@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 28

TITLE: FUEL-MAIN TRANSFER SYST-INTRO GROUND FAULT INTERRUPTERS

TO CENTER TANK FUEL PUMP CONTROL CIRCUIT

MODIFICATION No.: 200242H16135

This page transmits Revision No.01 of Service Bulletin No.A340-28-4129

ADDITIONAL WORK

**CONF ALL

No additional work is required by this revision for aircraft modified by any previous issue.

REASON

Revision No. 01 issued to include a preparation test procedure for the Ground Fault Interrupter FIN

97QL2.

CHANGES

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED R

REASON

History HISTORY UPDATED R

Objective/Action OBJECTIVE/ACTION UPDATED R

Operational/Maintenance

Consequences

OPERATIONAL/MAINTENANCE CONSEQUENCES

UPDATED

R

APPROVAL APPROVAL UPDATED R

WEIGHT AND BALANCE Minor editorial or document structure change R

BALANCE UPDATED R

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 1

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

PUBLICATION AFFECTED PUBLICATIONS AFFECTED UPDATED R

MATERIAL INFORMATION

TOOLING TOOLING UPDATED R

Tooling - Price and Availability TOOLING - PRICE AND AVAILABILITY

PARAGRAPH ADDED

N

Tools TOOLS PARAGRAPH ADDED N

Special Tools SPECIAL TOOLS PARAGRAPH ADDED N

ACCOMPLISHMENT INSTRUCTIONS

TASK 284129- 831-895-001-

MODIFICATION

TASK SOLUTION UPDATED

WARNING UPDATED

CAUTION UPDATED

R

Task associated data - 001 PANEL UPDATED R

Task associated data - 002 ZONE UPDATED

PANEL UPDATED

R

Subtask 284129-831-002-001 SUBTASK SOLUTION UPDATED R

Subtask 284129-800-401-001 SUBTASK SOLUTION UPDATED

PANEL UPDATED

ZONE UPDATED

FIGURE REFERENCE UPDATED

CONFIGURATION UPDATED

PART NUMBER UPDATED

FIN UPDATED

LOCATION UPDATED

REFERENCES UPDATED

R

Subtask 284129-710-401-001 SUBTASK SOLUTION UPDATED

FIGURE REFERENCE UPDATED

CONFIGURATION UPDATED

REFERENCES UPDATED

R

Subtask 284129-710-402-001 SUBTASK SOLUTION UPDATED

PANEL UPDATED

ZONE UPDATED

FIGURE REFERENCE UPDATED

CONFIGURATION UPDATED

REFERENCES UPDATED

R

Subtask 284129-800-402-003 SUBTASK SOLUTION ADDED N

Subtask 284129-710-401-002 SUBTASK SOLUTION ADDED N

Subtask 284129-800-401-001 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 284129-710-401-001 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 284129-942-401-002 SUBTASK SOLUTION UPDATED

LOCATION UPDATED

PANEL UPDATED

ZONE UPDATED

R

Subtask 284129-942-401-001 SUBTASK SOLUTION UPDATED

LOCATION UPDATED

PANEL UPDATED

ZONE UPDATED

MANPOWER RESSOURCE UPDATED

R

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 2

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Fig. A-FCAAA

Fig. A-FCAAA Sheet 01 SHEET UPDATED R

Fig. A-FCAAA Sheet 02 SHEET UPDATED R

Fig. A-FCBAA

Fig. A-FCBAA Sheet 01 SHEET UPDATED R

Fig. A-FCBAA Sheet 02 SHEET UPDATED R

Fig. A-UBAAA FIGURE SOLUTION ADDED N

Fig. A-UBAAA Sheet 01 SHEET ADDED N

Fig. A-UBAAA Sheet 02 SHEET ADDED N

Fig. A-UBAAB FIGURE SOLUTION ADDED N

Fig. A-UBAAB Sheet 01 SHEET ADDED N

Fig. A-UBAAB Sheet 02 SHEET ADDED N

Fig. A-UAA FIGURE DELETED FOR APPLICABLE MSN D

FILLING INSTRUCTIONS

This Service Bulletin has been generated electronically and is reissued as a complete document.

Replace the complete document.

Put this Revision Transmittal Sheet in front of the Service Bulletin.

HISTORY OF PREVIOUS REVISIONS

No previous revision

REVISION SEQUENCE

ORIGINAL: Jul 19/11

REVISION No. : 01 - Mar 27/12

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 4

7

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SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 28

TITLE: FUEL-MAIN TRANSFER SYST-INTRO GROUND FAULT INTERRUPTERS

TO CENTER TANK FUEL PUMP CONTROL CIRCUIT

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 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 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 A340-28-4903 (Mod. No. 200241H16397) was issued for operators

DLH, IBE, TAP and UAE. The Service Bulletin A340-28-4903 introduced a GFI and related base into

the electrical supply circuit of the A340-200/300 aircraft right center tank transfer pump.

This Service Bulletin introduces GFI, and related bases, into the electrical supply circuits of the

A340-200/300 aircraft left and right center tank 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.

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.

The embodiment of this SB affects the ALS part 5, section 5-4. This limitation is applicable to all aircraft

operated under FAA registration.

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 1

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SERVICE BULLETIN

SUMMARY

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO 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 284129A01R00 1 1,740.00 Placard Set, Relay, Base, Nuts

Kit 284129A02R00 1 1,740.00 Placard Set, Relay, Base, Nuts

TOTAL 3,480.00

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 284129A01R00 1 1,740.00 Placard Set, Relay, Base, Nuts

EFFECTIVITY

**CONF ALL

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

47W 56W AAW AFR ALK ARG CAL CCA CES CPA DGA DLH FIN

GAF GFA HFY IBE KAC KNE LAN M3R MAU MSR NMB OAL PAL

QAF RJA S3R SAA SAS SFB SLM SVW SWR TAP THT THY UAE

VCV VIR XAX

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 2

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@A340

SERVICE BULLETIN

SUMMARY

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 284129-831-895-001: MODIFICATION

TOTAL MANHOURS 10.00

ELAPSED TIME (HOURS) 10.00

**CONF 002

Task 284129-831-895-001: MODIFICATION

TOTAL MANHOURS 7.00

ELAPSED TIME (HOURS) 7.00

APPENDICES

**CONF ALL

None

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 3

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@A340

SERVICE BULLETIN

SUMMARY

**CONF 001

FR14

FR15A

751VU

752VU

F_SB_284129_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 4

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@A340

SERVICE BULLETIN

SUMMARY

**CONF 002

FR14

FR15A

751VU

F_SB_284129_5_SAAB_01_00

Figure A-FSAAB - Sheet 01

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 5

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 6

7

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@A340

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 TANK FUEL PUMP CONTROL CIRCUIT

MODIFICATION No.: 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

340-211 340-212 340-213 340-311 340-312 340-313

(2) Effectivity by MSN

0002-0006 0009 0011 0013-0015 0018-0029 0031-0035 0038 0041 0043-0044

0046-0049 0051-0053 0056-0058 0061 0063 0074-0076 0078-0081 0084-0085

0088-0091 0093-0094 0101 0104 0114-0115 0117 0123 0125-0126 0128-0129 0131

0133-0137 0139 0141-0142 0145-0147 0149-0152 0154 0156-0161 0163-0164

0166-0170 0173-0176 0178-0180 0182 0185-0187 0190 0192-0194 0196-0197 0199

0201-0202 0204 0207-0208 0210 0212-0218 0220-0221 0225 0227-0228 0233

0235-0237 0239 0242-0243 0245-0246 0252 0257 0260 0263-0264 0268 0270

0273-0274 0278 0280 0282 0292 0297 0302 0304 0307 0310 0318-0319 0321 0325

0327 0329 0331-0332 0335 0347 0352 0354-0355 0359 0363 0367 0373-0374

0377-0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413-0415 0424

0429-0430 0433-0435 0438 0442 0446-0447 0450 0459 0467 0470 0474 0483 0528

0538 0541 0544-0546 0554 0556 0559 0561-0562 0582 0585 0590 0598 0643 0646

0651 0668 0793 0800 0835 0844 0921 0938 0955

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

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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

47W 0009

56W 0002 0003 0013 0015

AAW 0151

AFR 0029 0078 0084 0186 0207 0210 0237 0245 0246 0260 0307 0310

0319 0377 0399

ALK 0032 0033 0034 0367 0374 0381

ARG 0048 0063 0074 0080 0085 0093 0094 0123 0126 0128 0373

CAL 0402 0406 0411 0415 0433 0541

CCA 0192 0199 0201 0242 0243 0264

CES 0129 0131 0141 0161 0182

CPA 0136 0137 0142 0147 0157 0160 0208 0218 0220 0227 0228

DGA 0075 0081

DLH 0020 0024 0027 0028 0035 0052 0053 0056 0135 0158 0213 0233

0252 0297 0304 0321 0325 0327 0335 0347 0352 0354 0379 0390

0434 0447

FIN 0058 0168 0174 0835 0844 0921 0938

GAF 0274 0355

GFA 0212 0215 0282 0554

HFY 0117 0133

IBE 0005 0088 0125 0134 0145 0146 0170 0193 0217 0221 0302 0318

0329 0332 0387 0414 0459 0474 0483

KAC 0089 0090 0101 0104

KNE 0004

LAN 0167 0359 0363 0429 0442

M3R 0061

MAU 0076 0152 0194 0268 0793 0800

MSR 0156 0159 0178

NMB 0047 0051

OAL 0235 0239 0280 0292

PAL 0173 0176 0187 0196

QAF 0026 0528

RJA 0014 0022 0038 0043

S3R 0204

SAA 0006 0011 0018 0019 0021 0197 0378 0544 0582 0590 0643 0646

0651

SAS 0413 0424 0430 0435 0450 0467 0470

SFB 0046

SLM 0049

SVW 0955

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

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@A340

SERVICE BULLETIN

OPERATOR MSN

SWR 0150 0154 0169 0175 0179 0263 0538 0545 0546 0556 0559 0561

0562 0585 0598

TAP 0041 0044 0079 0091

THT 0385 0395 0438 0446 0668

THY 0023 0025 0057 0115 0180 0216 0257 0270 0331

UAE 0139 0149 0163 0166 0185 0190 0202 0236

VCV 0031

VIR 0114 0164 0214 0225

XAX 0273 0278

(4) Configuration by MSN

MSN CONFIGURATION

0002 0003 0004 0006 0009 0011 0013 0014 0015 0018 0019

0021 0022 0023 0025 0026 0029 0031 0032 0033 0034 0038

0043 0046 0047 0048 0049 0051 0057 0058 0061 0063 0074

0075 0076 0078 0080 0081 0084 0085 0089 0090 0093 0094

0101 0104 0114 0115 0117 0123 0126 0128 0129 0131 0133

0136 0137 0141 0142 0147 0150 0151 0152 0154 0156 0157

0159 0160 0161 0164 0167 0168 0169 0173 0174 0175 0176

0178 0179 0180 0182 0186 0187 0192 0194 0196 0199 0201

0204 0207 0208 0210 0212 0214 0215 0216 0218 0220 0225

0227 0228 0235 0237 0239 0242 0243 0245 0246 0257 0260

0263 0264 0268 0270 0273 0274 0278 0280 0282 0292 0307

0310 0319 0331 0359 0363 0367 0373 0374 0377 0381 0385

0387 0395 0399 0402 0406 0411 0413 0415 0424 0429 0430

0433 0435 0438 0442 0446 0450 0467 0470 0528 0538 0541

0544 0545 0546 0554 0556 0559 0561 0562 0582 0585 0590

0598 0643 0646 0651 0668 0793 0800 0835 0844 0921 0938

0955

001

0005 0020 0024 0027 0028 0035 0041 0044 0052 0053 0056

0079 0088 0091 0125 0134 0135 0139 0145 0146 0149 0158

0163 0166 0170 0185 0190 0193 0197 0202 0213 0217 0221

0233 0236 0252 0297 0302 0304 0318 0321 0325 0327 0329

0332 0335 0347 0352 0354 0355 0378 0379 0390 0414 0434

0447 0459 0474 0483

001 002

(5) Configuration definition

**CONF 001

Config. 001 is valid for aircraft on which Evaluation Service Bulletin No. A340-28-4903 is

not accomplished or for aircraft on which the restoration of Evaluation Service Bulletin

No. A340-28-4903 is accomplished.

**CONF 002

Config. 002 is valid for aircraft on which Evaluation Service Bulletin No.A340-28-4903 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.

A340-28-4903.

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 3

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SERVICE BULLETIN

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Kit 284129A01R00 1

Kit 284129A02R00 1

Consumable CMLA01 1

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Kit 284129A01R00 1

Consumable CMLA01 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

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

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

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

Tank Safety.

The Evaluation Service Bulletin A340-28-4903 (Mod. No. 200241H16397) was issued for

operators DLH, IBE, TAP and UAE. The Service Bulletin A340-28-4903 introduced a GFI

and related base into the electrical supply circuit of the A340-200/300 aircraft right center

tank transfer pump.

(2) Objective/Action

This Service Bulletin introduces GFI, and related bases, into the electrical supply circuits

of the A340-200/300 aircraft left and right center tank 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.

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 4

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SERVICE BULLETIN

(4) Operational/Maintenance Consequences

The embodiment of this SB affects the ALS part 5, section 5-4. This limitation is

applicable to all aircraft operated under FAA registration.

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 284129-831-895-001: 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 284129-831-895-001: 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

The accomplishment timescale for this Service Bulletin will be 4 years.

This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued

to confirm this classification. It is anticipated that the AD will confirm the (thresholds

and/or intervals and/or date) given above but reference should be made to the AD for

confirmation of 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: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

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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 284129-831-895-001: MODIFICATION

Get Access 1.50

On Aircraft

Modify the Equipment and the Wiring in the LH Relay

Box 751VU.

3.00

Modify the Equipment and the Wiring in the RH Relay

Box 752VU.

3.00

Tests 1.00

Close-Up 1.50

TOTAL MANHOURS 10.00

ELAPSED TIME (HOURS) 10.00

**CONF 002

Task 284129-831-895-001: MODIFICATION

Get Access 1.50

On Aircraft

Modify the Equipment and the Wiring in the LH Relay

Box 751VU.

3.00

Tests 1.00

Close-Up 1.50

TOTAL MANHOURS 7.00

ELAPSED TIME (HOURS) 7.00

**CONF ALL

H. WEIGHT AND BALANCE

**CONF 001

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

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

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

Manufacturers Empty Weight +0.122 KG (+0.2689 LB)

Effect on Balance +1.170 KGM (+8.462 LB.FT )

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 6

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@A340

SERVICE BULLETIN

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

Manufacturers Empty Weight +0.061 KG (+0.1344 LB)

Effect on Balance +0.585 KGM (+4.231 LB.FT )

**CONF ALL

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

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

12-21-13 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

20-52-21 20-55-00

Service Bulletin (SB) A340-28-4903

Standards Manual (SM)

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

**CONF 002

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

12-21-13 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

20-52-21 20-55-00

Service Bulletin (SB) A340-28-4903

Standards Manual (SM)

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

**CONF ALL

K. PUBLICATION AFFECTED

Airworthiness Limitation Section (ALS)

Aircraft Schematic Manual (ASM) 28-20-01 28-26-02 28-26-03

28-26-06

Aircraft Wiring List (AWL)

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

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 7

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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 ALL

M. SPARES

None

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

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

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

Kit 284129A01R00

Kit 284129A02R00

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 by Email: airbus.kit@airbus.com

(2) Price and Availability

Kit 284129A01R00

Cost 1,740.00 USD

Availability 60 calendar days from receipt of order

Kit 284129A02R00

Cost 1,740.00 USD

Availability 60 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 commercial rate applicable to sales prices given

in the paragraph ’Price and Availability’ for orders placed before 31 December 2017.

C. LIST OF COMPONENTS

Kit 284129A01R00

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

NOTES

1 ABS1629-28A0 1 GFI (1) E0667A28A0

2 E0673C0S 1 Base (2) E0673A0S

3 MS21042-04 3 Nut

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 9

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

NOTES

EN3155-017F1216 6 Contact

EN3155-017F1620 4 Contact

F9100095214395 1 Set

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 284129A02R00

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

NOTES

1 ABS1629-28A0 1 GFI (1) E0667A28A0

2 E0673C0S 1 Base (2) E0673A0S

3 MS21042-04 3 Nut

EN3155-017F1216 6 Contact

EN3155-017F1620 4 Contact

F9100095214495 1 Set

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(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

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

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F. TOOLING

(1) Tooling - Price and Availability

None

(2) Tools

None

(3) Special Tools

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 11

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This Page Intentionally Left Blank

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 284129-831-895-001 - MODIFICATION

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

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING: THIS PROCEDURE USES A FUEL SYSTEM ITEM THAT IS IN A CATEGORY

KNOWN AS A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION

(CDCCL). CDCCL IDENTIFIES AN ITEM THAT CAN BE THE SOURCE OF A

POSSIBLE FUEL TANK IGNITION. YOU MUST KEEP ALL CDCCL ITEMS IN

THE APPROVED CONFIGURATION. DAMAGE, WEAR OR CHANGES TO A

CDCCL ITEM CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.

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 97QL1 97QL1A 97QL2 97QL2A

Access

Door 132AZ 821

Electrical panel 751VU 752VU

Manpower

TOTAL MANHOURS 10.00

ELAPSED TIME (HOURS) 10.00

**CONF 002

Zone

121 191 192 211 212

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 13

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SERVICE BULLETIN

Modified FIN

5QL1 5QL1A 97QL1 97QL1A

Access

Door 132AZ 821

Electrical panel 751VU

Manpower

TOTAL MANHOURS 7.00

ELAPSED TIME (HOURS) 7.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 284129-910-001-001 - 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

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

20-52-21

Standards Manual (SM)

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

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

Service Bulletin, (Refer to the Consumable Material List (CML)).

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

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

20-21-15-912-801).

(e) Obey the instructions for the general wiring installation (Refer to ESPM 20-30-00).

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

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SERVICE BULLETIN

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

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

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

Dry Cleaning

Solvent

(varsol/white Spirit)

11-002 As required

(2) Subtask 284129-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 284129-910-001-001 - 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

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

20-52-21

Standards Manual (SM)

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

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

Service Bulletin, (Refer to the Consumable Material List (CML)).

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

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

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SERVICE BULLETIN

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

20-21-15-912-801).

(e) Obey the instructions for the general wiring installation (Refer to ESPM 20-30-00).

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

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

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

Dry Cleaning

Solvent

(varsol/white Spirit)

11-002 As required

(2) Subtask 284129-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

(a) 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 284129-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

(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.

(2) Subtask 284129-010-001-001 - Remove/Open for Access

Manpower Resources

Skills NON SPECIFIC

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 16

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References

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

06-41-53, Page Block 001

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) 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).

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

52-52-00, Page Block 001).

(3) Subtask 284129-865-001-001 - 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)

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 002

(1) Subtask 284129-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

(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.

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

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(2) Subtask 284129-010-001-001 - Remove/Open 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 52-30-00-010-801

Task 52-30-00-010-802

Task 52-30-00-010-804

52-52-00, Page Block 001

(a) 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).

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

52-52-00, Page Block 001).

(3) Subtask 284129-865-001-002 - 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)

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 284129-831-001-001 - 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

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

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Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 284129A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS1629-28A0 1 GFI

2 E0673C0S 1 Base

3 MS21042-04 3 Nut

EN3155-017F1216 6 Contact

EN3155-017F1620 4 Contact

F9100095214395 1 Set

References

Fig. A-FCAAA

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

Sheet 03

Fig. A-FBBAA

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Open the LH relay box 751VU.

(b) Remove (Refer to Fig. A-FBBAA 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

(c) Modify the wiring in the LH Relay Box 751VU :

1 Modify the connections of the wires as shown in the wiring diagrams Fig. AFCAAA Sheet 01 and Fig. A-FCAAA Sheet 02 and as given in the hook-up

chart lines :

- 1 thru 20 (Refer to Fig. A-FCAAA Sheet 03).

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NOTE: If necessary, use :

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

2 Install the relay GFI 97QL1.

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

FIN 97QL1A

1 Base E0673C0S Item 2

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 1

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. AFBBAA Sheet 02, supplied in :

1 Placard Set F9100095214395

(d) Close the LH Relay Box 751VU.

(2) Subtask 284129-831-002-001 - 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

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Material necessary to do the job

Kit 284129A02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS1629-28A0 1 GFI

2 E0673C0S 1 Base

3 MS21042-04 3 Nut

EN3155-017F1216 6 Contact

EN3155-017F1620 4 Contact

F9100095214495 1 Set

References

Fig. A-FCBAA

Modification of the Wiring in the RH

Relay Box 752VU

Sheet 01

Sheet 02

Sheet 03

Fig. A-FBCAA

Modification of the Equipment in the RH

Relay Box 752VU

Sheet 01

Sheet 02

(a) Open the RH relay box 752VU.

(b) Remove (Refer to Fig. A-FBCAA 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

(c) Modify the wiring in the RH Relay Box 752VU :

1 Modify the connections of the wires as shown in the wiring diagrams Fig. AFCBAA Sheet 01 and Fig. A-FCBAA Sheet 02 and as given in the hook-up

chart lines :

- 1 thru 20 (Refer to Fig. A-FCBAA Sheet 03).

NOTE: If necessary, use :

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

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2 Install the relay GFI 97QL2.

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

FIN 97QL2A

1 Base E0673C0S Item 2

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 1

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. AFBCAA Sheet 02, supplied in :

1 Placard Set F9100095214495

(d) Close the RH Relay Box 752VU.

**CONF 002

(1) Subtask 284129-831-001-001 - 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 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 284129A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS1629-28A0 1 GFI

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 E0673C0S 1 Base

3 MS21042-04 3 Nut

EN3155-017F1216 6 Contact

EN3155-017F1620 4 Contact

F9100095214395 1 Set

References

Fig. A-FCAAA

Modification of the Wiring in the LH

Relay Box 751VU

Sheet 01

Sheet 02

Sheet 03

Fig. A-FBBAA

Modification of the Equipment in the LH

Relay Box 751VU

Sheet 01

Sheet 02

(a) Open the LH relay box 751VU.

(b) Remove (Refer to Fig. A-FBBAA 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

(c) Modify the wiring in the LH Relay Box 751VU :

1 Modify the connections of the wires as shown in the wiring diagrams Fig. AFCAAA Sheet 01 and Fig. A-FCAAA Sheet 02 and as given in the hook-up

chart lines :

- 1 thru 20 (Refer to Fig. A-FCAAA Sheet 03).

NOTE: If necessary, use :

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

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2 Install the relay GFI 97QL1.

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

FIN 97QL1A

1 Base E0673C0S Item 2

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 1

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. AFBBAA Sheet 02, supplied in :

1 Placard Set F9100095214395

(d) Close the LH Relay Box 751VU.

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 284129-865-002-001 - C/B Closing

Manpower Resources

Skills NON SPECIFIC

(a) Remove the safety clips and/or tags 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

722VU FUEL XFR R PUMP 1QL2 48 G (1)

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.

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SERVICE BULLETIN

(2) Subtask 284129-800-401-001 - 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 Interrupter (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 Ground Fault Interrupter (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.

(3) Subtask 284129-710-401-001 - 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

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 25

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@A340

SERVICE BULLETIN

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 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.

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 26

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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-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 284129-710-402-001 - 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 28-25-00-869-001

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 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).

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 27

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SERVICE BULLETIN

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 28-25-00-869-001).

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 28-25-00-869-001):

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.

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 28-25-00-869-001).

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 15QL (CTR TK TO INR XFR) to

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

**CONF 002

(1) Subtask 284129-865-002-002 - C/B Closing

Manpower Resources

Skills NON SPECIFIC

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 28

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SERVICE BULLETIN

(a) Remove the safety clips and/or tags 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

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

(2) Subtask 284129-800-402-003 - Preparation for Test Procedure

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

Fig. A-UBAAB

Test of Ground Fault Interrupter

Sheet 01

Sheet 02

(a) Examine the ABS1629-28A0 Ground Fault Interrupter (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 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.

(3) Subtask 284129-710-401-002 - 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

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 29

7

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@A340

SERVICE BULLETIN

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 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-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).

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 30

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SERVICE BULLETIN

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-UBAAB Sheet 02).

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 284129-410-001-001 - 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.

(2) Subtask 284129-942-401-002 - Close-up

Manpower Resources

Skills NON SPECIFIC

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 31

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@A340

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 12-21-13-860-051

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment (Refer to AMM Task 12-21-13-860-051).

(b) Remove the access platform(s).

(c) Restore the system and the aircraft to the normal operating condition.

**CONF 002

(1) Subtask 284129-410-001-001 - 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.

(2) Subtask 284129-942-401-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-21-13-860-051

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment (Refer to AMM Task 12-21-13-860-051).

(b) Remove the access platform(s).

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 32

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SERVICE BULLETIN

(c) Restore the system and the aircraft to the normal operating condition.

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 33

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SERVICE BULLETIN

**CONF ALL

BEFORE

B D

H

A

B

C

C

FR20

FR15A

FR14

FR1

(3 POS) (3)

(2)

(1)

751VU

A

5QL1

66

5QL1

F_SB_284129_5_BBAA_01_02

Figure A-FBBAA - Sheet 01

Modification of the Equipment in the LH Relay Box 751VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 34

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SERVICE BULLETIN

**CONF ALL

AFTER

H

(3 POS)

D

E

E

3

2

1

97QL1 ELECTRICAL BONDING

66

97QL1

F_SB_284129_5_BBAA_02_02

Figure A-FBBAA - Sheet 02

Modification of the Equipment in the LH Relay Box 751VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 35

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@A340

SERVICE BULLETIN

**CONF 001

BEFORE

A

H

A

B

5QL2

C

FR20

FR15A

FR14

FR1

(3 POS) (3)

(2)

(1)

752VU

5QL2

B

D

3

C

F_SB_284129_5_BCAA_01_01

Figure A-FBCAA - Sheet 01

Modification of the Equipment in the RH Relay Box 752VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 36

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@A340

SERVICE BULLETIN

**CONF 001

AFTER

(3 POS)

D

E

97QL2

3

2

1

ELECTRICAL BONDING

E

97QL2

B

87

F_SB_284129_5_BCAA_02_01

Figure A-FBCAA - Sheet 02

Modification of the Equipment in the RH Relay Box 752VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 37

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@A340

SERVICE BULLETIN

**CONF ALL

Figure A-FCAAA - Sheet 01

Modification of the Wiring in the LH Relay Box 751VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 38

7

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@A340

SERVICE BULLETIN

**CONF ALL

Figure A-FCAAA - Sheet 02

Modification of the Wiring in the LH Relay Box 751VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 39

7

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@A340

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 X2 2826−0058 1M DK24 751VU 1407VG GND M1O

14 751VU 97QL1−A X2 EN3155−017F1620 2826−0058 1M DK24 751VU 1407VG GND M1N

15 751VU 5QL1−A 12 2826−0059 1M DK24 751VU 1407VG GND M1O

16 751VU 97QL1−A 13 EN3155−017F1620 2826−0059 1M DK24 751VU 1407VG GND M1N

17 751VU 5QL1−A X1 2826−0063 1M DK24 751VU 4QL1−A 1 M1O

18 751VU 97QL1−A X1 EN3155−017F1620 2826−0063 1M DK24 751VU 4QL1−A 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-FCAAA - Sheet 03

Modification of the Wiring in the LH Relay Box 751VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 40

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SERVICE BULLETIN

**CONF 001

Figure A-FCBAA - Sheet 01

Modification of the Wiring in the RH Relay Box 752VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 41

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@A340

SERVICE BULLETIN

**CONF 001

Figure A-FCBAA - Sheet 02

Modification of the Wiring in the RH Relay Box 752VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 42

7

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@A340

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 752VU 5QL2−A A1 2826−0092 R 2M QG16 752VU 1536VC 40 M1O

 2 752VU 97QL2−A A2 EN3155−017F1216 2826−0092 R 2M QG16 752VU 1536VC 40 M1N

 3 752VU 5QL2−A B1 2826−0092 Y 2M QG16 752VU 1536VC 41 M1O

 4 752VU 97QL2−A B2 EN3155−017F1216 2826−0092 Y 2M QG16 752VU 1536VC 41 M1N

 5 752VU 5QL2−A C1 2826−0092 B 2M QG16 752VU 1536VC 42 M1O

 6 752VU 97QL2−A C2 EN3155−017F1216 2826−0092 B 2M QG16 752VU 1536VC 42 M1N

 7 752VU 5QL2−A X1 2826−0097 2M DK24 752VU 4QL2−A 1 M1O

 8 752VU 97QL2−A X1 EN3155−017F1620 2826−0097 2M DK24 752VU 4QL2−A 1 M1N

 9 752VU 5QL2−A X2 2826−0098 2M DK24 752VU 1402VG GND M1O

10 752VU 97QL2−A X2 EN3155−017F1620 2826−0098 2M DK24 752VU 1402VG GND M1N

11 752VU 5QL2−A 12 2826−0099 2M DK24 752VU 1402VG GND M1O

12 752VU 97QL2−A 13 EN3155−017F1620 2826−0099 2M DK24 752VU 1402VG GND 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-FCBAA - Sheet 03

Modification of the Wiring in the RH Relay Box 752VU

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 43

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 001

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

C

B

751VU

752VU

A

A

C

B

/

TRIP/RESET BUTTON

97QL1 97QL2

D

F_SB_284129_7_BAAA_01_01

(NOT TRIPPED) (TRIPPED)

Figure A-UBAAA - Sheet 01

Test of Ground Fault Interrupter

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 44

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 001

245VU

OFF OFF

FWD

OFF

ON

FAULT

OFF OFF

STBY 1 MODE STBY 4

1 2 3 4

ISOL

AUTO

OPEN

A

U

T

O

A

U

T

O

A

U

T

O

T TANK

L CTR TANK

ON

OPEN

XFR

OUTR TK

F

U

E

L

F

U

E

L

FAULT FAULT FAULT FAULT FAULT

FAULT

OFF

FAULT

OFF

FAULT

STBY 2

L INR TANK

OFF

FAULT

OFF

FAULT

STBY 3

R INR TANK

ON

OPEN A

U

T

O

A

U

T

O

ON

OPEN

X FEED4

X FEED2 X FEED3

ON

OPEN

X FEED1

FEED

OFF

FAULT

OFF

FAULT

XFR R

ENG 2

ENG 1

ENG 3

ENG 4

E

D

E

F_SB_284129_7_BAAA_02_00

3QL1 15QL 3QL2

Figure A-UBAAA - Sheet 02

Test of Ground Fault Interrupter

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 45

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002

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

A

TRIP/RESET BUTTON

97QL1

B

C

B

F_SB_284129_7_BAAB_01_01

(NOT TRIPPED) (TRIPPED)

Figure A-UBAAB - Sheet 01

Test of Ground Fault Interrupter

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 46

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

**CONF 002

245VU

OFF OFF

FWD

OFF

ON

FAULT

OFF OFF

STBY 1 MODE STBY 4

1 2 3 4

ISOL

AUTO

OPEN

A

U

T

O

A

U

T

O

A

U

T

O

T TANK

L CTR TANK

ON

OPEN

XFR

OUTR TK

F

U

E

L

F

U

E

L

FAULT FAULT FAULT FAULT FAULT

FAULT

OFF

FAULT

OFF

FAULT

STBY 2

L INR TANK

OFF

FAULT

OFF

FAULT

STBY 3

R INR TANK

ON

OPEN A

U

T

O

A

U

T

O

ON

OPEN

X FEED4

X FEED2 X FEED3

ON

OPEN

X FEED1

FEED

OFF

FAULT

OFF

FAULT

XFR R

ENG 2

ENG 1

ENG 3

ENG 4

3QL1 15QL

D

C

D

F_SB_284129_7_BAAB_02_01

Figure A-UBAAB - Sheet 02

Test of Ground Fault Interrupter

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 47

7

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A340

SERVICE BULLETIN

REPORTING SHEET

TITLE: FUEL-MAIN TRANSFER SYST-INTRO GROUND FAULT INTERRUPTERS

TO CENTER TANK FUEL PUMP CONTROL CIRCUIT

MODIFICATION No.: 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: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 1

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@A340

SERVICE BULLETIN

QUALITY PERCEPTION FORM

Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data

that you provide us will be used to analyse areas of difficulties and to take corrective action to further

improve the quality of our Service Bulletins.

We thank you for the time you have taken in completing this form.

(Please rate on a scale of 1 to 4, with 4 being the highest score)

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials Operator Supplied X Mod/Inspection

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Jul 19/11 SERVICE BULLETIN No.: A340-28-4129

REVISION No.: 01 - Mar 27/12 Page: 1

7

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