@A340-500/600

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is not approved for modification of the aircraft.

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 53

TITLE: FUSELAGE - 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

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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

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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

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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

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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

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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

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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

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

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SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 53

TITLE: FUSELAGE - 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

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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.

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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

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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

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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

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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

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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 and

analysis 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

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**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

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(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

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(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

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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

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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

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 12

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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 under EASA Design Organisation Approval No. EASA 21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied that is not of

AIRBUS origin, and which affects the content of this Service Bulletin, the operator is

responsible for obtaining approval by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

G. MANPOWER

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

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

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

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

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

included.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 13

5

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

SERVICE BULLETIN

**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

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 14

5

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@A340-500/600

SERVICE BULLETIN

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

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 15

5

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

SERVICE BULLETIN

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

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 16

5

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

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

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

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

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

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

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

SERVICE BULLETIN

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

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 20

5

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

SERVICE BULLETIN

**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

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 21

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@A340-500/600

SERVICE BULLETIN

**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

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 22

5

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@A340-500/600

SERVICE BULLETIN

**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

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 23

5

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

SERVICE BULLETIN

**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

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

SERVICE BULLETIN

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 25

5

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

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 26

5

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

SERVICE BULLETIN

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>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 27

5

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

SERVICE BULLETIN

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>

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 28

5

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

SERVICE BULLETIN

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

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

SERVICE BULLETIN

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

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

SERVICE BULLETIN

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 INFORMATION

AIRBUS 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

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

SERVICE BULLETIN

(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

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

SERVICE BULLETIN

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

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

SERVICE BULLETIN

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

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

SERVICE BULLETIN

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

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

SERVICE BULLETIN

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

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SERVICE BULLETIN

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

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SERVICE BULLETIN

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

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 56

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SERVICE BULLETIN

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

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SERVICE BULLETIN

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

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SERVICE BULLETIN

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

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SERVICE BULLETIN

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

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SERVICE BULLETIN

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

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 61

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SERVICE BULLETIN

**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

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SERVICE BULLETIN

**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)

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 63

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SERVICE BULLETIN

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

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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

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SERVICE BULLETIN

References

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

06-30-00, Page Block 001

06-31-53, Page Block 001

06-40-00, 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

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SERVICE BULLETIN

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

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SERVICE BULLETIN

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

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SERVICE BULLETIN

(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

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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

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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

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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

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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

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SERVICE BULLETIN

**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

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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

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SERVICE BULLETIN

**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

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SERVICE BULLETIN

(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

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SERVICE BULLETIN

**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

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SERVICE BULLETIN

(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

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SERVICE BULLETIN

**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

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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

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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).

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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).

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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

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

SERVICE BULLETIN

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

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

SERVICE BULLETIN

(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

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

SERVICE BULLETIN

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

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

SERVICE BULLETIN

**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

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

SERVICE BULLETIN

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

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

SERVICE BULLETIN

(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

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

SERVICE BULLETIN

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

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

SERVICE BULLETIN

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

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

SERVICE BULLETIN

(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

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

SERVICE BULLETIN

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

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

SERVICE BULLETIN

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

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

SERVICE BULLETIN

(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

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

SERVICE BULLETIN

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

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SERVICE BULLETIN

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

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SERVICE BULLETIN

(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

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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).

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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

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SERVICE BULLETIN

**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

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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

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SERVICE BULLETIN

(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)

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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

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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

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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

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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 in Fig. 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.

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(2) Subtask 535056-960-028-001 - Area 18, replace nuts from rear section FR54

stringer 54 LH side

Work 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

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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

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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 in Fig. 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

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

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

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

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

Work 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

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

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

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

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

Work 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

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

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

Work 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

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

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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

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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 side

Work 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

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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

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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

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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

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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 in Fig. 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

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: 139

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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

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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

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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

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

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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

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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

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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

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@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

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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

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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

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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

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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

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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

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@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

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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

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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

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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 side

Work 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

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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

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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

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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

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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

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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

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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 in Fig. 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

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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

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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

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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

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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

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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

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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

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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

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@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

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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

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(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

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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

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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

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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

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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

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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

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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

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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

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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

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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

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(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

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(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 side

Work 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

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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

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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

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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

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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

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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

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SERVICE BULLETIN

(a) Perform a visual inspection of the nuts looking for cracked or missing nuts as

described in Fig. 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

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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

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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

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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

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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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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

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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

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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

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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: 201

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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

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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

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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

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SERVICE BULLETIN

(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

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 205

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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: 206

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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 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

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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: 208

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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

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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 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

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 210

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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 535056-700-001-002 - Tests

Manpower Resources

Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 211

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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 25-37-41-400-801

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

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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

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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 535056-700-001-002 - Tests

Manpower Resources

Skills AIRFRAME

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 214

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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 25-37-41-400-801

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

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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 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

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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

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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 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

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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

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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

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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

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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

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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

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

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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

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

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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

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

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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

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

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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 in Fig. 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 in Fig. 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

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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

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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

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

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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 in Fig. 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 in Fig. 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

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(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

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(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

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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

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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

STGR42LH

STGR41LH

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

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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

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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

6 POS (1) 1

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

6 POS (3) 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

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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

NO NUT CRACKED YES

NO YES

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

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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

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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

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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

1 19 21 22 23 24 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

0 33 68

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

1 2 27 28 29 30 31 32 34 35 36 37 38 39 66 67

NUT REPLACEMENT IN 3.00 2.00 2

AREA 21

F_SB_535056_5_ABAB_01_00

A

1 AND 2

3 65

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

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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

TEST 1.00 1.00 1

1 9 2 3 4 5 6 7 8

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

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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)

0 1 2 3 4 16 17 18 19 20 21 22 23 24 25 26 27 43 44 45

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

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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)

0 1 2 3 17 18 19 20 21 22 23 24 25 26 27 28 29 53 54 55 56

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

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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

0 23 56

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

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

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

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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

NUT REPLACEMENT IN 9.50 5.00 2

AREA 2C

NUT REPLACEMENT IN 9.00 5.00 2

AREA 2D

NUT REPLACEMENT IN 6.00 4.00 2

AREA 2E

NUT REPLACEMENT IN 1.00 1.00 1

AREA 2F

NUT REPLACEMENT IN 1.50 1.50 1

AREA 3

NUT REPLACEMENT IN 0.50 0.50 1

AREA 4A

NUT REPLACEMENT IN 0.50 0.50 1

AREA 4C

NUT REPLACEMENT IN 1.00 1.00 1

AREA 4B

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

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

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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

215 216 217 218 219 220 221 222 223 224 225 226 227 228 229 230 231 232 233 234 377

NUT REPLACEMENT IN 12.00 8.00 2

AREA 8

NUT REPLACEMENT IN 1.00 1.00 1

AREA 9

NUT REPLACEMENT IN 1.50 1.50 1

AREA 10

NUT REPLACEMENT IN 2.00 1.00 2

AREA 11

NUT REPLACEMENT IN 9.00 5.00 2

AREA 12

NUT REPLACEMENT IN 8.50 5.00 2

AREA 13

NUT REPLACEMENT IN 3.00 1.50 2

AREA 14

NUT REPLACEMENT IN 1.00 1.00 1

AREA 15

NUT REPLACEMENT IN 5.00 3.00 2

AREA 16

NUT REPLACEMENT IN 5.00 3.00 2

AREA 17

NUT REPLACEMENT IN 2.50 1.50 2

AREA 18

NUT REPLACEMENT IN 1.50 1.50 1

AREA 20

NUT REPLACEMENT IN 10.00 3.00 4

AREA 21

1.75 1.75 1

NUT REPLACEMENT IN

AREAS OF CONCESSIONS

TEST 2.00 1.00 2

1 TO 6

209 210 211 212 213 214 235 376

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

NUT REPLACEMENT IN 9.50 5.00 2

AREA 2C

NUT REPLACEMENT IN 9.00 5.00 2

AREA 2D

NUT REPLACEMENT IN 6.00 4.00 2

AREA 2E

NUT REPLACEMENT IN 1.00 1.00 1

AREA 2F

NUT REPLACEMENT IN 1.50 1.50 1

AREA 3

NUT REPLACEMENT IN 0.50 0.50 1

AREA 4A

NUT REPLACEMENT IN 0.50 0.50 1

AREA 4C

NUT REPLACEMENT IN 1.00 1.00 1

AREA 4B

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

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

215 216 217 218 219 220 221 222 223 224 225 226 227 228 229 230 231 232 233 234 376

NUT REPLACEMENT IN 12.00 8.00 2

AREA 8

NUT REPLACEMENT IN 1.00 1.00 1

AREA 9

NUT REPLACEMENT IN 1.50 1.50 1

AREA 10

NUT REPLACEMENT IN 2.00 1.00 2

AREA 11

NUT REPLACEMENT IN 9.00 5.00 2

AREA 12

NUT REPLACEMENT IN 8.50 5.00 2

AREA 13

NUT REPLACEMENT IN 3.00 1.50 2

AREA 14

NUT REPLACEMENT IN 1.00 1.00 1

AREA 15

NUT REPLACEMENT IN 5.00 3.00 2

AREA 16

NUT REPLACEMENT IN 5.00 3.00 2

AREA 17

NUT REPLACEMENT IN 2.50 1.50 2

AREA 18

NUT REPLACEMENT IN 1.50 1.50 1

AREA 20

NUT REPLACEMENT IN 3.00 1.50 2

AREA 21

1.50 1.50 1

NUT REPLACEMENT IN

AREAS OF CONCESSIONS

TEST 2.00 1.00 2

1 TO 4

209 210 211 212 213 214 375

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

NUT REPLACEMENT IN 1.50 1.00 2

AREA CONCESSION 1

F_SB_535056_5_ABAI_01_00

ELAPSED TIME

(HOURS)

0 1 2 3 4 16 17 18 19 20 21 22 23 24 25 26 43 44 45 46

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

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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 BE embodied YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to

next normal revision or prior to SB embodiment, please indicate required service(s):

Either: Modification Operational Impact (MOI), if available YES/NO

Or : Intermediate revision YES/NO

Important Information: This SB will only be incorporated in your maintenance and operational

documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With

the next feasible revision, this will result in

- Updating of maintenance documentation to show pre and post SB data.

- Updating of maintenance and operational documentation to show post SB data after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically

include them in the manual revisions. Refer to SIL 00-037 for detailed information.

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.

DATE: Oct 07/10 SERVICE BULLETIN No.: A340-53-5056

REVISION No.: 00 - Oct 07/10 Page: 1

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 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

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