@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: 52

TITLE: DOORS-SERVICE DOORS-MODIFICATION OF LATCHING MECHANISM

OF POTABLE WATER SERVICE PANEL

MODIFICATION No.: 201938D50416 201938D50379 201939D59871 203344D50725 203563D50740

This page transmits Revision No.01 of Service Bulletin No.A340-52-4094

ADDITIONAL WORK

**CONF ALL

Additional work is required by this revision for aircraft modified by any previous issue of this Service

Bulletin to correct the adjusting stud installation and the sealant application.

REASON

Revision No. 01 issued to introduce a new Door Assy equipped with a new adjusting stud and new LISI

latches, to introduce additional work for the adjusting stud and to introduce minor changes.

CHANGES

FRONT MATTER

MODIFICATIONS MODIFICATION NUMBER(S) UPDATED R

SUMMARY

MODIFICATIONS MODIFICATION CLASSIFICATION UPDATED R

MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

EFFECTIVITY OPERATOR LIST UPDATED R

REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE

UPDATED

R

MANPOWER MANPOWER UPDATED R

MANPOWER UPDATED R

APPENDICES APPENDICES UPDATED R

Fig. A-GSAAA

Fig. A-GSAAA Sheet 01 SHEET UPDATED R

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 1

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@A340

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

MATERIAL EFFECTIVITY UPDATED

MATERIAL SET UPDATED

MATERIAL SET QUANTITY UPDATED

R

COMPLIANCE

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED R

MANPOWER MANPOWER UPDATED R

MANPOWER UPDATED

CONFIGURATION UPDATED

R

MANPOWER UPDATED

CONFIGURATION UPDATED

R

WEIGHT AND BALANCE WEIGHT AND BALANCE UPDATED R

REFERENCES REFERENCED DOCUMENTATION UPDATED R

REFERENCED DOCUMENTATION UPDATED R

PUBLICATION AFFECTED PUBLICATIONS AFFECTED UPDATED R

INTERCHANGEABILITY/MIXABILITY INTERCHANGEABILITY/MIXABILITY UPDATED R

INTERCHANGEABILITY/MIXABILITY 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 AVAILABILITY UPDATED

MATERIAL PRICE UPDATED

MATERIAL SET UPDATED

R

INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED R

LIST OF COMPONENTS

Kit 524094D01R01 PART MATERIAL SET UPDATED

MATERIAL SET LABEL UPDATED

PART NUMBER UPDATED

R

Kit 524094D02R01 PART MATERIAL SET UPDATED

MATERIAL SET LABEL UPDATED

PART NUMBER UPDATED

R

LIST OF MATERIALS - OPERATOR

SUPPLIED

Consumable Materials

Consumable CMLD10 CONSUMABLE MATERIAL SET UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

R

Components COMPONENTS UPDATED R

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 2

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@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Component COMPD03 PART MATERIAL SET ADDED N

PARTS TO BE RE-IDENTIFIED BY

OPERATOR

PARTS TO BE RE-IDENTIFIED BY OPERATOR

UPDATED

R

Reidentified part set REIDD07 PART MATERIAL SET ADDED N

Reidentified part set REIDD08 PART MATERIAL SET ADDED N

ACCOMPLISHMENT INSTRUCTIONS

TASK 524094- 831-848-001-Modification TASK SOLUTION UPDATED

NOTE UPDATED

R

Task associated data - 001 MAN HOURS UPDATED

ELAPSED TIME UPDATED

R

Task associated data - 002 MAN HOURS UPDATED

ELAPSED TIME UPDATED

R

Subtask 524094-910-201-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 524094-910-201-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 524094-941-201-001 SUBTASK SOLUTION UPDATED R

Subtask 524094-941-201-001 SUBTASK SOLUTION UPDATED R

Subtask 524094-831-201-001 SUBTASK SOLUTION ADDED N

Subtask 524094-420-201-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 524094-420-206-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 524094-420-202-001 SUBTASK SOLUTION UPDATED

PART NUMBER UPDATED

FIGURE REFERENCE UPDATED

MATERIAL LIST UPDATED

R

Subtask 524094-420-203-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

REFERENCED DOCUMENTATION UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 524094-420-204-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 3

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@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 524094-820-201-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

FIGURE REFERENCE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

MATERIAL LIST UPDATED

R

Subtask 524094-916-201-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 524094-420-205-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 524094-831-201-002 SUBTASK SOLUTION ADDED N

Subtask 524094-420-201-002 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 524094-420-206-002 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 524094-420-202-002 SUBTASK SOLUTION UPDATED

PART NUMBER UPDATED

FIGURE REFERENCE UPDATED

MATERIAL LIST UPDATED

R

Subtask 524094-420-203-002 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

REFERENCED DOCUMENTATION UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 524094-420-204-002 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 524094-820-201-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

FIGURE REFERENCE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

MATERIAL LIST UPDATED

R

Subtask 524094-916-201-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 4

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@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 524094-420-205-002 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 524094-700-201-001 SUBTASK SOLUTION UPDATED R

Subtask 524094-700-201-001 SUBTASK SOLUTION UPDATED R

Subtask 524094-942-201-001 SUBTASK SOLUTION UPDATED R

Subtask 524094-942-201-001 SUBTASK SOLUTION UPDATED R

TASK 524094- 831-849-001-Modification -

ADDITIONAL WORK for aircraft modified

by the original issue

TASK SOLUTION ADDED N

Task associated data - 001 TASK ASSOCIATED DATA ADDED N

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Subtask 524094-910-202-001 SUBTASK SOLUTION ADDED N

Subtask 524094-839-202-001 SUBTASK SOLUTION ADDED N

Subtask 524094-910-202-001 SUBTASK SOLUTION ADDED N

Subtask 524094-839-202-001 SUBTASK SOLUTION ADDED N

Subtask 524094-941-202-001 SUBTASK SOLUTION ADDED N

Subtask 524094-941-202-001 SUBTASK SOLUTION ADDED N

Subtask 524094-831-202-001 SUBTASK SOLUTION ADDED N

Subtask 524094-831-203-001 SUBTASK SOLUTION ADDED N

Subtask 524094-831-202-002 SUBTASK SOLUTION ADDED N

Subtask 524094-831-203-001 SUBTASK SOLUTION ADDED N

Subtask 524094-700-202-001 SUBTASK SOLUTION ADDED N

Subtask 524094-700-202-001 SUBTASK SOLUTION ADDED N

Subtask 524094-942-202-001 SUBTASK SOLUTION ADDED N

Subtask 524094-942-202-001 SUBTASK SOLUTION ADDED N

Fig. A-GBAAA

Fig. A-GBAAA Sheet 02 SHEET UPDATED R

Fig. A-GBBAA

Fig. A-GBBAA Sheet 02 SHEET UPDATED R

Fig. A-GBBAA Sheet 03 SHEET UPDATED R

Fig. A-GBBAA Sheet 04 SHEET UPDATED R

Fig. A-GBBAA Sheet 05 SHEET UPDATED R

Fig. A-GBCAA FIGURE SOLUTION UPDATED R

Fig. A-GBCAA Sheet 02 SHEET UPDATED R

Fig. A-GBCAA Sheet 03 SHEET UPDATED R

Fig. A-GBCAA Sheet 04 SHEET ADDED N

Fig. A-GBDAA FIGURE SOLUTION ADDED N

Fig. A-GBDAA Sheet 01 SHEET ADDED N

Fig. A-GBDAA Sheet 02 SHEET ADDED N

Fig. A-GBDAA Sheet 03 SHEET ADDED N

Fig. A-GBEAA FIGURE SOLUTION ADDED N

Fig. A-GBEAA Sheet 01 SHEET ADDED N

Fig. A-GBEAA Sheet 02 SHEET ADDED N

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 5

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@A340

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Fig. A-GBEAA Sheet 03 SHEET ADDED N

Appendix 01 - Elapsed Time Assumption

Fig. A-GGAAA

Fig. A-GGAAA Sheet 01 SHEET UPDATED R

Appendix 02 - Status of the aircraft after accomplishment of the Service Bulletin A340-52-4094

APPENDIX CONTENT APPENDIX CONTENT 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

No previous revision

REVISION SEQUENCE

ORIGINAL: Apr 27/12

REVISION No. : 01 - Apr 25/14

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 6

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: 52

TITLE: DOORS-SERVICE DOORS-MODIFICATION OF LATCHING MECHANISM

OF POTABLE WATER SERVICE PANEL

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 201938D50416 201938D50379 201939D59871 203344D50725 203563D50740

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 cases have been reported in which the potable water service panel access door 164AR has

been lost during flight. In one case, on an A340 aircraft the THS leading edge has been hit, in a second

case, on an A330 aircraft the door was presumed to have caused damage to the THS.

Investigations have shown difficulties with the latching mechanism of the potable water service panel

access door, which can lead to a potential unsafe condition. The potential unsafe condition could cause

possible injury to persons and damage to property on ground and potential loss of the potable water

service panel access door on runway.

The Inspection Service Bulletin A340-52-4088 was issued to inspect the access door 164AR, 154AR

and 171AL. The Modification Service Bulletin A340-52-4087 was issued as the final repair solution to

the Inspection Service Bulletin A340-52-4088. Further occurrences of access door 164AR lost during

flight have shown that the Modification Service Bulletin A340-52-4087 is not the definitive final repair

solution for this access door. Therefore, this mandatory Modification Service Bulletin, A340-52-4094, is

issued as the final repair solution for the access door 164AR. The loss of this door is classified to be a

potential unsafe condition.

To avoid further occurrences the design of the latching mechanism of the potable water service panel

access door has to be modified to mitigate the risk.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 1

6

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@A340

SERVICE BULLETIN

SUMMARY

This Service Bulletin mandates the operator to install a modified potable water service panel access

door with reinforced hinge screws and more robust latches, including an additional third latch.

After accomplishment of this Service Bulletin the handling and reliability of the potable water service

panel access door is improved.

This Service Bulletin meets the safety intent by making sure that the potable water service panel

access door can be correctly latched.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO LROPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 524094D01R01 1 15,280.00 Door, attachment parts

Component COMPD03 See SB Stud-adjusting

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 524094D02R01 1 15,280.00 Door, attachment parts

Component COMPD03 See SB Stud-adjusting

EFFECTIVITY

**CONF ALL

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

06Y 15R 15T 31V 36V 38W 58X 98X ABD AFR AIB ALK ARG

CAL CCA CPA DGA DLH FIN G8E GAF GFA HFY I2L IBE IRC

IRM KAC LAN M3R MAU MDG MSR NMB OAL PAL QAF RJA S3R

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

CONCURRENT REQUIREMENTS

None

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 2

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@A340

SERVICE BULLETIN

SUMMARY

REFERENCES / REPERCUSSIONS

TFU 52.42.00.015

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER SBIT 13-0016

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 524094-831-848-001: Modification

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

Task 524094-831-849-001: Modification - ADDITIONAL WORK for aircraft modified by the

original issue

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

**CONF 002

Task 524094-831-848-001: Modification

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

Task 524094-831-849-001: Modification - ADDITIONAL WORK for aircraft modified by the

original issue

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

APPENDICES

**CONF ALL

Appendix 01 - Elapsed Time Assumption

Appendix 02 - Status of the aircraft after accomplishment of the Service Bulletin A340-52-4094

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 3

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

SERVICE BULLETIN

SUMMARY

**CONF ALL

FR70

FR69

164AR

B

A

NEW 

POTABLE WATER

FR69

FR70

STGR50RH

B

SERVICE DOOR

164AR

A

Z160

F_SB_524094_6_SAAA_01_02

Figure A-GSAAA - Sheet 01

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 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: 52

TITLE: DOORS-SERVICE DOORS-MODIFICATION OF LATCHING MECHANISM

OF POTABLE WATER SERVICE PANEL

MODIFICATION No.: 201938D50416 201938D50379 201939D59871 203344D50725 203563D50740

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 0022-0027 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 0131

0134-0137 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

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: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 1

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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

31V 0048 0088 0257

36V 0024 0052

38W 0282

58X 0004

98X 0429

ABD 0210

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

0399

AIB 0131 0141 0161 0182

ALK 0032 0033 0034 0367 0374 0381

ARG 0063 0074 0080 0085 0093 0094 0123 0126 0128 0170 0193 0373

CAL 0402 0406 0411 0415 0433 0541

CCA 0192 0199 0201 0242 0243 0264

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

DGA 0075 0081

DLH 0027 0035 0053 0135 0158 0213 0233 0252 0297 0304 0321 0325

0327 0335 0347 0352 0354 0379 0390 0434 0447

FIN 0058 0168 0174 0835 0844 0921 0938

G8E 0414

GAF 0274 0355

GFA 0212 0215 0554

HFY 0117 0190 0202

I2L 0216

IBE 0125 0134 0145 0146 0217 0221 0329 0474 0483

IRC 0002

IRM 0020 0056

KAC 0089 0090 0101 0104

LAN 0359 0363 0442

M3R 0061

MAU 0076 0152 0194 0268 0793 0800

MDG 0319

MSR 0156 0159 0178

NMB 0047 0051

OAL 0280 0292

PAL 0173 0176 0187 0196 0302 0318 0332 0387 0459

QAF 0026 0528

RJA 0014 0022 0038 0043

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 2

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@A340

SERVICE BULLETIN

OPERATOR MSN

S3R 0204

SAA 0006 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 0164 0214 0225

XAX 0273 0278

(4) Configuration by MSN

MSN CONFIGURATION

0002 0004 0006 0009 0014 0020 0022 0023 0024 0025 0026

0027 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 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 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 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 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 0955

001

0793 0800 0835 0844 0921 0938 002

(5) Configuration definition

**CONF 001

Conf. 001 is valid for all aircraft which have not embodied Modification No. 53630 and

54779 and all aircraft which have embodied Modification No. 54779 which cancels the

embodiment of Modification No. 53630.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 3

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

SERVICE BULLETIN

**CONF 002

Conf. 002 is valid for all aircraft which have embodied Modification No. 53630 but have

not embodied Modification No. 54779.

The following table gives further information of the configuration description

MOD Config. 001 Config. 002

53630 - x x

54779 - x -

Configuration/Modification/Service Bulletin Cross Reference Chart

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Kit 524094D01R01 1

Component COMPD03 As required (1)

Reidentified part set REIDD05 1

Reidentified part set REIDD07 As required (2)

Consumable CMLD10 As required

NOTE (1): The matset Comp 524094D03 is applicable only for operators which

have already matset Kit 524094D01R00 or Kit 524094D02R00 on stock

or which have already accomplished this Service Bulletin at the original

issue and have to do the additional work.

NOTE (2): The part set Reid 524094D07 is to be used only for operators which

have already matset Kit 524094D01R00 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do

the additional work.

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Kit 524094D02R01 1

Component COMPD03 As required (1)

Reidentified part set REIDD06 1

Reidentified part set REIDD08 As required (2)

Consumable CMLD10 As required

NOTE (1): The matset Comp 524094D03 is applicable only for operators which

have already matset Kit 524094D01R00 or Kit 524094D02R00 on stock

or which have already accomplished this Service Bulletin at the original

issue and have to do the additional work.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 4

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NOTE (2): The part set Reid 524094D08 is to be used only for operators which

have already matset Kit 524094D02R00 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do

the additional work.

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Several cases have been reported in which the potable water service panel access door

164AR has been lost during flight. In one case, on an A340 aircraft the THS leading

edge has been hit, in a second case, on an A330 aircraft the door was presumed to

have caused damage to the THS.

Investigations have shown difficulties with the latching mechanism of the potable water

service panel access door, which can lead to a potential unsafe condition. The potential

unsafe condition could cause possible injury to persons and damage to property on

ground and potential loss of the potable water service panel access door on runway.

The Inspection Service Bulletin A340-52-4088 was issued to inspect the access door

164AR, 154AR and 171AL. The Modification Service Bulletin A340-52-4087 was issued

as the final repair solution to the Inspection Service Bulletin A340-52-4088. Further

occurrences of access door 164AR lost during flight have shown that the Modification

Service Bulletin A340-52-4087 is not the definitive final repair solution for this access

door. Therefore, this mandatory Modification Service Bulletin, A340-52-4094, is issued

as the final repair solution for the access door 164AR. The loss of this door is classified

to be a potential unsafe condition.

To avoid further occurrences the design of the latching mechanism of the potable water

service panel access door has to be modified to mitigate the risk.

(2) Objective/Action

This Service Bulletin mandates the operator to install a modified potable water service

panel access door with reinforced hinge screws and more robust latches, including an

additional third latch.

(3) Advantages

After accomplishment of this Service Bulletin the handling and reliability of the potable

water service panel access door is improved.

This Service Bulletin meets the safety intent by making sure that the potable water

service panel access door can be correctly latched.

(4) Operational/Maintenance Consequences

None

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 5

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SERVICE BULLETIN

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 524094-831-848-001: Modification

(1) Modify the potable water service panel access door PN F5348614401200

(2) Remove the potable water service panel access door

(3) Remove the fittings and the anchor nuts

(4) Install the new anchor nuts

(5) Install the new hinges

(6) Install the new potable water service panel access door PN F5348614401800

(7) Install the new fittings

(8) Install the bonding lead

(9) Reidentify the potable water service panel

(10) Adjust the new potable water service panel access door

(11) Restore the aircraft surface protection

(12) Install the placard

Task 524094-831-849-001: Modification - ADDITIONAL WORK for aircraft modified by the

original issue

(1) Modify the potable water service panel access door PN F5348614401200

(2) Apply sealant to the modified areas

**CONF 002

Task 524094-831-848-001: Modification

(1) Modify the potable water service panel access door PN F5348614401000

(2) Remove the potable water service panel access door

(3) Remove the fittings and the anchor nuts

(4) Install the new anchor nuts

(5) Install the new hinges

(6) Install the new potable water service panel access door PN F5348614401600

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 6

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SERVICE BULLETIN

(7) Install the new fittings

(8) Install the bonding lead

(9) Reidentify the potable water service panel

(10) Adjust the new potable water service panel access door

(11) Restore the aircraft surface protection

(12) Install the placard

Task 524094-831-849-001: Modification - ADDITIONAL WORK for aircraft modified by the

original issue

(1) Modify the potable water service panel access door PN F5348614401000

(2) Apply sealant to the modified areas

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

This Service Bulletin must be accomplished within 48 months after original issue date of

this Service Bulletin.

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 threshold

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

accomplishment timescale.

If original issue has been implemented on aircraft, it is recommended to perform the

additional work within 24 months from the issue date of this Service Bulletin revision 01.

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.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 7

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SERVICE BULLETIN

G. MANPOWER

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

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

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

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

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

included.

**CONF 001

Task 524094-831-848-001: Modification

Get Access 2.50

On Aircraft

Remove the potable water service panel access door 0.50

Remove the fittings and the anchor nuts 0.50

Install the new anchor nuts 1.00

Install the new hinges 0.50

Install the new potable water service panel access

door PN F5348614401800

0.50

Install the new fittings 2.00

Install the bonding lead 0.25

Reidentify the potable water service panel 0.25

Adjust the new potable water service panel access

door

0.75

Restore the aircraft surface protection 0.50

Install the placard 0.25

On Bench

Modify the potable water service panel access door PN

F5348614401200

0.25

Tests 1.25

Close-Up 2.50

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

Task 524094-831-849-001: Modification - ADDITIONAL WORK for aircraft modified by the

original issue

Get Access 2.50

On Aircraft

Modify the potable water service panel access door PN

F5348614401200

0.25

Apply sealant to the modified areas 1.00

Tests 1.25

Close-Up 2.50

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

NOTE: For a breakdown of the manhours and elapsed time, refer to the Gantt Chart,

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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

**CONF 002

Task 524094-831-848-001: Modification

Get Access 2.50

On Aircraft

Remove the potable water service panel access door 0.5

Remove the fittings and the anchor nuts 0.50

Install the new anchor nuts 1.00

Install the new hinges 0.50

Install the new potable water service panel access

door PN F5348614401600

0.50

Install the new fittings 2.00

Install the bonding lead 0.25

Reidentify the potable water service panel 0.25

Adjust the new potable water service panel access

door

0.75

Restore the aircraft surface protection 0.50

Install the placard 0.25

On Bench

Modify the potable water service panel access door PN

F5348614401000

0.25

Tests 1.25

Close-Up 2.50

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

Task 524094-831-849-001: Modification - ADDITIONAL WORK for aircraft modified by the

original issue

Get Access 2.50

On Aircraft

Modify the potable water service panel access door PN

F5348614401000

0.25

Apply sealant to the modified areas 1.00

Tests 1.25

Close-Up 2.50

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

NOTE: For a breakdown of the manhours and elapsed time, refer to the Gantt Chart,

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

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 9

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SERVICE BULLETIN

**CONF ALL

H. WEIGHT AND BALANCE

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

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

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

**CONF 001

A340-200 A340-300

Manufacturers Empty Weight +0.845 KG +1.863 LB +0.845 KG +1.863 LB

Effect on Balance +42.593 KGM +308.075

LBF.FT +46.201 KGM +334.171LBF.FT

**CONF 002

A340-300

Manufacturers Empty Weight +0.871 KG +1.920 LB

Effect on Balance +47.584 KGM +344.175 LBF.FT

**CONF ALL

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

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

06-41-52 06-41-53 11-00-00

12-34-24 20-11-00 20-28-00

24-41-00 38-10-00 53-00-00

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-00 51-24-00 51-40-00

51-42-00 51-43-00 51-44-00

51-46-00 51-75-12

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

**CONF 002

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

06-41-52 06-41-53 11-00-00

12-34-24 20-11-00 20-28-00

24-41-00 38-10-00 53-00-00

Consumable Material List (CML)

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 10

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SERVICE BULLETIN

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-00 51-24-00 51-40-00

51-42-00 51-43-00 51-44-00

51-46-00 51-75-12

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

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 52-42-13

Illustrated Parts Catalog (IPC) 11-21-38 52-42-04

Maintenance Planning Document (MPD) 524000-02-1

Structural Repair Manual (SRM) 52-42-11

L. INTERCHANGEABILITY/MIXABILITY

**CONF 001

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Door Assy F5348614400600 F5348614401800 03 Not

Applicable

Panel F5348612320400 F5348633920000 03 Not

Applicable

Door Assy F5348614401200 F5348614401800 03 Not

Applicable

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF 002

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Door Assy F5348614400800 F5348614401600 03 Not

Applicable

Panel F5348612320400 F5348634020000 03 Not

Applicable

Door Assy F5348614401000 F5348614401600 03 Not

Applicable

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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**CONF ALL

M. SPARES

None

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 12

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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 524094D01R01

Kit 524094D02R01

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 25 90

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

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:

Component COMPD03 AIRBUS Material, Logistics and Suppliers

IFD - In Flight Desk

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet:

http://spares.airbus.com

For ordering by fax: +49 40 50 76 40 12

For ordering by E-mail:

ifd.spares@airbus.com

(2) Price and Availability

Kit 524094D01R01

Cost 15,280.00 USD

Availability 120 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.

Kit 524094D02R01

Cost 15,280.00 USD

Availability 120 calendar days from receipt of order

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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SERVICE BULLETIN

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.

Component COMPD03

Operator supplied AIRBUS parts required to accomplish this Service Bulletin are to be

purchased by a spares purchase order.

B. INDUSTRY SUPPORT INFORMATION

As a special policy applied to this Service Bulletin, AIRBUS will provide a 45% reduction to

the applicable kits sales prices given in the paragraph Price and Availability for orders placed

before Jun 30/16.

C. LIST OF COMPONENTS

Kit 524094D01R01

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

NOTES

2 F5348614401800 1 DOOR (2) F5348614400600 03

8 NAS1100-3-7 1 SCREW

12 NAS1291C3M 9 NUT

14 NAS1149C0332R 10 WASHER

16 NAS1102E3-8 8 SCREW

20 NAS1801-4-9 4 SCREW

22 NAS1149C0432R 4 WASHER

24 F5348615700600 2 HINGE

26 F5348615520400 2 SPRING

28 F5348615620400 4 SHIM (1)

30 NSA5075-5 9 COLLAR

32 DAN6-5-4 9 PIN

34 F5348614120200 2 FITTING

35 F5348614120400 1 FITTING

50 NSA5414N24-10 16 RIVET

52 NAS1474R4K 4 NUT

54 F5348615620600 2 SHIM

60 F1121009420000 1 PLACARD

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

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.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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SERVICE BULLETIN

NOTE (1): A maximum of 4 shims necessary only if the door has to be adjusted.

Kit 524094D02R01

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

NOTES

2 F5348614401600 1 DOOR (2) F5348614400800 03

8 NAS1100-3-7 1 SCREW

12 NAS1291C3M 9 NUT

14 NAS1149C0332R 10 WASHER

16 NAS1102E3-8 8 SCREW

20 NAS1801-4-9 4 SCREW

22 NAS1149C0432R 4 WASHER

24 F5348615700600 2 HINGE

26 F5348615520400 2 SPRING

28 F5348615620400 4 SHIM (1)

30 NSA5075-5 9 COLLAR

32 DAN6-5-4 9 PIN

34 F5348614120200 2 FITTING

35 F5348614120400 1 FITTING

50 NSA5414N24-10 16 RIVET

52 NAS1474R4K 4 NUT

54 F5348615620600 2 SHIM

60 F1121009420000 1 PLACARD

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

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): A maximum of 4 shims necessary only if the door has to be adjusted.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Top Coat Polyurethane-- External

Structure

04JAA3 As required

Coating-- Flexible Structure 04QAB2 As required

Varnish Polyurethane-Low Voc

External Structure

04SBA3 As required

Varnish-- Electrical Bonding

Structure

04TMB2 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Threadlocking Adhesive-- Medium

Strength

05BAE1 As required

Polysulfide Sealant-General

Purpose Brushable

06AAA1 As required

Polysulfide Sealant-General

Purpose Fillet

06AAB1 As required

Aqueous Cleaner-Aircraft Exterior

Pressure Sprayi

08ABC1 As required

Non Aqueous Cleaner-General 08BAA9 As required

Corrosion Preventive CompoundWater Displacing Oi12ABE2 As required

Release Agent-- Liquid Wax 14DBB1 As required

Wire-Locking Dia: 0.5 Mm (0.020

Inch) Cres Nickel

14QDB1 As required

Textile-Lint Free Cotton 14SBA1 As required

(2) Components

Component COMPD03

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

NOTES

6 A9249715920200 1 STUD

NOTE: The matset Comp 524094D03 is applicable only for operators which

have already matset Kit 524094D01R00 or Kit 524094D02R00 on stock

or which have already accomplished this Service Bulletin at the original

issue and have to do the additional work.

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

Reidentified part set REIDD05

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348633920000 PANEL F5348612320400

Reidentified part set REIDD06

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348634020000 PANEL F5348612320400

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Reidentified part set REIDD07

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348614401800 DOOR F5348614401200

NOTE: The part set Reid 524094D07 is to be used only for operators which

have already matset Kit 524094D01R00 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do the

additional work.

Reidentified part set REIDD08

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348614401600 DOOR F5348614401000

NOTE: The part set Reid 524094D08 is to be used only for operators which

have already matset Kit 524094D02R00 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do the

additional work.

F. TOOLING

None

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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This Page Intentionally Left Blank

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 524094-831-848-001 - 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.

NOTE: The accomplishment instructions of this Service Bulletin refer to procedures

included in other AIRBUS documents. When the words ’refer to’ are used and the

operator has an accepted alternative procedure, the accepted alternative procedure

can be used. When the words ’in accordance with’ are included in the instruction,

the procedure in the AIRBUS document must be used.

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.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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SERVICE BULLETIN

Task Associated Data

**CONF 001

Zone

160

Manpower

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

**CONF 002

Zone

160

Manpower

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 524094-910-201-001 - 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

06-41-52, Page Block 001

06-41-53, Page Block 001

11-00-00, Page Block 201

Task 20-11-00-911-801

Consumable Material List (CML)

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-00

51-24-00

51-40-00

51-42-00

51-43-00

51-44-00

51-46-00

(a) For the specification of the materials (Mat. No.) given in this Service Bulletin, refer

to the Consumable Materials List (CML).

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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SERVICE BULLETIN

(b) Refer to the AIRBUS Standards Manual (SM) if you find part numbers for the

hardware components in the related kit(s) which you cannot identify in the LIST OF

COMPONENTS of this Service Bulletin. The SM will give you the correct part

number to part number relationship.

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

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

(e) For the location of the stringers (STGR), refer to AMM 06-30-00, Page Block 001.

(f) For the identification of access doors and panels, refer to AMM 06-41-52, Page

Block 001 and AMM 06-41-53, Page Block 001.

(g) Apply sealant in accordance with SRM 51-24-00.

(h) Renew the protective finish in accordance with SRM 51-23-00.

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

(j) Obtain alternative and substitute fastener data in accordance with SRM 51-43-00.

(k) 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.

(l) 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.

(m) Obtain fastener hole diameters and drill data in accordance with SRM 51-44-00.

(n) Obtain countersink data in accordance with SRM 51-46-00.

(o) For installation of lockwire, refer to AMM Task 20-11-00-911-801.

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

(2) Subtask 524094-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 524094-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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SERVICE BULLETIN

References

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

06-30-00, Page Block 001

06-31-53, Page Block 001

06-41-52, Page Block 001

06-41-53, Page Block 001

11-00-00, Page Block 201

Task 20-11-00-911-801

Consumable Material List (CML)

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-00

51-24-00

51-40-00

51-42-00

51-43-00

51-44-00

51-46-00

(a) For the specification of the materials (Mat. No.) given in this Service Bulletin, refer

to the Consumable Materials List (CML).

(b) Refer to the AIRBUS Standards Manual (SM) if you find part numbers for the

hardware components in the related kit(s) which you cannot identify in the LIST OF

COMPONENTS of this Service Bulletin. The SM will give you the correct part

number to part number relationship.

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

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

(e) For the location of the stringers (STGR), refer to AMM 06-30-00, Page Block 001.

(f) For the identification of access doors and panels, refer to AMM 06-41-52, Page

Block 001 and AMM 06-41-53, Page Block 001.

(g) Apply sealant in accordance with SRM 51-24-00.

(h) Renew the protective finish in accordance with SRM 51-23-00.

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

(j) Obtain alternative and substitute fastener data in accordance with SRM 51-43-00.

(k) 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.

(l) 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.

(m) Obtain fastener hole diameters and drill data in accordance with SRM 51-44-00.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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(n) Obtain countersink data in accordance with SRM 51-46-00.

(o) For installation of lockwire, refer to AMM Task 20-11-00-911-801.

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

(2) Subtask 524094-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 524094-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 24-41-00-861-801

Task 53-00-00-000-804

(a) The following items 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.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

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

12-34-24-860-802.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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SERVICE BULLETIN

(c) Energize the aircraft electrical circuits, refer to AMM Task 24-41-00-861-801.

(d) Put an access platform in position below the potable water service panel access

door 164AR.

(e) Remove the necessary Bulk Cargo Compartment floor panels to get access

to the inner area of the potable water service panel, refer to AMM Task

53-00-00-000-804.

**CONF 002

(1) Subtask 524094-941-201-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 24-41-00-861-801

Task 53-00-00-000-804

(a) The following items 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.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

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

12-34-24-860-802.

(c) Energize the aircraft electrical circuits, refer to AMM Task 24-41-00-861-801.

(d) Put an access platform in position below the potable water service panel access

door 164AR.

(e) Remove the necessary Bulk Cargo Compartment floor panels to get access

to the inner area of the potable water service panel, refer to AMM Task

53-00-00-000-804.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 524094-831-201-001 - Modify the potable water service panel access door

PN F5348614401200

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

Material necessary to do the job

Component COMPD03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

6 A9249715920200 1 STUD

NOTE: The matset Comp 524094D03 is applicable only for operators which

have already matset Kit 524094D01R00 or Kit 524094D02R00 on stock

or which have already accomplished this Service Bulletin at the original

issue and have to do the additional work.

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Reidentified part set REIDD07

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348614401800 DOOR F5348614401200

NOTE: The part set Reid 524094D07 is to be used only for operators which

have already matset Kit 524094D01R00 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do

the additional work.

References

Fig. A-GBDAA

Additional work - Modification of the

potable water service panel access door

Sheet 01

Sheet 02

Sheet 03

NOTE: All operator, which have already matset Kit 524094D01R00 on stock,

have to modify the Door Assy, delivered with the matset Kit

524094D01R00, following the subsequent worksteps.

Otherwise continue with SUBTASK 524094-020-201 001 Remove the

potable water service panel access door .

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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SERVICE BULLETIN

(a) If you have the matset Kit 524094D01 with revision 00, then on bench, remove

from the Door Assy, PN F5348614401200, as shown on Fig. A-GBDAA Sheet 01,

Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View C:

1 Stud-Adjusting Item (4) Discard

1 Nut Item (3) Retain

(b) Install to the Door Assy, PN F5348614401200, as shown on Fig. A-GBDAA Sheet

01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View C:

1 Nut Item (3) Retained at

removal

1 Stud-Adjusting A9249715920200 Item 6

(c) Reidentify the potable water service panel access door:

1 Door Assy F5348614401200

becomes

1 Door Assy F5348614401800

NOTE: Mark the new P/N on the Door Assy with a permanent marker.

(2) Subtask 524094-020-201-001 - Remove the potable water service panel access

door

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

References

Fig. A-GBAAA

Removal of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) From the door, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and

Fig. A-GBAAA Sheet 03, View C remove:

1 Nut Item (12) Discard

2 Washer Item (14) Discard

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SERVICE BULLETIN

1 Screw Item (8) Discard

and disconnect

1 Bonding lead Item (10) Retain

(b) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig.

A-GBAAA Sheet 03, View D:

8 Nut Item (12) Discard

8 Washer Item (14) Discard

8 Screw Item (16) Discard

1 Door Assy F5348614400600 Item (2) Discard

(c) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig.

A-GBAAA Sheet 03, View D:

4 Bolt Item (20) Discard

4 Washer Item (22) Discard

2 Hinge Item (24) Discard

2 Spring Item (26) Discard

2 Shim Item (28) Discard

(3) Subtask 524094-020-202-001 - Remove the fittings and the anchor nuts

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

References

Fig. A-GBAAA

Removal of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

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(a) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig.

A-GBAAA Sheet 04, View F:

4 Collar Item (30) Discard

4 Pin Item (32) Discard

2 Fitting Item (34) Discard

(b) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 03 and Fig.

A-GBAAA Sheet 04, View E:

8 Rivet Item (50) Discard

4 Anchor nut Item (52) Discard

(4) Subtask 524094-420-201-001 - Install the new anchor nuts

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 524094D01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

50 NSA5414N24-10 16 RIVET

52 NAS1474R4K 4 NUT

54 F5348615620600 2 SHIM

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Coating-- Flexible Structure 04QAB2 As required

Polysulfide Sealant-General

Purpose Brushable

06AAA1 As required

Polysulfide Sealant-General

Purpose Fillet

06AAB1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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SERVICE BULLETIN

References

Structural Repair Manual (SRM) 51-24-00

51-44-00

51-46-00

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Put the Shims, item 54, in position as shown on Fig. A-GBBAA Sheet 01, Fig. AGBBAA Sheet 04 and Fig. A-GBBAA Sheet 05, View G.

(b) Transfer drill the existing rivet holes to the Shims, item 54, as shown on Fig. AGBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. A-GBBAA Sheet 05, View G

and in accordance with SRM 51-44-00.

(c) Temporarily install the Shims, item 54, to the structure with set screws.

(d) Drill the new rivet holes using the Anchor nut, item 52, as shown on Fig. A-GBBAA

Sheet 01, Fig. A-GBBAA Sheet 04, Fig. A-GBBAA Sheet 05, View G and H and

Fig. A-GBBAA Sheet 06, View J and in accordance with SRM 51-44-00.

(e) Drill the existing holes to a diameter of 6.8 mm (0.27 in) as shown on Fig. AGBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. A-GBBAA Sheet 05, section EE.

(f) Remove the Shims, item 54, and deburr all drilled holes.

(g) Countersink where necessary the rivet holes with a 100 ̊ countersink drill as shown

on Fig. A-GBBAA Sheet 05, section D-D and section E-E and in accordance with

SRM 51-46-00.

(h) Clean the installation area and the Shims, item 54, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(i) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. AGBBAA Sheet 05, View G:

2 Shim F5348615620600 Item 54

and, with:

Polysulfide SealantGeneral Purpose

Fillet

06AAB1 As required

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8 Rivet NSA5414N24-10 Item 50

NOTE: Cut the rivets to the necessary length.

(j) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. AGBBAA Sheet 05, View H:

4 Anchor Nut NAS1474R4K Item 52

with:

8 Rivet NSA5414N24-10 Item 50

NOTE: Cut the rivets to the necessary length.

(k) Apply to the Shim, item 54, the Anchor Nut, item 52 and the rivets, item 50, as

shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. A-GBBAA

Sheet 05, View G and H, section D-D and E-E, and in accordance with SRM

51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

(l) Let the sealant cure.

(m) Apply to the sealed areas:

Coating-- Flexible

Structure

04QAB2 As required

(5) Subtask 524094-420-206-001 - Install the new hinges

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 524094D01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

20 NAS1801-4-9 4 SCREW

22 NAS1149C0432R 4 WASHER

24 F5348615700600 2 HINGE

26 F5348615520400 2 SPRING

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

28 F5348615620400 4 SHIM (1)

NOTE (1): A maximum of 4 shims necessary only if the door has to be adjusted.

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Clean the area where the hinges will be installed with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(b) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 04, View F:

2 Spring F5348615520400 Item 26

2 Hinge Assy F5348615700600 Item 24

with

4 Washer NAS1149C0432R Item 22

4 Screw NAS1801-4-9 Item 20

(c) Check the alignment of the hinges.

1 Carefully bring the hinges, item 24, in the closed position as shown on Fig. AGBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. A-GBBAA Sheet 04,

section C-C.

2 Make sure that the contour of the structure and the hinges are level and there

are no steps as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02

and Fig. A-GBBAA Sheet 04, section C-C.

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3 To adjust the hinges install, if necessary:

4 Shim F5348615620400 Item 28

NOTE: A maximum of two shims, item 28, per hinge are allowed.

(d) Tighten the screws, item 20, with a torque value of 8.2 Nm to 10.6 Nm (72.58 lbf.in

to 93.82 lbf.in).

(6) Subtask 524094-420-202-001 - Install the new potable water service panel access

door PN F5348614401800

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 524094D01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 F5348614401800 1 DOOR

12 NAS1291C3M 8 NUT

14 NAS1149C0332R 8 WASHER

16 NAS1102E3-8 8 SCREW

References

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Fig. A-GBCAA

Adjustment of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 04, View F:

1 Door Assy F5348614401800 Item 2

with

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8 Screw NAS1102E3-8 Item 16

8 Washer NAS1149C0332R Item 14

8 Nut NAS1291C3M Item 12

(b) Close and adjust the door, item 2, to achieve a circumferential gap as shown on

Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA Sheet 04,

section C-C.

(c) Tighten the screws, item 16, with a torque value of 3.7 Nm to 4.8 Nm (32.75 lbf.in

to 42.48 lbf.in).

(7) Subtask 524094-420-203-001 - Install the new fittings

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 524094D01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

30 NSA5075-5 9 COLLAR

32 DAN6-5-4 9 PIN

34 F5348614120200 2 FITTING

35 F5348614120400 1 FITTING

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Coating-- Flexible Structure 04QAB2 As required

Polysulfide Sealant-General

Purpose Brushable

06AAA1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Structural Repair Manual (SRM) 51-24-00

51-44-00

51-46-00

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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References

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the fittings, item 34, using the existing rivet holes, to the structure with set

screws as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 03, View E.

(b) Mark the position of the new rivet holes.

(c) Drill the new rivet holes in the structure through the pilot hole.

(d) Increase the hole diameter to the correct size for the given fasteners in accordance

with SRM 51-44-00.

(e) Remove the fittings, item 34.

(f) Deburr the fastener holes.

(g) Countersink the holes of the fittings, item 34, with a 100 ̊ countersink drill in

accordance with SRM 51-46-00.

(h) Clean the installation area of the fittings, item 34, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(i) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 03, View E:

2 Fitting F5348614120200 Item 34

with

6 Pin-Rivet DAN6-5-4 Item 32

6 Collar NSA5075-5 Item 30

(j) Mark the position of the fitting, item 35, to the structure as shown on Fig. A-GBBAA

Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. A-GBBAA Sheet 03, View C, D and

section A-A.

(k) Carefully close the door, item 2, and check that the center line of the fitting, item

35, is in line with the center line of the latch.

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(l) Open the door, item 2.

(m) If necessary, correct the position of the fitting, item 35, to make sure that the latch

of the door, item 2, engages correctly.

(n) Mark the position of the rivet holes.

(o) Drill the rivet holes in the structure.

(p) Increase the hole diameter to the correct size for the given fasteners in accordance

with SRM 51-44-00.

(q) Remove the fitting, item 35.

(r) Deburr the fastener holes.

(s) Countersink the holes of the fitting, item 35, with a 100 ̊ countersink drill in

accordance with SRM 51-46-00.

(t) Clean the installation area of the fitting, item 35, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(u) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 03, View C, D and section A-A:

1 Fitting F5348614120400 Item 35

with

3 Pin-Rivet DAN6-5-4 Item 32

3 Collar NSA5075-5 Item 30

(v) Apply to the Fittings, item 34 and 35, the Pin-Rivet, item 32 and the Collar, item 30,

in accordance with SRM 51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

(w) Let the sealant cure.

(x) Apply to the sealed areas:

Coating-- Flexible

Structure

04QAB2 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 35

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SERVICE BULLETIN

(8) Subtask 524094-420-204-001 - Install the bonding lead

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 AIRFRAME

Material necessary to do the job

Kit 524094D01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

8 NAS1100-3-7 1 SCREW

12 NAS1291C3M 1 NUT

14 NAS1149C0332R 2 WASHER

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish-- Electrical Bonding

Structure

04TMB2 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-802

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

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Clean the bonding points, as given in AMM Task 20-28-00-912-802 and ESPM

20-51-20, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 36

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SERVICE BULLETIN

(b) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 06, View K:

1 Bonding lead Item (10) Retained at

removal

with

1 Screw NAS1100-3-7 Item 8

2 Washer NAS1149C0332R Item 14

1 Nut NAS1291C3M Item 12

(c) Apply to the bonding points as given in AMM Task 20-28-00-912-802:

Varnish-- Electrical

Bonding Structure

04TMB2 As required

(9) Subtask 524094-930-201-001 - Reidentify the potable water service panel

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 AIRFRAME

Material necessary to do the job

Reidentified part set REIDD05

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348633920000 PANEL F5348612320400

Reidentify the potable water service panel:

1 Panel F5348612320400

becomes

1 Panel F5348633920000

NOTE: Mark the new P/N on the panel with a permanent marker.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 37

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SERVICE BULLETIN

(10) Subtask 524094-820-201-001 - Adjust the new potable water service panel access

door

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.75

Minimum number of person 1

Subtask elapsed time 0.75

Skills AIRFRAME

Material necessary to do the job

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Threadlocking Adhesive--

Medium Strength

05BAE1 As required

Polysulfide Sealant-General

Purpose Fillet

06AAB1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Release Agent-- Liquid Wax 14DBB1 As required

Wire-Locking Dia: 0.5 Mm

(0.020 Inch) Cres Nickel

14QDB1 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-820-801

Fig. A-GBCAA

Adjustment of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Open the door, item 2, and lock all latches. Adjust all adjustment bolts to a gap of

6.5 mm (0.26 in) to the door as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA

Sheet 02 and Fig. A-GBCAA Sheet 03, section A-A.

(b) Close the door, item 2, and lock all latches. Check the gap between the door, item

2, and the structure. Open the door, item 2, and adjust all adjustment bolts to

achieve a gap of 0.8 mm (0.031 in) +/- 0.5mm (0.020 in), as shown on .Fig. AGBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA Sheet 04, section

B-B.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 38

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SERVICE BULLETIN

(c) Open the door, item 2, and clean the area to be sealed as shown on Fig. AGBCAA Sheet 01 and Fig. A-GBCAA Sheet 02 with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(d) Apply to the door, item 2, and to the structure as shown on Fig. A-GBCAA Sheet

01 and Fig. A-GBCAA Sheet 02:

Polysulfide SealantGeneral Purpose

Fillet

06AAB1 As required

and

Release Agent--

Liquid Wax

14DBB1 As required

(e) Close the door, item 2, and lock all latches.

(f) Let the sealant cure.

(g) Remove the unwanted sealant from the door and from the fuselage skin.

(h) Clean the door and structure skin with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(i) Do the final adjustment of the door, item 2.

1 Check the gap between the door, item 2, and the structure.

2 Adjust the door, item 2, to the minimum possible gap between the door, item

2, and the structure by adjusting the adjustment bolts without putting tension

to the latches even when they are in locked position.

3 Ensure that:

- the latches snap in clearly noticeable and without delay

- the hand force necessary to lock the latches in the door closed position is

not larger as needed to lock the latches in the door open position

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 39

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SERVICE BULLETIN

(j) Safety the adjustment bolt as follows:

1 If a latch with a drilled nut at the adjustment bolt is installed, safety the

adjustment bolt as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 03, section A-A, with:

Wire-Locking Dia:

0.5 Mm (0.020

Inch) Cres Nickel

14QDB1 As required

2 If a latch with a self-locking nut at the adjustment bolt is installed, safety the

adjustment bolt as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 03, section B-B, by tightening the self-locking nut

with a torque value of 4.0 Nm to 6.0 Nm (35.40 lbf.in to 53.10 lbf.in).

(k) Adjust the door switch as given in AMM Task 38-10-00-820-801.

(l) Safety the door switch as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 04, View C, with:

Threadlocking

Adhesive-- Medium

Strength

05BAE1 As required

(11) Subtask 524094-916-201-001 - Restore the aircraft surface protection

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Top Coat Polyurethane--

External Structure

04JAA3 As required

Aqueous Cleaner-Aircraft

Exterior Pressure Sprayi

08ABC1 As required

Corrosion Preventive

Compound-Water

Displacing Oi

12ABE2 As required

Textile-Lint Free Cotton 14SBA1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 40

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SERVICE BULLETIN

References

Structural Repair Manual (SRM) 51-75-12

(a) Clean the potable water service panel access door with:

Aqueous CleanerAircraft Exterior

Pressure Sprayi

08ABC1 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(b) Apply, in accordance with your aircraft color scheme:

Top Coat

Polyurethane--

External Structure

04JAA3 As required

to the outside area of the potable water service panel access door, refer to SRM

51-75-12.

(c) Inside the fuselage, clean the area of the potable water service panel and make

sure that the area is dirt free.

(d) Restore the surface protection of the inner fuselage skin with:

Corrosion

Preventive

Compound-Water

Displacing Oi

12ABE2 As required

(12) Subtask 524094-420-205-001 - Install the placard

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 AIRFRAME

Material necessary to do the job

Kit 524094D01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

60 F1121009420000 1 PLACARD

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 41

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SERVICE BULLETIN

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish Polyurethane-Low

Voc External Structure

04SBA3 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Clean the installation area of the placard, item 60, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(b) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 06, View L:

1 Placard F1121009420000 Item 60

(c) Apply to the placard for protection:

Varnish

Polyurethane-Low

Voc External

Structure

04SBA3 As required

**CONF 002

(1) Subtask 524094-831-201-002 - Modify the potable water service panel access door

PN F5348614401000

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 42

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SERVICE BULLETIN

Material necessary to do the job

Component COMPD03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

6 A9249715920200 1 STUD

NOTE: The matset Comp 524094D03 is applicable only for operators which

have already matset Kit 524094D01R00 or Kit 524094D02R00 on stock

or which have already accomplished this Service Bulletin at the original

issue and have to do the additional work.

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Reidentified part set REIDD08

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348614401600 DOOR F5348614401000

NOTE: The part set Reid 524094D08 is to be used only for operators which

have already matset Kit 524094D02R00 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do

the additional work.

References

Fig. A-GBDAA

Additional work - Modification of the

potable water service panel access door

Sheet 01

Sheet 02

Sheet 03

NOTE: All operator, which have already matset Kit 524094D02R00 on stock,

have to modify the Door Assy, delivered with the matset Kit

524094D02R00, following the subsequent worksteps.

Otherwise continue with SUBTASK 524094-020-202 001 Remove the

fittings and the anchor nuts .

(a) If you have the matset Kit 524094D02 with revision 00, then on bench, remove

from the Door Assy, PN F5348614401000, as shown on Fig. A-GBDAA Sheet 01,

Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View C:

1 Stud-Adjusting Item (4) Discard

1 Nut Item (3) Retain

(b) Install to the Door Assy, PN F5348614401000, as shown on Fig. A-GBDAA Sheet

01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View C:

1 Nut Item (3) Retained at

removal

1 Stud-Adjusting A9249715920200 Item 6

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 43

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SERVICE BULLETIN

(c) Reidentify the potable water service panel access door:

1 Door Assy F5348614401000

becomes

1 Door Assy F5348614401600

NOTE: Mark the new P/N on the Door Assy with a permanent marker.

(2) Subtask 524094-020-201-002 - Remove the potable water service panel access

door

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.5

Minimum number of person 1

Subtask elapsed time 0.5

Skills AIRFRAME

References

Fig. A-GBAAA

Removal of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) From the door, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and

Fig. A-GBAAA Sheet 03, View C remove:

1 Nut Item (12) Discard

2 Washer Item (14) Discard

1 Screw Item (8) Discard

and disconnect

1 Bonding lead Item (10) Retain

(b) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig.

A-GBAAA Sheet 03, View D:

8 Nut Item (12) Discard

8 Washer Item (14) Discard

8 Screw Item (16) Discard

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 44

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SERVICE BULLETIN

1 Door Assy F5348614400800 Item (2) Discard

(c) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig.

A-GBAAA Sheet 03, View D:

4 Bolt Item (20) Discard

4 Washer Item (22) Discard

2 Hinge Item (24) Discard

2 Spring Item (26) Discard

2 Shim Item (28) Discard

(3) Subtask 524094-020-202-001 - Remove the fittings and the anchor nuts

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

References

Fig. A-GBAAA

Removal of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig.

A-GBAAA Sheet 04, View F:

4 Collar Item (30) Discard

4 Pin Item (32) Discard

2 Fitting Item (34) Discard

(b) Remove, as shown on Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 03 and Fig.

A-GBAAA Sheet 04, View E:

8 Rivet Item (50) Discard

4 Anchor nut Item (52) Discard

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 45

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SERVICE BULLETIN

(4) Subtask 524094-420-201-002 - Install the new anchor nuts

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 524094D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

50 NSA5414N24-10 16 RIVET

52 NAS1474R4K 4 NUT

54 F5348615620600 2 SHIM

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Coating-- Flexible Structure 04QAB2 As required

Polysulfide Sealant-General

Purpose Brushable

06AAA1 As required

Polysulfide Sealant-General

Purpose Fillet

06AAB1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Structural Repair Manual (SRM) 51-24-00

51-44-00

51-46-00

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Put the Shims, item 54, in position as shown on Fig. A-GBBAA Sheet 01, Fig. AGBBAA Sheet 04 and Fig. A-GBBAA Sheet 05, View G.

(b) Transfer drill the existing rivet holes to the Shims, item 54, as shown on Fig. AGBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. A-GBBAA Sheet 05, View G

and in accordance with SRM 51-44-00.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 46

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@A340

SERVICE BULLETIN

(c) Temporarily install the Shims, item 54, to the structure with set screws.

(d) Drill the new rivet holes using the Anchor nut, item 52, as shown on Fig. A-GBBAA

Sheet 01, Fig. A-GBBAA Sheet 04, Fig. A-GBBAA Sheet 05, View G and H and

Fig. A-GBBAA Sheet 06, View J and in accordance with SRM 51-44-00.

(e) Drill the existing holes to a diameter of 6.8 mm (0.27 in) as shown on Fig. AGBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. A-GBBAA Sheet 05, section EE.

(f) Remove the Shims, item 54, and deburr all drilled holes.

(g) Countersink where necessary the rivet holes with a 100 ̊ countersink drill as shown

on Fig. A-GBBAA Sheet 05, section D-D and section E-E and in accordance with

SRM 51-46-00.

(h) Clean the installation area and the Shims, item 54, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(i) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. AGBBAA Sheet 05, View G:

2 Shim F5348615620600 Item 54

and, with:

Polysulfide SealantGeneral Purpose

Fillet

06AAB1 As required

8 Rivet NSA5414N24-10 Item 50

NOTE: Cut the rivets to the necessary length.

(j) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. AGBBAA Sheet 05, View H:

4 Anchor Nut NAS1474R4K Item 52

with:

8 Rivet NSA5414N24-10 Item 50

NOTE: Cut the rivets to the necessary length.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 47

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@A340

SERVICE BULLETIN

(k) Apply to the Shim, item 54, the Anchor Nut, item 52 and the rivets, item 50, as

shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 04 and Fig. A-GBBAA

Sheet 05, View G and H, section D-D and E-E, and in accordance with SRM

51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

(l) Let the sealant cure.

(m) Apply to the sealed areas:

Coating-- Flexible

Structure

04QAB2 As required

(5) Subtask 524094-420-206-002 - Install the new hinges

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 524094D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

20 NAS1801-4-9 4 SCREW

22 NAS1149C0432R 4 WASHER

24 F5348615700600 2 HINGE

26 F5348615520400 2 SPRING

28 F5348615620400 4 SHIM (1)

NOTE (1): A maximum of 4 shims necessary only if the door has to be adjusted.

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 48

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@A340

SERVICE BULLETIN

References

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Clean the area where the hinges will be installed with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(b) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 04, View F:

2 Spring F5348615520400 Item 26

2 Hinge Assy F5348615700600 Item 24

with

4 Washer NAS1149C0432R Item 22

4 Screw NAS1801-4-9 Item 20

(c) Check the alignment of the hinges.

1 Carefully bring the hinges, item 24, in the closed position as shown on Fig. AGBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. A-GBBAA Sheet 04,

section C-C.

2 Make sure that the contour of the structure and the hinges are level and there

are no steps as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02

and Fig. A-GBBAA Sheet 04, section C-C.

3 To adjust the hinges install, if necessary:

4 Shim F5348615620400 Item 28

NOTE: A maximum of two shims, item 28, per hinge are allowed.

(d) Tighten the screws, item 20, with a torque value of 8.2 Nm to 10.6 Nm (72.58 lbf.in

to 93.82 lbf.in).

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 49

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@A340

SERVICE BULLETIN

(6) Subtask 524094-420-202-002 - Install the new potable water service panel access

door PN F5348614401600

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 524094D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 F5348614401600 1 DOOR

12 NAS1291C3M 8 NUT

14 NAS1149C0332R 8 WASHER

16 NAS1102E3-8 8 SCREW

References

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Fig. A-GBCAA

Adjustment of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 04, View F:

1 Door Assy F5348614401600 Item 2

with

8 Screw NAS1102E3-8 Item 16

8 Washer NAS1149C0332R Item 14

8 Nut NAS1291C3M Item 12

(b) Close and adjust the door, item 2, to achieve a circumferential gap as shown on

Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA Sheet 04,

section C-C.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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@A340

SERVICE BULLETIN

(c) Tighten the screws, item 16, with a torque value of 3.7 Nm to 4.8 Nm (32.75 lbf.in

to 42.48 lbf.in).

(7) Subtask 524094-420-203-002 - Install the new fittings

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Kit 524094D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

30 NSA5075-5 9 COLLAR

32 DAN6-5-4 9 PIN

34 F5348614120200 2 FITTING

35 F5348614120400 1 FITTING

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Coating-- Flexible Structure 04QAB2 As required

Polysulfide Sealant-General

Purpose Brushable

06AAA1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Structural Repair Manual (SRM) 51-24-00

51-44-00

51-46-00

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Install the fittings, item 34, using the existing rivet holes, to the structure with set

screws as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 03, View E.

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(b) Mark the position of the new rivet holes.

(c) Drill the new rivet holes in the structure through the pilot hole.

(d) Increase the hole diameter to the correct size for the given fasteners in accordance

with SRM 51-44-00.

(e) Remove the fittings, item 34.

(f) Deburr the fastener holes.

(g) Countersink the holes of the fittings, item 34, with a 100 ̊ countersink drill in

accordance with SRM 51-46-00.

(h) Clean the installation area of the fittings, item 34, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(i) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 03, View E:

2 Fitting F5348614120200 Item 34

with

6 Pin-Rivet DAN6-5-4 Item 32

6 Collar NSA5075-5 Item 30

(j) Mark the position of the fitting, item 35, to the structure as shown on Fig. A-GBBAA

Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. A-GBBAA Sheet 03, View C, D and

section A-A.

(k) Carefully close the door, item 2, and check that the center line of the fitting, item

35, is in line with the center line of the latch.

(l) Open the door, item 2.

(m) If necessary, correct the position of the fitting, item 35, to make sure that the latch

of the door, item 2, engages correctly.

(n) Mark the position of the rivet holes.

(o) Drill the rivet holes in the structure.

(p) Increase the hole diameter to the correct size for the given fasteners in accordance

with SRM 51-44-00.

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(q) Remove the fitting, item 35.

(r) Deburr the fastener holes.

(s) Countersink the holes of the fitting, item 35, with a 100 ̊ countersink drill in

accordance with SRM 51-46-00.

(t) Clean the installation area of the fitting, item 35, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(u) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 03, View C, D and section A-A:

1 Fitting F5348614120400 Item 35

with

3 Pin-Rivet DAN6-5-4 Item 32

3 Collar NSA5075-5 Item 30

(v) Apply to the Fittings, item 34 and 35, the Pin-Rivet, item 32 and the Collar, item 30,

in accordance with SRM 51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

(w) Let the sealant cure.

(x) Apply to the sealed areas:

Coating-- Flexible

Structure

04QAB2 As required

(8) Subtask 524094-420-204-002 - Install the bonding lead

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 AIRFRAME

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SERVICE BULLETIN

Material necessary to do the job

Kit 524094D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

8 NAS1100-3-7 1 SCREW

12 NAS1291C3M 1 NUT

14 NAS1149C0332R 2 WASHER

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish-- Electrical Bonding

Structure

04TMB2 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) Task 20-28-00-912-802

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

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Clean the bonding points, as given in AMM Task 20-28-00-912-802 and ESPM

20-51-20, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(b) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 06, View K:

1 Bonding lead Item (10) Retained at

removal

with

1 Screw NAS1100-3-7 Item 8

2 Washer NAS1149C0332R Item 14

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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1 Nut NAS1291C3M Item 12

(c) Apply to the bonding points as given in AMM Task 20-28-00-912-802:

Varnish-- Electrical

Bonding Structure

04TMB2 As required

(9) Subtask 524094-930-201-002 - Reidentify the potable water service panel

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 AIRFRAME

Material necessary to do the job

Reidentified part set REIDD06

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348634020000 PANEL F5348612320400

Reidentify the potable water service panel:

1 Panel F5348612320400

becomes

1 Panel F5348634020000

NOTE: Mark the new P/N on the panel with a permanent marker.

(10) Subtask 524094-820-201-001 - Adjust the new potable water service panel access

door

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.75

Minimum number of person 1

Subtask elapsed time 0.75

Skills AIRFRAME

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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Material necessary to do the job

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Threadlocking Adhesive--

Medium Strength

05BAE1 As required

Polysulfide Sealant-General

Purpose Fillet

06AAB1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Release Agent-- Liquid Wax 14DBB1 As required

Wire-Locking Dia: 0.5 Mm

(0.020 Inch) Cres Nickel

14QDB1 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-820-801

Fig. A-GBCAA

Adjustment of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(a) Open the door, item 2, and lock all latches. Adjust all adjustment bolts to a gap of

6.5 mm (0.26 in) to the door as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA

Sheet 02 and Fig. A-GBCAA Sheet 03, section A-A.

(b) Close the door, item 2, and lock all latches. Check the gap between the door, item

2, and the structure. Open the door, item 2, and adjust all adjustment bolts to

achieve a gap of 0.8 mm (0.031 in) +/- 0.5mm (0.020 in), as shown on .Fig. AGBCAA Sheet 01, Fig. A-GBCAA Sheet 02 and Fig. A-GBCAA Sheet 04, section

B-B.

(c) Open the door, item 2, and clean the area to be sealed as shown on Fig. AGBCAA Sheet 01 and Fig. A-GBCAA Sheet 02 with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(d) Apply to the door, item 2, and to the structure as shown on Fig. A-GBCAA Sheet

01 and Fig. A-GBCAA Sheet 02:

Polysulfide SealantGeneral Purpose

Fillet

06AAB1 As required

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and

Release Agent--

Liquid Wax

14DBB1 As required

(e) Close the door, item 2, and lock all latches.

(f) Let the sealant cure.

(g) Remove the unwanted sealant from the door and from the fuselage skin.

(h) Clean the door and structure skin with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(i) Do the final adjustment of the door, item 2.

1 Check the gap between the door, item 2, and the structure.

2 Adjust the door, item 2, to the minimum possible gap between the door, item

2, and the structure by adjusting the adjustment bolts without putting tension

to the latches even when they are in locked position.

3 Ensure that:

- the latches snap in clearly noticeable and without delay

- the hand force necessary to lock the latches in the door closed position is

not larger as needed to lock the latches in the door open position

(j) Safety the adjustment bolt as follows:

1 If a latch with a drilled nut at the adjustment bolt is installed, safety the

adjustment bolt as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 03, section A-A, with:

Wire-Locking Dia:

0.5 Mm (0.020

Inch) Cres Nickel

14QDB1 As required

2 If a latch with a self-locking nut at the adjustment bolt is installed, safety the

adjustment bolt as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 03, section B-B, by tightening the self-locking nut

with a torque value of 4.0 Nm to 6.0 Nm (35.40 lbf.in to 53.10 lbf.in).

(k) Adjust the door switch as given in AMM Task 38-10-00-820-801.

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(l) Safety the door switch as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 04, View C, with:

Threadlocking

Adhesive-- Medium

Strength

05BAE1 As required

(11) Subtask 524094-916-201-001 - Restore the aircraft surface protection

Work Zones and Access Panels

Zone Access/Work location

160

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Top Coat Polyurethane--

External Structure

04JAA3 As required

Aqueous Cleaner-Aircraft

Exterior Pressure Sprayi

08ABC1 As required

Corrosion Preventive

Compound-Water

Displacing Oi

12ABE2 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Structural Repair Manual (SRM) 51-75-12

(a) Clean the potable water service panel access door with:

Aqueous CleanerAircraft Exterior

Pressure Sprayi

08ABC1 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

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(b) Apply, in accordance with your aircraft color scheme:

Top Coat

Polyurethane--

External Structure

04JAA3 As required

to the outside area of the potable water service panel access door, refer to SRM

51-75-12.

(c) Inside the fuselage, clean the area of the potable water service panel and make

sure that the area is dirt free.

(d) Restore the surface protection of the inner fuselage skin with:

Corrosion

Preventive

Compound-Water

Displacing Oi

12ABE2 As required

(12) Subtask 524094-420-205-002 - Install the placard

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 AIRFRAME

Material necessary to do the job

Kit 524094D02R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

60 F1121009420000 1 PLACARD

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Varnish Polyurethane-Low

Voc External Structure

04SBA3 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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SERVICE BULLETIN

References

Fig. A-GBBAA

Installation of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

(a) Clean the installation area of the placard, item 60, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(b) Install, as shown on Fig. A-GBBAA Sheet 01, Fig. A-GBBAA Sheet 02 and Fig. AGBBAA Sheet 06, View L:

1 Placard F1121009420000 Item 60

(c) Apply to the placard for protection:

Varnish

Polyurethane-Low

Voc External

Structure

04SBA3 As required

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 524094-700-201-001 - Operational

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-710-801

Do the operational test of the limit switches, refer to AMM Task 38-10-00-710-801.

**CONF 002

(1) Subtask 524094-700-201-001 - Operational

Manpower Resources

Skills NON SPECIFIC

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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References

Aircraft Maintenance Manual (AMM) Task 38-10-00-710-801

Do the operational test of the limit switches, refer to AMM Task 38-10-00-710-801.

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 524094-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 53-00-00-400-804

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

equipment.

(b) Install the removed Bulk Cargo Compartment floor panels, refer to AMM Task

53-00-00-400-804.

(c) Remove the access platform from below the potable water service panel access

door 164AR.

(d) De-energize the aircraft electrical circuits, refer to AMM Task 24-41-00-862-801.

**CONF 002

(1) Subtask 524094-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 53-00-00-400-804

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

equipment.

(b) Install the removed Bulk Cargo Compartment floor panels, refer to AMM Task

53-00-00-400-804.

(c) Remove the access platform from below the potable water service panel access

door 164AR.

(d) De-energize the aircraft electrical circuits, refer to AMM Task 24-41-00-862-801.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 61

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This Page Intentionally Left Blank

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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SERVICE BULLETIN

Task 524094-831-849-001 - Modification - ADDITIONAL WORK for aircraft modified by the

original issue

**CONF ALL

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.

NOTE: The accomplishment instructions of this Service Bulletin refer to procedures

included in other AIRBUS documents. When the words ’refer to’ are used and the

operator has an accepted alternative procedure, the accepted alternative procedure

can be used. When the words ’in accordance with’ are included in the instruction,

the procedure in the AIRBUS document must be used.

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.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

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Task Associated Data

**CONF 001

Manpower

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

**CONF 002

Manpower

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 524094-910-202-001 - 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

06-41-52, Page Block 001

06-41-53, Page Block 001

Consumable Material List (CML)

Standards Manual (SM)

(a) For the specification of the materials (Mat. No.) given in this Service Bulletin, refer

to the Consumable Materials List (CML).

(b) Refer to the AIRBUS Standards Manual (SM) if you find part numbers for the

hardware components in the related kit(s) which you cannot identify in the LIST OF

COMPONENTS of this Service Bulletin. The SM will give you the correct part

number to part number relationship.

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

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

(e) For the location of the stringers (STGR), refer to AMM 06-30-00, Page Block 001.

(f) For the identification of access doors and panels, refer to AMM 06-41-52, Page

Block 001 and AMM 06-41-53, Page Block 001.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 64

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(2) Subtask 524094-839-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 524094-910-202-001 - 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

06-41-52, Page Block 001

06-41-53, Page Block 001

Consumable Material List (CML)

Standards Manual (SM)

(a) For the specification of the materials (Mat. No.) given in this Service Bulletin, refer

to the Consumable Materials List (CML).

(b) Refer to the AIRBUS Standards Manual (SM) if you find part numbers for the

hardware components in the related kit(s) which you cannot identify in the LIST OF

COMPONENTS of this Service Bulletin. The SM will give you the correct part

number to part number relationship.

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

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

(e) For the location of the stringers (STGR), refer to AMM 06-30-00, Page Block 001.

(f) For the identification of access doors and panels, refer to AMM 06-41-52, Page

Block 001 and AMM 06-41-53, Page Block 001.

(2) Subtask 524094-839-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 65

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**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 524094-941-202-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 24-41-00-861-801

Task 53-00-00-000-804

(a) The following items 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.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

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

12-34-24-860-802.

(c) Energize the aircraft electrical circuits, refer to AMM Task 24-41-00-861-801.

(d) Put an access platform in position below the potable water service panel access

door 164AR.

(e) Remove the necessary Bulk Cargo Compartment floor panels to get access

to the inner area of the potable water service panel, refer to AMM Task

53-00-00-000-804.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 66

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**CONF 002

(1) Subtask 524094-941-202-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 24-41-00-861-801

Task 53-00-00-000-804

(a) The following items 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.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

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

12-34-24-860-802.

(c) Energize the aircraft electrical circuits, refer to AMM Task 24-41-00-861-801.

(d) Put an access platform in position below the potable water service panel access

door 164AR.

(e) Remove the necessary Bulk Cargo Compartment floor panels to get access

to the inner area of the potable water service panel, refer to AMM Task

53-00-00-000-804.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 67

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**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 524094-831-202-001 - Modify the potable water service panel access door

PN F5348614401200

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

Material necessary to do the job

Component COMPD03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

6 A9249715920200 1 STUD

NOTE: The matset Comp 524094D03 is applicable only for operators which

have already matset Kit 524094D01R00 or Kit 524094D02R00 on stock

or which have already accomplished this Service Bulletin at the original

issue and have to do the additional work.

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Reidentified part set REIDD07

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348614401800 DOOR F5348614401200

NOTE: The part set Reid 524094D07 is to be used only for operators which

have already matset Kit 524094D01R00 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do

the additional work.

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Threadlocking Adhesive--

Medium Strength

05BAE1

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-820-801

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 68

6

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SERVICE BULLETIN

References

Fig. A-GBCAA

Adjustment of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GBDAA

Additional work - Modification of the

potable water service panel access door

Sheet 01

Sheet 02

Sheet 03

(a) Open the potable water service panel access door.

(b) Check the PN of the Stud-Adjusting:

1 If the PN is A9249715920200 continue with step (e).

2 If the PN is NAS563C25 continue with step (c).

(c) Remove from the Door Assy, PN F5348614401200, as shown on Fig. A-GBDAA

Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View C:

1 Stud-Adjusting Item (4) Discard

1 Nut Item (3) Retain

(d) Install to the Door Assy, PN F5348614401200, as shown on Fig. A-GBDAA Sheet

01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View D:

1 Nut Item (3) Retained at

removal

1 Stud-Adjusting A9249715920200 Item 6

(e) Reidentify the potable water service panel access door:

1 Door Assy F5348614401200

becomes

1 Door Assy F5348614401800

NOTE: Mark the new P/N on the Door Assy with a permanent marker.

(f) Adjust the door switch as given in AMM Task 38-10-00-820-801.

(g) Safety the door switch as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 04, View C, with:

Threadlocking

Adhesive-- Medium

Strength

05BAE1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 69

6

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SERVICE BULLETIN

(2) Subtask 524094-831-203-001 - Apply sealant to the modified areas

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Coating-- Flexible Structure 04QAB2 As required

Polysulfide Sealant-General

Purpose Brushable

06AAA1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Structural Repair Manual (SRM) 51-24-00

Fig. A-GBEAA

Additional work - Application of the

sealant

Sheet 01

Sheet 02

Sheet 03

(a) Apply sealant to the modified areas, as shown on Fig. A-GBEAA Sheet 01, Fig. AGBEAA Sheet 02 and Fig. A-GBEAA Sheet 03, view C, section A-A, B-B and C-C.

1 Clean the installation area of the Shim and the Anchor nut, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

2 Apply to the Shim, the Anchor Nut and the rivets, in accordance with SRM

51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

3 Clean the installation area of the fitting, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 70

6

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SERVICE BULLETIN

Textile-Lint Free

Cotton

14SBA1 As required

4 Apply to the Fittings, the Pin-Rivet and the Collar, in accordance with SRM

51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

(b) Let the sealant cure.

(c) Apply to the sealed areas:

Coating-- Flexible

Structure

04QAB2 As required

**CONF 002

(1) Subtask 524094-831-202-002 - Modify the potable water service panel access door

PN F5348614401000

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

Material necessary to do the job

Component COMPD03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

6 A9249715920200 1 STUD

NOTE: The matset Comp 524094D03 is applicable only for operators which

have already matset Kit 524094D01R00 or Kit 524094D02R00 on stock

or which have already accomplished this Service Bulletin at the original

issue and have to do the additional work.

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Reidentified part set REIDD08

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348614401600 DOOR F5348614401000

NOTE: The part set Reid 524094D08 is to be used only for operators which

have already matset Kit 524094D02R00 on stock or which have already

accomplished this Service Bulletin at the original issue and have to do

the additional work.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 71

6

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@A340

SERVICE BULLETIN

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Threadlocking Adhesive--

Medium Strength

05BAE1 As required

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-820-801

Fig. A-GBCAA

Adjustment of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Fig. A-GBDAA

Additional work - Modification of the

potable water service panel access door

Sheet 01

Sheet 02

Sheet 03

(a) Open the potable water service panel access door.

(b) Check the PN of the Stud-Adjusting:

1 If the PN is A9249715920200 continue with step (e).

2 If the PN is NAS563C25 continue with step (c).

(c) Remove from the Door Assy, PN F5348614401000, as shown on Fig. A-GBDAA

Sheet 01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View C:

1 Stud-Adjusting Item (4) Discard

1 Nut Item (3) Retain

(d) Install to the Door Assy, PN F5348614401000, as shown on Fig. A-GBDAA Sheet

01, Fig. A-GBDAA Sheet 02 and Fig. A-GBDAA Sheet 03, View D:

1 Nut Item (3) Retained at

removal

1 Stud-Adjusting A9249715920200 Item 6

(e) Reidentify the potable water service panel access door:

1 Door Assy F5348614401000

becomes

1 Door Assy F5348614401600

NOTE: Mark the new P/N on the Door Assy with a permanent marker.

(f) Adjust the door switch as given in AMM Task 38-10-00-820-801.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 72

6

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@A340

SERVICE BULLETIN

(g) Safety the door switch as shown on Fig. A-GBCAA Sheet 01, Fig. A-GBCAA Sheet

02 and Fig. A-GBCAA Sheet 04, View C, with:

Threadlocking

Adhesive-- Medium

Strength

05BAE1 As required

(2) Subtask 524094-831-203-001 - Apply sealant to the modified areas

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLD10

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Coating-- Flexible Structure 04QAB2 As required

Polysulfide Sealant-General

Purpose Brushable

06AAA1 As required

Non Aqueous CleanerGeneral08BAA9 As required

Textile-Lint Free Cotton 14SBA1 As required

References

Structural Repair Manual (SRM) 51-24-00

Fig. A-GBEAA

Additional work - Application of the

sealant

Sheet 01

Sheet 02

Sheet 03

(a) Apply sealant to the modified areas, as shown on Fig. A-GBEAA Sheet 01, Fig. AGBEAA Sheet 02 and Fig. A-GBEAA Sheet 03, view C, section A-A, B-B and C-C.

1 Clean the installation area of the Shim and the Anchor nut, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 73

6

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SERVICE BULLETIN

2 Apply to the Shim, the Anchor Nut and the rivets, in accordance with SRM

51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

3 Clean the installation area of the fitting, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

4 Apply to the Fittings, the Pin-Rivet and the Collar, in accordance with SRM

51-24-00:

Polysulfide SealantGeneral Purpose

Brushable

06AAA1 As required

(b) Let the sealant cure.

(c) Apply to the sealed areas:

Coating-- Flexible

Structure

04QAB2 As required

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 524094-700-202-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-710-801

Do the operational test of the limit switches, refer to AMM Task 38-10-00-710-801.

**CONF 002

(1) Subtask 524094-700-202-001 - Testing

Manpower Resources

Skills NON SPECIFIC

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 74

6

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 38-10-00-710-801

Do the operational test of the limit switches, refer to AMM Task 38-10-00-710-801.

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 524094-942-202-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 53-00-00-400-804

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

equipment.

(b) Install the removed Bulk Cargo Compartment floor panels, refer to AMM Task

53-00-00-400-804.

(c) Remove the access platform from below the potable water service panel access

door 164AR.

(d) De-energize the aircraft electrical circuits, refer to AMM Task 24-41-00-862-801.

**CONF 002

(1) Subtask 524094-942-202-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-862-801

Task 53-00-00-400-804

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

equipment.

(b) Install the removed Bulk Cargo Compartment floor panels, refer to AMM Task

53-00-00-400-804.

(c) Remove the access platform from below the potable water service panel access

door 164AR.

(d) De-energize the aircraft electrical circuits, refer to AMM Task 24-41-00-862-801.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 75

6

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@A340

SERVICE BULLETIN

**CONF ALL

FR70

FR69

164AR

A

B

A

F_SB_524094_6_BAAA_01_00

Z160

Figure A-GBAAA - Sheet 01

Removal of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 76

6

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@A340

SERVICE BULLETIN

**CONF ALL

(2)

POTABLE WATER

FR69

FR70

STGR50RH

B

SERVICE DOOR

164AR

F

F

C

D

D

F_SB_524094_6_BAAA_02_01

Figure A-GBAAA - Sheet 02

Removal of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 77

6

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@A340

SERVICE BULLETIN

**CONF ALL

(12)

(14)

(10)

(14)

(8)

(2)

C

D

F_SB_524094_6_BAAA_03_00

(2)

(26)

(28)

(22)

(20)

(24)

(4 POS)

(4 POS)

(4 POS)

(16)

(14)

(12)

E

Figure A-GBAAA - Sheet 03

Removal of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 78

6

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@A340

SERVICE BULLETIN

**CONF ALL

(34)

(30)

(32)

(52)

E (50)

F

F_SB_524094_6_BAAA_04_00

Figure A-GBAAA - Sheet 04

Removal of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 79

6

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@A340

SERVICE BULLETIN

**CONF ALL

FR70

FR69

164AR

B

A

A

Z160

F_SB_524094_6_BBAA_01_00

Figure A-GBBAA - Sheet 01

Installation of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 80

6

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@A340

SERVICE BULLETIN

**CONF ALL

2

NEW 

POTABLE WATER

FR69

FR70

STGR50RH

B

SERVICE DOOR

164AR

C

E

F E

F

L

K

NOTE:

01 OPTIONAL SOLUTION NOT SHOWN

01

TYPICAL

F_SB_524094_6_BBAA_02_02

Figure A-GBBAA - Sheet 02

Installation of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 81

6

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@A340

SERVICE BULLETIN

**CONF ALL

226.0 mm

(8.90 in)

D

35

32

30

D

FWD 3.5 mm 

(0.14 in)

35

C

34

32

30

E

02

NOTE:

02 USE EXISTING RIVET HOLES

03 04 03 04

03 APPLY SEALANT (MAT.NO.06AAA1)

04 APPLY COATING (MAT.NO.04QAB2)

FWD

34

03 04 03 04

B

B

B B

A A

A

A

F_SB_524094_6_BBAA_03_03

Figure A-GBBAA - Sheet 03

Installation of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 82

6

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@A340

SERVICE BULLETIN

**CONF ALL

2

26

28

22

20

24

F

G

07

07 USE IF NECESSARY FOR ADJUSTMENT

08

08 TORQUE VALUE = 8.2 Nm TO 10.6 Nm

(72.58 lbf.in TO 93.82 lbf.in)

(4 POS)

(4 POS)

(4 POS)

16

14

12

09

09 TORQUE VALUE = 3.7 Nm TO 4.8 Nm

(32.75 lbf.in TO 42.48 lbf.in)

24

06 HINGE SHOWN IN CLOSED POSITION

05

NOTE:

05 MAKE SURE THAT THE CONTOUR OF THE STRUCTURE

06

AND THE HINGES ARE LEVEL AND THERE ARE NO STEPS.

C

C

C C

F_SB_524094_6_BBAA_04_02

Figure A-GBBAA - Sheet 04

Installation of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 83

6

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@A340

SERVICE BULLETIN

**CONF ALL

NOTE:

50

52

50

54

54

G 10

H

H

J

6.8 mm DIA

(0.27 in)

54

50

54

50

50

52

03 04

03 APPLY SEALANT (MAT.NO.06AAA1)

04 APPLY COATING (MAT.NO.04QAB2)

03 04 03 04

D D

E E

D D

E E

10 APPLY SEALANT (MAT.NO.06AAB1)

F_SB_524094_6_BBAA_05_03

Figure A-GBBAA - Sheet 05

Installation of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 84

6

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@A340

SERVICE BULLETIN

**CONF ALL

54

52 52

J FWD

39° 39°

12

14

(10)

14

8

2

K

2 60

L FWD OUTSIDE PANEL DOOR

= =

= =

F_SB_524094_6_BBAA_06_01

Figure A-GBBAA - Sheet 06

Installation of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 85

6

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@A340

SERVICE BULLETIN

**CONF ALL

FR70

FR69

164AR

B

A

A

Z160

F_SB_524094_6_BCAA_01_00

Figure A-GBCAA - Sheet 01

Adjustment of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 86

6

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@A340

SERVICE BULLETIN

**CONF ALL

FR69

FR70

STGR50RH

B

02

03

02

03

NOTE:

01 OPTIONAL SOLUTION NOT SHOWN

01

TYPICAL

A

A

A

A

B

B

B

B

C

C

APPLY RELEASE AGENT (MAT.NO. 14DBB1) 

APPLY SEALANT (MAT.NO. 06AAB1)

B

B

A

A

C

F_SB_524094_6_BCAA_02_02

Figure A-GBCAA - Sheet 02

Adjustment of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 87

6

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@A340

SERVICE BULLETIN

**CONF ALL

6.5 mm

(0.26 in)

04

2

164AR

A A

6.5 mm

(0.26 in)

2

SECURE WITH LOCK WIRE (MAT. NO.14QDB1)

NOTE:

04

B B

05

05 TORQUE VALUE = 4.0 Nm TO 6.0 Nm (35.40 lbf.in TO 53.10 lbf.in)

164AR

F_SB_524094_6_BCAA_03_03

Figure A-GBCAA - Sheet 03

Adjustment of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 88

6

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@A340

SERVICE BULLETIN

**CONF ALL

NOTE:

2

2

0.8 mm +/− 0.5 mm

(0.031 in +/− 0.020 in) 06

07

B B

C

164AR

164AR

07 ADJUST THE POTABLE WATER SERVICE DOOR, SO THAT A CIRCUMFERENTIAL GAP IS ACHIEVED

08 ADJUST ON INSTALLATION

06 ADJUST THE POTABLE WATER SERVICE DOOR AS NECESSARY

09 08

09 SECURE WITH THREADLOCKING ADHESIVE (MAT.NO.05BAE1)

F_SB_524094_6_BCAA_04_01

Figure A-GBCAA - Sheet 04

Adjustment of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 89

6

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@A340

SERVICE BULLETIN

**CONF ALL

FR70

FR69

164AR

A

B

A

Z160

F_SB_524094_6_BDAA_01_00

Figure A-GBDAA - Sheet 01

Additional work - Modification of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 90

6

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@A340

SERVICE BULLETIN

**CONF ALL

(2)

POTABLE WATER

FR69

FR70

STGR50RH

B

SERVICE DOOR

164AR

C D

F_SB_524094_6_BDAA_02_00

Figure A-GBDAA - Sheet 02

Additional work - Modification of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 91

6

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@A340

SERVICE BULLETIN

**CONF ALL

C

D

BEFORE

AFTER

(4)

(3)

6

(3)

F_SB_524094_6_BDAA_03_00

Figure A-GBDAA - Sheet 03

Additional work - Modification of the potable water service panel access door

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 92

6

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@A340

SERVICE BULLETIN

**CONF ALL

FR70

FR69

164AR

A

B

A

Z160

F_SB_524094_6_BEAA_01_00

Figure A-GBEAA - Sheet 01

Additional work - Application of the sealant

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 93

6

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@A340

SERVICE BULLETIN

**CONF ALL

FR69

FR70

STGR50RH

B

TYPICAL

C

C

A

A

A

A A

A

F_SB_524094_6_BEAA_02_00

Figure A-GBEAA - Sheet 02

Additional work - Application of the sealant

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 94

6

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@A340

SERVICE BULLETIN

**CONF ALL

NOTE:

01 APPLY SEALANT (MAT.NO.06AAA1)

02 APPLY COATING (MAT.NO.04QAB2)

01 02 01 02

A A

01 02 01 02

C

C

B B

C

C C B B

01 02

01 02 01 02

01 02

F_SB_524094_6_BEAA_03_00

Figure A-GBEAA - Sheet 03

Additional work - Application of the sealant

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 95

6

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@A340

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 96

6

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@A340

SERVICE BULLETIN

Appendix 01 - Elapsed Time Assumption

**CONF ALL

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−52−4094

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

01

02

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

01

: 02 : IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

SB ELAPSED TIME

(HOURS)

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

13.50

12.00

STEPS

0.50 0.50

0 1 5 10

REIDENTIFY THE POTABLE WATER SERVICE PANEL

RESTORE THE AIRCRAFT SURFACE PROTECTION

TEST

PER

1

234 6789 11

GET ACCESS

REMOVE THE POTABLE WATER SERVICE DOOR

REMOVE THE FITTINGS AND THE ANCHOR NUTS

INSTALL THE BONDING LEAD

ADJUST THE NEW POTABLE WATER SERVICE DOOR

CLOSE−UP

INSTALL THE PLACARD

INSTALL THE NEW ANCHOR NUTS

INSTALL THE NEW POTABLE WATER 

INSTALL THE NEW FITTING

2.50 2.50 1

0.50 0.50 1

1.00 0.50 2

0.50 0.50 1

2.00 1.00 2

0.25 0.25 1

0.25 0.25 1

0.75 0.75 1

0.50 0.50 1

0.25 0.25 1

1.25 1.25 1

2.50 2.50 1

INSTALL THE NEW HINGES 0.50 0.50 1

SERVICE PANEL ACCESS DOOR

12

THIS CHART IS ONLY A PROPOSAL.

NOTES:

0.25 0.25 1

MODIFY THE NEW POTABLE WATER 

SERVICE PANEL ACCESS DOOR

F_SB_524094_6_GAAA_01_03

Figure A-GGAAA - Sheet 01

Gantt chart

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 1

6

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@A340

SERVICE BULLETIN

Appendix 01 - Elapsed Time Assumption

This Page Intentionally Left Blank

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 2

6

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

SERVICE BULLETIN

Appendix 02 - Status of the aircraft after accomplishment of the Service Bulletin A340-52-4094

**CONF ALL

MOD Config.001 Config.002

201938D50379 X -

201939D59871 X -

201938D50416 - X

203344D50725 X X

203563D50740 X X

NOTE: X is used for the modifications embodied on aircraft after accomplishment of the Service

Bulletin A340-52-4094.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 1

6

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

SERVICE BULLETIN

REPORTING SHEET

TITLE: DOORS-SERVICE DOORS-MODIFICATION OF LATCHING MECHANISM

OF POTABLE WATER SERVICE PANEL

MODIFICATION No.: 201938D50416 201938D50379 201939D59871 203344D50725 203563D50740

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: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 1

6

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@A340

SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

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

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

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

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Apr 27/12 SERVICE BULLETIN No.: A340-52-4094

REVISION No.: 01 - Apr 25/14 Page: 1

6

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