@A340-500/600

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 52

TITLE: DOORS-SERVICE DOORS-MODIFICATION OF LATCHING MECHANISM

OF POTABLE WATER SERVICE PANEL

MODIFICATION No.: 201938D50415 203344D50725 203563D50740

This page transmits Revision No.01 of Service Bulletin No.A340-52-5019

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, the bonding lead 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

EFFECTIVITY OPERATOR LIST UPDATED R

REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE

UPDATED

R

MANPOWER MANPOWER UPDATED R

Fig. A-GSAAA

Fig. A-GSAAA Sheet 01 SHEET UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Material Effectivity 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

WEIGHT AND BALANCE WEIGHT AND BALANCE UPDATED R

Minor editorial or document structure change R

REFERENCES REFERENCED DOCUMENTATION UPDATED R

PUBLICATION AFFECTED PUBLICATIONS AFFECTED UPDATED R

INTERCHANGEABILITY/MIXABILITY 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 525019D01R02 PART MATERIAL SET UPDATED

MATERIAL SET LABEL UPDATED

PART NUMBER UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

KEYWORD UPDATED

R

LIST OF MATERIALS - OPERATOR

SUPPLIED

Consumable Materials

Consumable CMLD10 CONSUMABLE MATERIAL SET UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

R

Components COMPONENTS UPDATED R

Component COMPD02 PART MATERIAL SET ADDED N

PARTS TO BE RE-IDENTIFIED BY

OPERATOR

PARTS TO BE RE-IDENTIFIED BY OPERATOR

UPDATED

R

Reidentified part set REIDD06 PART MATERIAL SET ADDED N

ACCOMPLISHMENT INSTRUCTIONS

TASK 525019- 831-848-001-Modification TASK SOLUTION UPDATED

NOTE UPDATED

R

Task associated data - 001 MAN HOURS UPDATED

ELAPSED TIME UPDATED

R

Subtask 525019-910-201-001 SUBTASK SOLUTION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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@A340-500/600

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 525019-941-201-001 SUBTASK SOLUTION UPDATED R

Subtask 525019-831-201-002 SUBTASK SOLUTION ADDED N

Subtask 525019-020-201-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

ITEM NUMBER UPDATED

PART NUMBER DESCRIPTION UPDATED

R

Subtask 525019-420-201-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

FIGURE REFERENCE UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 525019-420-202-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 525019-420-203-001 SUBTASK SOLUTION UPDATED

PART NUMBER UPDATED

FIGURE REFERENCE UPDATED

MATERIAL LIST UPDATED

R

Subtask 525019-420-204-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

REFERENCED DOCUMENTATION UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 525019-420-205-001 SUBTASK SOLUTION UPDATED

QUANTITY UPDATED

PART NUMBER UPDATED

ITEM NUMBER UPDATED

KEYWORD UPDATED

CONSUMABLE UPDATED

REFERENCED DOCUMENTATION UPDATED

PART NUMBER DESCRIPTION UPDATED

MATERIAL LIST UPDATED

REFERENCES UPDATED

R

Subtask 525019-820-201-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

QUANTITY UPDATED

FIGURE REFERENCE UPDATED

REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

MATERIAL LIST UPDATED

R

Subtask 525019-916-201-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

Subtask 525019-420-206-001 SUBTASK SOLUTION UPDATED

CONSUMABLE UPDATED

MATERIAL LIST UPDATED

R

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Subtask 525019-700-201-001 SUBTASK SOLUTION UPDATED R

Subtask 525019-942-201-001 SUBTASK SOLUTION UPDATED R

TASK 525019- 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

Subtask 525019-910-202-001 SUBTASK SOLUTION ADDED N

Subtask 525019-839-202-001 SUBTASK SOLUTION ADDED N

Subtask 525019-941-202-001 SUBTASK SOLUTION ADDED N

Subtask 525019-831-202-001 SUBTASK SOLUTION ADDED N

Subtask 525019-960-202-001 SUBTASK SOLUTION ADDED N

Subtask 525019-831-203-001 SUBTASK SOLUTION ADDED N

Subtask 525019-700-202-001 SUBTASK SOLUTION ADDED N

Subtask 525019-942-202-001 SUBTASK SOLUTION ADDED N

Fig. A-GBAAA

Fig. A-GBAAA Sheet 02 SHEET UPDATED R

Fig. A-GBAAA Sheet 03 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-GBBAA Sheet 06 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

Fig. A-GBEAA Sheet 03 SHEET ADDED N

Fig. A-GBEAA Sheet 04 SHEET ADDED N

Appendix 01 - Elapsed Time Assumption

Fig. A-GGAAA

Fig. A-GGAAA Sheet 01 SHEET UPDATED R

FILLING INSTRUCTIONS

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

Replace the complete document.

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

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

HISTORY OF PREVIOUS REVISIONS

No previous revision

REVISION SEQUENCE

ORIGINAL: May 29/12

REVISION No. : 01 - Apr 25/14

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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

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 201938D50415 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 154BR 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 A340-52-5011 was issued to inspect the access door 154BR and

171AL. The Modification Service Bulletin A340-52-5010 was issued as the final repair solution to the

Inspection Service Bulletin A340-52-5011. Further occurrences of access door 154BR lost during flight

have shown that the Modification Service Bulletin A340-52-5010 is not the definitive final repair solution

for this access door. Therefore, this mandatory Modification Service Bulletin, A340-52-5019, is issued

as the final repair solution for the access door 154BR. 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: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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

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

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 525019D01R02 1 15,280.00 Door, attachment parts

Component COMPD02 See SB Stud-adjusting

EFFECTIVITY

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

06U 25R 36V 70U 72W AHY AIB CES CHH DLH ETD HFM HFY

IBE QAF QTR SAA TAM THA UAE VIR

CONCURRENT REQUIREMENTS

None

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

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

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@A340-500/600

SERVICE BULLETIN

SUMMARY

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 525019-831-848-001: Modification

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

Task 525019-831-849-001: Modification - ADDITIONAL WORK for aircraft modified by the

original issue

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

APPENDICES

Appendix 01 - Elapsed Time Assumption

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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

SERVICE BULLETIN

SUMMARY

**CONF ALL

A

NEW 

POTABLE WATER

FR63

FR64

STGR51RH

B

SERVICE DOOR

B

FR64

FR63

154BR

154BR

A

Z150

F_SB_525019_6_SAAA_01_04

Figure A-GSAAA - Sheet 01

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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

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.: 201938D50415 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

340-541 340-542 340-642

(2) Effectivity by MSN

0371 0376 0383 0391 0394 0410 0416-0417 0426 0431 0436 0440 0445 0449 0453

0457 0460 0464 0468 0471 0475 0478 0482 0485 0488 0492 0495 0499 0514 0517

0520 0523 0531 0534 0537 0540 0543 0547 0557 0560 0563 0566 0569 0572 0575

0577 0580 0583 0586 0601 0604 0606 0608 0611 0615 0617 0619 0622 0624 0626

0628 0630 0639 0672 0677 0681 0685 0689 0694 0698 0702 0706 0710 0715 0719

0723 0727 0736 0740 0744 0748 0753 0757 0761-0768 0771 0775 0779 0783 0787

0790 0794 0798 0804 0812 0829 0837 0846 0848 0870 0886 0894 0897 0902 0910

0912 0917 0924 0929 0933 0953 0960 0972 0981 0987 0993 1005 1017 1030 1040

1079 1091 1102 1122

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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@A340-500/600

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

06U 1091 1102

25R 0924

36V 0391 0416

70U 0902

72W 0917

AHY 0779 0886 0894

AIB 0478 0492 0499 0560 0563

CES 0468 0488 0514 0577 0586

CHH 0436 0453 0475

DLH 0482 0517 0523 0537 0540 0543 0566 0569 0580 0583 0762 0763

0767 0771 0790 0794 0812 0846 0848 0897 0972 0981 0987 1005

ETD 0748 0757 0761 0783 0829 0837 0870 0929 0933 1030 1040

HFM 0383

HFY 0910 0912

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

0960 0993 1017 1079 1122

QAF 0495

QTR 0715 0740 0766 0798

SAA 0410 0417 0426 0531 0534 0547 0557 0626 0630

TAM 0445 0464

THA 0624 0628 0677 0681 0689 0698 0710 0719 0775 0953

UAE 0394 0457 0471 0485 0520 0572 0608 0611 0685 0694

VIR 0371 0376 0449 0575 0615 0622 0639 0706 0723 0736 0753 0764

0765 0768 0787 0804

(4) Configuration by MSN

MSN CONFIGURATION

0371 0376 0383 0391 0394 0410 0416 0417 0426 0431 0436

0440 0445 0449 0453 0457 0460 0464 0468 0471 0475 0478

0482 0485 0488 0492 0495 0499 0514 0517 0520 0523 0531

0534 0537 0540 0543 0547 0557 0560 0563 0566 0569 0572

0575 0577 0580 0583 0586 0601 0604 0606 0608 0611 0615

0617 0619 0622 0624 0626 0628 0630 0639 0672 0677 0681

0685 0689 0694 0698 0702 0706 0710 0715 0719 0723 0727

0736 0740 0744 0748 0753 0757 0761 0762 0763 0764 0765

0766 0767 0768 0771 0775 0779 0783 0787 0790 0794 0798

0804 0812 0829 0837 0846 0848 0870 0886 0894 0897 0902

0910 0912 0917 0924 0929 0933 0953 0960 0972 0981 0987

0993 1005 1017 1030 1040 1079 1091 1102 1122

001

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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@A340-500/600

SERVICE BULLETIN

(5) Configuration definition

**CONF 001

Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Kit 525019D01R02 1

Component COMPD02 As required (1)

Reidentified part set REIDD05 1

Reidentified part set REIDD06 As required (2)

Consumable CMLD10 As required

NOTE (1): The matset Comp 525019D02 is applicable only for operators which

have already matset Kit 525019D01R00 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 525019D06 is to be used only for operators which

have already matset Kit 525019D01R00 on stock or which have already

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

the additional work.

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

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

154BR 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 A340-52-5011 was issued to inspect the access door

154BR and 171AL. The Modification Service Bulletin A340-52-5010 was issued as the

final repair solution to the Inspection Service Bulletin A340-52-5011. Further occurrences

of access door 154BR lost during flight have shown that the Modification Service Bulletin

A340-52-5010 is not the definitive final repair solution for this access door. Therefore,

this mandatory Modification Service Bulletin, A340-52-5019, is issued as the final repair

solution for the access door 154BR. The loss of this door is classified to be a potential

unsafe condition.

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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

SERVICE BULLETIN

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

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 525019-831-848-001: Modification

(1) Modify the potable water service panel access door PN F5348654400600

(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 F5348654400800

(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 525019-831-849-001: Modification - ADDITIONAL WORK for aircraft modified by the

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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

SERVICE BULLETIN

original issue

(1) Modify the potable water service panel access door PN F5348654400600

(2) Replace the bonding lead

(3) Apply sealant to the modified areas

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.

G. MANPOWER

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

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

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

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

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

included.

Task 525019-831-848-001: 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

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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

SERVICE BULLETIN

Task 525019-831-848-001: Modification

Install the new hinges 0.50

Install the new potable water service panel access

door PN F5348654400800

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

F5348654400600

0.25

Tests 1.25

Close-Up 2.50

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

Task 525019-831-849-001: 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

F5348654400600

0.25

Replace the bonding lead 0.50

Apply sealant to the modified areas 1.00

Tests 1.25

Close-Up 2.50

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

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 .

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.

A340-500 A340-600

Manufacturers Empty Weight +0.264 KG +0.582 LB +0.264 KG +0.582 LB

Effect on Balance +14.435 KGM +104.444

LBF.FT +16.398 KGM +118.647LBF.FT

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

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SERVICE BULLETIN

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

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) 20-42-12 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

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 52-42-13

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

Maintenance Planning Document (MPD) 524000-04-1

Structural Repair Manual (SRM) 52-42-11

L. INTERCHANGEABILITY/MIXABILITY

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Door Assy F5348654400400 F5348654400800 03 Not

Applicable

Panel F5348652320400 F5348633820000 03 Not

Applicable

Door Assy F5348654400600 F5348654400800 03 Not

Applicable

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

Common Support Data Dictionary (CSDD), Chapter 2.

M. SPARES

None

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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This Page Intentionally Left Blank

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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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 525019D01R02 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 COMPD02 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 525019D01R02

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.

Component COMPD02

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

purchased by a spares purchase order.

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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SERVICE BULLETIN

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 525019D01R02

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

NOTES

2 F5348654400800 1 DOOR (2) F5348654400400 03

8 NAS1100-3-7 2 SCREW

10 E0091-10-250NN 1 LEAD

11 E0126-10B 0.25 (ME) TUBING

12 NAS1291C3M 10 NUT

14 NAS1149C0332R 12 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.

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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SERVICE BULLETIN

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

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 COMPD02

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

NOTES

6 A9249715920200 1 STUD

8 NAS1100-3-7 2 SCREW

10 E0091-10-250NN 1 LEAD

11 E0126-10B 0.25 (ME) TUBING

12 NAS1291C3M 2 NUT

14 NAS1149C0332R 4 WASHER

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: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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SERVICE BULLETIN

NOTE: The matset Comp 525019D02 is applicable only for operators which

have already matset Kit 525019D01R00 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

F5348633820000 PANEL F5348652320400

Reidentified part set REIDD06

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348654400800 DOOR F5348654400600

NOTE: The part set Reid 525019D06 is to be used only for operators which

have already matset Kit 525019D01R00 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: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 525019-831-848-001 - 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.

Task Associated Data

Zone

160

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SERVICE BULLETIN

Manpower

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 12.00

A. GENERAL

(1) Subtask 525019-910-201-001 - 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).

(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.

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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(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 525019-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 525019-941-201-001 - 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.

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- 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 154BR.

(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.

C. PROCEDURE

(1) Subtask 525019-831-201-002 - Modify the potable water service panel access door

PN F5348654400600

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 COMPD02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

6 A9249715920200 1 STUD

NOTE: The matset Comp 525019D02 is applicable only for operators which

have already matset Kit 525019D01R00 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 REIDD06

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348654400800 DOOR F5348654400600

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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SERVICE BULLETIN

NOTE: The part set Reid 525019D06 is to be used only for operators which

have already matset Kit 525019D01R00 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 525019D01R00 on stock,

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

525019D01R00, following the subsequent worksteps.

Otherwise continue with SUBTASK 525019-020-201 001 Remove the

potable water service panel access door .

(a) If you have the matset Kit 525019D01 with revision 00, then on bench, remove

from the Door Assy, PN F5348654400600, 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 F5348654400600, 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

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

1 Door Assy F5348654400600

becomes

1 Door Assy F5348654400800

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

(2) Subtask 525019-020-201-001 - Remove the potable water service panel access

door

Work Zones and Access Panels

Zone Access/Work location

160

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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:

2 Nut Item (12) Discard

4 Washer Item (14) Discard

2 Screw Item (8) Discard

1 Bonding lead Item (10) Discard

1 Tubing-Heat-Shrinkable Item (11) Discard

(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 F5348654400400 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

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(3) Subtask 525019-020-202-001 - 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

(4) Subtask 525019-420-201-001 - 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

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Material necessary to do the job

Kit 525019D01R02

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.

(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 and 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.

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(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.

(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

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SERVICE BULLETIN

(5) Subtask 525019-420-202-001 - 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 525019D01R02

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

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

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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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 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).

(6) Subtask 525019-420-203-001 - Install the new potable water service panel access

door PN F5348654400800

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 525019D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 F5348654400800 1 DOOR

12 NAS1291C3M 8 NUT

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 23

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SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

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 F5348654400800 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.

(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 525019-420-204-001 - 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

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 24

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SERVICE BULLETIN

Material necessary to do the job

Kit 525019D01R02

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.

(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.

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

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SERVICE BULLETIN

(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.

(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

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 26

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SERVICE BULLETIN

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 525019-420-205-001 - 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 525019D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

8 NAS1100-3-7 2 SCREW

10 E0091-10-250NN 1 LEAD

11 E0126-10B 0.25 (ME) TUBING

12 NAS1291C3M 2 NUT

14 NAS1149C0332R 4 WASHER

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 27

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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) 20-42-12

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:

0.25 (ME) Tubing-Heat-Shrinkable E0126-10B Item 11

together with

1 Lead Bonding E0091-10-250NN Item 10

and attach with

2 Screw NAS1100-3-7 Item 8

4 Washer NAS1149C0332R Item 14

2 Nut NAS1291C3M Item 12

(c) Shrink the Tubing-Heat-Shrinkable, item 11, in accordance with ESPM 20-42-12.

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 28

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SERVICE BULLETIN

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

Varnish-- Electrical

Bonding Structure

04TMB2 As required

(9) Subtask 525019-930-201-001 - 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

F5348633820000 PANEL F5348652320400

Reidentify the potable water service panel:

1 Panel F5348652320400

becomes

1 Panel F5348633820000

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

(10) Subtask 525019-820-201-001 - 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: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 29

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SERVICE BULLETIN

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

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 30

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SERVICE BULLETIN

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.

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 31

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SERVICE BULLETIN

(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 525019-916-201-001 - 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

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 32

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SERVICE BULLETIN

(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 525019-420-206-001 - 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 525019D01R02

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: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 33

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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

D. TEST

(1) Subtask 525019-700-201-001 - 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.

E. CLOSE-UP

(1) Subtask 525019-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

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

Task 53-00-00-400-804

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 34

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SERVICE BULLETIN

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

equipment.

(b) Install the 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 154BR.

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

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

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SERVICE BULLETIN

Task 525019-831-849-001 - Modification - ADDITIONAL WORK for aircraft modified by the

original issue

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.

Task Associated Data

Manpower

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

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SERVICE BULLETIN

A. GENERAL

(1) Subtask 525019-910-202-001 - 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 525019-839-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 525019-941-202-001 - 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

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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@A340-500/600

SERVICE BULLETIN

(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 154BR.

(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.

C. PROCEDURE

(1) Subtask 525019-831-202-001 - Modify the potable water service panel access door

PN F5348654400600

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 COMPD02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

6 A9249715920200 1 STUD

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

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@A340-500/600

SERVICE BULLETIN

NOTE: The matset Comp 525019D02 is applicable only for operators which

have already matset Kit 525019D01R00 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 REIDD06

ITEM NEW PART N ̊ KEYWORD ITEM OLD PART N ̊ SEE

NOTES

F5348654400800 DOOR F5348654400600

NOTE: The part set Reid 525019D06 is to be used only for operators which

have already matset Kit 525019D01R00 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

Fig. A-GBDAA

Additional work - Modification of the

potable water service panel access door

Sheet 01

Sheet 02

Sheet 03

Fig. A-GBCAA

Adjustment of the potable water service

panel access door

Sheet 01

Sheet 02

Sheet 03

Sheet 04

(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 F5348654400600, 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

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

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@A340-500/600

SERVICE BULLETIN

(d) Install to the Door Assy, PN F5348654400600, 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 F5348654400600

becomes

1 Door Assy F5348654400800

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

(2) Subtask 525019-960-202-001 - Replace the bonding lead

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Component COMPD02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

8 NAS1100-3-7 2 SCREW

10 E0091-10-250NN 1 LEAD

11 E0126-10B 0.25 (ME) TUBING

12 NAS1291C3M 2 NUT

14 NAS1149C0332R 4 WASHER

NOTE: The matset Comp 525019D02 is applicable only for operators which

have already matset Kit 525019D01R00 on stock or which have already

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

the additional work.

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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@A340-500/600

SERVICE BULLETIN

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

shall be ordered as necessary through the given channel.

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) 20-42-12

20-51-20

Fig. A-GBEAA

Additional work - Replacement of the

bonding lead

Sheet 01

Sheet 02

Sheet 03

Sheet 04

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

Fig. A-GBEAA Sheet 04, View D remove:

2 Nut Item (12) Discard

4 Washer Item (14) Discard

2 Screw Item (8) Discard

1 Bonding lead Item (10) Discard

1 Tubing-Heat-Shrinkable Item (11) Discard

(b) Clean the bonding points, as shown on AMM Task 20-28-00-912-802 and as given

in ESPM 20-51-20, with:

Non Aqueous

Cleaner-General

08BAA9 As required

and

Textile-Lint Free

Cotton

14SBA1 As required

(c) Install, as shown on Fig. A-GBEAA Sheet 01, Fig. A-GBEAA Sheet 02 and Fig. AGBEAA Sheet 04, View E:

0.25 (ME) Tubing-Heat-Shrinkable E0126-10B Item 11

together with

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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@A340-500/600

SERVICE BULLETIN

1 Lead Bonding E0091-10-250NN Item 10

and attach with

2 Screw NAS1100-3-7 Item 8

4 Washer NAS1149C0332R Item 14

2 Nut NAS1291C3M Item 12

(d) Shrink the Tubing-Heat-Shrinkable, item 11, in accordance with ESPM 20-42-12.

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

Varnish-- Electrical

Bonding Structure

04TMB2 As required

(3) Subtask 525019-831-203-001 - 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 - Replacement of the

bonding lead

Sheet 01

Sheet 02

Sheet 03

Sheet 04

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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@A340-500/600

SERVICE BULLETIN

(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

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

D. TEST

(1) Subtask 525019-700-202-001 - 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.

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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@A340-500/600

SERVICE BULLETIN

E. CLOSE-UP

(1) Subtask 525019-942-202-001 - 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 154BR.

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

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

B

A

FR64

FR63

A

154BR

Z150

F_SB_525019_6_BAAA_01_01

Figure A-GBAAA - Sheet 01

Removal of the potable water service panel access door

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

(2)

POTABLE WATER

FR63

FR64

STGR51RH

B

SERVICE DOOR

F

F

D

D

154BR

C

F_SB_525019_6_BAAA_02_02

Figure A-GBAAA - Sheet 02

Removal of the potable water service panel access door

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

(12)

(14)

(14)

(8)

(2)

D

(2)

(26)

(28)

(22)

(20)

(24)

(4 POS)

(4 POS)

(4 POS)

(16)

(14)

(12)

E

(8)

(14)

(14)

(12)

C

(10)

(11)

F_SB_525019_6_BAAA_03_01

Figure A-GBAAA - Sheet 03

Removal of the potable water service panel access door

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

(34)

(30)

(32)

(52)

E (50)

F

F_SB_525019_6_BAAA_04_00

Figure A-GBAAA - Sheet 04

Removal of the potable water service panel access door

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

B

A

FR64

FR63

A

154BR

Z150

F_SB_525019_6_BBAA_01_01

Figure A-GBBAA - Sheet 01

Installation of the potable water service panel access door

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 50

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

2

NEW 

POTABLE WATER

B

SERVICE DOOR

C

E

F E

F

L

TYPICAL

FR63

FR64

STGR51RH

154BR

K

F_SB_525019_6_BBAA_02_03

Figure A-GBBAA - Sheet 02

Installation of the potable water service panel access door

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 51

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

35

32

30

D

FWD 3.5 mm 

(0.14 in)

35

224.2 mm

(8.83 in)

D

C

34

32

30

E

01

NOTE:

01 USE EXISTING RIVET HOLES

02 03 02 03

02 APPLY SEALANT (MAT.NO.06AAA1)

03 APPLY COATING (MAT.NO.04QAB2)

FWD

34

02 03 02 03

A

A

B

B

B B

A A

F_SB_525019_6_BBAA_03_04

Figure A-GBBAA - Sheet 03

Installation of the potable water service panel access door

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

2

26

28

22

20

24

F

G

06

06 USE IF NECESSARY FOR ADJUSTMENT

07

07 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

08

08 TORQUE VALUE = 3.7 Nm TO 4.8 Nm

(32.75 lbf.in TO 42.48 lbf.in)

24

05 HINGE SHOWN IN CLOSED POSITION

04

NOTE:

04 MAKE SURE THAT THE CONTOUR OF THE STRUCTURE

05

AND THE HINGES ARE LEVEL AND THERE ARE NO STEPS.

C C

C

C

F_SB_525019_6_BBAA_04_03

Figure A-GBBAA - Sheet 04

Installation of the potable water service panel access door

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 53

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

NOTE:

50

52

50

54

54

G 09

H

H

J

6.8 mm DIA

(0.27 in)

54

50

54

50

50

52

02 03

02 APPLY SEALANT (MAT.NO.06AAA1)

03 APPLY COATING (MAT.NO.04QAB2)

02 03 02 03

D D

E E

D D

E E

09 APPLY SEALANT (MAT.NO.06AAB1)

F_SB_525019_6_BBAA_05_06

Figure A-GBBAA - Sheet 05

Installation of the potable water service panel access door

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 54

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

54

52 52

J FWD

39° 39°

2

60

L FWD OUTSIDE PANEL DOOR

= =

= =

12

14

10

14

8

2

8

14

14

12

K

11

F_SB_525019_6_BBAA_06_01

Figure A-GBBAA - Sheet 06

Installation of the potable water service panel access door

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 55

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

B

A

FR64

FR63

A

154BR

Z150

F_SB_525019_6_BCAA_01_01

Figure A-GBCAA - Sheet 01

Adjustment of the potable water service panel access door

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 56

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

FR63

FR64

STGR51RH

B

01 APPLY RELEASE AGENT (MAT.NO. 14DBB1) 

02

01

02 APPLY SEALANT (MAT.NO. 06AAB1)

A

A

A

A

NOTE: TYPICAL

B

B

B

B

A

A

B

B

C

C

C

F_SB_525019_6_BCAA_02_03

Figure A-GBCAA - Sheet 02

Adjustment of the potable water service panel access door

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 57

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

6.5 mm

(0.26 in)

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

NOTE:

03

03

2

A A

2

B B

04

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

154BR 6.5 mm

(0.26 in)

154BR

F_SB_525019_6_BCAA_03_02

Figure A-GBCAA - Sheet 03

Adjustment of the potable water service panel access door

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 58

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

2

2

0.8 mm +/− 0.5 mm

(0.031 in +/− 0.020 in) 05

06

C

154BR

154BR

C C

07

NOTE:

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

07 ADJUST ON INSTALLATION

05 ADJUST THE POTABLE WATER SERVICE DOOR AS NECESSARY

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

08

F_SB_525019_6_BCAA_04_00

Figure A-GBCAA - Sheet 04

Adjustment of the potable water service panel access door

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 59

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

B

A

FR64

FR63

A

154BR

Z150

F_SB_525019_6_BDAA_01_00

Figure A-GBDAA - Sheet 01

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

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 60

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

(2)

POTABLE WATER

FR63

FR64

STGR51RH

B

SERVICE DOOR

154BR

C D

F_SB_525019_6_BDAA_02_01

Figure A-GBDAA - Sheet 02

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

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

C

D

(4)

(3)

6

(3)

BEFORE

AFTER

F_SB_525019_6_BDAA_03_00

Figure A-GBDAA - Sheet 03

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

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 62

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

B

A

FR64

FR63

A

154BR

Z150

F_SB_525019_6_BEAA_01_00

Figure A-GBEAA - Sheet 01

Additional work - Replacement of the bonding lead

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

REVISION No.: 01 - Apr 25/14 Page: 63

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

FR63

FR64

STGR51RH

B

TYPICAL

A

A

A

A

A

A

C

D E

F_SB_525019_6_BEAA_02_00

Figure A-GBEAA - Sheet 02

Additional work - Replacement of the bonding lead

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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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_525019_6_BEAA_03_01

Figure A-GBEAA - Sheet 03

Additional work - Replacement of the bonding lead

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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@A340-500/600

SERVICE BULLETIN

**CONF ALL

D

(12)

(14)

(10)

(14)

(8)

(8)

(14)

(14)

(12)

12

14

10

14

8 8

14

14

12

(11)

11

E

BEFORE

AFTER

F_SB_525019_6_BEAA_04_00

Figure A-GBEAA - Sheet 04

Additional work - Replacement of the bonding lead

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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@A340-500/600

SERVICE BULLETIN

Appendix 01 - Elapsed Time Assumption

**CONF ALL

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−52−5019

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

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

01

02

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

01

02

NOTES:

PER

1

:

: IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

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

SERVICE PANEL ACCESS DOOR 0.25 0.25 1

MODIFY THE NEW PORTABLE WATER

F_SB_525019_6_GAAA_01_03

Figure A-GGAAA - Sheet 01

Gantt chart

DATE: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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

SERVICE BULLETIN

REPORTING SHEET

TITLE: DOORS-SERVICE DOORS-MODIFICATION OF LATCHING MECHANISM

OF POTABLE WATER SERVICE PANEL

MODIFICATION No.: 201938D50415 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: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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

SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 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: May 29/12 SERVICE BULLETIN No.: A340-52-5019

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

6

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