# @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



# MANDATORYMANDATORYMANDATORY 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

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# @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

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# @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

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# @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

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# @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. 

# MANDATORYMANDATORYMANDATORY 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

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# @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

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# @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

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# @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

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# @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



# MANDATORYMANDATORYMANDATORY 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

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# @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

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# @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

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# @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

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# @A340-500/600 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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# @A340-500/600 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 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

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# @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 6

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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 6

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# @A340-500/600 SERVICE BULLETIN

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# @A340-500/600 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 REVISION No.: 02 - Aug 03/11 Page: 11 6

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# @A340-500/600 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 6

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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 6

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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 acccessdoor 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 6

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# @A340-500/600 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 acccessdoor 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 acccessdoor 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 6

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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 REVISION No.: 02 - Aug 03/11 Page: 16 6

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# @A340-500/600 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 6

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# @A340-500/600 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 6

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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 REVISION No.: 02 - Aug 03/11 Page: 19 6

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# @A340-500/600 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 REVISION No.: 02 - Aug 03/11 Page: 20 6

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# @A340-500/600 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 6

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# @A340-500/600 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 6

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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 DATE: Jul 31/06 SERVICE BULLETIN No.: A340-53-5031 REVISION No.: 02 - Aug 03/11 Page: 23 6

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# @A340-500/600 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 6

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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 6

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# @A340-500/600 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
AH

FOR DIMENSIONS REFER TO SHEET 8 C

B

F_SB_535031_6_BAAA_03_00 

## AFTER

**NOTE:** STGR44LH STGR43LH

STGR45

**FWD** 

## C

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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# @A340-500/600 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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# @A340-500/600 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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# @A340-500/600 SERVICE BULLETIN

**CONF 001

STGR43LH

STGR44LH

2

**FWD** 

## G

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

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# @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)

ALTERNATIVE WASHER 06 **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 D01 5
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 4.790mm 4.730mm 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

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# @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

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# @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

**FWD** 

## C 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:** TRANSFER DRILL FROM ANGLE, ITEM 16, TO STRINGER 01 (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**

**H G** 

**FWD** 

## E 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

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

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

03 03

04 16

15

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

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

## 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

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

# @A340-500/600 SERVICE BULLETIN

**CONF 002 thru 003

STGR43LH

STGR44LH 16

15

**FWD** 

## G

SEAL AROUND THE EDGES 05 KEEP DRAIN HOLE FREE FROM SEALANT 06 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

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

# @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)

ALTERNATIVE WASHER 08 **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

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

# @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

TRANSITION FIT 5.113mm (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 6

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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 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: 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.