@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: 53

TITLE: FUSELAGE - CONE/REAR FUSELAGE - INSTALL DRAIN MAST TO

IMPROVE DRAINAGE AFT OF PRESSURE BULKHEAD

MODIFICATION No.: 54637D44815

This page transmits Revision No.02 of Service Bulletin No.A340-53-5031

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No.02 issued to update the Compliance to Mandatory, update the Evaluation table and

Industry Support paragraph.

This Service Bulletin has been validated on A340-600 aircraft MSN 0360.

CHANGES

SUMMARY

MODIFICATIONS Minor editorial or document structure change N

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

Minor editorial or document structure change N

GENERAL EVALUATION Minor editorial or document structure change N

MATERIAL PRICE INFORMATION Minor editorial or document structure change N

Minor editorial or document structure change N

Minor editorial or document structure change N

EFFECTIVITY Minor editorial or document structure change N

CONCURRENT REQUIREMENTS Minor editorial or document structure change N

REFERENCES / REPERCUSSIONS Minor editorial or document structure change N

NATURE OF THE WORK Minor editorial or document structure change N

MANPOWER Minor editorial or document structure change N

Minor editorial or document structure change N

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 1

6

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Minor editorial or document structure change N

APPENDICES Minor editorial or document structure change N

Fig. A-GSAAA Minor editorial or document structure change N

Fig. A-GSAAA Sheet 01 Minor editorial or document structure change N

PLANNING INFORMATION

EFFECTIVITY Minor editorial or document structure change N

Configuration definition Minor editorial or document structure change N

CONF 001 Minor editorial or document structure change N

CONF 002 Minor editorial or document structure change N

CONF 003 Minor editorial or document structure change N

Material Effectivity Minor editorial or document structure change N

Minor editorial or document structure change N

Minor editorial or document structure change N

Minor editorial or document structure change N

CONCURRENT REQUIREMENTS Minor editorial or document structure change N

REASON Minor editorial or document structure change N

History Minor editorial or document structure change N

Objective/Action Minor editorial or document structure change N

Advantages Minor editorial or document structure change N

Operational/Maintenance

Consequences

Minor editorial or document structure change N

DESCRIPTION Minor editorial or document structure change N

COMPLIANCE Minor editorial or document structure change N

Classification Minor editorial or document structure change N

Accomplishment Timescale Minor editorial or document structure change N

APPROVAL Minor editorial or document structure change N

Minor editorial or document structure change N

MANPOWER Minor editorial or document structure change N

Minor editorial or document structure change N

Minor editorial or document structure change N

Minor editorial or document structure change N

WEIGHT AND BALANCE Minor editorial or document structure change N

Minor editorial or document structure change N

Minor editorial or document structure change N

Minor editorial or document structure change N

ELECTRICAL LOAD DATA Minor editorial or document structure change N

REFERENCES Minor editorial or document structure change N

Minor editorial or document structure change N

Minor editorial or document structure change N

Minor editorial or document structure change N

PUBLICATION AFFECTED Minor editorial or document structure change N

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 2

6

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Minor editorial or document structure change N

INTERCHANGEABILITY/MIXABILITY Minor editorial or document structure change N

SPARES Minor editorial or document structure change N

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY Minor editorial or document structure change N

Procurement Addresses Minor editorial or document structure change N

Price and Availability Minor editorial or document structure change N

INDUSTRY SUPPORT INFORMATION Minor editorial or document structure change N

LIST OF COMPONENTS Minor editorial or document structure change N

Kit 535031D01R02 Minor editorial or document structure change N

Kit 535031D02R04 Minor editorial or document structure change N

LIST OF MATERIALS - OPERATOR

SUPPLIED

Minor editorial or document structure change N

Consumable Materials Minor editorial or document structure change N

Consumable CMLD01 Minor editorial or document structure change N

Components Minor editorial or document structure change N

Equipment Minor editorial or document structure change N

PARTS TO BE RE-IDENTIFIED BY

OPERATOR

Minor editorial or document structure change N

TOOLING Minor editorial or document structure change N

ACCOMPLISHMENT INSTRUCTIONS

TASK 535031- 831-849-001-Modification Minor editorial or document structure change N

Task associated data - 001 Minor editorial or document structure change N

Task associated data - 002 Minor editorial or document structure change N

Task associated data - 003 Minor editorial or document structure change N

Subtask 535031-839-202-001 Minor editorial or document structure change N

Subtask 535031-910-201-001 Minor editorial or document structure change N

Subtask 535031-839-202-001 Minor editorial or document structure change N

Subtask 535031-910-201-001 Minor editorial or document structure change N

Subtask 535031-839-202-001 Minor editorial or document structure change N

Subtask 535031-910-201-001 Minor editorial or document structure change N

Subtask 535031-941-201-001 Minor editorial or document structure change N

Subtask 535031-941-201-001 Minor editorial or document structure change N

Subtask 535031-941-201-001 Minor editorial or document structure change N

Subtask 535031-831-206-001 Minor editorial or document structure change N

Subtask 535031-831-206-002 Minor editorial or document structure change N

Subtask 535031-831-206-002 Minor editorial or document structure change N

Subtask 535031-942-201-001 Minor editorial or document structure change N

Subtask 535031-942-201-001 Minor editorial or document structure change N

Subtask 535031-942-201-001 Minor editorial or document structure change N

Fig. A-GBAAA Minor editorial or document structure change N

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 3

6

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Fig. A-GBAAA Sheet 01 Minor editorial or document structure change N

Fig. A-GBAAA Sheet 02 Minor editorial or document structure change N

Fig. A-GBAAA Sheet 03 Minor editorial or document structure change N

Fig. A-GBAAA Sheet 04 Minor editorial or document structure change N

Fig. A-GBAAA Sheet 05 Minor editorial or document structure change N

Fig. A-GBAAA Sheet 06 Minor editorial or document structure change N

Fig. A-GBAAA Sheet 07 Minor editorial or document structure change N

Fig. A-GBAAA Sheet 08 Minor editorial or document structure change N

Fig. A-GBAAB Minor editorial or document structure change N

Fig. A-GBAAB Sheet 01 Minor editorial or document structure change N

Fig. A-GBAAB Sheet 02 Minor editorial or document structure change N

Fig. A-GBAAB Sheet 03 Minor editorial or document structure change N

Fig. A-GBAAB Sheet 04 Minor editorial or document structure change N

Fig. A-GBAAB Sheet 05 Minor editorial or document structure change N

Fig. A-GBAAB Sheet 06 Minor editorial or document structure change N

Fig. A-GBAAB Sheet 07 Minor editorial or document structure change N

Fig. A-GBAAB Sheet 08 Minor editorial or document structure change N

FILLING INSTRUCTIONS

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

Replace the complete document.

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

HISTORY OF PREVIOUS REVISIONS

NOTE: This is only applicable for Revision No. 02 and subsequent. If information is required for

Revisions issued previous to this, please check your copies of Revision Transmittal

Sheets or contact AIRBUS.

REVISION SEQUENCE

ORIGINAL: Jul 31/06

REVISION No. : 02 - Aug 03/11

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 4

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: 53

TITLE: FUSELAGE - CONE/REAR FUSELAGE - INSTALL DRAIN MAST TO

IMPROVE DRAINAGE AFT OF PRESSURE BULKHEAD

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 54637D44815

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

Due to reports about water trapped in the bilge area of the fuselage, aft of the rear pressure bulkhead

at Frame (FR)80/82, an improved drainage principle has been designed in section 19 for the complete

Long Range program.

Following fire risk analysis in case of flammable fluid leak in section 19 area, this Service Bulletin

is rendered Mandatory in the frame of Special Federal Aviation Regulation (SFAR) Number 88

requirements.

This Service Bulletin details the installation of a drain mast between FR80/82 and FR83 between

STGR43 and STGR44.

The accomplishment of this Service Bulletin will permit drainage of the bilge area of the fuselage behind

rear pressure bulkhead in flight.

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

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 1

6

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

SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 535031D01R02 1 1,400.00 Plates, drain mast, hardware

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 535031D02R04 1 1,490.00 Plates, angle, drain mast, hardware

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 535031D02R04 1 1,490.00 Plates, angle, drain mast, hardware

EFFECTIVITY

**CONF ALL

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

CES CHH DLH ETD IBE QAF QTR SAA SIA TAM THA UAE VIR

NOTE: This Service Bulletin has been validated on A340-600 aircraft MSN 0360.

NOTE: This drain mast has been embodied in production by Modification 54636D44796.

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 2

6

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

SERVICE BULLETIN

SUMMARY

LIFE LIMIT None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 535031-831-849-001: Modification

TOTAL MANHOURS 4.25

ELAPSED TIME (HOURS) 4.25

**CONF 002

Task 535031-831-849-001: Modification

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

**CONF 003

Task 535031-831-849-001: Modification

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

APPENDICES

**CONF ALL

None

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 3

6

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

SERVICE BULLETIN

SUMMARY

**CONF ALL

Z310

A

STGR43LH

STGR44LH

FR83

FR80

FR91

A

NEW DRAIN MAST

F_SB_535031_6_SAAA_01_01

Figure A-GSAAA - Sheet 01

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 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: 53

TITLE: FUSELAGE - CONE/REAR FUSELAGE - INSTALL DRAIN MAST TO

IMPROVE DRAINAGE AFT OF PRESSURE BULKHEAD

MODIFICATION No.: 54637D44815

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

340-541 340-642

(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 0761-0766

(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.

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 1

6

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

SERVICE BULLETIN

OPERATOR MSN

CES 0468 0488 0514 0577 0586

CHH 0436 0453 0475

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

ETD 0748 0757 0761

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

QAF 0495

QTR 0715 0740 0766

SAA 0410 0417 0426 0531 0534 0547 0557 0626 0630

SIA 0478 0492 0499 0560 0563

TAM 0445 0464

THA 0624 0628 0677 0681 0689 0698 0710 0719

UAE 0394 0457 0471 0485 0520 0572 0608 0611 0685 0694

VIR 0371 0376 0383 0391 0416 0449 0575 0615 0622 0639 0706 0723

0736 0753 0764 0765

(4) Configuration by MSN

MSN CONFIGURATION

0371 001

0376 0383 0391 0410 0416 0417 0426 0431 0436 0440 0449

0453 0460 0468 0475 0482 0488 0514 0517 0523 0531 0534

0537 0540 0543 0547 0557 0566 0569 0575 0577 0580 0583

0586 0601 0604 0606 0615 0617 0619 0622 0626 0630 0639

0672 0677 0681 0689 0702 0706 0710 0715 0719 0723 0727

0736 0740 0744 0753 0762 0763 0764 0765 0766

002

0394 0445 0457 0464 0471 0478 0485 0492 0495 0499 0520

0560 0563 0572 0608 0611 0624 0628 0685 0694 0698 0748

0757 0761

003

(5) Configuration definition

**CONF 001

Config. 001 is valid for MSN371 given in the effectivity of this Service Bulletin as a

standard configuration.

**CONF 002

Config. 002 is valid for all A340-600 aircraft given in the effectivity of this Service Bulletin

as a standard configuration.

**CONF 003

Config. 003 is valid for all A340-500 aircraft given in the effectivity of this Service Bulletin

as a standard configuration.

(6) Material Effectivity

**CONF 001

MATERIAL QTY PER A/C SEE NOTES

Kit 535031D01R02 1

Consumable CMLD01 1

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 2

6

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

SERVICE BULLETIN

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Kit 535031D02R04 1

Consumable CMLD01 1

**CONF 003

MATERIAL QTY PER A/C SEE NOTES

Kit 535031D02R04 1

Consumable CMLD01 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Due to reports about water trapped in the bilge area of the fuselage, aft of the rear

pressure bulkhead at Frame (FR)80/82, an improved drainage principle has been

designed in section 19 for the complete Long Range program.

Following fire risk analysis in case of flammable fluid leak in section 19 area, this

Service Bulletin is rendered Mandatory in the frame of Special Federal Aviation

Regulation (SFAR) Number 88 requirements.

(2) Objective/Action

This Service Bulletin details the installation of a drain mast between FR80/82 and FR83

between STGR43 and STGR44.

(3) Advantages

The accomplishment of this Service Bulletin will permit drainage of the bilge area of the

fuselage behind rear pressure bulkhead in flight.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 535031-831-849-001: Modification

(1) Install the drain mast between FR80 and FR83

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 3

6

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

SERVICE BULLETIN

**CONF 002

Task 535031-831-849-001: Modification

(1) Install the drain mast between FR80 and FR83

**CONF 003

Task 535031-831-849-001: Modification

(1) Install the drain mast between FR80 and FR83

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

It is recommended to perform this Service Bulletin within 24 month after revision 02 has

been issued.

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 thresholds of 24

month after revision 02 has been issued but reference should be made to the AD for

confirmation of the mandated accomplishment timescale.

F. APPROVAL

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

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.

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 4

6

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

**CONF 001

Task 535031-831-849-001: Modification

Get Access 0.75

On Aircraft

Install the drain mast between FR80 and FR83 2.50

Close-Up 1.00

TOTAL MANHOURS 4.25

ELAPSED TIME (HOURS) 4.25

**CONF 002

Task 535031-831-849-001: Modification

Get Access 0.75

On Aircraft

Install the drain mast between FR80 and FR83 2.75

Close-Up 1.00

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

**CONF 003

Task 535031-831-849-001: Modification

Get Access 0.75

On Aircraft

Install the drain mast between FR80 and FR83 2.75

Close-Up 1.00

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

**CONF ALL

H. WEIGHT AND BALANCE

**CONF 001

Manufacturers Empty Weight +0.395 KG (+0.8708 LB)

Effect on Balance +28.244 KGM (+204.288 LB.FT )

**CONF 002

Manufacturers Empty Weight +0.490 KG (+1.0802 LB)

Effect on Balance +35.009 KGM (+253.220 LB.FT )

**CONF 003

Manufacturers Empty Weight +0.490 KG (+1.0802 LB)

Effect on Balance +31.365 KGM (+226.863 LB.FT )

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 5

6

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SERVICE BULLETIN

**CONF ALL

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-31-53 12-34-24 52-41-00

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

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-12 51-42-11 51-43-00

51-44-11 51-46-11

**CONF 002

Aircraft Maintenance Manual (AMM) 06-31-53 12-34-24 52-41-00

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

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-12 51-42-11 51-43-00

51-44-11 51-46-11

**CONF 003

Aircraft Maintenance Manual (AMM) 06-31-53 12-34-24 52-41-00

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

Standards Manual (SM)

Structural Repair Manual (SRM) 51-23-12 51-42-11 51-43-00

51-44-11 51-46-11

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 53-00-00 53-50-00 53-59-61

Illustrated Parts Catalog (IPC) 53-59-04

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 6

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@A340-500/600

SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 535031D01R02

Kit 535031D02R04

Customers with aircraft shown in the

effectivity of this Service Bulletin should send

a purchase order to AIRBUS. Quote the

number of this Service Bulletin. The address

is:

AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet:

http://spares.airbus.com

For ordering modification kits by fax: +49 40

50 76 25 90

For ordering of single spares by fax: +49 40

50 76 40 13

(2) Price and Availability

Kit 535031D01R02

Cost 1,400.00 USD

Availability 120 calendar days from receipt of order

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

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

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

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

at the issue date of the Service Bulletin.

Kit 535031D02R04

Cost 1,490.00 USD

Availability 120 calendar days from receipt of order

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

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

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

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

at the issue date of the Service Bulletin.

B. INDUSTRY SUPPORT INFORMATION

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

no charge.

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 7

6

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

SERVICE BULLETIN

For the accomplishment of this Service Bulletin, AIRBUS will credit the manhours indicated in

this Service Bulletin at the agreed in-house warranty labor rate for claims received not later

than 90 days after completion of the last affected aircraft of your fleet.

C. LIST OF COMPONENTS

Kit 535031D01R02

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

NOTES

1 MS21061L4 4 NUT

2 F5357584720000 1 PLATE

5 EN6069AD3-06 8 RIVET

6 EN6080D6-09 3 RIVET

7 DAN6-6-5X 2 PIN

8 DAN11-6X 2 COLLAR

9 EN6069D6-07 4 RIVET

10 F5357108000000 1 MAST

11 F5357609620000 4 BOLT

12 NAS1149C0463R 8 WASHER

13 F5357609520000 1 PLATE

14 AA55487-4 4 PIN

17 NAS1149C0432R 8 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.

Kit 535031D02R04

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

NOTES

1 MS21061L4 4 NUT

7 DAN6-6-5X 3 PIN

8 DAN11-6X 3 COLLAR

10 F5357108000000 1 MAST

11 F5357609620000 4 BOLT

12 NAS1149C0463R 8 WASHER

13 F5357609520000 1 PLATE

14 AA55487-4 4 PIN

15 F5357584820000 1 PLATE

16 F5357584920000 1 ANGLE

17 NAS1149C0432R 8 WASHER

20 EN6069KE6-07 7 RIVET

21 EN6101AD3-06 8 RIVET

22 DAN5-5-3 3 PIN

23 NSA5075-5 3 COLLAR

26 EN6069KE6-09 4 RIVET

27 DAN8-6-5X 1 PIN

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 8

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@A340-500/600

SERVICE BULLETIN

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

NOTES

28 DAN12-6X 1 COLLAR

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

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

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

to part number relationship.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Putty, Zinc Chromategeneral

Purpose

05-002 As required

Corrosion Inhibiting Fillet

Consistency

09-016 As required

Cleaning agent 11-026 As required

Flexible Polyurethane 16-021 As required

Lint-Free Cotton Cloth 19-003 As required

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 9

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SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 10

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 535031-831-849-001 - Modification

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS:

PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS.

REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER

CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

Task Associated Data

**CONF 001

Zone

310

Access

Door 312AR

Manpower

TOTAL MANHOURS 4.25

ELAPSED TIME (HOURS) 4.25

**CONF 002

Zone

310

Access

Door 312AR

Manpower

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

**CONF 003

Zone

310

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

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SERVICE BULLETIN

Access

Door 312AR

Manpower

TOTAL MANHOURS 4.50

ELAPSED TIME (HOURS) 4.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 535031-839-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

(2) Subtask 535031-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

Structural Repair Manual (SRM) 51-23-12

51-42-11

51-43-00

51-44-11

51-46-11

(a) For the identification of frames (Refer to AMM 06-31-53, Page Block 001).

(b) For the removal and installation of fasteners (Refer to SRM 51-42-11).

(c) For hole and drill data (Refer to SRM 51-44-11).

(d) For coutersinking the holes (Refer to SRM 51-46-11).

(e) For information about alternative fasteners (Refer to SRM 51-43-00).

(f) For information about the application of corrosion preventive (Refer to SRM

51-23-12).

**CONF 002

(1) Subtask 535031-839-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 12

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@A340-500/600

SERVICE BULLETIN

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

Service Bulletin.

(2) Subtask 535031-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

Structural Repair Manual (SRM) 51-23-12

51-42-11

51-43-00

51-44-11

51-46-11

(a) For the identification of frames (Refer to AMM 06-31-53, Page Block 001).

(b) For the removal and installation of fasteners (Refer to SRM 51-42-11).

(c) For hole and drill data (Refer to SRM 51-44-11).

(d) For coutersinking the holes (Refer to SRM 51-46-11).

(e) For information about alternative fasteners (Refer to SRM 51-43-00).

(f) For information about the application of corrosion preventive (Refer to SRM

51-23-12).

**CONF 003

(1) Subtask 535031-839-202-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

(2) Subtask 535031-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

Structural Repair Manual (SRM) 51-23-12

51-42-11

51-43-00

51-44-11

51-46-11

(a) For the identification of frames (Refer to AMM 06-31-53, Page Block 001).

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 13

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@A340-500/600

SERVICE BULLETIN

(b) For the removal and installation of fasteners (Refer to SRM 51-42-11).

(c) For hole and drill data (Refer to SRM 51-44-11).

(d) For coutersinking the holes (Refer to SRM 51-46-11).

(e) For information about alternative fasteners (Refer to SRM 51-43-00).

(f) For information about the application of corrosion preventive (Refer to SRM

51-23-12).

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 535031-941-201-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002

52-41-00, Page Block 001

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

12-34-24-869-002).

(b) Put access platform(s) in position under the access door 312AR and under the

working area at Zone 310.

(c) Open the acccess door 312AR (Refer to AMM 52-41-00, Page Block 001).

**CONF 002

(1) Subtask 535031-941-201-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002

52-41-00, Page Block 001

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 14

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SERVICE BULLETIN

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

12-34-24-869-002).

(b) Put access platform(s) in position under the access door 312AR and under the

working area at Zone 310.

(c) Open the acccess door 312AR (Refer to AMM 52-41-00, Page Block 001).

**CONF 003

(1) Subtask 535031-941-201-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002

52-41-00, Page Block 001

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

12-34-24-869-002).

(b) Put access platform(s) in position under the access door 312AR and under the

working area at Zone 310.

(c) Open the acccess door 312AR (Refer to AMM 52-41-00, Page Block 001).

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 535031-831-206-001 - Install the drain mast between FR80 and FR83

Manpower Resources

Manhours 2.50

Minimum number of person 1

Subtask elapsed time 2.50

Skills AIRFRAME

Material necessary to do the job

Kit 535031D01R02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 MS21061L4 4 NUT

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 15

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@A340-500/600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 F5357584720000 1 PLATE

5 EN6069AD3-06 8 RIVET

6 EN6080D6-09 3 RIVET

7 DAN6-6-5X 2 PIN

8 DAN11-6X 2 COLLAR

9 EN6069D6-07 4 RIVET

10 F5357108000000 1 MAST

11 F5357609620000 4 BOLT

12 NAS1149C0463R 8 WASHER

13 F5357609520000 1 PLATE

14 AA55487-4 4 PIN

17 NAS1149C0432R 8 WASHER

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Putty, Zinc Chromate

general Purpose

05-002 As required

Corrosion Inhibiting Fillet

Consistency

09-016 As required

Cleaning agent 11-026 As required

Flexible Polyurethane 16-021 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-GBAAA

Installation of the Drain Mast

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

(a) Remove the rivets , item (6), as shown on Fig. A-GBAAA Sheet 01, View A and

Fig. A-GBAAA Sheet 02, View B.

(b) Clean the work area, with:

Cleaning agent 11-026 As required

Lint-Free Cotton

Cloth

19-003 As required

(c) Drill the holes into the outer skin as shown on Fig. A-GBAAA Sheet 03, View C and

Fig. A-GBAAA Sheet 08. Use a 2.4mm (0.094in.) drill.

(d) Temporarily attach the plate, item 2, as shown on Fig. A-GBAAA Sheet 05, View F.

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

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SERVICE BULLETIN

(e) Transfer drill the holes from the outer skin to the aligned plate, item 2.

(f) Drill the holes to the final diameter as shown on Fig. A-GBAAA Sheet 03, View C

and Fig. A-GBAAA Sheet 08.

(g) Countersink the holes at the bottom outer skin.

(h) Remove the plate, item 2, and deburr the holes.

(i) To the drilled holes, apply:

Putty, Zinc

Chromate general

Purpose

05-002 As required

Flexible

Polyurethane

16-021 As required

(j) To the plate, item 2, and to the outer skin install as shown on Fig. A-GBAAA Sheet

04, View D:

4 Nut MS21061L4 Item 1

8 Rivet EN6069AD3-06 Item 5

(k) To the plate, item 2, apply:

Corrosion Inhibiting

Fillet Consistency

09-016 As required

(l) Install as shown on Fig. A-GBAAA Sheet 06, View G and Fig. A-GBAAA Sheet 08:

1 Plate F5357584720000 Item 2

4 Rivet EN6069D6-07 Item 9

3 Rivet EN6080D6-09 Item 6

2 Pin-Rivet DAN6-6-5X Item 7

2 Collar DAN11-6X Item 8

Wet install the rivets, with:

Corrosion Inhibiting

Fillet Consistency

09-016 As required

(m) To the drain mast, item 10, apply:

Corrosion Inhibiting

Fillet Consistency

09-016 As required

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 17

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SERVICE BULLETIN

(n) Install as shown on Fig. A-GBAAA Sheet 07:

1 Mast Assy-Drain F5357108000000 Item 10

1 Plate-Perforated F5357609520000 Item 13

4 Bolt F5357609620000 Item 11

8 Washer NAS1149C0463R Item 12

or

8 Washer NAS1149C0432R Item 17

4 Pin-Lock AA55487-4 Item 14

(o) Apply a bead of sealant to the edges of the plate, item 2 and the drain mast, item

10, with:

Corrosion Inhibiting

Fillet Consistency

09-016 As required

(p) To the rivets, collars, and the sealing beads, apply

Flexible

Polyurethane

16-021 As required

(q) Apply a new paint coat to the sealant bead of the drain mast, item 10, refer to the

aircraft colour code.

**CONF 002

(1) Subtask 535031-831-206-002 - Install the drain mast between FR80 and FR83

Manpower Resources

Manhours 2.75

Minimum number of person 1

Subtask elapsed time 2.75

Skills AIRFRAME

Material necessary to do the job

Kit 535031D02R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 MS21061L4 4 NUT

7 DAN6-6-5X 3 PIN

8 DAN11-6X 3 COLLAR

10 F5357108000000 1 MAST

11 F5357609620000 4 BOLT

12 NAS1149C0463R 8 WASHER

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 18

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@A340-500/600

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

13 F5357609520000 1 PLATE

14 AA55487-4 4 PIN

15 F5357584820000 1 PLATE

16 F5357584920000 1 ANGLE

17 NAS1149C0432R 8 WASHER

20 EN6069KE6-07 7 RIVET

21 EN6101AD3-06 8 RIVET

22 DAN5-5-3 3 PIN

23 NSA5075-5 3 COLLAR

26 EN6069KE6-09 4 RIVET

27 DAN8-6-5X 1 PIN

28 DAN12-6X 1 COLLAR

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Putty, Zinc Chromate

general Purpose

05-002 As required

Corrosion Inhibiting Fillet

Consistency

09-016 As required

Cleaning agent 11-026 As required

Flexible Polyurethane 16-021 As required

Lint-Free Cotton Cloth 19-003 As required

References

Fig. A-GBAAB

Installation of the Drain Mast

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

(a) Remove the rivets , item (26), as shown on Fig. A-GBAAB Sheet 01, View A and

Fig. A-GBAAB Sheet 02, View B.

(b) Clean the working area, with:

Cleaning agent 11-026 As required

Lint-Free Cotton

Cloth

19-003 As required

(c) Drill the holes into the outer skin as shown on Fig. A-GBAAB Sheet 03, View C and

Fig. A-GBAAB Sheet 08. Use a 2.4mm (0.094in.) drill.

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

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SERVICE BULLETIN

(d) Temporarily attach the plate, item 15, as shown on Fig. A-GBAAB Sheet 05, View

F.

(e) Transfer drill the holes from the outer skin to the aligned plate, item 15.

(f) Temporarily attach the angle, item 16, as shown on Fig. A-GBAAB Sheet 05, View

F and transfer drill the holes from the angle to the stringer and to the plate, item 15,

and the outer skin.

(g) Drill the holes to the final diameter as shown on Fig. A-GBAAB Sheet 03, View C

and Fig. A-GBAAB Sheet 08.

(h) Countersink the holes at the bottom outer skin.

(i) Remove the plate, item 15, the angle, item 16, and deburr the holes.

(j) To the drilled holes, apply:

Putty, Zinc

Chromate general

Purpose

05-002 As required

Flexible

Polyurethane

16-021 As required

(k) To the plate, item 15, install as shown on Fig. A-GBAAB Sheet 04:

4 Nut MS21061L4 Item 1

8 Rivet EN6101AD3-06 Item 21

(l) To the plate, item 15 and the angle, item 16, apply:

Corrosion Inhibiting

Fillet Consistency

09-016 As required

(m) Install as shown on Fig. A-GBAAB Sheet 04, View D, Fig. A-GBAAB Sheet 06,

View G and Fig. A-GBAAB Sheet 08:

1 Plate F5357584820000 Item 15

1 Angle-Reinforcement F5357584920000 Item 16

7 Rivet EN6069KE6-07 Item 20

4 Rivet EN6069KE6-09 Item 26

3 Pin-Rivet DAN5-5-3 Item 22

3 Collar NSA5075-5 Item 23

3 Pin-Rivet DAN6-6-5X Item 7

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

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SERVICE BULLETIN

3 Collar DAN11-6X Item 8

1 Pin-Rivet DAN8-6-5X Item 27

1 Collar DAN12-6X Item 28

Wet install the rivets, with:

Corrosion Inhibiting

Fillet Consistency

09-016 As required

(n) To the drain mast, item 10, apply:

Corrosion Inhibiting

Fillet Consistency

09-016 As required

(o) Install as shown on Fig. A-GBAAB Sheet 07:

1 Mast Assy-Drain F5357108000000 Item 10

1 Plate-Perforated F5357609520000 Item 13

4 Bolt F5357609620000 Item 11

8 Washer NAS1149C0463R Item 12

or

8 Washer NAS1149C0432R Item 17

4 Pin-Lock AA55487-4 Item 14

(p) Apply a bead of sealant to the edges of the plate, item 15 and the drain mast, item

10, with:

Corrosion Inhibiting

Fillet Consistency

09-016 As required

(q) To the rivets, collars, and to the sealant beads, apply

Flexible

Polyurethane

16-021 As required

(r) Apply a new paint coat the sealing bead of the drain mast, item 10, refer to the

aircraft colour code.

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 21

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SERVICE BULLETIN

**CONF 003

(1) Subtask 535031-831-206-002 - Install the drain mast between FR80 and FR83

Manpower Resources

Manhours 2.75

Minimum number of person 1

Subtask elapsed time 2.75

Skills AIRFRAME

Material necessary to do the job

Kit 535031D02R04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 MS21061L4 4 NUT

7 DAN6-6-5X 3 PIN

8 DAN11-6X 3 COLLAR

10 F5357108000000 1 MAST

11 F5357609620000 4 BOLT

12 NAS1149C0463R 8 WASHER

13 F5357609520000 1 PLATE

14 AA55487-4 4 PIN

15 F5357584820000 1 PLATE

16 F5357584920000 1 ANGLE

17 NAS1149C0432R 8 WASHER

20 EN6069KE6-07 7 RIVET

21 EN6101AD3-06 8 RIVET

22 DAN5-5-3 3 PIN

23 NSA5075-5 3 COLLAR

26 EN6069KE6-09 4 RIVET

27 DAN8-6-5X 1 PIN

28 DAN12-6X 1 COLLAR

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Putty, Zinc Chromate

general Purpose

05-002 As required

Corrosion Inhibiting Fillet

Consistency

09-016 As required

Cleaning agent 11-026 As required

Flexible Polyurethane 16-021 As required

Lint-Free Cotton Cloth 19-003 As required

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 22

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@A340-500/600

SERVICE BULLETIN

References

Fig. A-GBAAB

Installation of the Drain Mast

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Sheet 06

Sheet 07

Sheet 08

(a) Remove the rivets , item (26), as shown on Fig. A-GBAAB Sheet 01, View A and

Fig. A-GBAAB Sheet 02, View B.

(b) Clean the working area, with:

Cleaning agent 11-026 As required

Lint-Free Cotton

Cloth

19-003 As required

(c) Drill the holes into the outer skin as shown on Fig. A-GBAAB Sheet 03, View C and

Fig. A-GBAAB Sheet 08. Use a 2.4mm (0.094in.) drill.

(d) Temporarily attach the plate, item 15, as shown on Fig. A-GBAAB Sheet 05, View

F.

(e) Transfer drill the holes from the outer skin to the aligned plate, item 15.

(f) Temporarily attach the angle, item 16, as shown on Fig. A-GBAAB Sheet 05, View

F and transfer drill the holes from the angle to the stringer and to the plate, item 15,

and the outer skin.

(g) Drill the holes to the final diameter as shown on Fig. A-GBAAB Sheet 03, View C

and Fig. A-GBAAB Sheet 08.

(h) Countersink the holes at the bottom outer skin.

(i) Remove the plate, item 15, the angle, item 16, and deburr the holes.

(j) To the drilled holes, apply:

Putty, Zinc

Chromate general

Purpose

05-002 As required

Flexible

Polyurethane

16-021 As required

(k) To the plate, item 15, install as shown on Fig. A-GBAAB Sheet 04:

4 Nut MS21061L4 Item 1

8 Rivet EN6101AD3-06 Item 21

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REVISION No.: 02 - Aug 03/11 Page: 23

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SERVICE BULLETIN

(l) To the plate, item 15 and the angle, item 16, apply:

Corrosion Inhibiting

Fillet Consistency

09-016 As required

(m) Install as shown on Fig. A-GBAAB Sheet 04, View D, Fig. A-GBAAB Sheet 06,

View G and Fig. A-GBAAB Sheet 08:

1 Plate F5357584820000 Item 15

1 Angle-Reinforcement F5357584920000 Item 16

7 Rivet EN6069KE6-07 Item 20

4 Rivet EN6069KE6-09 Item 26

3 Pin-Rivet DAN5-5-3 Item 22

3 Collar NSA5075-5 Item 23

3 Pin-Rivet DAN6-6-5X Item 7

3 Collar DAN11-6X Item 8

1 Pin-Rivet DAN8-6-5X Item 27

1 Collar DAN12-6X Item 28

Wet install the rivets, with:

Corrosion Inhibiting

Fillet Consistency

09-016 As required

(n) To the drain mast, item 10, apply:

Corrosion Inhibiting

Fillet Consistency

09-016 As required

(o) Install as shown on Fig. A-GBAAB Sheet 07:

1 Mast Assy-Drain F5357108000000 Item 10

1 Plate-Perforated F5357609520000 Item 13

4 Bolt F5357609620000 Item 11

8 Washer NAS1149C0463R Item 12

or

8 Washer NAS1149C0432R Item 17

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 24

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@A340-500/600

SERVICE BULLETIN

4 Pin-Lock AA55487-4 Item 14

(p) Apply a bead of sealant to the edges of the plate, item 15 and the drain mast, item

10, with:

Corrosion Inhibiting

Fillet Consistency

09-016 As required

(q) To the rivets, collars, and to the sealant beads, apply

Flexible

Polyurethane

16-021 As required

(r) Apply a new paint coat the sealing bead of the drain mast, item 10, refer to the

aircraft colour code.

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF 003

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 535031-942-201-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 52-41-00, Page Block 001

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

equipment.

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 25

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SERVICE BULLETIN

(b) Close the access door 312AR (Refer to AMM 52-41-00, Page Block 001).

(c) Remove the access platform(s).

**CONF 002

(1) Subtask 535031-942-201-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 52-41-00, Page Block 001

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

equipment.

(b) Close the access door 312AR (Refer to AMM 52-41-00, Page Block 001).

(c) Remove the access platform(s).

**CONF 003

(1) Subtask 535031-942-201-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

310 Access Door 312AR

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 52-41-00, Page Block 001

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

equipment.

(b) Close the access door 312AR (Refer to AMM 52-41-00, Page Block 001).

(c) Remove the access platform(s).

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 26

6

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@A340-500/600

SERVICE BULLETIN

**CONF 001

Z310

A

STGR43LH

STGR44LH

FR83

FR80

FR91

A

B

F_SB_535031_6_BAAA_01_01

Figure A-GBAAA - Sheet 01

Installation of the Drain Mast

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 27

6

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@A340-500/600

SERVICE BULLETIN

**CONF 001

STGR44LH

STGR43LH

STGR45

FR80

B

BEFORE

C

D

(6)

F_SB_535031_6_BAAA_02_01

Figure A-GBAAA - Sheet 02

Installation of the Drain Mast

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 28

6

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@A340-500/600

SERVICE BULLETIN

**CONF 001

J

E

K

G

A

A

A

F

D

A

H

FOR DIMENSIONS REFER TO SHEET 8

C

B

F_SB_535031_6_BAAA_03_00

AFTER

NOTE:

STGR44LH

STGR43LH

STGR45

C FWD

Figure A-GBAAA - Sheet 03

Installation of the Drain Mast

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 29

6

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SERVICE BULLETIN

**CONF 001

AFTER

D

STGR44LH

STGR43LH

FR80

(2 POS)

(2 POS)

(2 POS)

(2 POS)

5

1

2

1

5

5

5

1

1

FWD

5°

E

E

F

G H

1

2

F_SB_535031_6_BAAA_04_01

Figure A-GBAAA - Sheet 04

Installation of the Drain Mast

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 30

6

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SERVICE BULLETIN

**CONF 001

STGR43LH

STGR44LH

NOTE:

01

02

TRANSFER DRILL FROM PLATE, ITEM 2, TO THE OUTER SKIN

02

FWD

TRANSFER DRILL FROM THE OUTER SKIN TO PLATE, ITEM 2

F

2

01

01

54.0 mm

(2.13 in)

63.0 mm

(2.48 in)

F_SB_535031_6_BAAA_05_01

Figure A-GBAAA - Sheet 05

Installation of the Drain Mast

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 31

6

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SERVICE BULLETIN

**CONF 001

STGR43LH

STGR44LH

2

G FWD

03 SEAL AROUND THE EDGES

04 KEEP DRAIN HOLE FREE FROM SEALANT

03 04

F_SB_535031_6_BAAA_06_01

05

05 WET INSTALL PLATE, ITEM 2, WITH MAT.NO. 09−016.

NOTE:

Figure A-GBAAA - Sheet 06

Installation of the Drain Mast

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 32

6

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

SERVICE BULLETIN

**CONF 001

AFTER

STGR44LH

STGR43LH

FR80

14

12

13

10

12

11

(4 POS)

(4 POS)

(4 POS)

(4 POS)

H

17

(4 POS)

17

(4 POS)

06 ALTERNATIVE WASHER

NOTE:

06

06

F_SB_535031_6_BAAA_07_01

Figure A-GBAAA - Sheet 07

Installation of the Drain Mast

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 33

6

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@A340-500/600

SERVICE BULLETIN

**CONF 001

DIMENSIONS

A

mm (in.)

B

C

D

E

F

G

H

J

K

24.3

28.0

0.957

1.102

45.8 TO 46.2

53.3 TO 53.7 2.098 TO 2.114

54.0 2.126

63.0 2.480

105.7 TO 106.1 4.161 TO 4.177

1.803 TO 1.819

8.0 DIA 0.315 DIA

P/N DESCRIPTION

MIN MAX

ITEM KIT HOLE

SYMBOL REMARKS

RIVET

HOLE DIAMETER

COLLAR

5 D01

6

7

8

9

DAN6−6−5X

D01

D01

D01

RIVET

PIN

RIVET

5.113mm 5.152mm

(0.2013 in.) (0.2028 in.)

TRANSITION FIT

FIRST OVERSIZE

2.350mm

(0.0925 in.)

2.410mm NOMINAL SIZE

NOMINAL SIZE

NOMINAL SIZE (0.1862 in.) (0.1886 in.)

4.730mm

(0.0949 in.)

(0.1862 in.) (0.1886 in.)

4.790mm

4.730mm 4.790mm

EN6069AD3−06

EN6080D6−09

DAN11−6X

EN6069D6−07

16.5 DIA 0.650 DIA

18.9 0.744

F_SB_535031_6_BAAA_08_00

Figure A-GBAAA - Sheet 08

Installation of the Drain Mast

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 34

6

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

SERVICE BULLETIN

**CONF 002 thru 003

Z310

A

STGR43LH

STGR44LH

FR83

FR80

FR91

A

B

F_SB_535031_6_BAAB_01_01

Figure A-GBAAB - Sheet 01

Installation of the Drain Mast

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 35

6

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

SERVICE BULLETIN

**CONF 002 thru 003

STGR44LH

STGR43LH

STGR45

FR80

B

BEFORE

C

D

(26)

F_SB_535031_6_BAAB_02_01

Figure A-GBAAB - Sheet 02

Installation of the Drain Mast

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 36

6

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

SERVICE BULLETIN

**CONF 002 thru 003

FOR DIMENSIONS REFER TO SHEET 8

AFTER

NOTE:

STGR44LH

STGR43LH

C FWD

E

A

A

F

D

A

G

H

A

J

D

B

C

F_SB_535031_6_BAAB_03_00

Figure A-GBAAB - Sheet 03

Installation of the Drain Mast

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 37

6

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

SERVICE BULLETIN

**CONF 002 thru 003

AFTER

D

STGR44LH

STGR43LH

FR80

NOTE:

01 TRANSFER DRILL FROM ANGLE, ITEM 16, TO STRINGER

(2 POS)

21

(2 POS)

21

(2 POS)

21 (3 POS)

22

(2 POS)

21

1

1

1

1

16

15

(3 POS)

23

01

15°

E

F

G H

E FWD

1

15

F_SB_535031_6_BAAB_04_01

Figure A-GBAAB - Sheet 04

Installation of the Drain Mast

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 38

6

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@A340-500/600

SERVICE BULLETIN

**CONF 002 thru 003

F_SB_535031_6_BAAB_05_00

21.8 mm

(0.858 in)

10.5 mm TO 13.5 mm

(0.413 in TO 0.531 in)

STGR43LH

STGR44LH

NOTE:

02 TRANSFER DRILL FROM THE ANGLE, ITEM 16, TO THE PLATE, ITEM 15 AND INTO THE OUTER SKIN

02

03

03

04

16

15

03 TRANSFER DRILL FROM THE PLATE, ITEM 15, TO THE OUTER SKIN

FWD

04 TRANSFER DRILL FROM THE OUTER SKIN, TO THE PLATE, ITEM 15.

F

Figure A-GBAAB - Sheet 05

Installation of the Drain Mast

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 39

6

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@A340-500/600

SERVICE BULLETIN

**CONF 002 thru 003

STGR43LH

STGR44LH

16

15

G FWD

05 SEAL AROUND THE EDGES

06 KEEP DRAIN HOLE FREE FROM SEALANT

05 06

07 WET INSTALL PLATE, ITEM 15, AND ANGLE, ITEM 16, WITH MAT.NO. 09−016. 

NOTE:

F_SB_535031_6_BAAB_06_01

07

07

Figure A-GBAAB - Sheet 06

Installation of the Drain Mast

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 40

6

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@A340-500/600

SERVICE BULLETIN

**CONF 002 thru 003

AFTER

STGR44LH

STGR43LH

FR80

13

10

H

14

12

12

11

(4 POS)

(4 POS)

(4 POS)

(4 POS)

17

(4 POS)

17

(4 POS)

08 ALTERNATIVE WASHER

NOTE:

08

08

F_SB_535031_6_BAAB_07_01

Figure A-GBAAB - Sheet 07

Installation of the Drain Mast

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 41

6

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@A340-500/600

SERVICE BULLETIN

**CONF 002 thru 003

F_SB_535031_6_BAAB_08_00

DIMENSIONS

A

mm (in.)

B

C

D

E

F

G

H

J

24.3

28.0

0.957

1.102

45.8 TO 46.2

53.3 TO 53.7 2.098 TO 2.114

1.803 TO 1.819

8.0 DIA 0.315 DIA

P/N DESCRIPTION

MIN MAX

ITEM KIT HOLE

SYMBOL REMARKS

RIVET

HOLE DIAMETER

COLLAR

RIVET

PIN

16.5 DIA 0.650 DIA

18.9 0.744

69.0 2.717

105.7 TO 106.1 4.161 TO 4.177

COLLAR

PIN

D02

D02

D02

D02

TRANSITION FIT

NOMINAL SIZE

TRANSITION FIT

4.125mm

(0.1624 in.)

4.160mm

(0.1638 in.)

NOMINAL SIZE

NOMINAL SIZE

4.730mm

(0.1862 in.)

4.790mm

(0.1886 in.)

2.350mm

(0.0925 in.)

2.410mm

(0.0949 in.)

NSA5075−5

RIVET D02 NOMINAL SIZE 4.730mm

(0.1862 in.)

4.790mm

(0.1886 in.) EN6069KE6−09

EN6069KE6−07

EN601AD3−06

D02

COLLAR

PIN

5.113mm

(0.2013 in.) (0.2028 in.)

5.152 mm

FIRST OVERSIZE

5.113mm TRANSITION FIT

(0.2013 in.) (0.2028 in.)

5.152 mm

FIRST OVERSIZE

DAN5−5−3

DAN6−6−5X

DAN11−6X

DAN8−6−5X

DAN12−6X

20

21

22

23

7

8

26

27

28

Figure A-GBAAB - Sheet 08

Installation of the Drain Mast

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 42

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@A340-500/600

SERVICE BULLETIN

REPORTING SHEET

TITLE: FUSELAGE - CONE/REAR FUSELAGE - INSTALL DRAIN MAST TO

IMPROVE DRAINAGE AFT OF PRESSURE BULKHEAD

MODIFICATION No.: 54637D44815

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: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 1

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

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

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

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

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031

REVISION No.: 02 - Aug 03/11 Page: 1

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