@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: 21

TITLE: AIR CONDITIONING - GENERAL - INSTALL NEW BONDING BRACKETS

AFTER FRAME64 LH BETWEEN P33-P34

MODIFICATION No.: 201500D50418

This page transmits Revision No.03 of Service Bulletin No.A340-21-4152

ADDITIONAL WORK

**CONF ALL

Additional work is required for aircraft which have been modified by revision 00 or revision 01.

Additional work is not required for aircraft which have been modified by revision 02.

REASON

Revision No. 03 issued to update the reason, accomplishment instruction and illustration.

CHANGES

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

Fig. A-GSAAA

Fig. A-GSAAA Sheet 01 SHEET UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED R

REASON

Objective/Action OBJECTIVE/ACTION UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 214152- 831-848-001-Modification

Subtask 214152-831-201-001 SUBTASK SOLUTION UPDATED R

Fig. A-GBAAA

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Fig. A-GBAAA Sheet 01 SHEET UPDATED R

Fig. A-GBBAA

Fig. A-GBBAA Sheet 01 SHEET UPDATED R

Fig. A-GBCAA

Fig. A-GBCAA Sheet 01 SHEET 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 update the effectivity, the Industry support paragraph, add that damaged

insulations must be repaired and update the Kit revision indicator.

Revision No. 02 issued to add the replacement of the bonding lead from waste water pipe to the new

bonding bracket and to improve the position of the bonding clamp at waste water pipe.

REVISION SEQUENCE

ORIGINAL: Sep 27/11

REVISION No. : 01 - Nov 21/11

REVISION No. : 02 - Mar 29/12

REVISION No. : 03 - Dec 07/12

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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: 21

TITLE: AIR CONDITIONING - GENERAL - INSTALL NEW BONDING BRACKETS

AFTER FRAME64 LH BETWEEN P33-P34

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 201500D50418

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

Maintenance experience has shown that the bonding lead from the isolation valve 283HN to Frame

(FR)64, between Stringer (STGR)33 and STGR34, is too close to the electrical harness 5871VB and

chafing might be possible.

The chafing might lead to a non-closure of the isolation valve 283HN through a short circuit of the

isolation valve by contact of the chafed bonding lead and wire harness 5871VB.

This Service Bulletin details the installation of a new bonding bracket and new bonding lead at

STGR34, between FR64 and FR65.

The accomplishment of this Service Bulletin will avoid possible chafing between the bonding lead and

the electrical harness 5871VB and ensure the correct control of the isolation valve 283HN.

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

COST SAVING NO LROPS AFFECTED NO

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SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

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 214152D01R03 1 33.00 Bracket, Rivet, Screw, Washer

Kit 214152D02R01 1 33.00

TOTAL 66.00

EFFECTIVITY

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

47W 56W 83V AAW ABQ AFR AIB ALK ARG CAH CAL CCA CES

CPA DGA DLH FIN GAF GFA HFY IBE IRC KAC KNE LAN M3R

MAU MDG MSR NMB PAL QAF RJA S3R SAA SAS SFB SLM SVW

SWR TAP THT THY UAE VCV VIR XAX

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 214152-831-848-001: Modification

TOTAL MANHOURS 3.25

ELAPSED TIME (HOURS) 3.25

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SERVICE BULLETIN

SUMMARY

Task 214152-831-849-001: Modification - ADDITIONAL WORK

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

APPENDICES

None

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SERVICE BULLETIN

SUMMARY

**CONF ALL

B

A

283HN

FR73

FR62

STGR34

FR64

FR63

FR62

STGR33

STGR32

B

283HN

A

Z160

NEW BONDING

BRACKET

F_SB_214152_6_SAAA_01_02

Figure A-GSAAA - Sheet 01

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

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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: 21

TITLE: AIR CONDITIONING - GENERAL - INSTALL NEW BONDING BRACKETS

AFTER FRAME64 LH BETWEEN P33-P34

MODIFICATION No.: 201500D50418

This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the

property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with

any information contained in it. It is delivered on the express condition that said document and the

information contained in it shall be treated as confidential, shall not be used for any purpose other than

that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall

not be duplicated in any manner (except for the purposes of performing the tasks described hereunder

and provided that any recipient of such document shall comply with the conditions herein), without

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

(1) Models

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

(2) Effectivity by MSN

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

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

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

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

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

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

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

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

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

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

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

0538 0541 0545-0546 0554 0556 0559 0561-0562 0585 0598 0668 0793 0800 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

47W 0009

56W 0003 0011 0013 0015 0018 0019 0021

83V 0235 0239 0280 0292

AAW 0151

ABQ 0216 0257

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

0399

AIB 0332

ALK 0032 0033 0034 0367 0374 0381

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

CAH 0020 0056

CAL 0402 0406 0411 0415 0433 0541

CCA 0192 0199 0201 0242 0243 0264

CES 0129 0131 0141 0161 0182

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

DGA 0075 0081

DLH 0024 0027 0028 0035 0052 0053 0135 0158 0213 0233 0252 0297

0304 0321 0325 0327 0335 0347 0352 0354 0379 0390 0434 0447

FIN 0058 0168 0174

GAF 0274 0355

GFA 0212 0215 0282 0554

HFY 0117 0133

IBE 0005 0088 0125 0134 0145 0146 0170 0193 0217 0221 0318 0329

0387 0414 0459 0474 0483

IRC 0002

KAC 0089 0090 0101 0104

KNE 0004

LAN 0167 0359 0363 0429 0442

M3R 0061

MAU 0076 0152 0194 0268 0793 0800

MDG 0210 0319

MSR 0156 0159 0178

NMB 0047 0051

PAL 0173 0176 0187 0196

QAF 0026 0528

RJA 0014 0022 0038 0043

S3R 0204

SAA 0006 0197 0378

SAS 0413 0424 0430 0435 0450 0467 0470

SFB 0046

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SERVICE BULLETIN

OPERATOR MSN

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 0139 0149 0163 0166 0185 0190 0202 0236

VCV 0031 0302

VIR 0114 0164 0214 0225

XAX 0273 0278

(4) Configuration by MSN

MSN CONFIGURATION

0002 0003 0004 0005 0006 0009 0011 0013 0014 0015 0018

0019 0020 0021 0022 0023 0024 0025 0026 0027 0028 0029

0031 0032 0033 0034 0035 0038 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 0101 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 0545 0546 0554 0556 0559 0561 0562

0585 0598 0668 0793 0800 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.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Consumable CMLD01 1

Kit 214152D01R03 1

Kit 214152D02R01 1

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SERVICE BULLETIN

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Maintenance experience has shown that the bonding lead from the isolation valve

283HN to Frame (FR)64, between Stringer (STGR)33 and STGR34, is too close to the

electrical harness 5871VB and chafing might be possible.

The chafing might lead to a non-closure of the isolation valve 283HN through a short

circuit of the isolation valve by contact of the chafed bonding lead and wire harness

5871VB.

(2) Objective/Action

This Service Bulletin details the installation of a new bonding bracket and new bonding

lead at STGR34, between FR64 and FR65.

(3) Advantages

The accomplishment of this Service Bulletin will avoid possible chafing between the

bonding lead and the electrical harness 5871VB and ensure the correct control of the

isolation valve 283HN.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 214152-831-848-001: Modification

(1) Modify the bonding lead installation

Task 214152-831-849-001: Modification - ADDITIONAL WORK

(1) Modify the bonding lead installation

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

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SERVICE BULLETIN

(2) Accomplishment Timescale

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. The accomplishment timescale, which has not yet been

defined, will be given in the AD.

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 214152-831-848-001: Modification

Get Access 1.00

On Aircraft

Modify the bonding lead installation 1.00

Tests 0.25

Close-Up 1.00

TOTAL MANHOURS 3.25

ELAPSED TIME (HOURS) 3.25

Task 214152-831-849-001: Modification - ADDITIONAL WORK

Get Access 1.00

On Aircraft

Modify the bonding lead installation 0.25

Tests 0.25

Close-Up 1.00

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

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SERVICE BULLETIN

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-30-00 06-31-53

06-41-53 12-34-24 20-28-00

25-53-00 25-80-00 52-30-00

Elec. Std. Practices Manual (ESPM) 20-51-20 20-51-21 20-55-00

Standards Manual (SM)

Structural Repair Manual (SRM) 51-42-11 51-44-00 51-44-11

K. PUBLICATION AFFECTED

Illustrated Parts Catalog (IPC) 21-28-04

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 214152D01R03

Kit 214152D02R01

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:

Airbus Material, Logistic and Suppliers

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet:

http//spares.airbus.com

For ordering modification kits by fax: +49 40

50 76 25 90

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

(2) Price and Availability

Kit 214152D01R03

Cost 33.00 USD

Availability 90 calendar days from receipt of order

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

order. If you require Kits before this time, please include a retrofit planning schedule with

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

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

at the issue date of the Service Bulletin.

Kit 214152D02R01

Cost 33.00 USD

Availability 90 calendar days from receipt of order

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

order. If you require Kits before this time, please include a retrofit planning schedule with

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

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

at the issue date of the Service Bulletin.

B. INDUSTRY SUPPORT INFORMATION

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

no charge for orders placed before 31. Dec. 2014.

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SERVICE BULLETIN

For the accomplishment of this Service Bulletin before 31. Dec. 2014, 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 214152D01R03

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

NOTES

6 EN6081D4-04 2 RIVET

7 ABS1577A05 1 BRACKET

8 EN6081D4-05 3 RIVET

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

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

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

to part number relationship.

Kit 214152D02R01

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

NOTES

1 NAS1801-3-7 2 SCREW

2 MS21042-3 1 NUT

3 NAS1149C0332R 2 WASHER

9 E0090-10-200NN 1 LEAD (10) E0091-10-160NN

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

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

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

to part number relationship.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Cleaning Solvent 11-016 As required

Lint-Free Cotton Cloth 19-003 As required

(2) Components

None

(3) Equipment

None

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SERVICE BULLETIN

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

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SERVICE BULLETIN

This Page Intentionally Left Blank

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 214152-831-848-001 - 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.

IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00.

Task Associated Data

Zone

160

Manpower

TOTAL MANHOURS 3.25

ELAPSED TIME (HOURS) 3.25

A. GENERAL

(1) Subtask 214152-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-30-00, Page Block 001

06-31-53, Page Block 001

06-41-53, Page Block 001

Structural Repair Manual (SRM) 51-44-00

(a) For identification of zones (Refer to AMM 06-20-00, Page Block 001).

(b) For Stringer (STGR) identification (Refer to AMM 06-30-00, Page Block 001).

(c) For Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

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SERVICE BULLETIN

(d) For sidewall panel identification (Refer to AMM 06-41-53, Page Block 001).

(e) For fastener hole diameter and drill and deburr data (Refer to SRM 51-44-00).

(2) Subtask 214152-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Bulletin.

B. PREPARATION

(1) Subtask 214152-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 25-53-00-000-801

Task 25-80-00-000-801

Task 52-30-00-010-801

Fig. A-GBAAA

Modify the bonding lead installation

Sheet 01

Sheet 02

Fig. A-GBBAA

Modify the bonding lead installation

Sheet 01

Sheet 02

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

12-34-24-860-802).

(b) Put an access platform in position at the Aft cargo-compartment door.

(c) Open the Aft cargo-compartment door (Refer to AMM Task 52-30-00-010-801).

(d) If a Cargo Loading System (CLS) is installed, put a warning notice in position on

the control panel to tell persons not to operate the CLS.

(e) Remove the access panel 151TW (Refer to AMM Task 25-53-00-000-801).

(f) In the work area, Zone 160, as shown onFig. A-GBAAA Sheet 01 and

Fig. A-GBBAA Sheet 01, remove the insulation blankets (Refer to AMM Task

25-80-00-000-801).

C. PROCEDURE

(1) Subtask 214152-831-201-001 - Modify the bonding lead installation

Work Zones and Access Panels

Zone Access/Work location

160

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

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SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 214152D01R03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

6 EN6081D4-04 2 RIVET

7 ABS1577A05 1 BRACKET

8 EN6081D4-05 3 RIVET

Kit 214152D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NAS1801-3-7 2 SCREW

2 MS21042-3 1 NUT

3 NAS1149C0332R 2 WASHER

9 E0090-10-200NN 1 LEAD

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Cleaning Solvent 11-016 As required

Lint-Free Cotton Cloth 19-003 As required

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-801

25-80-00, Page Block 801

Elec. Std. Practices Manual (ESPM) 20-51-20

20-51-21

Structural Repair Manual (SRM) 51-42-11

51-44-11

Fig. A-GBAAA

Modify the bonding lead installation

Sheet 01

Sheet 02

Fig. A-GBBAA

Modify the bonding lead installation

Sheet 01

Sheet 02

(a) As shown on Fig. A-GBAAA Sheet 01 and Fig. A-GBAAA Sheet 02, View C,

remove:

1 Nut Item (2) Discard

1 Washer Item (3) Discard

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

REVISION No.: 03 - Dec 07/12 Page: 13

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SERVICE BULLETIN

1 Screw Item (1) Discard

and disconnect:

1 Bonding Lead Item (4) Retain

1 Bonding Lead E0091-10-160NN Item (10) Discard

(b) As shown on Fig. A-GBAAA Sheet 01 and Fig. A-GBAAA Sheet 02, View E,

remove:

1 Nut Item (2) Discard

1 Washer Item (3) Discard

1 Screw Item (1) Discard

1 Bonding Lead E0091-10-160NN Item (10) Discard

(c) As shown on Fig. A-GBAAA Sheet 02, View C, at FR64, remove:

2 Rivet Item (6) Discard

1 Bracket Item (5) Discard

(d) As shown on Fig. A-GBAAA Sheet 02, View D, close the holes with:

2 Rivet EN6081D4-04 Item 6

(Refer to SRM 51-42-11).

(e) Install the new bracket at STGR34, between FR64 and FR65 LH, as shown on Fig.

A-GBBAA Sheet 01 and Fig. A-GBBAA Sheet 02, View E.

1 At STGR34 make marks to show the position of the holes.

2 Drill the pilot hole at STGR34 with a diameter of 2.4mm (0.094inch) (Refer to

SRM 51-44-11).

3 Temporarily install:

1 Bracket ABS1577A05 Item 7

NOTE: Use the new hole at STGR34.

4 Transfer drill the holes from the bracket, item 7, to STGR34 with a diameter of

3.3mm (0.13inch) (Refer to SRM 51-44-11).

5 Remove the bracket and deburr the holes at STGR34 and the bracket, item 7

(Refer to SRM 51-44-11).

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

REVISION No.: 03 - Dec 07/12 Page: 14

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SERVICE BULLETIN

6 Clean the contact surface of the STGR34 LH and the bracket, item 7, with:

Lint-Free Cotton

Cloth

19-003 As required

and

Cleaning Solvent 11-016 As required

7 Install:

1 Bracket ABS1577A05 Item 7

3 Rivet EN6081D4-05 Item 8

(Refer to SRM 51-42-11).

NOTE: Do the electrical bonding of the rivets (Refer to ESPM

20-51-20) and (Refer to AMM Task 20-28-00-912-801).

(f) Make a cutout in the insulation blanket in position of the new bracket, item 7, for

the installation of the insulation blanket (Refer to AMM 25-80-00, Page Block 801).

NOTE: Damaged insulations must be repaired

(g) Cut the waste water pipe insulation and move it in the old position.

(h) Install the bonding clamp on the new position as shown on Fig. A-GBBAA Sheet

02, View D.

(i) On the waste water pipe, as shown Fig. A-GBBAA Sheet 02, View D, install:

1 Bonding Lead E0090-10-200NN Item 9

with:

1 Screw NAS1801-3-7 Item 1

1 Washer NAS1149C0332R Item 3

1 Nut MS21042-3 Item 2

(j) As shown on Fig. A-GBBAA Sheet 02, View C, connect:

1 Lead Bonding Item (4) Retained at

removal

and:

1 Bonding Lead E0090-10-200NN Item 9

with:

1 Screw NAS1801-3-7 Item 1

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

REVISION No.: 03 - Dec 07/12 Page: 15

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SERVICE BULLETIN

1 Washer NAS1149C0332R Item 3

(k) Do the electrical bonding (Refer to ESPM 20-51-21).

D. TEST

(1) Subtask 214152-760-201-001 - Test of electrical bonding

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-720-805

(a) Check the electrical bonding of the bonding lead and the new bracket (Refer to

AMM Task 20-28-00-720-805).

E. CLOSE-UP

(1) Subtask 214152-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 25-53-00-400-801

Task 25-80-00-400-801

Task 52-30-00-410-801

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

equipment.

(b) In the work area, install the insulation blankets (Refer to AMM Task

25-80-00-400-801).

(c) Install the access panel 151TW (Refer to AMM Task 25-53-00-400-801).

(d) If installed, remove the warning notice from the CLS.

(e) Close the Aft cargo-compartment door (Refer to AMM Task 52-30-00-410-801).

(f) Remove the access platform(s).

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

REVISION No.: 03 - Dec 07/12 Page: 16

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SERVICE BULLETIN

Task 214152-831-849-001 - Modification - ADDITIONAL WORK

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.

IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00.

Task Associated Data

Zone

160

Manpower

TOTAL MANHOURS 2.50

ELAPSED TIME (HOURS) 2.50

A. GENERAL

(1) Subtask 214152-910-202-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-30-00, Page Block 001

06-31-53, Page Block 001

06-41-53, Page Block 001

(a) For identification of zones (Refer to AMM 06-20-00, Page Block 001).

(b) For Stringer (STGR) identification (Refer to AMM 06-30-00, Page Block 001).

(c) For Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

(d) For sidewall panel identification (Refer to AMM 06-41-53, Page Block 001).

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

REVISION No.: 03 - Dec 07/12 Page: 17

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SERVICE BULLETIN

(2) Subtask 214152-839-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Bulletin.

B. PREPARATION

(1) Subtask 214152-941-202-001 - Job Set-up

Manpower Resources

Skills ELECTRICAL

References

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

Task 25-53-00-000-801

Task 52-30-00-010-801

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

12-34-24-860-802).

(b) Put an access platform in position at the Aft cargo-compartment door.

(c) Open the Aft cargo-compartment door (Refer to AMM Task 52-30-00-010-801).

(d) If a Cargo Loading System (CLS) is installed, put a warning notice in position on

the control panel to tell persons not to operate the CLS.

(e) Remove the access panel 151TW (Refer to AMM Task 25-53-00-000-801).

C. PROCEDURE

(1) Subtask 214152-831-202-001 - Modify the bonding lead installation

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills ELECTRICAL

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

REVISION No.: 03 - Dec 07/12 Page: 18

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SERVICE BULLETIN

Material necessary to do the job

Kit 214152D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NAS1801-3-7 2 SCREW

2 MS21042-3 1 NUT

3 NAS1149C0332R 2 WASHER

9 E0090-10-200NN 1 LEAD

References

Elec. Std. Practices Manual (ESPM) 20-51-21

Fig. A-GBCAA

Modify the bonding lead installation -

ADDITIONAL WORK

Sheet 01

Sheet 02

(a) As shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBCAA Sheet 02, View C

remove:

1 Washer Item (3) Discard

1 Screw Item (1) Discard

and disconnect:

1 Bonding Lead Item (4) Retain

1 Bonding Lead E0091-10-160NN Item (10) Discard

(b) As shown on Fig. A-GBCAA Sheet 01 and Fig. A-GBCAA Sheet 02, View D,

remove:

1 Nut Item (2) Discard

1 Washer Item (3) Discard

1 Screw Item (1) Discard

1 Bonding Lead E0091-10-160NN Item (10) Discard

(c) Cut the waste water pipe insolation and move it to the old position.

(d) Install the bonding clamp on the new position, as shown on Fig. A-GBCAA Sheet

02, View D.

(e) On the waste water pipe, as shown on Fig. A-GBCAA Sheet 02, View D, install:

1 Bonding Lead E0090-10-200NN Item 9

with:

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

REVISION No.: 03 - Dec 07/12 Page: 19

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SERVICE BULLETIN

1 Screw NAS1801-3-7 Item 1

1 Washer NAS1149C0332R Item 3

1 Nut MS21042-3 Item 2

(f) As shown on Fig. A-GBCAA Sheet 02, View C, connect:

1 Bonding Lead Item (4) Retained at

removal

1 Bonding Lead E0090-10-200NN Item 9

with:

1 Screw NAS1801-3-7 Item 1

1 Washer NAS1149C0332R Item 3

(g) Do the electrical bonding (Refer to ESPM 20-51-21).

D. TEST

(1) Subtask 214152-760-202-001 - Electrical

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-720-805

(a) Check the electrical bonding of the bonding lead (Refer to AMM Task

20-28-00-720-805).

E. CLOSE-UP

(1) Subtask 214152-942-202-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Skills CABIN

References

Aircraft Maintenance Manual (AMM) Task 25-53-00-400-801

Task 52-30-00-410-801

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

REVISION No.: 03 - Dec 07/12 Page: 20

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SERVICE BULLETIN

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

equipment.

(b) Install the access panel 151TW (Refer to AMM Task 25-53-00-400-801).

(c) If installed, remove the warning notice from the CLS.

(d) Close the Aft cargo-compartment door (Refer to AMM Task 52-30-00-410-801).

(e) Remove the access platform(s).

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

REVISION No.: 03 - Dec 07/12 Page: 21

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@A340

SERVICE BULLETIN

**CONF ALL

B

A

283HN

FR73

FR62

STGR34

FR64

FR63

FR62

STGR33

STGR32

B

283HN

A

Z160

E

C D

F_SB_214152_6_BAAA_01_02

Figure A-GBAAA - Sheet 01

Modify the bonding lead installation

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

REVISION No.: 03 - Dec 07/12 Page: 22

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@A340

SERVICE BULLETIN

**CONF ALL

FR64

(1)

(2) (5)

(4)

(6)

BEFORE AFTER

(3)

C

FR64

6

D

(10)

(1)

(10)

(3)

(2)

E

(8)

F_SB_214152_6_BAAA_02_02

Figure A-GBAAA - Sheet 02

Modify the bonding lead installation

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

REVISION No.: 03 - Dec 07/12 Page: 23

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@A340

SERVICE BULLETIN

**CONF ALL

B

A

283HN

FR73

FR62

STGR34

FR64

FR63

FR62

STGR33

STGR32

B

283HN

C

A

Z160

D

F_SB_214152_6_BBAA_01_02

Figure A-GBBAA - Sheet 01

Modify the bonding lead installation

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

REVISION No.: 03 - Dec 07/12 Page: 24

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@A340

SERVICE BULLETIN

**CONF ALL

1

3

7

8

9

98.2 mm

(3.87 in)

(115.0 mm)

(4.53 in)

14.0 mm

(0.55 in)

FWD FR64

STGR34

STGR34

7

(4)

1

9

3

2

ca. 72.0 mm

(2.83 in)

(8)

OLD CLAMP 

POSITION

C D

E

E

F_SB_214152_6_BBAA_02_02

Figure A-GBBAA - Sheet 02

Modify the bonding lead installation

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

REVISION No.: 03 - Dec 07/12 Page: 25

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@A340

SERVICE BULLETIN

**CONF ALL

B

A

283HN

FR73

FR62

STGR34

FR64

FR63

FR62

STGR33

STGR32

B

283HN

C

D

A

Z160

F_SB_214152_6_BCAA_01_01

Figure A-GBCAA - Sheet 01

Modify the bonding lead installation - ADDITIONAL WORK

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

REVISION No.: 03 - Dec 07/12 Page: 26

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@A340

SERVICE BULLETIN

**CONF ALL

STGR34

1

3

(10)

(4)

1

(10)

3

2

ca. 72.0 mm

(2.83 in)

(8)

OLD CLAMP 

POSITION

C

D

(1)

(3)

9

9

(1)

(3)

(2)

F_SB_214152_6_BCAA_02_01

Figure A-GBCAA - Sheet 02

Modify the bonding lead installation - ADDITIONAL WORK

DATE: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

REVISION No.: 03 - Dec 07/12 Page: 27

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SERVICE BULLETIN

REPORTING SHEET

TITLE: AIR CONDITIONING - GENERAL - INSTALL NEW BONDING BRACKETS

AFTER FRAME64 LH BETWEEN P33-P34

MODIFICATION No.: 201500D50418

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 27/11 SERVICE BULLETIN No.: A340-21-4152

REVISION No.: 03 - Dec 07/12 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: Sep 27/11 SERVICE BULLETIN No.: A340-21-4152

REVISION No.: 03 - Dec 07/12 Page: 1

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