QN) goes off.

- OFF legend lamp on the FUEL/TRIM TK Pump 2 P/BSW

(8QN) comes on.

On Panel 107VU:

- Press (Select in) the trip/RESET

plunger on top of the FUEL/TRIM TK

Pump 2 GFI (10QN) until it latches in.

- FUEL/TRIM TK Pump 2 GFI (10QN) reset.

On Panel 430VU:

- Press (Select in) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

- FUEL/TRIM TK Pump 2 runs.

On Panel 430VU:

- OFF legend lamp goes off

- FAULT legend lamp comes on and then goes off.

On Panel 430VU:

- Press (Release out) the FUEL/TRIM TK

Pump 2 P/BSW (8QN).

- FUEL/TRIM TK Pump 2 stops.

On Panel 430VU:

- OFF legend lamp on the FUEL/TRIM TK Pump 2 P/BSW

(8QN) comes on.

Table 8 - Operational Test Procedure - 10QN Transfer Control Pump 2

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 286104-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

52-30-00, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Close the door 132AZ (Refer to AMM 06-41-52, Page Block 001).

(c) Close the FWD Cargo-compartment door 831 (Refer to AMM 52-30-00, Page Block

001 and AMM 06-41-52, Page Block 001).

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 106

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

(d) Remove the access platform(s).

(e) Restore the system and the aircraft to the normal operating condition.

**CONF 002

(1) Subtask 286104-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

52-30-00, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Close the door 132AZ (Refer to AMM 06-41-52, Page Block 001).

(c) Close the FWD Cargo-compartment door 831 (Refer to AMM 52-30-00, Page Block

001 and AMM 06-41-52, Page Block 001).

(d) Remove the access platform(s).

(e) Restore the system and the aircraft to the normal operating condition.

**CONF 003

(1) Subtask 286104-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

52-30-00, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Close the door 132AZ (Refer to AMM 06-41-52, Page Block 001).

(c) Close the FWD Cargo-compartment door 831 (Refer to AMM 52-30-00, Page Block

001 and AMM 06-41-52, Page Block 001).

(d) Remove the access platform(s).

(e) Restore the system and the aircraft to the normal operating condition.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 107

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 004

(1) Subtask 286104-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

52-30-00, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Close the door 132AZ (Refer to AMM 06-41-52, Page Block 001).

(c) Close the FWD Cargo-compartment door 831 (Refer to AMM 52-30-00, Page Block

001 and AMM 06-41-52, Page Block 001).

(d) Remove the access platform(s).

(e) Restore the system and the aircraft to the normal operating condition.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 108

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF ALL

PLUNGER NOT TRIPPED

PLUNGER TRIPPED

GFI

TRIP/RESET

PLUNGER

107VU

GROUND FAULT

INTERRUPTER

(GFI)

TEST

BUTTON

C

B

C

B

A

D_SB_286104_7_BAAA_01_00

FR20

FR1 Z120

A

Figure A-UBAAA - Sheet 01

Ground Fault Interrupter - Tripped/Not Tripped

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 109

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 001

FR20

FR1 Z120

36QA

41QA

42QA

109QA

110QA

35QA

D_SB_286104_5_BAAA_01_00

107VU

Figure A-FBAAA - Sheet 01

Location of the Modification

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 110

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002 thru 004

FR20

FR1 Z120

36QA

41QA

42QA

109QA

110QA

35QA

9QN

10QN

107VU

D_SB_286104_5_BAAB_01_00

Figure A-FBAAB - Sheet 01

Location of the Modification

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 111

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 001

(5)

(2)

(3)

(1)

(4)

(3 POS)

(3 POS)

(3 POS)

(3 POS)

(3 POS)

(3 POS)

2

1

5

4

3

B C

B C

B C

B C

B C

B C

110QA

42QA

41QA

109QA

35QA

36QA

107VU

A

BEFORE AFTER

B C

FR20

FR1 Z120

A

D_SB_286104_5_BBAA_01_00

Figure A-FBBAA - Sheet 01

Modification of the Equipment in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 112

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002 thru 004

(5)

(2)

(3)

(1)

(4)

(3 POS)

(3 POS)

(3 POS)

(3 POS)

(3 POS)

(3 POS)

2

1

5

4

3

B C

B C

B C

B C

B C

B C

110QA

42QA

41QA

109QA

35QA

36QA

107VU

A

BEFORE AFTER

B C

FR20

FR1 Z120

A

B C

B C

9QN

10QN

D_SB_286104_5_BBAB_01_00

Figure A-FBBAB - Sheet 01

Modification of the Equipment in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 113

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF ALL

Figure A-FWAAA - Sheet 01

Modification of the Wiring of the Relay 35QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 114

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF ALL

Figure A-FWAAA - Sheet 02

Modification of the Wiring of the Relay 35QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 115

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 107VU 35QA−A X 2821−0074 1M CF24 107VU 105QA−A 3 M1O

 2 107VU 35QA−A X1 EN3155−017F1620 2821−0074 1M CF24 107VU 105QA−A 3 M1N

 3 107VU 35QA−A Z 2821−0075 1M CF24 107VU 269VT 1E M1O

 4 107VU 35QA−A X2 EN3155−017F1620 2821−0075 1M CF24 107VU 269VT 1E M1N

 5 107VU 35QA−A 2 2821−0084 B 1M QF16 107VU 1809VC X M1O

 6 107VU 35QA−A A2 EN3155−017F1216 2821−0084 B 1M QF16 107VU 1809VC X M1N

 7 107VU 35QA−A 6 2821−0085 Y 1M QF16 107VU 1809VC V M1O

 8 107VU 35QA−A B2 EN3155−017F1216 2821−0085 Y 1M QF16 107VU 1809VC V M1N

 9 107VU 35QA−A 8 2821−0086 R 1M QF16 107VU 1809VC W M1O

10 107VU 35QA−A C2 EN3155−017F1216 2821−0086 R 1M QF16 107VU 1809VC W M1N

11 107VU 35QA−A 1 2821−0201 B 1M QF16 107VU 1815VC X M1O

12 107VU 35QA−A A1 EN3155−017F1216 2821−0201 B 1M QF16 107VU 1815VC X M1N

13 107VU 35QA−A 5 2821−0202 Y 1M QF16 107VU 1815VC V M1O

14 107VU 35QA−A B1 EN3155−017F1216 2821−0202 Y 1M QF16 107VU 1815VC V M1N

15 107VU 35QA−A 7 2821−0203 R 1M QF16 107VU 1815VC W M1O

16 107VU 35QA−A C1 EN3155−017F1216 2821−0203 R 1M QF16 107VU 1815VC W M1N

17 107VU 35QA−A 3 2821−0672 1M CF24 107VU 1369VT 1F M1O

18 107VU 35QA−A 12 EN3155−017F1620 2821−0672 1M CF24 107VU 1369VT 1F M1N

19 107VU 35QA−A 4 2821−0932 1M CF24 107VU 2040VC HH M1O

20 107VU 35QA−A 13 EN3155−017F1620 2821−0932 1M CF24 107VU 2040VC HH M1N

21 107VU 35QA−A B 2821−0933 1M CF24 107VU 1369VT 22L M1O

22 107VU 35QA−A 11 EN3155−017F1620 2821−0933 1M CF24 107VU 1369VT 22L M1N

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FHAAA - Sheet 01

Hook-up Chart of the Modification of the Wiring of the Relay 35QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 116

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 003 thru 004

Figure A-FWBAA - Sheet 01

Modification of the Wiring of the Relay 36QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 117

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 003 thru 004

Figure A-FWBAA - Sheet 02

Modification of the Wiring of the Relay 36QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 118

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 001 thru 002

Figure A-FWBAB - Sheet 01

Modification of the Wiring of the Relay 36QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 119

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 001 thru 002

Figure A-FWBAB - Sheet 02

Modification of the Wiring of the Relay 36QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 120

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 003 thru 004

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 107VU 36QA−A X 2821−0120 1M CF24 107VU 106QA−A 3 M1O

 2 107VU 36QA−A X1 EN3155−017F1620 2821−0120 1M CF24 107VU 106QA−A 3 M1N

 3 107VU 36QA−A Z 2821−0121 1M CF24 107VU 229VT 6A M1O

 4 107VU 36QA−A X2 SN3155−017F1620 2821−0121 1M CF24 107VU 229VT 6A M1N

 5 107VU 36QA−A 1 2821−0131 B 1M QF16 107VU 1815VC U M1O

 6 107VU 36QA−A A1 EN3155−017F1216 2821−0131 B 1M QF16 107VU 1815VC U M1N

 7 107VU 36QA−A 5 2821−0132 Y 1M QF16 107VU 1815VC T M1O

 8 107VU 36QA−A B1 EN3155−017F1216 2821−0132 Y 1M QF16 107VU 1815VC T M1N

 9 107VU 36QA−A 7 2821−0133 R 1M QF16 107VU 1815VC S M1O

10 107VU 36QA−A C1 EN3155−017F1216 2821−0133 R 1M QF16 107VU 1815VC S M1N

11 107VU 36QA−A 2 2821−0134 B 1M QF16 107VU 1809VC U M1O

12 107VU 36QA−A A2 EN3155−017F1216 2821−0134 B 1M QF16 107VU 1809VC U M1N

13 107VU 36QA−A 6 2821−0135 Y 1M QF16 107VU 1809VC T M1O

14 107VU 36QA−A B2 EN3155−017F1216 2821−0135 Y 1M QF16 107VU 1809VC T M1N

15 107VU 36QA−A 8 2821−0136 R 1M QF16 107VU 1809VC S M1O

16 107VU 36QA−A C2 EN3155−017F1216 2821−0136 R 1M QF16 107VU 1809VC S M1N

17 107VU 36QA−A 3 2821−0676 1M CF24 107VU 1369VT 1J M1O

18 107VU 36QA−A 12 SN3155−017F1620 2821−0676 1M CF24 107VU 1369VT 1J M1N

19 107VU 36QA−A 4 2821−0958 1M CF24 107VU 2040VC GG M1O

20 107VU 36QA−A 13 EN3155−017F1620 2821−0958 1M CF24 107VU 2040VC GG M1N

21 107VU 36QA−A B 2821−0959 1M CF24 107VU 1369VT 22M M1O

22 107VU 36QA−A 11 EN3155−017F1620 2821−0959 1M CF24 107VU 1369VT 22M M1N

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FHBAA - Sheet 01

Hook-up Chart of the Modification of the Wiring of the Relay 36QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 121

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 001 thru 002

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 107VU 36QA−A X 2821−0120 1M CF24 107VU 106QA−A 3 M1O

 2 107VU 36QA−A X1 EN3155−017F1620 2821−0120 1M CF24 107VU 106QA−A 3 M1N

 3 107VU 36QA−A Z 2821−0121 1M CF24 107VU 269VT 1F M1O

 4 107VU 36QA−A X2 SN3155−017F1620 2821−0121 1M CF24 107VU 269VT 1F M1N

 5 107VU 36QA−A 1 2821−0131 B 1M QF16 107VU 1815VC U M1O

 6 107VU 36QA−A A1 EN3155−017F1216 2821−0131 B 1M QF16 107VU 1815VC U M1N

 7 107VU 36QA−A 5 2821−0132 Y 1M QF16 107VU 1815VC T M1O

 8 107VU 36QA−A B1 EN3155−017F1216 2821−0132 Y 1M QF16 107VU 1815VC T M1N

 9 107VU 36QA−A 7 2821−0133 R 1M QF16 107VU 1815VC S M1O

10 107VU 36QA−A C1 EN3155−017F1216 2821−0133 R 1M QF16 107VU 1815VC S M1N

11 107VU 36QA−A 2 2821−0134 B 1M QF16 107VU 1809VC U M1O

12 107VU 36QA−A A2 EN3155−017F1216 2821−0134 B 1M QF16 107VU 1809VC U M1N

13 107VU 36QA−A 6 2821−0135 Y 1M QF16 107VU 1809VC T M1O

14 107VU 36QA−A B2 EN3155−017F1216 2821−0135 Y 1M QF16 107VU 1809VC T M1N

15 107VU 36QA−A 8 2821−0136 R 1M QF16 107VU 1809VC S M1O

16 107VU 36QA−A C2 EN3155−017F1216 2821−0136 R 1M QF16 107VU 1809VC S M1N

17 107VU 36QA−A 3 2821−0676 1M CF24 107VU 1369VT 1J M1O

18 107VU 36QA−A 12 SN3155−017F1620 2821−0676 1M CF24 107VU 1369VT 1J M1N

19 107VU 36QA−A 4 2821−0958 1M CF24 107VU 2040VC GG M1O

20 107VU 36QA−A 13 EN3155−017F1620 2821−0958 1M CF24 107VU 2040VC GG M1N

21 107VU 36QA−A B 2821−0959 1M CF24 107VU 1369VT 22M M1O

22 107VU 36QA−A 11 EN3155−017F1620 2821−0959 1M CF24 107VU 1369VT 22M M1N

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FHBAB - Sheet 01

Hook-up Chart of the Modification of the Wiring of the Relay 36QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 122

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF ALL

Figure A-FWCAA - Sheet 01

Modification of the Wiring of the Relay 41QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 123

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF ALL

Figure A-FWCAA - Sheet 02

Modification of the Wiring of the Relay 41QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 124

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 107VU 41QA−A X 2821−0028 2M CF24 107VU 103QA−A 3 M1O

 2 107VU 41QA−A X1 EN3155−017F1620 2821−0028 2M CF24 107VU 103QA−A 3 M1N

 3 107VU 41QA−A Z 2821−0029 2M CF24 107VU 269VT 1D M1O

 4 107VU 41QA−A X2 EN3155−017F1620 2821−0029 2M CF24 107VU 269VT 1D M1N

 5 107VU 41QA−A 7 2821−0035 R 2M QF16 107VU 1814VC S M1O

 6 107VU 41QA−A C1 EN3155−017F1216 2821−0035 R 2M QF16 107VU 1814VC S M1N

 7 107VU 41QA−A 1 2821−0196 B 2M QF16 107VU 1814VC U M1O

 8 107VU 41QA−A A1 EN3155−017F1216 2821−0196 B 2M QF16 107VU 1814VC U M1N

 9 107VU 41QA−A 5 2821−0197 Y 2M QF16 107VU 1814VC T M1O

10 107VU 41QA−A B1 EN3155−017F1216 2821−0197 Y 2M QF16 107VU 1814VC T M1N

11 107VU 41QA−A 2 2821−0038 B 2M QF16 107VU 1808VC U M1O

12 107VU 41QA−A A2 EN3155−017F1216 2821−0038 B 2M QF16 107VU 1808VC U M1N

13 107VU 41QA−A 6 2821−0041 Y 2M QF16 107VU 1808VC T M1O

14 107VU 41QA−A B2 EN3155−017F1216 2821−0041 Y 2M QF16 107VU 1808VC T M1N

15 107VU 41QA−A 8 2821−0044 R 2M QF16 107VU 1808VC S M1O

16 107VU 41QA−A C2 EN3155−017F1216 2821−0044 R 2M QF16 107VU 1808VC S M1N

17 107VU 41QA−A 3 2821−0668 2M CF24 107VU 269VT 4D M1O

18 107VU 41QA−A 12 EN3155−017F1620 2821−0668 2M CF24 107VU 269VT 4D M1N

19 107VU 41QA−A 4 2821−0916 2M CF24 107VU 427VC C M1O

20 107VU 41QA−A 13 EN3155−017F1620 2821−0916 2M CF24 107VU 427VC C M1N

21 107VU 41QA−A B 2821−0919 2M CF24 107VU 1369VT 2J M1O

22 107VU 41QA−A 11 EN3155−017F1620 2821−0919 2M CF24 107VU 1369VT 2J M1N

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FHCAA - Sheet 01

Hook-up Chart of the Modification of the Wiring of the Relay 41QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 125

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF ALL

Figure A-FWDAA - Sheet 01

Modification of the Wiring of the Relay 42QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 126

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF ALL

Figure A-FWDAA - Sheet 02

Modification of the Wiring of the Relay 42QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 127

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 107VU 42QA−A X 2821−0166 2M CF24 107VU 104QA−A 3 M1O

 2 107VU 42QA−A X1 EN3155−017F1620 2821−0166 2M CF24 107VU 104QA−A 3 M1N

 3 107VU 42QA−A Z 2821−0167 2M CF24 107VU 269VT 1G M1O

 4 107VU 42QA−A X2 EN3155−017F1620 2821−0167 2M CF24 107VU 269VT 1G M1N

 5 107VU 42QA−A 1 2821−0175 B 2M QF16 107VU 1814VC G M1O

 6 107VU 42QA−A A1 EN3155−017F1216 2821−0175 B 2M QF16 107VU 1814VC G M1N

 7 107VU 42QA−A 5 2821−0176 Y 2M QF16 107VU 1814VC H M1O

 8 107VU 42QA−A B1 EN3155−017F1216 2821−0176 Y 2M QF16 107VU 1814VC H M1N

 9 107VU 42QA−A 7 2821−0177 R 2M QF16 107VU 1814VC J M1O

10 107VU 42QA−A C1 EN3155−017F1216 2821−0177 R 2M QF16 107VU 1814VC J M1N

11 107VU 42QA−A 2 2821−0178 B 2M QF16 107VU 1808VC F M1O

12 107VU 42QA−A A2 EN3155−017F1216 2821−0178 B 2M QF16 107VU 1808VC F M1N

13 107VU 42QA−A 6 2821−0179 Y 2M QF16 107VU 1808VC E M1O

14 107VU 42QA−A B2 EN3155−017F1216 2821−0179 Y 2M QF16 107VU 1808VC E M1N

15 107VU 42QA−A 8 2821−0180 R 2M QF16 107VU 1808VC D M1O

16 107VU 42QA−A C2 EN3155−017F1216 2821−0180 R 2M QF16 107VU 1808VC D M1N

17 107VU 42QA−A 3 2821−0680 2M CF24 107VU 269VT 4F M1O

18 107VU 42QA−A 12 EN3155−017F1620 2821−0680 2M CF24 107VU 269VT 4F M1N

19 107VU 42QA−A 4 2821−0980 2M CF24 107VU 427VC D M1O

20 107VU 42QA−A 13 EN3155−017F1620 2821−0980 2M CF24 107VU 427VC D M1N

21 107VU 42QA−A B 2821−0981 2M CF24 107VU 1369VT 22K M1O

22 107VU 42QA−A 11 EN3155−017F1620 2821−0981 2M CF24 107VU 1369VT 22K M1N

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FHDAA - Sheet 01

Hook-up Chart of the Modification of the Wiring of the Relay 42QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 128

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 001 thru 002

Figure A-FWEAA - Sheet 01

Modification of the Wiring of the Relay 109QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 129

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 001 thru 002

Figure A-FWEAA - Sheet 02

Modification of the Wiring of the Relay 109QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 130

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 003 thru 004

Figure A-FWEAB - Sheet 01

Modification of the Wiring of the Relay 109QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 131

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 003 thru 004

Figure A-FWEAB - Sheet 02

Modification of the Wiring of the Relay 109QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 132

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 001 thru 002

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 107VU 109QA−A Z 2821−0559 1M CF24 107VU 269VT 1K M1O

 2 107VU 109QA−A X2 EN3155−017F1620 2821−0559 1M CF24 107VU 269VT 1K M1N

 3 107VU 109QA−A 1 2821−0563 B 1M QF16 107VU 1815VC G M1O

 4 107VU 109QA−A A1 EN3155−017F1216 2821−0563 B 1M QF16 107VU 1815VC G M1N

 5 107VU 109QA−A 5 2821−0567 Y 1M QF16 107VU 1815VC F M1O

 6 107VU 109QA−A B1 EN3155−017F1216 2821−0567 Y 1M QF16 107VU 1815VC F M1N

 7 107VU 109QA−A 7 2821−0571 R 1M QF16 107VU 1815VC E M1O

 8 107VU 109QA−A C1 EN3155−017F1216 2821−0571 R 1M QF16 107VU 1815VC E M1N

 9 107VU 109QA−A 2 2821−0564 B 1M QF16 107VU 1809VC G M1O

10 107VU 109QA−A A2 EN3155−017F1216 2821−0564 B 1M QF16 107VU 1809VC G M1N

11 107VU 109QA−A 6 2821−0568 Y 1M QF16 107VU 1809VC J M1O

12 107VU 109QA−A B2 EN3155−017F1216 2821−0568 Y 1M QF16 107VU 1809VC J M1N

13 107VU 109QA−A 8 2821−0572 R 1M QF16 107VU 1809VC H M1O

14 107VU 109QA−A C2 EN3155−017F1216 2821−0572 R 1M QF16 107VU 1809VC H M1N

15 107VU 109QA−A 3 2821−0662 1M CF24 107VU 1369VT 1G M1O

16 107VU 109QA−A 12 EN3155−017F1620 2821−0662 1M CF24 107VU 1369VT 1G M1N

17 107VU 109QA−A 4 2821−0994 1M CF24 107VU 2040VC FF M1O

18 107VU 109QA−A 13 EN3155−017F1620 2821−0994 1M CF24 107VU 2040VC FF M1N

19 107VU 109QA−A B 2821−0995 1M CF24 107VU 269VT 7E M1O

20 107VU 109QA−A 11 EN3155−017F1620 2821−0995 1M CF24 107VU 269VT 7E M1N

21 107VU 109QA−A X 2821−1002 1M CF24 107VU 107QA−A 1 M1O

22 107VU 109QA−A X1 EN3155−017F1620 2821−1002 1M CF24 107VU 107QA−A 1 M1N

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FHEAA - Sheet 01

Hook-up Chart of the Modification of the Wiring of the Relay 109QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 133

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 003 thru 004

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 107VU 109QA−A Z 2821−0559 1M CF24 107VU 229VT 6K M1O

 2 107VU 109QA−A X2 EN3155−017F1620 2821−0559 1M CF24 107VU 229VT 6K M1N

 3 107VU 109QA−A 1 2821−0563 B 1M QF16 107VU 1815VC G M1O

 4 107VU 109QA−A A1 EN3155−017F1216 2821−0563 B 1M QF16 107VU 1815VC G M1N

 5 107VU 109QA−A 5 2821−0567 Y 1M QF16 107VU 1815VC F M1O

 6 107VU 109QA−A B1 EN3155−017F1216 2821−0567 Y 1M QF16 107VU 1815VC F M1N

 7 107VU 109QA−A 7 2821−0571 R 1M QF16 107VU 1815VC E M1O

 8 107VU 109QA−A C1 EN3155−017F1216 2821−0571 R 1M QF16 107VU 1815VC E M1N

 9 107VU 109QA−A 2 2821−0564 B 1M QF16 107VU 1809VC G M1O

10 107VU 109QA−A A2 EN3155−017F1216 2821−0564 B 1M QF16 107VU 1809VC G M1N

11 107VU 109QA−A 6 2821−0568 Y 1M QF16 107VU 1809VC J M1O

12 107VU 109QA−A B2 EN3155−017F1216 2821−0568 Y 1M QF16 107VU 1809VC J M1N

13 107VU 109QA−A 8 2821−0572 R 1M QF16 107VU 1809VC H M1O

14 107VU 109QA−A C2 EN3155−017F1216 2821−0572 R 1M QF16 107VU 1809VC H M1N

15 107VU 109QA−A 3 2821−0662 1M CF24 107VU 1369VT 1G M1O

16 107VU 109QA−A 12 EN3155−017F1620 2821−0662 1M CF24 107VU 1369VT 1G M1N

17 107VU 109QA−A 4 2821−0994 1M CF24 107VU 2040VC FF M1O

18 107VU 109QA−A 13 EN3155−017F1620 2821−0994 1M CF24 107VU 2040VC FF M1N

19 107VU 109QA−A B 2821−0995 1M CF24 107VU 269VT 7E M1O

20 107VU 109QA−A 11 EN3155−017F1620 2821−0995 1M CF24 107VU 269VT 7E M1N

21 107VU 109QA−A X 2821−1002 1M CF24 107VU 107QA−A 1 M1O

22 107VU 109QA−A X1 EN3155−017F1620 2821−1002 1M CF24 107VU 107QA−A 1 M1N

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FHEAB - Sheet 01

Hook-up Chart of the Modification of the Wiring of the Relay 109QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 134

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF ALL

Figure A-FWFAA - Sheet 01

Modification of the Wiring of the Relay 110QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 135

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF ALL

Figure A-FWFAA - Sheet 02

Modification of the Wiring of the Relay 110QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 136

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF ALL

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 107VU 110QA−A Z 2821−0607 2M CF24 107VU 269VT 1A M1O

 2 107VU 110QA−A X2 EN3155−017F1620 2821−0607 2M CF24 107VU 269VT 1A M1N

 3 107VU 110QA−A 1 2821−0611 B 2M QF16 107VU 1814VC R M1O

 4 107VU 110QA−A A1 EN3155−017F1216 2821−0611 B 2M QF16 107VU 1814VC R M1N

 5 107VU 110QA−A 5 2821−0615 Y 2M QF16 107VU 1814VC P M1O

 6 107VU 110QA−A B1 EN3155−017F1216 2821−0615 Y 2M QF16 107VU 1814VC P M1N

 7 107VU 110QA−A 7 2821−0619 R 2M QF16 107VU 1814VC N M1O

 8 107VU 110QA−A C1 EN3155−017F1216 2821−0619 R 2M QF16 107VU 1814VC N M1N

 9 107VU 110QA−A 2 2821−0612 B 2M QF16 107VU 1808VC R M1O

10 107VU 110QA−A A2 EN3155−017F1216 2821−0612 B 2M QF16 107VU 1808VC R M1N

11 107VU 110QA−A 6 2821−0616 Y 2M QF16 107VU 1808VC P M1O

12 107VU 110QA−A B2 EN3155−017F1216 2821−0616 Y 2M QF16 107VU 1808VC P M1N

13 107VU 110QA−A 8 2821−0620 R 2M QF16 107VU 1808VC N M1O

14 107VU 110QA−A C2 EN3155−017F1216 2821−0620 R 2M QF16 107VU 1808VC N M1N

15 107VU 110QA−A 3 2821−0664 2M CF24 107VU 269VT 4E M1O

16 107VU 110QA−A 12 EN3155−017F1620 2821−0664 2M CF24 107VU 269VT 4E M1N

17 107VU 110QA−A 4 2821−1021 2M CF24 107VU 427VC G M1O

18 107VU 110QA−A 13 EN3155−017F1620 2821−1021 2M CF24 107VU 427VC G M1N

19 107VU 110QA−A B 2821−1022 2M CF24 107VU 269VT 7C M1O

20 107VU 110QA−A 11 EN3155−017F1620 2821−1022 2M CF24 107VU 269VT 7C M1N

21 107VU 110QA−A X 2821−1026 2M CF24 107VU 108QA−A 1 M1O

22 107VU 110QA−A X1 EN3155−017F1620 2821−1026 2M CF24 107VU 108QA−A 1 M1N

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FHFAA - Sheet 01

Hook-up Chart of the Modification of the Wiring of the Relay 110QA in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 137

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 004

Figure A-FWGAA - Sheet 01

Modification of the Wiring of the Relay 9QN in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 138

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 004

Figure A-FWGAA - Sheet 02

Modification of the Wiring of the Relay 9QN in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 139

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002 thru 003

Figure A-FWGAB - Sheet 01

Modification of the Wiring of the Relay 9QN in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 140

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002 thru 003

Figure A-FWGAB - Sheet 02

Modification of the Wiring of the Relay 9QN in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 141

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 004

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 107VU 9QN−A 1 2821−0059 B 1M QF16 107VU 1815VC D M1O

 2 107VU 9QN−A A1 EN3155−017F1216 2821−0059 B 1M QF16 107VU 1815VC D M1N

 3 107VU 9QN−A 5 2821−0060 Y 1M QF16 107VU 1815VC H M1O

 4 107VU 9QN−A B1 EN3155−017F1216 2821−0060 Y 1M QF16 107VU 1815VC H M1N

 5 107VU 9QN−A 7 2821−0061 R 1M QF16 107VU 1815VC J M1O

 6 107VU 9QN−A C1 EN3155−017F1216 2821−0061 R 1M QF16 107VU 1815VC J M1N

 7 107VU 9QN−A 2 2821−0062 B 1M QF16 107VU 1680VC −R M1O

 8 107VU 9QN−A A2 EN3155−017F1216 2821−0062 B 1M QF16 107VU 1680VC −R M1N

 9 107VU 9QN−A 6 2821−0063 Y 1M QF16 107VU 1680VC −S M1O

10 107VU 9QN−A B2 EN3155−017F1216 2821−0063 Y 1M QF16 107VU 1680VC −S M1N

11 107VU 9QN−A 8 2821−0064 R 1M QF16 107VU 1680VC −T M1O

12 107VU 9QN−A C2 EN3155−017F1216 2821−0064 R 1M QF16 107VU 1680VC −T M1N

13 107VU 9QN−A Z 2821−0068 1M CF24 107VU 226VT 9G M1O

14 107VU 9QN−A X2 EN3155−017F1620 2821−0068 1M CF24 107VU 226VT 9G M1N

15 107VU 9QN−A X 2821−0074 1M CF24 107VU 11QL−A 1 M1O

16 107VU 9QN−A X1 EN3155−017F1620 2821−0074 1M CF24 107VU 11QL−A 1 M1N

17 107VU 9QN−A 3 2821−1800 1M CF24 107VU 226VT 9C M1O

18 107VU 9QN−A 12 EN3155−017F1620 2821−1800 1M CF24 107VU 226VT 9C M1N

19 107VU 9QN−A B 2821−1804 1M CF24 107VU 709VC −Q M1O

20 107VU 9QN−A 11 EN3155−017F1620 2821−1804 1M CF24 107VU 709VC −Q M1N

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FHGAA - Sheet 01

Hook-up Chart of the Modification of the Wiring of the Relay 9QN in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 142

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002 thru 003

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 107VU 9QN−A 1 2821−0059 B 1M QF16 107VU 1815VC D M1O

 2 107VU 9QN−A A1 EN3155−017F1216 2821−0059 B 1M QF16 107VU 1815VC D M1N

 3 107VU 9QN−A 5 2821−0060 Y 1M QF16 107VU 1815VC H M1O

 4 107VU 9QN−A B1 EN3155−017F1216 2821−0060 Y 1M QF16 107VU 1815VC H M1N

 5 107VU 9QN−A 7 2821−0061 R 1M QF16 107VU 1815VC J M1O

 6 107VU 9QN−A C1 EN3155−017F1216 2821−0061 R 1M QF16 107VU 1815VC J M1N

 7 107VU 9QN−A 2 2821−0062 B 1M QF16 107VU 1680VC −R M1O

 8 107VU 9QN−A A2 EN3155−017F1216 2821−0062 B 1M QF16 107VU 1680VC −R M1N

 9 107VU 9QN−A 6 2821−0063 Y 1M QF16 107VU 1680VC −S M1O

10 107VU 9QN−A B2 EN3155−017F1216 2821−0063 Y 1M QF16 107VU 1680VC −S M1N

11 107VU 9QN−A 8 2821−0064 R 1M QF16 107VU 1680VC −T M1O

12 107VU 9QN−A C2 EN3155−017F1216 2821−0064 R 1M QF16 107VU 1680VC −T M1N

13 107VU 9QN−A Z 2821−0068 1M CF24 107VU 226VT 9G M1O

14 107VU 9QN−A X2 EN3155−017F1620 2821−0068 1M CF24 107VU 226VT 9G M1N

15 107VU 9QN−A X 2821−0074 1M CF24 107VU 11QL−A 1 M1O

16 107VU 9QN−A X1 EN3155−017F1620 2821−0074 1M CF24 107VU 11QL−A 1 M1N

17 107VU 9QN−A 3 2821−0082 1M CF24 107VU 226VT 9C M1O

18 107VU 9QN−A 12 EN3155−017F1620 2821−0082 1M CF24 107VU 226VT 9C M1N

19 107VU 9QN−A B 2821−0089 1M CF24 107VU 709VC −Q M1O

20 107VU 9QN−A 11 EN3155−017F1620 2821−0089 1M CF24 107VU 709VC −Q M1N

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FHGAB - Sheet 01

Hook-up Chart of the Modification of the Wiring of the Relay 9QN in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 143

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 004

Figure A-FWHAA - Sheet 01

Modification of the Wiring of the Relay 10QN in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 144

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 004

Figure A-FWHAA - Sheet 02

Modification of the Wiring of the Relay 10QN in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 145

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002 thru 003

Figure A-FWHAB - Sheet 01

Modification of the Wiring of the Relay 10QN in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 146

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002 thru 003

Figure A-FWHAB - Sheet 02

Modification of the Wiring of the Relay 10QN in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 147

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 004

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 107VU 10QN−A 1 2821−0023 B 2M QF16 107VU 1814VC A M1O

 2 107VU 10QN−A A1 EN3155−017F1216 2821−0023 B 2M QF16 107VU 1814VC A M1N

 3 107VU 10QN−A 5 2821−0024 Y 2M QF16 107VU 1814VC B M1O

 4 107VU 10QN−A B1 EN3155−017F1216 2821−0024 Y 2M QF16 107VU 1814VC B M1N

 5 107VU 10QN−A 7 2821−0025 R 2M QF16 107VU 1814VC C M1O

 6 107VU 10QN−A C1 EN3155−017F1216 2821−0025 R 2M QF16 107VU 1814VC C M1N

 7 107VU 10QN−A 2 2821−0026 B 2M QF16 107VU 1825VC −N M1O

 8 107VU 10QN−A A2 EN3155−017F1216 2821−0026 B 2M QF16 107VU 1825VC −N M1N

 9 107VU 10QN−A 6 2821−0027 Y 2M QF16 107VU 1825VC −P M1O

10 107VU 10QN−A B2 EN3155−017F1216 2821−0027 Y 2M QF16 107VU 1825VC −P M1N

11 107VU 10QN−A 8 2821−0028 R 2M QF16 107VU 1825VC −Q M1O

12 107VU 10QN−A C2 EN3155−017F1216 2821−0028 R 2M QF16 107VU 1825VC −Q M1N

13 107VU 10QN−A Z 2821−0032 2M CF24 107VU 226VT 9B M1O

14 107VU 10QN−A X2 EN3155−017F1620 2821−0032 2M CF24 107VU 226VT 9B M1N

15 107VU 10QN−A X 2821−0038 2M CF24 107VU 12QL−A 1 M1O

16 107VU 10QN−A X1 EN3155−017F1620 2821−0038 2M CF24 107VU 12QL−A 1 M1N

17 107VU 10QN−A 3 2821−1799 2M CF24 107VU 226VT 9A M1O

18 107VU 10QN−A 12 EN3155−017F1620 2821−1799 2M CF24 107VU 226VT 9A M1N

19 107VU 10QN−A B 2821−1803 2M CF24 107VU 427VC W M1O

20 107VU 10QN−A 11 EN3155−017F1620 2821−1803 2M CF24 105VU 427VC W M1N

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FHHAA - Sheet 01

Hook-up Chart of the Modification of the Wiring of the Relay 10QN in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 148

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

**CONF 002 thru 003

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 107VU 10QN−A 1 2821−0023 B 2M QF16 107VU 1814VC A M1O

 2 107VU 10QN−A A1 EN3155−017F1216 2821−0023 B 2M QF16 107VU 1814VC A M1N

 3 107VU 10QN−A 5 2821−0024 Y 2M QF16 107VU 1814VC B M1O

 4 107VU 10QN−A B1 EN3155−017F1216 2821−0024 Y 2M QF16 107VU 1814VC B M1N

 5 107VU 10QN−A 7 2821−0025 R 2M QF16 107VU 1814VC C M1O

 6 107VU 10QN−A C1 EN3155−017F1216 2821−0025 R 2M QF16 107VU 1814VC C M1N

 7 107VU 10QN−A 2 2821−0026 B 2M QF16 107VU 1825VC −N M1O

 8 107VU 10QN−A A2 EN3155−017F1216 2821−0026 B 2M QF16 107VU 1825VC −N M1N

 9 107VU 10QN−A 6 2821−0027 Y 2M QF16 107VU 1825VC −P M1O

10 107VU 10QN−A B2 EN3155−017F1216 2821−0027 Y 2M QF16 107VU 1825VC −P M1N

11 107VU 10QN−A 8 2821−0028 R 2M QF16 107VU 1825VC −Q M1O

12 107VU 10QN−A C2 EN3155−017F1216 2821−0028 R 2M QF16 107VU 1825VC −Q M1N

13 107VU 10QN−A Z 2821−0032 2M CF24 107VU 226VT 9B M1O

14 107VU 10QN−A X2 EN3155−017F1620 2821−0032 2M CF24 107VU 226VT 9B M1N

15 107VU 10QN−A X 2821−0038 2M CF24 107VU 12QL−A 1 M1O

16 107VU 10QN−A X1 EN3155−017F1620 2821−0038 2M CF24 107VU 12QL−A 1 M1N

17 107VU 10QN−A 3 2821−0079 2M CF24 107VU 226VT 9A M1O

18 107VU 10QN−A 12 EN3155−017F1620 2821−0079 2M CF24 107VU 226VT 9A M1N

19 107VU 10QN−A B 2821−0081 2M CF24 107VU 427VC W M1O

20 107VU 10QN−A 11 EN3155−017F1620 2821−0081 2M CF24 105VU 427VC W M1N

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FHHAB - Sheet 01

Hook-up Chart of the Modification of the Wiring of the Relay 10QN in the LH Relay Box 107VU.

DATE: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 149

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600

SERVICE BULLETIN

REPORTING SHEET

TITLE: FUEL SYSTEM - INTRODUCE GROUND FAULT INTERRUPTER (GFI)

MODIFICATION No.: 13382H5685

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: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 1

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@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: Feb 28/12 SERVICE BULLETIN No.: A300-28-6104

REVISION No.: 00 - Feb 28/12 Page: 1

7

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