@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: 92

TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - IMPROVE

EMP ELECTRICAL CONNECTOR AND SLEEVE.

MODIFICATION No.: 58773S30712

This page transmits Revision No.02 of Service Bulletin No.A340-92-4081

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

EFFECTIVITY OPERATOR LIST 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

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

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

MANPOWER MANPOWER UPDATED R

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

INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED R

LIST OF COMPONENTS

Kit 924081A01R02 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 924081- 831-801-001-Modification

Subtask 924081-910-001-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 924081-941-001-001 SUBTASK SOLUTION UPDATED R

Subtask 924081-831-003-001 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

Subtask 924081-831-002-001 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.: A340-92-4081

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@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 924081-831-004-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

KEYWORD UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

FIN UPDATED

NOTE UPDATED

REFERENCED DOCUMENTATION 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

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.: A340-92-4081

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.: A340-92-4081

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

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@A340

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 INSTALLATION - 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

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@A340

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 924081A01R02 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) :

44W 47W 56W 83V AAW AFR AIB ALK ARG B3R CAL CCA CES

CPA DGA DLH FIN GFA HFY IBE KAC LAN LHT M3R MAU MSR

NMB OAL PAL QAF R3L RJA S3R SAA SAS SFW 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

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

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@A340

SERVICE BULLETIN

SUMMARY

MANPOWER

Task 924081-831-801-001: Modification

TOTAL MANHOURS 12.50

ELAPSED TIME (HOURS) 4.50

APPENDICES

Appendix 01

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@A340

SERVICE BULLETIN

SUMMARY

**CONF ALL

F_SB_924081_5_SAAA_01_00

1JCA

1JJA

1JVA

Figure A-FSAAA - Sheet 01

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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 INSTALLATION - 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

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

(2) Effectivity by MSN

0002-0009 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 0097 0101 0103-0104 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

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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

44W 0007

47W 0009

56W 0013

83V 0040

AAW 0151

AFR 0029 0078 0084 0168 0174 0186 0207 0210 0237 0245 0246 0260

0307 0310 0319 0373 0377 0399

AIB 0197 0378

ALK 0032 0033 0034 0367 0374

ARG 0048 0063 0074 0080 0085 0093 0094

B3R 0046

CAL 0402 0406 0411 0415 0433 0541

CCA 0192 0199 0201 0242 0243 0264

CES 0129 0131 0141 0161 0182

CPA 0123 0126 0128 0136 0137 0142 0147 0157 0160 0208 0218 0220

0227 0228 0381

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 0355 0379

0390 0434 0447

FIN 0058 0835 0844 0921 0938

GFA 0039 0097 0103 0133 0212 0215 0282 0554

HFY 0117

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

LAN 0167 0359 0363 0429 0442

LHT 0274

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

R3L 0004

RJA 0014 0022 0038 0043

S3R 0204

SAA 0006 0008 0011 0018 0019 0021 0544 0582 0590 0643 0646 0651

SAS 0413 0424 0430 0435 0450 0467 0470

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SERVICE BULLETIN

OPERATOR MSN

SFW 0015

SLM 0049

SVW 0955

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 0002 0003 0114 0164 0214 0225

XAX 0273 0278

(4) Configuration by MSN

MSN CONFIGURATION

0002 0003 0004 0005 0006 0007 0008 0009 0011 0013 0014

0015 0018 0019 0020 0021 0022 0023 0024 0025 0026 0027

0028 0029 0031 0032 0033 0034 0035 0038 0039 0040 0041

0043 0044 0046 0047 0048 0049 0051 0052 0053 0056 0057

0058 0061 0063 0074 0075 0076 0078 0079 0080 0081 0084

0085 0088 0089 0090 0091 0093 0094 0097 0101 0103 0104

0114 0115 0117 0123 0125 0126 0128 0129 0131 0133 0134

0135 0136 0137 0139 0141 0142 0145 0146 0147 0149 0150

0151 0152 0154 0156 0157 0158 0159 0160 0161 0163 0164

0166 0167 0168 0169 0170 0173 0174 0175 0176 0178 0179

0180 0182 0185 0186 0187 0190 0192 0193 0194 0196 0197

0199 0201 0202 0204 0207 0208 0210 0212 0213 0214 0215

0216 0217 0218 0220 0221 0225 0227 0228 0233 0235 0236

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 0378

0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413

0414 0415 0424 0429 0430 0433 0434 0435 0438 0442 0446

0447 0450 0459 0467 0470 0474 0483 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

(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.

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SERVICE BULLETIN

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Kit 924081A01R02 1

Component COMPA01 1

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 924081-831-801-001: Modification

(1) Modify the equipment 1JCA

(2) Modify the equipment 1JJA

(3) Modify the equipment 1JVA

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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SERVICE BULLETIN

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

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

date.

Accomplishment of this Service Bulletin has been rendered mandatory by the issue of an

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

The AD must be used as the reference document for the mandatory 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 924081-831-801-001: 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

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SERVICE BULLETIN

I. ELECTRICAL LOAD DATA

Not Changed

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.: A340-92-4081

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

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

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

Kit 924081A01R02 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 924081A01R02

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 this Service Bulletin kit 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. Some Operators will require reducer PN NSA938186-04

and socket PN NSA938192DC0802 for connector PN MS3456KT24-10S as an alternative to

PN ASNE0233-24-10S. These two parts should be sourced directly by the Operator and will

be reimbursed by Airbus. Claims must be received not later than 90 days after completion of

the last affected aircraft of your fleet

C. LIST OF COMPONENTS

Kit 924081A01R02

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

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SERVICE BULLETIN

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

NOTES

NSA935401-04 30 TIE

NSA938186-03 6 REDUCER

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 924081A01R00 and 924081A01R02 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 NSA938192DC0802

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

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 924081-831-801-001 - 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 924081-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-41-53, Page Block 001

Task 12-34-24-860-802

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.: A340-92-4081

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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 924081-839-001-001 - 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 924081-941-001-001 - 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).

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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SERVICE BULLETIN

(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 924081-831-003-001 - Modify the equipment 1JCA

Work Zones and Access Panels

Zone Access/Work location

195 Work location from Frame 46 to Frame 47

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 924081A01R02

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 924081A01R00 and 924081A01R02 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-FADAA

Installation of the heat shrinking sleeves

Sheet 01

Fig. A-FAAAA

Location of the equipment

Sheet 01

Fig. A-FAEAA

Installation of the heat shrinking sleeves

Sheet 01

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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.: A340-92-4081

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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.).

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 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 :

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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 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.).

and

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)).

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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SERVICE BULLETIN

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.

(2) Subtask 924081-831-002-001 - 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 924081A01R02

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 924081A01R00 and 924081A01R02 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

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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SERVICE BULLETIN

References

Fig. A-FAEAA

Installation of the heat shrinking sleeves

Sheet 01

(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 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 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

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

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.).

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 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.).

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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SERVICE BULLETIN

5 Install on the wire :

1 Socket NSA938192DC0802

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 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.).

and

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).

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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SERVICE BULLETIN

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.

(3) Subtask 924081-831-004-001 - 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 924081A01R02

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 924081A01R00 and 924081A01R02 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

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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References

Fig. A-FADAA

Installation of the heat shrinking sleeves

Sheet 01

Fig. A-FAEAA

Installation of the heat shrinking sleeves

Sheet 01

(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

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.)

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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and

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

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 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.).

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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

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SERVICE BULLETIN

5 Install on the wire :

1 Socket NSA938192DC0802

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 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.).

and

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).

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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SERVICE BULLETIN

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.

D. TEST

(1) Subtask 924081-865-001-001 - 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 924081-710-001-001 - 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).

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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(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).

E. CLOSE-UP

(1) Subtask 924081-942-001-001 - 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.: A340-92-4081

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SERVICE BULLETIN

**CONF ALL

FR46

FR47

A

Z195

B

1JC

A

1JCA

B

BLUE ELECTRIC PUMP

F_SB_924081_5_AAAA_01_00

Figure A-FAAAA - Sheet 01

Location of the equipment

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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SERVICE BULLETIN

**CONF ALL

FR45

FR46

Z196

A

B

1JJ

1JJA B

A

YELLOW ELECTRIC PUMP

F_SB_924081_5_ABAA_01_00

Figure A-FABAA - Sheet 01

Location of the equipment

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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SERVICE BULLETIN

**CONF ALL

1JV

B

B

A

1JVA

F_SB_924081_5_ACAA_01_00

Z147

FR53.2

FR53.1

A

FR53.1

FR53.2

GREEN ELECTRIC PUMP

Figure A-FACAA - Sheet 01

Location of the equipment

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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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_924081_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.: A340-92-4081

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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_924081_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.: A340-92-4081

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

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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

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SERVICE BULLETIN

Appendix 01

**CONF ALL

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

shown below :

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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

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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_924081_5_BAAA_01_01

Figure A-FBAAA - Sheet 01

Gantt Chart

DATE: Sep 02/09 SERVICE BULLETIN No.: A340-92-4081

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

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SERVICE BULLETIN

REPORTING SHEET

TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION - 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.: A340-92-4081

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

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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.: A340-92-4081

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

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