@A340-500/600

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-MAIN TRANSFER SYST-INTRO GROUND FAULT INTERRUPTERS

TO CENTER AND REAR CENTER TANK FUEL PUMP CONTROL

CIRCUIT

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 200242H16513 200242H16135

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 the Ground Fault Interrupters (GFI)

are installed into the electrical supply circuits of fuel pumps where the inlets become uncovered during

normal operation. This is in response to SFAR88 - Fuel Tank Safety.

The Evaluation Service Bulletin A340-28-5902 (Mod. No. 200241H16397) was issued for operators

DLH, IBE and UAE. The Service Bulletin A340-28-5902 introduced a GFI and related base into the

electrical supply circuit of the A340-500/600 aircraft center tank right transfer pump, and A340-500

aircraft rear center tank Front (A) forward transfer pump.

This Service Bulletin introduces two modifications:

- Mod. No. 200242H16135 introduces GFIs and related bases into the electrical supply circuits of the

Left and Right transfer pumps of the A340-500/600 center tanks

- Mod. No. 200242H16513 introduces GFIs and related bases into the electrical supply circuits of the

A340-500 rear center tank (Front (A) and Rear (B)) transfer 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.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 1

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

SUMMARY

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.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO LROPS 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 285051A01R00 1 7,500.00 Bundle, Placard Set, Relay, Base, Nuts.

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 285051A01R00 1 7,500.00 Bundle, Placard Set, Relay, Base, Nuts.

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 285051A02R00 1 3,480.00 Placard Set, Relay, Base, Nuts.

**CONF 004

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 285051A03R00 1 3,480.00 Placard Set, Relay, Base, Nuts.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 2

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

SUMMARY

**CONF 005

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 285051A03R00 1 3,480.00 Placard Set, Relay, Base, Nuts.

**CONF 006

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 285051A04R00 1 1,740.00 Placard Set, Relay, Base, Nuts.

EFFECTIVITY

**CONF ALL

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

06U 62X 70U 72W 79W CES CHH DLH ETD HFY IBE QAF QTR

SAA SIA SOR TAM THA UAE VIR

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER ALS Part 5

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 285051-831-895-001: MODIFICATION

TOTAL MANHOURS 11.00

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 3

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

SUMMARY

Task 285051-831-895-001: MODIFICATION

ELAPSED TIME (HOURS) 11.00

**CONF 002

Task 285051-831-895-001: MODIFICATION

TOTAL MANHOURS 11.00

ELAPSED TIME (HOURS) 11.00

**CONF 003

Task 285051-831-895-001: MODIFICATION

TOTAL MANHOURS 6.50

ELAPSED TIME (HOURS) 6.50

**CONF 004

Task 285051-831-895-001: MODIFICATION

TOTAL MANHOURS 6.50

ELAPSED TIME (HOURS) 6.50

**CONF 005

Task 285051-831-895-001: MODIFICATION

TOTAL MANHOURS 6.50

ELAPSED TIME (HOURS) 6.50

**CONF 006

Task 285051-831-895-001: MODIFICATION

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

APPENDICES

**CONF ALL

None

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 4

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

SUMMARY

**CONF 001 thru 005

FR14

FR15A

751VU

752VU

F_SB_285051_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 5

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

SUMMARY

**CONF 006

FR14

FR15A

751VU

F_SB_285051_5_SAAB_01_00

Figure A-FSAAB - Sheet 01

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 6

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

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-MAIN TRANSFER SYST-INTRO GROUND FAULT INTERRUPTERS

TO CENTER AND REAR CENTER TANK FUEL PUMP CONTROL

CIRCUIT

MODIFICATION No.: 200242H16513 200242H16135

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

340-541 340-542 340-642

(2) Effectivity by MSN

0371 0376 0383 0391 0394 0410 0416-0417 0426 0431 0436 0440 0445 0449 0453

0457 0460 0464 0468 0471 0475 0478 0482 0485 0488 0492 0495 0499 0514 0517

0520 0523 0531 0534 0537 0540 0543 0547 0557 0560 0563 0566 0569 0572 0575

0577 0580 0583 0586 0601 0604 0606 0608 0611 0615 0617 0619 0622 0624 0626

0628 0630 0639 0672 0677 0681 0685 0689 0694 0698 0702 0706 0710 0715 0719

0723 0727 0736 0740 0744 0748 0753 0757 0761-0768 0771 0775 0779 0783 0787

0790 0794 0798 0804 0812 0829 0837 0846 0848 0870 0886 0894 0897 0902 0910

0912 0917 0924 0929 0933 0953 0960 0972 0981 0987 0993 1005 1017 1030 1040

1079 1091 1102 1122

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 1

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(3) Effectivity by Operator

The Operator/MSN relationship is provided for information only and is correct at the time

of issue in accordance with the information available to AIRBUS. Any future changes

resulting from transfer of an aircraft from one operator to another will not be reflected in

this list unless the Service Bulletin is revised for another reason.

OPERATOR MSN

06U 1091 1102

62X 0779

70U 0902

72W 0917

79W 0924

CES 0468 0488 0514 0577 0586

CHH 0436 0453 0475

DLH 0482 0517 0523 0537 0540 0543 0566 0569 0580 0583 0762 0763

0767 0771 0790 0794 0812 0846 0848 0897 0972 0981 0987 1005

ETD 0748 0757 0761 0783 0829 0837 0870 0929 0933 1030 1040

HFY 0910 0912

IBE 0431 0440 0460 0601 0604 0606 0617 0619 0672 0702 0727 0744

0960 0993 1017 1079 1122

QAF 0495

QTR 0715 0740 0766 0798

SAA 0410 0417 0426 0531 0534 0547 0557 0626 0630

SIA 0478 0492 0499 0560 0563

SOR 0886 0894

TAM 0445 0464

THA 0624 0628 0677 0681 0689 0698 0710 0719 0775 0953

UAE 0394 0457 0471 0485 0520 0572 0608 0611 0685 0694

VIR 0371 0376 0383 0391 0416 0449 0575 0615 0622 0639 0706 0723

0736 0753 0764 0765 0768 0787 0804

(4) Configuration by MSN

MSN CONFIGURATION

0371 0376 0383 0391 0410 0416 0417 0426 0436 0449 0453

0468 0475 0488 0514 0531 0534 0547 0557 0575 0577 0586

0615 0622 0626 0630 0639 0677 0681 0689 0706 0710 0715

0719 0723 0736 0740 0753 0764 0765 0766 0768 0779 0787

0798 0804 0829 0837 0870 0924 0929 0933 0953 1030 1040

003

0394 0457 0471 0485 0520 0572 0608 0611 002 005

0431 0440 0460 0482 0517 0523 0537 0540 0543 0566 0569

0580 0583 0601 0604 0606 0617 0619 0672 0702 0727 0744

0762 0763 0767 0771 0790 0794 0812 0846 0848 0897 0960

0972 0981 0987 0993 1005 1017 1079 1122

003 006

0445 0464 0495 0624 0628 002

0478 0492 0499 0560 0563 0698 0748 0757 0761 0775 0783

0886 0894 0902 0910 0912 0917 1091 1102

001

0685 0694 001 004

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 2

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(5) Configuration definition

**CONF 001

Config. 001 is valid for A340-500 aircraft on which:

- Mod. No. 53543H15530 is embodied or Service Bulletin No. A340-28-5018 is

accomplished

- Evaluation Service Bulletin No. A340-28-5902 is not accomplished or for aircraft on

which the restoration of Evaluation Service Bulletin No. A340-28-5902 is accomplished.

**CONF 002

Config. 002 is valid for A340-500 aircraft on which:

- Mod. No. 53543H15530 is not embodied or Service Bulletin No. A340-28-5018 is not

accomplished

- Evaluation Service Bulletin No. A340-28-5902 is not accomplished or for aircraft on

which the restoration of Evaluation Service Bulletin No. A340-28-5902 is accomplished.

**CONF 003

Config. 003 is valid for A340-600 aircraft on which Evaluation Service Bulletin No.

A340-28-5902 is not accomplished or for aircraft on which the restoration of Evaluation

Service Bulletin No. A340-28-5902 is accomplished.

**CONF 004

Config. 004 is valid for A340-500 aircraft on which:

- Mod. No. 53543H15530 is embodied or Service Bulletin No. A340-28-5018 is

accomplished

- Evaluation Service Bulletin No. A340-28-5902 is accomplished and the restoration is

not accomplished (during the evaluation period). These aircraft will not have to do the

restoration of Evaluation Service Bulletin No. A340-28-5902.

**CONF 005

Config. 005 is valid for A340-500 aircraft on which:

- Mod. No. 53543H15530 is not embodied or Service Bulletin No. A340-28-5018 is not

accomplished

- Evaluation Service Bulletin No. A340-28-5902 is accomplished and the restoration is

not accomplished (during the evaluation period). These aircraft will not have to do the

restoration of Evaluation Service Bulletin No. A340-28-5902.

**CONF 006

Config. 006 is valid for A340-600 aircraft on which Evaluation Service Bulletin No.

A340-28-5902 is accomplished and the restoration is not accomplished (during the

evaluation period). These aircraft will not have to do the restoration of Evaluation Service

Bulletin No. A340-28-5902.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Kit 285051A01R00 1

Consumable CMLA01 1

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 3

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Kit 285051A01R00 1

Consumable CMLA01 1

**CONF 003

MATERIAL QTY PER A/C SEE NOTES

Kit 285051A02R00 1

Consumable CMLA01 1

**CONF 004

MATERIAL QTY PER A/C SEE NOTES

Kit 285051A03R00 1

Consumable CMLA01 1

**CONF 005

MATERIAL QTY PER A/C SEE NOTES

Kit 285051A03R00 1

Consumable CMLA01 1

**CONF 006

MATERIAL QTY PER A/C SEE NOTES

Kit 285051A04R00 1

Consumable CMLA01 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

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

Interrupters (GFI) are installed into the electrical supply circuits of fuel pumps where the

inlets become uncovered during normal operation. This is in response to SFAR88 - Fuel

Tank Safety.

The Evaluation Service Bulletin A340-28-5902 (Mod. No. 200241H16397) was issued for

operators DLH, IBE and UAE. The Service Bulletin A340-28-5902 introduced a GFI and

related base into the electrical supply circuit of the A340-500/600 aircraft center tank

right transfer pump, and A340-500 aircraft rear center tank Front (A) forward transfer

pump.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 4

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(2) Objective/Action

This Service Bulletin introduces two modifications:

- Mod. No. 200242H16135 introduces GFIs and related bases into the electrical

supply circuits of the Left and Right transfer pumps of the A340-500/600 center

tanks

- Mod. No. 200242H16513 introduces GFIs and related bases into the electrical

supply circuits of the A340-500 rear center tank (Front (A) and Rear (B)) transfer

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.

(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.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 285051-831-895-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the LH Relay Box 751VU

(2) Modify the Equipment and the Wiring in the RH Relay Box 752VU

**CONF 002

Task 285051-831-895-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the LH Relay Box 751VU

(2) Modify the Equipment and the Wiring in the RH Relay Box 752VU

**CONF 003

Task 285051-831-895-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the LH Relay Box 751VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 5

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(2) Modify the Equipment and the Wiring in the RH Relay Box 752VU

**CONF 004

Task 285051-831-895-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the LH Relay Box 751VU

(2) Modify the Equipment and the Wiring in the RH Relay Box 752VU

**CONF 005

Task 285051-831-895-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the LH Relay Box 751VU

(2) Modify the Equipment and the Wiring in the RH Relay Box 752VU

**CONF 006

Task 285051-831-895-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the LH Relay Box 751VU

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

This Service Bulletin has been classified Mandatory by the issue of an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA). The AD must

be used as the reference document for the mandated accomplishment timescale.

F. APPROVAL

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

Organization Approval No. EASA.21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied that is not of

AIRBUS origin, and which affects the content of this Service Bulletin, the operator is

responsible for obtaining approval by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 6

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

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 285051-831-895-001: MODIFICATION

Get Access 1.50

On Aircraft

Modify the Equipment and the Wiring in the LH Relay

Box 751VU

4.00

Modify the Equipment and the Wiring in the RH Relay

Box 752VU

3.00

Tests 1.00

Close-Up 1.50

TOTAL MANHOURS 11.00

ELAPSED TIME (HOURS) 11.00

**CONF 002

Task 285051-831-895-001: MODIFICATION

Get Access 1.50

On Aircraft

Modify the Equipment and the Wiring in the LH Relay

Box 751VU

4.00

Modify the Equipment and the Wiring in the RH Relay

Box 752VU

3.00

Tests 1.00

Close-Up 1.50

TOTAL MANHOURS 11.00

ELAPSED TIME (HOURS) 11.00

**CONF 003

Task 285051-831-895-001: MODIFICATION

Get Access 1.50

On Aircraft

Modify the Equipment and the Wiring in the LH Relay

Box 751VU

1.50

Modify the Equipment and the Wiring in the RH Relay

Box 752VU

1.50

Tests 0.50

Close-Up 1.50

TOTAL MANHOURS 6.50

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 7

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Task 285051-831-895-001: MODIFICATION

ELAPSED TIME (HOURS) 6.50

**CONF 004

Task 285051-831-895-001: MODIFICATION

Get Access 1.50

On Aircraft

Modify the Equipment and the Wiring in the LH Relay

Box 751VU

1.50

Modify the Equipment and the Wiring in the RH Relay

Box 752VU

1.50

Tests 0.50

Close-Up 1.50

TOTAL MANHOURS 6.50

ELAPSED TIME (HOURS) 6.50

**CONF 005

Task 285051-831-895-001: MODIFICATION

Get Access 1.50

On Aircraft

Modify the Equipment and the Wiring in the LH Relay

Box 751VU

1.50

Modify the Equipment and the Wiring in the RH Relay

Box 752VU

1.50

Tests 0.50

Close-Up 1.50

TOTAL MANHOURS 6.50

ELAPSED TIME (HOURS) 6.50

**CONF 006

Task 285051-831-895-001: MODIFICATION

Get Access 1.50

On Aircraft

Modify the Equipment and the Wiring in the LH Relay

Box 751VU

1.50

Tests 0.50

Close-Up 1.50

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 8

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

H. WEIGHT AND BALANCE

**CONF 001 thru 002

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 Chapter 1-00-07 of the Weight and Balance Manual

(WBM).

Manufacturers Empty Weight +0.285 KG (+0.6283 LB)

Effect on Balance +2.734 KGM (+19.775 LB.FT )

**CONF 003

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 Chapter 1-00-07 of the Weight and Balance Manual

(WBM).

Manufacturers Empty Weight +0.140 KG (+0.3086 LB)

Effect on Balance +1.343 KGM (+9.713 LB.FT )

**CONF 004 thru 005

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 Chapter 1-00-07 of the Weight and Balance Manual

(WBM).

Manufacturers Empty Weight +0.145 KG (+0.3196 LB)

Effect on Balance +1.391 KGM (+10.061 LB.FT )

**CONF 006

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 Chapter 1-00-07 of the Weight and Balance Manual

(WBM).

Manufacturers Empty Weight +0.070 KG (+0.1543 LB)

Effect on Balance +0.671 KGM (+4.853 LB.FT )

**CONF ALL

I. ELECTRICAL LOAD DATA

Not Changed

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 9

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-41-52 06-41-53 11-00-00

12-34-24 20-21-15 20-28-00

28-25-00 52-30-00 52-52-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-30-00 20-33-00 20-46-50

20-51-20 20-52-21 20-55-00

Standards Manual (SM)

**CONF 002

Aircraft Maintenance Manual (AMM) 06-41-52 06-41-53 11-00-00

12-34-24 20-21-15 20-28-00

28-25-00 52-30-00 52-52-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-30-00 20-33-00 20-46-50

20-51-20 20-52-21 20-55-00

Standards Manual (SM)

**CONF 003

Aircraft Maintenance Manual (AMM) 06-41-52 06-41-53 11-00-00

12-34-24 20-21-15 20-28-00

28-25-00 52-30-00 52-52-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-30-00 20-33-00 20-46-50

20-51-20 20-52-21 20-55-00

Standards Manual (SM)

**CONF 004

Aircraft Maintenance Manual (AMM) 06-41-52 06-41-53 11-00-00

12-34-24 20-21-15 20-28-00

28-25-00 52-30-00 52-52-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-30-00 20-33-00 20-46-50

20-51-20 20-52-21 20-55-00

Standards Manual (SM)

**CONF 005

Aircraft Maintenance Manual (AMM) 06-41-52 06-41-53 11-00-00

12-34-24 20-21-15 20-28-00

28-25-00 52-30-00 52-52-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-30-00 20-33-00 20-46-50

20-51-20 20-52-21 20-55-00

Standards Manual (SM)

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 10

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 006

Aircraft Maintenance Manual (AMM) 06-41-52 06-41-53 11-00-00

12-34-24 20-21-15 20-28-00

28-25-00 52-30-00 52-52-00

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-30-00 20-33-00 20-46-50

20-51-20 20-52-21 20-55-00

Standards Manual (SM)

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Schematic Manual (ASM) 28-20-00 28-26-00

Aircraft Wiring List (AWL)

Aircraft Wiring Manual (AWM) 28-20-01 28-20-02 28-26-21

28-26-22 28-26-52

Illustrated Parts Catalog (IPC) 28-26-08

L. INTERCHANGEABILITY/MIXABILITY

**CONF 001

NOTE: One way interchangeable with conditions:

Conditions:

On embodiment existing socket and relay will be removed and replaced with

new ’fool proofed’ socket and GFI. Post mod only a GFI can be fitted in these

locations.

**CONF 002

NOTE: One way interchangeable with conditions:

Conditions:

On embodiment existing socket and relay will be removed and replaced with

new ’fool proofed’ socket and GFI. Post mod only a GFI can be fitted in these

locations.

**CONF 003

NOTE: One way interchangeable with conditions:

Conditions:

On embodiment existing socket and relay will be removed and replaced with

new ’fool proofed’ socket and GFI. Post mod only a GFI can be fitted in these

locations.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 11

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 004

NOTE: One way interchangeable with conditions:

Conditions:

On embodiment existing socket and relay will be removed and replaced with

new ’fool proofed’ socket and GFI. Post mod only a GFI can be fitted in these

locations.

**CONF 005

NOTE: One way interchangeable with conditions:

Conditions:

On embodiment existing socket and relay will be removed and replaced with

new ’fool proofed’ socket and GFI. Post mod only a GFI can be fitted in these

locations.

**CONF 006

NOTE: One way interchangeable with conditions:

Conditions:

On embodiment existing socket and relay will be removed and replaced with

new ’fool proofed’ socket and GFI. Post mod only a GFI can be fitted in these

locations.

**CONF ALL

M. SPARES

None

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 12

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Customers with aircraft shown in the effectivity of this Service Bulletin should send a

purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is:

Kit 285051A01R00

Kit 285051A02R00

Kit 285051A03R00

Kit 285051A04R00

AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet:

http://spares.airbus.com

For ordering modification kits by fax: +49 40

50 76 25 90

For ordering of single spares by fax: +49 40

50 76 40 13

(2) Price and Availability

Kit 285051A01R00

Cost 7,500.00 USD

Availability 90 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 285051A02R00

Cost 3,480.00 USD

Availability 90 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 285051A03R00

Cost 3,480.00 USD

Availability 90 calendar days from receipt of order

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 13

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

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 285051A04R00

Cost 1,740.00 USD

Availability 90 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

AIRBUS will provide a 15% reduction to the applicable sales prices given in the paragraph

’Price and Availability’ for orders placed before December 31/2017.

C. LIST OF COMPONENTS

Kit 285051A01R00

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

NOTES

3 MS21042-04 12 NUT (3) MS21042-04

6 ABS1629-28A0 4 GFI (1) E0667A28A0

(4) E0672D28A0

7 E0673C0S 4 BASE (5) E0311A0S

(2) E0673A0S

EN3155-017F1216 18 CONTACT

EN3155-017F1620 12 CONTACT

F9000095226895 1 BUNDLE

F9100095214695 1 PLACARD

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 285051A02R00

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

NOTES

3 MS21042-04 6 NUT (3) MS21042-04

6 ABS1629-28A0 2 GFI (1) E0667A28A0

7 E0673C0S 2 BASE (2) E0673A0S

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 14

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

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

NOTES

EN3155-017F1216 12 CONTACT

EN3155-017F1620 8 CONTACT

F9100095214795 1 PLACARD

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 285051A03R00

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

NOTES

3 MS21042-04 6 NUT (3) MS21042-04

6 ABS1629-28A0 2 GFI (1) E0667A28A0

(4) E0672D28A0

7 E0673C0S 2 BASE (5) E0311A0S

(2) E0673A0S

EN3155-017F1216 12 CONTACT

EN3155-017F1620 8 CONTACT

F9100095214895 1 PLACARD

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 285051A04R00

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

NOTES

3 MS21042-04 3 NUT (3) MS21042-04

6 ABS1629-28A0 1 GFI (1) E0667A28A0

7 E0673C0S 1 BASE (2) E0673A0S

EN3155-017F1216 6 CONTACT

EN3155-017F1620 4 CONTACT

F9100095214995 1 PLACARD

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.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 15

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent (Varsol/White

Spirit)

11-002 As required

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 16

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 285051-831-895-001 - MODIFICATION

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS:

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

Task Associated Data

**CONF 001

Zone

121 122 191 192 211 212

Modified FIN

5QL1 5QL1A 5QL2 5QL2A 79QL1 79QL1A 79QL2 79QL2A 97QL1 97QL1A 97QL2

97QL2A 98QL1 98QL1A 98QL2 98QL2A

Access

Door 132AZ 821

Electrical panel 751VU 752VU

Manpower

TOTAL MANHOURS 11.00

ELAPSED TIME (HOURS) 11.00

**CONF 002

Zone

121 122 191 192 211 212

Modified FIN

5QL1 5QL1A 5QL2 5QL2A 79QL1 79QL1A 79QL2 79QL2A 97QL1 97QL1A 97QL2

97QL2A 98QL1 98QL1A 98QL2 98QL2A

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 17

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Access

Door 132AZ 821

Electrical panel 751VU 752VU

Manpower

TOTAL MANHOURS 11.00

ELAPSED TIME (HOURS) 11.00

**CONF 003

Zone

121 122 191 192 211 212

Modified FIN

5QL1 5QL1A 5QL2 5QL2A 97QL1 97QL1A 97QL2 97QL2A

Access

Door 132AZ 821

Electrical panel 751VU 752VU

Manpower

TOTAL MANHOURS 6.50

ELAPSED TIME (HOURS) 6.50

**CONF 004

Zone

121 122 191 192 211 212

Modified FIN

5QL1 5QL1A 79QL2 79QL2A 97QL1 97QL1A 98QL2 98QL2A

Access

Door 132AZ 821

Electrical panel 751VU 752VU

Manpower

TOTAL MANHOURS 6.50

ELAPSED TIME (HOURS) 6.50

**CONF 005

Zone

121 122 191 192 211 212

Modified FIN

5QL1 5QL1A 79QL2 79QL2A 97QL1 97QL1A 98QL2 98QL2A

Access

Door 132AZ 821

Electrical panel 751VU 752VU

Manpower

TOTAL MANHOURS 6.50

ELAPSED TIME (HOURS) 6.50

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 18

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 006

Zone

121 191 192 211 212

Modified FIN

5QL1 5QL1A 97QL1 97QL1A

Access

Door 132AZ 821

Electrical panel 751VU

Manpower

TOTAL MANHOURS 5.00

ELAPSED TIME (HOURS) 5.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 285051-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent

(Varsol/White Spirit)

11-002 As required

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-802

Task 20-21-15-912-801

Task 20-28-00-912-802

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-30-00

20-33-00

20-46-50

20-51-20

20-52-21

Standards Manual (SM)

(a) Do the electrical bonding (Refer to AMM Task 20-28-00-912-802 and ESPM

20-51-20).

(b) For the specification of materials (Mat. No.) that you must use in this Service

Bulletin refer to Consumable Materials List (CML).

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 19

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

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

(f) To torque tighten the electrical component fasteners (Refer to AMM Task

20-21-15-912-801).

(g) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(h) Put blanking caps on the disconnected electrical connectors.

(i) To install new wires, cut them to the necessary length, crimp the terminals and

connect them.

(j) Route the new wires with the wires that are in the aircraft.

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

(l) For the installation of placards (Refer to AMM Task 11-00-00-400-802).

(m) Clean the surfaces at the location of the placards with:

Dry Cleaning

Solvent

(Varsol/White Spirit)

11-002 As required

(2) Subtask 285051-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 285051-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent

(Varsol/White Spirit)

11-002 As required

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 20

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-802

Task 20-21-15-912-801

Task 20-28-00-912-802

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-30-00

20-33-00

20-46-50

20-51-20

20-52-21

Standards Manual (SM)

(a) Do the electrical bonding (Refer to AMM Task 20-28-00-912-802 and ESPM

20-51-20).

(b) For the specification of materials (Mat. No.) that you must use in this Service

Bulletin refer to Consumable Materials List (CML).

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

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

(f) To torque tighten the electrical component fasteners (Refer to AMM Task

20-21-15-912-801).

(g) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(h) Put blanking caps on the disconnected electrical connectors.

(i) To install new wires, cut them to the necessary length, crimp the terminals and

connect them.

(j) Route the new wires with the wires that are in the aircraft.

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

(l) For the installation of placards (Refer to AMM Task 11-00-00-400-802).

(m) Clean the surfaces at the location of the placards with:

Dry Cleaning

Solvent

(Varsol/White Spirit)

11-002 As required

(2) Subtask 285051-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 21

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

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

Service Bulletin.

**CONF 003

(1) Subtask 285051-910-001-002 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent

(Varsol/White Spirit)

11-002 As required

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-802

Task 20-21-15-912-801

Task 20-28-00-912-802

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-30-00

20-33-00

20-46-50

20-51-20

20-52-21

Standards Manual (SM)

(a) Do the electrical bonding (Refer to AMM Task 20-28-00-912-802 and ESPM

20-51-20).

(b) For the specification of materials (Mat. No.) that you must use in this Service

Bulletin refer to Consumable Materials List (CML).

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

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

(f) To torque tighten the electrical component fasteners (Refer to AMM Task

20-21-15-912-801).

(g) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(h) Put blanking caps on the disconnected electrical connectors.

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

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 22

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(j) For the installation of placards (Refer to AMM Task 11-00-00-400-802).

(k) Clean the surfaces at the location of the placards with:

Dry Cleaning

Solvent

(Varsol/White Spirit)

11-002 As required

(2) Subtask 285051-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 004

(1) Subtask 285051-910-001-002 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent

(Varsol/White Spirit)

11-002 As required

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-802

Task 20-21-15-912-801

Task 20-28-00-912-802

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-30-00

20-33-00

20-46-50

20-51-20

20-52-21

Standards Manual (SM)

(a) Do the electrical bonding (Refer to AMM Task 20-28-00-912-802 and ESPM

20-51-20).

(b) For the specification of materials (Mat. No.) that you must use in this Service

Bulletin refer to Consumable Materials List (CML).

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 23

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(d) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

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

(f) To torque tighten the electrical component fasteners (Refer to AMM Task

20-21-15-912-801).

(g) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(h) Put blanking caps on the disconnected electrical connectors.

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

(j) For the installation of placards (Refer to AMM Task 11-00-00-400-802).

(k) Clean the surfaces at the location of the placards with:

Dry Cleaning

Solvent

(Varsol/White Spirit)

11-002 As required

(2) Subtask 285051-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 005

(1) Subtask 285051-910-001-002 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent

(Varsol/White Spirit)

11-002 As required

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-802

Task 20-21-15-912-801

Task 20-28-00-912-802

Consumable Material List (CML)

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 24

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

References

Elec. Std. Practices Manual (ESPM) 20-30-00

20-33-00

20-46-50

20-51-20

20-52-21

Standards Manual (SM)

(a) Do the electrical bonding (Refer to AMM Task 20-28-00-912-802 and ESPM

20-51-20).

(b) For the specification of materials (Mat. No.) that you must use in this Service

Bulletin refer to Consumable Materials List (CML).

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

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

(f) To torque tighten the electrical component fasteners (Refer to AMM Task

20-21-15-912-801).

(g) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(h) Put blanking caps on the disconnected electrical connectors.

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

(j) For the installation of placards (Refer to AMM Task 11-00-00-400-802).

(k) Clean the surfaces at the location of the placards with:

Dry Cleaning

Solvent

(Varsol/White Spirit)

11-002 As required

(2) Subtask 285051-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 006

(1) Subtask 285051-910-001-002 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 25

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent

(Varsol/White Spirit)

11-002 As required

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-802

Task 20-21-15-912-801

Task 20-28-00-912-802

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-30-00

20-33-00

20-46-50

20-51-20

20-52-21

Standards Manual (SM)

(a) Do the electrical bonding (Refer to AMM Task 20-28-00-912-802 and ESPM

20-51-20).

(b) For the specification of materials (Mat. No.) that you must use in this Service

Bulletin refer to Consumable Materials List (CML).

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

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

(f) To torque tighten the electrical component fasteners (Refer to AMM Task

20-21-15-912-801).

(g) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(h) Put blanking caps on the disconnected electrical connectors.

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

(j) For the installation of placards (Refer to AMM Task 11-00-00-400-802).

(k) Clean the surfaces at the location of the placards with:

Dry Cleaning

Solvent

(Varsol/White Spirit)

11-002 As required

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 26

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(2) Subtask 285051-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 285051-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

06-41-53, Page Block 001

Task 12-34-24-860-802

Task 52-30-00-010-801

Task 52-30-00-010-802

Task 52-30-00-010-804

52-52-00, Page Block 001

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platform(s) in position.

(c) Open the FWD cargo-compartment door 821 (Refer to AMM 06-41-52, Page Block

001, AMM Task 52-30-00-010-801 or AMM Task 52-30-00-010-802 or AMM Task

52-30-00-010-804).

(d) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(2) Subtask 285051-865-003-001 - C/B Opening

Manpower Resources

Skills NON SPECIFIC

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

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PUMP 1QL1 08 E (1)

721VU FUEL XFR L PUMP 1QL1 05 E (1)

721VU FUEL XFR L PUMP 1QL1 16 F (1)

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 27

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PMP CTL 2QL1 14 R (1)

721VU FUEL XFR L PMP CTL 2QL1 06 S (1)

721VU XFR PMP RCT A SPLY 75QL1 13 F

721VU XFR PMP RCT A CTL 76QL1 17 N

722VU FUEL XFR R PUMP 1QL2 48 G

722VU FUEL XFR R PMP CTL 2QL2 45 Q (1)

722VU FUEL XFR R PMP CTL 2QL2 46 Q (1)

722VU XFR PMP RCT B SPLY 75QL2 33 D (1)

722VU XFR PMP RCT B SPLY 75QL2 32 F (1)

722VU XFR PMP RCT B CTL 76QL2 33 P

NOTE (1): The location of the CB depends on the A/C configuration.

**CONF 002

(1) Subtask 285051-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

06-41-53, Page Block 001

Task 12-34-24-860-802

Task 52-30-00-010-801

Task 52-30-00-010-802

Task 52-30-00-010-804

52-52-00, Page Block 001

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platform(s) in position.

(c) Open the FWD cargo-compartment door 821 (Refer to AMM 06-41-52, Page Block

001, AMM Task 52-30-00-010-801 or AMM Task 52-30-00-010-802 or AMM Task

52-30-00-010-804).

(d) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(2) Subtask 285051-865-003-001 - C/B Opening

Manpower Resources

Skills NON SPECIFIC

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 28

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

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

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PUMP 1QL1 08 E (1)

721VU FUEL XFR L PUMP 1QL1 05 E (1)

721VU FUEL XFR L PUMP 1QL1 16 F (1)

721VU FUEL XFR L PMP CTL 2QL1 14 R (1)

721VU FUEL XFR L PMP CTL 2QL1 06 S (1)

721VU XFR PMP RCT A SPLY 75QL1 13 F

721VU XFR PMP RCT A CTL 76QL1 17 N

722VU FUEL XFR R PUMP 1QL2 48 G

722VU FUEL XFR R PMP CTL 2QL2 45 Q (1)

722VU FUEL XFR R PMP CTL 2QL2 46 Q (1)

722VU XFR PMP RCT B SPLY 75QL2 33 D (1)

722VU XFR PMP RCT B SPLY 75QL2 32 F (1)

722VU XFR PMP RCT B CTL 76QL2 33 P

NOTE (1): The location of the CB depends on the A/C configuration.

**CONF 003

(1) Subtask 285051-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

06-41-53, Page Block 001

Task 12-34-24-860-802

Task 52-30-00-010-801

Task 52-30-00-010-802

Task 52-30-00-010-804

52-52-00, Page Block 001

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platform(s) in position.

(c) Open the FWD cargo-compartment door 821 (Refer to AMM 06-41-52, Page Block

001, AMM Task 52-30-00-010-801 or AMM Task 52-30-00-010-802 or AMM Task

52-30-00-010-804).

(d) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(2) Subtask 285051-865-003-003 - C/B Opening

Manpower Resources

Skills NON SPECIFIC

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 29

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

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

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PUMP 1QL1 08 E (1)

721VU FUEL XFR L PUMP 1QL1 05 E (1)

721VU FUEL XFR L PUMP 1QL1 16 F (1)

721VU FUEL XFR L PMP CTL 2QL1 14 R (1)

721VU FUEL XFR L PMP CTL 2QL1 06 S (1)

722VU FUEL XFR R PUMP 1QL2 48 G

722VU FUEL XFR R PMP CTL 2QL2 45 Q (1)

722VU FUEL XFR R PMP CTL 2QL2 46 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

**CONF 004

(1) Subtask 285051-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

06-41-53, Page Block 001

Task 12-34-24-860-802

Task 52-30-00-010-801

Task 52-30-00-010-802

Task 52-30-00-010-804

52-52-00, Page Block 001

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platform(s) in position.

(c) Open the FWD cargo-compartment door 821 (Refer to AMM 06-41-52, Page Block

001, AMM Task 52-30-00-010-801 or AMM Task 52-30-00-010-802 or AMM Task

52-30-00-010-804).

(d) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(2) Subtask 285051-865-003-004 - C/B Opening

Manpower Resources

Skills NON SPECIFIC

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 30

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

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

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PUMP 1QL1 08 E (1)

721VU FUEL XFR L PUMP 1QL1 05 E (1)

721VU FUEL XFR L PUMP 1QL1 16 F (1)

721VU FUEL XFR L PMP CTL 2QL1 14 R (1)

721VU FUEL XFR L PMP CTL 2QL1 06 S (1)

722VU XFR PMP RCT B SPLY 75QL2 33 D (1)

722VU XFR PMP RCT B SPLY 75QL2 32 F (1)

722VU XFR PMP RCT B CTL 76QL2 33 P

NOTE (1): The location of the CB depends on the A/C configuration.

**CONF 005

(1) Subtask 285051-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

06-41-53, Page Block 001

Task 12-34-24-860-802

Task 52-30-00-010-801

Task 52-30-00-010-802

Task 52-30-00-010-804

52-52-00, Page Block 001

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platform(s) in position.

(c) Open the FWD cargo-compartment door 821 (Refer to AMM 06-41-52, Page Block

001, AMM Task 52-30-00-010-801 or AMM Task 52-30-00-010-802 or AMM Task

52-30-00-010-804).

(d) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(2) Subtask 285051-865-003-004 - C/B Opening

Manpower Resources

Skills NON SPECIFIC

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 31

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

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

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PUMP 1QL1 08 E (1)

721VU FUEL XFR L PUMP 1QL1 05 E (1)

721VU FUEL XFR L PUMP 1QL1 16 F (1)

721VU FUEL XFR L PMP CTL 2QL1 14 R (1)

721VU FUEL XFR L PMP CTL 2QL1 06 S (1)

722VU XFR PMP RCT B SPLY 75QL2 33 D (1)

722VU XFR PMP RCT B SPLY 75QL2 32 F (1)

722VU XFR PMP RCT B CTL 76QL2 33 P

NOTE (1): The location of the CB depends on the A/C configuration.

**CONF 006

(1) Subtask 285051-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

06-41-53, Page Block 001

Task 12-34-24-860-802

Task 52-30-00-010-801

Task 52-30-00-010-802

Task 52-30-00-010-804

52-52-00, Page Block 001

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-860-802).

(b) Put access platform(s) in position.

(c) Open the FWD cargo-compartment door 821 (Refer to AMM 06-41-52, Page Block

001, AMM Task 52-30-00-010-801 or AMM Task 52-30-00-010-802 or AMM Task

52-30-00-010-804).

(d) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(2) Subtask 285051-865-003-005 - C/B Opening

Manpower Resources

Skills NON SPECIFIC

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 32

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

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

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PUMP 1QL1 08 E (1)

721VU FUEL XFR L PUMP 1QL1 05 E (1)

721VU FUEL XFR L PUMP 1QL1 16 F (1)

721VU FUEL XFR L PMP CTL 2QL1 14 R (1)

721VU FUEL XFR L PMP CTL 2QL1 06 S (1)

NOTE (1): The location of the CB depends on the A/C configuration.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 285051-831-001-001 - Modify the Equipment and the Wiring in the LH

Relay Box 751VU

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Electrical panel 751VU

Work location Electrical panel 751VU

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 285051A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 MS21042-04 6 NUT

6 ABS1629-28A0 2 GFI

7 E0673C0S 2 BASE

EN3155-017F1216 6 CONTACT

EN3155-017F1620 4 CONTACT

F9000095226895 BUNDLE

F9100095214695 PLACARD

References

Fig. A-FBAAA

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Sheet 02

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 33

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

References

Fig. A-FBCAA

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Sheet 02

Fig. A-FHAAA

Hook-up Chart

Sheet 01

Fig. A-FHCAA

Hook-up Chart

Sheet 01

Fig. A-FWAAA

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

Fig. A-FWCAA

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Open the LH Relay Box 751VU.

(b) Modify the equipment and the wiring in the LH Relay Box 751VU (Refer to Fig. AFBAAA Sheet 01 and Fig. A-FBAAA Sheet 02).

1 Remove the relay 5QL1 (Refer to Fig. A-FBAAA Sheet 01):

FIN 5QL1

1 Relay E0667A28A0 Item (1) Discard

3 Nut MS21042-04 Item (3) Discard

FIN 5QL1A

1 Base E0673A0S Item (2) Discard

FIN 5QL1

1 Placard Discard

2 Modify the wiring in the LH Relay Box 751VU:

a Modify the connections of the wires as shown in the wiring diagrams Fig.

A-FWAAA Sheet 01 and Fig. A-FWAAA Sheet 02 and as given in the

hook-up chart lines:

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

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 34

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

3 Install the relay GFI 97QL1.

a Install (Refer to Fig. A-FBAAA Sheet 02):

FIN 97QL1A

1 Base E0673C0S Item 7

attach with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

FIN 97QL1

1 GFI ABS1629-28A0 Item 6

NOTE: Tighten the 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).

b Near the relay, bond the placard identified 97QL1 as shown in Fig. AFBAAA Sheet 02, supplied in:

Placard Set F9100095214695

(c) Modify the equipment and the wiring in the LH Relay Box 751VU (Refer to Fig. AFBCAA Sheet 01 and Fig. A-FBCAA Sheet 02).

1 Remove the relay 79QL1 (Refer to Fig. A-FBCAA Sheet 01):

FIN 79QL1

1 Relay E0672D28A0 Item (4) Discard

3 Nut MS21042-04 Item (3) Discard

FIN 79QL1A

1 Base E0311A0S Item (5) Discard

FIN 79QL1

1 Placard Discard

2 Modify the wiring in the LH Relay Box 751VU:

a Remove the wires as shown in the wiring diagram Fig. A-FWCAA Sheet

01 and as given in the Hook-up Chart lines:

- 1 thru 8 (Refer to Fig. A-FHCAA Sheet 01).

b Install the wires as shown in the wiring diagram Fig. A-FWCAA Sheet 02

and as given in the Hook-up Chart lines:

- 12 thru 19 (Refer to Fig. A-FHCAA Sheet 01).

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 35

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

supplied in:

Bundle F9000095226895

3 Install the relay GFI 98QL1.

a Install (Refer to Fig. A-FBCAA Sheet 02):

FIN 98QL1A

1 Base E0673C0S Item 7

attached with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

FIN 98QL1

1 GFI ABS1629-28A0 Item 6

NOTE: Tighten the 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).

b Near the relay, bond the placard identified 98QL1 as shown in Fig. AFBCAA Sheet 02, supplied in:

Placard Set F9100095214695

(d) Close the LH Relay Box 751VU.

(2) Subtask 285051-831-002-001 - Modify the Equipment and the Wiring in the RH

Relay Box 752VU

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Electrical panel 752VU

Work location Electrical panel 752VU

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 36

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Material necessary to do the job

Kit 285051A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 MS21042-04 6 NUT

6 ABS1629-28A0 2 GFI

7 E0673C0S 2 BASE

EN3155-017F1216 12 CONTACT

EN3155-017F1620 8 CONTACT

F9100095214695 PLACARD

References

Fig. A-FBBAA

Modification of the Equipment in the RH

Relay Box 752VU

Sheet 01

Sheet 02

Fig. A-FBDAA

Modification of the Equipment in the RH

Relay Box 752VU

Sheet 01

Sheet 02

Fig. A-FHBAA

Hook-up Chart

Sheet 01

Fig. A-FHDAA

Hook-up Chart

Sheet 01

Fig. A-FWBAA

Modification of the Wiring in the RH

Relay Box 752VU

Sheet 01

Sheet 02

Fig. A-FWDAA

Modification of the Wiring in the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Open the RH Relay Box 752VU.

(b) Modify the equipment and the wiring in the RH Relay Box 752VU (Refer to Fig. AFBBAA Sheet 01 and Fig. A-FBBAA Sheet 02).

1 Remove the relay 5QL2 (Refer to Fig. A-FBBAA Sheet 01):

FIN 5QL2

1 Relay E0667A28A0 Item (1) Discard

3 Nut MS21042-04 Item (3) Discard

FIN 5QL2A

1 Base E0673A0S Item (2) Discard

FIN 5QL2

1 Placard Discard

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 37

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

2 Modify the wiring in the RH Relay Box 752VU:

a Modify the connections of the wires as shown in the wiring diagrams Fig.

A-FWBAA Sheet 01 and Fig. A-FWBAA Sheet 02 and as given in the

hook-up chart lines:

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

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

3 Install the relay GFI 97QL2.

a Install (Refer to Fig. A-FBBAA Sheet 02):

FIN 97QL2A

1 Base E0673C0S Item 7

attach with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

FIN 97QL2

1 GFI ABS1629-28A0 Item 6

NOTE: Tighten the 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).

b Near the relay, bond the placard identified 97QL2 as shown in Fig. AFBBAA Sheet 02, supplied in:

Placard Set F9100095214695

(c) Modify the equipment and the wiring in the RH Relay Box 752VU (Refer to Fig. AFBDAA Sheet 01 and Fig. A-FBDAA Sheet 02).

1 Remove the relay 79QL2 (Refer to Fig. A-FBDAA Sheet 01):

FIN 79QL2

1 Relay E0672D28A0 Item (4) Discard

3 Nut MS21042-04 Item (3) Discard

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 38

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

FIN 79QL2A

1 Base E0311A0S Item (5) Discard

FIN 79QL2

1 Placard Discard

2 Modify the wiring in the RH Relay Box 752VU:

a Modify the connections of the wires as shown in the wiring diagrams Fig.

A-FWDAA Sheet 01 and Fig. A-FWDAA Sheet 02 and as given in the

hook-up chart lines:

- 1 thru 16 (Refer to Fig. A-FHDAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

3 Install the relay GFI 98QL2.

a Install (Refer to Fig. A-FBDAA Sheet 02):

FIN 98QL2A

1 Base E0673C0S Item 7

attach with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

FIN 98QL2

1 GFI ABS1629-28A0 Item 6

NOTE: Tighten the 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).

b Near the relay, bond the placard identified 98QL2 as shown in Fig. AFBDAA Sheet 02, supplied in:

Placard Set F9100095214695

(d) Close the RH Relay Box 752VU.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 39

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 002

(1) Subtask 285051-831-001-002 - Modify the Equipment and the Wiring in the LH

Relay Box 751VU

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Electrical panel 751VU

Work location Electrical panel 751VU

Manpower Resources

Manhours 4.00

Minimum number of person 1

Subtask elapsed time 4.00

Skills ELECTRICAL

Material necessary to do the job

Kit 285051A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 MS21042-04 6 NUT

6 ABS1629-28A0 2 GFI

7 E0673C0S 2 BASE

EN3155-017F1216 6 CONTACT

EN3155-017F1620 4 CONTACT

F9000095226895 BUNDLE

F9100095214695 PLACARD

References

Fig. A-FBAAA

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Sheet 02

Fig. A-FBCAB

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Sheet 02

Fig. A-FHAAA

Hook-up Chart

Sheet 01

Fig. A-FHCAB

Hook-up Chart

Sheet 01

Fig. A-FWAAA

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

Fig. A-FWCAB

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 40

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(a) Open the LH Relay Box 751VU.

(b) Modify the equipment and the wiring in the LH Relay Box 751VU (Refer to Fig. AFBAAA Sheet 01 and Fig. A-FBAAA Sheet 02).

1 Remove the relay 5QL1 (Refer to Fig. A-FBAAA Sheet 01):

FIN 5QL1

1 Relay E0667A28A0 Item (1) Discard

3 Nut MS21042-04 Item (3) Discard

FIN 5QL1A

1 Base E0673A0S Item (2) Discard

FIN 5QL1

1 Placard Discard

2 Modify the wiring in the LH Relay Box 751VU:

a Modify the connections of the wires as shown in the wiring diagrams Fig.

A-FWAAA Sheet 01 and Fig. A-FWAAA Sheet 02 and as given in the

hook-up chart lines:

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

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

3 Install the relay GFI 97QL1.

a Install (Refer to Fig. A-FBAAA Sheet 02):

FIN 97QL1A

1 Base E0673C0S Item 7

attach with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

FIN 97QL1

1 GFI ABS1629-28A0 Item 6

NOTE: Tighten the screws to a torque value comprised between

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

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 41

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

in.lb).

b Near the relay, bond the placard identified 97QL1 as shown in Fig. AFBAAA Sheet 02, supplied in:

Placard Set F9100095214695

(c) Modify the equipment and the wiring in the LH Relay Box 751VU (Refer to Fig. AFBCAB Sheet 01 and Fig. A-FBCAB Sheet 02).

1 Remove the relay 79QL1 (Refer to Fig. A-FBCAB Sheet 01):

FIN 79QL1

1 Relay E0667A28A0 Item (1) Discard

3 Nut MS21042-04 Item (3) Discard

FIN 79QL1A

1 Base E0673A0S Item (2) Discard

FIN 79QL1

1 Placard Discard

2 Modify the wiring in the LH Relay Box 751VU:

a Remove the wires as shown in the wiring diagram Fig. A-FWCAB Sheet

01 and as given in the Hook-up Chart lines:

- 1 thru 10 (Refer to Fig. A-FHCAB Sheet 01).

b Install the wires as shown in the wiring diagram Fig. A-FWCAB Sheet 02

and as given in the Hook-up Chart lines:

- 14 thru 23 (Refer to Fig. A-FHCAB Sheet 01).

supplied in:

Bundle F9000095226895

3 Install the relay GFI 98QL1.

a Install (Refer to Fig. A-FBCAB Sheet 02):

FIN 98QL1A

1 Base E0673C0S Item 7

attached with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 42

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

FIN 98QL1

1 GFI ABS1629-28A0 Item 6

NOTE: Tighten the 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).

b Near the relay, bond the placard identified 98QL1 as shown in Fig. AFBCAB Sheet 02, supplied in:

Placard Set F9100095214695

(d) Close the LH Relay Box 751VU.

(2) Subtask 285051-831-002-002 - Modify the Equipment and the Wiring in the RH

Relay Box 752VU

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Electrical panel 752VU

Work location Electrical panel 752VU

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 285051A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 MS21042-04 6 NUT

6 ABS1629-28A0 2 GFI

7 E0673C0S 2 BASE

EN3155-017F1216 12 CONTACT

EN3155-017F1620 8 CONTACT

F9100095214695 PLACARD

References

Fig. A-FBBAA

Modification of the Equipment in the RH

Relay Box 752VU

Sheet 01

Sheet 02

Fig. A-FBDAB

Modification of the Equipment in the RH

Relay Box 752VU

Sheet 01

Sheet 02

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 43

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

References

Fig. A-FHBAA

Hook-up Chart

Sheet 01

Fig. A-FHDAB

Hook-up Chart

Sheet 01

Fig. A-FWBAA

Modification of the Wiring in the RH

Relay Box 752VU

Sheet 01

Sheet 02

Fig. A-FWDAB

Modification of the Wiring in the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Open the RH Relay Box 752VU.

(b) Modify the equipment and the wiring in the RH Relay Box 752VU (Refer to Fig. AFBBAA Sheet 01 and Fig. A-FBBAA Sheet 02).

1 Remove the relay 5QL2 (Refer to Fig. A-FBBAA Sheet 01):

FIN 5QL2

1 Relay E0667A28A0 Item (1) Discard

3 Nut MS21042-04 Item (3) Discard

FIN 5QL2A

1 Base E0673A0S Item (2) Discard

FIN 5QL2

1 Placard Discard

2 Modify the wiring in the RH Relay Box 752VU:

a Modify the connections of the wires as shown in the wiring diagrams Fig.

A-FWBAA Sheet 01 and Fig. A-FWBAA Sheet 02 and as given in the

hook-up chart lines:

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

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 44

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

3 Install the relay GFI 97QL2.

a Install (Refer to Fig. A-FBBAA Sheet 02):

FIN 97QL2A

1 Base E0673C0S Item 7

attach with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

FIN 97QL2

1 GFI ABS1629-28A0 Item 6

NOTE: Tighten the 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).

b Near the relay, bond the placard identified 97QL2 as shown in Fig. AFBBAA Sheet 02, supplied in:

Placard Set F9100095214695

(c) Modify the equipment and the wiring in the RH Relay Box 752VU (Refer to Fig. AFBDAB Sheet 01 and Fig. A-FBDAB Sheet 02).

1 Remove the relay 79QL2 (Refer to Fig. A-FBDAB Sheet 01):

FIN 79QL2

1 Relay E0667A28A0 Item (1) Discard

3 Nut MS21042-04 Item (3) Discard

FIN 79QL2A

1 Base E0673A0S Item (2) Discard

FIN 79QL2

1 Placard Discard

2 Modify the wiring in the RH Relay Box 752VU:

a Modify the connections of the wires as shown in the wiring diagrams Fig.

A-FWDAB Sheet 01 and Fig. A-FWDAB Sheet 02 and as given in the

hook-up chart lines:

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

NOTE: If necessary, use:

6 Contact EN3155-017F1216

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 45

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

and

4 Contact EN3155-017F1620

3 Install the relay GFI 98QL2.

a Install (Refer to Fig. A-FBDAB Sheet 02):

FIN 98QL2A

1 Base E0673C0S Item 7

attach with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

FIN 98QL2

1 GFI ABS1629-28A0 Item 6

NOTE: Tighten the 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).

b Near the relay, bond the placard identified 98QL2 as shown in Fig. AFBDAB Sheet 02, supplied in:

Placard Set F9100095214695

(d) Close the RH Relay Box 752VU.

**CONF 003

(1) Subtask 285051-831-001-003 - Modify the Equipment and the Wiring in the LH

Relay Box 751VU

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Electrical panel 751VU

Work location Electrical panel 751VU

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills ELECTRICAL

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 46

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Material necessary to do the job

Kit 285051A02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 MS21042-04 3 NUT

6 ABS1629-28A0 1 GFI

7 E0673C0S 1 BASE

EN3155-017F1216 6 CONTACT

EN3155-017F1620 4 CONTACT

F9100095214795 PLACARD

References

Fig. A-FBAAA

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Sheet 02

Fig. A-FHAAA

Hook-up Chart

Sheet 01

Fig. A-FWAAA

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Open the LH Relay Box 751VU.

(b) Modify the equipment and the wiring in the LH Relay Box 751VU (Refer to Fig. AFBAAA Sheet 01 and Fig. A-FBAAA Sheet 02).

1 Remove the relay 5QL1 (Refer to Fig. A-FBAAA Sheet 01):

FIN 5QL1

1 Relay E0667A28A0 Item (1) Discard

3 Nut MS21042-04 Item (3) Discard

FIN 5QL1A

1 Base E0673A0S Item (2) Discard

FIN 5QL1

1 Placard Discard

2 Modify the wiring in the LH Relay Box 751VU:

a Modify the connections of the wires as shown in the wiring diagrams Fig.

A-FWAAA Sheet 01 and Fig. A-FWAAA Sheet 02 and as given in the

hook-up chart lines:

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

NOTE: If necessary, use:

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 47

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

3 Install the relay GFI 97QL1.

a Install (Refer to Fig. A-FBAAA Sheet 02):

FIN 97QL1A

1 Base E0673C0S Item 7

attach with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

FIN 97QL1

1 GFI ABS1629-28A0 Item 6

NOTE: Tighten the 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).

b Near the relay, bond the placard identified 97QL1 as shown in Fig. AFBAAA Sheet 02, supplied in:

Placard Set F9100095214795

(c) Close the LH Relay Box 751VU.

(2) Subtask 285051-831-002-003 - Modify the Equipment and the Wiring in the RH

Relay Box 752VU

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Electrical panel 752VU

Work location Electrical panel 752VU

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills ELECTRICAL

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 48

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Material necessary to do the job

Kit 285051A02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 MS21042-04 3 NUT

6 ABS1629-28A0 1 GFI

7 E0673C0S 1 BASE

EN3155-017F1216 6 CONTACT

EN3155-017F1620 4 CONTACT

F9100095214795 PLACARD

References

Fig. A-FBBAA

Modification of the Equipment in the RH

Relay Box 752VU

Sheet 01

Sheet 02

Fig. A-FHBAA

Hook-up Chart

Sheet 01

Fig. A-FWBAA

Modification of the Wiring in the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Open the RH Relay Box 752VU.

(b) Modify the equipment and the wiring in the RH Relay Box 752VU (Refer to Fig. AFBBAA Sheet 01 and Fig. A-FBBAA Sheet 02).

1 Remove the relay 5QL2 (Refer to Fig. A-FBBAA Sheet 01):

FIN 5QL2

1 Relay E0667A28A0 Item (1) Discard

3 Nut MS21042-04 Item (3) Discard

FIN 5QL2A

1 Base E0673A0S Item (2) Discard

FIN 5QL2

1 Placard Discard

2 Modify the wiring in the RH Relay Box 752VU:

a Modify the connections of the wires as shown in the wiring diagrams Fig.

A-FWBAA Sheet 01 and Fig. A-FWBAA Sheet 02 and as given in the

hook-up chart lines:

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

NOTE: If necessary, use:

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 49

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

3 Install the relay GFI 97QL2.

a Install (Refer to Fig. A-FBBAA Sheet 02):

FIN 97QL2A

1 Base E0673C0S Item 7

attach with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

FIN 97QL2

1 GFI ABS1629-28A0 Item 6

NOTE: Tighten the 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).

b Near the relay, bond the placard identified 97QL2 as shown in Fig. AFBBAA Sheet 02, supplied in:

Placard Set F9100095214795

(c) Close the RH Relay Box 752VU.

**CONF 004

(1) Subtask 285051-831-001-004 - Modify the Equipment and the Wiring in the LH

Relay Box 751VU

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Electrical panel 751VU

Work location Electrical panel 751VU

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills ELECTRICAL

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 50

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Material necessary to do the job

Kit 285051A03R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 MS21042-04 3 NUT

6 ABS1629-28A0 1 GFI

7 E0673C0S 1 BASE

EN3155-017F1216 6 CONTACT

EN3155-017F1620 4 CONTACT

F9100095214895 PLACARD

References

Fig. A-FBAAA

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Sheet 02

Fig. A-FHAAA

Hook-up Chart

Sheet 01

Fig. A-FWAAA

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Open the LH Relay Box 751VU.

(b) Modify the equipment and the wiring in the LH Relay Box 751VU (Refer to Fig. AFBAAA Sheet 01 and Fig. A-FBAAA Sheet 02).

1 Remove the relay 5QL1 (Refer to Fig. A-FBAAA Sheet 01):

FIN 5QL1

1 Relay E0667A28A0 Item (1) Discard

3 Nut MS21042-04 Item (3) Discard

FIN 5QL1A

1 Base E0673A0S Item (2) Discard

FIN 5QL1

1 Placard Discard

2 Modify the wiring in the LH Relay Box 751VU:

a Modify the connections of the wires as shown in the wiring diagrams Fig.

A-FWAAA Sheet 01 and Fig. A-FWAAA Sheet 02 and as given in the

hook-up chart lines:

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

NOTE: If necessary, use:

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 51

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

3 Install the relay GFI 97QL1.

a Install (Refer to Fig. A-FBAAA Sheet 02):

FIN 97QL1A

1 Base E0673C0S Item 7

attach with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

FIN 97QL1

1 GFI ABS1629-28A0 Item 6

NOTE: Tighten the 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).

b Near the relay, bond the placard identified 97QL1 as shown in Fig. AFBAAA Sheet 02, supplied in:

Placard Set F9100095214895

(c) Close the LH Relay Box 751VU.

(2) Subtask 285051-831-002-004 - Modify the Equipment and the Wiring in the RH

Relay Box 752VU

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Electrical panel 752VU

Work location Electrical panel 752VU

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills ELECTRICAL

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 52

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Material necessary to do the job

Kit 285051A03R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 MS21042-04 3 NUT

6 ABS1629-28A0 1 GFI

7 E0673C0S 1 BASE

EN3155-017F1216 6 CONTACT

EN3155-017F1620 4 CONTACT

F9100095214895 PLACARD

References

Fig. A-FBDAA

Modification of the Equipment in the RH

Relay Box 752VU

Sheet 01

Sheet 02

Fig. A-FHDAA

Hook-up Chart

Sheet 01

Fig. A-FWDAA

Modification of the Wiring in the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Open the RH Relay Box 752VU.

(b) Modify the equipment and the wiring in the RH Relay Box 752VU (Refer to Fig. AFBDAA Sheet 01 and Fig. A-FBDAA Sheet 02).

1 Remove the relay 79QL2 (Refer to Fig. A-FBDAA Sheet 01):

FIN 79QL2

1 Relay E0672D28A0 Item (4) Discard

3 Nut MS21042-04 Item (3) Discard

FIN 79QL2A

1 Base E0311A0S Item (5) Discard

FIN 79QL2

1 Placard Discard

2 Modify the wiring in the RH Relay Box 752VU:

a Modify the connections of the wires as shown in the wiring diagrams Fig.

A-FWDAA Sheet 01 and Fig. A-FWDAA Sheet 02 and as given in the

hook-up chart lines:

- 1 thru 16 (Refer to Fig. A-FHDAA Sheet 01).

NOTE: If necessary, use:

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 53

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

3 Install the relay GFI 98QL2.

a Install (Refer to Fig. A-FBDAA Sheet 02):

FIN 98QL2A

1 Base E0673C0S Item 7

attach with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

FIN 98QL2

1 GFI ABS1629-28A0 Item 6

NOTE: Tighten the 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).

b Near the relay, bond the placard identified 98QL2 as shown in Fig. AFBDAA Sheet 02, supplied in:

Placard Set F9100095214895

(c) Close the RH Relay Box 752VU.

**CONF 005

(1) Subtask 285051-831-001-005 - Modify the Equipment and the Wiring in the LH

Relay Box 751VU

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Electrical panel 751VU

Work location Electrical panel 751VU

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills ELECTRICAL

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 54

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Material necessary to do the job

Kit 285051A03R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 MS21042-04 3 NUT

6 ABS1629-28A0 1 GFI

7 E0673C0S 1 BASE

EN3155-017F1216 6 CONTACT

EN3155-017F1620 4 CONTACT

F9100095214895 PLACARD

References

Fig. A-FBAAA

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Sheet 02

Fig. A-FHAAA

Hook-up Chart

Sheet 01

Fig. A-FWAAA

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Open the LH Relay Box 751VU.

(b) Modify the equipment and the wiring in the LH Relay Box 751VU (Refer to Fig. AFBAAA Sheet 01 and Fig. A-FBAAA Sheet 02).

1 Remove the relay 5QL1 (Refer to Fig. A-FBAAA Sheet 01):

FIN 5QL1

1 Relay E0667A28A0 Item (1) Discard

3 Nut MS21042-04 Item (3) Discard

FIN 5QL1A

1 Base E0673A0S Item (2) Discard

FIN 5QL1

1 Placard Discard

2 Modify the wiring in the LH Relay Box 751VU:

a Modify the connections of the wires as shown in the wiring diagrams Fig.

A-FWAAA Sheet 01 and Fig. A-FWAAA Sheet 02 and as given in the

hook-up chart lines:

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

NOTE: If necessary, use:

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 55

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

3 Install the relay GFI 97QL1.

a Install (Refer to Fig. A-FBAAA Sheet 02):

FIN 97QL1A

1 Base E0673C0S Item 7

attach with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

FIN 97QL1

1 GFI ABS1629-28A0 Item 6

NOTE: Tighten the 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).

b Near the relay, bond the placard identified 97QL1 as shown in Fig. AFBAAA Sheet 02, supplied in:

Placard Set F9100095214895

(c) Close the LH Relay Box 751VU.

(2) Subtask 285051-831-002-005 - Modify the Equipment and the Wiring in the RH

Relay Box 752VU

Work Zones and Access Panels

Zone Access/Work location

122 Access Door 821, Door 132AZ

Electrical panel 752VU

Work location Panel 752VU

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills ELECTRICAL

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 56

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Material necessary to do the job

Kit 285051A03R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 MS21042-04 3 NUT

6 ABS1629-28A0 1 GFI

7 E0673C0S 1 BASE

EN3155-017F1216 6 CONTACT

EN3155-017F1620 4 CONTACT

F9100095214895 PLACARD

References

Fig. A-FBDAB

Modification of the Equipment in the RH

Relay Box 752VU

Sheet 01

Sheet 02

Fig. A-FHDAB

Hook-up Chart

Sheet 01

Fig. A-FWDAB

Modification of the Wiring in the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Open the RH Relay Box 752VU.

(b) Modify the equipment and the wiring in the RH Relay Box 752VU (Refer to Fig. AFBDAB Sheet 01 and Fig. A-FBDAB Sheet 02).

1 Remove the relay 79QL2 (Refer to Fig. A-FBDAB Sheet 01):

FIN 79QL2

1 Relay E0667A28A0 Item (1) Discard

3 Nut MS21042-04 Item (3) Discard

FIN 79QL2A

1 Base E0673A0S Item (2) Discard

FIN 79QL2

1 Placard Discard

2 Modify the wiring in the RH Relay Box 752VU:

a Modify the connections of the wires as shown in the wiring diagrams Fig.

A-FWDAB Sheet 01 and Fig. A-FWDAB Sheet 02 and as given in the

hook-up chart lines:

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

NOTE: If necessary, use:

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 57

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

3 Install the relay GFI 98QL2.

a Install (Refer to Fig. A-FBDAB Sheet 02):

FIN 98QL2A

1 Base E0673C0S Item 7

attach with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

FIN 98QL2

1 GFI ABS1629-28A0 Item 6

NOTE: Tighten the 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).

b Near the relay, bond the placard identified 98QL2 as shown in Fig. AFBDAB Sheet 02, supplied in:

Placard Set F9100095214895

(c) Close the RH Relay Box 752VU.

**CONF 006

(1) Subtask 285051-831-001-006 - Modify the Equipment and the Wiring in the LH

Relay Box 751VU

Work Zones and Access Panels

Zone Access/Work location

121 Access Door 821, Door 132AZ

Electrical panel 751VU

Work location Electrical panel 751VU

Manpower Resources

Manhours 1.50

Minimum number of person 1

Subtask elapsed time 1.50

Skills ELECTRICAL

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 58

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Material necessary to do the job

Kit 285051A04R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 MS21042-04 3 NUT

6 ABS1629-28A0 1 GFI

7 E0673C0S 1 BASE

EN3155-017F1216 6 CONTACT

EN3155-017F1620 4 CONTACT

F9100095214995 PLACARD

References

Fig. A-FBAAA

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Sheet 02

Fig. A-FHAAA

Hook-up Chart

Sheet 01

Fig. A-FWAAA

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Open the LH Relay Box 751VU.

(b) Modify the equipment and the wiring in the LH Relay Box 751VU (Refer to Fig. AFBAAA Sheet 01 and Fig. A-FBAAA Sheet 02).

1 Remove the relay 5QL1 (Refer to Fig. A-FBAAA Sheet 01):

FIN 5QL1

1 Relay E0667A28A0 Item (1) Discard

3 Nut MS21042-04 Item (3) Discard

FIN 5QL1A

1 Base E0673A0S Item (2) Discard

FIN 5QL1

1 Placard Discard

2 Modify the wiring in the LH Relay Box 751VU:

a Modify the connections of the wires as shown in the wiring diagrams Fig.

A-FWAAA Sheet 01 and Fig. A-FWAAA Sheet 02 and as given in the

hook-up chart lines:

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

NOTE: If necessary, use:

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 59

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

3 Install the relay GFI 97QL1.

a Install (Refer to Fig. A-FBAAA Sheet 02):

FIN 97QL1A

1 Base E0673C0S Item 7

attach with:

3 Nut MS21042-04 Item 3

NOTE: Tighten the three nuts item 3 to a torque value 0.10

m.daN (8.851 in.lb).

FIN 97QL1

1 GFI ABS1629-28A0 Item 6

NOTE: Tighten the 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).

b Near the relay, bond the placard identified 97QL1 as shown in Fig. AFBAAA Sheet 02, supplied in:

Placard Set F9100095214995

(c) Close the LH Relay Box 751VU.

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 285051-865-004-001 - C/B Closing

Manpower Resources

Skills NON SPECIFIC

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

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PUMP 1QL1 08 E (1)

721VU FUEL XFR L PUMP 1QL1 05 E (1)

721VU FUEL XFR L PUMP 1QL1 16 F (1)

721VU FUEL XFR L PMP CTL 2QL1 14 R (1)

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 60

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PMP CTL 2QL1 06 S (1)

721VU XFR PMP RCT A SPLY 75QL1 13 F

721VU XFR PMP RCT A CTL 76QL1 17 N

722VU FUEL XFR R PUMP 1QL2 48 G

722VU FUEL XFR R PMP CTL 2QL2 45 Q (1)

722VU FUEL XFR R PMP CTL 2QL2 46 Q (1)

722VU XFR PMP RCT B SPLY 75QL2 33 D (1)

722VU XFR PMP RCT B SPLY 75QL2 32 F (1)

722VU XFR PMP RCT B CTL 76QL2 33 P

NOTE (1): The location of the CB depends on the A/C configuration.

(2) Subtask 285051-800-401-001 - Preparation for Test Procedure

Work Zones and Access Panels

Zone Access/Work location

121 Work location Electrical panel 751VU

122 Work location Electrical panel 752VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Fig. A-UBAAA

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

(a) Examine the ABS1629-28A0 Ground Fault Interrupters (GFI), FIN 97QL1

1 On the panel 751VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAA Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 97QL1) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(b) Examine the ABS1629-28A0 GFI, FIN 97QL2

1 On the panel 752VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAA Sheet 01).

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 61

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 97QL2) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(c) Examine the ABS1629-28A0 GFI, FIN 98QL1

1 On the panel 751VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAA Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 98QL1) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(d) Examine the ABS1629-28A0 GFI, FIN 98QL2

1 On the panel 752VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAA Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 98QL2) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(3) Subtask 285051-710-402-001 - Test of the Ground Fault Interrupter - 97QL1

Work Zones and Access Panels

Zone Access/Work location

121 Work location Electrical panel 751VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-801

Fig. A-UBAAA

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 62

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Left-hand Pump)

1 On the panel 245VU, set the Push-Button Switch (P/BSW) FIN 15QL (CTR TK

TO INR XFR) to MAN (manual) (Refer to Fig. A-UBAAA Sheet 02).

2 Push the P/BSW FIN 3QL1 (CTR TK L) to operate the transfer fuel pump FIN

600QL1:

a Make sure that the transfer fuel pump FIN 600QL1 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL1 (CTR TK L) to stop the transfer fuel pump

FIN 600QL1.

3 Operate the transfer fuel pump FIN 600QL1 (to do a ground transfer) to move

some of the fuel from the center tank (Refer to AMM Task 28-25-00-869-801):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

97QL1, on the panel 751VU (Refer to Fig. A-UBAAA Sheet 01).

b Make sure that the GFI FIN 97QL1 trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 3QL1 (CTR TK L).

4 Push the P/BSW FIN 3QL1 (CTR TK L) to set the transfer fuel pump FIN

600QL1 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

5 On the panel 751VU, push in the trip RESET button of the GFI FIN 97QL1

until it latches in the closed (not tripped) position. Make sure that you cannot

see the metal shaft (Refer to Fig. A-UBAAA Sheet 01).

6 Push the P/BSW FIN 3QL1 (CTR TK L) to operate the transfer fuel pump FIN

600QL1:

a Make sure that the transfer fuel pump FIN 600QL1 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL1 (CTR TK L) to stop the transfer fuel pump

FIN 600QL1.

7 On the panel 245VU, push the P/BSW FIN 15QL (CTR TK TO INR XFR) to

de-select MAN (manual) mode (Refer to Fig. A-UBAAA Sheet 02).

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 63

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(4) Subtask 285051-710-403-001 - Test of Ground Fault Interrupter - 97QL2

Work Zones and Access Panels

Zone Access/Work location

122 Work location Electrical panel 752VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-801

Fig. A-UBAAA

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Right-hand Pump)

1 On the panel 245VU, set the Push-Button Switch (P/BSW) FIN 15QL (CTR TK

TO INR XFR) to MAN (manual) (Refer to Fig. A-UBAAA Sheet 02).

2 Push the P/BSW FIN 3QL2 (CTR TK R) to operate the transfer fuel pump FIN

600QL2

a Make sure that the transfer fuel pump FIN 600QL2 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL2 (CTR TK R) to stop the transfer fuel pump

FIN 600QL2.

3 Operate the transfer fuel pump FIN 600QL2 (to do a ground transfer) to move

some of the fuel from the center tank (Refer to AMM Task 28-25-00-869-801):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

97QL2, on the panel 752VU (Refer to Fig. A-UBAAA Sheet 01).

b Make sure that the GFI FIN 97QL2 trips (the metal shaft on the trip

RESET indicator comes out).

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 64

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 3QL2 (CTR TK R).

4 Push the P/BSW FIN 3QL2 (CTR TK R) to set the transfer fuel pump FIN

600QL2 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

5 On the panel 752VU, push in the trip RESET button of the GFI FIN 97QL2

until it latches in the closed (not tripped) position. Make sure you cannot see

the metal shaft (Refer to Fig. A-UBAAA Sheet 01).

6 Push the P/BSW FIN 3QL2 (CTR TK R) to operate the transfer fuel pump FIN

600QL2:

a Make sure that the transfer fuel pump FIN 600QL2 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL2 (CTR TK R) to stop the transfer fuel pump

FIN 600QL2.

7 On the panel 245VU, push the P/BSW FIN 15QL1 (CTR TK TO INR XFR) to

de-select MAN (manual) mode (Refer to Fig. A-UBAAA Sheet 02).

(5) Subtask 285051-710-404-003 - Test of Ground Fault Interrupter - 98QL1

Work Zones and Access Panels

Zone Access/Work location

121 Work location Electrical panel 751VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-801

Fig. A-UBAAA

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

WARNING: MAKE SURE THAT THE REAR CENTER TANK HAS SUFFICIENT

FUEL TO MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT

RUN IN THE DRY CONDITION.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 65

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(a) Do a Fuel Transfer Test (Pump A)

1 On the panel 245VU, set the P/BSW FIN 89QL (RCT XFR) to FWD (Refer to

Fig. A-UBAAA Sheet 02).

2 Push the P/BSW FIN 77QL1 (RCT PUMP A) to operate the transfer fuel pump

FIN 608QL1:

a Make sure that the transfer fuel pump FIN 608QL1 operates correctly (to

move some of the fuel from the rear center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 77QL1 (RCT PUMP A) to stop the transfer fuel

pump FIN 608QL1.

3 Operate the transfer fuel pump FIN 608QL1 (to do a ground transfer) to

move some of the fuel from the rear center tank (Refer to AMM Task

28-25-00-869-801):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

98QL1, on the panel 751VU (Refer to Fig. A-UBAAA Sheet 01).

b Make sure that the GFI FIN 98QL1 trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 77QL1 (RCT PUMP A).

4 Push the P/BSW FIN 77QL1 (RCT PUMP A) to set the transfer fuel pump FIN

608QL1 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

5 On the panel 751VU, push in the trip RESET button of the GFI FIN 98QL1

until it latches in the closed (not tripped) position. Make sure that you cannot

see the metal shaft (Refer to Fig. A-UBAAA Sheet 01).

6 Push the P/BSW FIN 77QL1 (RCT PUMP A) to operate the transfer fuel pump

FIN 608QL1:

a Make sure that the transfer fuel pump FIN 608QL1 operates correctly (to

move some of the fuel from the rear center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 77QL1 (RCT PUMP A) to stop the transfer fuel

pump FIN 608QL1.

7 On the panel 245VU, push the P/BSW FIN 89QL (RCT XFR ) to de-select

FWD mode (Refer to Fig. A-UBAAA Sheet 02).

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 66

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(6) Subtask 285051-710-405-001 - Test of Ground Fault Interrupter - 98QL2

Work Zones and Access Panels

Zone Access/Work location

122 Work location Electrical panel 752VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-801

Fig. A-UBAAA

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

WARNING: MAKE SURE THAT THE REAR CENTER TANK HAS SUFFICIENT

FUEL TO MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT

RUN IN THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Pump B)

1 On the panel 245VU, set the P/BSW FIN 89QL (RCT XFR) to FWD (Refer to

Fig. A-UBAAA Sheet 02).

2 Push the P/BSW FIN 77QL2 (RCT PUMP B) to operate the transfer fuel pump

FIN 608QL2:

a Make sure that the transfer fuel pump FIN 608QL2 operates correctly (to

move some of the fuel from the rear center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 77QL2 (RCT PUMP B) to stop the transfer fuel

pump FIN 608QL2.

3 Operate the transfer fuel pump FIN 608QL2 (to do a ground transfer) to

move some of the fuel from the rear center tank (Refer to AMM Task

28-25-00-869-801):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

98QL2, on the panel 752VU.

b Make sure that the GFI FIN 98QL2 trips (the metal shaft on the trip

RESET indicator comes out).

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 67

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 77QL2 (RCT PUMP B).

4 Push the P/BSW FIN 77QL2 (RCT PUMP B) to set the transfer fuel pump FIN

608QL2 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

5 On the panel 752VU, push in the trip RESET button of the GFI FIN 98QL2

until it latches in the closed (not tripped) position. Make sure that you cannot

see the metal shaft (Refer to Fig. A-UBAAA Sheet 01).

6 Push the P/BSW FIN 77QL2 (RCT PUMP B) to operate the transfer fuel pump

FIN 608QL2:

a Make sure that the transfer fuel pump FIN 608QL2 operates correctly (to

move some of the fuel from the rear center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 77QL2 (RCT PUMP B) to stop the transfer fuel

pump FIN 608QL2.

7 On the panel 245VU, push the P/BSW FIN 89QL (RCT XFR ) to de-select

FWD mode (Refer to Fig. A-UBAAA Sheet 02).

**CONF 002

(1) Subtask 285051-865-004-001 - C/B Closing

Manpower Resources

Skills NON SPECIFIC

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

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PUMP 1QL1 08 E (1)

721VU FUEL XFR L PUMP 1QL1 05 E (1)

721VU FUEL XFR L PUMP 1QL1 16 F (1)

721VU FUEL XFR L PMP CTL 2QL1 14 R (1)

721VU FUEL XFR L PMP CTL 2QL1 06 S (1)

721VU XFR PMP RCT A SPLY 75QL1 13 F

721VU XFR PMP RCT A CTL 76QL1 17 N

722VU FUEL XFR R PUMP 1QL2 48 G

722VU FUEL XFR R PMP CTL 2QL2 45 Q (1)

722VU FUEL XFR R PMP CTL 2QL2 46 Q (1)

722VU XFR PMP RCT B SPLY 75QL2 33 D (1)

722VU XFR PMP RCT B SPLY 75QL2 32 F (1)

722VU XFR PMP RCT B CTL 76QL2 33 P

NOTE (1): The location of the CB depends on the A/C configuration.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 68

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(2) Subtask 285051-800-401-001 - Preparation for Test Procedure

Work Zones and Access Panels

Zone Access/Work location

121 Work location Electrical panel 751VU

122 Work location Electrical panel 752VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Fig. A-UBAAA

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

(a) Examine the ABS1629-28A0 Ground Fault Interrupters (GFI), FIN 97QL1

1 On the panel 751VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAA Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 97QL1) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(b) Examine the ABS1629-28A0 GFI, FIN 97QL2

1 On the panel 752VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAA Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 97QL2) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(c) Examine the ABS1629-28A0 GFI, FIN 98QL1

1 On the panel 751VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAA Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 98QL1) until it latches in the closed (not tripped)

position.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 69

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

3 Make sure that you cannot see the metal shaft.

(d) Examine the ABS1629-28A0 GFI, FIN 98QL2

1 On the panel 752VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAA Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 98QL2) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(3) Subtask 285051-710-402-001 - Test of the Ground Fault Interrupter - 97QL1

Work Zones and Access Panels

Zone Access/Work location

121 Work location Electrical panel 751VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-801

Fig. A-UBAAA

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Left-hand Pump)

1 On the panel 245VU, set the Push-Button Switch (P/BSW) FIN 15QL (CTR TK

TO INR XFR) to MAN (manual) (Refer to Fig. A-UBAAA Sheet 02).

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 70

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

2 Push the P/BSW FIN 3QL1 (CTR TK L) to operate the transfer fuel pump FIN

600QL1:

a Make sure that the transfer fuel pump FIN 600QL1 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL1 (CTR TK L) to stop the transfer fuel pump

FIN 600QL1.

3 Operate the transfer fuel pump FIN 600QL1 (to do a ground transfer) to move

some of the fuel from the center tank (Refer to AMM Task 28-25-00-869-801):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

97QL1, on the panel 751VU (Refer to Fig. A-UBAAA Sheet 01).

b Make sure that the GFI FIN 97QL1 trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 3QL1 (CTR TK L).

4 Push the P/BSW FIN 3QL1 (CTR TK L) to set the transfer fuel pump FIN

600QL1 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

5 On the panel 751VU, push in the trip RESET button of the GFI FIN 97QL1

until it latches in the closed (not tripped) position. Make sure that you cannot

see the metal shaft (Refer to Fig. A-UBAAA Sheet 01).

6 Push the P/BSW FIN 3QL1 (CTR TK L) to operate the transfer fuel pump FIN

600QL1:

a Make sure that the transfer fuel pump FIN 600QL1 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL1 (CTR TK L) to stop the transfer fuel pump

FIN 600QL1.

7 On the panel 245VU, push the P/BSW FIN 15QL (CTR TK TO INR XFR) to

de-select MAN (manual) mode (Refer to Fig. A-UBAAA Sheet 02).

(4) Subtask 285051-710-403-001 - Test of Ground Fault Interrupter - 97QL2

Work Zones and Access Panels

Zone Access/Work location

122 Work location Electrical panel 752VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 71

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

191

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-801

Fig. A-UBAAA

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Right-hand Pump)

1 On the panel 245VU, set the Push-Button Switch (P/BSW) FIN 15QL (CTR TK

TO INR XFR) to MAN (manual) (Refer to Fig. A-UBAAA Sheet 02).

2 Push the P/BSW FIN 3QL2 (CTR TK R) to operate the transfer fuel pump FIN

600QL2

a Make sure that the transfer fuel pump FIN 600QL2 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL2 (CTR TK R) to stop the transfer fuel pump

FIN 600QL2.

3 Operate the transfer fuel pump FIN 600QL2 (to do a ground transfer) to move

some of the fuel from the center tank (Refer to AMM Task 28-25-00-869-801):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

97QL2, on the panel 752VU (Refer to Fig. A-UBAAA Sheet 01).

b Make sure that the GFI FIN 97QL2 trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 3QL2 (CTR TK R).

4 Push the P/BSW FIN 3QL2 (CTR TK R) to set the transfer fuel pump FIN

600QL2 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 72

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

5 On the panel 752VU, push in the trip RESET button of the GFI FIN 97QL2

until it latches in the closed (not tripped) position. Make sure you cannot see

the metal shaft (Refer to Fig. A-UBAAA Sheet 01).

6 Push the P/BSW FIN 3QL2 (CTR TK R) to operate the transfer fuel pump FIN

600QL2:

a Make sure that the transfer fuel pump FIN 600QL2 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL2 (CTR TK R) to stop the transfer fuel pump

FIN 600QL2.

7 On the panel 245VU, push the P/BSW FIN 15QL1 (CTR TK TO INR XFR) to

de-select MAN (manual) mode (Refer to Fig. A-UBAAA Sheet 02).

(5) Subtask 285051-710-404-003 - Test of Ground Fault Interrupter - 98QL1

Work Zones and Access Panels

Zone Access/Work location

121 Work location Electrical panel 751VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-801

Fig. A-UBAAA

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

WARNING: MAKE SURE THAT THE REAR CENTER TANK HAS SUFFICIENT

FUEL TO MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT

RUN IN THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Pump A)

1 On the panel 245VU, set the P/BSW FIN 89QL (RCT XFR) to FWD (Refer to

Fig. A-UBAAA Sheet 02).

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 73

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

2 Push the P/BSW FIN 77QL1 (RCT PUMP A) to operate the transfer fuel pump

FIN 608QL1:

a Make sure that the transfer fuel pump FIN 608QL1 operates correctly (to

move some of the fuel from the rear center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 77QL1 (RCT PUMP A) to stop the transfer fuel

pump FIN 608QL1.

3 Operate the transfer fuel pump FIN 608QL1 (to do a ground transfer) to

move some of the fuel from the rear center tank (Refer to AMM Task

28-25-00-869-801):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

98QL1, on the panel 751VU (Refer to Fig. A-UBAAA Sheet 01).

b Make sure that the GFI FIN 98QL1 trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 77QL1 (RCT PUMP A).

4 Push the P/BSW FIN 77QL1 (RCT PUMP A) to set the transfer fuel pump FIN

608QL1 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

5 On the panel 751VU, push in the trip RESET button of the GFI FIN 98QL1

until it latches in the closed (not tripped) position. Make sure that you cannot

see the metal shaft (Refer to Fig. A-UBAAA Sheet 01).

6 Push the P/BSW FIN 77QL1 (RCT PUMP A) to operate the transfer fuel pump

FIN 608QL1:

a Make sure that the transfer fuel pump FIN 608QL1 operates correctly (to

move some of the fuel from the rear center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 77QL1 (RCT PUMP A) to stop the transfer fuel

pump FIN 608QL1.

7 On the panel 245VU, push the P/BSW FIN 89QL (RCT XFR ) to de-select

FWD mode (Refer to Fig. A-UBAAA Sheet 02).

(6) Subtask 285051-710-405-001 - Test of Ground Fault Interrupter - 98QL2

Work Zones and Access Panels

Zone Access/Work location

122 Work location Electrical panel 752VU

211 Work location Electrical panel 245VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 74

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-801

Fig. A-UBAAA

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

WARNING: MAKE SURE THAT THE REAR CENTER TANK HAS SUFFICIENT

FUEL TO MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT

RUN IN THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Pump B)

1 On the panel 245VU, set the P/BSW FIN 89QL (RCT XFR) to FWD (Refer to

Fig. A-UBAAA Sheet 02).

2 Push the P/BSW FIN 77QL2 (RCT PUMP B) to operate the transfer fuel pump

FIN 608QL2:

a Make sure that the transfer fuel pump FIN 608QL2 operates correctly (to

move some of the fuel from the rear center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 77QL2 (RCT PUMP B) to stop the transfer fuel

pump FIN 608QL2.

3 Operate the transfer fuel pump FIN 608QL2 (to do a ground transfer) to

move some of the fuel from the rear center tank (Refer to AMM Task

28-25-00-869-801):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

98QL2, on the panel 752VU.

b Make sure that the GFI FIN 98QL2 trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 77QL2 (RCT PUMP B).

4 Push the P/BSW FIN 77QL2 (RCT PUMP B) to set the transfer fuel pump FIN

608QL2 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 75

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

5 On the panel 752VU, push in the trip RESET button of the GFI FIN 98QL2

until it latches in the closed (not tripped) position. Make sure that you cannot

see the metal shaft (Refer to Fig. A-UBAAA Sheet 01).

6 Push the P/BSW FIN 77QL2 (RCT PUMP B) to operate the transfer fuel pump

FIN 608QL2:

a Make sure that the transfer fuel pump FIN 608QL2 operates correctly (to

move some of the fuel from the rear center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 77QL2 (RCT PUMP B) to stop the transfer fuel

pump FIN 608QL2.

7 On the panel 245VU, push the P/BSW FIN 89QL (RCT XFR ) to de-select

FWD mode (Refer to Fig. A-UBAAA Sheet 02).

**CONF 003

(1) Subtask 285051-865-004-003 - C/B Closing

Manpower Resources

Skills NON SPECIFIC

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

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PUMP 1QL1 08 E (1)

721VU FUEL XFR L PUMP 1QL1 05 E (1)

721VU FUEL XFR L PUMP 1QL1 16 F (1)

721VU FUEL XFR L PMP CTL 2QL1 14 R (1)

721VU FUEL XFR L PMP CTL 2QL1 06 S (1)

722VU FUEL XFR R PUMP 1QL2 48 G

722VU FUEL XFR R PMP CTL 2QL2 45 Q (1)

722VU FUEL XFR R PMP CTL 2QL2 46 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

(2) Subtask 285051-800-401-003 - Preparation for Test Procedure

Work Zones and Access Panels

Zone Access/Work location

121 Work location Electrical panel 751VU

122 Work location Electrical panel 752VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 76

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

Manpower Resources

Skills ELECTRICAL

References

Fig. A-UBAAB

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

(a) Examine the ABS1629-28A0 Ground Fault Interrupters (GFI), FIN 97QL1

1 On the panel 751VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to.Fig. AUBAAB Sheet 01).

2 If the metal shafts are in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 97QL1) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(b) Examine the ABS1629-28A0 GFI, FIN 97QL2

1 On the Panel 752VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAB Sheet 01).

2 If the metal shafts are in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 97QL2) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(3) Subtask 285051-710-402-003 - Test of the Ground Fault Interrupter - 97QL1

Work Zones and Access Panels

Zone Access/Work location

121 Work location Electrical panel 751VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-801

Fig. A-UBAAB

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 77

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Left-hand Pump)

1 On the panel 245VU, set the Push-Button Switch (P/BSW) FIN 15QL1 (CTR

TK TO INR XFR) to MAN (manual) (Refer to Fig. A-UBAAB Sheet 02).

2 Push the P/BSW FIN 3QL1 (CTR TK L) to operate the transfer fuel pump FIN

600QL1:

a Make sure that the transfer fuel pump FIN 600QL1 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL1 (CTR TK L) to stop the transfer fuel pump

FIN 600QL1.

3 Operate the transfer fuel pump FIN 600QL1 (to do a ground transfer) to move

some of the fuel from the center tank (Refer to AMM Task 28-25-00-869-801):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

97QL1, on the panel 751VU (Refer to Fig. A-UBAAB Sheet 01).

b Make sure that the GFI FIN 97QL1 trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 3QL1 (CTR TK L).

4 Push the P/BSW FIN 3QL1 (CTR TK L) to set the transfer fuel pump FIN

600QL1 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

5 On the panel 751VU, push in the trip RESET button of the GFI FIN 97QL1

until it latches in the closed (not tripped) position. Make sure that you cannot

see the metal shaft (Refer to Fig. A-UBAAB Sheet 01).

6 Push the P/BSW FIN 3QL1 (CTR TK L) to operate the transfer fuel pump FIN

600QL1:

a Make sure that the transfer fuel pump FIN 600QL1 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL1 (CTR TK L) to stop the transfer fuel pump

FIN 600QL1.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 78

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

7 On the panel 245VU, push the P/BSW FIN 15QL (CTR TK TO INR XFR) to

de-select MAN (manual) mode (Refer to Fig. A-UBAAB Sheet 02).

(4) Subtask 285051-710-403-003 - Test of Ground Fault Interrupter - 97QL2

Work Zones and Access Panels

Zone Access/Work location

122 Work location Electrical panel 752VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-801

Fig. A-UBAAB

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Right-hand Pump)

1 On the panel 245VU, set the Push-Button Switch (P/BSW) FIN 15QL (CTR TK

TO INR XFR) to MAN (manual) (Refer to Fig. A-UBAAB Sheet 02).

2 Push the P/BSW FIN 3QL2 (CTR TK R) to operate the transfer fuel pump FIN

600QL2

a Make sure that the transfer fuel pump FIN 600QL2 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL2 (CTR TK R) to stop the transfer fuel pump

FIN 600QL2.

3 Operate the transfer fuel pump FIN 600QL2 (to do a ground transfer) to move

some of the fuel from the center tank (Refer to AMM Task 28-25-00-869-801):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

97QL2, on the panel 752VU (Refer to Fig. A-UBAAB Sheet 01).

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 79

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

b Make sure that the GFI FIN 97QL2 trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 3QL2 (CTR TK R).

4 Push the P/BSW FIN 3QL2 (CTR TK R) to set the transfer fuel pump FIN

600QL2 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

5 On the panel 752VU, push in the trip RESET button of the GFI FIN 97QL2

until it latches in the closed (not tripped) position. Make sure you cannot see

the metal shaft (Refer to Fig. A-UBAAB Sheet 01).

6 Push the P/BSW FIN 3QL2 (CTR TK R) to operate the transfer fuel pump FIN

600QL2:

a Make sure that the transfer fuel pump FIN 600QL2 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL2 (CTR TK R) to stop the transfer fuel pump

FIN 600QL2.

7 On the panel 245VU, push the P/BSW FIN 15QL1 (CTR TK TO INR XFR) to

de-select MAN (manual) mode (Refer to Fig. A-UBAAB Sheet 02).

**CONF 004

(1) Subtask 285051-865-004-004 - C/B Closing

Manpower Resources

Skills NON SPECIFIC

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

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PUMP 1QL1 08 E (1)

721VU FUEL XFR L PUMP 1QL1 05 E (1)

721VU FUEL XFR L PUMP 1QL1 16 F (1)

721VU FUEL XFR L PMP CTL 2QL1 14 R (1)

721VU FUEL XFR L PMP CTL 2QL1 06 S (1)

722VU XFR PMP RCT B SPLY 75QL2 33 D (1)

722VU XFR PMP RCT B SPLY 75QL2 32 F (1)

722VU XFR PMP RCT B CTL 76QL2 33 P

NOTE (1): The location of the CB depends on the A/C configuration.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 80

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(2) Subtask 285051-800-401-006 - Preparation for Test Procedure

Work Zones and Access Panels

Zone Access/Work location

121 Work location Electrical panel 751VU

122 Access Electrical panel 752VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Fig. A-UBAAC

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

(a) Examine the ABS1629-28A0 Ground Fault Interrupters (GFI), FIN 97QL1

1 On the panel 751VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAC Sheet 01).

2 If the metal shafts are in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 97QL1) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(b) Examine the ABS1629-28A0 GFI, FIN 98QL2

1 On the panel 752VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAC Sheet 01).

2 If the metal shafts are in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 98QL2) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(3) Subtask 285051-710-402-004 - Test of the Ground Fault Interrupter - 97QL1

Work Zones and Access Panels

Zone Access/Work location

121 Work location Electrical panel 751VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 81

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-801

Fig. A-UBAAC

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Left-hand Pump)

1 On the panel 245VU, set the Push-Button Switch (P/BSW) FIN 15QL1 (CTR

TK TO INR XFR) to MAN (manual) (Refer to Fig. A-UBAAC Sheet 02).

2 Push the P/BSW FIN 3QL1 (CTR TK L) to operate the transfer fuel pump FIN

600QL1:

a Make sure that the transfer fuel pump FIN 600QL1 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL1 (CTR TK L) to stop the transfer fuel pump

FIN 600QL1.

3 Operate the transfer fuel pump FIN 600QL1 (to do a ground transfer) to move

some of the fuel from the center tank (Refer to AMM Task 28-25-00-869-801):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

97QL1, on the panel 751VU (Refer to Fig. A-UBAAC Sheet 01).

b Make sure that the GFI FIN 97QL1 trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 3QL1 (CTR TK L).

4 Push the P/BSW FIN 3QL1 (CTR TK L) to set the transfer fuel pump FIN

600QL1 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 82

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

5 On the panel 751VU, push in the trip RESET button of the GFI FIN 97QL1

until it latches in the closed (not tripped) position. Make sure that you cannot

see the metal shaft (Refer to Fig. A-UBAAC Sheet 01).

6 Push the P/BSW FIN 3QL1 (CTR TK L) to operate the transfer fuel pump FIN

600QL1:

a Make sure that the transfer fuel pump FIN 600QL1 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL1 (CTR TK L) to stop the transfer fuel pump

FIN 600QL1.

7 On the panel 245VU, push the P/BSW FIN 15QL (CTR TK TO INR XFR) to

de-select MAN (manual) mode (Refer to Fig. A-UBAAC Sheet 02).

(4) Subtask 285051-710-405-003 - Test of Ground Fault Interrupter - 98QL2

Work Zones and Access Panels

Zone Access/Work location

122 Work location Electrical panel 752VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-801

Fig. A-UBAAC

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

WARNING: MAKE SURE THAT THE REAR CENTER TANK HAS SUFFICIENT

FUEL TO MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT

RUN IN THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Pump B)

1 On the panel 245VU, set the P/BSW FIN 89QL (RCT XFR) to FWD (Refer to

Fig. A-UBAAC Sheet 02).

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 83

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

2 Push the P/BSW FIN 77QL2 (RCT PUMP B) to operate the transfer fuel pump

FIN 608QL2:

a Make sure that the transfer fuel pump FIN 608QL2 operates correctly (to

move some of the fuel from the rear center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 77QL2 (RCT PUMP B) to stop the transfer fuel

pump FIN 608QL2.

3 Operate the transfer fuel pump FIN 608QL2 (to do a ground transfer) to

move some of the fuel from the rear center tank (Refer to AMM Task

28-25-00-869-801):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

98QL2, on the panel 752VU (Refer to Fig. A-UBAAC Sheet 01).

b Make sure that the GFI FIN 98QL2 trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 77QL2 (RCT PUMP B).

4 Push the P/BSW FIN 77QL2 (RCT PUMP B) to set the transfer fuel pump FIN

608QL2 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

5 On the panel 752VU, push in the trip RESET button of the GFI FIN 98QL2

until it latches in the closed (not tripped) position. Make sure that you cannot

see the metal shaft (Refer to Fig. A-UBAAC Sheet 01).

6 Push the P/BSW FIN 77QL2 (RCT PUMP B) to operate the transfer fuel pump

FIN 608QL2:

a Make sure that the transfer fuel pump FIN 608QL2 operates correctly (to

move some of the fuel from the rear center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 77QL2 (RCT PUMP B) to stop the transfer fuel

pump FIN 608QL2.

7 On the panel 245VU, push the P/BSW FIN 89QL (RCT XFR ) to de-select

FWD mode (Refer to Fig. A-UBAAC Sheet 02).

**CONF 005

(1) Subtask 285051-865-004-004 - C/B Closing

Manpower Resources

Skills NON SPECIFIC

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 84

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

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

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PUMP 1QL1 08 E (1)

721VU FUEL XFR L PUMP 1QL1 05 E (1)

721VU FUEL XFR L PUMP 1QL1 16 F (1)

721VU FUEL XFR L PMP CTL 2QL1 14 R (1)

721VU FUEL XFR L PMP CTL 2QL1 06 S (1)

722VU XFR PMP RCT B SPLY 75QL2 33 D (1)

722VU XFR PMP RCT B SPLY 75QL2 32 F (1)

722VU XFR PMP RCT B CTL 76QL2 33 P

NOTE (1): The location of the CB depends on the A/C configuration.

(2) Subtask 285051-800-401-006 - Preparation for Test Procedure

Work Zones and Access Panels

Zone Access/Work location

121 Work location Electrical panel 751VU

122 Access Electrical panel 752VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Fig. A-UBAAC

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

(a) Examine the ABS1629-28A0 Ground Fault Interrupters (GFI), FIN 97QL1

1 On the panel 751VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAC Sheet 01).

2 If the metal shafts are in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 97QL1) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(b) Examine the ABS1629-28A0 GFI, FIN 98QL2

1 On the panel 752VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAC Sheet 01).

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 85

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

2 If the metal shafts are in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 98QL2) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(3) Subtask 285051-710-402-004 - Test of the Ground Fault Interrupter - 97QL1

Work Zones and Access Panels

Zone Access/Work location

121 Work location Electrical panel 751VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-801

Fig. A-UBAAC

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Left-hand Pump)

1 On the panel 245VU, set the Push-Button Switch (P/BSW) FIN 15QL1 (CTR

TK TO INR XFR) to MAN (manual) (Refer to Fig. A-UBAAC Sheet 02).

2 Push the P/BSW FIN 3QL1 (CTR TK L) to operate the transfer fuel pump FIN

600QL1:

a Make sure that the transfer fuel pump FIN 600QL1 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL1 (CTR TK L) to stop the transfer fuel pump

FIN 600QL1.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 86

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

3 Operate the transfer fuel pump FIN 600QL1 (to do a ground transfer) to move

some of the fuel from the center tank (Refer to AMM Task 28-25-00-869-801):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

97QL1, on the panel 751VU (Refer to Fig. A-UBAAC Sheet 01).

b Make sure that the GFI FIN 97QL1 trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 3QL1 (CTR TK L).

4 Push the P/BSW FIN 3QL1 (CTR TK L) to set the transfer fuel pump FIN

600QL1 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

5 On the panel 751VU, push in the trip RESET button of the GFI FIN 97QL1

until it latches in the closed (not tripped) position. Make sure that you cannot

see the metal shaft (Refer to Fig. A-UBAAC Sheet 01).

6 Push the P/BSW FIN 3QL1 (CTR TK L) to operate the transfer fuel pump FIN

600QL1:

a Make sure that the transfer fuel pump FIN 600QL1 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL1 (CTR TK L) to stop the transfer fuel pump

FIN 600QL1.

7 On the panel 245VU, push the P/BSW FIN 15QL (CTR TK TO INR XFR) to

de-select MAN (manual) mode (Refer to Fig. A-UBAAC Sheet 02).

(4) Subtask 285051-710-405-003 - Test of Ground Fault Interrupter - 98QL2

Work Zones and Access Panels

Zone Access/Work location

122 Work location Electrical panel 752VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-801

Fig. A-UBAAC

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 87

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

WARNING: MAKE SURE THAT THE REAR CENTER TANK HAS SUFFICIENT

FUEL TO MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT

RUN IN THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Pump B)

1 On the panel 245VU, set the P/BSW FIN 89QL (RCT XFR) to FWD (Refer to

Fig. A-UBAAC Sheet 02).

2 Push the P/BSW FIN 77QL2 (RCT PUMP B) to operate the transfer fuel pump

FIN 608QL2:

a Make sure that the transfer fuel pump FIN 608QL2 operates correctly (to

move some of the fuel from the rear center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 77QL2 (RCT PUMP B) to stop the transfer fuel

pump FIN 608QL2.

3 Operate the transfer fuel pump FIN 608QL2 (to do a ground transfer) to

move some of the fuel from the rear center tank (Refer to AMM Task

28-25-00-869-801):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

98QL2, on the panel 752VU (Refer to Fig. A-UBAAC Sheet 01).

b Make sure that the GFI FIN 98QL2 trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 77QL2 (RCT PUMP B).

4 Push the P/BSW FIN 77QL2 (RCT PUMP B) to set the transfer fuel pump FIN

608QL2 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

5 On the panel 752VU, push in the trip RESET button of the GFI FIN 98QL2

until it latches in the closed (not tripped) position. Make sure that you cannot

see the metal shaft (Refer to Fig. A-UBAAC Sheet 01).

6 Push the P/BSW FIN 77QL2 (RCT PUMP B) to operate the transfer fuel pump

FIN 608QL2:

a Make sure that the transfer fuel pump FIN 608QL2 operates correctly (to

move some of the fuel from the rear center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-801).

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 88

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

b Push the P/BSW FIN 77QL2 (RCT PUMP B) to stop the transfer fuel

pump FIN 608QL2.

7 On the panel 245VU, push the P/BSW FIN 89QL (RCT XFR ) to de-select

FWD mode (Refer to Fig. A-UBAAC Sheet 02).

**CONF 006

(1) Subtask 285051-865-004-005 - C/B Closing

Manpower Resources

Skills NON SPECIFIC

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

PANEL DESIGNATION FIN LOCATION SEE

NOTES

721VU FUEL XFR L PUMP 1QL1 08 E (1)

721VU FUEL XFR L PUMP 1QL1 05 E (1)

721VU FUEL XFR L PUMP 1QL1 16 F (1)

721VU FUEL XFR L PMP CTL 2QL1 14 R (1)

721VU FUEL XFR L PMP CTL 2QL1 06 S (1)

NOTE (1): The location of the CB depends on the A/C configuration.

(2) Subtask 285051-800-401-005 - Preparation for Test Procedure

Work Zones and Access Panels

Zone Access/Work location

121 Access Electrical panel 751VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Fig. A-UBAAD

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

(a) Examine the ABS1629-28A0 Ground Fault Interrupters (GFI), FIN 97QL1

1 On the panel 751VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAD Sheet 01).

2 If the metal shafts are in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 97QL1) until it latches in the closed (not tripped)

position.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 89

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

3 Make sure that you cannot see the metal shaft.

(3) Subtask 285051-710-402-005 - Test of the Ground Fault Interrupter - 97QL1

Work Zones and Access Panels

Zone Access/Work location

121 Work location Electrical panel 751VU

211 Work location Electrical panel 245VU

212 Work location Electrical panel 245VU

191

192

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-801

Fig. A-UBAAD

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

WARNING: MONITOR THE MOVEMENT OF FUEL VERY CAREFULLY DURING

THE GROUND FUEL TRANSFER. MOVEMENT OF FUEL TO THE

TRIM TANK CAN CAUSE THE AIRCRAFT TO OVERBALANCE.

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Left-hand Pump)

1 On the panel 245VU, set the Push-Button Switch (P/BSW) FIN 15QL1 (CTR

TK TO INR XFR) to MAN (manual) (Refer to Fig. A-UBAAD Sheet 02).

2 Push the P/BSW FIN 3QL1 (CTR TK L) to operate the transfer fuel pump FIN

600QL1:

a Make sure that the transfer fuel pump FIN 600QL1 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL1 (CTR TK L) to stop the transfer fuel pump

FIN 600QL1.

3 Operate the transfer fuel pump FIN 600QL1 (to do a ground transfer) to move

some of the fuel from the center tank (Refer to AMM Task 28-25-00-869-801):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

97QL1, on the panel 751VU (Refer to Fig. A-UBAAD Sheet 01).

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 90

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

b Make sure that the GFI FIN 97QL1 trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 3QL1 (CTR TK L).

4 Push the P/BSW FIN 3QL1 (CTR TK L) to set the transfer fuel pump FIN

600QL1 to OFF. Make sure that the illuminated FAULT legend goes off and

the OFF legend illuminates on the related P/BSW.

5 On the panel 751VU, push in the trip RESET button of the GFI FIN 97QL1

until it latches in the closed (not tripped) position. Make sure that you cannot

see the metal shaft (Refer to Fig. A-UBAAD Sheet 01).

6 Push the P/BSW FIN 3QL1 (CTR TK L) to operate the transfer fuel pump FIN

600QL1:

a Make sure that the transfer fuel pump FIN 600QL1 operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-801).

b Push the P/BSW FIN 3QL1 (CTR TK L) to stop the transfer fuel pump

FIN 600QL1.

7 On the panel 245VU, push the P/BSW FIN 15QL1 (CTR TK TO INR XFR) to

de-select MAN (manual) mode (Refer to Fig. A-UBAAD Sheet 02).

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 285051-410-001-001 - Install/Close Items Removed/Opened for access

Manpower Resources

Skills NON SPECIFIC

References

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

06-41-53, Page Block 001

Task 52-30-00-410-801

Task 52-30-00-410-802

Task 52-30-00-410-804

52-52-00, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Close the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 91

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(c) Close the FWD cargo-compartment door 821 (Refer to AMM 06-41-52, Page Block

001, AMM Task 52-30-00-410-801, AMM Task 52-30-00-410-802, AMM Task

52-30-00-410-804).

(d) Remove the access platform(s).

(e) Restore the systems and the aircraft to normal operating condition.

**CONF 002

(1) Subtask 285051-410-001-001 - Install/Close Items Removed/Opened for access

Manpower Resources

Skills NON SPECIFIC

References

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

06-41-53, Page Block 001

Task 52-30-00-410-801

Task 52-30-00-410-802

Task 52-30-00-410-804

52-52-00, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Close the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(c) Close the FWD cargo-compartment door 821 (Refer to AMM 06-41-52, Page Block

001, AMM Task 52-30-00-410-801, AMM Task 52-30-00-410-802, AMM Task

52-30-00-410-804).

(d) Remove the access platform(s).

(e) Restore the systems and the aircraft to normal operating condition.

**CONF 003

(1) Subtask 285051-410-001-001 - Install/Close Items Removed/Opened for access

Manpower Resources

Skills NON SPECIFIC

References

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

06-41-53, Page Block 001

Task 52-30-00-410-801

Task 52-30-00-410-802

Task 52-30-00-410-804

52-52-00, Page Block 001

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 92

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

(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 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(c) Close the FWD cargo-compartment door 821 (Refer to AMM 06-41-52, Page Block

001, AMM Task 52-30-00-410-801, AMM Task 52-30-00-410-802, AMM Task

52-30-00-410-804).

(d) Remove the access platform(s).

(e) Restore the systems and the aircraft to normal operating condition.

**CONF 004

(1) Subtask 285051-410-001-001 - Install/Close Items Removed/Opened for access

Manpower Resources

Skills NON SPECIFIC

References

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

06-41-53, Page Block 001

Task 52-30-00-410-801

Task 52-30-00-410-802

Task 52-30-00-410-804

52-52-00, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Close the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(c) Close the FWD cargo-compartment door 821 (Refer to AMM 06-41-52, Page Block

001, AMM Task 52-30-00-410-801, AMM Task 52-30-00-410-802, AMM Task

52-30-00-410-804).

(d) Remove the access platform(s).

(e) Restore the systems and the aircraft to normal operating condition.

**CONF 005

(1) Subtask 285051-410-001-001 - Install/Close Items Removed/Opened for access

Manpower Resources

Skills NON SPECIFIC

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 93

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

References

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

06-41-53, Page Block 001

Task 52-30-00-410-801

Task 52-30-00-410-802

Task 52-30-00-410-804

52-52-00, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Close the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(c) Close the FWD cargo-compartment door 821 (Refer to AMM 06-41-52, Page Block

001, AMM Task 52-30-00-410-801, AMM Task 52-30-00-410-802, AMM Task

52-30-00-410-804).

(d) Remove the access platform(s).

(e) Restore the systems and the aircraft to normal operating condition.

**CONF 006

(1) Subtask 285051-410-001-001 - Install/Close Items Removed/Opened for access

Manpower Resources

Skills NON SPECIFIC

References

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

06-41-53, Page Block 001

Task 52-30-00-410-801

Task 52-30-00-410-802

Task 52-30-00-410-804

52-52-00, Page Block 001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Close the door 132AZ (Refer to AMM 06-41-53, Page Block 001 and AMM

52-52-00, Page Block 001).

(c) Close the FWD cargo-compartment door 821 (Refer to AMM 06-41-52, Page Block

001, AMM Task 52-30-00-410-801, AMM Task 52-30-00-410-802, AMM Task

52-30-00-410-804).

(d) Remove the access platform(s).

(e) Restore the systems and the aircraft to normal operating condition.

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 94

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

BEFORE

B D

H

A

B

C

FR20

FR15A

FR14

FR1

751VU

A

66

5QL1

C

5QL1

(3 POS)

(2)

(1)

(3)

F_SB_285051_5_BAAA_01_03

Figure A-FBAAA - Sheet 01

Modification of the Equipment in the LH Relay Box 751VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 95

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

AFTER

H

(3 POS)

D

E

E

3

7

6

97QL1 ELECTRICAL BONDING

66

97QL1

F_SB_285051_5_BAAA_02_03

Figure A-FBAAA - Sheet 02

Modification of the Equipment in the LH Relay Box 751VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 96

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001 thru 003

BEFORE

A

H

A

B

FR20

FR15A

FR14

FR1

752VU

5QL2

B

D

3

C

(3 POS)

(2)

(1)

(3)

5QL2

C

F_SB_285051_5_BBAA_01_03

Figure A-FBBAA - Sheet 01

Modification of the Equipment in the RH Relay Box 752VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 97

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001 thru 003

AFTER

(3 POS)

D

E

97QL2

3

7

6

ELECTRICAL BONDING

E

97QL2

B

87

F_SB_285051_5_BBAA_02_03

Figure A-FBBAA - Sheet 02

Modification of the Equipment in the RH Relay Box 752VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 98

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001

BEFORE

(3 POS) (3)

FR20

FR15A

FR14

FR1 D

A

A

L M

79QL1

79QL1 59

C

B

B

C

(5)

(4)

751VU

F_SB_285051_5_BCAA_01_02

Figure A-FBCAA - Sheet 01

Modification of the Equipment in the LH Relay Box 751VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 99

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001

H

(3 POS)

87

ELECTRICAL BONDING

98QL1

D

3

6

7

98QL1

E

AFTER

E

F_SB_285051_5_BCAA_02_03

Figure A-FBCAA - Sheet 02

Modification of the Equipment in the LH Relay Box 751VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 100

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 002

BEFORE

(3 POS) (3)

FR20

FR15A

FR14

FR1 D

A

A

L M

79QL1

79QL1 59

C

B

B

C

(2)

(1)

751VU

F_SB_285051_5_BCAB_01_02

Figure A-FBCAB - Sheet 01

Modification of the Equipment in the LH Relay Box 751VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 101

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 002

H

(3 POS)

87

ELECTRICAL BONDING

98QL1

D

3

6

7

98QL1

E

AFTER

E

F_SB_285051_5_BCAB_02_03

Figure A-FBCAB - Sheet 02

Modification of the Equipment in the LH Relay Box 751VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 102

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001, 004

87

F

(3 POS)

C

(4)

(5)

(3)

79QL2

BEFORE

B D

A

752VU

FR20

FR15A

FR14

FR1 A

79QL2

B C

F_SB_285051_5_BDAA_01_03

Figure A-FBDAA - Sheet 01

Modification of the Equipment in the RH Relay Box 752VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 103

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001, 004

(3 POS)

87

ELECTRICAL BONDING

D

3

6

7

E

98QL2

98QL2

AFTER

E

F_SB_285051_5_BDAA_02_03

Figure A-FBDAA - Sheet 02

Modification of the Equipment in the RH Relay Box 752VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 104

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 002, 005

87

F

(3 POS)

C

(1)

(2)

(3)

79QL2

BEFORE

B D

A

752VU

FR20

FR15A

FR14

FR1 A

79QL2

B C

F_SB_285051_5_BDAB_01_03

Figure A-FBDAB - Sheet 01

Modification of the Equipment in the RH Relay Box 752VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 105

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 002, 005

(3 POS)

87

ELECTRICAL BONDING

D

3

6

7

E

98QL2

98QL2

AFTER

E

F_SB_285051_5_BDAB_02_03

Figure A-FBDAB - Sheet 02

Modification of the Equipment in the RH Relay Box 752VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 106

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FWAAA - Sheet 01

Modification of the Wiring in the LH Relay Box 751VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 107

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF ALL

Figure A-FWAAA - Sheet 02

Modification of the Wiring in the LH Relay Box 751VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 108

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

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 751VU 5QL1−A C1 2826−0056 B 1M QG16 751VU 1521VC 42 M1O

 2 751VU 97QL1−A C2 EN3155−017F1216 2826−0056 B 1M QG16 751VU 1521VC 42 M1N

 3 751VU 5QL1−A A1 2826−0056 R 1M QG16 751VU 1521VC 40 M1O

 4 751VU 97QL1−A A2 EN3155−017F1216 2826−0056 R 1M QG16 751VU 1521VC 40 M1N

 5 751VU 5QL1−A B1 2826−0056 Y 1M QG16 751VU 1521VC 41 M1O

 6 751VU 97QL1−A B2 EN3155−017F1216 2826−0056 Y 1M QG16 751VU 1521VC 41 M1N

 7 751VU 5QL1−A C2 2826−0057 B 1M QG16 751VU 1521VC 45 M1O

 8 751VU 97QL1−A C1 EN3155−017F1216 2826−0057 B 1M QG16 751VU 1521VC 45 M1N

 9 751VU 5QL1−A A2 2826−0057 R 1M QG16 751VU 1521VC 43 M1O

10 751VU 97QL1−A A1 EN3155−017F1216 2826−0057 R 1M QG16 751VU 1521VC 43 M1N

11 751VU 5QL1−A B2 2826−0057 Y 1M QG16 751VU 1521VC 44 M1O

12 751VU 97QL1−A B1 EN3155−017F1216 2826−0057 Y 1M QG16 751VU 1521VC 44 M1N

13 751VU 5QL1−A 12 2826−0059 1M DK24 751VU 1407VG GND M1O

14 751VU 97QL1−A 13 EN3155−017F1620 2826−0059 1M DK24 751VU 1407VG GND M1N

15 751VU 5QL1−A X2 2826−0063 1M DK24 751VU 17QL−A D2 M1O

16 751VU 97QL1−A X2 EN3155−017F1620 2826−0063 1M DK24 751VU 17QL−A D2 M1N

17 751VU 5QL1−A X1 2826−0070 1M DK24 751VU 1517VC 1 M1O

18 751VU 97QL1−A X1 EN3155−017F1620 2826−0070 1M DK24 751VU 1517VC 1 M1N

19 751VU 5QL1−A 13 2826−0090 1M DK24 751VU 1521VC 1 M1O

20 751VU 97QL1−A 12 EN3155−017F1620 2826−0090 1M DK24 751VU 1521VC 1 M1N

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

 GND = GROUND

Figure A-FHAAA - Sheet 01

Hook-up Chart

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 109

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001 thru 003

Figure A-FWBAA - Sheet 01

Modification of the Wiring in the RH Relay Box 752VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 110

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001 thru 003

Figure A-FWBAA - Sheet 02

Modification of the Wiring in the RH Relay Box 752VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 111

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001 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 752VU 5QL2−A C1 2826−0092 B 2M QG16 752VU 1536VC 42 M1O

 2 752VU 97QL2−A C2 EN3155−017F1216 2826−0092 B 2M QG16 752VU 1536VC 42 M1N

 3 752VU 5QL2−A A1 2826−0092 R 2M QG16 752VU 1536VC 40 M1O

 4 752VU 97QL2−A A2 EN3155−017F1216 2826−0092 R 2M QG16 752VU 1536VC 40 M1N

 5 752VU 5QL2−A B1 2826−0092 Y 2M QG16 752VU 1536VC 41 M1O

 6 752VU 97QL2−A B2 EN3155−017F1216 2826−0092 Y 2M QG16 752VU 1536VC 41 M1N

 7 752VU 5QL2−A X2 2826−0095 2M DK24 752VU 1528VC 24 M1O

 8 752VU 97QL2−A X2 EN3155−017F1620 2826−0095 2M DK24 752VU 1528VC 24 M1N

 9 752VU 5QL2−A 12 2826−0099 2M DK24 752VU 1402VG / M1O

10 752VU 97QL2−A 13 EN3155−017F1620 2826−0099 2M DK24 752VU 1402VG / M1N

11 752VU 5QL2−A X1 2826−0105 2M DK24 752VU 1528VC 23 M1O

12 752VU 97QL2−A X1 EN3155−017F1620 2826−0105 2M DK24 752VU 1528VC 23 M1N

13 752VU 5QL2−A 13 2826−0108 2M DK24 752VU 1536VC 5 M1O

14 752VU 97QL2−A 12 EN3155−017F1620 2826−0108 2M DK24 752VU 1536VC 5 M1N

15 752VU 5QL2−A C2 2826−0110 B 2M QG16 752VU 1536VC 45 M1O

16 752VU 97QL2−A C1 EN3155−017F1216 2826−0110 B 2M QG16 752VU 1536VC 45 M1N

17 752VU 5QL2−A A2 2826−0110 R 2M QG16 752VU 1536VC 43 M1O

18 752VU 97QL2−A A1 EN3155−017F1216 2826−0110 R 2M QG16 752VU 1536VC 43 M1N

19 752VU 5QL2−A B2 2826−0110 Y 2M QG16 752VU 1536VC 44 M1O

20 752VU 97QL2−A B1 EN3155−017F1216 2826−0110 Y 2M QG16 752VU 1536VC 44 M1N

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

 GND = GROUND

Figure A-FHBAA - Sheet 01

Hook-up Chart

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 112

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001

Figure A-FWCAA - Sheet 01

Modification of the Wiring in the LH Relay Box 751VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 113

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001

Figure A-FWCAA - Sheet 02

Modification of the Wiring in the LH Relay Box 751VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 114

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 002

Figure A-FWCAB - Sheet 01

Modification of the Wiring in the LH Relay Box 751VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 115

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 002

Figure A-FWCAB - Sheet 02

Modification of the Wiring in the LH Relay Box 751VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 116

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001

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 751VU 79QL1−A C2 2826−1528 B 1M QG12 751VU 1445VC 3 D

 2 751VU 79QL1−A A2 2826−1528 R 1M QG12 751VU 1445VC 1 D

 3 751VU 79QL1−A B2 2826−1528 Y 1M QG12 751VU 1445VC 2 D

 4 751VU 79QL1−A X1 2826−1548 1M DK24 751VU 1525VC 23 D

 5 751VU 79QL1−A X2 2826−1549 1M DK24 751VU 1513VT 7D D

 6 751VU 79QL1−A C1 2826−1620 B 1M QG12 751VU 1513VT 19K D

 7 751VU 79QL1−A A1 2826−1620 R 1M QG12 751VU 1513VT 16F D

 8 751VU 79QL1−A B1 2826−1620 Y 1M QG12 751VU 1513VT 17D D

 9

10

11

12 751VU 98QL1−A C1 EN3155−017F1212 2826−1528 B 1M QG12 5000 200 751VU 1445VC 3 EN3155−008M1212 (a) A

13 751VU 98QL1−A A1 EN3155−017F1212 2826−1528 R 1M QG12 5000 200 751VU 1445VC 1 EN3155−008M1212 (a) A

14 751VU 98QL1−A B1 EN3155−017F1212 2826−1528 Y 1M QG12 5000 200 751VU 1445VC 2 EN3155−008M1212 (a) A

15 751VU 98QL1−A X1 EN3155−017F1620 2826−1548 1M DK24 5000 200 751VU 1525VC 23 EN3155−008M2222 (a) A

16 751VU 98QL1−A X2 EN3155−017F1620 2826−1549 1M DK24 5000 200 751VU 1513VT 7D EN3155−016M2222 (a) A

17 751VU 98QL1−A C2 EN3155−017F1212 2826−1620 B 1M QG12 5000 200 751VU 1513VT 19K EN3155−016M1212 (a) A

18 751VU 98QL1−A A2 EN3155−017F1212 2826−1620 R 1M QG12 5000 200 751VU 1513VT 16F EN3155−016M1212 (a) A

19 751VU 98QL1−A B2 EN3155−017F1212 2826−1620 Y 1M QG12 5000 200 751VU 1513VT 17D EN3155−016M1212 (a) A

20

21

22

23

24

25

 (a) = BUNDLE F9000095226895

 A = ADDED WIRE

 D = DELETED WIRE

Figure A-FHCAA - Sheet 01

Hook-up Chart

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 117

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 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 751VU 79QL1−A C2 2826−1528 B 1M QG12 751VU 1445VC 3 D

 2 751VU 79QL1−A A2 2826−1528 R 1M QG12 751VU 1445VC 1 D

 3 751VU 79QL1−A B2 2826−1528 Y 1M QG12 751VU 1445VC 2 D

 4 751VU 79QL1−A C1 2826−1529 B 1M QG12 751VU 1445VC 6 D

 5 751VU 79QL1−A A1 2826−1529 R 1M QG12 751VU 1445VC 4 D

 6 751VU 79QL1−A B1 2826−1529 Y 1M QG12 751VU 1445VC 5 D

 7 751VU 79QL1−A 12 2826−1531 1M DK24 751VU 1421VG / D

 8 751VU 79QL1−A 13 2826−1545 1M DK24 751VU 1513VT 7M D

 9 751VU 79QL1−A X1 2826−1548 1M DK24 751VU 1525VC 23 D

10 751VU 79QL1−A X2 2826−1549 1M DK24 751VU 1513VT 7D D

11

12

13

14 751VU 98QL1−A A1 EN3155−017F1212 2826−1528 R 1M QG12 5000 200 751VU 1445VC 1 EN3155−008M1212 (a) A

15 751VU 98QL1−A B1 EN3155−017F1212 2826−1528 Y 1M QG12 5000 200 751VU 1445VC 2 EN3155−008M1212 (a) A

16 751VU 98QL1−A C1 EN3155−017F1212 2826−1528 B 1M QG12 5000 200 751VU 1445VC 3 EN3155−008M1212 (a) A

17 751VU 98QL1−A C2 EN3155−017F1212 2826−1529 B 1M QG12 5000 200 751VU 1445VC 6 EN3155−008M1212 (a) A

18 751VU 98QL1−A A2 EN3155−017F1212 2826−1529 R 1M QG12 5000 200 751VU 1445VC 4 EN3155−008M1212 (a) A

19 751VU 98QL1−A B2 EN3155−017F1212 2826−1529 Y 1M QG12 5000 200 751VU 1445VC 5 EN3155−008M1212 (a) A

20 751VU 98QL1−A 13 EN3155−017F1620 2826−1531 1M DK24 5000 200 751VU 1421VG / EN3155−015F2018 (a) A

21 751VU 98QL1−A 12 EN3155−017F1620 2826−1545 1M DK24 5000 200 751VU 1513VT 7M EN3155−016M2222 (a) A

22 751VU 98QL1−A X1 EN3155−017F1620 2826−1548 1M DK24 5000 200 751VU 1525VC 23 EN3155−008M2222 (a) A

23 751VU 98QL1−A X2 EN3155−017F1620 2826−1549 1M DK24 5000 200 751VU 1513VT 7D EN3155−016M2222 (a) A

24

25

 (a) = BUNDLE F9000095226895 GND = GROUND

 A = ADDED WIRE

 D = DELETED WIRE

Figure A-FHCAB - Sheet 01

Hook-up Chart

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 118

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001, 004

Figure A-FWDAA - Sheet 01

Modification of the Wiring in the RH Relay Box 752VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 119

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001, 004

Figure A-FWDAA - Sheet 02

Modification of the Wiring in the RH Relay Box 752VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 120

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 002, 005

Figure A-FWDAB - Sheet 01

Modification of the Wiring in the RH Relay Box 752VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 121

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 002, 005

Figure A-FWDAB - Sheet 02

Modification of the Wiring in the RH Relay Box 752VU

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 122

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001, 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 752VU 79QL2−A C2 2826−1559 B 2M QG12 752VU 1512VC 3 M1O

 2 752VU 98QL2−A C1 EN3155−017F1212 2826−1559 B 2M QG12 752VU 1512VC 3 M1N

 3 752VU 79QL2−A A2 2826−1559 R 2M QG12 752VU 1512VC 1 M1O

 4 752VU 98QL2−A A1 EN3155−017F1212 2826−1559 R 2M QG12 752VU 1512VC 1 M1N

 5 752VU 79QL2−A B2 2826−1559 Y 2M QG12 752VU 1512VC 2 M1O

 6 752VU 98QL2−A B1 EN3155−017F1212 2826−1559 Y 2M QG12 752VU 1512VC 2 M1N

 7 752VU 79QL2−A C1 2826−1560 B 2M QG12 752VU 1502VT 4K M1O

 8 752VU 98QL2−A C2 EN3155−017F1212 2826−1560 B 2M QG12 752VU 1502VT 4K M1N

 9 752VU 79QL2−A A1 2826−1560 R 2M QG12 752VU 1502VT 2D M1O

10 752VU 98QL2−A A2 EN3155−017F1212 2826−1560 R 2M QG12 752VU 1502VT 2D M1N

11 752VU 79QL2−A B1 2826−1560 Y 2M QG12 752VU 1502VT 3D M1O

12 752VU 98QL2−A B2 EN3155−017F1212 2826−1560 Y 2M QG12 752VU 1502VT 3D M1N

13 752VU 79QL2−A X1 2826−1579 2M DK24 752VU 1530VC 20 M1O

14 752VU 98QL2−A X1 EN3155−017F1620 2826−1579 2M DK24 752VU 1530VC 20 M1N

15 752VU 79QL2−A X2 2826−1580 2M DK24 752VU 1500VT 30L M1O

16 752VU 98QL2−A X2 EN3155−017F1620 2826−1580 2M DK24 752VU 1500VT 30L M1N

17

18

19

20

21

22

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

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 123

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 002, 005

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 752VU 79QL2−A C2 2826−1559 B 2M QG12 752VU 1512VC 3 M1O

 2 752VU 98QL2−A C1 EN3155−017F1212 2826−1559 B 2M QG12 752VU 1512VC 3 M1N

 3 752VU 79QL2−A A2 2826−1559 R 2M QG12 752VU 1512VC 1 M1O

 4 752VU 98QL2−A A1 EN3155−017F1212 2826−1559 R 2M QG12 752VU 1512VC 1 M1N

 5 752VU 79QL2−A B2 2826−1559 Y 2M QG12 752VU 1512VC 2 M1O

 6 752VU 98QL2−A B1 EN3155−017F1212 2826−1559 Y 2M QG12 752VU 1512VC 2 M1N

 7 752VU 79QL2−A C1 2826−1560 B 2M QG12 752VU 1512VC 6 M1O

 8 752VU 98QL2−A C2 EN3155−017F1212 2826−1560 B 2M QG12 752VU 1512VC 6 M1N

 9 752VU 79QL2−A A1 2826−1560 R 2M QG12 752VU 1512VC 4 M1O

10 752VU 98QL2−A A2 EN3155−017F1212 2826−1560 R 2M QG12 752VU 1512VC 4 M1N

11 752VU 79QL2−A B1 2826−1560 Y 2M QG12 752VU 1512VC 5 M1O

12 752VU 98QL2−A B2 EN3155−017F1212 2826−1560 Y 2M QG12 752VU 1512VC 5 M1N

13 752VU 79QL2−A 12 2826−1562 2M DK24 752VU 1408VG GND M1O

14 752VU 98QL2−A 13 EN3155−017F1620 2826−1562 2M DK24 752VU 1408VG GND M1N

15 752VU 79QL2−A 13 2826−1576 2M DK24 752VU 1500VT 30M M1O

16 752VU 98QL2−A 12 EN3155−017F1620 2826−1576 2M DK24 752VU 1500VT 30M M1N

17 752VU 79QL2−A X1 2826−1579 2M DK24 752VU 1530VC 20 M1O

18 752VU 98QL2−A X1 EN3155−017F1620 2826−1579 2M DK24 752VU 1530VC 20 M1N

19 752VU 79QL2−A X2 2826−1580 2M DK24 752VU 1500VT 30L M1O

20 752VU 98QL2−A X2 EN3155−017F1620 2826−1580 2M DK24 752VU 1500VT 30L M1N

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

 GND = GROUND

Figure A-FHDAB - Sheet 01

Hook-up Chart

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 124

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001 thru 002

F_SB_285051_7_BAAA_01_01

FR20

FR15A

FR14

FR1

GFI AUTO−TEST

BUTTON

GFI METAL SHAFT IN

CLOSED POSITION

GFI METAL SHAFT IN

OPEN POSITION

RH RELAY BOX

LH RELAY BOX

C

B

D

751VU

752VU

A

A

B

97QL1

97QL2

C

C

98QL2

C

98QL1

C

Figure A-UBAAA - Sheet 01

Test of Ground Fault Interrupter

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 125

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 001 thru 002

D

E

F_SB_285051_7_BAAA_02_02

OFF

FWD

OFF

ON

FAULT

MAN

XFR

1

ISOL

AUTO

OPEN

A

U

T

O

A

U

T

O

A

U

T

O

T TK

L

CTR TK

XFR

OUTR TK

FAULT

FAULT

FAULT

STBY

INR TK

ON

OPEN

X FEED2

ON

OPEN

X FEED1

FEED

MAN

FAULT

OFF

FAULT

TO INR XFR R

ON

OPEN

X FEED3

ON

OPEN

X FEED4

OFF

FAULT

OFF

FAULT

L AFT XFR R

OFF

FAULT

OFF

FAULT

OFF

FAULT

MAN 2 STBY

AFT XFR1

OFF

FAULT

AFT XFR2

OFF

FAULT

OFF

MAN 3

FAULT

STBY

INR TK

OFF

FAULT

OFF

FAULT

OFF

FAULT

MAN 4 STBY

OFF

FAULT

AFT XFR4

OFF

FAULT

AFT XFR3

FWD

L

FAULT

FWD

R

FAULT

1

2 3 4

F

U

E

L

F

U

E FWD L

XFR

FAULT

RCT

OFF

FAULT

OFF

FAULT A

U

T

O

A B

245VU

E

3QL1 15QL 3QL2

77QL1 89QL 77QL2

Figure A-UBAAA - Sheet 02

Test of Ground Fault Interrupter

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 126

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 003

FR20

FR15A

FR14

FR1

GFI AUTO−TEST

BUTTON

GFI METAL SHAFT IN

CLOSED POSITION

GFI METAL SHAFT IN

OPEN POSITION

RH RELAY BOX

LH RELAY BOX

C

B

D

751VU

752VU

A

A

C

B

F_SB_285051_7_BAAB_01_01

97QL1

C

97QL2

Figure A-UBAAB - Sheet 01

Test of Ground Fault Interrupter

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 127

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 003

E

D

245VU

E

OFF

FWD

OFF

ON

FAULT

MAN

XFR

1

ISOL

AUTO

OPEN

A

U

T

O

A

U

T

O

A

U

T

O

T TK

L

CTR TK

XFR

OUTR TK

FAULT

FAULT

FAULT

STBY

INR TK

ON

OPEN

X FEED2

ON

OPEN

X FEED1

FEED

MAN

FAULT

OFF

FAULT

TO INR XFR R

ON

OPEN

X FEED3

ON

OPEN

X FEED4

OFF

FAULT

OFF

FAULT

L AFT XFR R

OFF

FAULT

OFF

FAULT

OFF

FAULT

MAN 2 STBY

AFT XFR1

OFF

FAULT

AFT XFR2

OFF

FAULT

OFF

MAN 3

FAULT

STBY

INR TK

OFF

FAULT

OFF

FAULT

OFF

FAULT

MAN 4 STBY

OFF

FAULT

AFT XFR4

OFF

FAULT

AFT XFR3

FWD

L

FAULT

FWD

R

FAULT

1

2 3 4

F

U

E

L

F

U

E

L

3QL1 15QL 3QL2

F_SB_285051_7_BAAB_02_01

Figure A-UBAAB - Sheet 02

Test of Ground Fault Interrupter

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 128

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 004 thru 005

F_SB_285051_7_BAAC_01_01

FR20

FR15A

FR14

FR1

GFI AUTO−TEST

BUTTON

GFI METAL SHAFT IN

CLOSED POSITION

GFI METAL SHAFT IN

OPEN POSITION

RH RELAY BOX

LH RELAY BOX

C

B

D

751VU

752VU

A

A

B

97QL1

C

98QL2

C

Figure A-UBAAC - Sheet 01

Test of Ground Fault Interrupter

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 129

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 004 thru 005

OFF

FWD

OFF

ON

FAULT

MAN

XFR

1

ISOL

AUTO

OPEN

A

U

T

O

A

U

T

O

A

U

T

O

T TK

L

CTR TK

XFR

OUTR TK

FAULT

FAULT

FAULT

STBY

INR TK

ON

OPEN

X FEED2

ON

OPEN

X FEED1

FEED

MAN

FAULT

OFF

FAULT

TO INR XFR R

ON

OPEN

X FEED3

ON

OPEN

X FEED4

OFF

FAULT

OFF

FAULT

L AFT XFR R

OFF

FAULT

OFF

FAULT

OFF

FAULT

MAN 2 STBY

AFT XFR1

OFF

FAULT

AFT XFR2

OFF

FAULT

OFF

MAN 3

FAULT

STBY

INR TK

OFF

FAULT

OFF

FAULT

OFF

FAULT

MAN 4 STBY

OFF

FAULT

AFT XFR4

OFF

FAULT

AFT XFR3

FWD

L

FAULT

FWD

R

FAULT

1

2 3 4

F

U

E

L

F

U

E FWD L

XFR

FAULT

RCT

OFF

FAULT

OFF

FAULT A

U

T

O

A B

245VU

E

D

E

F_SB_285051_7_BAAC_02_02

3QL1 15QL 3QL2

77QL1 89QL 77QL2

Figure A-UBAAC - Sheet 02

Test of Ground Fault Interrupter

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 130

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 006

FR20

FR15A

FR14

FR1

GFI AUTO−TEST

BUTTON

GFI METAL SHAFT IN

CLOSED POSITION

GFI METAL SHAFT IN

OPEN POSITION

LH RELAY BOX

751VU

A

B

B

C

A

F_SB_285051_7_BAAD_01_01

97QL1

Figure A-UBAAD - Sheet 01

Test of Ground Fault Interrupter

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 131

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

**CONF 006

OFF

FWD

OFF

ON

FAULT

MAN

XFR

1

ISOL

AUTO

OPEN

A

U

T

O

A

U

T

O

A

U

T

O

T TK

L

CTR TK

XFR

OUTR TK

FAULT

FAULT

FAULT

STBY

INR TK

ON

OPEN

X FEED2

ON

OPEN

X FEED1

FEED

MAN

FAULT

OFF

FAULT

TO INR XFR R

ON

OPEN

X FEED3

ON

OPEN

X FEED4

OFF

FAULT

OFF

FAULT

L AFT XFR R

OFF

FAULT

OFF

FAULT

OFF

FAULT

MAN 2 STBY

AFT XFR1

OFF

FAULT

AFT XFR2

OFF

FAULT

OFF

MAN 3

FAULT

STBY

INR TK

OFF

FAULT

OFF

FAULT

OFF

FAULT

MAN 4 STBY

OFF

FAULT

AFT XFR4

OFF

FAULT

AFT XFR3

FWD

L

FAULT

FWD

R

FAULT

1

2 3 4

F

U

E

L

F

U

E

L

245VU

3QL1 15QL 3QL2

C

D

D

F_SB_285051_7_BAAD_02_01

Figure A-UBAAD - Sheet 02

Test of Ground Fault Interrupter

DATE: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 132

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

SERVICE BULLETIN

REPORTING SHEET

TITLE: FUEL-MAIN TRANSFER SYST-INTRO GROUND FAULT INTERRUPTERS

TO CENTER AND REAR CENTER TANK FUEL PUMP CONTROL

CIRCUIT

MODIFICATION No.: 200242H16513 200242H16135

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: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 1

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340-500/600

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: Sep 01/11 SERVICE BULLETIN No.: A340-28-5051

REVISION No.: 00 - Sep 01/11 Page: 1

7

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