@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-CABLE LOOM

INSTALLATION DRAWINGS-IMPROVEMENT OF FEEDER ROUTING

ATTACHMENT IN WING/PYLON

MODIFICATION No.: 203672D50692

This page transmits Revision No.01 of Service Bulletin No.A340-92-4100

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No. 01 issued to:

- replace the consumable material 08ADB1 with consumable 08BPA1

- add the correct ESPM references

- add work steps in Para 3.C. to rework the holes in bracket, Item 3, if necessary

- correct figure A-GBAAA

- add Appendix 02

- update the Service Bulletin effectivity.

CHANGES

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE

UPDATED

R

EFFECTIVITY OPERATOR LIST UPDATED R

APPENDICES APPENDICES UPDATED R

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 1

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED R

Material Effectivity MATERIAL EFFECTIVITY UPDATED

MATERIAL SET UPDATED

MATERIAL SET QUANTITY UPDATED

R

REASON

Objective/Action OBJECTIVE/ACTION 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

LIST OF COMPONENTS

Kit 924100D01R03 PART MATERIAL SET UPDATED

MATERIAL SET LABEL UPDATED

QUANTITY UPDATED

NOTE UPDATED

R

LIST OF MATERIALS - OPERATOR

SUPPLIED

Consumable Materials

Consumable CMLD01 CONSUMABLE MATERIAL SET UPDATED

CONSUMABLE UPDATED

R

ACCOMPLISHMENT INSTRUCTIONS

TASK 924100- 831-848-001-Modification

Subtask 924100-910-201-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 924100-831-201-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 924100-831-202-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 2

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 924100-942-201-001 SUBTASK SOLUTION UPDATED R

Fig. A-GBAAA FIGURE SOLUTION UPDATED R

Fig. A-GBAAA Sheet 01 SHEET UPDATED R

Fig. A-GBAAA Sheet 02 SHEET ADDED N

Appendix 02 - Post SB Installation Details

APPENDIX CONTENT APPENDIX CONTENT ADDED N

Fig. A-GABAA FIGURE SOLUTION ADDED N

Fig. A-GABAA Sheet 01 SHEET ADDED N

Fig. A-GABAA Sheet 02 SHEET ADDED N

FILING INSTRUCTIONS

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

Replace the complete document.

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

HISTORY OF PREVIOUS REVISIONS

No previous revision

REVISION SEQUENCE

ORIGINAL: Jun 19/14

REVISION No. : 01 - May 21/15

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 4

6

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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-CABLE LOOM

INSTALLATION DRAWINGS-IMPROVEMENT OF FEEDER ROUTING

ATTACHMENT IN WING/PYLON

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 203672D50692

MINOR None

NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the

mass, balance, structural strength, reliability, operational characteristics affecting the

airworthiness of the product. All other changes are major changes.

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

The G-route wiring looms 7701VB and 7702VB are fixed with plastic brackets and metallic clamps at

the first attachment point in the wing after each inboard pylon in the LH and RH wings. Due to vibration,

cracks have been found to occur in the bracket and the metallic strap has been found to be missing.

This can cause chafing of the wiring loom on the aircraft structure.

This modification installs a new metallic bracket with electrical bonding, reinforced clamp and grommet

to replace the existing parts at the first attachment point in the wing after each inboard pylon in the LH

and RH wings.

Accomplishment of this Service Bulletin will improve the wiring installation in the wing/pylon area to

prevent chafing, possible short circuits and damage to systems. This will prevent potential system

misbehavior, improve reliability and avoid unscheduled maintenance action.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED YES PAX COMFORT AFFECTED NO

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

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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 924100D01R03 1 900.00 Grommets, Brackets and Attaching Parts

EFFECTIVITY

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

06Y 15R 15T 22O 31V 56W 74W 83V 98W 98X ABD AFR AIB

ALD ALK ARG BOE CAL CCA CPA DGA DLH F2I FIN G8E GAF

HFM IBE IRC IRM KAC LAN M3R MAU MDG MHK PAL PUE QAF

S3R SAA SAS SFB SLM SVW SWR TAP THT THY UAE VCV VIR

XAX

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 924100-831-848-001: Modification

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.00

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 2

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@A340

SERVICE BULLETIN

SUMMARY

APPENDICES

Appendix 01 - Elapsed Time Assumption

Appendix 02 - Post SB Installation Details

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

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@A340

SERVICE BULLETIN

SUMMARY

**CONF ALL

A

LH SHOWN

RH SIMILAR

B

RIB11A

B

NOTE:

AREA OF MODIFICATION

A

A

Z462 Z521 , 

Z472 Z621 , 

F_SB_924100_6_SAAA_01_01

Figure A-GSAAA - Sheet 01

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 4

6

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

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 92

TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION-CABLE LOOM

INSTALLATION DRAWINGS-IMPROVEMENT OF FEEDER ROUTING

ATTACHMENT IN WING/PYLON

MODIFICATION No.: 203672D50692

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 0004 0006 0009 0014 0020 0022-0023 0025-0026 0029 0031-0034 0038 0041

0043-0044 0046-0047 0049 0051 0053 0056-0058 0061 0063 0074-0076 0078-0081

0084-0085 0089-0091 0093-0094 0101 0104 0114-0115 0117 0123 0125-0126 0128

0131 0134-0137 0139 0141-0142 0145-0147 0149-0152 0154 0156-0161 0163-0164

0166-0170 0173-0175 0178-0180 0182 0185-0187 0190 0192-0194 0196-0197 0199

0201-0202 0204 0207-0208 0210 0212-0218 0220-0221 0227-0228 0233 0236-0237

0242-0243 0245-0246 0252 0257 0260 0263-0264 0268 0270 0273-0274 0278 0280

0282 0292 0297 0302 0304 0307 0310 0318-0319 0321 0325 0327 0329 0331-0332

0335 0347 0352 0354-0355 0359 0363 0367 0373-0374 0377-0379 0381 0385 0387

0390 0395 0399 0402 0406 0411 0413 0415 0424 0429-0430 0433-0435 0438 0442

0446-0447 0450 0459 0467 0470 0474 0483 0528 0538 0541 0544-0546 0554 0556

0559 0561-0562 0582 0585 0590 0598 0643 0646 0651 0668 0793 0800 0835 0844

0921 0938 0955

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

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@A340

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

06Y 0139 0149

15R 0151

15T 0009

22O 0257

31V 0093

56W 0006

74W 0047 0051

83V 0216 0280 0292

98W 0014 0022

98X 0429

ABD 0210

AFR 0029 0078 0084 0186 0207 0237 0245 0246 0260 0307 0310 0377

0399

AIB 0131 0141 0161 0182 0192 0199

ALD 0156 0159 0178

ALK 0032 0033 0034 0367 0374 0381

ARG 0085 0094 0123 0126 0128 0170 0193 0373

BOE 0554

CAL 0402 0406 0411 0415 0433 0541

CCA 0201 0242 0243 0264

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

DGA 0075 0081

DLH 0053 0135 0158 0213 0233 0252 0297 0304 0321 0325 0327 0335

0347 0352 0354 0379 0390 0434 0447

F2I 0038 0043 0063 0074 0080

FIN 0058 0168 0174 0835 0844 0921 0938

G8E 0173 0187 0196

GAF 0274 0355

HFM 0117 0190 0202

IBE 0125 0134 0145 0146 0217 0221 0329 0483

IRC 0002

IRM 0020 0056 0282

KAC 0089 0090 0101 0104

LAN 0359 0363 0442

M3R 0061

MAU 0076 0152 0194 0268 0793 0800

MDG 0319

MHK 0164

PAL 0302 0318 0332 0387 0459 0474

PUE 0212 0215

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

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@A340

SERVICE BULLETIN

OPERATOR MSN

QAF 0026 0528

S3R 0004 0204

SAA 0197 0378 0544 0582 0590 0643 0646 0651

SAS 0167 0413 0424 0430 0435 0450 0467 0470

SFB 0046

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 0270 0331

UAE 0163 0166 0185 0236

VCV 0031

VIR 0114 0214

XAX 0273 0278

(4) Configuration by MSN

MSN CONFIGURATION

0002 0004 0006 0009 0014 0020 0022 0023 0025 0026 0029

0031 0032 0033 0034 0038 0041 0043 0044 0046 0047 0049

0051 0053 0056 0057 0058 0061 0063 0074 0075 0076 0078

0079 0080 0081 0084 0085 0089 0090 0091 0093 0094 0101

0104 0114 0115 0117 0123 0125 0126 0128 0131 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 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 0227 0228 0233 0236 0237 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 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. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

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SERVICE BULLETIN

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Kit 924100D01R03 1

Consumable CMLD01 1

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

The G-route wiring looms 7701VB and 7702VB are fixed with plastic brackets and

metallic clamps at the first attachment point in the wing after each inboard pylon in the

LH and RH wings. Due to vibration, cracks have been found to occur in the bracket and

the metallic strap has been found to be missing. This can cause chafing of the wiring

loom on the aircraft structure.

(2) Objective/Action

This modification installs a new metallic bracket with electrical bonding, reinforced clamp

and grommet to replace the existing parts at the first attachment point in the wing after

each inboard pylon in the LH and RH wings.

(3) Advantages

Accomplishment of this Service Bulletin will improve the wiring installation in the

wing/pylon area to prevent chafing, possible short circuits and damage to systems. This

will prevent potential system misbehavior, improve reliability and avoid unscheduled

maintenance action.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 924100-831-848-001: Modification

(1) Modify the Cable Loom Support Bracket of the G-route 7701VB LH

(2) Modify the Cable Loom Support Bracket of the G-route 7702VB RH

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

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SERVICE BULLETIN

(2) Accomplishment Timescale

This Service Bulletin must be accomplished before Oct 31/16.

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

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

to confirm this classification. It is anticipated that the AD will confirm the date given

above but reference should be made to the AD for confirmation of the mandated

accomplishment timescale.

F. APPROVAL

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

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 924100-831-848-001: Modification

Get Access 2.00

On Aircraft

Modify the Cable Loom Support Bracket of the G-route

7701VB LH

2.00

Modify the Cable Loom Support Bracket of the G-route

7702VB RH

2.00

Close-Up 2.00

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.00

NOTE: For an explanation of the manhours and elapsed time, refer to the Gantt

Chart, Fig. A-GAAAA given in Appendix 01 - Elapsed Time Assumption .

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

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SERVICE BULLETIN

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53

11-00-00 12-34-24 20-21-11

20-28-00 57-41-37 57-42-37

Elec. Std. Practices Manual (ESPM) 20-33-00 20-33-11 20-33-41

20-51-20 20-51-22 20-55-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-21-00 51-23-11 51-40-00

51-42-00 51-44-00

K. PUBLICATION AFFECTED

Elec. Std. Practices Manual (ESPM) 20-33-11 20-33-41

Illustrated Parts Catalog (IPC) 57-26-05

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

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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 924100D01R03 AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 HAMBURG

GERMANY

For ordering by internet:

http://spares.airbus.com

For ordering by fax: +49 40 50 76 2590

For ordering by E-mail: airbus.kit@airbus.com

(2) Price and Availability

Kit 924100D01R03

Cost 900.00 USD

Availability 90 calendar days from receipt of order

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

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

The sales terms (costs and availability) are estimated in relation to economic conditions.

The latest valid price and lead time for ordering purposes shall be obtained through the

AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will share the costs of accomplishment of this Service Bulletin by providing the kits at

no charge for orders placed before Dec 31/17.

For aircraft under warranty at Jan 01/13, AIRBUS will credit the manhours indicated in this

Service Bulletin at the 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 924100D01R03

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

NOTES

1 MS21042L3 4 NUT

2 NAS1149D0363H 8 WASHER

3 F9249296220000 2 BRACKET

4 ASNA0032-060 2 CLAMP

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

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SERVICE BULLETIN

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

NOTES

5 NAS1801-3-12 4 SCREW

6 ABS0678B02 2 SUPPORT

8 NSA939510CN 0.578 STRIP

9 F9239026810200 1 PLCRDSET (1)

11 NSA935401-03 2 TIE

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 (1): This placard set contains Service Bulletin accomplishment placards for both

LH and RH wings.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Varnish-- Electrical Bonding

Structure

04TMB2 As required

Coating Sealant-Fuel Tank

Brushable

06HAA1 As required

Non Aqueous Cleaner - Non

Structural Use

08BPA1 As required

Textile-Lint Free Cotton 14SBA1 As required

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 924100-831-848-001 - 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.

NOTE: The accomplishment instructions of this Service Bulletin include procedures given

in other documents or in other sections of the Service Bulletin. When the words

"refer to" are used and the operator has a procedure accepted by the local

authority he belongs to, the accepted alternative procedure can be used. When the

words "in accordance with" are used then the given procedure must be followed.

NOTE: The access and close-up instructions, not comprising return to service tests, in this

Service Bulletin do not constitute or affect the technical intent of the Service

Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or

close-up steps to add flexibility to their maintenance operations as long as the

technical intent of the Service Bulletin is met within the set parameters.

NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms.

Refer to paragraph 1.J., References, for the definition of acronyms.

NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory

by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these

accomplishment instructions are Required for Compliance (RC) and must be done

to comply with the AD. Other paragraphs are recommended and may be deviated

from, done as part of other actions or done with accepted methods different from

those given in the Service Bulletin, as long as the RC paragraphs can be done and

the aircraft can be put back into a serviceable condition.

Task Associated Data

Zone

452 462 472 521 522 621 622

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 9

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SERVICE BULLETIN

Manpower

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.00

A. GENERAL

(1) Subtask 924100-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-31-53, Page Block 001

06-41-53, Page Block 001

11-00-00, Page Block 201

Task 20-21-11-911-801

Task 20-28-00-912-802

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

20-51-20

Structural Repair Manual (SRM) 51-21-00

51-23-11

51-40-00

51-42-00

51-44-00

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

(b) For the identification of zones, refer to AMM 06-20-00, Page Block 001.

(c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

(d) Remove and install fasteners in accordance with SRM 51-42-00.

(e) To torque tighten the standard threaded fasteners, refer to AMM Task

20-21-11-911-801.

(f) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00 ’Mating Part’

column.

(g) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(h) For the general installation of electrical harnesses, refer to ESPM 20-33-00.

(i) For the electrical bonding, refer to ESPM 20-51-20 and refer to AMM Task

20-28-00-912-802.

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 10

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SERVICE BULLETIN

(j) For the installation of placards, refer to AMM 11-00-00, Page Block 201.

(k) Apply protective treatment in accordance with SRM 51-21-00.

(l) Apply paint coatings in accordance with SRM 51-23-11.

(m) Obtain fastener hole diameters and drill and de-burr data in accordance with SRM

51-44-00.

(2) Subtask 924100-839-201-001 - 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 924100-941-201-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

452

462

522

622

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-860-802

Task 57-41-37-000-801

Task 57-42-37-000-801

NOTE: The items given in this note shall be considered as the basic Aircraft

configuration before you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety

locks and the wheel chocks are in position on the landing gear)

- Engine shut down, thrust reversers closed and locked

- Aircraft in clean configuration

- Parking brake applied

- Aircraft electrical network de-energized

- Hydraulic systems depressurized

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 11

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SERVICE BULLETIN

- Access to the cockpit and cabin is available

- All circuit breakers are in closed position

- All controls in NORM, AUTO or OFF position.

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

12-34-24-860-802.

(b) To get access for the LH Wing:

1 Remove the fixed leading edge access panels 522AB and 522BB, refer to

AMM Task 57-41-37-000-801 and AMM Task 57-42-37-000-801.

2 Remove the inboard pylon access panels 462GL and 462HR, refer to AMM

06-41-53, Page Block 001.

(c) To get access for the RH Wing:

1 Remove the fixed leading edge access panels 622AB and 622BB, refer to

AMM Task 57-41-37-000-801 and AMM Task 57-42-37-000-801.

2 Remove the inboard pylon access panels 472JR and 472HL, refer to AMM

06-41-53, Page Block 001.

C. PROCEDURE

(1) Subtask 924100-831-201-001 - Modify the Cable Loom Support Bracket of the Groute 7701VB LH

Work Zones and Access Panels

Zone Access/Work location

462

472

521

621

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Kit 924100D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 MS21042L3 2 NUT

2 NAS1149D0363H 4 WASHER

3 F9249296220000 1 BRACKET

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 12

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

4 ASNA0032-060 1 CLAMP

5 NAS1801-3-12 2 SCREW

6 ABS0678B02 1 SUPPORT

8 NSA939510CN 0.29 STRIP

9 F9239026810200 1 PLCRDSET (1)

11 NSA935401-03 1 TIE

NOTE (1): This placard set contains Service Bulletin accomplishment placards for

both LH and RH wings.

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish-- Electrical Bonding

Structure

04TMB2 As required

Coating Sealant-Fuel Tank

Brushable

06HAA1 As required

Non Aqueous Cleaner -

Non Structural Use

08BPA1

Textile-Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) 11-00-00, Page Block 001

Task 20-28-00-912-802

Elec. Std. Practices Manual (ESPM) 20-33-11

20-33-41

20-51-22

Structural Repair Manual (SRM) 51-44-00

Fig. A-GBAAA

Modification of the Cable Loom Support

Bracket, LH and RH

Sheet 01

Sheet 02

(a) At the attachment point in the LH wing after the inboard pylon, remove from the

wiring loom 7701VB, Item (7), refer to Fig. A-GBAAA Sheet 01, View C:

2 Nut MS21042L3 Item (1) Discard

2 Screw NAS1096-3-8 Item (5) Discard

4 Washer NAS1149D0316H Item (2) Discard

1 Bracket ABS0679-01 Item (3) Discard

1 Clamp ASNA0033-060 Item (4) Discard

1 Tie-Cable NSA935401-03 Item (11) Discard

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 13

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SERVICE BULLETIN

2 Support ABS0678B01 Item (6) Discard

NOTE: Item (6) is removed as 2 parts.

(b) At the bracket attachment point in the LH wing after the inboard pylon, clean the

bonding point contact surface, refer to Fig. A-GBAAA Sheet 01, View D, with:

Textile-Lint Free

Cotton

14SBA1 As required

and

Non Aqueous

Cleaner - Non

Structural Use

08BPA1 As required

(c) If necessary, rework the holes in the bracket, Item 3 in accordance with SRM

51-44-00 and refer to Fig. A-GBAAA Sheet 01 and Fig. A-GBAAA Sheet 02, View

D, View E and View F.

NOTE: If holes are reworked apply protective treatment as necessary.

(d) Install the new cable loom support bracket and fasteners, refer to Fig. A-GBAAA

Sheet 01 and Fig. A-GBAAA Sheet 02, View D, View E and View F:

1 Bracket F9249296220000 Item 3

2 Screw NAS1801-3-12 Item 5

4 Washer NAS1149D0363H Item 2

2 Nut MS21042L3 Item 1

NOTE: The bracket, Item 3, is installed inside the wing, refer to Appendix

02 - Post SB Installation Details .

(e) Apply a layer of:

Coating SealantFuel Tank

Brushable

06HAA1 As required

and

Varnish-- Electrical

Bonding Structure

04TMB2 As required

over the nut, Item 1, in accordance with ESPM 20-51-22 and refer to AMM Task

20-28-00-912-802.

(f) Install, refer to ESPM 20-33-11 and Fig. A-GBAAA Sheet 01, View D:

0.289 Grommet NSA939510CN Item 8

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 14

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SERVICE BULLETIN

(g) Install the wiring loom 7701VB, Item (7), refer to ESPM 20-33-11, ESPM 20-33-41

and Fig. A-GBAAA Sheet 01, View D, on:

1 Support ABS0678B02 Item 6

Attach the E-route cables, Item (10), to the support, Item 6, with:

1 Tie-Cable NSA935401-03 Item 11

On the new bracket, Item 3, install:

1 Clamp ASNA0032-060 Item 4

(h) Install, refer to AMM 11-00-00, Page Block 001 and Fig. A-GBAAA Sheet 01, View

D:

1 Placard F9239026810200 Item 9

(2) Subtask 924100-831-202-001 - Modify the Cable Loom Support Bracket of the Groute 7702VB RH

Work Zones and Access Panels

Zone Access/Work location

462

472

521

621

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Kit 924100D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 MS21042L3 2 NUT

2 NAS1149D0363H 4 WASHER

3 F9249296220000 1 BRACKET

4 ASNA0032-060 1 CLAMP

5 NAS1801-3-12 2 SCREW

6 ABS0678B02 1 SUPPORT

8 NSA939510CN 0.29 STRIP

9 F9239026810200 1 PLCRDSET (1)

11 NSA935401-03 1 TIE

NOTE (1): This placard set contains Service Bulletin accomplishment placards for

both LH and RH wings.

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 15

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SERVICE BULLETIN

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish-- Electrical Bonding

Structure

04TMB2 As required

Coating Sealant-Fuel Tank

Brushable

06HAA1 As required

Non Aqueous Cleaner -

Non Structural Use

08BPA1 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) 11-00-00, Page Block 001

Task 20-28-00-912-802

Elec. Std. Practices Manual (ESPM) 20-33-11

20-33-41

20-51-22

Structural Repair Manual (SRM) 51-44-00

Fig. A-GBAAA

Modification of the Cable Loom Support

Bracket, LH and RH

Sheet 01

Sheet 02

(a) At the bracket attachment point in the RH wing after the inboard pylon, remove the

support bracket from the wiring loom 7702VB, Item (7), refer to Fig. A-GBAAA

Sheet 01, View C:

2 Nut MS21042L3 Item (1) Discard

2 Screw NAS1096-3-8 Item (5) Discard

4 Washer NAS1149D0316H Item (2) Discard

1 Bracket ABS0679-01 Item (3) Discard

1 Clamp ASNA0033-060 Item (4) Discard

1 Tie-Cable NSA935401-03 Item (11) Discard

2 Support ABS0678B01 Item (6) Discard

NOTE: Item (6) is removed as 2 parts.

(b) At the bracket attachment point in the RH wing after the inboard pylon, clean the

bonding point contact surface, refer to Fig. A-GBAAA Sheet 01, View D, with:

Textile-Lint Free

Cotton

14SBA1 As required

and

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 16

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SERVICE BULLETIN

Non Aqueous

Cleaner - Non

Structural Use

08BPA1 As required

(c) If necessary, rework the holes in the bracket, Item 3 in accordance with SRM

51-44-00 and refer to Fig. A-GBAAA Sheet 01 and Fig. A-GBAAA Sheet 02, View

D and View E.

NOTE: If holes are reworked apply protective treatment as necessary.

(d) Install the new cable loom support bracket and fasteners, refer to Fig. A-GBAAA

Sheet 01 and Fig. A-GBAAA Sheet 02, View D, View E and View F:

1 Bracket F9249296220000 Item 3

2 Screw NAS1801-3-12 Item 5

4 Washer NAS1149D0363H Item 2

2 Nut MS21042L3 Item 1

NOTE: The bracket, Item 3, is installed inside the wing, refer to Appendix

02 - Post SB Installation Details .

(e) Apply a layer of:

Coating SealantFuel Tank

Brushable

06HAA1 As required

and

Varnish-- Electrical

Bonding Structure

04TMB2 As required

over the nut, Item 1, in accordance with ESPM 20-51-22 and refer to AMM Task

20-28-00-912-802.

(f) Install, refer to Refer to ESPM 20-33-11 and Fig. A-GBAAA Sheet 01, View D:

0.289 Grommet NSA939510CN Item 8

(g) Install the wiring loom 7702VB, Item (7), refer to ESPM 20-33-11, ESPM 20-33-41

and Fig. A-GBAAA Sheet 01, View D, on:

1 Support ABS0678B02 Item 6

Attach the E-route cables, Item (10), to the support, Item 6, with:

1 Tie-Cable NSA935401-03 Item 11

On the new bracket, Item 3, install:

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 17

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SERVICE BULLETIN

1 Clamp ASNA0032-060 Item 4

(h) Install, refer to AMM 11-00-00, Page Block 001 and Fig. A-GBAAA Sheet 01, View

D:

1 Placard F9239026810200 Item 9

D. TEST

None

E. CLOSE-UP

(1) Subtask 924100-942-201-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

462

472

521

621

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 57-41-37-400-801

Task 57-42-37-400-801

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

equipment.

(b) Install the access panels for the LH wing:

1 Install the fixed leading edge access panels 522AB and 522BB, refer to AMM

Task 57-41-37-400-801 and AMM Task 57-42-37-400-801.

2 Install the inboard pylon access panels 462GL and 462HR, refer to AMM

06-41-53, Page Block 001.

(c) Install the access panels for the RH wing:

1 Install the fixed leading edge access panels 622AB and 622BB, refer to AMM

Task 57-41-37-400-801 and AMM Task 57-42-37-400-801.

2 Install the inboard pylon access panels 472JR and 472HL, refer to AMM

06-41-53, Page Block 001.

(d) Put the aircraft back to its original configuration.

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 18

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SERVICE BULLETIN

**CONF ALL

E

A

LH SHOWN

RH SIMILAR

B

RIB11A

A

A

Z462 Z521

Z472 Z621 , 

(5)

(2)

(4)

(6)

(1)

(2)

(3)

C

AFTER

SB92−4100

7701VB

9

(7)

D

4

6

1

2

3

8

5

2

(11)

11

(10)

(7702VB)

C D

B

BEFORE

(7)

(10)

VIEW FROM OUTSIDE

THE WING

VIEW FROM OUTSIDE

THE WING

VIEW FROM INSIDE

THE WING

7701VB

(7702VB)

F_SB_924100_6_BAAA_01_05

Figure A-GBAAA - Sheet 01

Modification of the Cable Loom Support Bracket, LH and RH

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 19

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SERVICE BULLETIN

**CONF ALL

01 01

30 mm (1.81 in) ± 0.1 mm (0.0039 in)

FOR THE INSTALLATION OF BRACKET ITEM 3, THE HOLES CAN

NOTE:

01

BE REWORKED ECCENTRICALLY TO A MAXIMUM OF 1 mm (0.039 in)

3

TO GET AN INCREASED HOLE PITCH OF 31 mm (1.220 in).

02 HOLES OF THE BRACKET ENLARGED TO A MAXIMUM OF 1 mm (0.039 in).

03 INITIAL HOLES OF THE BRACKET BEFORE REWORK.

04 HOLES ON THE WING SUPPORT.

02 04

30 mm (1.181 in) DISTANCE BETWEEN 

THE HOLES ON THE BRACKET

UP TO 31.4 mm (1.236 in) − 31.7 mm (1.248 in) DISTANCE

BETWEEN THE HOLES ON THE WING SUPPORT

F

E

02

F

03

03

04

F_SB_924100_6_BAAA_02_03

Figure A-GBAAA - Sheet 02

Modification of the Cable Loom Support Bracket, LH and RH

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 20

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SERVICE BULLETIN

Appendix 01 - Elapsed Time Assumption

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A340−92−4100

01

02

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

01

02

NOTE:

:

: IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

TOTAL MANHOURS

SB ELAPSED TIME

8.00

4.00

0 12 3

JOB SET−UP

STEPS MH ET/S

2.00 1.00

MODIFY THE LH CABLE LOOM 2.00 2.00

2.00 2.00

PER

2

1

1

CLOSE−UP 2.00 1.00 2

SB ELAPSED TIME

(HOURS)

4

SUPPORT BRACKET OF THE

G ROUTE 7701VB LH

MODIFY THE RH CABLE LOOM

SUPPORT BRACKET OF THE

G ROUTE 7702VB RH

F_SB_924100_6_AAAA_01_04

Figure A-GAAAA - Sheet 01

Gantt Chart

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 1

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SERVICE BULLETIN

Appendix 01 - Elapsed Time Assumption

This Page Intentionally Left Blank

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 2

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SERVICE BULLETIN

Appendix 02 - Post SB Installation Details

**CONF ALL

(1) The following photographs illustrate the correct installation.

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 1

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SERVICE BULLETIN

Appendix 02 - Post SB Installation Details

**CONF ALL

FRONT VIEW (OUTSIDE)

FRONT VIEW (OUTSIDE)

F_SB_924100_6_ABAA_01_00

Figure A-GABAA - Sheet 01

Post SB Installation Details

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 2

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SERVICE BULLETIN

Appendix 02 - Post SB Installation Details

**CONF ALL

VIEW FOR THE POSITION OF THE CLAMP, ITEM 4

VIEW IN THE WING (INSIDE)

GROMMET,

ITEM 8

BRACKET,

ITEM 3

F_SB_924100_6_ABAA_02_00

Figure A-GABAA - Sheet 02

Post SB Installation Details

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 3

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SERVICE BULLETIN

REPORTING SHEET

TITLE: ELECTRIC AND ELECTRONIC COMMON INSTALLATION-CABLE LOOM

INSTALLATION DRAWINGS-IMPROVEMENT OF FEEDER ROUTING

ATTACHMENT IN WING/PYLON

MODIFICATION No.: 203672D50692

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: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 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 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

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

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

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

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Jun 19/14 SERVICE BULLETIN No.: A340-92-4100

REVISION No.: 01 - May 21/15 Page: 1

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