@A340-500/600

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 92

TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALL-IMPROVE EMP

ELECTRICAL CONNECTOR AND SLEEVE.

MODIFICATION No.: 58773S30712

This page transmits Revision No.02 of Service Bulletin No.A340-92-5053

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No. 02 issued to take into account connector PN MS3456KT24-10S :

- Material paragraph modified, COMPA01 added,

- Accomplishment instructions paragraph modified.

CHANGES

SUMMARY

GENERAL EVALUATION GENERAL EVALUATION TABLE UPDATED R

MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE

UPDATED

R

REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE

UPDATED

R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Material Effectivity MATERIAL EFFECTIVITY UPDATED

MATERIAL SET QUANTITY UPDATED

MATERIAL SET UPDATED

R

COMPLIANCE

Classification CLASSIFICATION UPDATED R

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R

MANPOWER MANPOWER UPDATED R

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REVISION No.: 02 - Sep 01/10 Page: 1

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

REFERENCES REFERENCED DOCUMENTATION UPDATED R

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATED

MATERIAL SET UPDATED

R

Price and Availability PRICE AND AVAILABILITY UPDATED

MATERIAL SET UPDATED

R

LIST OF COMPONENTS

Kit 925053A01R02 PART MATERIAL SET UPDATED

MATERIAL SET LABEL UPDATED

R

LIST OF MATERIALS - OPERATOR

SUPPLIED

Minor editorial or document structure change R

Consumable Materials CONSUMABLE MATERIALS PARAGRAPH ADDED N

Components COMPONENTS PARAGRAPH ADDED N

Component COMPA01 PART MATERIAL SET ADDED N

Equipment EQUIPMENT PARAGRAPH ADDED N

ACCOMPLISHMENT INSTRUCTIONS

TASK 925053- 831-801-001-Modification

Subtask 925053-910-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 925053-831-001-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

REFERENCED DOCUMENTATION UPDATED

FIN UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 925053-831-002-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

REFERENCED DOCUMENTATION UPDATED

FIN UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 2

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 925053-831-003-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

NOTE UPDATED

REFERENCED DOCUMENTATION UPDATED

FIN UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Fig. A-FADAA

Fig. A-FADAA Sheet 01 SHEET UPDATED R

Fig. A-FAEAA FIGURE SOLUTION ADDED N

Fig. A-FAEAA Sheet 01 SHEET ADDED N

Appendix 01

APPENDIX CONTENT APPENDIX CONTENT UPDATED R

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

Revision No. 01 issued to change the commercial policy and to create a Kit.

REVISION SEQUENCE

ORIGINAL: Sep 02/09

REVISION No. : 01 - Feb 22/10

REVISION No. : 02 - Sep 01/10

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 4

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SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 92

TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALL-IMPROVE EMP

ELECTRICAL CONNECTOR AND SLEEVE.

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 58773S30712

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

Several A330/A340 aircraft family operators have reported in service occurrences of hydraulic pump

electrical motor connector internal arcing resulting in false hydraulic system overheat Electronic

Centralized Aircraft Monitoring (ECAM) warnings and/or hydraulic pump electrical motor malfunction.

Investigations have shown that under some conditions of the cables and the connectors rear grommet

manufacturing tolerances, there is a possible path for fluid ingress resulting in the connector internal

arcing and hydraulic system failure.

This modification introduces heat shrink sleeves to the rear of the gauge 12 and 10 cable contacts and

a sealing plug to the connector free cavity to increase the water tightness of the hydraulic pump

electrical motor connectors 1JCA, 1JJA and 1JVA.

The accomplishment of this Service Bulletin will prevent the possible hydraulic pump electrical motor

connectors fluid ingress from the rear of the connector grommet and will prevent the false hydraulic

system overheat ECAM warnings and/or hydraulic pump electrical motor malfunction.

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

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

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SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

COST SAVING NO LROPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 925053A01R02 1 877.00 Tubing-heat, Tie-cables, Sealing plugs,

Sockets, Sleeve reducers

Component COMPA01 1 See SB Sockets, Sleeve reducers

EFFECTIVITY

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

62X 72W 79W ARA CES CHH DLH ETD IBE QAF QTR SAA SIA

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 OIT : SE 999.0040/09 dated 25 May 2009

OTHER SBIT : SEMB/914.0742/09

OTHER SBIT : SEMB F92M10018658 dated 6 May 2010

OTHER SBIT : 10-0034 dated 23 August 2010

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 925053-831-801-001: Modification

TOTAL MANHOURS 12.50

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

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SERVICE BULLETIN

SUMMARY

Task 925053-831-801-001: Modification

ELAPSED TIME (HOURS) 4.50

APPENDICES

Appendix 01

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 3

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SERVICE BULLETIN

SUMMARY

**CONF ALL

1JCA

1JJA

1JVA

F_SB_925053_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 4

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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: 92

TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALL-IMPROVE EMP

ELECTRICAL CONNECTOR AND SLEEVE.

MODIFICATION No.: 58773S30712

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 0897 0910 0912 0917 0924

0929 0933 0953 0972 0981 0987

(3) Effectivity by Operator

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

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

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

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

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

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SERVICE BULLETIN

OPERATOR MSN

62X 0779

72W 0917

79W 0924

ARA 0910 0912

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

ETD 0748 0757 0761 0783 0829 0837 0870 0929 0933

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

QAF 0495

QTR 0715 0740 0766 0798

SAA 0410 0417 0426 0531 0534 0547 0557 0626 0630

SIA 0478 0492 0499 0560 0563

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 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 0762 0763 0764 0765

0766 0767 0768 0771 0775 0779 0783 0787 0790 0794 0798

0804 0812 0829 0837 0846 0848 0870 0897 0910 0912 0917

0924 0929 0933 0953 0972 0981 0987

001

(5) Configuration definition

**CONF 001

Config. 01 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

NOTE: On the same aircraft, it is possible to find both connectors PN

ASNE0233-24-10S and PN MS3456KT24-10S.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Kit 925053A01R02 1

Component COMPA01 1

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

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B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Several A330/A340 aircraft family operators have reported in service occurrences of

hydraulic pump electrical motor connector internal arcing resulting in false hydraulic

system overheat Electronic Centralized Aircraft Monitoring (ECAM) warnings and/or

hydraulic pump electrical motor malfunction. Investigations have shown that under some

conditions of the cables and the connectors rear grommet manufacturing tolerances,

there is a possible path for fluid ingress resulting in the connector internal arcing and

hydraulic system failure.

(2) Objective/Action

This modification introduces heat shrink sleeves to the rear of the gauge 12 and 10

cable contacts and a sealing plug to the connector free cavity to increase the water

tightness of the hydraulic pump electrical motor connectors 1JCA, 1JJA and 1JVA.

(3) Advantages

The accomplishment of this Service Bulletin will prevent the possible hydraulic pump

electrical motor connectors fluid ingress from the rear of the connector grommet and will

prevent the false hydraulic system overheat ECAM warnings and/or hydraulic pump

electrical motor malfunction.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 925053-831-801-001: Modification

(1) Modify the equipment 1JCA

(2) Modify the equipment 1JJA

(3) Modify the equipment 1JVA

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

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SERVICE BULLETIN

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is requested within 3600 FH from AD effective

date.

Accomplishment of this Service Bulletin is expected to be rendered mandatory by the

issue of an Airworthiness Directive (AD) published by the European Aviation Safety

Agency (EASA). 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

Approved under EASA Design Organisation Approval No. EASA 21J.031.

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

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

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

before incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost to

do the work. These estimates assume that the work will be done by experienced personnel,

and may need to be revised upwards to suit operator’s circumstances. The estimates do not

include the time to prepare, plan or inspect the work. Manufacture and procurement of parts

and tools, drying times for paints, sealants, etc., and general administration work are also not

included.

Task 925053-831-801-001: Modification

Get Access 3.00

On Aircraft

Modify the equipment 1JCA 2.00

Modify the equipment 1JJA 2.00

Modify the equipment 1JVA 2.00

Tests 0.50

Close-Up 3.00

TOTAL MANHOURS 12.50

ELAPSED TIME (HOURS) 4.50

NOTE: For detail concerning the elapsed time assumptions, refer to Appendix 01 .

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

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J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-53 12-34-24

29-21-51 29-22-51 29-23-51

Aircraft Wiring List (AWL)

Elec. Std. Practices Manual (ESPM) 20-33-00 20-33-34 20-42-12

20-48-23 20-48-41 20-55-00

Standards Manual (SM)

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

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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 925053A01R02 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 925053A01R02

Cost 877.00 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.

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will provide the material at no charge for orders placed before December 2012.

AIRBUS will also credit the manhours indicated in this Service Bulletin at the operator’s

agreed in-house warranty labor rate for claims received not later than 90 days after

completion of the last affected aircraft of your fleet.

C. LIST OF COMPONENTS

Kit 925053A01R02

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

NOTES

E0347DR0801 6 SOCKET E0347DR0801

E0616BB0800 30 PLUG

E0718-02 1 (M) TUBING

E0718-03 1 (M) TUBING

NSA935401-04 30 TIE

NSA938186-03 6 REDUCER

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

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

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

to part number relationship.

NOTE: For information, kits 925053A01R00 and 925053A01R02 contents are

identical.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

None

(2) Components

Component COMPA01

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

NOTES

NSA938186-04 3 REDUCER

NSA938192DC0802 6 SOCKET

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.

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 925053-831-801-001 - Modification

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

Task Associated Data

Zone

147 195 196

Modified FIN

1JCA 1JJA 1JVA

Manpower

TOTAL MANHOURS 12.50

ELAPSED TIME (HOURS) 4.50

A. GENERAL

(1) Subtask 925053-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-41-53, Page Block 001

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

20-33-34

20-42-12

20-48-23

20-48-41

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

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

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SERVICE BULLETIN

(b) Obey the instructions for the heat shrink sleeves installation, (Refer to ESPM

20-33-34).

(c) For the description and the primary characteristics of the heat shrink sleeves,

(Refer to ESPM 20-42-12).

(d) Obey the instructions for the crimping, (Refer to ESPM 20-48-23).

(e) Obey the instructions for the blanking plugs installation, (Refer to ESPM 20-48-41).

(f) For the identification of the frames (FR), (Refer to AMM 06-31-53, Page Block 001).

(g) For the identification of the access panels, (Refer to AMM 06-41-53, Page Block

001).

(2) Subtask 925053-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 925053-941-001-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

195

196

147

Manpower Resources

Skills NON SPECIFIC

References

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

Task 29-21-51-000-801

Task 29-22-51-000-801

Task 29-23-51-000-801

(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) Do the preparation procedure as specified in the removal of the Green Electric

Pump (1JV), (Refer to AMM Task 29-21-51-000-801).

(d) Do the preparation procedure as specified in the removal of the Blue Electric Pump

(1JC), (Refer to AMM Task 29-22-51-000-801).

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(e) Do the preparation procedure as specified in the removal of the Yellow Electric

Pump (1JJ), (Refer to AMM Task 29-23-51-000-801).

C. PROCEDURE

(1) Subtask 925053-831-001-001 - Modify the equipment 1JCA

Work Zones and Access Panels

Zone Access/Work location

195 Work location from Frame 42 to Frame 43

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 925053A01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

E0347DR0801 2 SOCKET

E0616BB0800 10 PLUG

E0718-02 1 (M) TUBING

E0718-03 1 (M) TUBING

NSA935401-04 10 TIE

NSA938186-03 2 REDUCER

NOTE: For information, kits 925053A01R00 and 925053A01R02 contents are

identical.

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA938186-04 1 REDUCER

NSA938192DC0802 2 SOCKET

References

Aircraft Wiring List (AWL)

Fig. A-FAAAA

Location of the Equipment

Sheet 01

Fig. A-FADAA

Installation of the heat shrinking sleeves

Sheet 01

Fig. A-FAEAA

Installation of the heat shrinking sleeves

Sheet 01

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 11

5

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@A340-500/600

SERVICE BULLETIN

(a) If connector PN ASNE0233-24-10S is installed :

1 Disconnect the plug 1JCA.

2 Disconnect the wire 2922-0099 (gauge DK10) from the plug 1JCA (if installed).

3 Remove :

1 Socket E0347DR0801 Discard

from the wire.

4 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

5 Install on the wire :

1 Socket E0347DR0801

with :

1 Reducer NSA938186-03

NOTE: The sleeve has to be shrunk on the cable insulator.

NOTE: Put the sleeve front at the edge of the cable’s stripped

extremity.

6 Disconnect the wire 2922-0100 (gauge CF12 or DK12) from the plug 1JCA (if

installed).

7 Remove :

1 Socket E0347DR0801 Discard

from the wire.

NOTE: If a tubing heat shrinkable sleeve is already installed on the wire,

remove it.

8 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 35 mm (1.378 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 30 mm (1.181 in.)

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 12

5

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SERVICE BULLETIN

and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

1 Socket E0347DR0801

with :

1 Reducer NSA938186-03

NOTE: The sleeves have to be shrunk on the cable insulator.

NOTE:

Put each sleeve front at the edge of the cable’s stripped

extremity (Refer to Fig. A-FADAA).

9 Reconnect the wires on the plug 1JCA (Refer to Aircraft Wiring List (AWL)).

10 Use if necessary :

10 Tie-Cable NSA935401-04

11 On the plug, at the location on which the holes are not occupied, install :

10 Plug-Sealing E0616BB0800

12 Reconnect the plug 1JCA.

(b) If connector PN MS3456KT24-10S is installed :

1 Disconnect the plug 1JCA.

2 Disconnect the wire 2922-0099 (gauge DK10) from the plug 1JCA (if installed).

3 Remove :

1 Socket NSA938192DC0802 Discard

from the wire.

4 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

5 Install on the wire :

1 Socket NSA938192DC0802

with :

1 Reducer NSA938186-03

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 13

5

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@A340-500/600

SERVICE BULLETIN

NOTE: The sleeve has to be shrunk on the cable insulator.

NOTE: Put the sleeve front at the edge of the cable’s stripped

extremity.

6 Disconnect the wire 2922-0100 (gauge CF12 or DK12) from the plug 1JCA (if

installed).

7 Remove :

1 Socket NSA938192DC0802 Discard

from the wire.

NOTE: If a tubing heat shrinkable sleeve is already installed on the wire,

remove it.

8 If the PN of the removed socket is NSA938192DC0802, then install on the

wire :

1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 35 mm (1.378 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 30 mm (1.181 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

1 Socket NSA938192DC0802

with :

1 Reducer NSA938186-04

NOTE: The sleeves have to be shrunk on the cable insulator.

NOTE:

Put each sleeve front at the edge of the cable’s stripped

extremity (Refer to Fig. A-FAEAA).

9 Reconnect the wires on the plug 1JCA (Refer to Aircraft Wiring List (AWL)).

10 Use if necessary :

10 Tie-Cable NSA935401-04

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 14

5

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@A340-500/600

SERVICE BULLETIN

11 On the plug, at the location on which the holes are not occupied, install :

10 Plug-Sealing E0616BB0800

12 Reconnect the plug 1JCA.

(2) Subtask 925053-831-002-001 - Modify the equipment 1JJA

Work Zones and Access Panels

Zone Access/Work location

196 Work location from Frame 45 to Frame 46

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 925053A01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

E0347DR0801 2 SOCKET

E0616BB0800 10 PLUG

E0718-02 1 (M) TUBING

E0718-03 1 (M) TUBING

NSA935401-04 10 TIE

NSA938186-03 2 REDUCER

NOTE: For information, kits 925053A01R00 and 925053A01R02 contents are

identical.

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA938186-04 1 REDUCER

NSA938192DC0802 2 SOCKET

References

Aircraft Wiring List (AWL)

Fig. A-FABAA

Location of the Equipment

Sheet 01

Fig. A-FADAA

Installation of the heat shrinking sleeves

Sheet 01

Fig. A-FAEAA

Installation of the heat shrinking sleeves

Sheet 01

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 15

5

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

SERVICE BULLETIN

(a) If connector PN ASNE0233-24-10S is installed :

1 Disconnect the plug 1JJA.

2 Disconnect the wire 2923-0211 (gauge DK10) from the plug 1JJA (if installed).

3 Remove :

1 Socket E0347DR0801

from the wire.

4 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

5 Install on the wire :

1 Socket E0347DR0801

with :

1 Reducer NSA938186-03

NOTE: The sleeve has to be shrunk on the cable insulator.

NOTE: Put the sleeve front at the edge of the cable’s stripped

extremity.

6 Disconnect the wire 2923-0212 (gauge CF12 or DK12) from the plug 1JJA (if

installed).

7 Remove :

1 Socket E0347DR0801 Discard

from the wire.

NOTE: If a tubing heat shrinkable sleeve is already installed on the wire,

remove it.

8 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 35 mm (1.378 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 30 mm (1.181 in.)

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 16

5

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

SERVICE BULLETIN

and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

1 Socket E0347DR0801

with :

1 Reducer NSA938186-03

NOTE: The sleeves have to be shrunk on the cable insulator.

NOTE:

Put each sleeve front at the edge of the cable’s stripped

extremity (Refer to Fig. A-FADAA).

9 Reconnect the wires on the plug 1JJA (Refer to Aircraft Wiring List (AWL)).

10 Use if necessary :

10 Tie-Cable NSA935401-04

11 On the plug, at the location on which the holes are not occupied, install :

10 Plug-Sealing E0616BB0800

12 Reconnect the plug 1JJA.

(b) If connector PN MS3456KT24-10S is installed :

1 Disconnect the plug 1JJA.

2 Disconnect the wire 2923-0211 (gauge DK10) from the plug 1JJA (if installed).

3 Remove :

1 Socket NSA938192DC0802 Discard

from the wire.

4 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

5 Install on the wire :

1 Socket NSA938192DC0802

with :

1 Reducer NSA938186-03

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 17

5

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@A340-500/600

SERVICE BULLETIN

NOTE: The sleeve has to be shrunk on the cable insulator.

NOTE: Put the sleeve front at the edge of the cable’s stripped

extremity.

6 Disconnect the wire 2923-0212 (gauge CF12 or DK12) from the plug 1JJA (if

installed).

7 Remove :

1 Socket NSA938192DC0802 Discard

from the wire.

NOTE: If a tubing heat shrinkable sleeve is already installed on the wire,

remove it.

8 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 35 mm (1.378 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 30 mm (1.181 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

1 Socket NSA938192DC0802

with :

1 Reducer NSA938186-04

NOTE: The sleeves have to be shrunk on the cable insulator.

NOTE:

Put each sleeve front at the edge of the cable’s stripped

extremity (Refer to Fig. A-FAEAA).

9 Reconnect the wires on the plug 1JJA (Refer to Aircraft Wiring List (AWL)).

10 Use if necessary :

10 Tie-Cable NSA935401-04

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 18

5

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@A340-500/600

SERVICE BULLETIN

11 On the plug, at the location on which the holes are not occupied, install :

10 Plug-Sealing E0616BB0800

12 Reconnect the plug 1JJA.

(3) Subtask 925053-831-003-001 - Modify the equipment 1JVA

Work Zones and Access Panels

Zone Access/Work location

147 Work location from Frame 53.1 to Frame 53.2

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

Material necessary to do the job

Kit 925053A01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

E0347DR0801 2 SOCKET

E0616BB0800 10 PLUG

E0718-02 1 (M) TUBING

E0718-03 1 (M) TUBING

NSA935401-04 10 TIE

NSA938186-03 2 REDUCER

NOTE: For information, kits 925053A01R00 and 925053A01R02 contents are

identical.

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

NSA938186-04 1 REDUCER

NSA938192DC0802 2 SOCKET

References

Aircraft Wiring List (AWL)

Fig. A-FACAA

Location of the Equipment

Sheet 01

Fig. A-FADAA

Installation of the heat shrinking sleeves

Sheet 01

Fig. A-FAEAA

Installation of the heat shrinking sleeves

Sheet 01

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 19

5

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

SERVICE BULLETIN

(a) If connector PN ASNE0233-24-10S is installed :

1 Disconnect the plug 1JVA.

2 Disconnect the wire 2921-0183 (gauge DK10) from the plug 1JVA (if installed).

3 Remove :

1 Socket E0347DR0801 Discard

from the wire.

4 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

5 Install on the wire :

1 Socket E0347DR0801

with :

1 Reducer NSA938186-03

NOTE: The sleeve has to be shrunk on the cable insulator.

NOTE: Put the sleeve front at the edge of the cable’s stripped

extremity.

6 Disconnect the wire 2921-0184 (gauge CF12 or DK12) from the plug 1JVA (if

installed).

7 Remove :

1 Socket E0347DR0801 Discard

from the wire.

NOTE: If a tubing heat shrinkable sleeve is already installed on the wire,

remove it.

8 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 35 mm (1.378 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 30 mm (1.181 in.)

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 20

5

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

SERVICE BULLETIN

and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

and

1 Socket E0347DR0801

with :

1 Reducer NSA938186-03

NOTE: The sleeves have to be shrunk on the cable insulator.

NOTE:

Put each sleeve front at the edge of the cable’s stripped

extremity (Refer to Fig. A-FADAA).

9 Reconnect the wires on the plug 1JVA (Refer to Aircraft Wiring List (AWL)).

10 Use if necessary :

10 Tie-Cable NSA935401-04

11 On the plug, at the location on which the holes are not occupied, install :

10 Plug-Sealing E0616BB0800

12 Reconnect the plug 1JVA.

(b) If connector PN MS3456KT24-10S is installed :

1 Disconnect the plug 1JVA.

2 Disconnect the wire 2921-0183 (gauge DK10) from the plug 1JVA (if installed).

3 Remove :

1 Socket NSA938192DC0802 Discard

from the wire.

4 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

5 Install on the wire :

1 Socket NSA938192DC0802

with :

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 21

5

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@A340-500/600

SERVICE BULLETIN

1 Reducer NSA938186-03

NOTE: The sleeve has to be shrunk on the cable insulator.

NOTE: Put the sleeve front at the edge of the cable’s stripped

extremity.

6 Disconnect the wire 2921-0184 (gauge CF12 or DK12) from the plug 1JVA (if

installed).

7 Remove :

1 Socket NSA938192DC0802 Discard

from the wire.

NOTE: If a tubing heat shrinkable sleeve is already installed on the wire,

remove it.

8 Install on the wire :

1 (M) Tubing-Heat-Shrinkable E0718-02

NOTE: Cut the tubing-heat at 35 mm (1.378 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 30 mm (1.181 in.)

and

1 (M) Tubing-Heat-Shrinkable E0718-03

NOTE: Cut the tubing-heat at 25 mm (0.984 in.).

1 Socket NSA938192DC0802

with :

1 Reducer NSA938186-04

NOTE: The sleeves have to be shrunk on the cable insulator.

NOTE:

Put each sleeve front at the edge of the cable’s stripped

extremity (Refer to Fig. A-FAEAA).

9 Reconnect the wires on the plug 1JVA (Refer to Aircraft Wiring List (AWL)).

10 Use if necessary :

10 Tie-Cable NSA935401-04

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 22

5

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@A340-500/600

SERVICE BULLETIN

11 On the plug, at the location on which the holes are not occupied, install :

10 Plug-Sealing E0616BB0800

12 Reconnect the plug 1JVA.

D. TEST

(1) Subtask 925053-865-001-001 - C/B Closing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 29-21-51-400-801

Task 29-22-51-400-801

Task 29-23-51-400-801

(a) Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the green electric pump (1JV), (Refer to AMM Task

29-21-51-400-801).

(b) Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the blue electric pump (1JC), (Refer to AMM Task

29-22-51-400-801)

(c) Remove the safety clips and tags and close the circuit breakers as specified

after the installation of the yellow electric pump (1JJ), (Refer to AMM Task

29-23-51-400-801)

(2) Subtask 925053-710-001-001 - Operational

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 29-21-51-400-801

Task 29-22-51-400-801

Task 29-23-51-400-801

(a) Do the test procedure as specified after the installation of the Green Electric Pump

(1JV), (Refer to AMM Task 29-21-51-400-801).

(b) Do the test procedure as specified after the installation of the Blue Electric Pump

(1JC), (Refer to AMM Task 29-22-51-400-801).

(c) Do the test procedure as specified after the installation of the Yellow Electric Pump

(1JJ), (Refer to AMM Task 29-23-51-400-801).

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 23

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@A340-500/600

SERVICE BULLETIN

E. CLOSE-UP

(1) Subtask 925053-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 29-21-51-400-801

Task 29-22-51-400-801

Task 29-23-51-400-801

(a) Do the close-up procedure as specified after the installation of the Green Electric

Pump (1JV), (Refer to AMM Task 29-21-51-400-801).

(b) Do the close-up procedure as specified after the installation of the Blue Electric

Pump (1JC), (Refer to AMM Task 29-22-51-400-801).

(c) Do the close-up procedure as specified after the installation of the Yellow Electric

Pump (1JJ), (Refer to AMM Task 29-23-51-400-801).

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

equipment.

(e) Restore the systems and the aircraft to normal operating condition.

(f) Remove the access platform(s).

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 24

5

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

F_SB_925053_5_AAAA_01_00

1JCA

B

A Z190

B

1JC

FR40.4

FR40.5

FR40.6

FR41

FR43

FR42

A

BLUE ELECTRIC PUMP

Figure A-FAAAA - Sheet 01

Location of the Equipment

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 25

5

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

Z196

1JJA

F_SB_925053_5_ABAA_01_00

FR45

FR46

A

1JJ

B

A

B

YELLOW ELECTRIC PUMP

Figure A-FABAA - Sheet 01

Location of the Equipment

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 26

5

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

F_SB_925053_5_ACAA_01_00

1JV

B

FR53.1

FR53.2

1JVA

A

Z147

FR53.1

FR53.2

A

GREEN ELECTRIC PUMP

B

Figure A-FACAA - Sheet 01

Location of the Equipment

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 27

5

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

CABLE GAUGE CF12 OR DK12

(L : 25 mm (0.984 in ))

SLEEVE ASNE0718−03

HEAT−SHRINKING

(L : 30 mm (1.181 in ))

SLEEVE ASNE0718−02

HEAT−SHRINKING

CONTACT

(L : 35 mm (1.378 in ))

SLEEVE ASNE0718−02

HEAT−SHRINKING

01

F_SB_925053_5_ADAA_01_03

NOTE:

01 THIS INSTALLATION IS VALID FOR CONNECTOR PN ASNE0233−24−10S

Figure A-FADAA - Sheet 01

Installation of the heat shrinking sleeves

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 28

5

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

CABLE GAUGE CF12 OR DK12

(L : 25 mm (0.984 in ))

SLEEVE ASNE0718−03

HEAT−SHRINKING

(L : 30 mm (1.181 in ))

SLEEVE ASNE0718−03

HEAT−SHRINKING

CONTACT

(L : 35 mm (1.378 in ))

SLEEVE ASNE0718−02

HEAT−SHRINKING

01

F_SB_925053_5_AEAA_01_02

NOTE:

01 THIS INSTALLATION IS VALID FOR CONNECTOR PN MS3456KT24−10S

Figure A-FAEAA - Sheet 01

Installation of the heat shrinking sleeves

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 29

5

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@A340-500/600

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 30

5

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@A340-500/600

SERVICE BULLETIN

Appendix 01

**CONF ALL

(1) For detail concerning the elapsed time assumption of the modification, refer to the Gantt chart next

page :

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 1

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@A340-500/600

SERVICE BULLETIN

Appendix 01

**CONF ALL

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−92−3088

ELAPSED TIME

(HOURS)

NOTE: THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

MH ET PER

MH:

ET:

PER:

MANHOURS

ELAPSED TIME

NUMBER OF PERSONS

TOTAL MANHOURS (MH)

ELAPSED TIME (ET)

12.50

4.50

STEPS

0 1 2 3 4 5

GET ACCESS 3.00 1.00 3

MODIF. OF THE EQUIPMENT 1JJ−A 2.00 2.00 1

MODIFICATION 6.00 2.00 3

MODIF. OF THE EQUIPMENT 1JV−A 2.00 2.00 1

TEST 0.50 0.50 1

CLOSE−UP 3.00 1.00 3

MODIF. OF THE EQUIPMENT 1JC−A 2.00 2.00 1

F_SB_925053_5_BAAA_01_01

Figure A-FBAAA - Sheet 01

Gantt Chart

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 2

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@A340-500/600

SERVICE BULLETIN

REPORTING SHEET

TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALL-IMPROVE EMP

ELECTRICAL CONNECTOR AND SLEEVE.

MODIFICATION No.: 58773S30712

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 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 1

5

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 4 3 2 1

- Quality rating of the Accomplishment Instructions 4 3 2 1

- Quality rating of the Illustrations 4 3 2 1

- Is this SB easy to understand ? Y / N

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

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

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

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-5053

REVISION No.: 02 - Sep 01/10 Page: 1

5

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