# @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 - GENERAL - INSPECTION OF SUSPECTED NON CONFORMING NUTS ASNA2531-4 **CONF ALL MODIFICATIONS None REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES During structural parts assembly on the production line, some nuts were detected cracked. An investigation was immediately launched to determine the affected nut types and the associated batches. AIRBUS and the nut manufacturer, LISI Monadnock, have identified that the affected nut type is ASNA2531-4. These suspected non conforming nuts have been installed in production on aircraft listed in effectivity paragraph. Extensive static, fatigue and corrosion tests have been performed, results from tests and analysis indicated that no immediate maintenance action is required on the affected in-service aircraft. However, as this event impacts a large amount of nuts associated to the primary structure assembly, Airbus requests the replacement of all nuts in order to restore the original design intent. This One Time Inspection Service Bulletin consists in replacing all the suspect nuts with new ones of same type. Accomplishment of this Service Bulletin will restore the aircraft structure to its original design configuration. NOTE: It is suggested to accomplish this service Bulletin during a major servicing because of the time-consuming get access and close-up procedures for the removal and installation of the galleys and the lavatories for example. 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: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 1 5

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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 Component COMPA28 1 See SB ASNA2531-4 Component COMPA31 1 See SB ASNA2531-4 Component COMPA32 1 See SB ASNA2531-4 Component COMPA40 1 See SB ASNA2531-4 Component COMPA41 1 See SB ASNA2531-4 **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPA01 1 See SB ASNA2531-4 Component COMPA02 1 See SB ASNA2531-4 Component COMPA03 1 See SB ASNA2531-4 Component COMPA23 1 See SB ASNA2531-4 Component COMPA28 1 See SB ASNA2531-4 Component COMPA30 1 See SB ASNA2531-4 Component COMPA31 1 See SB ASNA2531-4 Component COMPA33 1 See SB ASNA2531-4 Component COMPA40 1 See SB ASNA2531-4 Component COMPA41 1 See SB ASNA2531-4 **CONF 003 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPA31 1 See SB ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 2 5

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# @A340-500/600
SERVICE BULLETIN SUMMARY **CONF 004 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPA28 1 See SB ASNA2531-4 Component COMPA31 1 See SB ASNA2531-4 Component COMPA34 1 See SB ASNA2531-4 Component COMPA40 1 See SB ASNA2531-4 **CONF 005 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPA02 1 See SB ASNA2531-4 Component COMPA03 1 See SB ASNA2531-4 Component COMPA29 1 See SB ASNA2531-4 Component COMPA31 1 See SB ASNA2531-4 Component COMPA35 1 See SB ASNA2531-4 Component COMPA40 1 See SB ASNA2531-4 **CONF 006 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPA02 1 See SB ASNA2531-4 Component COMPA03 1 See SB ASNA2531-4 Component COMPA29 1 See SB ASNA2531-4 Component COMPA30 1 See SB ASNA2531-4 Component COMPA31 1 See SB ASNA2531-4 Component COMPA36 1 See SB ASNA2531-4 Component COMPA40 1 See SB ASNA2531-4 **CONF 007 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPA02 1 See SB ASNA2531-4 Component COMPA03 1 See SB ASNA2531-4 Component COMPA04 1 See SB ASNA2531-4 Component COMPA05 1 See SB ASNA2531-4 Component COMPA06 1 See SB ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 3 5

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# @A340-500/600
SERVICE BULLETIN SUMMARY
MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPA07 1 See SB ASNA2531-4 Component COMPA08 1 See SB ASNA2531-4 Component COMPA09 1 See SB ASNA2531-4 Component COMPA10 1 See SB ASNA2531-4 Component COMPA11 1 See SB ASNA2531-4 Component COMPA12 1 See SB ASNA2531-4 Component COMPA13 1 See SB ASNA2531-4 Component COMPA14 1 See SB ASNA2531-4 Component COMPA15 1 See SB ASNA2531-4 Component COMPA16 1 See SB ASNA2531-4 Component COMPA17 1 See SB ASNA2531-4 Component COMPA18 1 See SB ASNA2531-4 Component COMPA19 1 See SB ASNA2531-4 Component COMPA20 1 See SB ASNA2531-4 Component COMPA21 1 See SB ASNA2531-4 Component COMPA22 1 See SB ASNA2531-4 Component COMPA24 1 See SB ASNA2531-4 Component COMPA25 1 See SB ASNA2531-4 Component COMPA26 1 See SB ASNA2531-4 Component COMPA27 1 See SB ASNA2531-4 Component COMPA29 1 See SB ASNA2531-4 Component COMPA31 1 See SB ASNA2531-4 Component COMPA37 1 See SB ASNA2531-4 Component COMPA40 1 See SB ASNA2531-4 Component COMPA41 1 See SB ASNA2531-4 Component COMPA42 1 See SB ASNA2531-4 Component COMPA43 1 See SB ASNA2531-4 Component COMPA44 1 See SB ASNA2531-4 Component COMPA45 1 See SB ASNA2531-4 **CONF 008 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPA02 1 See SB ASNA2531-4 Component COMPA03 1 See SB ASNA2531-4 Component COMPA04 1 See SB ASNA2531-4 Component COMPA05 1 See SB ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 4 5

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# @A340-500/600
SERVICE BULLETIN SUMMARY
MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPA06 1 See SB ASNA2531-4 Component COMPA07 1 See SB ASNA2531-4 Component COMPA08 1 See SB ASNA2531-4 Component COMPA09 1 See SB ASNA2531-4 Component COMPA10 1 See SB ASNA2531-4 Component COMPA11 1 See SB ASNA2531-4 Component COMPA12 1 See SB ASNA2531-4 Component COMPA13 1 See SB ASNA2531-4 Component COMPA14 1 See SB ASNA2531-4 Component COMPA15 1 See SB ASNA2531-4 Component COMPA16 1 See SB ASNA2531-4 Component COMPA17 1 See SB ASNA2531-4 Component COMPA18 1 See SB ASNA2531-4 Component COMPA19 1 See SB ASNA2531-4 Component COMPA20 1 See SB ASNA2531-4 Component COMPA21 1 See SB ASNA2531-4 Component COMPA22 1 See SB ASNA2531-4 Component COMPA24 1 See SB ASNA2531-4 Component COMPA25 1 See SB ASNA2531-4 Component COMPA26 1 See SB ASNA2531-4 Component COMPA27 1 See SB ASNA2531-4 Component COMPA29 1 See SB ASNA2531-4 Component COMPA31 1 See SB ASNA2531-4 Component COMPA38 1 See SB ASNA2531-4 Component COMPA39 1 See SB ASNA2531-4 Component COMPA40 1 See SB ASNA2531-4 Component COMPA41 1 See SB ASNA2531-4 Component COMPA42 1 See SB ASNA2531-4 Component COMPA43 1 See SB ASNA2531-4 **CONF 009 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPA19 1 See SB ASNA2531-4 Component COMPA20 1 See SB ASNA2531-4 Component COMPA40 1 See SB ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 5 5

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# @A340-500/600
SERVICE BULLETIN SUMMARY EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :

70U 72W ARA DLH ETD SOR CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO OBRM NO MANPOWER **CONF 001 Task 535056-832-801-001: Inspection TOTAL MANHOURS 183.00 ELAPSED TIME (HOURS) 51.00 **CONF 002 Task 535056-832-801-001: Inspection TOTAL MANHOURS 261.25 ELAPSED TIME (HOURS) 68.0 **CONF 003 Task 535056-832-801-001: Inspection TOTAL MANHOURS 15.50 ELAPSED TIME (HOURS) 9.00

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 6 5

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# @A340-500/600
SERVICE BULLETIN SUMMARY **CONF 004 Task 535056-832-801-001: Inspection TOTAL MANHOURS 155.75 ELAPSED TIME (HOURS) 45.00 **CONF 005 Task 535056-832-801-001: Inspection TOTAL MANHOURS 183.75 ELAPSED TIME (HOURS) 56.00 **CONF 006 Task 535056-832-801-001: Inspection TOTAL MANHOURS 185.50 ELAPSED TIME (HOURS) 56.00 **CONF 007 Task 535056-832-801-001: Inspection TOTAL MANHOURS 1193.00 ELAPSED TIME (HOURS) 378.0 **CONF 008 Task 535056-832-801-001: Inspection TOTAL MANHOURS 1155.50 ELAPSED TIME (HOURS) 377.0 **CONF 009 Task 535056-832-801-001: Inspection TOTAL MANHOURS 180.00 ELAPSED TIME (HOURS) 46.00 APPENDICES **CONF ALL Appendix 01 Inspection Report. Appendix 02 Elapsed Time Assumptions

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 7 5

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# @A340-500/600
SERVICE BULLETIN SUMMARY

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DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 8 5

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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 - GENERAL - INSPECTION OF SUSPECTED NON CONFORMING NUTS ASNA2531-4 MODIFICATION No.: None 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 The equivalent of this Service Bulletin has been accomplished on A340-600 aircraft MSN 0924. (1) Models 340-541 340-542 340-642 (2) Effectivity by MSN 0846 0848 0894 0897 0902 0910 0912 0917 0929 (3) Effectivity by Operator The Operator/MSN relationship is provided for information only and is correct at the time of issue in accordance with the information available to AIRBUS. Any future changes resulting from transfer of an aircraft from one operator to another will not be reflected in this list unless the Service Bulletin is revised for another reason. OPERATOR MSN 70U 0902

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 1 5

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# @A340-500/600
SERVICE BULLETIN

OPERATOR MSN 72W 0917 ARA 0910 0912 DLH 0846 0848 0897 ETD 0929 SOR 0894 (4) Configuration by MSN MSN CONFIGURATION 0846 001 0848 002 0894 003 0897 004 0902 005 0910 006 0912 007 0917 008 0929 009 (5) Configuration definition **CONF 001 The definition of this configuration corresponds to the necessary areas to inspect. These areas result from the investigation performed by Airbus. **CONF 002 The definition of this configuration corresponds to the necessary areas to inspect. These areas result from the investigation performed by Airbus. **CONF 003 The definition of this configuration corresponds to the necessary areas to inspect. These areas result from the investigation performed by Airbus. **CONF 004 The definition of this configuration corresponds to the necessary areas to inspect. These areas result from the investigation performed by Airbus. **CONF 005 The definition of this configuration corresponds to the necessary areas to inspect. These areas result from the investigation performed by Airbus. **CONF 006 The definition of this configuration corresponds to the necessary areas to inspect. These areas result from the investigation performed by Airbus. **CONF 007 The definition of this configuration corresponds to the necessary areas to inspect. These areas result from the investigation performed by Airbus.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 2 5

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# @A340-500/600
SERVICE BULLETIN

**CONF 008 The definition of this configuration corresponds to the necessary areas to inspect. These areas result from the investigation performed by Airbus. **CONF 009 The definition of this configuration corresponds to the necessary areas to inspect. These areas result from the investigation performed by Airbus. (6) Material Effectivity **CONF 001 MATERIAL QTY PER A/C SEE NOTES Component COMPA28 1 Component COMPA31 1 Component COMPA32 1 Component COMPA40 1 Component COMPA41 1 Consumable CMLA01 1 **CONF 002 MATERIAL QTY PER A/C SEE NOTES Component COMPA01 1 Component COMPA02 1 Component COMPA03 1 Component COMPA23 1 Component COMPA28 1 Component COMPA30 1 Component COMPA31 1 Component COMPA33 1 Component COMPA40 1 Component COMPA41 1 Consumable CMLA01 1 **CONF 003 MATERIAL QTY PER A/C SEE NOTES Component COMPA31 1 Consumable CMLA01 1 **CONF 004 MATERIAL QTY PER A/C SEE NOTES Component COMPA28 1 Component COMPA31 1 Component COMPA34 1
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 3 5

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# @A340-500/600
SERVICE BULLETIN

MATERIAL QTY PER A/C SEE NOTES Component COMPA40 1 Consumable CMLA01 1 **CONF 005 MATERIAL QTY PER A/C SEE NOTES Component COMPA02 1 Component COMPA03 1 Component COMPA29 1 Component COMPA31 1 Component COMPA35 1 Component COMPA40 1 Consumable CMLA01 1 **CONF 006 MATERIAL QTY PER A/C SEE NOTES Component COMPA02 1 Component COMPA03 1 Component COMPA29 1 Component COMPA30 1 Component COMPA31 1 Component COMPA36 1 Component COMPA40 1 Consumable CMLA01 1 **CONF 007 MATERIAL QTY PER A/C SEE NOTES Component COMPA02 1 Component COMPA03 1 Component COMPA04 1 Component COMPA05 1 Component COMPA06 1 Component COMPA07 1 Component COMPA08 1 Component COMPA09 1 Component COMPA10 1 Component COMPA11 1 Component COMPA12 1 Component COMPA13 1 Component COMPA14 1 Component COMPA15 1

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 4 5

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# @A340-500/600
SERVICE BULLETIN

MATERIAL QTY PER A/C SEE NOTES Component COMPA16 1 Component COMPA17 1 Component COMPA18 1 Component COMPA19 1 Component COMPA20 1 Component COMPA21 1 Component COMPA22 1 Component COMPA24 1 Component COMPA25 1 Component COMPA26 1 Component COMPA27 1 Component COMPA29 1 Component COMPA31 1 Component COMPA37 1 Component COMPA40 1 Component COMPA41 1 Component COMPA42 1 Component COMPA43 1 Component COMPA44 1 Component COMPA45 1 Consumable CMLA01 1 **CONF 008 MATERIAL QTY PER A/C SEE NOTES Component COMPA02 1 Component COMPA03 1 Component COMPA04 1 Component COMPA05 1 Component COMPA06 1 Component COMPA07 1 Component COMPA08 1 Component COMPA09 1 Component COMPA10 1 Component COMPA11 1 Component COMPA12 1 Component COMPA13 1 Component COMPA14 1 Component COMPA15 1 Component COMPA16 1 Component COMPA17 1

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 5 5

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# @A340-500/600
SERVICE BULLETIN

MATERIAL QTY PER A/C SEE NOTES Component COMPA18 1 Component COMPA19 1 Component COMPA20 1 Component COMPA21 1 Component COMPA22 1 Component COMPA24 1 Component COMPA25 1 Component COMPA26 1 Component COMPA27 1 Component COMPA29 1 Component COMPA31 1 Component COMPA38 1 Component COMPA39 1 Component COMPA40 1 Component COMPA41 1 Component COMPA42 1 Component COMPA43 1 Consumable CMLA01 1 **CONF 009 MATERIAL QTY PER A/C SEE NOTES Component COMPA19 1 Component COMPA20 1 Component COMPA40 1 Consumable CMLA01 1 **CONF ALL B. CONCURRENT REQUIREMENTS None

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 6 5

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# @A340-500/600
SERVICE BULLETIN

C. REASON (1) History During structural parts assembly on the production line, some nuts were detected cracked. An investigation was immediately launched to determine the affected nut types and the associated batches. AIRBUS and the nut manufacturer, LISI Monadnock, have identified that the affected nut type is ASNA2531-4. These suspected non conforming nuts have been installed in production on aircraft listed in effectivity paragraph. Extensive static, fatigue and corrosion tests have been performed, results from tests andanalysis indicated that no immediate maintenance action is required on the affected inservice aircraft. However, as this event impacts a large amount of nuts associated to the primary structure assembly, Airbus requests the replacement of all nuts in order to restore the original design intent. (2) Objective/Action This One Time Inspection Service Bulletin consists in replacing all the suspect nuts with new ones of same type. (3) Advantages Accomplishment of this Service Bulletin will restore the aircraft structure to its original design configuration. NOTE: It is suggested to accomplish this service Bulletin during a major servicing because of the time-consuming get access and close-up procedures for the removal and installation of the galleys and the lavatories for example. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : **CONF 001 Task 535056-832-801-001: Inspection (1) Inspection / Repair (2) Area 18, replace nuts from rear section FR54 stringer 54 LH side (3) Area 20, replace nuts from LH and RH fixed inner shroud boxes (4) Area 21, replace nuts at FR38 and FR54 circumferential junctions (5) Area concession 1 (6) Area concession 2

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 7 5

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# @A340-500/600
SERVICE BULLETIN

**CONF 002 Task 535056-832-801-001: Inspection (1) Inspection / Repair (2) Area 1a, replace the nuts in FWD LH hard points (3) Area 1a, replace the nuts in FWD RH hard points (4) Area 1b, replace nuts of 800VU RH support (5) Area 14, replace nuts from LH and RH dado panel support struts (6) Area 18, replace nuts from rear section FR54 stringer 54 LH side (7) Area 19, replace nut from LH side of outer wing centre spar (8) Area 20, replace nuts from LH and RH fixed inner shroud boxes (9) Area 21, replace nuts at FR38 and FR54 circumferential junctions (10) Area concession 1 (11) Area concession 2 **CONF 003 Task 535056-832-801-001: Inspection (1) Inspection / Repair (2) Area 20, replace nuts from LH and RH fixed inner shroud boxes **CONF 004 Task 535056-832-801-001: Inspection (1) Inspection / Repair (2) Area 18, replace nuts from rear section FR54 stringer 54 LH side (3) Area 20, replace nuts from LH and RH fixed inner shroud boxes (4) Area 21, replace nuts at FR38 and FR54 circumferential junctions (5) Area concession 1 **CONF 005 Task 535056-832-801-001: Inspection (1) Inspection / Repair

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 8 5

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# @A340-500/600
SERVICE BULLETIN
(2) Area 1a, replace the nuts in FWD RH hard points (3) Area 1b, replace nuts of 800VU RH support (4) Area 18, replace nuts from rear section FR54 stringer 54 LH side (5) Area 20, replace nuts from LH and RH fixed inner shroud boxes (6) Area 21, replace nuts at FR38 and FR54 circumferential junctions (7) Area concession 1 **CONF 006 Task 535056-832-801-001: Inspection (1) Inspection / Repair (2) Area 1a, replace the nuts in FWD RH hard points (3) Area 1b, replace nuts of 800VU RH support (4) Area 18, replace nuts from rear section FR54 stringer 54 LH side (5) Area 19, replace nut from LH side of outer wing centre spar (6) Area 20, replace nuts from LH and RH fixed inner shroud boxes (7) Area 21, replace nuts at FR38 and FR54 circumferential junctions (8) Area concession 1 **CONF 007 Task 535056-832-801-001: Inspection (1) Inspection / Repair (2) Area 1a, replace the nuts in FWD RH hard points (3) Area 1b, replace nuts of 800VU RH support (4) Area 2a, replace nuts of LH and RH keel lower angle fittings (5) Area 2b, replace nuts of LH and RH lower fuselage to FR40 attachments (6) Area 2c, replace nuts of fuselage to LH and RH inner keel beam attachments (7) Area 2d, replace nuts of fuselage to LH and RH outer keel beam attachments (8) Area 2e, replace nuts below LH and RH lower panels of FR40-1 to section 21 attachments (9) Area 2f, replace nuts from inboard of LH and RH center wing rear spars
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 9 5

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# @A340-500/600
SERVICE BULLETIN
(10) Area 3, replace nuts from LH and RH zones of belly fairing structure (11) Area 4a, replace nuts of LH and RH canted lateral panel attachments (12) Area 4b, replace nuts of LH and RH FWD canted beams (13) Area 4c, replace nuts of LH and RH aft canted beams (14) Area 5, replace nuts of LH and RH fuselage to outer keel beam attachments (15) Area 6, replace nuts of LH and RH FWD inner keel beams (16) Area 7, replace nuts of LH keel beam attachment tees (17) Area 8, replace nuts from RH keel beam attachment tees (18) Area 9, replace nuts from RH side of floor structure (19) Area 10, replace nuts from LH and RH sides of longitudinal joint (20) Area 11, replace nuts of LH and RH cleat attachments (21) Area 12, replace nuts from FWD LH side of canted beam attachment (22) Area 13, replace nuts from FWD RH side of canted beam attachment (23) Area 14, replace nuts from LH and RH dado panel support struts (24) Area 15, replace nuts from LH and RH sides of FR53-6 splicing (25) Area 16, replace nuts from LH and RH seat track splicings (26) Area 17, replace nuts from LH and RH seat track splicings (27) Area 18, replace nuts from rear section FR54 stringer 54 LH side (28) Area 20, replace nuts from LH and RH fixed inner shroud boxes (29) Area 21, replace nuts at FR38 and FR54 circumferential junctions (30) Area concession 1 (31) Area concession 2 (32) Area concession 3 (33) Area concession 4 (34) Area concession 5 (35) Area concession 6

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 10 5

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# @A340-500/600
SERVICE BULLETIN

**CONF 008 Task 535056-832-801-001: Inspection (1) Inspection / Repair (2) Area 1a, replace the nuts in FWD RH hard points (3) Area 1b, replace nuts of 800VU RH support (4) Area 2a, replace nuts of LH and RH keel lower angle fittings (5) Area 2b, replace nuts of LH and RH lower fuselage to FR40 attachments (6) Area 2c, replace nuts of fuselage to LH and RH inner keel beam attachments (7) Area 2d, replace nuts of fuselage to LH and RH outer keel beam attachments (8) Area 2e, replace nuts below LH and RH lower panels of FR40-1 to section 21 attachments (9) Area 2f, replace nuts from inboard of LH and RH center wing rear spars (10) Area 3, replace nuts from LH and RH zones of belly fairing structure (11) Area 4a, replace nuts of LH and RH canted lateral panel attachments (12) Area 4b, replace nuts of LH and RH FWD canted beams (13) Area 4c, replace nuts of LH and RH aft canted beams (14) Area 5, replace nuts of LH and RH fuselage to outer keel beam attachments (15) Area 6, replace nuts of LH and RH FWD inner keel beams (16) Area 7, replace nuts of LH keel beam attachment tees (17) Area 8, replace nuts from RH keel beam attachment tees (18) Area 9, replace nuts from RH side of floor structure (19) Area 10, replace nuts from LH and RH sides of longitudinal joint (20) Area 11, replace nuts of LH and RH cleat attachments (21) Area 12, replace nuts from FWD LH side of canted beam attachment (22) Area 13, replace nuts from FWD RH side of canted beam attachment (23) Area 14, replace nuts from LH and RH dado panel support struts (24) Area 15, replace nuts from LH and RH sides of FR53-6 splicing (25) Area 16, replace nuts from LH and RH seat track splicings
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 11 5

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# @A340-500/600
SERVICE BULLETIN
(26) Area 17, replace nuts from LH and RH seat track splicings (27) Area 18, replace nuts from rear section FR54 stringer 54 LH side (28) Area 20, replace nuts from LH and RH fixed inner shroud boxes (29) Area 21, replace nuts at FR38 and FR54 circumferential junctions (30) Area 23, replace nut in belly fairing zone 5 (31) Area concession 1 (32) Area concession 2 (33) Area concession 3 (34) Area concession 4 **CONF 009 Task 535056-832-801-001: Inspection (1) Inspection / Repair (2) Area 10, replace nuts from LH and RH sides of longitudinal joint (3) Area 11, replace nuts of LH and RH cleat attachments (4) Area concession 1 **CONF ALL E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale CONDITION ACTION COMPLIANCE TIME WHICHEVER OCCURS REPETITIVE INTERVAL All areas except areas 2f, 7, 8 and 19 Perform detailed visual inspection of nuts P/N ASNA2531-4 for cracked and missing nuts 4C check or 6 years from production delivery date Not applicable

Missing nut found Contact AIRBUS for additional instructions Before next flight No further action Cracked nut found Inform AIRBUS and replace the nut as per given Repair Instructions R51415000 and R51415001 Before next flight No further action

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# @A340-500/600
SERVICE BULLETIN

CONDITION ACTION COMPLIANCE TIME WHICHEVER OCCURS REPETITIVE INTERVAL No findings Replace the nut P/N ASNA2531-4 as per given Repair Instructions R51415000 and R51415001 Before next flight No further action

Table 1 : Detailed visual inspection of nuts not located in fuel tank areas overcoated with sealant. CONDITION ACTION COMPLIANCE TIME WHICHEVER OCCURS REPETITIVE INTERVAL For areas 2f, 7, 8 and 19 Perform detailed visual inspection of nuts P/N ASNA2531-4 for cracked and missing nuts 8C check or 12 years from production delivery date Not applicable

Missing nut found Contact AIRBUS for additional instructions Before next flight No further action Cracked nut found Inform AIRBUS and replace the nut as per given Repair Instructions R51415000 and R51415001 Before next flight No further action
No findings Replace the nut P/N ASNA2531-4 as per given Repair Instructions R51415000 and R51415001 Before next flight No further action

Table 2 : Detailed visual inspection of nuts located in fuel tank areas overcoated with sealant. NOTE: Areas to be inspected and associated numbering are defined within Repair Instructions R51415000 and R51415001. F. APPROVAL Approved underEASA Design Organisation Approval No. EASA21J.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: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 13 5

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**CONF 001 Task 535056-832-801-001: Inspection Get Access 80.00 On Aircraft Inspection / Repair 4.00 Area 18, replace nuts from rear section FR54 stringer 54 LH side 4.00 Area 20, replace nuts from LH and RH fixed inner shroud boxes 1.50 Area 21, replace nuts at FR38 and FR54 circumferential junctions 6.00 Area concession 1 0.25 Area concession 2 0.25 Tests 2.00 Close-Up 85.00 TOTAL MANHOURS 183.00 ELAPSED TIME (HOURS) 51.00 NOTE: For detail concerning elapsed time assumptions, refer to Appendix 02 Elapsed Time Assumptions . **CONF 002 Task 535056-832-801-001: Inspection Get Access 120.0 On Aircraft Inspection / Repair 4.00 Area 1a, replace the nuts in FWD LH hard points 0.50 Area 1a, replace the nuts in FWD RH hard points 0.50 Area 1b, replace nuts of 800VU RH support 0.50 Area 14, replace nuts from LH and RH dado panel support struts 4.00 Area 18, replace nuts from rear section FR54 stringer 54 LH side 4.00 Area 19, replace nut from LH side of outer wing centre spar 0.50 Area 20, replace nuts from LH and RH fixed inner shroud boxes 1.50 Area 21, replace nuts at FR38 and FR54 circumferential junctions 3.00 Area concession 1 0.25 Area concession 2 0.50 Tests 2.00 Close-Up 120.0 TOTAL MANHOURS 261.25 ELAPSED TIME (HOURS) 68.0
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NOTE: For detail concerning elapsed time assumptions, refer to Appendix 02 Elapsed Time Assumptions . **CONF 003 Task 535056-832-801-001: Inspection Get Access 5.00 On Aircraft Inspection / Repair 2.00 Area 20, replace nuts from LH and RH fixed inner shroud boxes 1.50 Tests 2.00 Close-Up 5.00 TOTAL MANHOURS 15.50 ELAPSED TIME (HOURS) 9.00 NOTE: For detail concerning elapsed time assumptions, refer to Appendix 02 Elapsed Time Assumptions . **CONF 004 Task 535056-832-801-001: Inspection Get Access 70.00 On Aircraft Inspection / Repair 4.00 Area 18, replace nuts from rear section FR54 stringer 54 LH side 4.00 Area 20, replace nuts from LH and RH fixed inner shroud boxes 1.50 Area 21, replace nuts at FR38 and FR54 circumferential junctions 3.75 Area concession 1 0.50 Tests 2.00 Close-Up 70.00 TOTAL MANHOURS 155.75 ELAPSED TIME (HOURS) 45.00 NOTE: For detail concerning elapsed time assumptions, refer to Appendix 02 Elapsed Time Assumptions . **CONF 005 Task 535056-832-801-001: Inspection Get Access 80.00 On Aircraft Inspection / Repair 4.00 Area 1a, replace the nuts in FWD RH hard points 0.50 Area 1b, replace nuts of 800VU RH support 0.50
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Task 535056-832-801-001: Inspection Area 18, replace nuts from rear section FR54 stringer 54 LH side 2.50 Area 20, replace nuts from LH and RH fixed inner shroud boxes 1.50 Area 21, replace nuts at FR38 and FR54 circumferential junctions 7.25 Area concession 1 0.50 Tests 2.00 Close-Up 85.00 TOTAL MANHOURS 183.75 ELAPSED TIME (HOURS) 56.00 NOTE: For detail concerning elapsed time assumptions, refer to Appendix 02 Elapsed Time Assumptions . **CONF 006 Task 535056-832-801-001: Inspection Get Access 80.00 On Aircraft Inspection / Repair 4.00 Area 1a, replace the nuts in FWD RH hard points 0.50 Area 1b, replace nuts of 800VU RH support 0.50 Area 18, replace nuts from rear section FR54 stringer 54 LH side 2.50 Area 19, replace nut from LH side of outer wing centre spar 0.50 Area 20, replace nuts from LH and RH fixed inner shroud boxes 1.50 Area 21, replace nuts at FR38 and FR54 circumferential junctions 8.50 Area concession 1 0.50 Tests 2.00 Close-Up 85.00 TOTAL MANHOURS 185.50 ELAPSED TIME (HOURS) 56.00 NOTE: For detail concerning elapsed time assumptions, refer to Appendix 02 Elapsed Time Assumptions . **CONF 007 Task 535056-832-801-001: Inspection Get Access 520.0 On Aircraft Inspection / Repair 4.00

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Task 535056-832-801-001: Inspection Area 1a, replace the nuts in FWD RH hard points 0.50 Area 1b, replace nuts of 800VU RH support 0.50 Area 2a, replace nuts of LH and RH keel lower angle fittings 5.25 Area 2b, replace nuts of LH and RH lower fuselage to FR40 attachments 22.50 Area 2c, replace nuts of fuselage to LH and RH inner keel beam attachments 9.50 Area 2d, replace nuts of fuselage to LH and RH outer keel beam attachments 9.00 Area 2e, replace nuts below LH and RH lower panels of FR40-1 to section 21 attachments 6.00 Area 2f, replace nuts from inboard of LH and RH center wing rear spars 1.00 Area 3, replace nuts from LH and RH zones of belly fairing structure 1.50 Area 4a, replace nuts of LH and RH canted lateral panel attachments 0.50 Area 4b, replace nuts of LH and RH FWD canted beams 1.00 Area 4c, replace nuts of LH and RH aft canted beams 0.50 Area 5, replace nuts of LH and RH fuselage to outer keel beam attachments 1.75 Area 6, replace nuts of LH and RH FWD inner keel beams 1.75 Area 7, replace nuts of LH keel beam attachment tees 12.00 Area 8, replace nuts from RH keel beam attachment tees 12.00 Area 9, replace nuts from RH side of floor structure 1.00 Area 10, replace nuts from LH and RH sides of longitudinal joint 1.50 Area 11, replace nuts of LH and RH cleat attachments 2.00 Area 12, replace nuts from FWD LH side of canted beam attachment 9.00 Area 13, replace nuts from FWD RH side of canted beam attachment 8.50 Area 14, replace nuts from LH and RH dado panel support struts 3.00 Area 15, replace nuts from LH and RH sides of FR53-6 splicing 1.00 Area 16, replace nuts from LH and RH seat track splicings 5.00 Area 17, replace nuts from LH and RH seat track splicings 5.00 Area 18, replace nuts from rear section FR54 stringer 54 LH side 2.50

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 17 5

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Task 535056-832-801-001: Inspection Area 20, replace nuts from LH and RH fixed inner shroud boxes 1.50 Area 21, replace nuts at FR38 and FR54 circumferential junctions 10.00 Area concession 1 0.50 Area concession 2 0.25 Area concession 3 0.25 Area concession 4 0.25 Area concession 5 0.25 Area concession 6 0.25 Tests 2.00 Close-Up 530.0 TOTAL MANHOURS 1193.00 ELAPSED TIME (HOURS) 378.0 NOTE: For detail concerning elapsed time assumptions, refer to Appendix 02 Elapsed Time Assumptions . **CONF 008 Task 535056-832-801-001: Inspection Get Access 510.0 On Aircraft Inspection / Repair 4.00 Area 1a, replace the nuts in FWD RH hard points 0.50 Area 1b, replace nuts of 800VU RH support 0.50 Area 2a, replace nuts of LH and RH keel lower angle fittings 5.25 Area 2b, replace nuts of LH and RH lower fuselage to FR40 attachments 22.50 Area 2c, replace nuts of fuselage to LH and RH inner keel beam attachments 9.50 Area 2d, replace nuts of fuselage to LH and RH outer keel beam attachments 9.00 Area 2e, replace nuts below LH and RH lower panels of FR40-1 to section 21 attachments 6.00 Area 2f, replace nuts from inboard of LH and RH center wing rear spars 1.00 Area 3, replace nuts from LH and RH zones of belly fairing structure 1.50 Area 4a, replace nuts of LH and RH canted lateral panel attachments 0.50 Area 4b, replace nuts of LH and RH FWD canted beams 1.00 Area 4c, replace nuts of LH and RH aft canted beams 0.50

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 18 5

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Task 535056-832-801-001: Inspection Area 5, replace nuts of LH and RH fuselage to outer keel beam attachments 1.75 Area 6, replace nuts of LH and RH FWD inner keel beams 1.75 Area 7, replace nuts of LH keel beam attachment tees 12.00 Area 8, replace nuts from RH keel beam attachment tees 12.00 Area 9, replace nuts from RH side of floor structure 1.00 Area 10, replace nuts from LH and RH sides of longitudinal joint 1.50 Area 11, replace nuts of LH and RH cleat attachments 2.00 Area 12, replace nuts from FWD LH side of canted beam attachment 9.00 Area 13, replace nuts from FWD RH side of canted beam attachment 8.50 Area 14, replace nuts from LH and RH dado panel support struts 3.00 Area 15, replace nuts from LH and RH sides of FR53-6 splicing 1.00 Area 16, replace nuts from LH and RH seat track splicings 5.00 Area 17, replace nuts from LH and RH seat track splicings 5.00 Area 18, replace nuts from rear section FR54 stringer 54 LH side 2.50 Area 20, replace nuts from LH and RH fixed inner shroud boxes 1.50 Area 21, replace nuts at FR38 and FR54 circumferential junctions 3.00 Area 23, replace nut in belly fairing zone 5 0.25 Area concession 1 0.25 Area concession 2 0.25 Area concession 3 0.25 Area concession 4 0.25 Tests 2.00 Close-Up 510.0 TOTAL MANHOURS 1155.50 ELAPSED TIME (HOURS) 377.0 NOTE: For detail concerning elapsed time assumptions, refer to Appendix 02 Elapsed Time Assumptions . **CONF 009 Task 535056-832-801-001: Inspection Get Access 80.00

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 19 5

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Task 535056-832-801-001: Inspection On Aircraft Inspection / Repair 4.00 Area 10, replace nuts from LH and RH sides of longitudinal joint 1.50 Area 11, replace nuts of LH and RH cleat attachments 1.00 Area concession 1 1.50 Tests 2.00 Close-Up 90.00 TOTAL MANHOURS 180.00 ELAPSED TIME (HOURS) 46.00 NOTE: For detail concerning elapsed time assumptions, refer to Appendix 02 Elapsed Time Assumptions **CONF ALL H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES **CONF 001 Aircraft Maintenance Manual (AMM) 06-20-00 06-30-00 06-31-53 06-40-00 12-34-24 20-21-11 20-28-00 21-20-00 21-26-00 21-28-00 21-42-41 21-52-41 21-53-00 21-63-00 22-96-00 22-97-00 24-41-00 25-21-41 25-22-44 25-23-41 25-23-43 25-23-44 25-23-61 25-24-61 25-28-41 25-28-42 25-28-43 25-37-41 25-42-41 25-42-42 25-52-00 25-53-00 25-77-38 25-80-00 27-50-00 31-50-00 31-60-00 33-13-00 33-14-00 52-10-00 52-30-00 53-00-00 53-35-41 Consumable Material List (CML) Drawing R51415000 R51415001 Elec. Std. Practices Manual (ESPM) 20-52-10 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12
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**CONF 002 Aircraft Maintenance Manual (AMM) 06-20-00 06-30-00 06-31-53 06-40-00 12-34-24 20-21-11 20-28-00 21-20-00 21-26-00 21-28-00 21-42-41 21-52-41 21-53-00 21-63-00 22-96-00 22-97-00 24-41-00 25-21-41 25-22-44 25-23-41 25-23-43 25-23-44 25-23-61 25-24-61 25-28-41 25-28-42 25-28-43 25-37-41 25-42-41 25-42-42 25-52-00 25-53-00 25-77-38 25-80-00 27-50-00 28-10-00 28-25-00 31-50-00 31-60-00 33-13-00 33-14-00 52-10-00 52-30-00 53-00-00 53-12-13 53-35-41 57-17-11 57-27-11 Consumable Material List (CML) Drawing R51415000 R51415001 Elec. Std. Practices Manual (ESPM) 20-52-10 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12 **CONF 003 Aircraft Maintenance Manual (AMM) 06-20-00 06-30-00 06-31-53 06-40-00 12-34-24 20-21-11 20-28-00 21-20-00 21-26-00 21-28-00 21-42-41 21-52-41 21-53-00 21-63-00 22-96-00 22-97-00 24-41-00 25-21-41 25-23-41 25-42-41 25-42-42 27-50-00 31-50-00 31-60-00 32-12-00 33-13-00 33-14-00 53-35-41 Consumable Material List (CML) Drawing R51415000 R51415001 Elec. Std. Practices Manual (ESPM) 20-52-10 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12

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**CONF 004 Aircraft Maintenance Manual (AMM) 06-20-00 06-30-00 06-31-53 06-40-00 12-34-24 20-21-11 20-28-00 21-20-00 21-26-00 21-28-00 21-42-41 21-52-41 21-53-00 21-63-00 22-96-00 22-97-00 24-41-00 25-21-41 25-22-44 25-23-41 25-23-43 25-23-44 25-23-61 25-24-61 25-28-41 25-28-42 25-28-43 25-37-41 25-42-41 25-42-42 25-52-00 25-53-00 25-77-38 25-80-00 27-50-00 31-50-00 31-60-00 33-13-00 33-14-00 52-10-00 52-30-00 53-00-00 53-35-41 Consumable Material List (CML) Drawing R51415000 R51415001 Elec. Std. Practices Manual (ESPM) 20-52-10 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12 **CONF 005 Aircraft Maintenance Manual (AMM) 06-20-00 06-30-00 06-31-53 06-40-00 12-34-24 20-21-11 20-28-00 21-20-00 21-26-00 21-28-00 21-42-41 21-52-41 21-53-00 21-63-00 22-96-00 22-97-00 24-41-00 25-21-41 25-22-44 25-23-41 25-23-43 25-23-44 25-23-61 25-24-61 25-28-41 25-28-42 25-28-43 25-32-84 25-42-41 25-42-42 25-52-00 25-53-00 25-80-00 27-50-00 28-10-00 31-50-00 31-60-00 33-13-00 33-14-00 52-10-00 52-30-00 53-00-00 53-12-13 53-35-41 57-17-11 57-27-11 Consumable Material List (CML) Drawing R51415000 R51415001 Elec. Std. Practices Manual (ESPM) 20-52-10 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12

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**CONF 006 Aircraft Maintenance Manual (AMM) 06-20-00 06-30-00 06-31-53 06-40-00 12-34-24 20-21-11 20-28-00 21-20-00 21-26-00 21-28-00 21-42-41 21-52-41 21-53-00 21-63-00 22-96-00 22-97-00 24-41-00 25-21-41 25-22-44 25-23-41 25-23-43 25-23-44 25-23-61 25-24-61 25-28-41 25-28-42 25-28-43 25-32-84 25-42-41 25-42-42 25-52-00 25-53-00 25-77-38 25-80-00 27-50-00 28-10-00 28-25-00 31-50-00 31-60-00 33-13-00 33-14-00 52-10-00 52-30-00 53-00-00 53-12-13 53-35-41 57-17-11 57-27-11 Consumable Material List (CML) Drawing R51415000 R51415001 Elec. Std. Practices Manual (ESPM) 20-52-10 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12 **CONF 007 Aircraft Maintenance Manual (AMM) 06-20-00 06-30-00 06-31-53 06-40-00 12-34-24 20-21-11 20-28-00 21-20-00 21-26-00 21-28-00 21-42-41 21-52-41 21-53-00 21-53-51 21-63-00 22-96-00 22-97-00 24-41-00 25-21-41 25-22-44 25-23-41 25-23-43 25-23-44 25-23-61 25-24-61 25-28-41 25-28-42 25-28-43 25-32-84 25-37-41 25-42-41 25-42-42 25-52-00 25-53-00 25-77-38 25-80-00 27-50-00 28-10-00 28-25-00 31-50-00 31-60-00 32-12-00 33-13-00 33-14-00 52-10-00 52-30-00 53-00-00 53-12-13 53-35-11 53-35-13 53-35-41 57-17-11 57-27-11 Consumable Material List (CML) Drawing R51415000 R51415001 Elec. Std. Practices Manual (ESPM) 20-52-10 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12
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**CONF 008 Aircraft Maintenance Manual (AMM) 06-20-00 06-30-00 06-31-53 06-40-00 12-34-24 20-21-11 20-28-00 21-20-00 21-26-00 21-28-00 21-42-41 21-52-41 21-53-00 21-53-51 21-63-00 22-96-00 22-97-00 24-41-00 25-21-41 25-22-44 25-23-41 25-23-43 25-23-44 25-23-61 25-24-61 25-28-41 25-28-42 25-28-43 25-32-84 25-37-41 25-42-41 25-42-42 25-52-00 25-53-00 25-77-38 25-80-00 27-50-00 28-10-00 28-25-00 31-50-00 31-60-00 32-12-00 33-13-00 33-14-00 52-10-00 52-30-00 53-00-00 53-12-13 53-35-11 53-35-13 53-35-41 57-17-11 57-27-11 Consumable Material List (CML) Drawing R51415000 R51415001 Elec. Std. Practices Manual (ESPM) 20-52-10 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12 **CONF 009 Aircraft Maintenance Manual (AMM) 06-20-00 06-30-00 06-31-53 06-40-00 12-34-24 20-21-11 20-28-00 21-20-00 21-26-00 21-28-00 21-42-41 21-52-41 21-53-00 21-63-00 22-96-00 22-97-00 24-41-00 25-21-41 25-23-41 25-23-43 25-23-61 25-42-41 25-42-42 25-52-00 25-80-00 31-50-00 31-60-00 33-13-00 33-14-00 52-10-00 52-30-00 53-35-13 53-35-41 Consumable Material List (CML) Drawing R51415000 R51415001 Elec. Std. Practices Manual (ESPM) 20-52-10 20-55-00 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12 **CONF ALL K. PUBLICATION AFFECTED None DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 24 5

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L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None

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This Page Intentionally Left Blank

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2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Component COMPA01 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA02 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

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Component COMPA03 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA04 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

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# @A340-500/600
SERVICE BULLETIN
Component COMPA05 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA06 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 29 5

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

# @A340-500/600
SERVICE BULLETIN
Component COMPA07 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA08 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 30 5

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

# @A340-500/600
SERVICE BULLETIN
Component COMPA09 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA10 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 31 5

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

# @A340-500/600
SERVICE BULLETIN
Component COMPA11 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA12 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 32 5

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

# @A340-500/600
SERVICE BULLETIN
Component COMPA13 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA14 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 33 5

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

# @A340-500/600
SERVICE BULLETIN
Component COMPA15 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA16 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 34 5

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

# @A340-500/600
SERVICE BULLETIN
Component COMPA17 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA18 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 35 5

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

# @A340-500/600
SERVICE BULLETIN
Component COMPA19 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA20 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 36 5

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

# @A340-500/600
SERVICE BULLETIN
Component COMPA21 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA22 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 37 5

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

# @A340-500/600
SERVICE BULLETIN
Component COMPA23 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA24 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 38 5

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

# @A340-500/600
SERVICE BULLETIN
Component COMPA25 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA26 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 39 5

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

# @A340-500/600
SERVICE BULLETIN
Component COMPA27 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA28 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 40 5

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

# @A340-500/600
SERVICE BULLETIN
Component COMPA29 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA30 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 41 5

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

# @A340-500/600
SERVICE BULLETIN
Component COMPA31 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA32 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 42 5

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

# @A340-500/600
SERVICE BULLETIN
Component COMPA33 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA34 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 43 5

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

# @A340-500/600
SERVICE BULLETIN
Component COMPA35 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA36 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 44 5

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

# @A340-500/600
SERVICE BULLETIN
Component COMPA37 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA38 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 45 5

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

# @A340-500/600
SERVICE BULLETIN
Component COMPA39 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA40 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 46 5

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

# @A340-500/600
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Component COMPA41 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA42 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 47 5

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Component COMPA43 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> Component COMPA44 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 48 5

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Component COMPA45 Customers with aircraft shown in the effectivity of this Service Bulletin can send a purchase order to B/E Aerospace. Quote the number of this Service Bulletin. The address is: B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15th Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com web address www.beconsumables.com <http://www.beconsumables.com> (2) Price and Availability No AIRBUS kit will be provided. Parts required to accomplish this Service Bulletin are to be supplied from Operators’ stock. B. INDUSTRY SUPPORT INFORMATIONAIRBUS will credit the manhours indicated in this Service Bulletin at the operator’s agreed inhouse warranty labor rate as well as the material costs for claims received not later than 90 days after completion of the last affected aircraft of your fleet. C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials To accomplish this Service Bulletin it is necessary to use the expendable parts listed in AMM tasks mentioned in paragraph TASK 535056-832-801 001 Inspection . Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005A As required Solvent General Purpose 11-026 As required Polyurethane Primer 16-001C As required Polyurethane Finish Paint (for External Applic.) 16-018C As required

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 49 5

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(2) Components Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 2 NUT 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. Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 2 NUT 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. Component COMPA03 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 4 NUT 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. Component COMPA04 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 62 NUT 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. Component COMPA05 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 269 NUT

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 50 5

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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. Component COMPA06 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 112 NUT 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. Component COMPA07 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 106 NUT 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. Component COMPA08 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 70 NUT 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. Component COMPA09 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 10 NUT NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 51 5

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Component COMPA10 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 16 NUT 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. Component COMPA11 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 6 NUT 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. Component COMPA12 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 12 NUT 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. Component COMPA13 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 2 NUT 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. Component COMPA14 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 20 NUT

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 52 5

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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. Component COMPA15 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 20 NUT 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. Component COMPA16 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 72 NUT 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. Component COMPA17 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 72 NUT 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. Component COMPA18 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 6 NUT NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 53 5

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Component COMPA19 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 10 NUT 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. Component COMPA20 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 16 NUT 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. Component COMPA21 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 NSA5050-3 2 NUT 4 EN6115V4X-10 3 SCREW ASNA2531-4 90 NUT 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. Component COMPA22 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 NSA5050-3 6 NUT 10 ASNA2027V4X-9 6 SCREW ASNA2531-4 83 NUT 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. Component COMPA23 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 40 NUT DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 54 5

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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. Component COMPA24 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 32 NUT 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. Component COMPA25 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 6 NUT 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. Component COMPA26 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 44 NUT 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. Component COMPA27 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 44 NUT NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 55 5

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Component COMPA28 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 33 NUT 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. Component COMPA29 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 22 NUT 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. Component COMPA30 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 1 NUT 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. Component COMPA31 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 16 NUT 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. Component COMPA32 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 59 NUT

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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. Component COMPA33 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 31 NUT 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. Component COMPA34 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 37 NUT 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. Component COMPA35 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 72 NUT 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. Component COMPA36 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 84 NUT NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 57 5

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Component COMPA37 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 101 NUT 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. Component COMPA38 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 29 NUT 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. Component COMPA39 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 1 NUT 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. Component COMPA40 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 16 NUT 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. Component COMPA41 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 6 NUT

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 58 5

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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. Component COMPA42 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 1 NUT 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. Component COMPA43 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 1 NUT 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. Component COMPA44 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 1 NUT 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. Component COMPA45 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES ASNA2531-4 2 NUT 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. (3) Equipment None

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 59 5

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E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING (1) Tooling - Price and Availability None (2) Tools To accomplish this Service Bulletin it is necessary to use the tools listed in AMM tasks mentioned in paragraph TASK 535056-832-801 001 Inspection . (3) Special Tools None

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 60 5

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3. ACCOMPLISHMENT INSTRUCTIONS Task 535056-832-801-001 - Inspection 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 100 200 260 570 670 Modified FIN 6710ML 6691NW Manpower TOTAL MANHOURS 183.00 ELAPSED TIME (HOURS) 51.00 **CONF 002 Zone 100 120 200 250 260 540 570 670 Modified FIN 6710ML 6691NW Access Door 132AZ 821 Manpower TOTAL MANHOURS 261.25 ELAPSED TIME (HOURS) 68.0

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**CONF 003 Zone 100 200 570 670 Manpower TOTAL MANHOURS 15.50 ELAPSED TIME (HOURS) 9.00 **CONF 004 Zone 100 200 260 570 670 Modified FIN 6710ML 6691NW Manpower TOTAL MANHOURS 155.75 ELAPSED TIME (HOURS) 45.00 **CONF 005 Zone 100 120 200 260 570 670 Access Door 132AZ 821 Manpower TOTAL MANHOURS 183.75 ELAPSED TIME (HOURS) 56.00 **CONF 006 Zone 100 120 200 260 540 570 670 Access Door 132AZ 821 Manpower TOTAL MANHOURS 185.50 ELAPSED TIME (HOURS) 56.00 **CONF 007 Zone 100 120 130 140 150 190 200 250 260 570 670 Access Door 132AZ 821 Manpower TOTAL MANHOURS 1193.00 ELAPSED TIME (HOURS) 378.0

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 62 5

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**CONF 008 Zone 100 120 130 140 150 190 200 250 260 570 670 Access Door 132AZ 821 Manpower TOTAL MANHOURS 1155.50 ELAPSED TIME (HOURS) 377.0 **CONF 009 Zone 100 130 200 250 Manpower TOTAL MANHOURS 180.00 ELAPSED TIME (HOURS) 46.00 **CONF ALL A. GENERAL **CONF 001 (1) Subtask 535056-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005A As required Solvent General Purpose 11-026 As required Polyurethane Primer 16-001C As required Polyurethane Finish Paint (for External Applic.) 16-018C As required

References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-30-00, Page Block 001 06-31-53, Page Block 001 06-40-00, Page Block 001 Task 20-21-11-911-801 20-28-00, Page Block 201 Consumable Material List (CML)

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References Drawing R51415000 R51415001 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12 (a) For the specification of the material numbers (Mat. No.), refer to Consumable Material List (CML). (b) Protect the areas to prevent damage to the equipment and structure and all the parts. (c) Clean the surfaces with Solvent General Purpose 11-026 As required (d) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001). (e) For the identification of zones, (Refer to AMM 06-20-00, Page Block 001). (f) For the identification of access panels, (Refer to AMM 06-40-00, Page Block 001). (g) For the identification of stringers (Refer to AMM 06-30-00, Page Block 001). (h) For each area, check if the installed nut corresponds to nut ASNA2531-4. (identified by not having a spherical washer underneath and with correct diameter, refer to Standards Manual (SM)). 1 If not, leave the nut in place. 2 If it corresponds, do the operations described in SUBTASK 535056-832-001 001 Inspection / Repair . (i) For the removal and installation of fasteners (Refer to SRM 51-42-00). (j) Apply Interfay Sealant 09-005A As required to the interfaces of the structure and the reinstalled parts. (k) For fastener hole diameters, drill and deburr data (Refer to SRM 51-44-00). (l) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00). (m) To torque tighten the standard threaded fasteners (Refer to AMM Task 20-21-11-911-801).
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 64 5

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# @A340-500/600
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(n) Install the fasteners (wet assembly) with Interfay Sealant 09-005A As required (o) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201). (p) In fuel tanks, overcoat the nuts after replacement (Refer to SRM 51-76-12). (q) Renew the protective coating (Refer to SRM 51-23-12). (r) Renew the protective finish (Refer to SRM 51-75-12) with Polyurethane Primer 16-001C As required
Polyurethane Finish Paint (for External Applic.) 16-018C As required

(2) Subtask 535056-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 002 (1) Subtask 535056-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005A As required Solvent General Purpose 11-026 As required Polyurethane Primer 16-001C As required Polyurethane Finish Paint (for External Applic.) 16-018C As required

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 65 5

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# @A340-500/600
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References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-30-00, Page Block 001 06-31-53, Page Block 001 06-40-00, Page Block 001 Task 20-21-11-911-801 20-28-00, Page Block 201 Consumable Material List (CML) Drawing R51415000 R51415001 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12 (a) For the specification of the material numbers (Mat. No.), refer to Consumable Material List (CML). (b) Protect the areas to prevent damage to the equipment and structure and all the parts. (c) Clean the surfaces with Solvent General Purpose 11-026 As required (d) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001). (e) For the identification of zones, (Refer to AMM 06-20-00, Page Block 001). (f) For the identification of access panels, (Refer to AMM 06-40-00, Page Block 001). (g) For the identification of stringers (Refer to AMM 06-30-00, Page Block 001). (h) For each area, check if the installed nut corresponds to nut ASNA2531-4. (identified by not having a spherical washer underneath and with correct diameter, refer to Standards Manual (SM)). 1 If not, leave the nut in place. 2 If it corresponds, do the operations described in SUBTASK 535056-832-001 003 Inspection / Repair . (i) For the removal and installation of fasteners (Refer to SRM 51-42-00). (j) Apply Interfay Sealant 09-005A As required

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 66 5

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# @A340-500/600
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to the interfaces of the structure and the reinstalled parts. (k) For fastener hole diameters, drill and deburr data (Refer to SRM 51-44-00). (l) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00). (m) To torque tighten the standard threaded fasteners (Refer to AMM Task 20-21-11-911-801). (n) Install the fasteners (wet assembly) with Interfay Sealant 09-005A As required (o) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201). (p) In fuel tanks, overcoat the nuts after replacement (Refer to SRM 51-76-12). (q) Renew the protective coating (Refer to SRM 51-23-12). (r) Renew the protective finish (Refer to SRM 51-75-12) with Polyurethane Primer 16-001C As required
Polyurethane Finish Paint (for External Applic.) 16-018C As required

(2) Subtask 535056-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 003 (1) Subtask 535056-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005A As required Solvent General Purpose 11-026 As required Polyurethane Primer 16-001C As required

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 67 5

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# @A340-500/600
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ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Polyurethane Finish Paint (for External Applic.) 16-018C As required

References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-30-00, Page Block 001 06-31-53, Page Block 001 06-40-00, Page Block 001 Task 20-21-11-911-801 20-28-00, Page Block 201 Consumable Material List (CML) Drawing R51415000 R51415001 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12 (a) For the specification of the material numbers (Mat. No.), refer to Consumable Material List (CML). (b) Protect the areas to prevent damage to the equipment and structure and all the parts. (c) Clean the surfaces with Solvent General Purpose 11-026 As required (d) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001). (e) For the identification of zones, (Refer to AMM 06-20-00, Page Block 001). (f) For the identification of access panels, (Refer to AMM 06-40-00, Page Block 001). (g) For the identification of stringers (Refer to AMM 06-30-00, Page Block 001). (h) For each area, check if the installed nut corresponds to nut ASNA2531-4. (identified by not having a spherical washer underneath and with correct diameter, refer to Standards Manual (SM)). 1 If not, leave the nut in place. 2 If it corresponds, do the operations described in SUBTASK 535056-832-001 002 Inspection / Repair . (i) For the removal and installation of fasteners (Refer to SRM 51-42-00).
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 68 5

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# @A340-500/600
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(j) Apply Interfay Sealant 09-005A As required to the interfaces of the structure and the reinstalled parts. (k) For fastener hole diameters, drill and deburr data (Refer to SRM 51-44-00). (l) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00). (m) To torque tighten the standard threaded fasteners (Refer to AMM Task 20-21-11-911-801). (n) Install the fasteners (wet assembly) with Interfay Sealant 09-005A As required (o) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201). (p) In fuel tanks, overcoat the nuts after replacement (Refer to SRM 51-76-12). (q) Renew the protective coating (Refer to SRM 51-23-12). (r) Renew the protective finish (Refer to SRM 51-75-12) with Polyurethane Primer 16-001C As required
Polyurethane Finish Paint (for External Applic.) 16-018C As required

(2) Subtask 535056-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 004 (1) Subtask 535056-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005A As required DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 69 5

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# @A340-500/600
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ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Solvent General Purpose 11-026 As required Polyurethane Primer 16-001C As required Polyurethane Finish Paint (for External Applic.) 16-018C As required

References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-30-00, Page Block 001 06-31-53, Page Block 001 06-40-00, Page Block 001 Task 20-21-11-911-801 20-28-00, Page Block 201 Consumable Material List (CML) Drawing R51415000 R51415001 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12 (a) For the specification of the material numbers (Mat. No.), refer to Consumable Material List (CML). (b) Protect the areas to prevent damage to the equipment and structure and all the parts. (c) Clean the surfaces with Solvent General Purpose 11-026 As required (d) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001). (e) For the identification of zones, (Refer to AMM 06-20-00, Page Block 001). (f) For the identification of access panels, (Refer to AMM 06-40-00, Page Block 001). (g) For the identification of stringers (Refer to AMM 06-30-00, Page Block 001). (h) For each area, check if the installed nut corresponds to nut ASNA2531-4. (identified by not having a spherical washer underneath and with correct diameter, refer to Standards Manual (SM)). 1 If not, leave the nut in place.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 70 5

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# @A340-500/600
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2 If it corresponds, do the operations described in SUBTASK 535056-832-001 004 Inspection / Repair . (i) For the removal and installation of fasteners (Refer to SRM 51-42-00). (j) Apply Interfay Sealant 09-005A As required to the interfaces of the structure and the reinstalled parts. (k) For fastener hole diameters, drill and deburr data (Refer to SRM 51-44-00). (l) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00). (m) To torque tighten the standard threaded fasteners (Refer to AMM Task 20-21-11-911-801). (n) Install the fasteners (wet assembly) with Interfay Sealant 09-005A As required (o) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201). (p) In fuel tanks, overcoat the nuts after replacement (Refer to SRM 51-76-12). (q) Renew the protective coating (Refer to SRM 51-23-12). (r) Renew the protective finish (Refer to SRM 51-75-12) with Polyurethane Primer 16-001C As required
Polyurethane Finish Paint (for External Applic.) 16-018C As required

(2) Subtask 535056-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. **CONF 005 (1) Subtask 535056-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 71 5

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# @A340-500/600
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Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005A As required Solvent General Purpose 11-026 As required Polyurethane Primer 16-001C As required Polyurethane Finish Paint (for External Applic.) 16-018C As required

References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-30-00, Page Block 001 06-31-53, Page Block 001 06-40-00, Page Block 001 Task 20-21-11-911-801 20-28-00, Page Block 201 Consumable Material List (CML) Drawing R51415000 R51415001 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12 (a) For the specification of the material numbers (Mat. No.), refer to Consumable Material List (CML). (b) Protect the areas to prevent damage to the equipment and structure and all the parts. (c) Clean the surfaces with Solvent General Purpose 11-026 As required (d) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001). (e) For the identification of zones, (Refer to AMM 06-20-00, Page Block 001). (f) For the identification of access panels, (Refer to AMM 06-40-00, Page Block 001). (g) For the identification of stringers (Refer to AMM 06-30-00, Page Block 001).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 72 5

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# @A340-500/600
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(h) For each area, check if the installed nut corresponds to nut ASNA2531-4. (identified by not having a spherical washer underneath and with correct diameter, refer to Standards Manual (SM)). 1 If not, leave the nut in place. 2 If it corresponds, do the operations described in SUBTASK 535056-832-001 005 Inspection / Repair . (i) For the removal and installation of fasteners (Refer to SRM 51-42-00). (j) Apply Interfay Sealant 09-005A As required to the interfaces of the structure and the reinstalled parts. (k) For fastener hole diameters, drill and deburr data (Refer to SRM 51-44-00). (l) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00). (m) To torque tighten the standard threaded fasteners (Refer to AMM Task 20-21-11-911-801). (n) Install the fasteners (wet assembly) with Interfay Sealant 09-005A As required (o) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201). (p) In fuel tanks, overcoat the nuts after replacement (Refer to SRM 51-76-12). (q) Renew the protective coating (Refer to SRM 51-23-12). (r) Renew the protective finish (Refer to SRM 51-75-12) with Polyurethane Primer 16-001C As required
Polyurethane Finish Paint (for External Applic.) 16-018C As required

(2) Subtask 535056-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 73 5

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**CONF 006 (1) Subtask 535056-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005A As required Solvent General Purpose 11-026 As required Polyurethane Primer 16-001C As required Polyurethane Finish Paint (for External Applic.) 16-018C As required

References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-30-00, Page Block 001 06-31-53, Page Block 001 06-40-00, Page Block 001 Task 20-21-11-911-801 20-28-00, Page Block 201 Consumable Material List (CML) Drawing R51415000 R51415001 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12 (a) For the specification of the material numbers (Mat. No.), refer to Consumable Material List (CML). (b) Protect the areas to prevent damage to the equipment and structure and all the parts. (c) Clean the surfaces with Solvent General Purpose 11-026 As required (d) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001). (e) For the identification of zones, (Refer to AMM 06-20-00, Page Block 001).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 74 5

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# @A340-500/600
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(f) For the identification of access panels, (Refer to AMM 06-40-00, Page Block 001). (g) For the identification of stringers (Refer to AMM 06-30-00, Page Block 001). (h) For each area, check if the installed nut corresponds to nut ASNA2531-4. (identified by not having a spherical washer underneath and with correct diameter, refer to Standards Manual (SM)). 1 If not, leave the nut in place. 2 If it corresponds, do the operations described in SUBTASK 535056-832-001 006 Inspection / Repair . (i) For the removal and installation of fasteners (Refer to SRM 51-42-00). (j) Apply Interfay Sealant 09-005A As required to the interfaces of the structure and the reinstalled parts. (k) For fastener hole diameters, drill and deburr data (Refer to SRM 51-44-00). (l) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00). (m) To torque tighten the standard threaded fasteners (Refer to AMM Task 20-21-11-911-801). (n) Install the fasteners (wet assembly) with Interfay Sealant 09-005A As required (o) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201). (p) In fuel tanks, overcoat the nuts after replacement (Refer to SRM 51-76-12). (q) Renew the protective coating (Refer to SRM 51-23-12). (r) Renew the protective finish (Refer to SRM 51-75-12) with Polyurethane Primer 16-001C As required
Polyurethane Finish Paint (for External Applic.) 16-018C As required

(2) Subtask 535056-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 75 5

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# @A340-500/600
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**CONF 007 (1) Subtask 535056-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005A As required Solvent General Purpose 11-026 As required Polyurethane Primer 16-001C As required Polyurethane Finish Paint (for External Applic.) 16-018C As required

References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-30-00, Page Block 001 06-31-53, Page Block 001 06-40-00, Page Block 001 Task 20-21-11-911-801 20-28-00, Page Block 201 Consumable Material List (CML) Drawing R51415000 R51415001 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12 (a) For the specification of the material numbers (Mat. No.), refer to Consumable Material List (CML). (b) Protect the areas to prevent damage to the equipment and structure and all the parts. (c) Clean the surfaces with Solvent General Purpose 11-026 As required (d) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001). (e) For the identification of zones, (Refer to AMM 06-20-00, Page Block 001).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 76 5

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# @A340-500/600
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(f) For the identification of access panels, (Refer to AMM 06-40-00, Page Block 001). (g) For the identification of stringers (Refer to AMM 06-30-00, Page Block 001). (h) For each area, check if the installed nut corresponds to nut ASNA2531-4. (identified by not having a spherical washer underneath and with correct diameter, refer to Standards Manual (SM)). 1 If not, leave the nut in place. 2 If it corresponds, do the operations described in SUBTASK 535056-832-001 007 Inspection / Repair . (i) For the removal and installation of fasteners (Refer to SRM 51-42-00). (j) Apply Interfay Sealant 09-005A As required to the interfaces of the structure and the reinstalled parts. (k) For fastener hole diameters, drill and deburr data (Refer to SRM 51-44-00). (l) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00). (m) To torque tighten the standard threaded fasteners (Refer to AMM Task 20-21-11-911-801). (n) Install the fasteners (wet assembly) with Interfay Sealant 09-005A As required (o) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201). (p) In fuel tanks, overcoat the nuts after replacement (Refer to SRM 51-76-12). (q) Renew the protective coating (Refer to SRM 51-23-12). (r) Renew the protective finish (Refer to SRM 51-75-12) with Polyurethane Primer 16-001C As required
Polyurethane Finish Paint (for External Applic.) 16-018C As required

(2) Subtask 535056-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 77 5

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# @A340-500/600
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**CONF 008 (1) Subtask 535056-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005A As required Solvent General Purpose 11-026 As required Polyurethane Primer 16-001C As required Polyurethane Finish Paint (for External Applic.) 16-018C As required

References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-30-00, Page Block 001 06-31-53, Page Block 001 06-40-00, Page Block 001 Task 20-21-11-911-801 20-28-00, Page Block 201 Consumable Material List (CML) Drawing R51415000 R51415001 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12 (a) For the specification of the material numbers (Mat. No.), refer to Consumable Material List (CML). (b) Protect the areas to prevent damage to the equipment and structure and all the parts. (c) Clean the surfaces with Solvent General Purpose 11-026 As required (d) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001). (e) For the identification of zones, (Refer to AMM 06-20-00, Page Block 001).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 78 5

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# @A340-500/600
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(f) For the identification of access panels, (Refer to AMM 06-40-00, Page Block 001). (g) For the identification of stringers (Refer to AMM 06-30-00, Page Block 001). (h) For each area, check if the installed nut corresponds to nut ASNA2531-4. (identified by not having a spherical washer underneath and with correct diameter, refer to Standards Manual (SM)). 1 If not, leave the nut in place. 2 If it corresponds, do the operations described in SUBTASK 535056-832-001 008 Inspection / Repair . (i) For the removal and installation of fasteners (Refer to SRM 51-42-00). (j) Apply Interfay Sealant 09-005A As required to the interfaces of the structure and the reinstalled parts. (k) For fastener hole diameters, drill and deburr data (Refer to SRM 51-44-00). (l) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00). (m) To torque tighten the standard threaded fasteners (Refer to AMM Task 20-21-11-911-801). (n) Install the fasteners (wet assembly) with Interfay Sealant 09-005A As required (o) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201). (p) In fuel tanks, overcoat the nuts after replacement (Refer to SRM 51-76-12). (q) Renew the protective coating (Refer to SRM 51-23-12). (r) Renew the protective finish (Refer to SRM 51-75-12) with Polyurethane Primer 16-001C As required
Polyurethane Finish Paint (for External Applic.) 16-018C As required

(2) Subtask 535056-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 79 5

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# @A340-500/600
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**CONF 009 (1) Subtask 535056-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005A As required Solvent General Purpose 11-026 As required Polyurethane Primer 16-001C As required Polyurethane Finish Paint (for External Applic.) 16-018C As required

References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-30-00, Page Block 001 06-31-53, Page Block 001 06-40-00, Page Block 001 Task 20-21-11-911-801 20-28-00, Page Block 201 Consumable Material List (CML) Drawing R51415000 R51415001 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-44-00 51-75-12 51-76-12 (a) For the specification of the material numbers (Mat. No.), refer to Consumable Material List (CML). (b) Protect the areas to prevent damage to the equipment and structure and all the parts. (c) Clean the surfaces with Solvent General Purpose 11-026 As required (d) For the frames (FR) identification, (Refer to AMM 06-31-53, Page Block 001). (e) For the identification of zones, (Refer to AMM 06-20-00, Page Block 001).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 80 5

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(f) For the identification of access panels, (Refer to AMM 06-40-00, Page Block 001). (g) For the identification of stringers (Refer to AMM 06-30-00, Page Block 001). (h) For each area, check if the installed nut corresponds to nut ASNA2531-4. (identified by not having a spherical washer underneath and with correct diameter, refer to Standards Manual (SM)). 1 If not, leave the nut in place. 2 If it corresponds, do the operations described in SUBTASK 535056-832-001 009 Inspection / Repair . (i) For the removal and installation of fasteners (Refer to SRM 51-42-00). (j) Apply Interfay Sealant 09-005A As required to the interfaces of the structure and the reinstalled parts. (k) For fastener hole diameters, drill and deburr data (Refer to SRM 51-44-00). (l) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00). (m) To torque tighten the standard threaded fasteners (Refer to AMM Task 20-21-11-911-801). (n) Install the fasteners (wet assembly) with Interfay Sealant 09-005A As required (o) Do the electrical bonding (Refer to AMM 20-28-00, Page Block 201). (p) In fuel tanks, overcoat the nuts after replacement (Refer to SRM 51-76-12). (q) Renew the protective coating (Refer to SRM 51-23-12). (r) Renew the protective finish (Refer to SRM 51-75-12) with Polyurethane Primer 16-001C As required
Polyurethane Finish Paint (for External Applic.) 16-018C As required

(2) Subtask 535056-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 81 5

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**CONF ALL B. PREPARATION **CONF 001 (1) Subtask 535056-941-001-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 100 200 Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 25-21-41-000-801 Task 25-22-44-000-801 Task 25-23-41-000-801 Task 25-23-43-000-802 Task 25-23-44-000-801 Task 25-23-61-000-801 Task 25-24-61-000-801 Task 25-28-41-000-801 Task 25-28-42-000-803 Task 25-28-43-000-801 Task 25-37-41-000-801 Task 25-42-41-000-801 Task 25-42-42-000-801 Task 25-52-00-000-801 Task 25-53-00-000-801 Task 25-77-38-000-801 Task 25-80-00-000-801 Task 27-50-00-866-801 Task 52-10-00-010-801 Task 52-30-00-010-801 Task 52-30-00-480-801 Task 53-00-00-000-801 Task 53-00-00-000-802 Task 53-00-00-000-803 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put the access platform(s) in position. (c) Open the passenger/crew door 831 (Refer to AMM Task 52-10-00-010-801).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 82 5

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(d) In the cockpit, on the panel 235VU, make sure that these push-button switches are released : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B). (e) Open, safety and tag this (these) circuit breaker(s) PANEL DESIGNATION FIN LOCATION SEE NOTES 742 701PP 10PB1 72 S 742 702PP 10PB2 71 S (f) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to operate the push-button switches on the overhead panel : - 211VU (EMER ELEC PWR) ; - 235VU (ELEC). (g) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to start the APU. (h) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PWR A (B). (i) Make sure that there is warning notice at the access door 121EL to tell persons not to connect the external power connector(s). (j) Open the aft cargo compartment door 822 and FWD cargo compartment door 821 (Refer to AMM Task 52-30-00-010-801). 1 Install the safety lock (Refer to AMM Task 52-30-00-480-801). (k) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task 27-50-00-866-801). (l) Depending on aircraft configuration, remove only the necessary accesses to the work areas : 1 Remove the passenger seats (Refer to AMM Task 25-21-41-000-801). 2 Remove the cabin attendant seat (Refer to AMM Task 25-22-44-000-801). 3 Remove the lavatory H (Refer to AMM Task 25-42-41-000-801). 4 Remove the lavatory K (Refer to AMM Task 25-42-42-000-801). 5 Remove the cabin floor panels (Refer to AMM Task 53-00-00-000-801) and/or FWD cargo panels (Refer to AMM Task 53-00-00-000-802) and/or the aft cargo floor panels (Refer to AMM Task 53-00-00-000-803).
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 83 5

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6 Remove the floor panel 251XJ (Refer to AMM Task 53-00-00-000-801) 7 Remove the textile floor covering (Refer to AMM Task 25-28-41-000-801). 8 Remove the non-textile floor covering (Refer to AMM Task 25-28-42-000-803). 9 Remove the moisture barrier foil (Refer to AMM Task 25-28-43-000-801). 10 Remove FWD cargo LH sidewall panels 131XM, 131WM and RH sidewall panels 132XM or 132XN, 132WM (Refer to AMM Task 25-52-00-000-801). 11 If necessary, remove the water dispenser unit 6691NW (Refer to AMM Task 25-77-38-000-801). 12 If necessary, remove the lower deck galley 6710ML (Refer to AMM Task 25-37-41-000-801). 13 Remove aft cargo LH sidewall panels 151CM, 151DM and RH sidewall panels 152CM, 152DM (Refer to AMM Task 25-53-00-000-801). 14 Remove upper LH sidewall panels 251SN; 251TN and upper RH sidewall panels 252FM; 252SN and 252TN and necessary dado panels (Refer to AMM Task 25-23-43-000-802 and AMM Task 25-23-44-000-801). 15 Remove if necessary upper RH ceiling panels 252CA; 252DA; 252QE; 252RE and LH ceiling panels 251QE and 251RE (Refer to AMM Task 25-23-41-000-801). 16 Remove the lateral light covers (Refer to AMM Task 25-23-61-000-801). 17 Remove if necessary the overhead stowage-compartments at FR38 and/or FR54 (Refer to AMM Task 25-24-61-000-801). (m) Move the insulation blanket to get access to the work area and if necessary remove it (Refer to AMM Task 25-80-00-000-801). **CONF 002 (1) Subtask 535056-941-001-002 - Job Set-up Work Zones and Access Panels Zone Access/Work location 100 200 570 670 Manpower Resources Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 84 5

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References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 25-21-41-000-801 Task 25-22-44-000-801 Task 25-23-41-000-801 Task 25-23-43-000-802 Task 25-23-44-000-801 Task 25-23-61-000-801 Task 25-24-61-000-801 Task 25-28-41-000-801 Task 25-28-42-000-803 Task 25-28-43-000-801 Task 25-37-41-000-801 Task 25-42-41-000-801 Task 25-42-42-000-801 Task 25-52-00-000-801 Task 25-53-00-000-801 Task 25-77-38-000-801 Task 25-80-00-000-801 Task 27-50-00-866-801 28-10-00, Page Block 301 28-25-00, Page Block 301 Task 52-10-00-010-801 Task 52-30-00-010-801 Task 52-30-00-480-801 Task 53-00-00-000-801 Task 53-00-00-000-802 Task 53-00-00-000-803 Task 53-12-13-000-801 Task 57-17-11-000-801 Task 57-27-11-000-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put the access platform(s) in position. (c) Open the passenger/crew door 831 (Refer to AMM Task 52-10-00-010-801) (d) In the cockpit, on the panel 235VU, make sure that these push-button switches are released : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 85 5

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(e) Open, safety and tag this (these) circuit breaker(s) PANEL DESIGNATION FIN LOCATION SEE NOTES 742 701PP 10PB1 72 S 742 702PP 10PB2 71 S (f) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to operate the push-button switches on the overhead panel : - 211VU (EMER ELEC PWR) ; - 235VU (ELEC). (g) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to start the APU. (h) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PWR A (B). (i) Make sure that there is warning notice at the access door 121EL to tell persons not to connect the external power connector(s). (j) Open the FWD and aft cargo compartment doors 821 and 822 (Refer to AMM Task 52-30-00-010-801). 1 Install the safety locks (Refer to AMM Task 52-30-00-480-801). (k) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task 27-50-00-866-801). (l) Depending on aircraft configuration, remove only the necessary accesses to the work areas : 1 Open the access door 132AZ. 2 In electronic compartment, remove the floor panel 122JF at FR20 (Refer to AMM Task 53-12-13-000-801). 3 Remove the passenger seats (Refer to AMM Task 25-21-41-000-801). 4 Remove the cabin attendant seat (Refer to AMM Task 25-22-44-000-801). 5 Remove the lavatory H (Refer to AMM Task 25-42-41-000-801). 6 Remove the lavatory K (Refer to AMM Task 25-42-42-000-801). 7 Remove the avionics floor panels (Refer to AMM Task 53-12-13-000-801) and/or the cabin floor panels (Refer to AMM Task 53-00-00-000-801) and/or FWD cargo panels (Refer to AMM Task 53-00-00-000-802) and/or the aft cargo floor panels (Refer to AMM Task 53-00-00-000-803). 8 Remove the textile floor covering (Refer to AMM Task 25-28-41-000-801).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 86 5

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9 Remove the non-textile floor covering (Refer to AMM Task 25-28-42-000-803). 10 Remove the moisture barrier foil (Refer to AMM Task 25-28-43-000-801). 11 Remove FWD cargo LH sidewall panels 131XM, 131WM and RH sidewall panels 132XM or 132XN, 132WM (Refer to AMM Task 25-52-00-000-801). 12 If necessary, remove the water dispenser unit 6691NW (Refer to AMM Task 25-77-38-000-801). 13 If necessary, remove the lower deck galley 6710ML (Refer to AMM Task 25-37-41-000-801). 14 Remove aft cargo LH sidewall panels 151CM, 151DM (Refer to AMM Task 25-53-00-000-801). 15 Remove upper LH sidewall panels 251SN; 251TN and upper RH sidewall panels 252SN and 252TN and necessary dado panels (Refer to AMM Task 25-23-43-000-802 and AMM Task 25-23-44-000-801). 16 Remove if necessary upper RH ceiling panels 252CA; 252DA; 252QE; 252RE and LH ceiling panels 251QE and 251RE (Refer to AMM Task 25-23-41-000-801). 17 Remove LH sidewall panel 251BN and RH sidewall panel 252BN (Refer to AMM Task 25-23-43-000-802). 18 Remove the dado panels (Refer to AMM Task 25-23-44-000-801). 19 Remove the lateral light covers (Refer to AMM Task 25-23-61-000-801). 20 Remove if necessary the overhead stowage-compartments at FR38 and/or FR54 (Refer to AMM Task 25-24-61-000-801). (m) Move the insulation blanket to get access to the work area and if necessary remove it (Refer to AMM Task 25-80-00-000-801). (n) Depending on aircraft configuration and findings, access to center tank and inner tanks could be necessary and should be accomplished during 8C check. 1 You must obey the safety procedures when you work in fuel tanks (Refer to AMM 28-10-00, Page Block 301). 2 De-fuel and vent the concerned fuel tanks (Refer to AMM 28-25-00, Page Block 301). 3 Put all switches related to the fuel system to OFF. 4 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801). 5 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 87 5

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**CONF 003 (1) Subtask 535056-941-001-003 - Job Set-up Work Zones and Access Panels Zone Access/Work location 570 670 Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 27-50-00-866-801 Task 32-12-00-010-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put the access platform(s) in position. (c) Open the MLG door for maintenance (Refer to AMM Task 32-12-00-010-801) (d) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task 27-50-00-866-801). **CONF 004 (1) Subtask 535056-941-001-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 100 200 Manpower Resources Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 88 5

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# @A340-500/600
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References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 25-21-41-000-801 Task 25-22-44-000-801 Task 25-23-41-000-801 Task 25-23-43-000-802 Task 25-23-44-000-801 Task 25-23-61-000-801 Task 25-24-61-000-801 Task 25-28-41-000-801 Task 25-28-42-000-803 Task 25-28-43-000-801 Task 25-37-41-000-801 Task 25-42-41-000-801 Task 25-42-42-000-801 Task 25-52-00-000-801 Task 25-53-00-000-801 Task 25-77-38-000-801 Task 25-80-00-000-801 Task 27-50-00-866-801 Task 52-10-00-010-801 Task 52-30-00-010-801 Task 52-30-00-480-801 Task 53-00-00-000-801 Task 53-00-00-000-802 Task 53-00-00-000-803 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put the access platform(s) in position. (c) Open the passenger/crew door 831 (Refer to AMM Task 52-10-00-010-801). (d) In the cockpit, on the panel 235VU, make sure that these push-button switches are released : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B). (e) Open, safety and tag this (these) circuit breaker(s) PANEL DESIGNATION FIN LOCATION SEE NOTES 742 701PP 10PB1 72 S 742 702PP 10PB2 71 S

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 89 5

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(f) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to operate the push-button switches on the overhead panel : - 211VU (EMER ELEC PWR) ; - 235VU (ELEC). (g) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to start the APU. (h) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PWR A (B). (i) Make sure that there is warning notice at the access door 121EL to tell persons not to connect the external power connector(s). (j) Open the aft cargo compartment door 822 and FWD cargo compartment door 821 (Refer to AMM Task 52-30-00-010-801). 1 Install the safety lock (Refer to AMM Task 52-30-00-480-801). (k) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task 27-50-00-866-801). (l) Depending on aircraft configuration, remove only the necessary accesses to the work areas : 1 Remove the passenger seats (Refer to AMM Task 25-21-41-000-801). 2 Remove the cabin attendant seat (Refer to AMM Task 25-22-44-000-801). 3 Remove the lavatory H (Refer to AMM Task 25-42-41-000-801). 4 Remove the lavatory K (Refer to AMM Task 25-42-42-000-801). 5 Remove the cabin floor panels (Refer to AMM Task 53-00-00-000-801) and/or FWD cargo panels (Refer to AMM Task 53-00-00-000-802) and/or the aft cargo floor panels (Refer to AMM Task 53-00-00-000-803). 6 Remove the floor panel 251XJ (Refer to AMM Task 53-00-00-000-801) 7 Remove the textile floor covering (Refer to AMM Task 25-28-41-000-801). 8 Remove the non-textile floor covering (Refer to AMM Task 25-28-42-000-803). 9 Remove the moisture barrier foil (Refer to AMM Task 25-28-43-000-801). 10 Remove FWD cargo LH sidewall panels 131XM, 131WM and RH sidewall panels 132XM or 132XN, 132WM (Refer to AMM Task 25-52-00-000-801). 11 If necessary, remove the water dispenser unit 6691NW (Refer to AMM Task 25-77-38-000-801).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 90 5

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12 If necessary, remove the lower deck galley 6710ML (Refer to AMM Task 25-37-41-000-801). 13 Remove aft cargo LH sidewall panels 151CM, 151DM and RH sidewall panels 152CM, 152DM (Refer to AMM Task 25-53-00-000-801). 14 Remove upper LH sidewall panels 251SN; 251TN and upper RH sidewall panels 252FM; 252SN and 252TN and necessary dado panels (Refer to AMM Task 25-23-43-000-802 and AMM Task 25-23-44-000-801). 15 Remove if necessary upper RH ceiling panels 252CA; 252DA; 252QE; 252RE and LH ceiling panels 251QE and 251RE (Refer to AMM Task 25-23-41-000-801). 16 Remove the lateral light covers (Refer to AMM Task 25-23-61-000-801). 17 Remove if necessary the overhead stowage-compartments at FR38 and/or FR54 (Refer to AMM Task 25-24-61-000-801). (m) Move the insulation blanket to get access to the work area and if necessary remove it (Refer to AMM Task 25-80-00-000-801). **CONF 005 (1) Subtask 535056-941-001-005 - Job Set-up Work Zones and Access Panels Zone Access/Work location 100 570 670 200 Manpower Resources Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 91 5

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References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 25-21-41-000-801 Task 25-22-44-000-801 Task 25-23-41-000-801 Task 25-23-43-000-802 Task 25-23-44-000-801 Task 25-23-61-000-801 Task 25-24-61-000-801 Task 25-28-41-000-801 Task 25-28-42-000-803 Task 25-28-43-000-801 Task 25-32-84-000-801 Task 25-42-41-000-801 Task 25-42-42-000-801 Task 25-52-00-000-801 Task 25-53-00-000-801 Task 25-80-00-000-801 Task 27-50-00-866-801 Task 52-10-00-010-801 Task 52-30-00-010-801 Task 52-30-00-480-801 Task 53-00-00-000-801 Task 53-00-00-000-802 Task 53-00-00-000-803 Task 53-12-13-000-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put the access platform(s) in position. (c) Open the passenger/crew door 831 (Refer to AMM Task 52-10-00-010-801) (d) In the cockpit, on the panel 235VU, make sure that these push-button switches are released : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B). (e) Open, safety and tag this (these) circuit breaker(s) PANEL DESIGNATION FIN LOCATION SEE NOTES 742 701PP 10PB1 72 S 742 702PP 10PB2 71 S

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 92 5

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(f) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to operate the push-button switches on the overhead panel : - 211VU (EMER ELEC PWR) ; - 235VU (ELEC). (g) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to start the APU. (h) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PWR A (B). (i) Make sure that there is warning notice at the access door 121EL to tell persons not to connect the external power connector(s). (j) Open FWD and aft cargo compartment doors 821 and 822 (Refer to AMM Task 52-30-00-010-801). 1 Install the safety lock (Refer to AMM Task 52-30-00-480-801). (k) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task 27-50-00-866-801). (l) Depending on aircraft configuration, remove only the necessary accesses to the work areas : 1 Open the access door 132AZ. 2 In electronic compartment, remove the floor panel 122JF at FR20 (Refer to AMM Task 53-12-13-000-801). 3 Remove the mid galley unit (Refer to AMM Task 25-32-84-000-801). 4 Remove the passenger seats (Refer to AMM Task 25-21-41-000-801). 5 Remove the cabin attendant seat (Refer to AMM Task 25-22-44-000-801). 6 Remove the lavatory H (Refer to AMM Task 25-42-41-000-801). 7 Remove the lavatory K (Refer to AMM Task 25-42-42-000-801). 8 Remove the cabin floor panels (Refer to AMM Task 53-00-00-000-801) and/or FWD cargo panels (Refer to AMM Task 53-00-00-000-802) and/or the aft cargo floor panels (Refer to AMM Task 53-00-00-000-803). 9 Remove the textile floor covering (Refer to AMM Task 25-28-41-000-801). 10 Remove the non-textile floor covering (Refer to AMM Task 25-28-42-000-803). 11 Remove the moisture barrier foil (Refer to AMM Task 25-28-43-000-801). 12 Remove FWD cargo LH sidewall panels 131XM, 131WM and RH sidewall panels 132XM or 132XN, 132WM (Refer to AMM Task 25-52-00-000-801). DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 93 5

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13 Remove aft cargo LH sidewall panels 151UM, 151VM and RH sidewall panels 152UM, 152VM (Refer to AMM Task 25-53-00-000-801). 14 Remove upper LH sidewall panels 251EM; 251CN; 251DN and upper RH sidewall panels 262CN and 262DN and necessary dado panels (Refer to AMM Task 25-23-43-000-802 and AMM Task 25-23-44-000-801). 15 Remove if necessary upper RH ceiling panels 252CA; 252DA; 262EE; 262FE and LH ceiling panels 251CA; 251DA; 261EE and 261FE (Refer to AMM Task 25-23-41-000-801). 16 Remove the lateral light covers (Refer to AMM Task 25-23-61-000-801). 17 Remove if necessary the overhead stowage-compartments at FR38 and/or FR54 (Refer to AMM Task 25-24-61-000-801). (m) Move the insulation blanket to get access to the work area and if necessary remove it (Refer to AMM Task 25-80-00-000-801). **CONF 006 (1) Subtask 535056-941-001-008 - Job Set-up Work Zones and Access Panels Zone Access/Work location 100 200 540 570 670 Manpower Resources Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 94 5

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References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 25-21-41-000-801 Task 25-22-44-000-801 Task 25-23-41-000-801 Task 25-23-43-000-802 Task 25-23-44-000-801 Task 25-23-61-000-801 Task 25-24-61-000-801 Task 25-28-41-000-801 Task 25-28-42-000-803 Task 25-28-43-000-801 Task 25-32-84-000-801 Task 25-42-41-000-801 Task 25-42-42-000-801 Task 25-52-00-000-801 Task 25-53-00-000-801 Task 25-80-00-000-801 Task 27-50-00-866-801 28-10-00, Page Block 301 28-25-00, Page Block 301 Task 52-10-00-010-801 Task 52-30-00-010-801 Task 52-30-00-480-801 Task 53-00-00-000-801 Task 53-00-00-000-802 Task 53-00-00-000-803 Task 53-12-13-000-801 Task 57-17-11-000-801 Task 57-27-11-000-801 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put the access platform(s) in position. (c) Open the passenger/crew door 831 (Refer to AMM Task 52-10-00-010-801) (d) In the cockpit, on the panel 235VU, make sure that these push-button switches are released : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B). (e) Open, safety and tag this (these) circuit breaker(s) PANEL DESIGNATION FIN LOCATION SEE NOTES 742 701PP 10PB1 72 S 742 702PP 10PB2 71 S
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 95 5

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(f) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to operate the push-button switches on the overhead panel : - 211VU (EMER ELEC PWR) ; - 235VU (ELEC). (g) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to start the APU. (h) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PWR A (B). (i) Make sure that there is warning notice at the access door 121EL to tell persons not to connect the external power connector(s). (j) Open FWD and aft cargo compartment doors 821 and 822 (Refer to AMM Task 52-30-00-010-801). 1 Install the safety lock (Refer to AMM Task 52-30-00-480-801). (k) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task 27-50-00-866-801). (l) Depending on aircraft configuration, remove only the necessary accesses to the work areas : 1 Open the access door 132AZ. 2 In electronic compartment, remove the floor panel 122JF at FR20 (Refer to AMM Task 53-12-13-000-801). 3 Remove the mid galley unit (Refer to AMM Task 25-32-84-000-801). 4 Remove the passenger seats (Refer to AMM Task 25-21-41-000-801). 5 Remove the cabin attendant seat (Refer to AMM Task 25-22-44-000-801). 6 Remove the lavatory H (Refer to AMM Task 25-42-41-000-801). 7 Remove the lavatory K (Refer to AMM Task 25-42-42-000-801). 8 Remove the cabin floor panels (Refer to AMM Task 53-00-00-000-801) and/or FWD cargo panels (Refer to AMM Task 53-00-00-000-802) and/or the aft cargo floor panels (Refer to AMM Task 53-00-00-000-803). 9 Remove the textile floor covering (Refer to AMM Task 25-28-41-000-801). 10 Remove the non-textile floor covering (Refer to AMM Task 25-28-42-000-803). 11 Remove the moisture barrier foil (Refer to AMM Task 25-28-43-000-801). 12 Remove FWD cargo LH sidewall panels 131XM, 131WM and RH sidewall panels 132XM or 132XN, 132WM (Refer to AMM Task 25-52-00-000-801). DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 96 5

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13 Remove aft cargo LH sidewall panels 151UM, 151VM and RH sidewall panels 152UM, 152VM (Refer to AMM Task 25-53-00-000-801). 14 Remove upper LH sidewall panels 251EM; 251FM; 251CN; 251DN and upper RH sidewall panels 262CN and 262DN and necessary dado panels (Refer to AMM Task 25-23-43-000-802 and AMM Task 25-23-44-000-801). 15 Remove if necessary upper RH ceiling panels 252CA; 252DA; 262EE; 262FE and LH ceiling panels 251CA; 251DA; 261EE and 261FE (Refer to AMM Task 25-23-41-000-801). 16 Remove the lateral light covers (Refer to AMM Task 25-23-61-000-801). 17 Remove if necessary the overhead stowage-compartments at FR38 and/or FR54 (Refer to AMM Task 25-24-61-000-801). (m) Move the insulation blanket to get access to the work area and if necessary remove it (Refer to AMM Task 25-80-00-000-801). (n) Depending on aircraft configuration and findings, access to center tank and inner tanks could be necessary and should be accomplished during 8C check. 1 You must obey the safety procedures when you work in fuel tanks (Refer to AMM 28-10-00, Page Block 301). 2 De-fuel and vent the concerned fuel tanks (Refer to AMM 28-25-00, Page Block 301). 3 Put all switches related to the fuel system to OFF. 4 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801). 5 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801). **CONF 007 (1) Subtask 535056-941-001-006 - Job Set-up Work Zones and Access Panels Zone Access/Work location 100 200 570 670 Manpower Resources Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 97 5

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References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 21-52-41-000-801 Task 21-53-51-000-801 Task 25-21-41-000-801 Task 25-22-44-000-801 Task 25-23-41-000-801 Task 25-23-43-000-802 Task 25-23-44-000-801 Task 25-23-61-000-801 Task 25-24-61-000-801 Task 25-28-41-000-801 Task 25-28-42-000-803 Task 25-28-43-000-801 Task 25-32-84-000-801 Task 25-42-41-000-801 Task 25-42-42-000-801 Task 25-52-00-000-801 Task 25-53-00-000-801 Task 25-80-00-000-801 Task 27-50-00-866-801 28-10-00, Page Block 301 28-25-00, Page Block 301 Task 32-12-00-010-801 Task 52-10-00-010-801 Task 52-30-00-010-801 Task 52-30-00-480-801 Task 53-00-00-000-801 Task 53-00-00-000-802 Task 53-00-00-000-803 Task 53-12-13-000-801 Task 53-35-11-000-802 Task 53-35-13-000-801 Task 53-35-13-000-802 Task 57-17-11-000-801 Task 57-27-11-000-801 Fig. A-FBAAA Canted beam attachment FWD of FR53-2 LH, Removal of the Pipes Support for Access Sheet 01 Sheet 02
Fig. A-FBBAA Canted beam attachment FWD of FR53-2 RH, Removal of the Pipes Support for Access Sheet 01 Sheet 02

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put the access platform(s) in position. (c) Open the passenger/crew door 831 (Refer to AMM Task 52-10-00-010-801)

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 98 5

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# @A340-500/600
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(d) In the cockpit, on the panel 235VU, make sure that these push-button switches are released : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B). (e) Open, safety and tag this (these) circuit breaker(s) PANEL DESIGNATION FIN LOCATION SEE NOTES 742 701PP 10PB1 72 S 742 702PP 10PB2 71 S (f) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to operate the push-button switches on the overhead panel : - 211VU (EMER ELEC PWR) ; - 235VU (ELEC). (g) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to start the APU. (h) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PWR A (B). (i) Make sure that there is warning notice at the access door 121EL to tell persons not to connect the external power connector(s). (j) Open FWD and aft cargo compartment doors 821 and 822 (Refer to AMM Task 52-30-00-010-801). 1 Install the safety lock (Refer to AMM Task 52-30-00-480-801). (k) Open the MLG door for maintenance (Refer to AMM Task 32-12-00-010-801). (l) In order to get access to area 12, remove the pipe support from LH canted beam attachment FWD of FR53.2 as described in Fig. A-FBAAA

. 1 Remove and retain the 2 fasteners (1) and (2) from the pipe. NOTE: Do not disconnect the pipe. 2 Remove and retain the 3 fasteners (3) and (4) from the support item (5). 3 Move slightly the support item (5) to gain access to work area.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 99 5

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(m) In order to get access to area 13, remove the pipes support from RH canted beam attachment FWD of FR53.2 as described in Fig. A-FBBAA

. 1 Remove and retain the fasteners (9) and (10) from the clamp of the pipe. NOTE: Do not disconnect the pipe. 2 Remove and retain the 6 fasteners (1), (6) and (7) from the support item (8). 3 Remove and retain the 6 fasteners (3) and (10) from the support item (8). 4 Move slightly the support item (8) to gain access to work area. (n) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task 27-50-00-866-801). (o) Depending on aircraft configuration, remove only the necessary accesses to the work areas : 1 Open the access door 132AZ. 2 In electronic compartment, remove the floor panel 122JF at FR20 (Refer to AMM Task 53-12-13-000-801). 3 If installed, remove the passenger seats (Refer to AMM Task 25-21-41-000-801). 4 If installed, remove the mid galley unit (Refer to AMM Task 25-32-84-000-801). 5 Remove the cabin attendant seat (Refer to AMM Task 25-22-44-000-801). 6 Remove the lavatory H (Refer to AMM Task 25-42-41-000-801). 7 Remove the lavatory K (Refer to AMM Task 25-42-42-000-801). 8 Remove the cabin floor panels (Refer to AMM Task 53-00-00-000-801) and/or FWD cargo panels (Refer to AMM Task 53-00-00-000-802) and/or the aft cargo floor panels (Refer to AMM Task 53-00-00-000-803). 9 Remove the floor panel 251XJ (Refer to AMM Task 53-00-00-000-801) 10 Remove the textile floor covering (Refer to AMM Task 25-28-41-000-801). 11 Remove the non-textile floor covering (Refer to AMM Task 25-28-42-000-803). 12 Remove the moisture barrier foil (Refer to AMM Task 25-28-43-000-801). 13 Remove FWD cargo LH sidewall panels 131XM, 131WM and RH sidewall panels 132XM or 132XN, 132WM (Refer to AMM Task 25-52-00-000-801). 14 Remove the FWD cargo partition panels 132DX, 132CX, 131BX, 131CX and 131DX (Refer to AMM Task 25-52-00-000-801).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 100 5

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# @A340-500/600
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15 Remove aft cargo LH sidewall panels 151UM, 151VM and RH sidewall panels 152UM, 152VM (Refer to AMM Task 25-53-00-000-801). 16 Remove if necessary upper LH sidewall panels 251EM; 251FM; 251BN; 251CN; 251DN and upper RH sidewall panels 251BN; 262CN and 262DN (Refer to AMM Task 25-23-43-000-802). 17 Remove if necessary upper RH ceiling panels 252CA; 252DA; 262EE; 262FE and LH ceiling panels 251CA; 251DA; 261EE and 261FE (Refer to AMM Task 25-23-41-000-801). 18 Remove the lateral light covers (Refer to AMM Task 25-23-61-000-801). 19 Remove if necessary the overhead stowage-compartments at FR38 and/or FR54 (Refer to AMM Task 25-24-61-000-801). 20 Remove the dado panels (Refer to AMM Task 25-23-44-000-801). 21 Remove the fairing panels (Refer to AMM Task 53-35-13-000-801). 22 Remove the fairing panels (Refer to AMM Task 53-35-13-000-802). 23 Remove LH and RH fairing panels (Refer to AMM Task 53-35-11-000-802). (p) Move the insulation blanket to get access to the work area and if necessary remove it (Refer to AMM Task 25-80-00-000-801). (q) Remove LH and RH air conditioning packs 521HH and 522HH (Refer to AMM Task 21-52-41-000-801). (r) Remove LH and RH air inlet assemblies 533HH and 534HH (Refer to AMM Task 21-53-51-000-801). (s) Depending on aircraft configuration and findings, access to center tank and inner tanks could be necessary and should be accomplished during 8C check. 1 You must obey the safety procedures when you work in fuel tanks (Refer to AMM 28-10-00, Page Block 301). 2 De-fuel and vent the concerned fuel tanks (Refer to AMM 28-25-00, Page Block 301). 3 Put all switches related to the fuel system to OFF. 4 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801). 5 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 101 5

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**CONF 008 (1) Subtask 535056-941-001-006 - Job Set-up Work Zones and Access Panels Zone Access/Work location 100 200 570 670 Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 21-52-41-000-801 Task 21-53-51-000-801 Task 25-21-41-000-801 Task 25-22-44-000-801 Task 25-23-41-000-801 Task 25-23-43-000-802 Task 25-23-44-000-801 Task 25-23-61-000-801 Task 25-24-61-000-801 Task 25-28-41-000-801 Task 25-28-42-000-803 Task 25-28-43-000-801 Task 25-32-84-000-801 Task 25-42-41-000-801 Task 25-42-42-000-801 Task 25-52-00-000-801 Task 25-53-00-000-801 Task 25-80-00-000-801 Task 27-50-00-866-801 28-10-00, Page Block 301 28-25-00, Page Block 301 Task 32-12-00-010-801 Task 52-10-00-010-801 Task 52-30-00-010-801 Task 52-30-00-480-801 Task 53-00-00-000-801 Task 53-00-00-000-802 Task 53-00-00-000-803 Task 53-12-13-000-801 Task 53-35-11-000-802 Task 53-35-13-000-801 Task 53-35-13-000-802 Task 57-17-11-000-801 Task 57-27-11-000-801

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 102 5

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References Fig. A-FBAAA Canted beam attachment FWD of FR53-2 LH, Removal of the Pipes Support for Access Sheet 01 Sheet 02
Fig. A-FBBAA Canted beam attachment FWD of FR53-2 RH, Removal of the Pipes Support for Access Sheet 01 Sheet 02

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put the access platform(s) in position. (c) Open the passenger/crew door 831 (Refer to AMM Task 52-10-00-010-801) (d) In the cockpit, on the panel 235VU, make sure that these push-button switches are released : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B). (e) Open, safety and tag this (these) circuit breaker(s) PANEL DESIGNATION FIN LOCATION SEE NOTES 742 701PP 10PB1 72 S 742 702PP 10PB2 71 S (f) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to operate the push-button switches on the overhead panel : - 211VU (EMER ELEC PWR) ; - 235VU (ELEC). (g) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to start the APU. (h) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PWR A (B). (i) Make sure that there is warning notice at the access door 121EL to tell persons not to connect the external power connector(s). (j) Open FWD and aft cargo compartment doors 821 and 822 (Refer to AMM Task 52-30-00-010-801). 1 Install the safety lock (Refer to AMM Task 52-30-00-480-801).
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 103 5

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# @A340-500/600
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(k) Open the MLG door for maintenance (Refer to AMM Task 32-12-00-010-801). (l) In order to get access to area 12, remove the pipe support from LH canted beam attachment FWD of FR53.2 as described in Fig. A-FBAAA

. 1 Remove and retain the 2 fasteners (1) and (2) from the pipe. NOTE: Do not disconnect the pipe. 2 Remove and retain the 3 fasteners (3) and (4) from the support item (5). 3 Move slightly the support item (5) to gain access to work area. (m) In order to get access to area 13, remove the pipes support from RH canted beam attachment FWD of FR53.2 as described in Fig. A-FBBAA

. 1 Remove and retain the fasteners (9) and (10) from the clamp of the pipe. NOTE: Do not disconnect the pipe. 2 Remove and retain the 6 fasteners (1), (6) and (7) from the support item (8). 3 Remove and retain the 6 fasteners (3) and (10) from the support item (8). 4 Move slightly the support item (8) to gain access to work area. (n) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task 27-50-00-866-801). (o) Depending on aircraft configuration, remove only the necessary accesses to the work areas : 1 Open the access door 132AZ. 2 In electronic compartment, remove the floor panel 122JF at FR20 (Refer to AMM Task 53-12-13-000-801). 3 If installed, remove the passenger seats (Refer to AMM Task 25-21-41-000-801). 4 If installed, remove the mid galley unit (Refer to AMM Task 25-32-84-000-801). 5 Remove the cabin attendant seat (Refer to AMM Task 25-22-44-000-801). 6 Remove the lavatory H (Refer to AMM Task 25-42-41-000-801). 7 Remove the lavatory K (Refer to AMM Task 25-42-42-000-801). 8 Remove the cabin floor panels (Refer to AMM Task 53-00-00-000-801) and/or FWD cargo panels (Refer to AMM Task 53-00-00-000-802) and/or the aft cargo floor panels (Refer to AMM Task 53-00-00-000-803). 9 Remove the floor panel 251XJ (Refer to AMM Task 53-00-00-000-801) DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 104 5

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10 Remove the textile floor covering (Refer to AMM Task 25-28-41-000-801). 11 Remove the non-textile floor covering (Refer to AMM Task 25-28-42-000-803). 12 Remove the moisture barrier foil (Refer to AMM Task 25-28-43-000-801). 13 Remove FWD cargo LH sidewall panels 131XM, 131WM and RH sidewall panels 132XM or 132XN, 132WM (Refer to AMM Task 25-52-00-000-801). 14 Remove the FWD cargo partition panels 132DX, 132CX, 131BX, 131CX and 131DX (Refer to AMM Task 25-52-00-000-801). 15 Remove aft cargo LH sidewall panels 151UM, 151VM and RH sidewall panels 152UM, 152VM (Refer to AMM Task 25-53-00-000-801). 16 Remove if necessary upper LH sidewall panels 251EM; 251FM; 251BN; 251CN; 251DN and upper RH sidewall panels 251BN; 262CN and 262DN (Refer to AMM Task 25-23-43-000-802). 17 Remove if necessary upper RH ceiling panels 252CA; 252DA; 262EE; 262FE and LH ceiling panels 251CA; 251DA; 261EE and 261FE (Refer to AMM Task 25-23-41-000-801). 18 Remove the lateral light covers (Refer to AMM Task 25-23-61-000-801). 19 Remove if necessary the overhead stowage-compartments at FR38 and/or FR54 (Refer to AMM Task 25-24-61-000-801). 20 Remove the dado panels (Refer to AMM Task 25-23-44-000-801). 21 Remove the fairing panels (Refer to AMM Task 53-35-13-000-801). 22 Remove the fairing panels (Refer to AMM Task 53-35-13-000-802). 23 Remove LH and RH fairing panels (Refer to AMM Task 53-35-11-000-802). (p) Move the insulation blanket to get access to the work area and if necessary remove it (Refer to AMM Task 25-80-00-000-801). (q) Remove LH and RH air conditioning packs 521HH and 522HH (Refer to AMM Task 21-52-41-000-801). (r) Remove LH and RH air inlet assemblies 533HH and 534HH (Refer to AMM Task 21-53-51-000-801). (s) Depending on aircraft configuration and findings, access to center tank and inner tanks could be necessary and should be accomplished during 8C check. 1 You must obey the safety procedures when you work in fuel tanks (Refer to AMM 28-10-00, Page Block 301). 2 De-fuel and vent the concerned fuel tanks (Refer to AMM 28-25-00, Page Block 301).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 105 5

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3 Put all switches related to the fuel system to OFF. 4 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801). 5 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801). **CONF 009 (1) Subtask 535056-941-001-007 - Job Set-up Work Zones and Access Panels Zone Access/Work location 100 200 Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 25-23-43-000-802 Task 25-23-61-000-801 Task 25-52-00-000-801 Task 25-80-00-000-801 Task 52-10-00-010-801 Task 52-30-00-010-801 Task 52-30-00-480-801 Task 53-35-13-000-802 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Put the access platform(s) in position. (c) Open the passenger/crew door 831 (Refer to AMM Task 52-10-00-010-801) (d) In the cockpit, on the panel 235VU, make sure that these push-button switches are released : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B). (e) Open, safety and tag this (these) circuit breaker(s) PANEL DESIGNATION FIN LOCATION SEE NOTES 742 701PP 10PB1 72 S 742 702PP 10PB2 71 S

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 106 5

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(f) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to operate the push-button switches on the overhead panel : - 211VU (EMER ELEC PWR) ; - 235VU (ELEC). (g) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to start the APU. (h) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PWR A (B). (i) Make sure that there is warning notice at the access door 121EL to tell persons not to connect the external power connector(s). (j) Open FWD cargo compartment door 821 (Refer to AMM Task 52-30-00-010-801). 1 Install the safety lock (Refer to AMM Task 52-30-00-480-801). (k) Depending on aircraft configuration, remove only the necessary accesses to the work areas : 1 Remove LH sidewall panel 131XM and RH sidewall panel 132XM; LH partition panels 131BX; 131CX; 131DX and RH partition panels 132CX; 132DX; and if necessary LH ceiling panel 132XA and RH ceiling panel 131XA (Refer to AMM Task 25-52-00-000-801). 2 Remove the fairing panels (Refer to AMM Task 53-35-13-000-802). 3 Remove LH sidewall panel 251BN and RH sidewall panel 252BN (Refer to AMM Task 25-23-43-000-802). 4 Remove upper LH sidewall panel 251DN and upper RH sidewall panel 252DN (Refer to AMM Task 25-23-43-000-802). 5 Remove the lateral light covers (Refer to AMM Task 25-23-61-000-801). (l) Move the insulation blanket to get access to the work area and if necessary remove it (Refer to AMM Task 25-80-00-000-801). **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 535056-832-001-001 - Inspection / Repair Work Zones and Access Panels Zone Access/Work location 100 200
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 107 5

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570 670 Manpower Resources Manhours 4.00 Minimum number of person 4 Subtask elapsed time 1.00 Skills AIRFRAME References Drawing R51415000 R51415001 Fig. A-FBCAA Flow Chart Sheet 01 (a) Perform a visual inspection of the nuts looking for cracked or missing nuts as described inFig. A-FBCAA: 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 18, 20, 21 and areas concessions 1 and 2. - For the inspection areas, refer to Repair Instruction (RI) R51415000 and Repair Instruction (RI) R51415001. - For the inspection report, refer to Appendix 01 Inspection Report. . 3 If no findings, replace the nut before next flight. (b) Replacement principle of the nut : 1 Remove half of the required nuts equally spread.
a Remove the nut using an ALLEN key to maintain the fastener. 2 Install new nuts.
a Install the nut using an ALLEN key to maintain the fastener. 3 Perform the replacement of the half remaining nuts. NOTE: If the fastener rotates, refer to Repair Instruction (RI) R51415000 and Repair Instruction (RI) R51415001.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 108 5

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(2) Subtask 535056-960-028-001 - Area 18, replace nuts from rear section FR54 stringer 54 LH sideWork Zones and Access Panels Zone Access/Work location 260 Work location Frame 54 Stringer 54 Manpower Resources Manhours 4.00 Minimum number of person 2 Subtask elapsed time 2.00 Skills AIRFRAME Material necessary to do the job Component COMPA28 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 33 NUT Replace 33 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 33 Nut ASNA2531-4 Discard (b) Install : 33 Nut ASNA2531-4

(3) Subtask 535056-960-030-001 - Area 20, replace nuts from LH and RH fixed inner shroud boxes Work Zones and Access Panels Zone Access/Work location 570 670 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 109 5

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Material necessary to do the job Component COMPA31 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 16 NUT Replace 16 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 8 nuts on LH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4 (b) Replace 8 nuts on RH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4

(4) Subtask 535056-960-031-001 - Area 21, replace nuts at FR38 and FR54 circumferential junctions Work Zones and Access Panels Zone Access/Work location 100 Work location Frame 38 Frame 54 200 Work location Frame 38 Frame 54 Manpower Resources Manhours 6.00 Minimum number of person 2 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Component COMPA32 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 59 NUT

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 110 5

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SERVICE BULLETIN

References Drawing R51415001 Replace 59 nuts as described in Repair Instruction (RI) R51415001. (a) Remove : 59 Nut ASNA2531-4 Discard (b) Install : 59 Nut ASNA2531-4

(5) Subtask 535056-960-032-001 - Area concession 1 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME Material necessary to do the job Component COMPA40 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 1 NUT References Drawing R51415001 Replace 1 nut as described in Repair Instruction (RI) R51415001. (a) Remove : 1 Nut ASNA2531-4 Discard (b) Install : 1 Nut ASNA2531-4

(6) Subtask 535056-960-033-001 - Area concession 2 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 111 5

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

# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA41 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 1 NUT References Drawing R51415001 Replace 1 nut as described in Repair Instruction (RI) R51415001. (a) Remove : 1 Nut ASNA2531-4 Discard (b) Install : 1 Nut ASNA2531-4 **CONF 002 (1) Subtask 535056-832-001-003 - Inspection / Repair Work Zones and Access Panels Zone Access/Work location 100 200 570 670 Manpower Resources Manhours 4.00 Minimum number of person 4 Subtask elapsed time 1.00 Skills AIRFRAME References Drawing R51415000 R51415001 Fig. A-FBCAA Flow Chart Sheet 01 (a) Perform a visual inspection of the nuts looking for cracked or missing nuts as described inFig. A-FBCAA: 1 In case of missing nut, contact Airbus before next flight for additional instructions.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 112 5

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# @A340-500/600
SERVICE BULLETIN

2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 1b, 14, 18, 19, 20, 21 and areas concessions 1 and 2. - For the inspection areas, refer to Repair Instruction (RI) R51415000 and Repair Instruction (RI) R51415001. - For the inspection report, refer to Appendix 01 Inspection Report. . 3 If no findings, replace the nut before next flight. (b) Replacement principle of the nut : 1 Remove half of the required nuts equally spread.
a Remove the nut using an ALLEN key to maintain the fastener. 2 Install new nuts.
a Install the nut using an ALLEN key to maintain the fastener. 3 Perform the replacement of the half remaining nuts. NOTE: If the fastener rotates, refer to Repair Instruction (RI) R51415000 and Repair Instruction (RI) R51415001. (2) Subtask 535056-960-002-001 - Area 1a, replace the nuts in FWD LH hard points Work Zones and Access Panels Zone Access/Work location 120 Access Door 821, Door 132AZ Work location from Frame 16 to Frame 17 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 2 NUT References Drawing R51415000
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 113 5

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# @A340-500/600
SERVICE BULLETIN
Replace 2 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 2 Nut ASNA2531-4 Discard (b) Install : 2 Nut ASNA2531-4

(3) Subtask 535056-960-001-001 - Area 1a, replace the nuts in FWD RH hard points Work Zones and Access Panels Zone Access/Work location 120 Access Door 821, Door 132AZ Work location from Frame 16 to Frame 17 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 2 NUT References Drawing R51415000 Replace 2 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 2 Nut ASNA2531-4 Discard (b) Install : 2 Nut ASNA2531-4

(4) Subtask 535056-960-003-001 - Area 1b, replace nuts of 800VU RH support Work Zones and Access Panels Zone Access/Work location 120 Access Door 821, Door 132AZ Work location from Frame 19 to Frame 20

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 114 5

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# @A340-500/600
SERVICE BULLETIN
Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA03 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 4 NUT References Drawing R51415000 Replace 4 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 4 Nut ASNA2531-4 Discard (b) Install : 4 Nut ASNA2531-4

(5) Subtask 535056-960-024-001 - Area 14, replace nuts from LH and RH dado panel support struts Work Zones and Access Panels Zone Access/Work location 250 Work location from Frame 40-1 to Frame 43 from Stringer 25 to Stringer 27 Manpower Resources Manhours 4.00 Minimum number of person 2 Subtask elapsed time 2.00 Skills AIRFRAME Material necessary to do the job Component COMPA23 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 40 NUT Replace 40 nuts as described in Repair Instruction (RI) R51415000.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 115 5

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# @A340-500/600
SERVICE BULLETIN
(a) Replace 20 nuts on LH side. 1 Remove : 20 Nut ASNA2531-4 Discard 2 Install : 20 Nut ASNA2531-4 (b) Replace 20 nuts on RH side. 1 Remove : 20 Nut ASNA2531-4 Discard 2 Install : 20 Nut ASNA2531-4

(6) Subtask 535056-960-028-001 - Area 18, replace nuts from rear section FR54 stringer 54 LH sideWork Zones and Access Panels Zone Access/Work location 260 Work location Frame 54 Stringer 54 Manpower Resources Manhours 4.00 Minimum number of person 2 Subtask elapsed time 2.00 Skills AIRFRAME Material necessary to do the job Component COMPA28 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 33 NUT Replace 33 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 33 Nut ASNA2531-4 Discard (b) Install : 33 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 116 5

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

# @A340-500/600
SERVICE BULLETIN
(7) Subtask 535056-960-029-001 - Area 19, replace nut from LH side of outer wing centre spar Work Zones and Access Panels Zone Access/Work location 540 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA30 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 1 NUT References Drawing R51415001 Replace 1 nut as described in Repair Instruction (RI) R51415001. NOTE: The work to perform in this area can need access to inner tanks and should be accomplished during 8C check. (a) Remove : 1 Nut ASNA2531-4 Discard (b) Install : 1 Nut ASNA2531-4

(8) Subtask 535056-960-030-001 - Area 20, replace nuts from LH and RH fixed inner shroud boxes Work Zones and Access Panels Zone Access/Work location 570 670 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 117 5

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# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA31 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 16 NUT Replace 16 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 8 nuts on LH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4 (b) Replace 8 nuts on RH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4

(9) Subtask 535056-960-031-002 - Area 21, replace nuts at FR38 and FR54 circumferential junctions Work Zones and Access Panels Zone Access/Work location 100 Work location Frame 38 Frame 54 200 Work location Frame 38 Frame 54 Manpower Resources Manhours 3.00 Minimum number of person 2 Subtask elapsed time 2.00 Skills AIRFRAME Material necessary to do the job Component COMPA33 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 31 NUT

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 118 5

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# @A340-500/600
SERVICE BULLETIN

References Drawing R51415001 Replace 31 nuts as described in Repair Instruction (RI) R51415001. (a) Remove : 31 Nut ASNA2531-4 Discard (b) Install : 31 Nut ASNA2531-4

(10) Subtask 535056-960-032-001 - Area concession 1 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME Material necessary to do the job Component COMPA40 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 1 NUT References Drawing R51415001 Replace 1 nut as described in Repair Instruction (RI) R51415001. (a) Remove : 1 Nut ASNA2531-4 Discard (b) Install : 1 Nut ASNA2531-4

(11) Subtask 535056-960-033-003 - Area concession 2 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 119 5

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

# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA41 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 6 NUT References Drawing R51415001 Replace 6 nuts as described in Repair Instruction (RI) R51415001. (a) Remove : 6 Nut ASNA2531-4 Discard (b) Install : 6 Nut ASNA2531-4 **CONF 003 (1) Subtask 535056-832-001-002 - Inspection / Repair Work Zones and Access Panels Zone Access/Work location 100 200 570 670 Manpower Resources Manhours 2.00 Minimum number of person 2 Subtask elapsed time 1.00 Skills AIRFRAME References Drawing R51415000 Fig. A-FBCAA Flow Chart Sheet 01 (a) Perform a visual inspection of the nuts looking for cracked or missing nuts as described inFig. A-FBCAA: 1 In case of missing nut, contact Airbus before next flight for additional instructions.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 120 5

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# @A340-500/600
SERVICE BULLETIN

2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on area 20. - For the inspection areas, refer to Repair Instruction (RI) R51415000. - For the inspection report, refer to Appendix 01 Inspection Report. . 3 If no findings, replace the nut before next flight. (b) Replacement principle of the nut : 1 Remove half of the required nuts equally spread.
a Remove the nut using an ALLEN key to maintain the fastener. 2 Install new nuts.
a Install the nut using an ALLEN key to maintain the fastener. 3 Perform the replacement of the half remaining nuts. NOTE: If the fastener rotates, refer to Repair Instruction (RI) R51415000. (2) Subtask 535056-960-030-001 - Area 20, replace nuts from LH and RH fixed inner shroud boxes Work Zones and Access Panels Zone Access/Work location 570 670 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills AIRFRAME Material necessary to do the job Component COMPA31 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 16 NUT Replace 16 nuts as described in Repair Instruction (RI) R51415000.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 121 5

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

# @A340-500/600
SERVICE BULLETIN
(a) Replace 8 nuts on LH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4 (b) Replace 8 nuts on RH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4 **CONF 004 (1) Subtask 535056-832-001-004 - Inspection / Repair Work Zones and Access Panels Zone Access/Work location 100 200 570 670 Manpower Resources Manhours 4.00 Minimum number of person 4 Subtask elapsed time 1.00 Skills AIRFRAME References Drawing R51415000 R51415001 Fig. A-FBCAA Flow Chart Sheet 01 (a) Perform a visual inspection of the nuts looking for cracked or missing nuts as described inFig. A-FBCAA: 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 18, 20, 21 and
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 122 5

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# @A340-500/600
SERVICE BULLETIN

area concession 1. - For the inspection areas, refer to Repair Instruction (RI) R51415000 and Repair Instruction (RI) R51415001. - For the inspection report, refer to Appendix 01 Inspection Report. . 3 If no findings, replace the nut before next flight. (b) Replacement principle of the nut : 1 Remove half of the required nuts equally spread.
a Remove the nut using an ALLEN key to maintain the fastener. 2 Install new nuts.
a Install the nut using an ALLEN key to maintain the fastener. 3 Perform the replacement of the half remaining nuts. NOTE: If the fastener rotates, refer to Repair Instruction (RI) R51415000 and Repair Instruction (RI) R51415001. (2) Subtask 535056-960-028-001 - Area 18, replace nuts from rear section FR54 stringer 54 LH sideWork Zones and Access Panels Zone Access/Work location 260 Work location Frame 54 Stringer 54 Manpower Resources Manhours 4.00 Minimum number of person 2 Subtask elapsed time 2.00 Skills AIRFRAME Material necessary to do the job Component COMPA28 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 33 NUT Replace 33 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 33 Nut ASNA2531-4 Discard

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 123 5

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# @A340-500/600
SERVICE BULLETIN
(b) Install : 33 Nut ASNA2531-4

(3) Subtask 535056-960-030-001 - Area 20, replace nuts from LH and RH fixed inner shroud boxes Work Zones and Access Panels Zone Access/Work location 570 670 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills AIRFRAME Material necessary to do the job Component COMPA31 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 16 NUT Replace 16 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 8 nuts on LH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4 (b) Replace 8 nuts on RH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 124 5

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

# @A340-500/600
SERVICE BULLETIN
(4) Subtask 535056-960-031-003 - Area 21, replace nuts at FR38 and FR54 circumferential junctions Work Zones and Access Panels Zone Access/Work location 100 Work location Frame 38 Frame 54 200 Work location Frame 38 Frame 54 Manpower Resources Manhours 3.75 Minimum number of person 2 Subtask elapsed time 2.00 Skills AIRFRAME Material necessary to do the job Component COMPA34 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 37 NUT References Drawing R51415001 Replace 37 nuts as described in Repair Instruction (RI) R51415001. (a) Remove : 37 Nut ASNA2531-4 Discard (b) Install : 37 Nut ASNA2531-4

(5) Subtask 535056-960-032-002 - Area concession 1 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA40 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 2 NUT
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 125 5

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

# @A340-500/600
SERVICE BULLETIN

References Drawing R51415001 Replace 2 nuts as described in Repair Instruction (RI) R51415001. (a) Remove : 2 Nut ASNA2531-4 Discard (b) Install : 2 Nut ASNA2531-4 **CONF 005 (1) Subtask 535056-832-001-005 - Inspection / Repair Work Zones and Access Panels Zone Access/Work location 100 200 570 670 Manpower Resources Manhours 4.00 Minimum number of person 4 Subtask elapsed time 1.00 Skills AIRFRAME References Drawing R51415000 R51415001 Fig. A-FBCAA Flow Chart Sheet 01 (a) Perform a visual inspection of the nuts looking for cracked or missing nuts as described inFig. A-FBCAA: 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 1b, 14, 18, 20, 21 and area concession 1. - For the inspection areas, refer to Repair Instruction (RI) R51415000 and Repair Instruction (RI) R51415001. - For the inspection report, refer to Appendix 01 Inspection
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 126 5

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# @A340-500/600
SERVICE BULLETIN
Report. . 3 If no findings, replace the nut before next flight. (b) Replacement principle of the nut : 1 Remove half of the required nuts equally spread.
a Remove the nut using an ALLEN key to maintain the fastener. 2 Install new nuts.
a Install the nut using an ALLEN key to maintain the fastener. 3 Perform the replacement of the half remaining nuts. NOTE: If the fastener rotates, refer to Repair Instruction (RI) R51415000 and Repair Instruction (RI) R51415001. (2) Subtask 535056-960-001-001 - Area 1a, replace the nuts in FWD RH hard points Work Zones and Access Panels Zone Access/Work location 120 Access Door 821, Door 132AZ Work location from Frame 16 to Frame 17 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 2 NUT References Drawing R51415000 Replace 2 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 2 Nut ASNA2531-4 Discard (b) Install : 2 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 127 5

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

# @A340-500/600
SERVICE BULLETIN
(3) Subtask 535056-960-003-001 - Area 1b, replace nuts of 800VU RH support Work Zones and Access Panels Zone Access/Work location 120 Access Door 821, Door 132AZ Work location from Frame 19 to Frame 20 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA03 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 4 NUT References Drawing R51415000 Replace 4 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 4 Nut ASNA2531-4 Discard (b) Install : 4 Nut ASNA2531-4

(4) Subtask 535056-960-028-002 - Area 18, replace nuts from rear section FR54 stringer 54 LH sideWork Zones and Access Panels Zone Access/Work location 260 Work location Frame 54 Stringer 54 Manpower Resources Manhours 2.50 Minimum number of person 2 Subtask elapsed time 1.50 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 128 5

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

# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA29 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 22 NUT Replace 22 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 22 Nut ASNA2531-4 Discard (b) Install : 22 Nut ASNA2531-4

(5) Subtask 535056-960-030-001 - Area 20, replace nuts from LH and RH fixed inner shroud boxes Work Zones and Access Panels Zone Access/Work location 570 670 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills AIRFRAME Material necessary to do the job Component COMPA31 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 16 NUT Replace 16 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 8 nuts on LH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 129 5

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# @A340-500/600
SERVICE BULLETIN
(b) Replace 8 nuts on RH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4

(6) Subtask 535056-960-031-004 - Area 21, replace nuts at FR38 and FR54 circumferential junctions Work Zones and Access Panels Zone Access/Work location 100 Work location Frame 38 Frame 54 200 Work location Frame 38 Frame 54 Manpower Resources Manhours 7.25 Minimum number of person 2 Subtask elapsed time 5.00 Skills AIRFRAME Material necessary to do the job Component COMPA35 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 72 NUT References Drawing R51415001 Replace 72 nuts as described in Repair Instruction (RI) R51415001. (a) Remove : 72 Nut ASNA2531-4 Discard (b) Install : 72 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 130 5

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

# @A340-500/600
SERVICE BULLETIN
(7) Subtask 535056-960-032-003 - Area concession 1 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA40 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 4 NUT References Drawing R51415001 Replace 4 nuts as described in Repair Instruction (RI) R51415001. (a) Remove : 4 Nut ASNA2531-4 Discard (b) Install : 4 Nut ASNA2531-4 **CONF 006 (1) Subtask 535056-832-001-006 - Inspection / Repair Work Zones and Access Panels Zone Access/Work location 100 200 570 670 Manpower Resources Manhours 4.00 Minimum number of person 4 Subtask elapsed time 1.00 Skills AIRFRAME References Drawing R51415000 R51415001 Fig. A-FBCAA Flow Chart Sheet 01

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 131 5

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

# @A340-500/600
SERVICE BULLETIN
(a) Perform a visual inspection of the nuts looking for cracked or missing nuts as described inFig. A-FBCAA: 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 1b, 18, 19, 20, 21 and area concession 1. - For the inspection areas, refer to Repair Instruction (RI) R51415000 and Repair Instruction (RI) R51415001. - For the inspection report, refer to Appendix 01 Inspection Report. . 3 If no findings, replace the nut before next flight. (b) Replacement principle of the nut : 1 Remove half of the required nuts equally spread.
a Remove the nut using an ALLEN key to maintain the fastener. 2 Install new nuts.
a Install the nut using an ALLEN key to maintain the fastener. 3 Perform the replacement of the half remaining nuts. NOTE: If the fastener rotates, refer to Repair Instruction (RI) R51415000 and Repair Instruction (RI) R51415001. (2) Subtask 535056-960-001-001 - Area 1a, replace the nuts in FWD RH hard points Work Zones and Access Panels Zone Access/Work location 120 Access Door 821, Door 132AZ Work location from Frame 16 to Frame 17 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 132 5

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

# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 2 NUT References Drawing R51415000 Replace 2 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 2 Nut ASNA2531-4 Discard (b) Install : 2 Nut ASNA2531-4

(3) Subtask 535056-960-003-001 - Area 1b, replace nuts of 800VU RH support Work Zones and Access Panels Zone Access/Work location 120 Access Door 821, Door 132AZ Work location from Frame 19 to Frame 20 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA03 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 4 NUT References Drawing R51415000 Replace 4 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 4 Nut ASNA2531-4 Discard

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 133 5

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# @A340-500/600
SERVICE BULLETIN
(b) Install : 4 Nut ASNA2531-4

(4) Subtask 535056-960-028-002 - Area 18, replace nuts from rear section FR54 stringer 54 LH sideWork Zones and Access Panels Zone Access/Work location 260 Work location Frame 54 Stringer 54 Manpower Resources Manhours 2.50 Minimum number of person 2 Subtask elapsed time 1.50 Skills AIRFRAME Material necessary to do the job Component COMPA29 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 22 NUT Replace 22 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 22 Nut ASNA2531-4 Discard (b) Install : 22 Nut ASNA2531-4

(5) Subtask 535056-960-029-001 - Area 19, replace nut from LH side of outer wing centre spar Work Zones and Access Panels Zone Access/Work location 540 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 134 5

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

# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA30 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 1 NUT References Drawing R51415001 Replace 1 nut as described in Repair Instruction (RI) R51415001. NOTE: The work to perform in this area can need access to inner tanks and should be accomplished during 8C check. (a) Remove : 1 Nut ASNA2531-4 Discard (b) Install : 1 Nut ASNA2531-4

(6) Subtask 535056-960-030-001 - Area 20, replace nuts from LH and RH fixed inner shroud boxes Work Zones and Access Panels Zone Access/Work location 570 670 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills AIRFRAME Material necessary to do the job Component COMPA31 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 16 NUT Replace 16 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 8 nuts on LH side. 1 Remove : 8 Nut ASNA2531-4 Discard
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 135 5

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# @A340-500/600
SERVICE BULLETIN

2 Install : 8 Nut ASNA2531-4 (b) Replace 8 nuts on RH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4

(7) Subtask 535056-960-031-005 - Area 21, replace nuts at FR38 and FR54 circumferential junctions Work Zones and Access Panels Zone Access/Work location 100 Work location Frame 38 Frame 54 200 Work location Frame 38 Frame 54 Manpower Resources Manhours 8.50 Minimum number of person 2 Subtask elapsed time 5.00 Skills AIRFRAME Material necessary to do the job Component COMPA36 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 84 NUT References Drawing R51415001 Replace 84 nuts as described in Repair Instruction (RI) R51415001. (a) Remove : 84 Nut ASNA2531-4 Discard (b) Install : 84 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 136 5

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

# @A340-500/600
SERVICE BULLETIN
(8) Subtask 535056-960-032-004 - Area concession 1 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA40 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 7 NUT References Drawing R51415001 Replace 7 nuts as described in Repair Instruction (RI) R51415001. (a) Remove : 7 Nut ASNA2531-4 Discard (b) Install : 7 Nut ASNA2531-4 **CONF 007 (1) Subtask 535056-832-001-007 - Inspection / Repair Work Zones and Access Panels Zone Access/Work location 100 200 570 670 Manpower Resources Manhours 4.00 Minimum number of person 4 Subtask elapsed time 1.00 Skills AIRFRAME References Drawing R51415000 R51415001 Fig. A-FBCAA Flow Chart Sheet 01

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 137 5

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# @A340-500/600
SERVICE BULLETIN
(a) Perform a visual inspection of the nuts looking for cracked or missing nuts as described inFig. A-FBCAA: 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 1b, 2a, 2b, 2c, 2d, 2e, 2f, 3, 4a, 4b, 4c, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 20, 21 and areas concessions 1 thru 6. - For the inspection areas, refer to Repair Instruction (RI) R51415000 and Repair Instruction (RI) R51415001. - For the inspection report, refer to Appendix 01 Inspection Report. . 3 If no findings, replace the nut before next flight. (b) Replacement principle of the nut : 1 Remove half of the required nuts equally spread.
a Remove the nut using an ALLEN key to maintain the fastener. 2 Install new nuts.
a Install the nut using an ALLEN key to maintain the fastener. 3 Perform the replacement of the half remaining nuts. NOTE: If the fastener rotates, refer to Repair Instruction (RI) R51415000 and Repair Instruction (RI) R51415001. (2) Subtask 535056-960-001-001 - Area 1a, replace the nuts in FWD RH hard points Work Zones and Access Panels Zone Access/Work location 120 Access Door 821, Door 132AZ Work location from Frame 16 to Frame 17 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 138 5

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# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 2 NUT References Drawing R51415000 Replace 2 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 2 Nut ASNA2531-4 Discard (b) Install : 2 Nut ASNA2531-4

(3) Subtask 535056-960-003-001 - Area 1b, replace nuts of 800VU RH support Work Zones and Access Panels Zone Access/Work location 120 Access Door 821, Door 132AZ Work location from Frame 19 to Frame 20 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA03 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 4 NUT References Drawing R51415000 Replace 4 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 4 Nut ASNA2531-4 Discard

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 139 5

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# @A340-500/600
SERVICE BULLETIN
(b) Install : 4 Nut ASNA2531-4

(4) Subtask 535056-960-004-001 - Area 2a, replace nuts of LH and RH keel lower angle fittings Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 40 Manpower Resources Manhours 5.25 Minimum number of person 2 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Component COMPA04 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 62 NUT References Drawing R51415000 Replace 62 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 31 nuts on LH side. 1 Remove : 31 Nut ASNA2531-4 Discard 2 Install : 31 Nut ASNA2531-4 (b) Replace 31 nuts on RH side. 1 Remove : 31 Nut ASNA2531-4 Discard 2 Install : 31 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 140 5

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

# @A340-500/600
SERVICE BULLETIN
(5) Subtask 535056-960-006-001 - Area 2b, replace nuts of LH and RH lower fuselage to FR40 attachments Work Zones and Access Panels Zone Access/Work location 140 Work location Frame 40 from Stringer 30 to Stringer 54 Manpower Resources Manhours 22.50 Minimum number of person 2 Subtask elapsed time 12.00 Skills NON SPECIFIC Material necessary to do the job Component COMPA05 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 269 NUT References Drawing R51415000 Replace 269 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 269 Nut ASNA2531-4 Discard (b) Install : 269 Nut ASNA2531-4

(6) Subtask 535056-960-007-001 - Area 2c, replace nuts of fuselage to LH and RH inner keel beam attachments Work Zones and Access Panels Zone Access/Work location 100 Work location from Frame 39 to Frame 40 Manpower Resources Manhours 9.50 Minimum number of person 2 Subtask elapsed time 5.00 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 141 5

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

# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA06 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 112 NUT References Drawing R51415000 Replace 112 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 56 nuts on LH side. 1 Remove : 56 Nut ASNA2531-4 Discard 2 Install : 56 Nut ASNA2531-4 (b) Replace 56 nuts on RH side. 1 Remove : 56 Nut ASNA2531-4 Discard 2 Install : 56 Nut ASNA2531-4

(7) Subtask 535056-960-008-001 - Area 2d, replace nuts of fuselage to LH and RH outer keel beam attachments Work Zones and Access Panels Zone Access/Work location 100 Work location from Frame 39 to Frame 40 Manpower Resources Manhours 9.00 Minimum number of person 2 Subtask elapsed time 5.00 Skills AIRFRAME Material necessary to do the job Component COMPA07 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 106 NUT

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 142 5

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# @A340-500/600
SERVICE BULLETIN

References Drawing R51415000 Replace 106 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 53 nuts on LH side. 1 Remove : 53 Nut ASNA2531-4 Discard 2 Install : 53 Nut ASNA2531-4 (b) Replace 53 nuts on RH side. 1 Remove : 53 Nut ASNA2531-4 Discard 2 Install : 53 Nut ASNA2531-4

(8) Subtask 535056-960-009-001 - Area 2e, replace nuts below LH and RH lower panels of FR40-1 to section 21 attachments Work Zones and Access Panels Zone Access/Work location 140 Work location Frame 40-1 Manpower Resources Manhours 6.00 Minimum number of person 2 Subtask elapsed time 4.00 Skills AIRFRAME Material necessary to do the job Component COMPA08 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 70 NUT References Drawing R51415000 Replace 70 nuts as described in Repair Instruction (RI) R51415000.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 143 5

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

# @A340-500/600
SERVICE BULLETIN
(a) Replace 35 nuts on LH side. 1 Remove : 35 Nut ASNA2531-4 Discard 2 Install : 35 Nut ASNA2531-4 (b) Replace 35 nuts on RH side. 1 Remove : 35 Nut ASNA2531-4 Discard 2 Install : 35 Nut ASNA2531-4

(9) Subtask 535056-960-010-001 - Area 2f, replace nuts from inboard of LH and RH center wing rear spars Work Zones and Access Panels Zone Access/Work location 140 Work location Frame 40 Rib 1 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Component COMPA09 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 10 NUT References Drawing R51415000 Replace 10 nuts as described in Repair Instruction (RI) R51415000. NOTE: The work to perform in this area can need access to center tank and should be accomplished during 8C check.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 144 5

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

# @A340-500/600
SERVICE BULLETIN
(a) Replace 5 nuts on LH side. 1 Remove : 5 Nut ASNA2531-4 Discard 2 Install : 5 Nut ASNA2531-4 (b) Replace 5 nuts on RH side. 1 Remove : 5 Nut ASNA2531-4 Discard 2 Install : 5 Nut ASNA2531-4

(10) Subtask 535056-960-011-001 - Area 3, replace nuts from LH and RH zones of belly fairing structure Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills AIRFRAME Material necessary to do the job Component COMPA10 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 16 NUT Replace 16 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 8 nuts on LH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 145 5

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# @A340-500/600
SERVICE BULLETIN
(b) Replace 8 nuts on RH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4

(11) Subtask 535056-960-012-001 - Area 4a, replace nuts of LH and RH canted lateral panel attachments Work Zones and Access Panels Zone Access/Work location 140 Work location from Frame 47 to Frame 48 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA11 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 6 NUT Replace 6 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 3 nuts on LH side. 1 Remove : 3 Nut ASNA2531-4 Discard 2 Install : 3 Nut ASNA2531-4 (b) Replace 3 nuts on RH side. 1 Remove : 3 Nut ASNA2531-4 Discard 2 Install : 3 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 146 5

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

# @A340-500/600
SERVICE BULLETIN
(12) Subtask 535056-960-013-001 - Area 4b, replace nuts of LH and RH FWD canted beams Work Zones and Access Panels Zone Access/Work location 140 Work location from Frame 48 to Frame 50 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Component COMPA12 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 12 NUT Replace 12 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 6 nuts on LH side. 1 Remove : 6 Nut ASNA2531-4 Discard 2 Install : 6 Nut ASNA2531-4 (b) Replace 6 nuts on RH side. 1 Remove : 6 Nut ASNA2531-4 Discard 2 Install : 6 Nut ASNA2531-4

(13) Subtask 535056-960-014-001 - Area 4c, replace nuts of LH and RH aft canted beams Work Zones and Access Panels Zone Access/Work location 140 Work location Frame 53-2

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 147 5

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# @A340-500/600
SERVICE BULLETIN
Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA13 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 2 NUT Replace 2 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 1 nut on LH side. 1 Remove : 1 Nut ASNA2531-4 Discard 2 Install : 1 Nut ASNA2531-4 (b) Replace 1 nut on RH side. 1 Remove : 1 Nut ASNA2531-4 Discard 2 Install : 1 Nut ASNA2531-4

(14) Subtask 535056-960-015-001 - Area 5, replace nuts of LH and RH fuselage to outer keel beam attachments Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53-2 to Frame 53-7 Manpower Resources Manhours 1.75 Minimum number of person 2 Subtask elapsed time 1.00 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 148 5

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

# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA14 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 20 NUT Replace 20 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 10 nuts on LH side. 1 Remove : 10 Nut ASNA2531-4 Discard 2 Install : 10 Nut ASNA2531-4 (b) Replace 10 nuts on RH side. 1 Remove : 10 Nut ASNA2531-4 Discard 2 Install : 10 Nut ASNA2531-4

(15) Subtask 535056-960-016-001 - Area 6, replace nuts of LH and RH FWD inner keel beams Work Zones and Access Panels Zone Access/Work location 150 Work location Frame 53-7 Manpower Resources Manhours 1.75 Minimum number of person 2 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Component COMPA15 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 20 NUT Replace 20 nuts as described in Repair Instruction (RI) R51415000.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 149 5

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

# @A340-500/600
SERVICE BULLETIN
(a) Replace 10 nuts on LH side. 1 Remove : 10 Nut ASNA2531-4 Discard 2 Install : 10 Nut ASNA2531-4 (b) Replace 10 nuts on RH side. 1 Remove : 10 Nut ASNA2531-4 Discard 2 Install : 10 Nut ASNA2531-4

(16) Subtask 535056-960-017-001 - Area 7, replace nuts of LH keel beam attachment tees Work Zones and Access Panels Zone Access/Work location 140 Work location from Frame 40-3 to Frame 47 Manpower Resources Manhours 12.00 Minimum number of person 2 Subtask elapsed time 8.00 Skills AIRFRAME Material necessary to do the job Component COMPA16 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 72 NUT Replace 72 nuts as described in Repair Instruction (RI) R51415000. NOTE: The work to perform in this area can need access to center tank and should be accomplished during 8C check. (a) Remove : 72 Nut ASNA2531-4 Discard (b) Install : 72 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 150 5

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# @A340-500/600
SERVICE BULLETIN
(17) Subtask 535056-960-018-001 - Area 8, replace nuts from RH keel beam attachment tees Work Zones and Access Panels Zone Access/Work location 140 Work location from Frame 40-3 to Frame 47 Manpower Resources Manhours 12.00 Minimum number of person 2 Subtask elapsed time 8.00 Skills AIRFRAME Material necessary to do the job Component COMPA17 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 72 NUT Replace 72 nuts as described in Repair Instruction (RI) R51415000. NOTE: The work to perform in this area can need access to center tank and should be accomplished during 8C check. (a) Remove : 72 Nut ASNA2531-4 Discard (b) Install : 72 Nut ASNA2531-4

(18) Subtask 535056-960-019-001 - Area 9, replace nuts from RH side of floor structure Work Zones and Access Panels Zone Access/Work location 250 Work location Frame 47 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 151 5

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# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA18 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 6 NUT Replace 6 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 6 Nut ASNA2531-4 Discard (b) Install : 6 Nut ASNA2531-4

(19) Subtask 535056-960-020-001 - Area 10, replace nuts from LH and RH sides of longitudinal joint Work Zones and Access Panels Zone Access/Work location 130 Work location Frame 39 from Stringer 28 to Stringer 29 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills AIRFRAME Material necessary to do the job Component COMPA19 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 10 NUT Replace 10 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 5 nuts on LH side. 1 Remove : 5 Nut ASNA2531-4 Discard 2 Install : 5 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 152 5

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# @A340-500/600
SERVICE BULLETIN
(b) Replace 5 nuts on RH side. 1 Remove : 5 Nut ASNA2531-4 Discard 2 Install : 5 Nut ASNA2531-4

(20) Subtask 535056-960-021-001 - Area 11, replace nuts of LH and RH cleat attachments Work Zones and Access Panels Zone Access/Work location 250 Work location Frame 47 Stringer 23 Manpower Resources Manhours 2.00 Minimum number of person 2 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Component COMPA20 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 16 NUT Replace 16 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 8 nuts on LH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4 (b) Replace 8 nuts on RH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 153 5

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# @A340-500/600
SERVICE BULLETIN
(21) Subtask 535056-960-022-001 - Area 12, replace nuts from FWD LH side of canted beam attachment Work Zones and Access Panels Zone Access/Work location 150 Work location Frame 53-2 Manpower Resources Manhours 9.00 Minimum number of person 2 Subtask elapsed time 5.00 Skills AIRFRAME Material necessary to do the job Component COMPA21 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 87 NUT References Fig. A-FBAAA Canted beam attachment FWD of FR53-2 LH, Removal of the Pipes Support for Access Sheet 01 Sheet 02

Replace 87 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 87 Nut ASNA2531-4 Discard (b) Install : 87 Nut ASNA2531-4 NOTE: 3 nuts have been removed during preparation procedure to unscrew the pipes support. Do not install these 3 nuts before installation of the concerned pipes support (Refer to paragraph (c) of SUBTASK 535056-942-001 007 Close-up and Fig. A-FBAAA). (22) Subtask 535056-960-023-001 - Area 13, replace nuts from FWD RH side of canted beam attachment Work Zones and Access Panels Zone Access/Work location 150 Work location Frame 53-2

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 154 5

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# @A340-500/600
SERVICE BULLETIN
Manpower Resources Manhours 8.50 Minimum number of person 2 Subtask elapsed time 5.00 Skills AIRFRAME Material necessary to do the job Component COMPA22 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 77 NUT References Fig. A-FBBAA Canted beam attachment FWD of FR53-2 RH, Removal of the Pipes Support for Access Sheet 01 Sheet 02

Replace 83 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 77 Nut ASNA2531-4 Discard (b) Install : 77 Nut ASNA2531-4 NOTE: 6 nuts have been removed during preparation procedure to unscrew the pipes support. Do not install these 6 nuts before installation of the concerned pipes support (Refer to paragraph (d) of SUBTASK 535056-942-001 007 Close-up and Fig. A-FBBAA). (23) Subtask 535056-960-024-002 - Area 14, replace nuts from LH and RH dado panel support struts Work Zones and Access Panels Zone Access/Work location 250 Work location from Frame 40-1 to Frame 43 from Stringer 25 to Stringer 27 Manpower Resources Manhours 3.00 Minimum number of person 2 Subtask elapsed time 1.50 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 155 5

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

# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA24 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 32 NUT Replace 32 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 16 nuts on LH side. 1 Remove : 16 Nut ASNA2531-4 Discard 2 Install : 16 Nut ASNA2531-4 (b) Replace 16 nuts on RH side. 1 Remove : 16 Nut ASNA2531-4 Discard 2 Install : 16 Nut ASNA2531-4

(24) Subtask 535056-960-025-001 - Area 15, replace nuts from LH and RH sides of FR53-6 splicing Work Zones and Access Panels Zone Access/Work location 260 Work location Frame 53-6 from Stringer 27 to Stringer 28 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Component COMPA25 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 6 NUT Replace 6 nuts as described in Repair Instruction (RI) R51415000.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 156 5

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

# @A340-500/600
SERVICE BULLETIN
(a) Replace 3 nuts on LH side. 1 Remove : 3 Nut ASNA2531-4 Discard 2 Install : 3 Nut ASNA2531-4 (b) Replace 3 nuts on RH side. 1 Remove : 3 Nut ASNA2531-4 Discard 2 Install : 3 Nut ASNA2531-4

(25) Subtask 535056-960-026-001 - Area 16, replace nuts from LH and RH seat track splicings Work Zones and Access Panels Zone Access/Work location 250 Work location from Frame 53-1 to Frame 53-2 Manpower Resources Manhours 5.00 Minimum number of person 2 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Component COMPA26 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 44 NUT Replace 44 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 20 nuts on LH side. 1 Remove : 20 Nut ASNA2531-4 Discard 2 Install : 20 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 157 5

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

# @A340-500/600
SERVICE BULLETIN
(b) Replace 20 nuts on RH side. 1 Remove : 20 Nut ASNA2531-4 Discard 2 Install : 20 Nut ASNA2531-4 (c) Replace 4 nuts at Y0. 1 Remove : 4 Nut ASNA2531-4 Discard 2 Install : 4 Nut ASNA2531-4

(26) Subtask 535056-960-027-001 - Area 17, replace nuts from LH and RH seat track splicings Work Zones and Access Panels Zone Access/Work location 260 Work location Frame 53-7 Manpower Resources Manhours 5.00 Minimum number of person 2 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Component COMPA27 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 44 NUT Replace 44 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 20 nuts on LH side. 1 Remove : 20 Nut ASNA2531-4 Discard 2 Install : 20 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 158 5

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

# @A340-500/600
SERVICE BULLETIN
(b) Replace 20 nuts on RH side. 1 Remove : 20 Nut ASNA2531-4 Discard 2 Install : 20 Nut ASNA2531-4 (c) Replace 4 nuts at Y0. 1 Remove : 4 Nut ASNA2531-4 Discard 2 Install : 4 Nut ASNA2531-4

(27) Subtask 535056-960-028-002 - Area 18, replace nuts from rear section FR54 stringer 54 LH sideWork Zones and Access Panels Zone Access/Work location 260 Work location Frame 54 Stringer 54 Manpower Resources Manhours 2.50 Minimum number of person 2 Subtask elapsed time 1.50 Skills AIRFRAME Material necessary to do the job Component COMPA29 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 22 NUT Replace 22 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 22 Nut ASNA2531-4 Discard (b) Install : 22 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 159 5

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

# @A340-500/600
SERVICE BULLETIN
(28) Subtask 535056-960-030-001 - Area 20, replace nuts from LH and RH fixed inner shroud boxes Work Zones and Access Panels Zone Access/Work location 570 670 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills AIRFRAME Material necessary to do the job Component COMPA31 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 16 NUT Replace 16 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 8 nuts on LH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4 (b) Replace 8 nuts on RH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4

(29) Subtask 535056-960-031-006 - Area 21, replace nuts at FR38 and FR54 circumferential junctions Work Zones and Access Panels Zone Access/Work location 100 Work location Frame 38 Frame 54 200 Work location Frame 38 Frame 54
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 160 5

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# @A340-500/600
SERVICE BULLETIN
Manpower Resources Manhours 10.00 Minimum number of person 4 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Component COMPA37 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 101 NUT References Drawing R51415001 Replace 101 nuts as described in Repair Instruction (RI) R51415001. (a) Remove : 101 Nut ASNA2531-4 Discard (b) Install : 101 Nut ASNA2531-4

(30) Subtask 535056-960-032-003 - Area concession 1 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA40 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 4 NUT References Drawing R51415001 Replace 4 nuts as described in Repair Instruction (RI) R51415001. (a) Remove : 4 Nut ASNA2531-4 Discard

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 161 5

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# @A340-500/600
SERVICE BULLETIN
(b) Install : 4 Nut ASNA2531-4

(31) Subtask 535056-960-033-001 - Area concession 2 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME Material necessary to do the job Component COMPA41 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 1 NUT References Drawing R51415001 Replace 1 nut as described in Repair Instruction (RI) R51415001. (a) Remove : 1 Nut ASNA2531-4 Discard (b) Install : 1 Nut ASNA2531-4

(32) Subtask 535056-960-034-001 - Area concession 3 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME Material necessary to do the job Component COMPA42 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 1 NUT References Drawing R51415001 Replace 1 nut as described in Repair Instruction (RI) R51415001. DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 162 5

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# @A340-500/600
SERVICE BULLETIN
(a) Remove : 1 Nut ASNA2531-4 Discard (b) Install : 1 Nut ASNA2531-4

(33) Subtask 535056-960-035-001 - Area concession 4 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME Material necessary to do the job Component COMPA43 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 1 NUT References Drawing R51415001 Replace 1 nut as described in Repair Instruction (RI) R51415001. (a) Remove : 1 Nut ASNA2531-4 Discard (b) Install : 1 Nut ASNA2531-4

(34) Subtask 535056-960-038-001 - Area concession 5 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME Material necessary to do the job Component COMPA44 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 1 NUT

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 163 5

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# @A340-500/600
SERVICE BULLETIN

References Drawing R51415001 Replace 1 nut as described in Repair Instruction (RI) R51415001. (a) Remove : 1 Nut ASNA2531-4 Discard (b) Install : 1 Nut ASNA2531-4

(35) Subtask 535056-960-036-002 - Area concession 6 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME Material necessary to do the job Component COMPA45 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 2 NUT References Drawing R51415001 Replace 2 nuts as described in Repair Instruction (RI) R51415001. (a) Remove : 2 Nut ASNA2531-4 Discard (b) Install : 2 Nut ASNA2531-4 **CONF 008 (1) Subtask 535056-832-001-008 - Inspection / Repair Work Zones and Access Panels Zone Access/Work location 100 200 570 670

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 164 5

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# @A340-500/600
SERVICE BULLETIN
Manpower Resources Manhours 4.00 Minimum number of person 4 Subtask elapsed time 1.00 Skills AIRFRAME References Drawing R51415000 R51415001 Fig. A-FBCAA Flow Chart Sheet 01 (a) Perform a visual inspection of the nuts looking for cracked or missing nuts as described inFig. A-FBCAA: 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 1b, 2a, 2b, 2c, 2d, 2e, 2f, 3, 4a, 4b, 4c, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 20, 21, 23 and areas concessions 1 thru 4. - For the inspection areas, refer to Repair Instruction (RI) R51415000 and Repair Instruction (RI) R51415001. - For the inspection report, refer to Appendix 01 Inspection Report. . 3 If no findings, replace the nut before next flight. (b) Replacement principle of the nut : 1 Remove half of the required nuts equally spread.
a Remove the nut using an ALLEN key to maintain the fastener. 2 Install new nuts.
a Install the nut using an ALLEN key to maintain the fastener. 3 Perform the replacement of the half remaining nuts. NOTE: If the fastener rotates, refer to Repair Instruction (RI) R51415000 and Repair Instruction (RI) R51415001.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 165 5

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# @A340-500/600
SERVICE BULLETIN
(2) Subtask 535056-960-001-001 - Area 1a, replace the nuts in FWD RH hard points Work Zones and Access Panels Zone Access/Work location 120 Access Door 821, Door 132AZ Work location from Frame 16 to Frame 17 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 2 NUT References Drawing R51415000 Replace 2 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 2 Nut ASNA2531-4 Discard (b) Install : 2 Nut ASNA2531-4

(3) Subtask 535056-960-003-001 - Area 1b, replace nuts of 800VU RH support Work Zones and Access Panels Zone Access/Work location 120 Access Door 821, Door 132AZ Work location from Frame 19 to Frame 20 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 166 5

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# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA03 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 4 NUT References Drawing R51415000 Replace 4 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 4 Nut ASNA2531-4 Discard (b) Install : 4 Nut ASNA2531-4

(4) Subtask 535056-960-004-001 - Area 2a, replace nuts of LH and RH keel lower angle fittings Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 40 Manpower Resources Manhours 5.25 Minimum number of person 2 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Component COMPA04 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 62 NUT References Drawing R51415000 Replace 62 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 31 nuts on LH side. 1 Remove : 31 Nut ASNA2531-4 Discard

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 167 5

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# @A340-500/600
SERVICE BULLETIN

2 Install : 31 Nut ASNA2531-4 (b) Replace 31 nuts on RH side. 1 Remove : 31 Nut ASNA2531-4 Discard 2 Install : 31 Nut ASNA2531-4

(5) Subtask 535056-960-006-001 - Area 2b, replace nuts of LH and RH lower fuselage to FR40 attachments Work Zones and Access Panels Zone Access/Work location 140 Work location Frame 40 from Stringer 30 to Stringer 54 Manpower Resources Manhours 22.50 Minimum number of person 2 Subtask elapsed time 12.00 Skills NON SPECIFIC Material necessary to do the job Component COMPA05 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 269 NUT References Drawing R51415000 Replace 269 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 269 Nut ASNA2531-4 Discard (b) Install : 269 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 168 5

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# @A340-500/600
SERVICE BULLETIN
(6) Subtask 535056-960-007-001 - Area 2c, replace nuts of fuselage to LH and RH inner keel beam attachments Work Zones and Access Panels Zone Access/Work location 100 Work location from Frame 39 to Frame 40 Manpower Resources Manhours 9.50 Minimum number of person 2 Subtask elapsed time 5.00 Skills AIRFRAME Material necessary to do the job Component COMPA06 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 112 NUT References Drawing R51415000 Replace 112 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 56 nuts on LH side. 1 Remove : 56 Nut ASNA2531-4 Discard 2 Install : 56 Nut ASNA2531-4 (b) Replace 56 nuts on RH side. 1 Remove : 56 Nut ASNA2531-4 Discard 2 Install : 56 Nut ASNA2531-4

(7) Subtask 535056-960-008-001 - Area 2d, replace nuts of fuselage to LH and RH outer keel beam attachments Work Zones and Access Panels Zone Access/Work location 100 Work location from Frame 39 to Frame 40

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 169 5

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# @A340-500/600
SERVICE BULLETIN
Manpower Resources Manhours 9.00 Minimum number of person 2 Subtask elapsed time 5.00 Skills AIRFRAME Material necessary to do the job Component COMPA07 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 106 NUT References Drawing R51415000 Replace 106 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 53 nuts on LH side. 1 Remove : 53 Nut ASNA2531-4 Discard 2 Install : 53 Nut ASNA2531-4 (b) Replace 53 nuts on RH side. 1 Remove : 53 Nut ASNA2531-4 Discard 2 Install : 53 Nut ASNA2531-4

(8) Subtask 535056-960-009-001 - Area 2e, replace nuts below LH and RH lower panels of FR40-1 to section 21 attachments Work Zones and Access Panels Zone Access/Work location 140 Work location Frame 40-1 Manpower Resources Manhours 6.00 Minimum number of person 2 Subtask elapsed time 4.00 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 170 5

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# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA08 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 70 NUT References Drawing R51415000 Replace 70 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 35 nuts on LH side. 1 Remove : 35 Nut ASNA2531-4 Discard 2 Install : 35 Nut ASNA2531-4 (b) Replace 35 nuts on RH side. 1 Remove : 35 Nut ASNA2531-4 Discard 2 Install : 35 Nut ASNA2531-4

(9) Subtask 535056-960-010-001 - Area 2f, replace nuts from inboard of LH and RH center wing rear spars Work Zones and Access Panels Zone Access/Work location 140 Work location Frame 40 Rib 1 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 171 5

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# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA09 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 10 NUT References Drawing R51415000 Replace 10 nuts as described in Repair Instruction (RI) R51415000. NOTE: The work to perform in this area can need access to center tank and should be accomplished during 8C check. (a) Replace 5 nuts on LH side. 1 Remove : 5 Nut ASNA2531-4 Discard 2 Install : 5 Nut ASNA2531-4 (b) Replace 5 nuts on RH side. 1 Remove : 5 Nut ASNA2531-4 Discard 2 Install : 5 Nut ASNA2531-4

(10) Subtask 535056-960-011-001 - Area 3, replace nuts from LH and RH zones of belly fairing structure Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 172 5

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

# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA10 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 16 NUT Replace 16 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 8 nuts on LH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4 (b) Replace 8 nuts on RH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4

(11) Subtask 535056-960-012-001 - Area 4a, replace nuts of LH and RH canted lateral panel attachments Work Zones and Access Panels Zone Access/Work location 140 Work location from Frame 47 to Frame 48 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA11 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 6 NUT Replace 6 nuts as described in Repair Instruction (RI) R51415000.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 173 5

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# @A340-500/600
SERVICE BULLETIN
(a) Replace 3 nuts on LH side. 1 Remove : 3 Nut ASNA2531-4 Discard 2 Install : 3 Nut ASNA2531-4 (b) Replace 3 nuts on RH side. 1 Remove : 3 Nut ASNA2531-4 Discard 2 Install : 3 Nut ASNA2531-4

(12) Subtask 535056-960-013-001 - Area 4b, replace nuts of LH and RH FWD canted beams Work Zones and Access Panels Zone Access/Work location 140 Work location from Frame 48 to Frame 50 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Component COMPA12 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 12 NUT Replace 12 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 6 nuts on LH side. 1 Remove : 6 Nut ASNA2531-4 Discard 2 Install : 6 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 174 5

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# @A340-500/600
SERVICE BULLETIN
(b) Replace 6 nuts on RH side. 1 Remove : 6 Nut ASNA2531-4 Discard 2 Install : 6 Nut ASNA2531-4

(13) Subtask 535056-960-014-001 - Area 4c, replace nuts of LH and RH aft canted beams Work Zones and Access Panels Zone Access/Work location 140 Work location Frame 53-2 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA13 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 2 NUT Replace 2 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 1 nut on LH side. 1 Remove : 1 Nut ASNA2531-4 Discard 2 Install : 1 Nut ASNA2531-4 (b) Replace 1 nut on RH side. 1 Remove : 1 Nut ASNA2531-4 Discard 2 Install : 1 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 175 5

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# @A340-500/600
SERVICE BULLETIN
(14) Subtask 535056-960-015-001 - Area 5, replace nuts of LH and RH fuselage to outer keel beam attachments Work Zones and Access Panels Zone Access/Work location 150 Work location from Frame 53-2 to Frame 53-7 Manpower Resources Manhours 1.75 Minimum number of person 2 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Component COMPA14 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 20 NUT Replace 20 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 10 nuts on LH side. 1 Remove : 10 Nut ASNA2531-4 Discard 2 Install : 10 Nut ASNA2531-4 (b) Replace 10 nuts on RH side. 1 Remove : 10 Nut ASNA2531-4 Discard 2 Install : 10 Nut ASNA2531-4

(15) Subtask 535056-960-016-001 - Area 6, replace nuts of LH and RH FWD inner keel beams Work Zones and Access Panels Zone Access/Work location 150 Work location Frame 53-7

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 176 5

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# @A340-500/600
SERVICE BULLETIN
Manpower Resources Manhours 1.75 Minimum number of person 2 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Component COMPA15 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 20 NUT Replace 20 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 10 nuts on LH side. 1 Remove : 10 Nut ASNA2531-4 Discard 2 Install : 10 Nut ASNA2531-4 (b) Replace 10 nuts on RH side. 1 Remove : 10 Nut ASNA2531-4 Discard 2 Install : 10 Nut ASNA2531-4

(16) Subtask 535056-960-017-001 - Area 7, replace nuts of LH keel beam attachment tees Work Zones and Access Panels Zone Access/Work location 140 Work location from Frame 40-3 to Frame 47 Manpower Resources Manhours 12.00 Minimum number of person 2 Subtask elapsed time 8.00 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 177 5

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# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA16 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 72 NUT Replace 72 nuts as described in Repair Instruction (RI) R51415000. NOTE: The work to perform in this area can need access to center tank and should be accomplished during 8C check. (a) Remove : 72 Nut ASNA2531-4 Discard (b) Install : 72 Nut ASNA2531-4

(17) Subtask 535056-960-018-001 - Area 8, replace nuts from RH keel beam attachment tees Work Zones and Access Panels Zone Access/Work location 140 Work location from Frame 40-3 to Frame 47 Manpower Resources Manhours 12.00 Minimum number of person 2 Subtask elapsed time 8.00 Skills AIRFRAME Material necessary to do the job Component COMPA17 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 72 NUT Replace 72 nuts as described in Repair Instruction (RI) R51415000. NOTE: The work to perform in this area can need access to center tank and should be accomplished during 8C check. (a) Remove : 72 Nut ASNA2531-4 Discard (b) Install : 72 Nut ASNA2531-4
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 178 5

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# @A340-500/600
SERVICE BULLETIN
(18) Subtask 535056-960-019-001 - Area 9, replace nuts from RH side of floor structure Work Zones and Access Panels Zone Access/Work location 250 Work location Frame 47 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Component COMPA18 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 6 NUT Replace 6 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 6 Nut ASNA2531-4 Discard (b) Install : 6 Nut ASNA2531-4

(19) Subtask 535056-960-020-001 - Area 10, replace nuts from LH and RH sides of longitudinal joint Work Zones and Access Panels Zone Access/Work location 130 Work location Frame 39 from Stringer 28 to Stringer 29 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills AIRFRAME Material necessary to do the job Component COMPA19 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 10 NUT

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 179 5

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# @A340-500/600
SERVICE BULLETIN
Replace 10 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 5 nuts on LH side. 1 Remove : 5 Nut ASNA2531-4 Discard 2 Install : 5 Nut ASNA2531-4 (b) Replace 5 nuts on RH side. 1 Remove : 5 Nut ASNA2531-4 Discard 2 Install : 5 Nut ASNA2531-4

(20) Subtask 535056-960-021-001 - Area 11, replace nuts of LH and RH cleat attachments Work Zones and Access Panels Zone Access/Work location 250 Work location Frame 47 Stringer 23 Manpower Resources Manhours 2.00 Minimum number of person 2 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Component COMPA20 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 16 NUT Replace 16 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 8 nuts on LH side. 1 Remove : 8 Nut ASNA2531-4 Discard

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 180 5

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# @A340-500/600
SERVICE BULLETIN

2 Install : 8 Nut ASNA2531-4 (b) Replace 8 nuts on RH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4

(21) Subtask 535056-960-022-001 - Area 12, replace nuts from FWD LH side of canted beam attachment Work Zones and Access Panels Zone Access/Work location 150 Work location Frame 53-2 Manpower Resources Manhours 9.00 Minimum number of person 2 Subtask elapsed time 5.00 Skills AIRFRAME Material necessary to do the job Component COMPA21 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 87 NUT References Fig. A-FBAAA Canted beam attachment FWD of FR53-2 LH, Removal of the Pipes Support for Access Sheet 01 Sheet 02

Replace 87 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 87 Nut ASNA2531-4 Discard (b) Install : 87 Nut ASNA2531-4 NOTE: 3 nuts have been removed during preparation procedure to unscrew the pipes support. Do not install these 3 nuts before installation of the concerned pipes support (Refer to paragraph (c) of SUBTASK DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 181 5

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# @A340-500/600
SERVICE BULLETIN
535056-942-001 007 Close-up and Fig. A-FBAAA). (22) Subtask 535056-960-023-001 - Area 13, replace nuts from FWD RH side of canted beam attachment Work Zones and Access Panels Zone Access/Work location 150 Work location Frame 53-2 Manpower Resources Manhours 8.50 Minimum number of person 2 Subtask elapsed time 5.00 Skills AIRFRAME Material necessary to do the job Component COMPA22 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 77 NUT References Fig. A-FBBAA Canted beam attachment FWD of FR53-2 RH, Removal of the Pipes Support for Access Sheet 01 Sheet 02

Replace 83 nuts as described in Repair Instruction (RI) R51415000. (a) Remove : 77 Nut ASNA2531-4 Discard (b) Install : 77 Nut ASNA2531-4 NOTE: 6 nuts have been removed during preparation procedure to unscrew the pipes support. Do not install these 6 nuts before installation of the concerned pipes support (Refer to paragraph (d) of SUBTASK 535056-942-001 007 Close-up and Fig. A-FBBAA). (23) Subtask 535056-960-024-002 - Area 14, replace nuts from LH and RH dado panel support struts Work Zones and Access Panels Zone Access/Work location 250 Work location from Frame 40-1 to Frame 43 from Stringer 25 to Stringer 27

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 182 5

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# @A340-500/600
SERVICE BULLETIN
Manpower Resources Manhours 3.00 Minimum number of person 2 Subtask elapsed time 1.50 Skills AIRFRAME Material necessary to do the job Component COMPA24 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 32 NUT Replace 32 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 16 nuts on LH side. 1 Remove : 16 Nut ASNA2531-4 Discard 2 Install : 16 Nut ASNA2531-4 (b) Replace 16 nuts on RH side. 1 Remove : 16 Nut ASNA2531-4 Discard 2 Install : 16 Nut ASNA2531-4

(24) Subtask 535056-960-025-001 - Area 15, replace nuts from LH and RH sides of FR53-6 splicing Work Zones and Access Panels Zone Access/Work location 260 Work location Frame 53-6 from Stringer 27 to Stringer 28 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 183 5

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# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA25 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 6 NUT Replace 6 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 3 nuts on LH side. 1 Remove : 3 Nut ASNA2531-4 Discard 2 Install : 3 Nut ASNA2531-4 (b) Replace 3 nuts on RH side. 1 Remove : 3 Nut ASNA2531-4 Discard 2 Install : 3 Nut ASNA2531-4

(25) Subtask 535056-960-026-001 - Area 16, replace nuts from LH and RH seat track splicings Work Zones and Access Panels Zone Access/Work location 250 Work location from Frame 53-1 to Frame 53-2 Manpower Resources Manhours 5.00 Minimum number of person 2 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Component COMPA26 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 44 NUT Replace 44 nuts as described in Repair Instruction (RI) R51415000.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 184 5

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# @A340-500/600
SERVICE BULLETIN
(a) Replace 20 nuts on LH side. 1 Remove : 20 Nut ASNA2531-4 Discard 2 Install : 20 Nut ASNA2531-4 (b) Replace 20 nuts on RH side. 1 Remove : 20 Nut ASNA2531-4 Discard 2 Install : 20 Nut ASNA2531-4 (c) Replace 4 nuts at Y0. 1 Remove : 4 Nut ASNA2531-4 Discard 2 Install : 4 Nut ASNA2531-4

(26) Subtask 535056-960-027-001 - Area 17, replace nuts from LH and RH seat track splicings Work Zones and Access Panels Zone Access/Work location 260 Work location Frame 53-7 Manpower Resources Manhours 5.00 Minimum number of person 2 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Component COMPA27 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 44 NUT Replace 44 nuts as described in Repair Instruction (RI) R51415000.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 185 5

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# @A340-500/600
SERVICE BULLETIN
(a) Replace 20 nuts on LH side. 1 Remove : 20 Nut ASNA2531-4 Discard 2 Install : 20 Nut ASNA2531-4 (b) Replace 20 nuts on RH side. 1 Remove : 20 Nut ASNA2531-4 Discard 2 Install : 20 Nut ASNA2531-4 (c) Replace 4 nuts at Y0. 1 Remove : 4 Nut ASNA2531-4 Discard 2 Install : 4 Nut ASNA2531-4

(27) Subtask 535056-960-028-002 - Area 18, replace nuts from rear section FR54 stringer 54 LH sideWork Zones and Access Panels Zone Access/Work location 260 Work location Frame 54 Stringer 54 Manpower Resources Manhours 2.50 Minimum number of person 2 Subtask elapsed time 1.50 Skills AIRFRAME Material necessary to do the job Component COMPA29 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 22 NUT Replace 22 nuts as described in Repair Instruction (RI) R51415000.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 186 5

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# @A340-500/600
SERVICE BULLETIN
(a) Remove : 22 Nut ASNA2531-4 Discard (b) Install : 22 Nut ASNA2531-4

(28) Subtask 535056-960-030-001 - Area 20, replace nuts from LH and RH fixed inner shroud boxes Work Zones and Access Panels Zone Access/Work location 570 670 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills AIRFRAME Material necessary to do the job Component COMPA31 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 16 NUT Replace 16 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 8 nuts on LH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4 (b) Replace 8 nuts on RH side. 1 Remove : 8 Nut ASNA2531-4 Discard 2 Install : 8 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 187 5

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# @A340-500/600
SERVICE BULLETIN
(29) Subtask 535056-960-031-007 - Area 21, replace nuts at FR38 and FR54 circumferential junctions Work Zones and Access Panels Zone Access/Work location 100 Work location Frame 38 Frame 54 200 Work location Frame 38 Frame 54 Manpower Resources Manhours 3.00 Minimum number of person 2 Subtask elapsed time 1.50 Skills AIRFRAME Material necessary to do the job Component COMPA38 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 29 NUT References Drawing R51415001 Replace 29 nuts as described in Repair Instruction (RI) R51415001. (a) Remove : 29 Nut ASNA2531-4 Discard (b) Install : 29 Nut ASNA2531-4

(30) Subtask 535056-960-037-001 - Area 23, replace nut in belly fairing zone 5 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME Material necessary to do the job Component COMPA39 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 1 NUT DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 188 5

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# @A340-500/600
SERVICE BULLETIN

References Drawing R51415001 Replace 1 nut as described in Repair Instruction (RI) R51415001. (a) Remove : 1 Nut ASNA2531-4 Discard (b) Install : 1 Nut ASNA2531-4

(31) Subtask 535056-960-032-001 - Area concession 1 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME Material necessary to do the job Component COMPA40 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 1 NUT References Drawing R51415001 Replace 1 nut as described in Repair Instruction (RI) R51415001. (a) Remove : 1 Nut ASNA2531-4 Discard (b) Install : 1 Nut ASNA2531-4

(32) Subtask 535056-960-033-002 - Area concession 2 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 189 5

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# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA41 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 2 NUT References Drawing R51415001 Replace 2 nuts as described in Repair Instruction (RI) R51415001. (a) Remove : 2 Nut ASNA2531-4 Discard (b) Install : 2 Nut ASNA2531-4

(33) Subtask 535056-960-034-001 - Area concession 3 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME Material necessary to do the job Component COMPA42 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 1 NUT References Drawing R51415001 Replace 1 nut as described in Repair Instruction (RI) R51415001. (a) Remove : 1 Nut ASNA2531-4 Discard (b) Install : 1 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 190 5

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# @A340-500/600
SERVICE BULLETIN
(34) Subtask 535056-960-035-001 - Area concession 4 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills AIRFRAME Material necessary to do the job Component COMPA43 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 1 NUT References Drawing R51415001 Replace 1 nut as described in Repair Instruction (RI) R51415001. (a) Remove : 1 Nut ASNA2531-4 Discard (b) Install : 1 Nut ASNA2531-4 **CONF 009 (1) Subtask 535056-832-001-009 - Inspection / Repair Work Zones and Access Panels Zone Access/Work location 100 200 Manpower Resources Manhours 4.00 Minimum number of person 4 Subtask elapsed time 1.00 Skills AIRFRAME References Drawing R51415000 R51415001 Fig. A-FBCAA Flow Chart Sheet 01

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 191 5

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# @A340-500/600
SERVICE BULLETIN
(a) Perform a visual inspection of the nuts looking for cracked or missing nuts as described inFig. A-FBCAA: 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 10, 11 and area concession 1. - For the inspection areas, refer to Repair Instruction (RI) R51415000. - For the inspection report, refer to Appendix 01 Inspection Report. . 3 If no findings, replace the nut before next flight. (b) Replacement principle of the nut : 1 Remove half of the required nuts equally spread.
a Remove the nut using an ALLEN key to maintain the fastener. 2 Install new nuts.
a Install the nut using an ALLEN key to maintain the fastener. 3 Perform the replacement of the half remaining nuts. NOTE: If the fastener rotates, refer to Repair Instruction (RI) R51415000. (2) Subtask 535056-960-020-001 - Area 10, replace nuts from LH and RH sides of longitudinal joint Work Zones and Access Panels Zone Access/Work location 130 Work location Frame 39 from Stringer 28 to Stringer 29 Manpower Resources Manhours 1.50 Minimum number of person 1 Subtask elapsed time 1.50 Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 192 5

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# @A340-500/600
SERVICE BULLETIN
Material necessary to do the job Component COMPA19 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 10 NUT Replace 10 nuts as described in Repair Instruction (RI) R51415000. (a) Replace 5 nuts on LH side. 1 Remove : 5 Nut ASNA2531-4 Discard 2 Install : 5 Nut ASNA2531-4 (b) Replace 5 nuts on RH side. 1 Remove : 5 Nut ASNA2531-4 Discard 2 Install : 5 Nut ASNA2531-4

(3) Subtask 535056-960-021-003 - Area 11, replace nuts of LH and RH cleat attachments Work Zones and Access Panels Zone Access/Work location 250 Work location Frame 47 Stringer 23 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Component COMPA20 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 4 NUT

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 193 5

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# @A340-500/600
SERVICE BULLETIN

References Drawing R51415000 Replace 4 nuts as described in Repair Instruction (RI) R51415000). (a) Replace 2 nuts on LH side. 1 Remove : 2 Nut ASNA2531-4 Discard 2 Install : 2 Nut ASNA2531-4 (b) Replace 2 nuts on RH side. 1 Remove : 2 Nut ASNA2531-4 Discard 2 Install : 2 Nut ASNA2531-4

(4) Subtask 535056-960-032-005 - Area concession 1 Manpower Resources Manhours 1.50 Minimum number of person 2 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Component COMPA40 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES ASNA2531-4 16 NUT References Drawing R51415001 Replace 16 nuts as described in Repair Instruction (RI) R51415001. (a) Remove : 16 Nut ASNA2531-4 Discard (b) Install : 16 Nut ASNA2531-4

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 194 5

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# @A340-500/600
SERVICE BULLETIN

**CONF ALL D. TEST **CONF 001 (1) Subtask 535056-941-002-001 - Test Job Set-up Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801 NOTE: Before the tests, do not forget to install the parts and/or equipment as required in SUBTASK 535056-942-001 001 Close-up . (a) In the cockpit, on the panel 235VU, push the push-button switches : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B). (b) Remove the warning notices. (c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801) (2) Subtask 535056-865-001-001 - C/B Closing Manpower Resources Skills AIRFRAME (a) Close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 742 701PP 10PB1 72 S 742 702PP 10PB2 71 S

(3) Subtask 535056-941-003-001 - Preliminary Tests Manpower Resources Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 195 5

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# @A340-500/600
SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) Task 21-26-00-710-803 Task 22-96-00-740-801 Task 22-97-00-740-801 Task 31-50-00-710-803 Task 31-50-00-740-801 Task 31-60-00-710-802 Task 33-13-00-710-801 Task 33-14-00-710-801 Elec. Std. Practices Manual (ESPM) 20-52-10 NOTE: If the aircraft is operated in actual CAT III conditions, you must also do the LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801). (a) On each connector which was disconnected : 1 Do the checks as defined by ESPM 20-52-10. NOTE: The functional test and/or operational test requested by the ESPM procedure are given hereafter. (b) Do the operational test of the instrument and panel integral lighting (Refer to AMM Task 33-13-00-710-801). (c) Do the operational test of lights (Refer to AMM Task 33-14-00-710-801). (d) Do the operational test of the avionics-equipment ventilation system (Refer to AMM Task 21-26-00-710-803). (e) Do the BITE test of the auto flight system (SYSTEM TEST) (Refer to AMM Task 22-96-00-740-801). (f) Do the operational test of the ECAM control panel (Refer to AMM Task 31-50-00-710-803). (g) Do the test of FWS (Refer to AMM Task 31-50-00-740-801). (h) Do the operational test of EIS (Refer to AMM Task 31-60-00-710-802). (4) Subtask 535056-700-001-003 - Tests Manpower Resources Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 196 5

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# @A340-500/600
SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 21-20-00, Page Block 201 Task 21-28-00-710-802 Task 21-42-41-400-801 Task 21-52-41-400-801 Task 21-53-00-710-801 Task 21-53-00-710-802 Task 21-53-00-710-803 Task 21-63-00-710-801 Task 25-21-41-400-801 Task 25-23-41-400-801 Task 25-42-41-400-801 Task 25-42-42-400-801 Task 53-35-41-400-801 (a) If removed during preparation, do the test procedure as specified after the installation of the air-conditioning distribution ducts (Refer to AMM 21-20-00, Page Block 201). (b) 212HG, 213HG : - Do the operational test of LDCC ventilation system (Refer to AMM Task 21-28-00-710-802). (c) 681HK, 682HK : - Do the operational test of the cockpit and cabin temperature control-system (Refer to AMM Task 21-63-00-710-801). (d) If removed during preparation, do the test procedure as specified after the installation of the air inlet flap assembly (Refer to AMM Task 53-35-41-400-801). (e) If removed during preparation, do the test procedure as specified after the installation of the lavatory H (Refer to AMM Task 25-42-41-400-801). (f) If removed during preparation, do the test procedure as specified after the installation of the lavatory K (Refer to AMM Task 25-42-42-400-801). (g) If removed during preparation, do the test procedure as specified after the installation of the ceiling panels (Refer to AMM Task 25-23-41-400-801). **CONF 002 (1) Subtask 535056-941-002-001 - Test Job Set-up Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801 NOTE: Before the tests, do not forget to install the parts and/or equipment as required in SUBTASK 535056-942-001 004 Close-up . DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 197 5

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# @A340-500/600
SERVICE BULLETIN
(a) In the cockpit, on the panel 235VU, push the push-button switches : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B). (b) Remove the warning notices. (c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801) (2) Subtask 535056-865-001-001 - C/B Closing Manpower Resources Skills AIRFRAME (a) Close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 742 701PP 10PB1 72 S 742 702PP 10PB2 71 S

(3) Subtask 535056-941-003-001 - Preliminary Tests Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-26-00-710-803 Task 22-96-00-740-801 Task 22-97-00-740-801 Task 31-50-00-710-803 Task 31-50-00-740-801 Task 31-60-00-710-802 Task 33-13-00-710-801 Task 33-14-00-710-801 Elec. Std. Practices Manual (ESPM) 20-52-10 NOTE: If the aircraft is operated in actual CAT III conditions, you must also do the LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801). (a) On each connector which was disconnected : 1 Do the checks as defined by ESPM 20-52-10. NOTE: The functional test and/or operational test requested by the ESPM procedure are given hereafter. (b) Do the operational test of the instrument and panel integral lighting (Refer to AMM Task 33-13-00-710-801).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 198 5

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# @A340-500/600
SERVICE BULLETIN
(c) Do the operational test of lights (Refer to AMM Task 33-14-00-710-801). (d) Do the operational test of the avionics-equipment ventilation system (Refer to AMM Task 21-26-00-710-803). (e) Do the BITE test of the auto flight system (SYSTEM TEST) (Refer to AMM Task 22-96-00-740-801). (f) Do the operational test of the ECAM control panel (Refer to AMM Task 31-50-00-710-803). (g) Do the test of FWS (Refer to AMM Task 31-50-00-740-801). (h) Do the operational test of EIS (Refer to AMM Task 31-60-00-710-802). (4) Subtask 535056-700-001-004 - Tests Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 21-20-00, Page Block 201 Task 21-28-00-710-802 Task 21-42-41-400-801 Task 21-52-41-400-801 Task 21-53-00-710-801 Task 21-53-00-710-802 Task 21-53-00-710-803 Task 21-63-00-710-801 Task 25-21-41-400-801 Task 25-23-41-400-801 Task 25-42-41-400-801 Task 25-42-42-400-801 Task 25-77-38-400-801 Task 53-35-41-400-801 Task 57-17-11-400-801 Task 57-27-11-400-801 (a) Do the test procedure as specified after installation of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801). (b) Do the test procedure as specified after installation of the fuel tank access covers 147AZ and 148AZ (Refer to AMM Task 57-17-11-400-801). (c) If removed during preparation, do the test procedure as specified after the installation of the air-conditioning distribution ducts (Refer to AMM 21-20-00, Page Block 201). (d) 212HG, 213HG : - Do the operational test of LDCC ventilation system (Refer to AMM Task 21-28-00-710-802).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 199 5

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# @A340-500/600
SERVICE BULLETIN
(e) 681HK, 682HK : - Do the operational test of the cockpit and cabin temperature control-system (Refer to AMM Task 21-63-00-710-801). (f) If removed during preparation, do the test procedure as specified after the installation of the air inlet flap assembly (Refer to AMM Task 53-35-41-400-801). (g) If removed during preparation, do the test procedure as specified after the installation of the lavatory H (Refer to AMM Task 25-42-41-400-801). (h) If removed during preparation, do the test procedure as specified after the installation of the lavatory K (Refer to AMM Task 25-42-42-400-801). (i) If removed during preparation, do the test procedure as specified after the installation of the ceiling panels (Refer to AMM Task 25-23-41-400-801). **CONF 003 (1) Subtask 535056-941-002-001 - Test Job Set-up Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801 NOTE: Before the tests, do not forget to install the parts and/or equipment as required in SUBTASK 535056-942-001 005 Close-up . (a) In the cockpit, on the panel 235VU, push the push-button switches : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B). (b) Remove the warning notices. (c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801) (2) Subtask 535056-865-001-001 - C/B Closing Manpower Resources Skills AIRFRAME (a) Close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 742 701PP 10PB1 72 S 742 702PP 10PB2 71 S
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 200 5

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# @A340-500/600
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(3) Subtask 535056-941-003-001 - Preliminary Tests Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-26-00-710-803 Task 22-96-00-740-801 Task 22-97-00-740-801 Task 31-50-00-710-803 Task 31-50-00-740-801 Task 31-60-00-710-802 Task 33-13-00-710-801 Task 33-14-00-710-801 Elec. Std. Practices Manual (ESPM) 20-52-10 NOTE: If the aircraft is operated in actual CAT III conditions, you must also do the LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801). (a) On each connector which was disconnected : 1 Do the checks as defined by ESPM 20-52-10. NOTE: The functional test and/or operational test requested by the ESPM procedure are given hereafter. (b) Do the operational test of the instrument and panel integral lighting (Refer to AMM Task 33-13-00-710-801). (c) Do the operational test of lights (Refer to AMM Task 33-14-00-710-801). (d) Do the operational test of the avionics-equipment ventilation system (Refer to AMM Task 21-26-00-710-803). (e) Do the BITE test of the auto flight system (SYSTEM TEST) (Refer to AMM Task 22-96-00-740-801). (f) Do the operational test of the ECAM control panel (Refer to AMM Task 31-50-00-710-803). (g) Do the test of FWS (Refer to AMM Task 31-50-00-740-801). (h) Do the operational test of EIS (Refer to AMM Task 31-60-00-710-802). (4) Subtask 535056-700-001-003 - Tests Manpower Resources Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 201 5

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# @A340-500/600
SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 21-20-00, Page Block 201 Task 21-28-00-710-802 Task 21-42-41-400-801 Task 21-52-41-400-801 Task 21-53-00-710-801 Task 21-53-00-710-802 Task 21-53-00-710-803 Task 21-63-00-710-801 Task 25-21-41-400-801 Task 25-23-41-400-801 Task 25-42-41-400-801 Task 25-42-42-400-801 Task 53-35-41-400-801 (a) If removed during preparation, do the test procedure as specified after the installation of the air-conditioning distribution ducts (Refer to AMM 21-20-00, Page Block 201). (b) 212HG, 213HG : - Do the operational test of LDCC ventilation system (Refer to AMM Task 21-28-00-710-802). (c) 681HK, 682HK : - Do the operational test of the cockpit and cabin temperature control-system (Refer to AMM Task 21-63-00-710-801). (d) If removed during preparation, do the test procedure as specified after the installation of the air inlet flap assembly (Refer to AMM Task 53-35-41-400-801). (e) If removed during preparation, do the test procedure as specified after the installation of the lavatory H (Refer to AMM Task 25-42-41-400-801). (f) If removed during preparation, do the test procedure as specified after the installation of the lavatory K (Refer to AMM Task 25-42-42-400-801). (g) If removed during preparation, do the test procedure as specified after the installation of the ceiling panels (Refer to AMM Task 25-23-41-400-801). **CONF 004 (1) Subtask 535056-941-002-001 - Test Job Set-up Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801 NOTE: Before the tests, do not forget to install the parts and/or equipment as required in SUBTASK 535056-942-001 001 Close-up . DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 202 5

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# @A340-500/600
SERVICE BULLETIN
(a) In the cockpit, on the panel 235VU, push the push-button switches : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B). (b) Remove the warning notices. (c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801) (2) Subtask 535056-865-001-001 - C/B Closing Manpower Resources Skills AIRFRAME (a) Close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 742 701PP 10PB1 72 S 742 702PP 10PB2 71 S

(3) Subtask 535056-941-003-001 - Preliminary Tests Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-26-00-710-803 Task 22-96-00-740-801 Task 22-97-00-740-801 Task 31-50-00-710-803 Task 31-50-00-740-801 Task 31-60-00-710-802 Task 33-13-00-710-801 Task 33-14-00-710-801 Elec. Std. Practices Manual (ESPM) 20-52-10 NOTE: If the aircraft is operated in actual CAT III conditions, you must also do the LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801). (a) On each connector which was disconnected : 1 Do the checks as defined by ESPM 20-52-10. NOTE: The functional test and/or operational test requested by the ESPM procedure are given hereafter. (b) Do the operational test of the instrument and panel integral lighting (Refer to AMM Task 33-13-00-710-801).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 203 5

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# @A340-500/600
SERVICE BULLETIN
(c) Do the operational test of lights (Refer to AMM Task 33-14-00-710-801). (d) Do the operational test of the avionics-equipment ventilation system (Refer to AMM Task 21-26-00-710-803). (e) Do the BITE test of the auto flight system (SYSTEM TEST) (Refer to AMM Task 22-96-00-740-801). (f) Do the operational test of the ECAM control panel (Refer to AMM Task 31-50-00-710-803). (g) Do the test of FWS (Refer to AMM Task 31-50-00-740-801). (h) Do the operational test of EIS (Refer to AMM Task 31-60-00-710-802). (4) Subtask 535056-700-001-003 - Tests Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 21-20-00, Page Block 201 Task 21-28-00-710-802 Task 21-42-41-400-801 Task 21-52-41-400-801 Task 21-53-00-710-801 Task 21-53-00-710-802 Task 21-53-00-710-803 Task 21-63-00-710-801 Task 25-21-41-400-801 Task 25-23-41-400-801 Task 25-42-41-400-801 Task 25-42-42-400-801 Task 53-35-41-400-801 (a) If removed during preparation, do the test procedure as specified after the installation of the air-conditioning distribution ducts (Refer to AMM 21-20-00, Page Block 201). (b) 212HG, 213HG : - Do the operational test of LDCC ventilation system (Refer to AMM Task 21-28-00-710-802). (c) 681HK, 682HK : - Do the operational test of the cockpit and cabin temperature control-system (Refer to AMM Task 21-63-00-710-801). (d) If removed during preparation, do the test procedure as specified after the installation of the air inlet flap assembly (Refer to AMM Task 53-35-41-400-801).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 204 5

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# @A340-500/600
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(e) If removed during preparation, do the test procedure as specified after the installation of the lavatory H (Refer to AMM Task 25-42-41-400-801). (f) If removed during preparation, do the test procedure as specified after the installation of the lavatory K (Refer to AMM Task 25-42-42-400-801). (g) If removed during preparation, do the test procedure as specified after the installation of the ceiling panels (Refer to AMM Task 25-23-41-400-801). **CONF 005 (1) Subtask 535056-941-002-001 - Test Job Set-up Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801 NOTE: Before the tests, do not forget to install the parts and/or equipment as required in SUBTASK 535056-942-001 006 Close-up . (a) In the cockpit, on the panel 235VU, push the push-button switches : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B). (b) Remove the warning notices. (c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801) (2) Subtask 535056-865-001-001 - C/B Closing Manpower Resources Skills AIRFRAME (a) Close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 742 701PP 10PB1 72 S 742 702PP 10PB2 71 S

(3) Subtask 535056-941-003-001 - Preliminary Tests Manpower Resources Skills AIRFRAME

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# @A340-500/600
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References Aircraft Maintenance Manual (AMM) Task 21-26-00-710-803 Task 22-96-00-740-801 Task 22-97-00-740-801 Task 31-50-00-710-803 Task 31-50-00-740-801 Task 31-60-00-710-802 Task 33-13-00-710-801 Task 33-14-00-710-801 Elec. Std. Practices Manual (ESPM) 20-52-10 NOTE: If the aircraft is operated in actual CAT III conditions, you must also do the LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801). (a) On each connector which was disconnected : 1 Do the checks as defined by ESPM 20-52-10. NOTE: The functional test and/or operational test requested by the ESPM procedure are given hereafter. (b) Do the operational test of the instrument and panel integral lighting (Refer to AMM Task 33-13-00-710-801). (c) Do the operational test of lights (Refer to AMM Task 33-14-00-710-801). (d) Do the operational test of the avionics-equipment ventilation system (Refer to AMM Task 21-26-00-710-803). (e) Do the BITE test of the auto flight system (SYSTEM TEST) (Refer to AMM Task 22-96-00-740-801). (f) Do the operational test of the ECAM control panel (Refer to AMM Task 31-50-00-710-803). (g) Do the test of FWS (Refer to AMM Task 31-50-00-740-801). (h) Do the operational test of EIS (Refer to AMM Task 31-60-00-710-802). (4) Subtask 535056-700-001-003 - Tests Manpower Resources Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 206 5

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# @A340-500/600
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References Aircraft Maintenance Manual (AMM) 21-20-00, Page Block 201 Task 21-28-00-710-802 Task 21-42-41-400-801 Task 21-52-41-400-801 Task 21-53-00-710-801 Task 21-53-00-710-802 Task 21-53-00-710-803 Task 21-63-00-710-801 Task 25-21-41-400-801 Task 25-23-41-400-801 Task 25-42-41-400-801 Task 25-42-42-400-801 Task 53-35-41-400-801 (a) If removed during preparation, do the test procedure as specified after the installation of the air-conditioning distribution ducts (Refer to AMM 21-20-00, Page Block 201). (b) 212HG, 213HG : - Do the operational test of LDCC ventilation system (Refer to AMM Task 21-28-00-710-802). (c) 681HK, 682HK : - Do the operational test of the cockpit and cabin temperature control-system (Refer to AMM Task 21-63-00-710-801). (d) If removed during preparation, do the test procedure as specified after the installation of the air inlet flap assembly (Refer to AMM Task 53-35-41-400-801). (e) If removed during preparation, do the test procedure as specified after the installation of the lavatory H (Refer to AMM Task 25-42-41-400-801). (f) If removed during preparation, do the test procedure as specified after the installation of the lavatory K (Refer to AMM Task 25-42-42-400-801). (g) If removed during preparation, do the test procedure as specified after the installation of the ceiling panels (Refer to AMM Task 25-23-41-400-801). **CONF 006 (1) Subtask 535056-941-002-001 - Test Job Set-up Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801 NOTE: Before the tests, do not forget to install the parts and/or equipment as required in SUBTASK 535056-942-001 009 Close-up . DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 207 5

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# @A340-500/600
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(a) In the cockpit, on the panel 235VU, push the push-button switches : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B). (b) Remove the warning notices. (c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801) (2) Subtask 535056-865-001-001 - C/B Closing Manpower Resources Skills AIRFRAME (a) Close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 742 701PP 10PB1 72 S 742 702PP 10PB2 71 S

(3) Subtask 535056-941-003-001 - Preliminary Tests Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-26-00-710-803 Task 22-96-00-740-801 Task 22-97-00-740-801 Task 31-50-00-710-803 Task 31-50-00-740-801 Task 31-60-00-710-802 Task 33-13-00-710-801 Task 33-14-00-710-801 Elec. Std. Practices Manual (ESPM) 20-52-10 NOTE: If the aircraft is operated in actual CAT III conditions, you must also do the LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801). (a) On each connector which was disconnected : 1 Do the checks as defined by ESPM 20-52-10. NOTE: The functional test and/or operational test requested by the ESPM procedure are given hereafter. (b) Do the operational test of the instrument and panel integral lighting (Refer to AMM Task 33-13-00-710-801).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 208 5

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# @A340-500/600
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(c) Do the operational test of lights (Refer to AMM Task 33-14-00-710-801). (d) Do the operational test of the avionics-equipment ventilation system (Refer to AMM Task 21-26-00-710-803). (e) Do the BITE test of the auto flight system (SYSTEM TEST) (Refer to AMM Task 22-96-00-740-801). (f) Do the operational test of the ECAM control panel (Refer to AMM Task 31-50-00-710-803). (g) Do the test of FWS (Refer to AMM Task 31-50-00-740-801). (h) Do the operational test of EIS (Refer to AMM Task 31-60-00-710-802). (4) Subtask 535056-700-001-004 - Tests Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) 21-20-00, Page Block 201 Task 21-28-00-710-802 Task 21-42-41-400-801 Task 21-52-41-400-801 Task 21-53-00-710-801 Task 21-53-00-710-802 Task 21-53-00-710-803 Task 21-63-00-710-801 Task 25-21-41-400-801 Task 25-23-41-400-801 Task 25-42-41-400-801 Task 25-42-42-400-801 Task 25-77-38-400-801 Task 53-35-41-400-801 Task 57-17-11-400-801 Task 57-27-11-400-801 (a) Do the test procedure as specified after installation of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801). (b) Do the test procedure as specified after installation of the fuel tank access covers 147AZ and 148AZ (Refer to AMM Task 57-17-11-400-801). (c) If removed during preparation, do the test procedure as specified after the installation of the air-conditioning distribution ducts (Refer to AMM 21-20-00, Page Block 201). (d) 212HG, 213HG : - Do the operational test of LDCC ventilation system (Refer to AMM Task 21-28-00-710-802).

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# @A340-500/600
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(e) 681HK, 682HK : - Do the operational test of the cockpit and cabin temperature control-system (Refer to AMM Task 21-63-00-710-801). (f) If removed during preparation, do the test procedure as specified after the installation of the air inlet flap assembly (Refer to AMM Task 53-35-41-400-801). (g) If removed during preparation, do the test procedure as specified after the installation of the lavatory H (Refer to AMM Task 25-42-41-400-801). (h) If removed during preparation, do the test procedure as specified after the installation of the lavatory K (Refer to AMM Task 25-42-42-400-801). (i) If removed during preparation, do the test procedure as specified after the installation of the ceiling panels (Refer to AMM Task 25-23-41-400-801). **CONF 007 (1) Subtask 535056-941-002-001 - Test Job Set-up Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801 NOTE: Before the tests, do not forget to install the parts and/or equipment as required in SUBTASK 535056-942-001 007 Close-up . (a) In the cockpit, on the panel 235VU, push the push-button switches : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B). (b) Remove the warning notices. (c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801) (2) Subtask 535056-865-001-001 - C/B Closing Manpower Resources Skills AIRFRAME (a) Close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 742 701PP 10PB1 72 S 742 702PP 10PB2 71 S
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# @A340-500/600
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(3) Subtask 535056-941-003-001 - Preliminary Tests Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-26-00-710-803 Task 22-96-00-740-801 Task 22-97-00-740-801 Task 31-50-00-710-803 Task 31-50-00-740-801 Task 31-60-00-710-802 Task 33-13-00-710-801 Task 33-14-00-710-801 Elec. Std. Practices Manual (ESPM) 20-52-10 NOTE: If the aircraft is operated in actual CAT III conditions, you must also do the LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801). (a) On each connector which was disconnected : 1 Do the checks as defined by ESPM 20-52-10. NOTE: The functional test and/or operational test requested by the ESPM procedure are given hereafter. (b) Do the operational test of the instrument and panel integral lighting (Refer to AMM Task 33-13-00-710-801). (c) Do the operational test of lights (Refer to AMM Task 33-14-00-710-801). (d) Do the operational test of the avionics-equipment ventilation system (Refer to AMM Task 21-26-00-710-803). (e) Do the BITE test of the auto flight system (SYSTEM TEST) (Refer to AMM Task 22-96-00-740-801). (f) Do the operational test of the ECAM control panel (Refer to AMM Task 31-50-00-710-803). (g) Do the test of FWS (Refer to AMM Task 31-50-00-740-801). (h) Do the operational test of EIS (Refer to AMM Task 31-60-00-710-802). (4) Subtask 535056-700-001-002 - Tests Manpower Resources Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 211 5

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# @A340-500/600
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References Aircraft Maintenance Manual (AMM) 21-20-00, Page Block 201 Task 21-28-00-710-802 Task 21-42-41-400-801 Task 21-52-41-400-801 Task 21-53-00-710-801 Task 21-53-00-710-802 Task 21-53-00-710-803 Task 21-63-00-710-801 Task 25-21-41-400-801 Task 25-23-41-400-801 Task 25-37-41-400-801 Task 25-42-41-400-801 Task 25-42-42-400-801 Task 25-77-38-400-801 Task 53-35-41-400-801 Task 57-17-11-400-801 Task 57-27-11-400-801 (a) Do the test procedure as specified after installation of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801). (b) Do the test procedure as specified after installation of the fuel tank access covers 147AZ and 148AZ (Refer to AMM Task 57-17-11-400-801). (c) Do the tests after/removal of the air-conditioning distribution ducts (Refer to AMM 21-20-00, Page Block 201). (d) 521HH1, 522HH1 : - Do the system test of the pack control and indicating system (Refer to AMM Task 21-53-00-710-802). (e) 521HH3, 522HH3, 521HH6, 522HH6, 521HH7, 522HH7, 521HH8, 522HH8, 541HH, 542HH, 539HH, 540HH : - Do the operational test of the pack control and indicating system (Refer to AMM Task 21-53-00-710-801). (f) 533HH, 534HH : - Do the operational test of the pack 1/2 ram-air doors (Refer to AMM Task 21-53-00-710-803). (g) 212HG, 213HG : - Do the operational test of LDCC ventilation system (Refer to AMM Task 21-28-00-710-802). (h) 681HK, 682HK : - Do the operational test of the cockpit and cabin temperature control-system (Refer to AMM Task 21-63-00-710-801).
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 212 5

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# @A340-500/600
SERVICE BULLETIN
(i) Do the test procedure as specified after the installation of the air conditioning packs (521HH, 522HH (Refer to AMM Task 21-52-41-400-801). (j) Do the test procedure as specified after the installation of the air inlet flap assembly (Refer to AMM Task 53-35-41-400-801). (k) If removed during preparation, do the test procedure as specified after the installation of the lavatory H (Refer to AMM Task 25-42-41-400-801). (l) If removed during preparation, do the test procedure as specified after the installation of the ceiling panels (Refer to AMM Task 25-23-41-400-801). (m) If removed during preparation, do the test procedure as specified after the installation of the lavatory K (Refer to AMM Task 25-42-42-400-801). **CONF 008 (1) Subtask 535056-941-002-001 - Test Job Set-up Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801 NOTE: Before the tests, do not forget to install the parts and/or equipment as required in SUBTASK 535056-942-001 007 Close-up . (a) In the cockpit, on the panel 235VU, push the push-button switches : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B). (b) Remove the warning notices. (c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801) (2) Subtask 535056-865-001-001 - C/B Closing Manpower Resources Skills AIRFRAME (a) Close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 742 701PP 10PB1 72 S 742 702PP 10PB2 71 S

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 213 5

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# @A340-500/600
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(3) Subtask 535056-941-003-001 - Preliminary Tests Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-26-00-710-803 Task 22-96-00-740-801 Task 22-97-00-740-801 Task 31-50-00-710-803 Task 31-50-00-740-801 Task 31-60-00-710-802 Task 33-13-00-710-801 Task 33-14-00-710-801 Elec. Std. Practices Manual (ESPM) 20-52-10 NOTE: If the aircraft is operated in actual CAT III conditions, you must also do the LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801). (a) On each connector which was disconnected : 1 Do the checks as defined by ESPM 20-52-10. NOTE: The functional test and/or operational test requested by the ESPM procedure are given hereafter. (b) Do the operational test of the instrument and panel integral lighting (Refer to AMM Task 33-13-00-710-801). (c) Do the operational test of lights (Refer to AMM Task 33-14-00-710-801). (d) Do the operational test of the avionics-equipment ventilation system (Refer to AMM Task 21-26-00-710-803). (e) Do the BITE test of the auto flight system (SYSTEM TEST) (Refer to AMM Task 22-96-00-740-801). (f) Do the operational test of the ECAM control panel (Refer to AMM Task 31-50-00-710-803). (g) Do the test of FWS (Refer to AMM Task 31-50-00-740-801). (h) Do the operational test of EIS (Refer to AMM Task 31-60-00-710-802). (4) Subtask 535056-700-001-002 - Tests Manpower Resources Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 214 5

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# @A340-500/600
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References Aircraft Maintenance Manual (AMM) 21-20-00, Page Block 201 Task 21-28-00-710-802 Task 21-42-41-400-801 Task 21-52-41-400-801 Task 21-53-00-710-801 Task 21-53-00-710-802 Task 21-53-00-710-803 Task 21-63-00-710-801 Task 25-21-41-400-801 Task 25-23-41-400-801 Task 25-37-41-400-801 Task 25-42-41-400-801 Task 25-42-42-400-801 Task 25-77-38-400-801 Task 53-35-41-400-801 Task 57-17-11-400-801 Task 57-27-11-400-801 (a) Do the test procedure as specified after installation of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801). (b) Do the test procedure as specified after installation of the fuel tank access covers 147AZ and 148AZ (Refer to AMM Task 57-17-11-400-801). (c) Do the tests after/removal of the air-conditioning distribution ducts (Refer to AMM 21-20-00, Page Block 201). (d) 521HH1, 522HH1 : - Do the system test of the pack control and indicating system (Refer to AMM Task 21-53-00-710-802). (e) 521HH3, 522HH3, 521HH6, 522HH6, 521HH7, 522HH7, 521HH8, 522HH8, 541HH, 542HH, 539HH, 540HH : - Do the operational test of the pack control and indicating system (Refer to AMM Task 21-53-00-710-801). (f) 533HH, 534HH : - Do the operational test of the pack 1/2 ram-air doors (Refer to AMM Task 21-53-00-710-803). (g) 212HG, 213HG : - Do the operational test of LDCC ventilation system (Refer to AMM Task 21-28-00-710-802). (h) 681HK, 682HK : - Do the operational test of the cockpit and cabin temperature control-system (Refer to AMM Task 21-63-00-710-801).
DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 215 5

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# @A340-500/600
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(i) Do the test procedure as specified after the installation of the air conditioning packs (521HH, 522HH (Refer to AMM Task 21-52-41-400-801). (j) Do the test procedure as specified after the installation of the air inlet flap assembly (Refer to AMM Task 53-35-41-400-801). (k) If removed during preparation, do the test procedure as specified after the installation of the lavatory H (Refer to AMM Task 25-42-41-400-801). (l) If removed during preparation, do the test procedure as specified after the installation of the ceiling panels (Refer to AMM Task 25-23-41-400-801). (m) If removed during preparation, do the test procedure as specified after the installation of the lavatory K (Refer to AMM Task 25-42-42-400-801). **CONF 009 (1) Subtask 535056-941-002-001 - Test Job Set-up Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801 NOTE: Before the tests, do not forget to install the parts and/or equipment as required in SUBTASK 535056-942-001 008 Close-up . (a) In the cockpit, on the panel 235VU, push the push-button switches : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B). (b) Remove the warning notices. (c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801) (2) Subtask 535056-865-001-001 - C/B Closing Manpower Resources Skills AIRFRAME (a) Close the following circuit breakers : PANEL DESIGNATION FIN LOCATION SEE NOTES 742 701PP 10PB1 72 S 742 702PP 10PB2 71 S

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 216 5

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# @A340-500/600
SERVICE BULLETIN
(3) Subtask 535056-941-003-001 - Preliminary Tests Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 21-26-00-710-803 Task 22-96-00-740-801 Task 22-97-00-740-801 Task 31-50-00-710-803 Task 31-50-00-740-801 Task 31-60-00-710-802 Task 33-13-00-710-801 Task 33-14-00-710-801 Elec. Std. Practices Manual (ESPM) 20-52-10 NOTE: If the aircraft is operated in actual CAT III conditions, you must also do the LAND CAT III capability test (Refer to AMM Task 22-97-00-740-801). (a) On each connector which was disconnected : 1 Do the checks as defined by ESPM 20-52-10. NOTE: The functional test and/or operational test requested by the ESPM procedure are given hereafter. (b) Do the operational test of the instrument and panel integral lighting (Refer to AMM Task 33-13-00-710-801). (c) Do the operational test of lights (Refer to AMM Task 33-14-00-710-801). (d) Do the operational test of the avionics-equipment ventilation system (Refer to AMM Task 21-26-00-710-803). (e) Do the BITE test of the auto flight system (SYSTEM TEST) (Refer to AMM Task 22-96-00-740-801). (f) Do the operational test of the ECAM control panel (Refer to AMM Task 31-50-00-710-803). (g) Do the test of FWS (Refer to AMM Task 31-50-00-740-801). (h) Do the operational test of EIS (Refer to AMM Task 31-60-00-710-802). (4) Subtask 535056-700-001-003 - Tests Manpower Resources Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 217 5

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# @A340-500/600
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References Aircraft Maintenance Manual (AMM) 21-20-00, Page Block 201 Task 21-28-00-710-802 Task 21-42-41-400-801 Task 21-52-41-400-801 Task 21-53-00-710-801 Task 21-53-00-710-802 Task 21-53-00-710-803 Task 21-63-00-710-801 Task 25-21-41-400-801 Task 25-23-41-400-801 Task 25-42-41-400-801 Task 25-42-42-400-801 Task 53-35-41-400-801 (a) If removed during preparation, do the test procedure as specified after the installation of the air-conditioning distribution ducts (Refer to AMM 21-20-00, Page Block 201). (b) 212HG, 213HG : - Do the operational test of LDCC ventilation system (Refer to AMM Task 21-28-00-710-802). (c) 681HK, 682HK : - Do the operational test of the cockpit and cabin temperature control-system (Refer to AMM Task 21-63-00-710-801). (d) If removed during preparation, do the test procedure as specified after the installation of the air inlet flap assembly (Refer to AMM Task 53-35-41-400-801). (e) If removed during preparation, do the test procedure as specified after the installation of the lavatory H (Refer to AMM Task 25-42-41-400-801). (f) If removed during preparation, do the test procedure as specified after the installation of the lavatory K (Refer to AMM Task 25-42-42-400-801). (g) If removed during preparation, do the test procedure as specified after the installation of the ceiling panels (Refer to AMM Task 25-23-41-400-801). **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 535056-942-001-001 - Close-up Work Zones and Access Panels Zone Access/Work location 100 200 DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 218 5

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# @A340-500/600
SERVICE BULLETIN

570 670 Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 25-21-41-400-801 Task 25-22-44-400-801 Task 25-23-41-400-801 Task 25-23-43-400-801 Task 25-23-44-400-801 Task 25-23-61-400-801 Task 25-24-61-400-801 Task 25-28-41-400-801 Task 25-28-42-400-803 Task 25-28-43-400-801 Task 25-37-41-400-801 Task 25-42-41-400-801 Task 25-42-42-400-801 Task 25-52-00-400-801 Task 25-53-00-400-801 Task 25-77-38-400-801 Task 25-80-00-400-801 Task 27-50-00-866-802 Task 52-10-00-410-801 Task 52-30-00-080-801 Task 52-30-00-410-801 Task 53-00-00-400-801 Task 53-00-00-400-802 Task 53-00-00-400-803 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Depending on aircraft configuration, install the parts and/or equipment removed for access before SUBTASK 535056-941-002 001 Test Job Set-up : 1 Restore the insulation blankets moved or removed for access to their initial position (Refer to AMM Task 25-80-00-400-801). 2 Install the removed cabin floor panels (Refer to AMM Task 53-00-00-400-801) and/or FWD cargo panels (Refer to AMM Task 53-00-00-400-802) and/or the aft cargo floor panels (Refer to AMM Task 53-00-00-400-803). 3 Install the moisture barrier foil (Refer to AMM Task 25-28-43-400-801). 4 Install the non-textile floor covering (Refer to AMM Task 25-28-42-400-803). 5 Install the textile floor covering (Refer to AMM Task 25-28-41-400-801). 6 Install the passenger seats (Refer to AMM Task 25-21-41-400-801).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 219 5

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# @A340-500/600
SERVICE BULLETIN

7 Install the lavatory H (Refer to AMM Task 25-42-41-400-801). 8 Install the lavatory K (Refer to AMM Task 25-42-42-400-801). 9 Install the cabin attendant seat (Refer to AMM Task 25-22-44-400-801). 10 Install FWD cargo sidewall panels (Refer to AMM Task 25-52-00-400-801). 11 If removed, install the water dispenser unit 6691NW (Refer to AMM Task 25-77-38-400-801). 12 If removed, install the lower deck galley 6710ML (Refer to AMM Task 25-37-41-400-801). 13 Install aft cargo sidewall panels (Refer to AMM Task 25-53-00-400-801). 14 If removed, install the overhead stowage-compartments at FR38 and/or FR54 (Refer to AMM Task 25-24-61-400-801). 15 Install the upper sidewall panels and dado panels (Refer to AMM Task 25-23-43-400-801 and AMM Task 25-23-44-400-801). 16 Install the upper ceiling panels (Refer to AMM Task 25-23-41-400-801). 17 Install the lateral light covers (Refer to AMM Task 25-23-61-400-801). (c) Retract the flaps (Refer to AMM Task 27-50-00-866-802). (d) Restore the systems and aircraft to normal operating condition. (e) Close the aft and FWD cargo compartment doors 822 and 821 (Refer to AMM Task 52-30-00-410-801). 1 Remove the safety lock (Refer to AMM Task 52-30-00-080-801). (f) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801). (g) Remove the access platform(s). **CONF 002 (1) Subtask 535056-942-001-004 - Close-up Work Zones and Access Panels Zone Access/Work location 100 200 570 670 540 Manpower Resources Skills AIRFRAME DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 220 5

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# @A340-500/600
SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) Task 25-21-41-400-801 Task 25-22-44-400-801 Task 25-23-41-400-801 Task 25-23-43-400-801 Task 25-23-44-400-801 Task 25-23-61-400-801 Task 25-24-61-400-801 Task 25-28-41-400-801 Task 25-28-42-400-803 Task 25-28-43-400-801 Task 25-37-41-400-801 Task 25-42-41-400-801 Task 25-42-42-400-801 Task 25-52-00-400-801 Task 25-53-00-400-801 Task 25-77-38-400-801 Task 25-80-00-400-801 Task 27-50-00-866-802 28-10-00, Page Block 301 Task 52-10-00-410-801 Task 52-30-00-080-801 Task 52-30-00-410-801 Task 53-00-00-400-801 Task 53-00-00-400-802 Task 53-00-00-400-803 Task 53-12-13-400-801 Task 57-17-11-400-801 Task 57-27-11-400-801 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Depending on aircraft configuration and findings, access to center tank and inner tanks could be performed during the accomplishment of this Service Bulletin : 1 You must obey the safety procedures when you work in fuel tanks (Refer to AMM 28-10-00, Page Block 301). 2 Install the fuel tank access covers (Refer to AMM Task 57-17-11-400-801). 3 Install the fuel tank access panels (Refer to AMM Task 57-27-11-400-801). (c) Depending on aircraft configuration, install the parts and/or equipment removed for access before SUBTASK 535056-941-002 001 Test Job Set-up : 1 Restore the insulation blankets moved or removed for access to their initial position (Refer to AMM Task 25-80-00-400-801). 2 Install the floor panels removed in electronic compartment (Refer to AMM Task 53-12-13-400-801).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 221 5

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# @A340-500/600
SERVICE BULLETIN

3 Install the removed cabin floor panels (Refer to AMM Task 53-00-00-400-801) and/or FWD cargo panels (Refer to AMM Task 53-00-00-400-802) and/or the aft cargo floor panels (Refer to AMM Task 53-00-00-400-803). 4 Install the moisture barrier foil (Refer to AMM Task 25-28-43-400-801). 5 Install the non-textile floor covering (Refer to AMM Task 25-28-42-400-803). 6 Install the textile floor covering (Refer to AMM Task 25-28-41-400-801). 7 Install the passenger seats (Refer to AMM Task 25-21-41-400-801). 8 Install the lavatory H (Refer to AMM Task 25-42-41-400-801). 9 Install the lavatory K (Refer to AMM Task 25-42-42-400-801). 10 Install the cabin attendant seat (Refer to AMM Task 25-22-44-400-801). 11 Install FWD cargo sidewall panels (Refer to AMM Task 25-52-00-400-801). 12 If removed, install the water dispenser unit 6691NW (Refer to AMM Task 25-77-38-400-801). 13 If removed, install the lower deck galley 6710ML (Refer to AMM Task 25-37-41-400-801). 14 Install aft cargo sidewall panels (Refer to AMM Task 25-53-00-400-801). 15 Install the upper sidewall panels (Refer to AMM Task 25-23-43-400-801). 16 Install the upper ceiling panels (Refer to AMM Task 25-23-41-400-801). 17 Install the removed dado panels (Refer to AMM Task 25-23-44-400-801). 18 If removed, install the overhead stowage-compartments at FR38 and/or FR54 (Refer to AMM Task 25-24-61-400-801). 19 Install the lateral light covers (Refer to AMM Task 25-23-61-400-801). (d) Retract the flaps (Refer to AMM Task 27-50-00-866-802). (e) Close the access door 132AZ. (f) Restore the systems and aircraft to normal operating condition. (g) Close the aft and FWD cargo compartment doors 822 and 821 (Refer to AMM Task 52-30-00-410-801). 1 Remove the safety lock (Refer to AMM Task 52-30-00-080-801). (h) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801). (i) Remove the access platform(s).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 222 5

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# @A340-500/600
SERVICE BULLETIN

**CONF 003 (1) Subtask 535056-942-001-005 - Close-up Work Zones and Access Panels Zone Access/Work location 570 670 Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 27-50-00-866-802 Task 32-12-00-410-801 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the MLG door (Refer to AMM Task 32-12-00-410-801). (c) Retract the flaps (Refer to AMM Task 27-50-00-866-802). (d) Restore the systems and aircraft to normal operating condition. (e) Remove the access platform(s). **CONF 004 (1) Subtask 535056-942-001-001 - Close-up Work Zones and Access Panels Zone Access/Work location 100 200 570 670 Manpower Resources Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 223 5

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# @A340-500/600
SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) Task 25-21-41-400-801 Task 25-22-44-400-801 Task 25-23-41-400-801 Task 25-23-43-400-801 Task 25-23-44-400-801 Task 25-23-61-400-801 Task 25-24-61-400-801 Task 25-28-41-400-801 Task 25-28-42-400-803 Task 25-28-43-400-801 Task 25-37-41-400-801 Task 25-42-41-400-801 Task 25-42-42-400-801 Task 25-52-00-400-801 Task 25-53-00-400-801 Task 25-77-38-400-801 Task 25-80-00-400-801 Task 27-50-00-866-802 Task 52-10-00-410-801 Task 52-30-00-080-801 Task 52-30-00-410-801 Task 53-00-00-400-801 Task 53-00-00-400-802 Task 53-00-00-400-803 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Depending on aircraft configuration, install the parts and/or equipment removed for access before SUBTASK 535056-941-002 001 Test Job Set-up : 1 Restore the insulation blankets moved or removed for access to their initial position (Refer to AMM Task 25-80-00-400-801). 2 Install the removed cabin floor panels (Refer to AMM Task 53-00-00-400-801) and/or FWD cargo panels (Refer to AMM Task 53-00-00-400-802) and/or the aft cargo floor panels (Refer to AMM Task 53-00-00-400-803). 3 Install the moisture barrier foil (Refer to AMM Task 25-28-43-400-801). 4 Install the non-textile floor covering (Refer to AMM Task 25-28-42-400-803). 5 Install the textile floor covering (Refer to AMM Task 25-28-41-400-801). 6 Install the passenger seats (Refer to AMM Task 25-21-41-400-801). 7 Install the lavatory H (Refer to AMM Task 25-42-41-400-801). 8 Install the lavatory K (Refer to AMM Task 25-42-42-400-801). 9 Install the cabin attendant seat (Refer to AMM Task 25-22-44-400-801).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 224 5

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# @A340-500/600
SERVICE BULLETIN

10 Install FWD cargo sidewall panels (Refer to AMM Task 25-52-00-400-801). 11 If removed, install the water dispenser unit 6691NW (Refer to AMM Task 25-77-38-400-801). 12 If removed, install the lower deck galley 6710ML (Refer to AMM Task 25-37-41-400-801). 13 Install aft cargo sidewall panels (Refer to AMM Task 25-53-00-400-801). 14 If removed, install the overhead stowage-compartments at FR38 and/or FR54 (Refer to AMM Task 25-24-61-400-801). 15 Install the upper sidewall panels and dado panels (Refer to AMM Task 25-23-43-400-801 and AMM Task 25-23-44-400-801). 16 Install the upper ceiling panels (Refer to AMM Task 25-23-41-400-801). 17 Install the lateral light covers (Refer to AMM Task 25-23-61-400-801). (c) Retract the flaps (Refer to AMM Task 27-50-00-866-802). (d) Restore the systems and aircraft to normal operating condition. (e) Close the aft and FWD cargo compartment doors 822 and 821 (Refer to AMM Task 52-30-00-410-801). 1 Remove the safety lock (Refer to AMM Task 52-30-00-080-801). (f) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801). (g) Remove the access platform(s). **CONF 005 (1) Subtask 535056-942-001-006 - Close-up Work Zones and Access Panels Zone Access/Work location 100 200 570 670 Manpower Resources Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 225 5

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# @A340-500/600
SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) Task 25-21-41-400-801 Task 25-22-44-400-801 Task 25-23-41-400-801 Task 25-23-43-400-802 Task 25-23-44-400-801 Task 25-23-61-400-801 Task 25-24-61-400-801 Task 25-28-41-400-801 Task 25-28-42-400-803 Task 25-28-43-400-801 Task 25-32-84-400-801 Task 25-42-41-400-801 Task 25-42-42-400-801 Task 25-52-00-400-801 Task 25-53-00-400-801 Task 25-80-00-400-801 Task 27-50-00-866-802 28-10-00, Page Block 301 Task 52-10-00-410-801 Task 52-30-00-080-801 Task 52-30-00-410-801 Task 53-00-00-400-801 Task 53-00-00-400-802 Task 53-00-00-400-803 Task 53-12-13-400-801 Task 57-17-11-400-801 Task 57-27-11-400-801 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Depending on aircraft configuration, install the parts and/or equipment removed for access before SUBTASK 535056-941-002 001 Test Job Set-up : 1 Restore the insulation blankets moved or removed for access to their initial position (Refer to AMM Task 25-80-00-400-801). 2 Install the floor panels removed in electronic compartment (Refer to AMM Task 53-12-13-400-801). 3 Install the removed cabin floor panels (Refer to AMM Task 53-00-00-400-801) and/or FWD cargo panels (Refer to AMM Task 53-00-00-400-802) and/or the aft cargo floor panels (Refer to AMM Task 53-00-00-400-803). 4 Install the moisture barrier foil (Refer to AMM Task 25-28-43-400-801). 5 Install the non-textile floor covering (Refer to AMM Task 25-28-42-400-803). 6 Install the textile floor covering (Refer to AMM Task 25-28-41-400-801). 7 Install the passenger seats (Refer to AMM Task 25-21-41-400-801).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 226 5

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# @A340-500/600
SERVICE BULLETIN

8 Install the lavatory H (Refer to AMM Task 25-42-41-400-801). 9 Install the lavatory K (Refer to AMM Task 25-42-42-400-801). 10 Install the mid galley unit (Refer to AMM Task 25-32-84-400-801). 11 Install the cabin attendant seat (Refer to AMM Task 25-22-44-400-801). 12 Install FWD cargo sidewall panels (Refer to AMM Task 25-52-00-400-801). 13 Install aft cargo sidewall panels (Refer to AMM Task 25-53-00-400-801). 14 If removed, install the overhead stowage-compartments at FR38 and/or FR54 (Refer to AMM Task 25-24-61-400-801). 15 Install the upper sidewall panels and dado panels (Refer to AMM Task 25-23-43-400-802 and AMM Task 25-23-44-400-801). 16 Install the upper ceiling panels (Refer to AMM Task 25-23-41-400-801). 17 Install the lateral light covers (Refer to AMM Task 25-23-61-400-801). (c) Retract the flaps (Refer to AMM Task 27-50-00-866-802). (d) Close the access door 132AZ. (e) Restore the systems and aircraft to normal operating condition. (f) Close the aft and FWD cargo compartment doors 822 and 821 (Refer to AMM Task 52-30-00-410-801). 1 Remove the safety lock (Refer to AMM Task 52-30-00-080-801). (g) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801). (h) Remove the access platform(s). **CONF 006 (1) Subtask 535056-942-001-009 - Close-up Work Zones and Access Panels Zone Access/Work location 100 200 540 570 670 Manpower Resources Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 227 5

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# @A340-500/600
SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) Task 25-21-41-400-801 Task 25-22-44-400-801 Task 25-23-41-400-801 Task 25-23-43-400-801 Task 25-23-44-400-801 Task 25-23-61-400-801 Task 25-24-61-400-801 Task 25-28-41-400-801 Task 25-28-42-400-803 Task 25-28-43-400-801 Task 25-32-84-400-801 Task 25-42-41-400-801 Task 25-42-42-400-801 Task 25-52-00-400-801 Task 25-53-00-400-801 Task 25-80-00-400-801 Task 27-50-00-866-802 28-10-00, Page Block 301 Task 52-10-00-410-801 Task 52-30-00-080-801 Task 52-30-00-410-801 Task 53-00-00-400-801 Task 53-00-00-400-802 Task 53-00-00-400-803 Task 53-12-13-400-801 Task 57-17-11-400-801 Task 57-27-11-400-801 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Depending on aircraft configuration and findings, access to center tank and inner tanks could be performed during the accomplishment of this Service Bulletin : 1 Install the fuel tank access covers (Refer to AMM Task 57-17-11-400-801). NOTE: You must obey the safety procedures when you work in fuel tanks (Refer to AMM 28-10-00, Page Block 301). 2 Install the fuel tank access panels (Refer to AMM Task 57-27-11-400-801). 3 Remove all switches related to the fuel system from OFF. (c) Depending on aircraft configuration, install the parts and/or equipment removed for access before SUBTASK 535056-941-002 001 Test Job Set-up : 1 Restore the insulation blankets moved or removed for access to their initial position (Refer to AMM Task 25-80-00-400-801). 2 Install the floor panels removed in electronic compartment (Refer to AMM Task 53-12-13-400-801).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 228 5

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# @A340-500/600
SERVICE BULLETIN

3 Install the removed cabin floor panels (Refer to AMM Task 53-00-00-400-801) and/or FWD cargo panels (Refer to AMM Task 53-00-00-400-802) and/or the aft cargo floor panels (Refer to AMM Task 53-00-00-400-803). 4 Install the moisture barrier foil (Refer to AMM Task 25-28-43-400-801). 5 Install the non-textile floor covering (Refer to AMM Task 25-28-42-400-803). 6 Install the textile floor covering (Refer to AMM Task 25-28-41-400-801). 7 Install the passenger seats (Refer to AMM Task 25-21-41-400-801). 8 Install the lavatory H (Refer to AMM Task 25-42-41-400-801). 9 Install the lavatory K (Refer to AMM Task 25-42-42-400-801). 10 Install the mid galley unit (Refer to AMM Task 25-32-84-400-801). 11 Install the cabin attendant seat (Refer to AMM Task 25-22-44-400-801). 12 Install FWD cargo sidewall panels (Refer to AMM Task 25-52-00-400-801). 13 Install aft cargo sidewall panels (Refer to AMM Task 25-53-00-400-801). 14 If removed, install the overhead stowage-compartments at FR38 and/or FR54 (Refer to AMM Task 25-24-61-400-801). 15 Install the upper sidewall panels and dado panels (Refer to AMM Task 25-23-43-400-801 and AMM Task 25-23-44-400-801). 16 Install the upper ceiling panels (Refer to AMM Task 25-23-41-400-801). 17 Install the lateral light covers (Refer to AMM Task 25-23-61-400-801). (d) Retract the flaps (Refer to AMM Task 27-50-00-866-802). (e) Close the access door 132AZ. (f) Restore the systems and aircraft to normal operating condition. (g) Close the aft and FWD cargo compartment doors 822 and 821 (Refer to AMM Task 52-30-00-410-801). 1 Remove the safety lock (Refer to AMM Task 52-30-00-080-801). (h) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801). (i) Remove the access platform(s).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 229 5

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

# @A340-500/600
SERVICE BULLETIN

**CONF 007 (1) Subtask 535056-942-001-007 - Close-up Work Zones and Access Panels Zone Access/Work location 100 200 570 670 Manpower Resources Skills AIRFRAME Material necessary to do the job Component COMPA21 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 NSA5050-3 2 NUT 4 EN6115V4X-10 3 SCREW ASNA2531-4 3 NUT Component COMPA22 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 NSA5050-3 6 NUT 10 ASNA2027V4X-9 6 SCREW ASNA2531-4 6 NUT

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 230 5

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# @A340-500/600
SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) Task 21-52-41-400-801 Task 21-53-51-400-801 Task 25-21-41-400-801 Task 25-22-44-400-801 Task 25-23-41-400-801 Task 25-23-43-400-802 Task 25-23-44-400-801 Task 25-23-61-400-801 Task 25-24-61-400-801 Task 25-28-41-400-801 Task 25-28-42-400-803 Task 25-28-43-400-801 Task 25-32-84-400-801 Task 25-42-41-400-801 Task 25-42-42-400-801 Task 25-52-00-400-801 Task 25-53-00-400-801 Task 25-80-00-400-801 Task 27-50-00-866-802 28-10-00, Page Block 301 Task 32-12-00-410-801 Task 52-10-00-410-801 Task 52-30-00-080-801 Task 52-30-00-410-801 Task 53-00-00-400-801 Task 53-00-00-400-802 Task 53-00-00-400-803 Task 53-12-13-400-801 Task 53-35-11-400-802 Task 53-35-13-400-801 Task 53-35-13-400-802 Task 57-17-11-400-801 Task 57-27-11-400-801 Structural Repair Manual (SRM) 51-43-00 Fig. A-FBAAA Canted beam attachment FWD of FR53-2 LH, Removal of the Pipes Support for Access Sheet 01 Sheet 02
Fig. A-FBBAA Canted beam attachment FWD of FR53-2 RH, Removal of the Pipes Support for Access Sheet 01 Sheet 02

(a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Depending on aircraft configuration and findings, access to center tank and inner tanks could be performed during the accomplishment of this Service Bulletin : 1 You must obey the safety procedures when you work in fuel tanks (Refer to AMM 28-10-00, Page Block 301). DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 231 5

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# @A340-500/600
SERVICE BULLETIN

2 Install the fuel tank access covers (Refer to AMM Task 57-17-11-400-801). 3 Install the fuel tank access panels (Refer to AMM Task 57-27-11-400-801). 4 Remove all switches related to the fuel system from OFF. (c) Install the pipe support on LH canted beam attachment FWD of FR53.2 as described inFig. A-FBAAA

. 1 Oversize the 3 holes of the structure corresponding to the support attachments item 4 (Refer to SRM 51-43-00). 2 Move slightly the support item (5) to put back to its initial position. 3 Install the fasteners 1 and (2) on the pipe. 2 Nut NSA5050-3 Item 1 2 Screw NAS6603-3 Item (2) Retained at removal NOTE: The screws item (2) were retained at removal. 4 Install the fasteners 3 and 4 on the support item (5). 3 Nut ASNA2531-4 3 Screw EN6115V4X-10 Item 4 (d) Install the pipes support on RH canted beam attachment FWD of FR53.2 as described inFig. A-FBBAA

. 1 Oversize the 6 holes of the structure corresponding to the support attachments item 10 (Refer to SRM 51-43-00). 2 Move slightly the support item (8) to put back to its initial position. 3 Install the 6 fasteners 3 and 10 on the support item (8). 6 Nut ASNA2531-4 6 Screw ASNA2027V4X-9 Item 10 4 Install the fasteners (9) and (10) on the clamp of the pipe. NOTE: The fasteners item (9) and item (10) were retained at removal. 5 Install the 6 fasteners 1, (6) and (7) on the support item (8). 6 Nut NSA5050-3 Item 1 NOTE: The screws item (6) and the washers item (7) were retained at removal.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 232 5

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# @A340-500/600
SERVICE BULLETIN
(e) Depending on aircraft configuration, install the parts and/or equipment removed for access before SUBTASK 535056-941-002 001 Test Job Set-up : 1 Restore to their initial position the insulation blankets moved or removed for access (Refer to AMM Task 25-80-00-400-801). 2 Install the floor panels removed in electronic compartment (Refer to AMM Task 53-12-13-400-801). 3 Install the removed cabin floor panels (Refer to AMM Task 53-00-00-400-801) and/or FWD cargo panels (Refer to AMM Task 53-00-00-400-802) and/or the aft cargo floor panels (Refer to AMM Task 53-00-00-400-803). 4 Install the moisture barrier foil (Refer to AMM Task 25-28-43-400-801). 5 Install the non-textile floor covering (Refer to AMM Task 25-28-42-400-803). 6 Install the textile floor covering (Refer to AMM Task 25-28-41-400-801). 7 Install FWD cargo sidewall panels and partition panels (Refer to AMM Task 25-52-00-400-801). 8 Install aft cargo sidewall panels (Refer to AMM Task 25-53-00-400-801). 9 If removed, install the overhead stowage-compartments at FR38 and/or FR54 (Refer to AMM Task 25-24-61-400-801). 10 Install the upper sidewall panels and dado panels (Refer to AMM Task 25-23-43-400-802 and AMM Task 25-23-44-400-801). 11 Install the upper ceiling panels (Refer to AMM Task 25-23-41-400-801). 12 Install the dado panels (Refer to AMM Task 25-23-44-400-801). 13 Install the lateral light covers (Refer to AMM Task 25-23-61-400-801). 14 If removed, install the mid galley unit (Refer to AMM Task 25-32-84-400-801). 15 Install the cabin attendant seat (Refer to AMM Task 25-22-44-400-801). 16 Install the lavatory H (Refer to AMM Task 25-42-41-400-801). 17 Install the lavatory K (Refer to AMM Task 25-42-42-400-801). 18 If removed, install the passenger seats (Refer to AMM Task 25-21-41-400-801). 19 Install the fairing panels (Refer to AMM Task 53-35-11-400-802, AMM Task 53-35-13-400-801 and AMM Task 53-35-13-400-802). (f) Install LH and RH air conditioning packs 521HH and 522HH (Refer to AMM Task 21-52-41-400-801).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 233 5

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# @A340-500/600
SERVICE BULLETIN
(g) Install LH and RH air inlet assemblies 533HH and 534HH (Refer to AMM Task 21-53-51-400-801). (h) Retract the flaps (Refer to AMM Task 27-50-00-866-802). (i) Close the access door 132AZ. (j) Restore the systems and aircraft to normal operating condition. (k) Close the MLG door (Refer to AMM Task 32-12-00-410-801). (l) Close the aft and FWD cargo compartment doors 822 and 821 (Refer to AMM Task 52-30-00-410-801). 1 Remove the safety lock (Refer to AMM Task 52-30-00-080-801). (m) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801). (n) Remove the access platform(s). **CONF 008 (1) Subtask 535056-942-001-007 - Close-up Work Zones and Access Panels Zone Access/Work location 100 200 570 670 Manpower Resources Skills AIRFRAME Material necessary to do the job Component COMPA21 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 NSA5050-3 2 NUT 4 EN6115V4X-10 3 SCREW ASNA2531-4 3 NUT Component COMPA22 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 NSA5050-3 6 NUT 10 ASNA2027V4X-9 6 SCREW ASNA2531-4 6 NUT

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 234 5

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# @A340-500/600
SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) Task 21-52-41-400-801 Task 21-53-51-400-801 Task 25-21-41-400-801 Task 25-22-44-400-801 Task 25-23-41-400-801 Task 25-23-43-400-802 Task 25-23-44-400-801 Task 25-23-61-400-801 Task 25-24-61-400-801 Task 25-28-41-400-801 Task 25-28-42-400-803 Task 25-28-43-400-801 Task 25-32-84-400-801 Task 25-42-41-400-801 Task 25-42-42-400-801 Task 25-52-00-400-801 Task 25-53-00-400-801 Task 25-80-00-400-801 Task 27-50-00-866-802 28-10-00, Page Block 301 Task 32-12-00-410-801 Task 52-10-00-410-801 Task 52-30-00-080-801 Task 52-30-00-410-801 Task 53-00-00-400-801 Task 53-00-00-400-802 Task 53-00-00-400-803 Task 53-12-13-400-801 Task 53-35-11-400-802 Task 53-35-13-400-801 Task 53-35-13-400-802 Task 57-17-11-400-801 Task 57-27-11-400-801 Structural Repair Manual (SRM) 51-43-00 Fig. A-FBAAA Canted beam attachment FWD of FR53-2 LH, Removal of the Pipes Support for Access Sheet 01 Sheet 02
Fig. A-FBBAA Canted beam attachment FWD of FR53-2 RH, Removal of the Pipes Support for Access Sheet 01 Sheet 02

(a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Depending on aircraft configuration and findings, access to center tank and inner tanks could be performed during the accomplishment of this Service Bulletin : 1 You must obey the safety procedures when you work in fuel tanks (Refer to AMM 28-10-00, Page Block 301). DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 235 5

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SERVICE BULLETIN

2 Install the fuel tank access covers (Refer to AMM Task 57-17-11-400-801). 3 Install the fuel tank access panels (Refer to AMM Task 57-27-11-400-801). 4 Remove all switches related to the fuel system from OFF. (c) Install the pipe support on LH canted beam attachment FWD of FR53.2 as described inFig. A-FBAAA

. 1 Oversize the 3 holes of the structure corresponding to the support attachments item 4 (Refer to SRM 51-43-00). 2 Move slightly the support item (5) to put back to its initial position. 3 Install the fasteners 1 and (2) on the pipe. 2 Nut NSA5050-3 Item 1 2 Screw NAS6603-3 Item (2) Retained at removal NOTE: The screws item (2) were retained at removal. 4 Install the fasteners 3 and 4 on the support item (5). 3 Nut ASNA2531-4 3 Screw EN6115V4X-10 Item 4 (d) Install the pipes support on RH canted beam attachment FWD of FR53.2 as described inFig. A-FBBAA

. 1 Oversize the 6 holes of the structure corresponding to the support attachments item 10 (Refer to SRM 51-43-00). 2 Move slightly the support item (8) to put back to its initial position. 3 Install the 6 fasteners 3 and 10 on the support item (8). 6 Nut ASNA2531-4 6 Screw ASNA2027V4X-9 Item 10 4 Install the fasteners (9) and (10) on the clamp of the pipe. NOTE: The fasteners item (9) and item (10) were retained at removal. 5 Install the 6 fasteners 1, (6) and (7) on the support item (8). 6 Nut NSA5050-3 Item 1 NOTE: The screws item (6) and the washers item (7) were retained at removal.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 236 5

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# @A340-500/600
SERVICE BULLETIN
(e) Depending on aircraft configuration, install the parts and/or equipment removed for access before SUBTASK 535056-941-002 001 Test Job Set-up : 1 Restore to their initial position the insulation blankets moved or removed for access (Refer to AMM Task 25-80-00-400-801). 2 Install the floor panels removed in electronic compartment (Refer to AMM Task 53-12-13-400-801). 3 Install the removed cabin floor panels (Refer to AMM Task 53-00-00-400-801) and/or FWD cargo panels (Refer to AMM Task 53-00-00-400-802) and/or the aft cargo floor panels (Refer to AMM Task 53-00-00-400-803). 4 Install the moisture barrier foil (Refer to AMM Task 25-28-43-400-801). 5 Install the non-textile floor covering (Refer to AMM Task 25-28-42-400-803). 6 Install the textile floor covering (Refer to AMM Task 25-28-41-400-801). 7 Install FWD cargo sidewall panels and partition panels (Refer to AMM Task 25-52-00-400-801). 8 Install aft cargo sidewall panels (Refer to AMM Task 25-53-00-400-801). 9 If removed, install the overhead stowage-compartments at FR38 and/or FR54 (Refer to AMM Task 25-24-61-400-801). 10 Install the upper sidewall panels and dado panels (Refer to AMM Task 25-23-43-400-802 and AMM Task 25-23-44-400-801). 11 Install the upper ceiling panels (Refer to AMM Task 25-23-41-400-801). 12 Install the dado panels (Refer to AMM Task 25-23-44-400-801). 13 Install the lateral light covers (Refer to AMM Task 25-23-61-400-801). 14 If removed, install the mid galley unit (Refer to AMM Task 25-32-84-400-801). 15 Install the cabin attendant seat (Refer to AMM Task 25-22-44-400-801). 16 Install the lavatory H (Refer to AMM Task 25-42-41-400-801). 17 Install the lavatory K (Refer to AMM Task 25-42-42-400-801). 18 If removed, install the passenger seats (Refer to AMM Task 25-21-41-400-801). 19 Install the fairing panels (Refer to AMM Task 53-35-11-400-802, AMM Task 53-35-13-400-801 and AMM Task 53-35-13-400-802). (f) Install LH and RH air conditioning packs 521HH and 522HH (Refer to AMM Task 21-52-41-400-801).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 237 5

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# @A340-500/600
SERVICE BULLETIN
(g) Install LH and RH air inlet assemblies 533HH and 534HH (Refer to AMM Task 21-53-51-400-801). (h) Retract the flaps (Refer to AMM Task 27-50-00-866-802). (i) Close the access door 132AZ. (j) Restore the systems and aircraft to normal operating condition. (k) Close the MLG door (Refer to AMM Task 32-12-00-410-801). (l) Close the aft and FWD cargo compartment doors 822 and 821 (Refer to AMM Task 52-30-00-410-801). 1 Remove the safety lock (Refer to AMM Task 52-30-00-080-801). (m) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801). (n) Remove the access platform(s). **CONF 009 (1) Subtask 535056-942-001-008 - Close-up Work Zones and Access Panels Zone Access/Work location 100 200 Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 25-23-43-400-802 Task 25-23-61-400-801 Task 25-52-00-400-801 Task 25-80-00-400-801 Task 52-10-00-410-801 Task 52-30-00-080-801 Task 52-30-00-410-801 Task 53-35-13-400-802 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Depending on aircraft configuration, install the parts and/or equipment removed for access before SUBTASK 535056-941-002 001 Test Job Set-up : 1 Restore to their initial position the insulation blankets moved or removed for access (Refer to AMM Task 25-80-00-400-801). 2 Install the removed sidewall panels, partition panels and ceiling panels (Refer to AMM Task 25-52-00-400-801 and AMM Task 25-23-43-400-802). DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 238 5

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# @A340-500/600
SERVICE BULLETIN

3 Install the fairing panels (Refer to AMM Task 53-35-13-400-802). 4 Install the lateral light covers (Refer to AMM Task 25-23-61-400-801). (c) Close the FWD cargo compartment door 821 (Refer to AMM Task 52-30-00-410-801). 1 Remove the safety lock (Refer to AMM Task 52-30-00-080-801). (d) Restore the systems and aircraft to normal operating condition. (e) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801). (f) Remove the access platform(s).

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 239 5

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# @A340-500/600
SERVICE BULLETIN

**CONF 007 thru 008

F_SB_535056_5_BAAA_01_00 Z140 

### A FR53.1 FR53.2



### B

VIEW LOOKING AFT CANTED BEAM ATTACH. FWD OF FR53.2 LH SIDE 

## A

1JV 11JS STGR43LH STGR42LHSTGR41LH



### C



## B

Figure A-FBAAA - Sheet 01 Canted beam attachment FWD of FR53-2 LH, Removal of the Pipes Support for Access

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 240 5

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# @A340-500/600
SERVICE BULLETIN

**CONF 007 thru 008

VIEW LOOKING AFT FRONT OF FR53.2

3 (3) (4) GREEN HYDRAULIC CIRCUIT



## C

**D** 1 (1) (2) 

### D (5)

F_SB_535056_5_BAAA_02_02 4

Figure A-FBAAA - Sheet 02 Canted beam attachment FWD of FR53-2 LH, Removal of the Pipes Support for Access

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 241 5

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# @A340-500/600
SERVICE BULLETIN

**CONF 007 thru 008

Z140



### B


## A

FRONT OF FR53−2 RH SIDE VIEW LOOKING AFT FR53.2

(9) (10) IF INSTALLED 

### D **C**

1 (1) 6 POS



## B (6) (7) (8)

F_SB_535056_5_BBAA_01_01 Figure A-FBBAA - Sheet 01 Canted beam attachment FWD of FR53-2 RH, Removal of the Pipes Support for Access

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 242 5

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# @A340-500/600
SERVICE BULLETIN

**CONF 007 thru 008

VIEW LOOKING FWD STGR42 FR53.2

3 6 POS(3) 1 (1) (3) 3



## C

**D** (6) (7) (8)

F_SB_535056_5_BBAA_02_02 (10)10

10 (10)

Figure A-FBBAA - Sheet 02 Canted beam attachment FWD of FR53-2 RH, Removal of the Pipes Support for Access

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 243 5

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# @A340-500/600
SERVICE BULLETIN

**CONF ALL

QUESTION
ACTION
FINDING PERFORM DETAILED INSPECTION OF NUTS P/N ASNA2531−4 AT THRESHOLD GIVEN IN THE

PLANNING INFORMATION PARAGRAPH E.(2)

NUT MISSING

REPLACE THE NUT BEFORE NEXT FLIGHT AS DESCRIBED IN THE MODIFICATION TASK 535056−831−801−001 AND IN REPAIR DRAWINGS R51415000 AND R51415001 INFORM AIRBUS BEFORE NEXT FLIGHT NUT CRACKED NO YES YES NO

CONTACT AIRBUS BEFORE NEXT FLIGHT FOR FURTHER INSTRUCTIONS

NO FURTHER ACTION

SEND INSPECTION REPORT TO AIRBUS FILL THE TABLE OF INSPECTION REPORT IN CASE OF FINDING(S)

F_SB_535056_5_BCAA_01_02 Figure A-FBCAA - Sheet 01 Flow Chart

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 244 5

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# @A340-500/600
SERVICE BULLETIN Appendix 01 Inspection Report. **CONF ALL The results of the inspection, including no findings, replacement or action to be done, must be forwarded to Airbus department SEES1, on the attached inspection report sheet.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 1 5

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# @A340-500/600
SERVICE BULLETIN Appendix 01 Inspection Report.

**CONF ALL

INSPECTION REPORT SERVICE BULLETIN No. : A340−53−5056 A/C MSN : FLIGHT CYCLES : FLIGHT HOURS : DATE OF INSPECTION : INSPECTION METHOD : DETAILED INSPECTION

FINDING NUMBER NUT MISSING NUT CRACKED AREA NUMBER LH SIDE RH SIDE

PLEASE RECORD OTHER FINDINGS: YES NO YES NO YES NO YES NO NO MISSING NUT AND NO CRACKED NUT (IN CASE OF FINDING(S) FILL THE TABLE BELOW)

F_SB_535056_5_AAAA_01_01 Figure A-FAAAA - Sheet 01 Inspection Report

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 2 5

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# @A340-500/600
SERVICE BULLETIN Appendix 02 Elapsed Time Assumptions

**CONF 001

**ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−53−5056**

ELAPSED TIME (HOURS)

**NOTE:** THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. GET ACCESS MH ET PER

MH: ET: PER: MANHOURS ELAPSED TIME NUMBER OF PERSONS

TOTAL MANHOURS (MH) ELAPSED TIME (ET) 183.00 51.00 STEPS

80.00 20.00 4

0 INSPECTION 4.00 1.00 4

4.00 2.00 2

1.50 1.50 1

6.00 3.00 2

0.50 0.50 1

TEST 2.00 1.00 2

CLOSE UP 85.00 25.00 4 NUT REPLACEMENT IN AREA 18
NUT REPLACEMENT IN AREA 20
NUT REPLACEMENT IN AREA 21
NUT REPLACEMENT IN AREA CONCESSION 1

20 25

F_SB_535056_5_ABAA_01_00 21 22 23 24 19 1 26 50 51

Figure A-FABAA - Sheet 01 Elapsed Time Assumptions

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 1 5

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# @A340-500/600
SERVICE BULLETIN Appendix 02 Elapsed Time Assumptions

**CONF 002

**ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−53−5056**

ELAPSED TIME (HOURS)

**NOTE:** THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. GET ACCESS MH ET PER

MH: ET: PER: MANHOURS ELAPSED TIME NUMBER OF PERSONS

TOTAL MANHOURS (MH) ELAPSED TIME (ET) 261.25 68.00 STEPS

120.00 30.00 4

33 68 0 INSPECTION 4.00 1.00 4
1.00 0.50 2
0.50 0.50 1
4.00 2.00 2
4.00 2.00 2
0.50 0.50 1
1.50 1.50 1

0.75 0.50 2

TEST 2.00 1.00 2
CLOSE UP 120.00 32.00 4 NUT REPLACEMENT IN AREA 1A NUT REPLACEMENT IN AREA 1B NUT REPLACEMENT IN AREA 14 NUT REPLACEMENT IN AREA 18 NUT REPLACEMENT IN AREA 19 NUT REPLACEMENT IN AREA 20

NUT REPLACEMENT IN AREAS OF CONCESSIONS

30 29 31 32 34 35 36 37 28 27 39 38 1 2 67 66 3.00 2.00 2 NUT REPLACEMENT IN AREA 21

F_SB_535056_5_ABAB_01_00 A 1 AND 2

65 3

Figure A-FABAB - Sheet 01 Elapsed Time Assumptions

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 2 5

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# @A340-500/600
SERVICE BULLETIN Appendix 02 Elapsed Time Assumptions

**CONF 003

**ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−53−5056**

ELAPSED TIME (HOURS)

**NOTE:** THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. GET ACCESS MH ET PER

MH: ET: PER: MANHOURS ELAPSED TIME NUMBER OF PERSONS

TOTAL MANHOURS (MH) ELAPSED TIME (ET) 14.50 9.00 STEPS

5.00 3.00 2

0 INSPECTION 2.00 1.00 2

1.50 1.50 1

CLOSE UP 5.00 3.00 2 NUT REPLACEMENT IN AREA 20

1.00 1.00 1 TEST

8 7 6 5 4 3 2 1 9

F_SB_535056_5_ABAC_01_00 Figure A-FABAC - Sheet 01 Elapsed Time Assumptions

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 3 5

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# @A340-500/600
SERVICE BULLETIN Appendix 02 Elapsed Time Assumptions

**CONF 004

**ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−53−5056**

**NOTE:** THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. GET ACCESS MH ET PER

MH: ET: PER: MANHOURS ELAPSED TIME NUMBER OF PERSONS

TOTAL MANHOURS (MH) ELAPSED TIME (ET) 160.75 45.00 STEPS

70.00 20.00 4

INSPECTION 4.00 1.00 4

4.00 2.00 2

1.50 1.50 1

3.75 2.00 2

0.50 0.50 1

TEST 2.00 1.00 2

CLOSE UP 75.00 20.00 4 NUT REPLACEMENT IN AREA 18
NUT REPLACEMENT IN AREA 20
NUT REPLACEMENT IN AREA 21
NUT REPLACEMENT IN AREA CONCESSION 1

F_SB_535056_5_ABAD_01_00 ELAPSED TIME (HOURS) 21 45 0 18 17 19 20 22 23 24 25 16 4 27 26 1 2 44 43 3

Figure A-FABAD - Sheet 01 Elapsed Time Assumptions

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 4 5

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# @A340-500/600
SERVICE BULLETIN Appendix 02 Elapsed Time Assumptions

**CONF 005

**ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−53−5056**

**NOTE:** THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. GET ACCESS MH ET PER

MH: ET: PER: MANHOURS ELAPSED TIME NUMBER OF PERSONS

TOTAL MANHOURS (MH) ELAPSED TIME (ET) 184.00 56.00 STEPS

80.00 20.00 4
INSPECTION 4.00 1.00 4

0.50 0.50 1

0.50 0.50 1

2.50 1.50 2

1.50 1.50 1

7.50 5.00 2

0.50 0.50 1 NUT REPLACEMENT IN AREA 1A NUT REPLACEMENT IN AREA 1B NUT REPLACEMENT IN AREA 18 NUT REPLACEMENT IN AREA 20 NUT REPLACEMENT IN AREA 21

F_SB_535056_5_ABAE_01_00 ELAPSED TIME (HOURS) 23 56 0 20 19 21 22 24 25 26 27 18 17 29 28 1 2 55 54 3 53 TEST 2.00 1.00 2
CLOSE UP 85.00 29.50 4 NUT REPLACEMENT IN AREA CONCESSION 1

Figure A-FABAE - Sheet 01 Elapsed Time Assumptions

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 5 5

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# @A340-500/600
SERVICE BULLETIN Appendix 02 Elapsed Time Assumptions

**CONF 006

**ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−53−5056**

ELAPSED TIME (HOURS)

**NOTE:** THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. GET ACCESS MH ET PER

MH: ET: PER: MANHOURS ELAPSED TIME NUMBER OF PERSONS

TOTAL MANHOURS (MH) ELAPSED TIME (ET) 185.50 56.00 STEPS

80.00 20.00 4

23 56 0 INSPECTION 4.00 1.00 4
0.50 0.50 1
0.50 0.50 1
2.50 1.50 2
0.50 0.50 1
1.50 1.50 1
8.50 5.00 2
0.50 0.50 1 NUT REPLACEMENT IN AREA 1A NUT REPLACEMENT IN AREA 1B NUT REPLACEMENT IN AREA 18 NUT REPLACEMENT IN AREA 19 NUT REPLACEMENT IN AREA 20 NUT REPLACEMENT IN AREA 21

20 19 21 22 24 25 26 27 18 17 29 28 1 2 55 54

F_SB_535056_5_ABAF_01_00 3 53 TEST 2.00 1.00 2

CLOSE UP 85.00 29.50 4 NUT REPLACEMENT IN AREA CONCESSION 1

Figure A-FABAF - Sheet 01 Elapsed Time Assumptions

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 6 5

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# @A340-500/600
SERVICE BULLETIN Appendix 02 Elapsed Time Assumptions

**CONF 007 **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−53−5056**

ELAPSED TIME (HOURS)

**NOTE:** THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. GET ACCESS MH ET PER

MH: ET: PER: MANHOURS ELAPSED TIME NUMBER OF PERSONS

TOTAL MANHOURS (MH) ELAPSED TIME (ET) 1193.00 378.00 STEPS

520.00 190.00 4

0 INSPECTION 4.00 1.00 4 0.50 0.50 1 0.50 0.50 1 5.25 3.00 2 22.50 12.00 2

1.75 1.00 2 1.75 1.00 2 NUT REPLACEMENT IN AREA 1A NUT REPLACEMENT IN AREA 1B NUT REPLACEMENT IN AREA 2A NUT REPLACEMENT IN AREA 2B

1 208 NUT REPLACEMENT IN AREA 5 NUT REPLACEMENT IN AREA 6 9.50 5.00 2 NUT REPLACEMENT IN AREA 2C 9.00 5.00 2 NUT REPLACEMENT IN AREA 2D 6.00 4.00 2 NUT REPLACEMENT IN AREA 2E 1.00 1.00 1 NUT REPLACEMENT IN AREA 2F 1.50 1.50 1 NUT REPLACEMENT IN AREA 3 0.50 0.50 1 NUT REPLACEMENT IN AREA 4A

0.50 0.50 1 NUT REPLACEMENT IN AREA 4C 1.00 1.00 1 NUT REPLACEMENT IN AREA 4B

207 206 205 204 203 202 201 200 199 198 197 196 195 194 193 192 191 190 189 188 187 186 185 2 3 4 5

F_SB_535056_5_ABAG_01_01 Figure A-FABAG - Sheet 01 Elapsed Time Assumptions

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 7 5

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# @A340-500/600
SERVICE BULLETIN Appendix 02 Elapsed Time Assumptions

**CONF 007 **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−53−5056**

ELAPSED TIME (HOURS)

**NOTE:** THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. MH ET PER

MH: ET: PER: MANHOURS ELAPSED TIME NUMBER OF PERSONS

TOTAL MANHOURS (MH) ELAPSED TIME (ET) 1193.00 378.00 STEPS

208 12.00 8.00 2

530.00 145.00 4 NUT REPLACEMENT IN AREA 7

378 CLOSE UP
377 234 233 232 231 230 229 228 227 226 225 224 223 222 221 220 219 218 217 216 215 12.00 8.00 2 NUT REPLACEMENT IN AREA 8 1.00 1.00 1 NUT REPLACEMENT IN AREA 9 1.50 1.50 1 NUT REPLACEMENT IN AREA 10 2.00 1.00 2 NUT REPLACEMENT IN AREA 11 9.00 5.00 2 NUT REPLACEMENT IN AREA 12 8.50 5.00 2 NUT REPLACEMENT IN AREA 13 3.00 1.50 2 NUT REPLACEMENT IN AREA 14 1.00 1.00 1 NUT REPLACEMENT IN AREA 15 5.00 3.00 2 NUT REPLACEMENT IN AREA 16 5.00 3.00 2 NUT REPLACEMENT IN AREA 17 2.50 1.50 2 NUT REPLACEMENT IN AREA 18 1.50 1.50 1 NUT REPLACEMENT IN AREA 20 10.00 3.00 4 NUT REPLACEMENT IN AREA 21 1.75 1.75 1 NUT REPLACEMENT IN AREAS OF CONCESSIONS 2.00 1.00 2 TEST 1 TO 6

214 213 212 211 210 209 235 376

F_SB_535056_5_ABAG_02_01 Figure A-FABAG - Sheet 02 Elapsed Time Assumptions

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 8 5

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# @A340-500/600
SERVICE BULLETIN Appendix 02 Elapsed Time Assumptions

**CONF 008 **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−53−5056**

ELAPSED TIME (HOURS)

**NOTE:** THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. GET ACCESS MH ET PER

MH: ET: PER: MANHOURS ELAPSED TIME NUMBER OF PERSONS

TOTAL MANHOURS (MH) ELAPSED TIME (ET) 1155.75 377.00 STEPS

510.00 190.00 4

0 INSPECTION 4.00 1.00 4 0.50 0.50 1 0.50 0.50 1 5.25 3.00 2 22.50 12.00 2

1.75 1.00 2 1.75 1.00 2 NUT REPLACEMENT IN AREA 1A NUT REPLACEMENT IN AREA 1B NUT REPLACEMENT IN AREA 2A NUT REPLACEMENT IN AREA 2B

1 208 NUT REPLACEMENT IN AREA 5 NUT REPLACEMENT IN AREA 6 9.50 5.00 2 NUT REPLACEMENT IN AREA 2C 9.00 5.00 2 NUT REPLACEMENT IN AREA 2D 6.00 4.00 2 NUT REPLACEMENT IN AREA 2E 1.00 1.00 1 NUT REPLACEMENT IN AREA 2F 1.50 1.50 1 NUT REPLACEMENT IN AREA 3 0.50 0.50 1 NUT REPLACEMENT IN AREA 4A

0.50 0.50 1 NUT REPLACEMENT IN AREA 4C 1.00 1.00 1 NUT REPLACEMENT IN AREA 4B

207 206 205 204 203 202 201 200 199 198 197 196 195 194 193 192 191 190 189 188 187 186 185 2 3 4 5

F_SB_535056_5_ABAH_01_00 Figure A-FABAH - Sheet 01 Elapsed Time Assumptions

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 9 5

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

# @A340-500/600
SERVICE BULLETIN Appendix 02 Elapsed Time Assumptions

**CONF 008 **ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−53−5056**

ELAPSED TIME (HOURS)

**NOTE:** THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. MH ET PER

MH: ET: PER: MANHOURS ELAPSED TIME NUMBER OF PERSONS

TOTAL MANHOURS (MH) ELAPSED TIME (ET) 1155.75 377.00 STEPS

208 12.00 8.00 2

510.00 145.50 4 NUT REPLACEMENT IN AREA 7

377 CLOSE UP
376 234 233 232 231 230 229 228 227 226 225 224 223 222 221 220 219 218 217 216 215 12.00 8.00 2 NUT REPLACEMENT IN AREA 8 1.00 1.00 1 NUT REPLACEMENT IN AREA 9 1.50 1.50 1 NUT REPLACEMENT IN AREA 10 2.00 1.00 2 NUT REPLACEMENT IN AREA 11 9.00 5.00 2 NUT REPLACEMENT IN AREA 12 8.50 5.00 2 NUT REPLACEMENT IN AREA 13 3.00 1.50 2 NUT REPLACEMENT IN AREA 14 1.00 1.00 1 NUT REPLACEMENT IN AREA 15 5.00 3.00 2 NUT REPLACEMENT IN AREA 16 5.00 3.00 2 NUT REPLACEMENT IN AREA 17 2.50 1.50 2 NUT REPLACEMENT IN AREA 18 1.50 1.50 1 NUT REPLACEMENT IN AREA 20 3.00 1.50 2 NUT REPLACEMENT IN AREA 21 1.50 1.50 1 NUT REPLACEMENT IN AREAS OF CONCESSIONS 2.00 1.00 2 TEST 1 TO 4

214 213 212 211 210 209 375

F_SB_535056_5_ABAH_02_01 Figure A-FABAH - Sheet 02 Elapsed Time Assumptions

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 10 5

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

# @A340-500/600
SERVICE BULLETIN Appendix 02 Elapsed Time Assumptions

**CONF 009

**ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A340−53−5056**

**NOTE:** THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. GET ACCESS MH ET PER

MH: ET: PER: MANHOURS ELAPSED TIME NUMBER OF PERSONS

TOTAL MANHOURS (MH) ELAPSED TIME (ET) 177.75 46.00 STEPS

80.00 20.00 4

INSPECTION 4.00 1.00 4

1.25 1.00 2

1.00 1.00 1

TEST 2.00 1.00 2

CLOSE UP 90.00 23.00 4 NUT REPLACEMENT IN AREA 10

NUT REPLACEMENT IN AREA 11

1.50 1.00 2 NUT REPLACEMENT IN AREA CONCESSION 1

F_SB_535056_5_ABAI_01_00 ELAPSED TIME (HOURS) 21 46 0 18 17 19 20 22 23 24 25 16 4 26 1 2 45 44 43 3

Figure A-FABAI - Sheet 01 Elapsed Time Assumptions

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 11 5

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# @A340-500/600
SERVICE BULLETIN REPORTING SHEET 

### TITLE: FUSELAGE - GENERAL - INSPECTION OF SUSPECTED NON CONFORMING NUTS ASNA2531-4 MODIFICATION No.: None Please complete the appropriate item (A or B): A - SB WILL BEembodied 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 BEENembodied 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: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 1 5

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# @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 4 3 2 1 - Quality rating of the Accomplishment Instructions 4 3 2 1 - Quality rating of the Illustrations 4 3 2 1 - 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: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056 REVISION No.: 00 - Oct 07/10 Page: 1 5

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