@A330

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 test have been performed, results from

tests and analysis indicated that no immediate maintenance action is required on the affected in-service

aircraft. Howewer, as this event impacts a large amount of nuts associated to the primary structure

assembly, Airbus request 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.

It is suggested to accomplish this Service Bulletin during a major servicing because of the timeconsuming 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 ETOPS AFFECTED NO

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 1

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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 COMPA01 1 See SB Nuts

Component COMPA03 1 See SB Nuts

Component COMPA04 1 See SB Nuts

Component COMPA05 1 See SB Nuts

Component COMPA06 1 See SB Nuts

Component COMPA07 1 See SB Nuts

Component COMPA14 1 See SB Nuts

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA18 1 See SB Nuts

Component COMPA22 1 See SB Nuts

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 1 See SB Nuts

Component COMPA03 1 See SB Nuts

Component COMPA04 1 See SB Nuts

Component COMPA05 1 See SB Nuts

Component COMPA06 1 See SB Nuts

Component COMPA14 1 See SB Nuts

Component COMPA17 1 See SB Nuts

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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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 COMPA01 1 See SB Nuts

Component COMPA03 1 See SB Nuts

Component COMPA04 1 See SB Nuts

Component COMPA05 1 See SB Nuts

Component COMPA06 1 See SB Nuts

Component COMPA07 1 See SB Nuts

Component COMPA14 1 See SB Nuts

**CONF 005

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 1 See SB Nuts

Component COMPA06 1 See SB Nuts

Component COMPA07 1 See SB Nuts

Component COMPA14 1 See SB Nuts

**CONF 006

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 1 See SB Nuts

Component COMPA06 1 See SB Nuts

Component COMPA14 1 See SB Nuts

**CONF 007

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA06 1 See SB Nuts

Component COMPA14 1 See SB Nuts

**CONF 008

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA06 1 See SB Nuts

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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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 COMPA14 1 See SB Nuts

**CONF 009

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA06 1 See SB Nuts

Component COMPA14 1 See SB Nuts

**CONF 010

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA06 1 See SB Nuts

Component COMPA14 1 See SB Nuts

**CONF 011

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA06 1 See SB Nuts

Component COMPA08 1 See SB Nuts

Component COMPA14 1 See SB Nuts

**CONF 012

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA06 1 See SB Nuts

Component COMPA09 1 See SB Nuts

Component COMPA14 1 See SB Nuts

**CONF 013

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA07 1 See SB Nuts

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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SERVICE BULLETIN

SUMMARY

**CONF 014

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA10 1 See SB Nuts

**CONF 015

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA11 1 See SB Nuts

**CONF 017

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 1 See SB Nuts

Component COMPA03 1 See SB Nuts

Component COMPA04 1 See SB Nuts

Component COMPA05 1 See SB Nuts

Component COMPA06 1 See SB Nuts

Component COMPA14 1 See SB Nuts

Component COMPA20 1 See SB Nuts

**CONF 018

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 1 See SB Nuts

Component COMPA03 1 See SB Nuts

Component COMPA04 1 See SB Nuts

Component COMPA05 1 See SB Nuts

Component COMPA06 1 See SB Nuts

Component COMPA13 1 See SB Nuts

Component COMPA14 1 See SB Nuts

**CONF 019

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 1 See SB Nuts

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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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 COMPA03 1 See SB Nuts

Component COMPA04 1 See SB Nuts

Component COMPA05 1 See SB Nuts

Component COMPA06 1 See SB Nuts

Component COMPA14 1 See SB Nuts

**CONF 020

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 1 See SB Nuts

Component COMPA03 1 See SB Nuts

Component COMPA04 1 See SB Nuts

Component COMPA05 1 See SB Nuts

Component COMPA06 1 See SB Nuts

Component COMPA08 1 See SB Nuts

Component COMPA14 1 See SB Nuts

**CONF 021

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA07 1 See SB Nuts

**CONF 022

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA06 1 See SB Nuts

Component COMPA14 1 See SB Nuts

**CONF 023

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA06 1 See SB Nuts

Component COMPA07 1 See SB Nuts

Component COMPA14 1 See SB Nuts

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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SERVICE BULLETIN

SUMMARY

**CONF 024

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA06 1 See SB Nuts

Component COMPA14 1 See SB Nuts

Component COMPA15 1 See SB Nuts

**CONF 025

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA06 1 See SB Nuts

Component COMPA07 1 See SB Nuts

Component COMPA14 1 See SB Nuts

**CONF 026

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 1 See SB Nuts

Component COMPA06 1 See SB Nuts

Component COMPA14 1 See SB Nuts

**CONF 027

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 1 See SB Nuts

Component COMPA06 1 See SB Nuts

Component COMPA14 1 See SB Nuts

Component COMPA16 1 See SB Nuts

**CONF 028

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 1 See SB Nuts

Component COMPA06 1 See SB Nuts

Component COMPA14 1 See SB Nuts

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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SERVICE BULLETIN

SUMMARY

**CONF 029

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 1 See SB Nuts

Component COMPA02 1 See SB Nuts

Component COMPA03 1 See SB Nuts

Component COMPA04 1 See SB Nuts

Component COMPA05 1 See SB Nuts

Component COMPA06 1 See SB Nuts

Component COMPA07 1 See SB Nuts

Component COMPA14 1 See SB Nuts

**CONF 030

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA21 1 See SB Nuts

Component COMPA24 1 See SB Nuts

**CONF 031

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA21 1 See SB Nuts

Component COMPA25 1 See SB Nuts

Component COMPA26 1 See SB Nuts

**CONF 032

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 1 See SB Nuts

Component COMPA03 1 See SB Nuts

Component COMPA04 1 See SB Nuts

Component COMPA05 1 See SB Nuts

Component COMPA06 1 See SB Nuts

Component COMPA12 1 See SB Nuts

Component COMPA14 1 See SB Nuts

Component COMPA19 1 See SB Nuts

Component COMPA23 1 See SB Nuts

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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SERVICE BULLETIN

SUMMARY

EFFECTIVITY

**CONF ALL

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

99Y AEA CAL CCA CES CHH CPA CSN DLH JAI KFR KLM LTU

MEA QFA QTR TAP

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 NO

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 307.50

ELAPSED TIME (HOURS) 103.0

**CONF 002

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 45.75

ELAPSED TIME (HOURS) 30.50

**CONF 003

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 331.00

ELAPSED TIME (HOURS) 113.0

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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SERVICE BULLETIN

SUMMARY

**CONF 004

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 307.50

ELAPSED TIME (HOURS) 103.0

**CONF 005

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 42.50

ELAPSED TIME (HOURS) 26.00

**CONF 006

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 41.00

ELAPSED TIME (HOURS) 25.00

**CONF 007

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 35.75

ELAPSED TIME (HOURS) 23.00

**CONF 008

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 35.75

ELAPSED TIME (HOURS) 23.00

**CONF 009

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 35.75

ELAPSED TIME (HOURS) 23.00

**CONF 010

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 35.75

ELAPSED TIME (HOURS) 25.00

**CONF 011

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 20.00

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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SERVICE BULLETIN

SUMMARY

**CONF 012

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 20.00

**CONF 014

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 13.00

ELAPSED TIME (HOURS) 13.00

**CONF 015

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 13.00

**CONF 013

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 13.00

ELAPSED TIME (HOURS) 13.00

**CONF 017

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 307.50

ELAPSED TIME (HOURS) 113.0

**CONF 018

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 309.00

ELAPSED TIME (HOURS) 103.0

**CONF 019

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 131.00

ELAPSED TIME (HOURS) 44.00

**CONF 020

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 307.50

ELAPSED TIME (HOURS) 103.0

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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SERVICE BULLETIN

SUMMARY

**CONF 021

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 13.00

ELAPSED TIME (HOURS) 13.00

**CONF 022

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 35.75

ELAPSED TIME (HOURS) 23.00

**CONF 023

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 20.00

**CONF 024

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 36.50

ELAPSED TIME (HOURS) 23.00

**CONF 025

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 20.00

**CONF 026

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 41.00

ELAPSED TIME (HOURS) 25.00

**CONF 027

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 43.50

ELAPSED TIME (HOURS) 26.00

**CONF 028

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 41.00

ELAPSED TIME (HOURS) 25.50

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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SERVICE BULLETIN

SUMMARY

**CONF 029

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 316.00

ELAPSED TIME (HOURS) 103.0

**CONF 030

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 35.00

ELAPSED TIME (HOURS) 21.00

**CONF 031

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 55.50

ELAPSED TIME (HOURS) 35.00

**CONF 032

Task 533183-832-801-001: Inspection

TOTAL MANHOURS 396.00

ELAPSED TIME (HOURS) 133.0

APPENDICES

**CONF ALL

Appendix 01 Inspection Report

Appendix 02 Elapsed Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 14

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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 validated on A340-600 aircraft MSN 0924.

(1) Models

330-202 330-203 330-223 330-243 330-302 330-342 330-343

(2) Effectivity by MSN

0895 0898-0900 0903-0909 0911 0913-0916 0918-0920 0922-0923 0926-0927

0930-0932 0934-0936 0940 0951

(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

99Y 0951

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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SERVICE BULLETIN

OPERATOR MSN

AEA 0931

CAL 0920

CCA 0903 0909 0930

CES 0916 0936

CHH 0906 0919

CPA 0895 0915

CSN 0908 0935

DLH 0905 0913 0922

JAI 0923 0932

KFR 0927

KLM 0900

LTU 0911

MEA 0926

QFA 0898 0940

QTR 0907 0918

TAP 0899 0904 0914 0934

(4) Configuration by MSN

MSN CONFIGURATION

0895 021

0898 015

0899 014

0900 013

0903 012

0904 011

0905 022

0906 010

0907 023

0908 024

0909 009

0911 008

0913 025

0914 007

0915 026

0916 006

0918 027

0919 005

0920 028

0922 029

0923 004

0926 003

0927 002

0930 001

0931 032

0932 017

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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SERVICE BULLETIN

MSN CONFIGURATION

0934 018

0935 030

0936 031

0940 019

0951 020

(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.

**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.

**CONF 010

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 011

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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SERVICE BULLETIN

**CONF 012

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 014

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 015

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 013

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 017

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 018

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 019

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 020

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 021

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 022

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 023

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 024

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 025

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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@A330

SERVICE BULLETIN

**CONF 026

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 027

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 028

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 029

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 030

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 031

The definition of this configuration corresponds to the necessary areas to inspect. These

areas result from the investigation performed by Airbus.

**CONF 032

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, 004

MATERIAL QTY PER A/C SEE NOTES

Component COMPA01 1

Component COMPA03 1

Component COMPA04 1

Component COMPA05 1

Component COMPA06 1

Component COMPA07 1

Component COMPA14 1

Consumable CMLA01 1

**CONF 002

MATERIAL QTY PER A/C SEE NOTES

Component COMPA18 1

Component COMPA22 1

Consumable CMLA01 1

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**CONF 003

MATERIAL QTY PER A/C SEE NOTES

Component COMPA01 1

Component COMPA03 1

Component COMPA04 1

Component COMPA05 1

Component COMPA06 1

Component COMPA14 1

Component COMPA17 1

Consumable CMLA01 1

**CONF 005

MATERIAL QTY PER A/C SEE NOTES

Component COMPA01 1

Component COMPA06 1

Component COMPA07 1

Component COMPA14 1

Consumable CMLA01 1

**CONF 006, 026, 028

MATERIAL QTY PER A/C SEE NOTES

Component COMPA01 1

Component COMPA06 1

Component COMPA14 1

Consumable CMLA01 1

**CONF 007 thru 010, 022

MATERIAL QTY PER A/C SEE NOTES

Component COMPA06 1

Component COMPA14 1

Consumable CMLA01 1

**CONF 011

MATERIAL QTY PER A/C SEE NOTES

Component COMPA06 1

Component COMPA08 1

Component COMPA14 1

Consumable CMLA01 1

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**CONF 012

MATERIAL QTY PER A/C SEE NOTES

Component COMPA06 1

Component COMPA09 1

Component COMPA14 1

Consumable CMLA01 1

**CONF 013, 021

MATERIAL QTY PER A/C SEE NOTES

Component COMPA07 1

Consumable CMLA01 1

**CONF 014

MATERIAL QTY PER A/C SEE NOTES

Component COMPA10 1

Consumable CMLA01 1

**CONF 015

MATERIAL QTY PER A/C SEE NOTES

Component COMPA11 1

Consumable CMLA01 1

**CONF 017

MATERIAL QTY PER A/C SEE NOTES

Component COMPA01 1

Component COMPA03 1

Component COMPA04 1

Component COMPA05 1

Component COMPA06 1

Component COMPA14 1

Component COMPA20 1

Consumable CMLA01 1

**CONF 018

MATERIAL QTY PER A/C SEE NOTES

Component COMPA01 1

Component COMPA03 1

Component COMPA04 1

Component COMPA05 1

Component COMPA06 1

Component COMPA13 1

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MATERIAL QTY PER A/C SEE NOTES

Component COMPA14 1

Consumable CMLA01 1

**CONF 019

MATERIAL QTY PER A/C SEE NOTES

Component COMPA01 1

Component COMPA03 1

Component COMPA04 1

Component COMPA05 1

Component COMPA06 1

Component COMPA14 1

Consumable CMLA01 1

**CONF 020

MATERIAL QTY PER A/C SEE NOTES

Component COMPA01 1

Component COMPA03 1

Component COMPA04 1

Component COMPA05 1

Component COMPA06 1

Component COMPA08 1

Component COMPA14 1

Consumable CMLA01 1

**CONF 023, 025

MATERIAL QTY PER A/C SEE NOTES

Component COMPA06 1

Component COMPA07 1

Component COMPA14 1

Consumable CMLA01 1

**CONF 024

MATERIAL QTY PER A/C SEE NOTES

Component COMPA06 1

Component COMPA14 1

Component COMPA15 1

Consumable CMLA01 1

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**CONF 027

MATERIAL QTY PER A/C SEE NOTES

Component COMPA01 1

Component COMPA06 1

Component COMPA14 1

Component COMPA16 1

Consumable CMLA01 1

**CONF 029

MATERIAL QTY PER A/C SEE NOTES

Component COMPA01 1

Component COMPA02 1

Component COMPA03 1

Component COMPA04 1

Component COMPA05 1

Component COMPA06 1

Component COMPA07 1

Component COMPA14 1

Consumable CMLA01 1

**CONF 030

MATERIAL QTY PER A/C SEE NOTES

Component COMPA21 1

Component COMPA24 1

Consumable CMLA01 1

**CONF 031

MATERIAL QTY PER A/C SEE NOTES

Component COMPA21 1

Component COMPA25 1

Component COMPA26 1

Consumable CMLA01 1

**CONF 032

MATERIAL QTY PER A/C SEE NOTES

Component COMPA01 1

Component COMPA03 1

Component COMPA04 1

Component COMPA05 1

Component COMPA06 1

Component COMPA12 1

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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MATERIAL QTY PER A/C SEE NOTES

Component COMPA14 1

Component COMPA19 1

Component COMPA23 1

Consumable CMLA01 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

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 test have been performed, results from tests and

analysis indicated that no immediate maintenance action is required on the affected inservice aircraft. Howewer, as this event impacts a large amount of nuts associated to the

primary structure assembly, Airbus request 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.

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 :

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**CONF 001

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 1a, replace the nuts in FWD LH and RH hard points

(3) Area 2a, replace the nuts of LH and RH keel lower angle fittings

(4) Area 2b, replace nuts of LH and RH flight control fittings

(5) Area 2c, replace the nuts in center wing rear spar inboard of rib 1, RH and LH

(6) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(7) Area C7, replace the nuts in outer wing center spar between ribs 1 and 2

(8) Area 20, replace the nuts in fixed inner shroud box

**CONF 002

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area C4 concession 1

(3) Area C5 concession 2

**CONF 003

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 1a, replace the nuts in FWD LH and RH hard points

(3) Area 2a, replace the nuts of LH and RH keel lower angle fittings

(4) Area 2b, replace nuts of LH and RH flight control fittings

(5) Area 2c, replace the nuts in center wing rear spar inboard of rib 1, RH and LH

(6) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(7) Area 20, replace the nuts in fixed inner shroud box

(8) Area C3 concession 1

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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**CONF 004

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 1a, replace the nuts in FWD LH and RH hard points

(3) Area 2a, replace the nuts of LH and RH keel lower angle fittings

(4) Area 2b, replace nuts of LH and RH flight control fittings

(5) Area 2c, replace the nuts in center wing rear spar inboard of rib 1, RH and LH

(6) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(7) Area C7, replace the nuts in outer wing center spar between ribs 1 and 2

(8) Area 20, replace the nuts in fixed inner shroud box

**CONF 005

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 1a, replace the nuts in FWD LH and RH hard points

(3) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(4) Area C7, replace the nuts in outer wing center spar between ribs 1 and 2

(5) Area 20, replace the nuts in fixed inner shroud box

**CONF 006

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 1a, replace the nuts in FWD LH and RH hard points

(3) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(4) Area 20, replace the nuts in fixed inner shroud box

**CONF 007

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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(3) Area 20, replace the nuts in fixed inner shroud box

**CONF 008

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(3) Area 20, replace the nuts in fixed inner shroud box

**CONF 009

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(3) Area 20, replace the nuts in fixed inner shroud box

**CONF 010

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(3) Area 20, replace the nuts in fixed inner shroud box

**CONF 011

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(3) Area C7, replace the nuts in outer wing center spar between ribs 1 and 2

(4) Area 20, replace the nuts in fixed inner shroud box

**CONF 012

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(3) Area C7, replace the nuts in outer wing center spar between ribs 1 and 2

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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(4) Area 20, replace the nuts in fixed inner shroud box

**CONF 013

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area C7, replace the nuts in outer wing center spar between ribs 1 and 2

**CONF 014

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area C7, replace the nuts in outer wing center spar between ribs 1 and 2

**CONF 015

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area C7, replace the nuts in outer wing center spar between ribs 1 and 2

**CONF 017

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 1a, replace the nuts in FWD LH and RH hard points

(3) Area 2a, replace the nuts of LH and RH keel lower angle fittings

(4) Area 2b, replace nuts of LH and RH flight control fittings

(5) Area 2c, replace the nuts in center wing rear spar inboard of rib 1, RH and LH

(6) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(7) Area 20, replace the nuts in fixed inner shroud box

(8) Area C4 concession 1

**CONF 018

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 1a, replace the nuts in FWD LH and RH hard points

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(3) Area 2a, replace the nuts of LH and RH keel lower angle fittings

(4) Area 2b, replace nuts of LH and RH flight control fittings

(5) Area 2c, replace the nuts in center wing rear spar inboard of rib 1, RH and LH

(6) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(7) Area C7, replace the nuts in outer wing center spar between ribs 1 and 2

(8) Area 20, replace the nuts in fixed inner shroud box

**CONF 019

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 1a, replace the nuts in FWD LH and RH hard points

(3) Area 2a, replace the nuts of LH and RH keel lower angle fittings

(4) Area 2b, replace nuts of LH and RH flight control fittings

(5) Area 2c, replace the nuts in center wing rear spar inboard of rib 1, RH and LH

(6) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(7) Area 20, replace the nuts in fixed inner shroud box

**CONF 020

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 1a, replace the nuts in FWD LH and RH hard points

(3) Area 2a, replace the nuts of LH and RH keel lower angle fittings

(4) Area 2b, replace nuts of LH and RH flight control fittings

(5) Area 2c, replace the nuts in center wing rear spar inboard of rib 1, RH and LH

(6) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(7) Area C7, replace the nuts in outer wing center spar between ribs 1 and 2

(8) Area 20, replace the nuts in fixed inner shroud box

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 15

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**CONF 021

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area C7, replace the nuts in outer wing center spar between ribs 1 and 2

**CONF 022

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(3) Area 20, replace the nuts in fixed inner shroud box

**CONF 023

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(3) Area C7, replace the nuts in outer wing center spar between ribs 1 and 2

(4) Area 20, replace the nuts in fixed inner shroud box

**CONF 024

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(3) Area 20, replace the nuts in fixed inner shroud box

(4) Area C1 concession 1, replace the nuts

**CONF 025

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(3) Area C7, replace the nuts in outer wing center spar between ribs 1 and 2

(4) Area 20, replace the nuts in fixed inner shroud box

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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**CONF 026

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 1a, replace the nuts in FWD LH and RH hard points

(3) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(4) Area 20, replace the nuts in fixed inner shroud box

**CONF 027

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 1a, replace the nuts in FWD LH and RH hard points

(3) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(4) Area 20, replace the nuts in fixed inner shroud box

(5) Area C2 concession 1

**CONF 028

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 1a, replace the nuts in FWD LH and RH hard points

(3) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(4) Area 20, replace the nuts in fixed inner shroud box

**CONF 029

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 1a, replace the nuts in FWD LH and RH hard points

(3) Area 1b, replace the nuts of 800VU FR18 LH support

(4) Area 2a, replace the nuts of LH and RH keel lower angle fittings

(5) Area 2b, replace nuts of LH and RH flight control fittings

(6) Area 2c, replace the nuts in center wing rear spar inboard of rib 1, RH and LH

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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(7) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(8) Area C7, replace the nuts in outer wing center spar between ribs 1 and 2

(9) Area 20, replace the nuts in fixed inner shroud box

**CONF 030

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area C4 concession 1

(3) Area C5 concession 1

**CONF 031

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area C4 concession 2

(3) Area C5 concession 3

(4) Area C6 concession 1

**CONF 032

Task 533183-832-801-001: Inspection

(1) Inspection / Repair

(2) Area 1a, replace the nuts in FWD LH and RH hard points

(3) Area 2a, replace the nuts of LH and RH keel lower angle fittings

(4) Area 2b, replace nuts of LH and RH flight control fittings

(5) Area 2c, replace the nuts in center wing rear spar inboard of rib 1, RH and LH

(6) Area 3, replace the nuts in outer wing front/rear spars just outboard of rib 1

(7) Area C7, replace the nuts in outer wing center spar between ribs 1 and 2

(8) Area 20, replace the nuts in fixed inner shroud box

(9) Area C4 concession 1

(10) Area C5 concession 2

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**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

**CONF 001 thru 015, 017 thru 020, 029, 032

CONDITION ACTION COMPLIANCE TIME

WHICHEVER OCCURS

REPETITIVE

INTERVAL

All areas except areas

2c, 3 and C7

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

Instruction R51415002

Before next flight No further

action

No findings Replace the nut P/N

ASNA2531-4 as per given

Repair Instruction R51415002

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 2c, 3 and C7 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

Instruction R51415002

Before next flight No further

action

No findings Replace the nut P/N

ASNA2531-4 as per given

Repair Instruction R51415002

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 Instruction R51415002.

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**CONF 021 thru 028, 030 thru 031

CONDITION ACTION COMPLIANCE TIME

WHICHEVER OCCURS

REPETITIVE

INTERVAL

All areas except areas 3

and C7

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

Instruction R51415002

Before next flight No further

action

No findings Replace the nut P/N

ASNA2531-4 as per given

Repair Instruction R51415002

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 3 and C7 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

Instruction R51415002

Before next flight No further

action

No findings Replace the nut P/N

ASNA2531-4 as per given

Repair Instruction R51415002

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 Instruction R51415002.

**CONF ALL

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.

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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.

**CONF 001

Task 533183-832-801-001: Inspection

Get Access 136.0

On Aircraft

Inspection / Repair 4.00

Area 1a, replace the nuts in FWD LH and RH hard

points

0.50

Area 2a, replace the nuts of LH and RH keel lower

angle fittings

6.00

Area 2b, replace nuts of LH and RH flight control

fittings

2.50

Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

1.50

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

0.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 4.00

Close-Up 150.0

TOTAL MANHOURS 307.50

ELAPSED TIME (HOURS) 103.0

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 002

Task 533183-832-801-001: Inspection

Get Access 19.25

On Aircraft

Inspection / Repair 1.00

Area C4 concession 1 1.00

Area C5 concession 2 0.50

Tests 1.00

Close-Up 23.00

TOTAL MANHOURS 45.75

ELAPSED TIME (HOURS) 30.50

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NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 003

Task 533183-832-801-001: Inspection

Get Access 147.5

On Aircraft

Inspection / Repair 4.00

Area 1a, replace the nuts in FWD LH and RH hard

points

0.50

Area 2a, replace the nuts of LH and RH keel lower

angle fittings

6.00

Area 2b, replace nuts of LH and RH flight control

fittings

2.50

Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

1.50

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Area C3 concession 1 0.50

Tests 4.00

Close-Up 162.0

TOTAL MANHOURS 331.00

ELAPSED TIME (HOURS) 113.0

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 004

Task 533183-832-801-001: Inspection

Get Access 136.0

On Aircraft

Inspection / Repair 4.00

Area 1a, replace the nuts in FWD LH and RH hard

points

0.50

Area 2a, replace the nuts of LH and RH keel lower

angle fittings

6.00

Area 2b, replace nuts of LH and RH flight control

fittings

2.50

Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

1.50

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

0.50

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 22

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Task 533183-832-801-001: Inspection

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 4.00

Close-Up 150.0

TOTAL MANHOURS 307.50

ELAPSED TIME (HOURS) 103.0

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 005

Task 533183-832-801-001: Inspection

Get Access 16.50

On Aircraft

Inspection / Repair 2.00

Area 1a, replace the nuts in FWD LH and RH hard

points

0.50

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

0.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 1.00

Close-Up 19.50

TOTAL MANHOURS 42.50

ELAPSED TIME (HOURS) 26.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 006

Task 533183-832-801-001: Inspection

Get Access 16.50

On Aircraft

Inspection / Repair 1.00

Area 1a, replace the nuts in FWD LH and RH hard

points

0.50

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 1.00

Close-Up 19.50

TOTAL MANHOURS 41.00

ELAPSED TIME (HOURS) 25.00

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 23

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 007

Task 533183-832-801-001: Inspection

Get Access 11.75

On Aircraft

Inspection / Repair 1.00

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 1.00

Close-Up 19.50

TOTAL MANHOURS 35.75

ELAPSED TIME (HOURS) 23.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 008

Task 533183-832-801-001: Inspection

Get Access 11.75

On Aircraft

Inspection / Repair 1.00

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 1.00

Close-Up 19.50

TOTAL MANHOURS 35.75

ELAPSED TIME (HOURS) 23.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 009

Task 533183-832-801-001: Inspection

Get Access 11.75

On Aircraft

Inspection / Repair 1.00

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 1.00

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 24

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Task 533183-832-801-001: Inspection

Close-Up 19.50

TOTAL MANHOURS 35.75

ELAPSED TIME (HOURS) 23.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 010

Task 533183-832-801-001: Inspection

Get Access 11.75

On Aircraft

Inspection / Repair 1.00

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 1.00

Close-Up 19.50

TOTAL MANHOURS 35.75

ELAPSED TIME (HOURS) 25.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 011

Task 533183-832-801-001: Inspection

Get Access 11.75

On Aircraft

Inspection / Repair 1.00

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

0.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 1.00

Close-Up 13.75

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 20.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 012

Task 533183-832-801-001: Inspection

Get Access 11.75

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 25

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Task 533183-832-801-001: Inspection

On Aircraft

Inspection / Repair 1.00

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

0.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 1.00

Close-Up 13.75

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 20.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 014

Task 533183-832-801-001: Inspection

Get Access 5.00

On Aircraft

Inspection / Repair 0.50

Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

1.00

Tests 0.50

Close-Up 6.00

TOTAL MANHOURS 13.00

ELAPSED TIME (HOURS) 13.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 015

Task 533183-832-801-001: Inspection

Get Access 5.00

On Aircraft

Inspection / Repair 0.50

Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

1.00

Tests 1.00

Close-Up 6.00

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 13.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 26

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF 013

Task 533183-832-801-001: Inspection

Get Access 5.00

On Aircraft

Inspection / Repair 0.50

Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

0.50

Tests 1.00

Close-Up 6.00

TOTAL MANHOURS 13.00

ELAPSED TIME (HOURS) 13.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 017

Task 533183-832-801-001: Inspection

Get Access 136.0

On Aircraft

Inspection / Repair 4.00

Area 1a, replace the nuts in FWD LH and RH hard

points

0.50

Area 2a, replace the nuts of LH and RH keel lower

angle fittings

6.00

Area 2b, replace nuts of LH and RH flight control

fittings

2.50

Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

1.50

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Area C4 concession 1 0.50

Tests 4.00

Close-Up 150.0

TOTAL MANHOURS 307.50

ELAPSED TIME (HOURS) 113.0

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 018

Task 533183-832-801-001: Inspection

Get Access 136.0

On Aircraft

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 27

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Task 533183-832-801-001: Inspection

Inspection / Repair 4.00

Area 1a, replace the nuts in FWD LH and RH hard

points

0.50

Area 2a, replace the nuts of LH and RH keel lower

angle fittings

6.00

Area 2b, replace nuts of LH and RH flight control

fittings

2.50

Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

1.50

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

2.00

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 4.00

Close-Up 150.0

TOTAL MANHOURS 309.00

ELAPSED TIME (HOURS) 103.0

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 019

Task 533183-832-801-001: Inspection

Get Access 51.00

On Aircraft

Inspection / Repair 4.00

Area 1a, replace the nuts in FWD LH and RH hard

points

0.50

Area 2a, replace the nuts of LH and RH keel lower

angle fittings

6.00

Area 2b, replace nuts of LH and RH flight control

fittings

2.50

Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

1.50

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 1.00

Close-Up 62.00

TOTAL MANHOURS 131.00

ELAPSED TIME (HOURS) 44.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 28

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF 020

Task 533183-832-801-001: Inspection

Get Access 136.0

On Aircraft

Inspection / Repair 4.00

Area 1a, replace the nuts in FWD LH and RH hard

points

0.50

Area 2a, replace the nuts of LH and RH keel lower

angle fittings

6.00

Area 2b, replace nuts of LH and RH flight control

fittings

2.50

Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

1.50

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

0.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 4.00

Close-Up 150.0

TOTAL MANHOURS 307.50

ELAPSED TIME (HOURS) 103.0

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 021

Task 533183-832-801-001: Inspection

Get Access 5.00

On Aircraft

Inspection / Repair 0.50

Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

0.50

Tests 1.00

Close-Up 6.00

TOTAL MANHOURS 13.00

ELAPSED TIME (HOURS) 13.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 022

Task 533183-832-801-001: Inspection

Get Access 11.75

On Aircraft

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 29

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Task 533183-832-801-001: Inspection

Inspection / Repair 1.00

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 1.00

Close-Up 19.50

TOTAL MANHOURS 35.75

ELAPSED TIME (HOURS) 23.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 023

Task 533183-832-801-001: Inspection

Get Access 11.75

On Aircraft

Inspection / Repair 1.00

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

0.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 1.00

Close-Up 13.75

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 20.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 024

Task 533183-832-801-001: Inspection

Get Access 12.00

On Aircraft

Inspection / Repair 1.00

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Area C1 concession 1, replace the nuts 0.50

Tests 1.00

Close-Up 19.5

TOTAL MANHOURS 36.50

ELAPSED TIME (HOURS) 23.00

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 30

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 025

Task 533183-832-801-001: Inspection

Get Access 11.75

On Aircraft

Inspection / Repair 1.00

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

0.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 1.00

Close-Up 13.75

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 20.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 026

Task 533183-832-801-001: Inspection

Get Access 16.50

On Aircraft

Inspection / Repair 1.00

Area 1a, replace the nuts in FWD LH and RH hard

points

0.50

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 1.00

Close-Up 19.50

TOTAL MANHOURS 41.00

ELAPSED TIME (HOURS) 25.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 027

Task 533183-832-801-001: Inspection

Get Access 16.50

On Aircraft

Inspection / Repair 2.00

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 31

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Task 533183-832-801-001: Inspection

Area 1a, replace the nuts in FWD LH and RH hard

points

0.50

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Area C2 concession 1 0.50

Tests 2.00

Close-Up 19.50

TOTAL MANHOURS 43.50

ELAPSED TIME (HOURS) 26.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 028

Task 533183-832-801-001: Inspection

Get Access 16.50

On Aircraft

Inspection / Repair 1.00

Area 1a, replace the nuts in FWD LH and RH hard

points

0.50

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 1.00

Close-Up 19.50

TOTAL MANHOURS 41.00

ELAPSED TIME (HOURS) 25.50

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 029

Task 533183-832-801-001: Inspection

Get Access 139.0

On Aircraft

Inspection / Repair 4.00

Area 1a, replace the nuts in FWD LH and RH hard

points

0.50

Area 1b, replace the nuts of 800VU FR18 LH support 0.50

Area 2a, replace the nuts of LH and RH keel lower

angle fittings

6.00

Area 2b, replace nuts of LH and RH flight control

fittings

2.50

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 32

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Task 533183-832-801-001: Inspection

Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

1.50

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

0.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Tests 4.00

Close-Up 155.0

TOTAL MANHOURS 316.00

ELAPSED TIME (HOURS) 103.0

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 030

Task 533183-832-801-001: Inspection

Get Access 15.00

On Aircraft

Inspection / Repair 1.00

Area C4 concession 1 0.50

Area C5 concession 1 0.50

Tests 1.00

Close-Up 17.00

TOTAL MANHOURS 35.00

ELAPSED TIME (HOURS) 21.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF 031

Task 533183-832-801-001: Inspection

Get Access 24.5

On Aircraft

Inspection / Repair 1.00

Area C4 concession 2 0.50

Area C5 concession 3 1.00

Area C6 concession 1 0.50

Tests 1.00

Close-Up 27.00

TOTAL MANHOURS 55.50

ELAPSED TIME (HOURS) 35.00

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 33

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF 032

Task 533183-832-801-001: Inspection

Get Access 176.0

On Aircraft

Inspection / Repair 4.00

Area 1a, replace the nuts in FWD LH and RH hard

points

0.50

Area 2a, replace the nuts of LH and RH keel lower

angle fittings

6.00

Area 2b, replace nuts of LH and RH flight control

fittings

2.50

Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

1.50

Area 3, replace the nuts in outer wing front/rear spars

just outboard of rib 1

1.50

Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

1.50

Area 20, replace the nuts in fixed inner shroud box 1.00

Area C4 concession 1 2.00

Area C5 concession 2 0.50

Tests 4.00

Close-Up 195.0

TOTAL MANHOURS 396.00

ELAPSED TIME (HOURS) 133.0

NOTE: For detail concerning elapsed time assumption, refer to Appendix 02 Elapsed

Time Assumptions

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 34

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

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 21-26-00 22-96-00

22-97-00 24-41-00 25-52-00

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 53-35-11 53-35-13

57-17-11 57-27-11 57-41-37

Consumable Material List (CML)

Drawing R51415002

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 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 21-26-00 22-96-00

22-97-00 24-41-00 25-21-41

25-23-41 25-23-43 25-24-61

25-53-00 25-80-00 31-50-00

31-60-00 33-13-00 33-14-00

52-10-00 52-30-00 53-00-00

Consumable Material List (CML)

Drawing R51415002

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 21-26-00 22-96-00

22-97-00 24-41-00 25-21-41

25-23-41 25-24-61 25-52-00

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 53-35-11

53-35-13 57-17-11 57-27-11

57-41-37

Consumable Material List (CML)

Drawing R51415002

Elec. Std. Practices Manual (ESPM) 20-52-10 20-55-00

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 35

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

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 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 21-26-00 22-96-00

22-97-00 24-41-00 25-52-00

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 53-35-11 53-35-13

57-17-11 57-27-11 57-41-37

Consumable Material List (CML)

Drawing R51415002

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 21-26-00 22-96-00

22-97-00 24-41-00 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 53-35-11

57-17-11 57-27-11 57-41-37

Consumable Material List (CML)

Drawing R51415002

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 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 21-26-00 22-96-00

22-97-00 24-41-00 25-21-41

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

57-17-11 57-27-11 57-41-37

Consumable Material List (CML)

Drawing R51415002

Elec. Std. Practices Manual (ESPM) 20-52-10 20-55-00

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 36

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

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 21-26-00 22-96-00

22-97-00 24-41-00 27-50-00

28-10-00 28-25-00 31-50-00

31-60-00 33-13-00 33-14-00

52-10-00 57-17-11 57-27-11

Consumable Material List (CML)

Drawing R51415002

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 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 21-26-00 22-96-00

22-97-00 24-41-00 27-50-00

28-10-00 28-25-00 31-50-00

31-60-00 33-13-00 33-14-00

52-10-00 57-17-11 57-27-11

Consumable Material List (CML)

Drawing R51415002

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 21-26-00 22-96-00

22-97-00 24-41-00 27-50-00

28-10-00 28-25-00 31-50-00

31-60-00 33-13-00 33-14-00

52-10-00 57-17-11 57-27-11

Consumable Material List (CML)

Drawing R51415002

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: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 37

5

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@A330

SERVICE BULLETIN

**CONF 010

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 21-26-00 22-96-00

22-97-00 24-41-00 27-50-00

28-10-00 28-25-00 31-50-00

31-60-00 33-13-00 33-14-00

52-10-00 57-17-11 57-27-11

Consumable Material List (CML)

Drawing R51415002

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 011

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 21-26-00 22-96-00

22-97-00 24-41-00 27-50-00

28-10-00 28-25-00 31-50-00

31-60-00 33-13-00 33-14-00

52-10-00 57-17-11 57-27-11

Consumable Material List (CML)

Drawing R51415002

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 012

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 21-26-00 22-96-00

22-97-00 24-41-00 27-50-00

28-10-00 28-25-00 31-50-00

31-60-00 33-13-00 33-14-00

52-10-00 57-17-11 57-27-11

Consumable Material List (CML)

Drawing R51415002

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: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 38

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF 013

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 21-26-00 22-96-00

22-97-00 24-41-00 28-10-00

28-25-00 31-50-00 31-60-00

33-13-00 33-14-00 52-10-00

57-17-11 57-27-11

Consumable Material List (CML)

Drawing R51415002

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 014

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 21-26-00 22-96-00

22-97-00 24-41-00 28-10-00

28-25-00 31-50-00 31-60-00

33-13-00 33-14-00 52-10-00

57-17-11 57-27-11

Consumable Material List (CML)

Drawing R51415002

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 015

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 21-26-00 22-96-00

22-97-00 24-41-00 28-10-00

28-25-00 31-50-00 31-60-00

33-13-00 33-14-00 52-10-00

57-17-11 57-27-11

Consumable Material List (CML)

Drawing R51415002

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: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 39

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

**CONF 017

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 21-26-00 22-96-00

22-97-00 24-41-00 25-21-41

25-23-41 25-24-61 25-52-00

25-53-00 25-63-61 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 53-35-11 53-35-13

57-17-11 57-27-11 57-41-37

Consumable Material List (CML)

Drawing R51415002

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 018

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 21-26-00 22-96-00

22-97-00 24-41-00 25-52-00

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 53-35-11 53-35-13

57-17-11 57-27-11 57-41-37

Consumable Material List (CML)

Drawing R51415002

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 019

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 21-26-00 22-96-00

22-97-00 24-41-00 25-52-00

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 53-35-11 53-35-13

57-17-11 57-27-11 57-41-37

Consumable Material List (CML)

Drawing R51415002

Elec. Std. Practices Manual (ESPM) 20-52-10 20-55-00

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 40

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

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 020

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 21-26-00 22-96-00

22-97-00 24-41-00 25-52-00

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 53-35-11 53-35-13

57-17-11 57-27-11 57-41-37

Consumable Material List (CML)

Drawing R51415002

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 021

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 21-26-00 22-96-00

22-97-00 24-41-00 28-10-00

28-25-00 31-50-00 31-60-00

33-13-00 33-14-00 52-10-00

57-17-11 57-27-11

Consumable Material List (CML)

Drawing R51415002

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 022

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 21-26-00 22-96-00

22-97-00 24-41-00 27-50-00

28-10-00 28-25-00 31-50-00

31-60-00 33-13-00 33-14-00

52-10-00 57-17-11 57-27-11

Consumable Material List (CML)

Drawing R51415002

Elec. Std. Practices Manual (ESPM) 20-52-10 20-55-00

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 41

5

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@A330

SERVICE BULLETIN

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 023

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 21-26-00 22-96-00

22-97-00 24-41-00 27-50-00

28-10-00 28-25-00 31-50-00

31-60-00 33-13-00 33-14-00

52-10-00 57-17-11 57-27-11

Consumable Material List (CML)

Drawing R51415002

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 024

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 21-26-00 22-96-00

22-97-00 24-41-00 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 53-35-11

53-35-13 57-17-11 57-27-11

57-41-37

Consumable Material List (CML)

Drawing R51415002

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 025

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 21-26-00 22-96-00

22-97-00 24-41-00 27-50-00

28-10-00 28-25-00 31-50-00

31-60-00 33-13-00 33-14-00

52-10-00 57-17-11 57-27-11

Consumable Material List (CML)

Drawing R51415002

Elec. Std. Practices Manual (ESPM) 20-52-10 20-55-00

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 42

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

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 026

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 21-26-00 22-96-00

22-97-00 24-41-00 25-21-41

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

57-17-11 57-27-11 57-41-37

Consumable Material List (CML)

Drawing R51415002

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 027

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 21-26-00 22-96-00

22-97-00 24-41-00 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 53-35-11

53-35-13 57-17-11 57-27-11

57-41-37

Consumable Material List (CML)

Drawing R51415002

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 028

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 21-26-00 22-96-00

22-97-00 24-41-00 25-21-41

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

57-17-11 57-27-11 57-41-37

Consumable Material List (CML)

Drawing R51415002

Elec. Std. Practices Manual (ESPM) 20-52-10 20-55-00

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 43

5

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@A330

SERVICE BULLETIN

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 029

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 21-26-00 22-96-00

22-97-00 24-41-00 25-52-00

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 53-12-13

53-35-11 53-35-13 57-17-11

57-27-11 57-41-37

Consumable Material List (CML)

Drawing R51415002

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 030

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 21-26-00 22-96-00

22-97-00 24-41-00 25-23-41

25-24-61 25-52-00 25-53-00

25-80-00 31-50-00 31-60-00

33-13-00 33-14-00 52-10-00

52-30-00 53-00-00

Consumable Material List (CML)

Drawing R51415002

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 031

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 21-26-00 22-96-00

22-97-00 24-41-00 25-21-41

25-23-41 25-23-43 25-23-61

25-24-61 25-52-00 25-80-00

31-50-00 31-60-00 33-13-00

33-14-00 52-10-00 52-30-00

53-00-00

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 44

5

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@A330

SERVICE BULLETIN

Consumable Material List (CML)

Drawing R51415002

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 032

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 21-26-00 22-96-00

22-97-00 24-41-00 25-21-41

25-23-41 25-23-43 25-23-44

25-23-61 25-24-61 25-51-41

25-52-00 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 53-35-11 53-35-13

57-17-11 57-27-11 57-41-37

Consumable Material List (CML)

Drawing R51415002

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

Not Changed

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 45

5

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@A330

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 46

5

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@A330

SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Component COMPA01

Component COMPA02

Component COMPA03

Component COMPA04

Component COMPA05

Component COMPA06

Component COMPA07

Component COMPA08

Component COMPA09

Component COMPA10

Component COMPA11

Component COMPA12

Component COMPA13

Component COMPA14

Component COMPA15

Component COMPA16

Component COMPA17

Component COMPA18

Component COMPA19

Component COMPA20

Component COMPA21

Component COMPA22

Component COMPA23

Component COMPA24

Component COMPA25

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>

(2) Price and Availability

No AIRBUS kit will be provided. Parts required to accomplish this Service Bulletin are to

be supplied from Operator’s 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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 47

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@A330

SERVICE BULLETIN

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

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

(2) Components

Component COMPA01

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 COMPA02

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 COMPA03

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

NOTES

ASNA2531-4 60 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: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 48

5

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@A330

SERVICE BULLETIN

Component COMPA04

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

NOTES

ASNA2531-4 26 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 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 COMPA06

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 COMPA07

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 COMPA08

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

NOTES

ASNA2531-4 2 Nut

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 49

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@A330

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 COMPA09

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 COMPA10

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

NOTES

ASNA2531-4 11 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 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 COMPA12

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

NOTES

ASNA2531-4 14 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: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 50

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SERVICE BULLETIN

Component COMPA13

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

NOTES

ASNA2531-4 23 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 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 COMPA15

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 COMPA16

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 COMPA17

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

NOTES

ASNA2531-4 4 Nut

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 51

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@A330

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 COMPA18

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

NOTES

ASNA2531-4 11 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 COMPA19

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

NOTES

ASNA2531-4 25 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 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 COMPA21

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: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 52

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@A330

SERVICE BULLETIN

Component COMPA22

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 COMPA23

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 COMPA24

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 COMPA25

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 COMPA26

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

NOTES

ASNA2531-4 1 Nut

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 53

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@A330

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.

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

(1) Tooling - Price and Availability

No

(2) Tools

To accomplish this Service Bulletin it is necessary to use the tools listed in AMM tasks

mentioned in paragraph TASK 538153-831-801-01 Modification.

(3) Special Tools

None

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 54

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 533183-832-801-001 - 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

100 120 140 190 540 570 640 670

Access

Door 132AZ 821 831

Panel 541AB 641AB

Manpower

TOTAL MANHOURS 307.50

ELAPSED TIME (HOURS) 103.0

**CONF 002

Zone

130 150 250 260

Access

Door 822 831

Manpower

TOTAL MANHOURS 45.75

ELAPSED TIME (HOURS) 30.50

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 55

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SERVICE BULLETIN

**CONF 003

Zone

100 120 130 140 150 190 260 540 640

Access

Door 132AZ 821 831

Manpower

TOTAL MANHOURS 331.00

ELAPSED TIME (HOURS) 113.0

**CONF 004

Zone

100 120 140 190 540 570 640 670

Access

Door 132AZ 821 831

Panel 541AB 641AB

Manpower

TOTAL MANHOURS 307.50

ELAPSED TIME (HOURS) 103.0

**CONF 005

Zone

100 120 140 540 570 640 670

Access

Door 132AZ 821 831

Panel 541AB 641AB

Manpower

TOTAL MANHOURS 42.50

ELAPSED TIME (HOURS) 26.00

**CONF 006

Zone

100 120 140 540 640

Access

Door 132AZ 821 831

Manpower

TOTAL MANHOURS 41.00

ELAPSED TIME (HOURS) 25.00

**CONF 007

Zone

140 540 640

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 56

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SERVICE BULLETIN

Manpower

TOTAL MANHOURS 35.75

ELAPSED TIME (HOURS) 23.00

**CONF 008

Zone

140 540 640

Manpower

TOTAL MANHOURS 35.75

ELAPSED TIME (HOURS) 23.00

**CONF 009

Zone

140 540 640

Manpower

TOTAL MANHOURS 35.75

ELAPSED TIME (HOURS) 23.00

**CONF 010

Zone

140 540 640

Manpower

TOTAL MANHOURS 35.75

ELAPSED TIME (HOURS) 25.00

**CONF 011

Zone

140 540 570 640 670

Access

Panel 541AB 641AB

Manpower

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 20.00

**CONF 012

Zone

140 540 570 640 670

Access

Panel 541AB 641AB

Manpower

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 20.00

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 57

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SERVICE BULLETIN

**CONF 013

Zone

540 640

Access

Panel 541AB 641AB

Manpower

TOTAL MANHOURS 13.00

ELAPSED TIME (HOURS) 13.00

**CONF 014

Zone

540 640

Access

Panel 541AB 641AB

Manpower

TOTAL MANHOURS 13.00

ELAPSED TIME (HOURS) 13.00

**CONF 015

Zone

540 640

Access

Panel 541AB 641AB

Manpower

TOTAL MANHOURS 13.50

ELAPSED TIME (HOURS) 13.00

**CONF 017

Zone

100 120 140 150 190 260 540 570 640 670

Access

Door 132AZ 821 822 831

Manpower

TOTAL MANHOURS 307.50

ELAPSED TIME (HOURS) 113.0

**CONF 018

Zone

100 120 140 190 540 570 640 670

Access

Door 132AZ 821 831

Panel 541AB 641AB

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 58

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SERVICE BULLETIN

Manpower

TOTAL MANHOURS 309.00

ELAPSED TIME (HOURS) 103.0

**CONF 019

Zone

100 120 140 190 540 640

Access

Door 132AZ 821 831

Manpower

TOTAL MANHOURS 131.00

ELAPSED TIME (HOURS) 44.00

**CONF 020

Zone

100 120 140 190 540 570 640 670

Access

Door 132AZ 821 831

Panel 541AB 641AB

Manpower

TOTAL MANHOURS 307.50

ELAPSED TIME (HOURS) 103.0

**CONF 021

Zone

540 640

Access

Panel 541AB 641AB

Manpower

TOTAL MANHOURS 13.00

ELAPSED TIME (HOURS) 13.00

**CONF 022

Zone

140 540 640

Manpower

TOTAL MANHOURS 35.75

ELAPSED TIME (HOURS) 23.00

**CONF 023

Zone

140 540 570 640 670

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 59

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@A330

SERVICE BULLETIN

Access

Panel 541AB 641AB

Manpower

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 20.00

**CONF 024

Zone

100 140 540 570 640 670

Manpower

TOTAL MANHOURS 36.50

ELAPSED TIME (HOURS) 23.00

**CONF 025

Zone

140 540 570 640 670

Access

Panel 541AB 641AB

Manpower

TOTAL MANHOURS 30.50

ELAPSED TIME (HOURS) 20.00

**CONF 026

Zone

100 120 140 540 640

Access

Door 132AZ 821 831

Manpower

TOTAL MANHOURS 41.00

ELAPSED TIME (HOURS) 25.00

**CONF 027

Zone

100 120 140 540 570 640 670

Access

Door 132AZ 821 831

Manpower

TOTAL MANHOURS 43.50

ELAPSED TIME (HOURS) 26.00

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 60

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SERVICE BULLETIN

**CONF 028

Zone

100 120 140 540 640

Access

Door 132AZ 821 831

Manpower

TOTAL MANHOURS 41.00

ELAPSED TIME (HOURS) 25.50

**CONF 029

Zone

100 120 140 190 540 570 640 670

Access

Door 132AZ 821 831

Panel 541AB 641AB

Manpower

TOTAL MANHOURS 316.00

ELAPSED TIME (HOURS) 103.0

**CONF 030

Zone

130 150 250 260

From 250 to 260

Access

Door 821 831

Manpower

TOTAL MANHOURS 35.00

ELAPSED TIME (HOURS) 21.00

**CONF 031

Zone

130 150 250 260

From 250 to 260

Access

Door 821 822 831

Manpower

TOTAL MANHOURS 55.50

ELAPSED TIME (HOURS) 35.00

**CONF 032

Zone

100 120 130 140 150 190 250 260 540 570 640 670

From 250 to 260

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 61

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SERVICE BULLETIN

Access

Door 132AZ 821 822 831

Panel 541AB 641AB

Manpower

TOTAL MANHOURS 396.00

ELAPSED TIME (HOURS) 133.0

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 62

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SERVICE BULLETIN

(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 533183-832-001

001 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 63

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SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 64

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SERVICE BULLETIN

(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 533183-832-001

002 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 65

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SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 66

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

003 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 67

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 68

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

001 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 69

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 70

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

004 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 71

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 006

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 72

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

008 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 73

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 007

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 74

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

005 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 75

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 008

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 76

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

005 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 77

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 009

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 78

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

005 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 79

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 010

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 80

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

005 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 81

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 011

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 82

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

006 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 83

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 012

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 84

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

006 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 85

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 013

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 86

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

007 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 87

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 014

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 88

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

007 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 89

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 015

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 90

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

007 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 91

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 017

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 92

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

009 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 93

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 018

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 94

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

001 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 95

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 019

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 96

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

010 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 97

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 020

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 98

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

001 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 99

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 021

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 100

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

007 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 101

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 022

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 102

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

005 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 103

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 023

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 104

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

006 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 105

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 024

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 106

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

011 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 107

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 025

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 108

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

(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 533183-832-001

006 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 109

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 026

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 110

5

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@A330

SERVICE BULLETIN

(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 533183-832-001

008 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 111

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 027

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 112

5

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@A330

SERVICE BULLETIN

(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 533183-832-001

012 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 113

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 028

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 114

5

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@A330

SERVICE BULLETIN

(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 533183-832-001

008 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 115

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 029

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 116

5

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@A330

SERVICE BULLETIN

(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 533183-832-001

013 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 117

5

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@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 030

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 118

5

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@A330

SERVICE BULLETIN

(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 533183-832-001

015 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 119

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 031

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 120

5

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@A330

SERVICE BULLETIN

(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 533183-832-001

014 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 121

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 032

(1) Subtask 533183-910-001-001 - 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 R51415002

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 122

5

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@A330

SERVICE BULLETIN

(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 533183-832-001

016 Inspection / Repair .

(i) For the removal and installation of fasteners (Refer to SRM 51-42-00).

(j) For fastener hole diameters and drill and deburr data (Refer to SRM 51-44-00).

(k) For oversize, alternative and substitute fasteners (Refer to SRM 51-43-00).

(l) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-801).

(m) Install the fasteners (wet assembly) with

Interfay Sealant 09-005A As required

(n) Apply

Interfay Sealant 09-005A As required

to the interfaces of the structure and the reinstalled parts.

(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 123

5

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@A330

SERVICE BULLETIN

Polyurethane Finish

Paint (for External

Applic.)

16-018C As required

(2) Subtask 533183-839-001-001 - 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 ALL

B. PREPARATION

**CONF 001

(1) Subtask 533183-941-001-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

100

190

540

640

670

570

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 25-52-00-000-801

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 53-35-11-000-801

Task 53-35-13-000-801

Task 57-17-11-000-801

Task 57-27-11-000-801

Task 57-41-37-000-801

(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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 124

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@A330

SERVICE BULLETIN

(c) Open the passenger/crew door 831 (Refer to AMM Task 52-10-00-010-801).

(d) Open the forward 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).

(e) Open the avionics compartment door 132AZ.

(f) Open the MLG doors (Refer to AMM Task 32-12-00-010-801).

(g) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(h) 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).

(i) 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

(j) 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).

(k) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(l) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(m) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(n) Put warning notices in position before you start work on the aircraft.

(o) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary fairing panels (Refer to AMM Task 53-35-13-000-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 125

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SERVICE BULLETIN

2 Remove the necessary access panels (Refer to AMM Task

57-41-37-000-801).

3 Remove the necessary ceiling panels, partition panels and sidewall panels in

FWD cargo compartment (Refer to AMM Task 25-52-00-000-801).

4 Remove the necessary wing to fuselage fairings (Refer to AMM Task

53-35-11-000-801).

(p) Depending on aircraft configuration and findings, accesses 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 do work in the fuel tank

(Refer to AMM 28-10-00, Page Block 301).

2 De-fuel and vent the 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 panels (Refer to AMM Task 57-27-11-000-801).

5 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 002

(1) Subtask 533183-941-001-002 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

260

150

130

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 25-23-41-000-801

Task 25-23-43-000-802

Task 25-24-61-000-801

Task 25-53-00-000-801

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 53-00-00-000-803

(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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 126

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SERVICE BULLETIN

(c) Open the passenger/crew door 831 (Refer to AMM Task 52-10-00-010-801).

(d) Open the forward and aft cargo compartment door 822 and 821 (Refer to AMM

Task 52-30-00-010-801).

1 Install the safety lock (Refer to AMM Task 52-30-00-480-801).

(e) 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).

(f) 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

(g) 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).

(h) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(i) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(j) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(k) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary ceiling panels (Refer to AMM Task 25-23-41-000-801).

2 Remove the necessary sidewall panels (Refer to AMM Task

25-23-43-000-802).

3 Remove if necessary the overhead stowage-compartments at FR38 and/or

FR54 (Refer to AMM Task 25-24-61-000-801).

4 Remove the necessary cargo sidewall panels (Refer to AMM Task

53-00-00-000-803).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 127

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SERVICE BULLETIN

5 Remove the necessary cargo floor panels (Refer to AMM Task

25-53-00-000-801).

6 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 003

(1) Subtask 533183-941-001-003 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

100

150

190

540

640

260

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 25-24-61-000-801

Task 25-52-00-000-801

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 53-35-11-000-801

Task 53-35-13-000-801

Task 57-17-11-000-801

Task 57-27-11-000-801

Task 57-41-37-000-801

(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) Open the forward 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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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SERVICE BULLETIN

(e) Open the avionics compartment door 132AZ.

(f) Open the MLG doors (Refer to AMM Task 32-12-00-010-801).

(g) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(h) 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).

(i) 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

(j) 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).

(k) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(l) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(m) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(n) Put warning notices in position before you start work on the aircraft.

(o) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary fairing panels (Refer to AMM Task 53-35-13-000-801).

2 Remove the necessary access panels (Refer to AMM Task

57-41-37-000-801).

3 Remove if necessary the overhead stowage-compartments at FR38 and/or

FR54 (Refer to AMM Task 25-24-61-000-801).

4 Remove the necessary the wing to fuselage fairings (Refer to AMM Task

53-35-11-000-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 129

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@A330

SERVICE BULLETIN

5 Remove the necessary ceiling panels, partition panels and sidewall panels in

FWD cargo compartment (Refer to AMM Task 25-52-00-000-801).

6 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).

(p) Depending on aircraft configuration and findings, accesses 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 do work in the fuel tank

(Refer to AMM 28-10-00, Page Block 301).

2 De-fuel and vent the 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 panels (Refer to AMM Task 57-27-11-000-801).

5 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 004

(1) Subtask 533183-941-001-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

100

190

540

640

670

570

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 25-52-00-000-801

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 53-35-11-000-801

Task 53-35-13-000-801

Task 57-17-11-000-801

Task 57-27-11-000-801

Task 57-41-37-000-801

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 130

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SERVICE BULLETIN

(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) Open the forward 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).

(e) Open the avionics compartment door 132AZ.

(f) Open the MLG doors (Refer to AMM Task 32-12-00-010-801).

(g) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(h) 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).

(i) 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

(j) 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).

(k) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(l) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(m) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(n) Put warning notices in position before you start work on the aircraft.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 131

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SERVICE BULLETIN

(o) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary fairing panels (Refer to AMM Task 53-35-13-000-801).

2 Remove the necessary access panels (Refer to AMM Task

57-41-37-000-801).

3 Remove the necessary ceiling panels, partition panels and sidewall panels in

FWD cargo compartment (Refer to AMM Task 25-52-00-000-801).

4 Remove the necessary wing to fuselage fairings (Refer to AMM Task

53-35-11-000-801).

(p) Depending on aircraft configuration and findings, accesses 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 do work in the fuel tank

(Refer to AMM 28-10-00, Page Block 301).

2 De-fuel and vent the 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 panels (Refer to AMM Task 57-27-11-000-801).

5 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 005

(1) Subtask 533183-941-001-005 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

100

540

640

670

570

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 132

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

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 53-35-11-000-801

Task 57-17-11-000-801

Task 57-27-11-000-801

Task 57-41-37-000-801

(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) Open the forward 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).

(e) Open the avionics compartment door 132AZ.

(f) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(g) 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).

(h) 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

(i) 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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 133

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SERVICE BULLETIN

(j) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(k) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(l) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(m) Put warning notices in position before you start work on the aircraft.

(n) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary access panels (Refer to AMM Task

57-41-37-000-801).

2 Remove the necessary wing to fuselage fairings (Refer to AMM Task

53-35-11-000-801).

(o) Depending on aircraft configuration and findings, accesses 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 do work in the fuel tank

(Refer to AMM 28-10-00, Page Block 301).

2 De-fuel and vent the 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 panels (Refer to AMM Task 57-27-11-000-801).

5 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 006

(1) Subtask 533183-941-001-006 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

100

540

640

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 134

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

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 57-17-11-000-801

Task 57-27-11-000-801

Task 57-41-37-000-801

(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) Open the forward 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).

(e) Open the avionics compartment door 132AZ.

(f) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(g) 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).

(h) 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

(i) 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).

(j) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 135

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SERVICE BULLETIN

(k) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(l) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(m) Put warning notices in position before you start work on the aircraft.

(n) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary access panels (Refer to AMM Task

57-41-37-000-801).

(o) Depending on aircraft configuration and findings, accesses 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 do work in the fuel tank

(Refer to AMM 28-10-00, Page Block 301).

2 De-fuel and vent the 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 panels (Refer to AMM Task 57-27-11-000-801).

5 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 007

(1) Subtask 533183-941-001-007 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

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 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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 136

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@A330

SERVICE BULLETIN

(c) Open the passenger/crew door 831 (Refer to AMM Task 52-10-00-010-801).

(d) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(e) 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).

(f) 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

(g) 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).

(h) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(i) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(j) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(k) Put warning notices in position before you start work on the aircraft.

(l) You must obey the safety procedures when you do work in the fuel tank (Refer to

AMM 28-10-00, Page Block 301).

(m) De-fuel and vent the fuel tanks (Refer to AMM 28-25-00, Page Block 301).

(n) Put all switches related to the fuel system to OFF.

(o) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801).

2 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 137

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SERVICE BULLETIN

**CONF 008

(1) Subtask 533183-941-001-007 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

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 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) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(e) 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).

(f) 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

(g) 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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 138

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SERVICE BULLETIN

(h) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(i) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(j) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(k) Put warning notices in position before you start work on the aircraft.

(l) You must obey the safety procedures when you do work in the fuel tank (Refer to

AMM 28-10-00, Page Block 301).

(m) De-fuel and vent the fuel tanks (Refer to AMM 28-25-00, Page Block 301).

(n) Put all switches related to the fuel system to OFF.

(o) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801).

2 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 009

(1) Subtask 533183-941-001-007 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

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 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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 139

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SERVICE BULLETIN

(d) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(e) 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).

(f) 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

(g) 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).

(h) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(i) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(j) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(k) Put warning notices in position before you start work on the aircraft.

(l) You must obey the safety procedures when you do work in the fuel tank (Refer to

AMM 28-10-00, Page Block 301).

(m) De-fuel and vent the fuel tanks (Refer to AMM 28-25-00, Page Block 301).

(n) Put all switches related to the fuel system to OFF.

(o) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801).

2 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 140

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@A330

SERVICE BULLETIN

**CONF 010

(1) Subtask 533183-941-001-007 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

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 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) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(e) 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).

(f) 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

(g) 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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 141

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@A330

SERVICE BULLETIN

(h) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(i) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(j) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(k) Put warning notices in position before you start work on the aircraft.

(l) You must obey the safety procedures when you do work in the fuel tank (Refer to

AMM 28-10-00, Page Block 301).

(m) De-fuel and vent the fuel tanks (Refer to AMM 28-25-00, Page Block 301).

(n) Put all switches related to the fuel system to OFF.

(o) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801).

2 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 011

(1) Subtask 533183-941-001-008 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

540

640

670

570

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

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 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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 142

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@A330

SERVICE BULLETIN

(c) Open the passenger/crew door 831 (Refer to AMM Task 52-10-00-010-801).

(d) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(e) 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).

(f) 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

(g) 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).

(h) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(i) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(j) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(k) Put warning notices in position before you start work on the aircraft.

(l) You must obey the safety procedures when you do work in the fuel tank (Refer to

AMM 28-10-00, Page Block 301).

(m) De-fuel and vent the fuel tanks (Refer to AMM 28-25-00, Page Block 301).

(n) Put all switches related to the fuel system to OFF.

(o) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801).

2 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 143

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@A330

SERVICE BULLETIN

**CONF 012

(1) Subtask 533183-941-001-008 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

540

640

670

570

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

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 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) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(e) 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).

(f) 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

(g) 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) ;

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 144

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SERVICE BULLETIN

- 235VU (ELEC).

(h) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(i) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(j) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(k) Put warning notices in position before you start work on the aircraft.

(l) You must obey the safety procedures when you do work in the fuel tank (Refer to

AMM 28-10-00, Page Block 301).

(m) De-fuel and vent the fuel tanks (Refer to AMM 28-25-00, Page Block 301).

(n) Put all switches related to the fuel system to OFF.

(o) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801).

2 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 013

(1) Subtask 533183-941-001-009 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

28-10-00, Page Block 301

28-25-00, Page Block 301

Task 52-10-00-010-801

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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 145

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@A330

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) Put warning notices in position before you start work on the aircraft.

(k) You must obey the safety procedures when you do work in the fuel tank (Refer to

AMM 28-10-00, Page Block 301).

(l) De-fuel and vent the fuel tanks (Refer to AMM 28-25-00, Page Block 301).

(m) Put all switches related to the fuel system to OFF.

(n) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801).

2 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 146

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@A330

SERVICE BULLETIN

**CONF 014

(1) Subtask 533183-941-001-009 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

28-10-00, Page Block 301

28-25-00, Page Block 301

Task 52-10-00-010-801

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

(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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 147

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@A330

SERVICE BULLETIN

(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) Put warning notices in position before you start work on the aircraft.

(k) You must obey the safety procedures when you do work in the fuel tank (Refer to

AMM 28-10-00, Page Block 301).

(l) De-fuel and vent the fuel tanks (Refer to AMM 28-25-00, Page Block 301).

(m) Put all switches related to the fuel system to OFF.

(n) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801).

2 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 015

(1) Subtask 533183-941-001-009 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

28-10-00, Page Block 301

28-25-00, Page Block 301

Task 52-10-00-010-801

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 ;

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 148

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@A330

SERVICE BULLETIN

- 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) Put warning notices in position before you start work on the aircraft.

(k) You must obey the safety procedures when you do work in the fuel tank (Refer to

AMM 28-10-00, Page Block 301).

(l) De-fuel and vent the fuel tanks (Refer to AMM 28-25-00, Page Block 301).

(m) Put all switches related to the fuel system to OFF.

(n) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801).

2 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 017

(1) Subtask 533183-941-001-010 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

100

190

260

540

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 149

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@A330

SERVICE BULLETIN

640

670

570

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 25-23-41-000-801

Task 25-24-61-000-801

Task 25-52-00-000-801

Task 25-53-00-000-801

Task 25-63-61-000-801

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 53-35-11-000-801

Task 53-35-13-000-801

Task 57-17-11-000-801

Task 57-27-11-000-801

Task 57-41-37-000-801

(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) Open the forward and aft cargo compartment door 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).

(e) Open the avionics compartment door 132AZ.

(f) Open the MLG doors (Refer to AMM Task 32-12-00-010-801).

(g) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(h) 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 ;

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 150

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@A330

SERVICE BULLETIN

- EXT A (B).

(i) 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

(j) 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).

(k) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(l) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(m) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(n) Put warning notices in position before you start work on the aircraft.

(o) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary fairing panels (Refer to AMM Task 53-35-13-000-801).

2 Remove the necessary access panels (Refer to AMM Task

57-41-37-000-801).

3 Remove the necessary wing to fuselage fairings (Refer to AMM Task

53-35-11-000-801).

4 Remove the necessary ceiling panels (Refer to AMM Task 25-23-41-000-801).

5 Remove the necessary light cover (Refer to AMM Task 25-63-61-000-801).

6 Remove if necessary the overhead stowage-compartments at FR38 and/or

FR54 (Refer to AMM Task 25-24-61-000-801).

7 Remove the necessary ceiling panels, partition panels and sidewall panels in

FWD cargo compartment (Refer to AMM Task 25-52-00-000-801).

8 Remove the necessary aft cargo sidewall panels (Refer to AMM Task

25-53-00-000-801).

9 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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 151

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SERVICE BULLETIN

(p) Depending on aircraft configuration and findings, accesses 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 do work in the fuel tank

(Refer to AMM 28-10-00, Page Block 301).

2 De-fuel and vent the 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 panels (Refer to AMM Task 57-27-11-000-801).

5 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 018

(1) Subtask 533183-941-001-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

100

190

540

640

670

570

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 25-52-00-000-801

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 53-35-11-000-801

Task 53-35-13-000-801

Task 57-17-11-000-801

Task 57-27-11-000-801

Task 57-41-37-000-801

(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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 152

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SERVICE BULLETIN

(d) Open the forward 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).

(e) Open the avionics compartment door 132AZ.

(f) Open the MLG doors (Refer to AMM Task 32-12-00-010-801).

(g) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(h) 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).

(i) 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

(j) 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).

(k) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(l) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(m) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(n) Put warning notices in position before you start work on the aircraft.

(o) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary fairing panels (Refer to AMM Task 53-35-13-000-801).

2 Remove the necessary access panels (Refer to AMM Task

57-41-37-000-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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SERVICE BULLETIN

3 Remove the necessary ceiling panels, partition panels and sidewall panels in

FWD cargo compartment (Refer to AMM Task 25-52-00-000-801).

4 Remove the necessary wing to fuselage fairings (Refer to AMM Task

53-35-11-000-801).

(p) Depending on aircraft configuration and findings, accesses 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 do work in the fuel tank

(Refer to AMM 28-10-00, Page Block 301).

2 De-fuel and vent the 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 panels (Refer to AMM Task 57-27-11-000-801).

5 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 019

(1) Subtask 533183-941-001-011 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

100

190

540

640

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 25-52-00-000-801

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 53-35-11-000-801

Task 53-35-13-000-801

Task 57-17-11-000-801

Task 57-27-11-000-801

Task 57-41-37-000-801

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

12-34-24-860-802).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 154

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SERVICE BULLETIN

(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) Open the forward 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).

(e) Open the avionics compartment door 132AZ.

(f) Open the MLG doors (Refer to AMM Task 32-12-00-010-801).

(g) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(h) 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).

(i) 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

(j) 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).

(k) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(l) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(m) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(n) Put warning notices in position before you start work on the aircraft.

(o) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary fairing panels (Refer to AMM Task 53-35-13-000-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 155

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@A330

SERVICE BULLETIN

2 Remove the necessary access panels (Refer to AMM Task

57-41-37-000-801).

3 Remove the necessary ceiling panels, partition panels and sidewall panels in

FWD cargo compartment (Refer to AMM Task 25-52-00-000-801).

4 Remove the necessary wing to fuselage fairings (Refer to AMM Task

53-35-11-000-801).

(p) Depending on aircraft configuration and findings, accesses 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 do work in the fuel tank

(Refer to AMM 28-10-00, Page Block 301).

2 De-fuel and vent the 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 panels (Refer to AMM Task 57-27-11-000-801).

5 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 020

(1) Subtask 533183-941-001-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

100

190

540

640

670

570

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 156

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 25-52-00-000-801

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 53-35-11-000-801

Task 53-35-13-000-801

Task 57-17-11-000-801

Task 57-27-11-000-801

Task 57-41-37-000-801

(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) Open the forward 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).

(e) Open the avionics compartment door 132AZ.

(f) Open the MLG doors (Refer to AMM Task 32-12-00-010-801).

(g) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(h) 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).

(i) 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: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 157

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@A330

SERVICE BULLETIN

(j) 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).

(k) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(l) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(m) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(n) Put warning notices in position before you start work on the aircraft.

(o) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary fairing panels (Refer to AMM Task 53-35-13-000-801).

2 Remove the necessary access panels (Refer to AMM Task

57-41-37-000-801).

3 Remove the necessary ceiling panels, partition panels and sidewall panels in

FWD cargo compartment (Refer to AMM Task 25-52-00-000-801).

4 Remove the necessary wing to fuselage fairings (Refer to AMM Task

53-35-11-000-801).

(p) Depending on aircraft configuration and findings, accesses 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 do work in the fuel tank

(Refer to AMM 28-10-00, Page Block 301).

2 De-fuel and vent the 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 panels (Refer to AMM Task 57-27-11-000-801).

5 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 021

(1) Subtask 533183-941-001-009 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

540

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 158

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@A330

SERVICE BULLETIN

640

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

28-10-00, Page Block 301

28-25-00, Page Block 301

Task 52-10-00-010-801

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

(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) Put warning notices in position before you start work on the aircraft.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 159

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@A330

SERVICE BULLETIN

(k) You must obey the safety procedures when you do work in the fuel tank (Refer to

AMM 28-10-00, Page Block 301).

(l) De-fuel and vent the fuel tanks (Refer to AMM 28-25-00, Page Block 301).

(m) Put all switches related to the fuel system to OFF.

(n) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801).

2 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 022

(1) Subtask 533183-941-001-007 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

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 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) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(e) 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: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 160

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@A330

SERVICE BULLETIN

(f) 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

(g) 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).

(h) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(i) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(j) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(k) Put warning notices in position before you start work on the aircraft.

(l) You must obey the safety procedures when you do work in the fuel tank (Refer to

AMM 28-10-00, Page Block 301).

(m) De-fuel and vent the fuel tanks (Refer to AMM 28-25-00, Page Block 301).

(n) Put all switches related to the fuel system to OFF.

(o) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801).

2 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 023

(1) Subtask 533183-941-001-008 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

540

640

670

570

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 161

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

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 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) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(e) 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).

(f) 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

(g) 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).

(h) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(i) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(j) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(k) Put warning notices in position before you start work on the aircraft.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 162

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@A330

SERVICE BULLETIN

(l) You must obey the safety procedures when you do work in the fuel tank (Refer to

AMM 28-10-00, Page Block 301).

(m) De-fuel and vent the fuel tanks (Refer to AMM 28-25-00, Page Block 301).

(n) Put all switches related to the fuel system to OFF.

(o) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801).

2 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 024

(1) Subtask 533183-941-001-013 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

100

540

640

570

670

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

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 53-35-11-000-801

Task 53-35-13-000-801

Task 57-17-11-000-801

Task 57-27-11-000-801

Task 57-41-37-000-801

(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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 163

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SERVICE BULLETIN

(d) Open the forward 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).

(e) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(f) 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).

(g) 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

(h) 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).

(i) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(j) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(k) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(l) Put warning notices in position before you start work on the aircraft.

(m) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary access panels (Refer to AMM Task

57-41-37-000-801).

2 Remove the necessary wing to fuselage fairings (Refer to AMM Task

53-35-11-000-801).

3 Remove the necessary fairing panels (Refer to AMM Task 53-35-13-000-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 164

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@A330

SERVICE BULLETIN

(n) Depending on aircraft configuration and findings, accesses 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 do work in the fuel tank

(Refer to AMM 28-10-00, Page Block 301).

2 De-fuel and vent the 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 panels (Refer to AMM Task 57-27-11-000-801).

5 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 025

(1) Subtask 533183-941-001-008 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

540

640

670

570

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

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 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) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(e) 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 ;

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 165

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@A330

SERVICE BULLETIN

- EXT A (B).

(f) 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

(g) 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).

(h) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(i) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(j) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(k) Put warning notices in position before you start work on the aircraft.

(l) You must obey the safety procedures when you do work in the fuel tank (Refer to

AMM 28-10-00, Page Block 301).

(m) De-fuel and vent the fuel tanks (Refer to AMM 28-25-00, Page Block 301).

(n) Put all switches related to the fuel system to OFF.

(o) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801).

2 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 026

(1) Subtask 533183-941-001-006 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

100

540

640

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 166

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

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 57-17-11-000-801

Task 57-27-11-000-801

Task 57-41-37-000-801

(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) Open the forward 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).

(e) Open the avionics compartment door 132AZ.

(f) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(g) 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).

(h) 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

(i) 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).

(j) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 167

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@A330

SERVICE BULLETIN

(k) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(l) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(m) Put warning notices in position before you start work on the aircraft.

(n) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary access panels (Refer to AMM Task

57-41-37-000-801).

(o) Depending on aircraft configuration and findings, accesses 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 do work in the fuel tank

(Refer to AMM 28-10-00, Page Block 301).

2 De-fuel and vent the 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 panels (Refer to AMM Task 57-27-11-000-801).

5 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 027

(1) Subtask 533183-941-001-014 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

100

540

640

570

670

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 168

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

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 53-35-11-000-801

Task 53-35-13-000-801

Task 57-17-11-000-801

Task 57-27-11-000-801

Task 57-41-37-000-801

(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) Open the forward 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).

(e) Open the avionics compartment door 132AZ.

(f) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(g) 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).

(h) 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

(i) 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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 169

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@A330

SERVICE BULLETIN

(j) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(k) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(l) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(m) Put warning notices in position before you start work on the aircraft.

(n) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary access panels (Refer to AMM Task

57-41-37-000-801).

2 Remove the necessary wing to fuselage fairings (Refer to AMM Task

53-35-11-000-801).

3 Remove the necessary fairing panels (Refer to AMM Task 53-35-13-000-801).

(o) Depending on aircraft configuration and findings, accesses 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 do work in the fuel tank

(Refer to AMM 28-10-00, Page Block 301).

2 De-fuel and vent the 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 panels (Refer to AMM Task 57-27-11-000-801).

5 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 028

(1) Subtask 533183-941-001-006 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

100

540

640

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 170

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

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 57-17-11-000-801

Task 57-27-11-000-801

Task 57-41-37-000-801

(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) Open the forward 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).

(e) Open the avionics compartment door 132AZ.

(f) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(g) 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).

(h) 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

(i) 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).

(j) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 171

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@A330

SERVICE BULLETIN

(k) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(l) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(m) Put warning notices in position before you start work on the aircraft.

(n) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary access panels (Refer to AMM Task

57-41-37-000-801).

(o) Depending on aircraft configuration and findings, accesses 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 do work in the fuel tank

(Refer to AMM 28-10-00, Page Block 301).

2 De-fuel and vent the 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 panels (Refer to AMM Task 57-27-11-000-801).

5 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 029

(1) Subtask 533183-941-001-015 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

100

540

640

570

670

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 172

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 25-52-00-000-801

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 53-12-13-000-801

Task 53-35-11-000-801

Task 53-35-13-000-801

Task 57-17-11-000-801

Task 57-27-11-000-801

Task 57-41-37-000-801

(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) Open the forward 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).

(e) Open the avionics compartment door 132AZ.

(f) Open the MLG doors (Refer to AMM Task 32-12-00-010-801).

(g) Open access door Z811.

(h) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(i) 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: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 173

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SERVICE BULLETIN

(j) 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

(k) 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).

(l) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(m) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(n) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(o) Put warning notices in position before you start work on the aircraft.

(p) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary floor panel and assy panel in electronic compartment

FR20 (Refer to AMM Task 53-12-13-000-801).

2 Remove the necessary fairing panels (Refer to AMM Task 53-35-13-000-801).

3 Remove the necessary access panels (Refer to AMM Task

57-41-37-000-801).

4 Remove the necessary ceiling panels, partition panels and sidewall panels in

FWD cargo compartment (Refer to AMM Task 25-52-00-000-801).

5 Remove the necessary wing to fuselage fairings (Refer to AMM Task

53-35-11-000-801).

6 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) Depending on aircraft configuration and findings, accesses 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 do work in the fuel tank

(Refer to AMM 28-10-00, Page Block 301).

2 De-fuel and vent the fuel tanks (Refer to AMM 28-25-00, Page Block 301).

3 Put all switches related to the fuel system to OFF.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 174

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SERVICE BULLETIN

4 Remove the fuel tank access panels (Refer to AMM Task 57-27-11-000-801).

5 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF 030

(1) Subtask 533183-941-001-016 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

130

150

From 250

To 260

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 25-23-41-000-801

Task 25-24-61-000-801

Task 25-52-00-000-801

Task 25-53-00-000-801

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 53-00-00-000-802

(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) Open the forward and aft cargo compartment door 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).

(e) 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: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 175

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SERVICE BULLETIN

(f) 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

(g) 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).

(h) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(i) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(j) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(k) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary upper ceiling panels (Refer to AMM Task

25-23-41-000-801).

2 Remove if necessary the overhead stowage-compartments at FR38 and/or

FR54 (Refer to AMM Task 25-24-61-000-801).

3 Remove the necessary forward cargo sidewall panel (Refer to AMM Task

25-52-00-000-801).

4 Remove the necessary after cargo sidewall panel (Refer to AMM Task

25-53-00-000-801).

5 Remove the necessary cargo floor panel (Refer to AMM Task

53-00-00-000-802).

6 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 031

(1) Subtask 533183-941-001-017 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

130

150

From 250

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 176

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SERVICE BULLETIN

To 260

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 25-23-41-000-801

Task 25-23-43-000-802

Task 25-23-61-000-801

Task 25-24-61-000-801

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 53-00-00-000-803

(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) Open the forward and aft cargo compartment door 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).

(e) 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).

(f) 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

(g) 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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 177

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@A330

SERVICE BULLETIN

(h) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(i) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(j) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(k) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary ceiling panel (Refer to AMM Task 25-23-41-000-801).

2 Remove the necessary light cover (Refer to AMM Task 25-23-61-000-801).

3 Remove if necessary the overhead stowage-compartments at FR38 and/or

FR54 (Refer to AMM Task 25-24-61-000-801).

4 Remove the necessary sidewall panel (Refer to AMM Task 25-23-43-000-802).

5 Remove the necessary cargo sidewall panel (Refer to AMM Task

25-52-00-000-801).

6 Remove the necessary cargo floor panel (Refer to AMM Task

53-00-00-000-803).

7 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 032

(1) Subtask 533183-941-001-018 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

100

130

150

190

From 250

To 260

540

640

570

670

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 178

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802

Task 25-21-41-000-801

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 25-52-00-000-801

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 53-00-00-000-802

Task 53-00-00-000-803

Task 53-35-11-000-801

Task 53-35-13-000-801

Task 57-17-11-000-801

Task 57-27-11-000-801

Task 57-41-37-000-801

(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) Open the forward and aft cargo compartment door 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).

(e) Open the avionics compartment door 132AZ.

(f) Open access door Z801.

(g) Open the MLG doors (Refer to AMM Task 32-12-00-010-801).

(h) Fully extend the flaps to gain access to the rear spar (Refer to AMM Task

27-50-00-866-801).

(i) 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 ;

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 179

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@A330

SERVICE BULLETIN

- EXT A (B).

(j) 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

(k) 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).

(l) Make sure that there is (are) warning notice(s) in the cockpit to tell persons not to

start the APU.

(m) Make sure that the external connector(s) is (are) not connected to the aircraft

receptacle(s) EXT PWR A (B).

(n) Make sure that there is warning notice at the access door 121EL to tell persons not

to connect the external power connector(s).

(o) Put warning notices in position before you start work on the aircraft.

(p) Depending on aircraft configuration, remove only the necessary accesses to the

work areas :

1 Remove the necessary fairing panels (Refer to AMM Task 53-35-13-000-801).

2 Remove the necessary access panels (Refer to AMM Task

57-41-37-000-801).

3 Remove the necessary ceiling panels, partition panels and sidewall panels in

FWD cargo compartment (Refer to AMM Task 25-52-00-000-801).

4 Remove the necessary wing to fuselage fairings (Refer to AMM Task

53-35-11-000-801).

5 Remove the necessary passenger seats (Refer to AMM Task

25-21-41-000-801).

6 Remove the necessary ceiling panel (Refer to AMM Task 25-23-41-000-801).

7 Remove the necessary light cover (Refer to AMM Task 25-23-61-000-801).

8 Remove if necessary the overhead stowage-compartments at FR38 and/or

FR54 (Refer to AMM Task 25-24-61-000-801).

9 Remove the necessary sidewall panel (Refer to AMM Task 25-23-43-000-802).

10 Remove the necessary dado panels (Refer to AMM Task 25-23-44-000-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 180

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SERVICE BULLETIN

11 Remove the necessary cargo sidewall (Refer to AMM Task

25-52-00-000-801).

12 Remove the necessary after cargo floor panel (Refer to AMM Task

53-00-00-000-803).

13 Remove the necessary forward cargo floor panel (Refer to AMM Task

53-00-00-000-802).

14 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) Depending on aircraft configuration and findings, accesses 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 do work in the fuel tank

(Refer to AMM 28-10-00, Page Block 301).

2 De-fuel and vent the 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 panels (Refer to AMM Task 57-27-11-000-801).

5 Remove the fuel tank access covers (Refer to AMM Task 57-17-11-000-801).

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 533183-832-001-001 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

100

190

540

640

570

670

Manpower Resources

Manhours 4.00

Minimum number of person 4

Subtask elapsed time 1.00

Skills AIRFRAME

References

Drawing R51415002

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 181

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SERVICE BULLETIN

References

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, 2a, 2b, 2c, 3,

C7 and 20.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

R51415002.

(2) Subtask 533183-960-001-001 - Area 1a, replace the nuts in FWD LH and RH hard

points

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ, Door 831

Work location from Frame 16 to Frame 17

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 182

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SERVICE BULLETIN

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

(b) Install :

4 Nut ASNA2531-4

(3) Subtask 533183-960-003-001 - Area 2a, replace the 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 6.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 60 Nut

References

Drawing R51415002

Replace 60 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

60 Attachment-Retention ASNA2531-4 Discard

(b) Install :

60 Nut ASNA2531-4

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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SERVICE BULLETIN

(4) Subtask 533183-960-004-001 - Area 2b, replace nuts of LH and RH flight control

fittings

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 40

from Stringer 38 to Stringer 40

Manpower Resources

Manhours 2.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 26 Nut

References

Drawing R51415002

Replace 26 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

26 Attachment-Retention ASNA2531-4 Discard

(b) Install :

26 Nut ASNA2531-4

(5) Subtask 533183-960-005-001 - Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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SERVICE BULLETIN

Material necessary to do the job

Component COMPA05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(6) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 185

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SERVICE BULLETIN

(b) Install :

16 Nut ASNA2531-4

(7) Subtask 533183-960-007-001 - Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

Work Zones and Access Panels

Zone Access/Work location

540 Access Panel 541AB

Work location from Rib 1 to Rib 2

640 Access Panel 641AB

Work location from Rib 1 to Rib 2

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 1 Nut

References

Drawing R51415002

Replace 1 nut as described in Repair Instruction (RI) R51415002.

(a) Remove :

1 Attachment-Retention ASNA2531-4 Discard

(b) Install :

1 Nut ASNA2531-4

(8) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 186

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

**CONF 002

(1) Subtask 533183-832-001-002 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

130

150

260

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

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 C4 concession 1

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 187

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SERVICE BULLETIN

and C5 concession 2.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

R51415002.

(2) Subtask 533183-960-012-001 - Area C4 concession 1

Work Zones and Access Panels

Zone Access/Work location

150 Access Door 831, Door 822

Work location Frame 54

from Stringer 3 to Stringer 4

Stringer 30

Stringer 38

Stringer 44

Stringer 49

Stringer 52

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA18

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 11 Nut

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 188

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SERVICE BULLETIN

References

Drawing R51415002

Replace 11 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

11 Attachment-Retention ASNA2531-4 Discard

(b) Install :

11 Nut ASNA2531-4

(3) Subtask 533183-960-013-001 - Area C5 concession 2

Work Zones and Access Panels

Zone Access/Work location

250 Access Door 831

Work location Frame 38

Stringer 15

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA22

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 1 Nut

References

Drawing R51415002

Replace 1 nut as described in Repair Instruction (RI) R51415002.

(a) Remove :

1 Attachment-Retention ASNA2531-4 Discard

(b) Install :

1 Nut ASNA2531-4

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 189

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SERVICE BULLETIN

**CONF 003

(1) Subtask 533183-832-001-003 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

100

150

190

260

540

640

Manpower Resources

Manhours 4.00

Minimum number of person 4

Subtask elapsed time 1.00

Skills AIRFRAME

References

Drawing R51415002

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, 2a, 2b, 2c, 3,

20 and C3 concession 1.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 190

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SERVICE BULLETIN

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)

R51415002.

(2) Subtask 533183-960-001-001 - Area 1a, replace the nuts in FWD LH and RH hard

points

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ, Door 831

Work location from Frame 16 to Frame 17

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

(b) Install :

4 Nut ASNA2531-4

(3) Subtask 533183-960-003-001 - Area 2a, replace the nuts of LH and RH keel lower

angle fittings

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 40

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 191

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Manpower Resources

Manhours 6.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 60 Nut

References

Drawing R51415002

Replace 60 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

60 Attachment-Retention ASNA2531-4 Discard

(b) Install :

60 Nut ASNA2531-4

(4) Subtask 533183-960-004-001 - Area 2b, replace nuts of LH and RH flight control

fittings

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 40

from Stringer 38 to Stringer 40

Manpower Resources

Manhours 2.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 26 Nut

References

Drawing R51415002

Replace 26 nuts as described in Repair Instruction (RI) R51415002.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 192

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SERVICE BULLETIN

(a) Remove :

26 Attachment-Retention ASNA2531-4 Discard

(b) Install :

26 Nut ASNA2531-4

(5) Subtask 533183-960-005-001 - Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(6) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 193

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Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(7) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 194

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(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(8) Subtask 533183-960-011-001 - Area C3 concession 1

Work Zones and Access Panels

Zone Access/Work location

130 Access Door 831, Door 821

Work location Frame 37

Stringer 37

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA17

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

(b) Install :

4 Nut ASNA2531-4

**CONF 004

(1) Subtask 533183-832-001-001 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

100

190

540

640

570

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 195

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SERVICE BULLETIN

670

Manpower Resources

Manhours 4.00

Minimum number of person 4

Subtask elapsed time 1.00

Skills AIRFRAME

References

Drawing R51415002

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, 2a, 2b, 2c, 3,

C7 and 20.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

R51415002.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 196

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@A330

SERVICE BULLETIN

(2) Subtask 533183-960-001-001 - Area 1a, replace the nuts in FWD LH and RH hard

points

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ, Door 831

Work location from Frame 16 to Frame 17

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

(b) Install :

4 Nut ASNA2531-4

(3) Subtask 533183-960-003-001 - Area 2a, replace the 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 6.00

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 197

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 60 Nut

References

Drawing R51415002

Replace 60 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

60 Attachment-Retention ASNA2531-4 Discard

(b) Install :

60 Nut ASNA2531-4

(4) Subtask 533183-960-004-001 - Area 2b, replace nuts of LH and RH flight control

fittings

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 40

from Stringer 38 to Stringer 40

Manpower Resources

Manhours 2.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 26 Nut

References

Drawing R51415002

Replace 26 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

26 Attachment-Retention ASNA2531-4 Discard

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 198

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@A330

SERVICE BULLETIN

(b) Install :

26 Nut ASNA2531-4

(5) Subtask 533183-960-005-001 - Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(6) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 199

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(7) Subtask 533183-960-007-001 - Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

Work Zones and Access Panels

Zone Access/Work location

540 Access Panel 541AB

Work location from Rib 1 to Rib 2

640 Access Panel 641AB

Work location from Rib 1 to Rib 2

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 1 Nut

References

Drawing R51415002

Replace 1 nut as described in Repair Instruction (RI) R51415002.

(a) Remove :

1 Attachment-Retention ASNA2531-4 Discard

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 200

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SERVICE BULLETIN

(b) Install :

1 Nut ASNA2531-4

(8) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

**CONF 005

(1) Subtask 533183-832-001-004 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

100

540

640

570

670

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 201

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Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

References

Drawing R51415002

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, 3, C7 and 20.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

R51415002.

(2) Subtask 533183-960-001-001 - Area 1a, replace the nuts in FWD LH and RH hard

points

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ, Door 831

Work location from Frame 16 to Frame 17

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 202

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Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

(b) Install :

4 Nut ASNA2531-4

(3) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 203

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SERVICE BULLETIN

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(4) Subtask 533183-960-007-001 - Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

Work Zones and Access Panels

Zone Access/Work location

540 Access Panel 541AB

Work location from Rib 1 to Rib 2

640 Access Panel 641AB

Work location from Rib 1 to Rib 2

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 1 Nut

References

Drawing R51415002

Replace 1 nut as described in Repair Instruction (RI) R51415002.

(a) Remove :

1 Attachment-Retention ASNA2531-4 Discard

(b) Install :

1 Nut ASNA2531-4

(5) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 204

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@A330

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

**CONF 006

(1) Subtask 533183-832-001-008 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

100

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

Fig. A-FBCAA

Flow Chart

Sheet 01

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 205

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@A330

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, 3, and 20.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

R51415002.

(2) Subtask 533183-960-001-001 - Area 1a, replace the nuts in FWD LH and RH hard

points

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ, Door 831

Work location from Frame 16 to Frame 17

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 206

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

(b) Install :

4 Nut ASNA2531-4

(3) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 207

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@A330

SERVICE BULLETIN

(b) Install :

16 Nut ASNA2531-4

(4) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

**CONF 007

(1) Subtask 533183-832-001-005 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 208

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@A330

SERVICE BULLETIN

References

Drawing R51415002

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 3 and 20.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

R51415002.

(2) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 209

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(3) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 210

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@A330

SERVICE BULLETIN

**CONF 008

(1) Subtask 533183-832-001-005 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

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 3 and 20.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 211

5

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@A330

SERVICE BULLETIN

R51415002.

(2) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(3) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 212

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

**CONF 009

(1) Subtask 533183-832-001-005 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

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 3 and 20.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 213

5

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@A330

SERVICE BULLETIN

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

R51415002.

(2) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 214

5

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@A330

SERVICE BULLETIN

(b) Install :

16 Nut ASNA2531-4

(3) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

**CONF 010

(1) Subtask 533183-832-001-005 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 215

5

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@A330

SERVICE BULLETIN

References

Drawing R51415002

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 3 and 20.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

R51415002.

(2) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 216

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(3) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 217

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@A330

SERVICE BULLETIN

**CONF 011

(1) Subtask 533183-832-001-006 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

540

640

570

670

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

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 3, C7 and 20.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 218

5

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@A330

SERVICE BULLETIN

3 Perform the replacement of the half remaining nuts.

NOTE: If the fastener rotates, refer to Repair Instruction (RI)

R51415002.

(2) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(3) Subtask 533183-960-007-002 - Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

Work Zones and Access Panels

Zone Access/Work location

540 Access Panel 541AB

Work location from Rib 1 to Rib 2

640 Access Panel 641AB

Work location from Rib 1 to Rib 2

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 219

5

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@A330

SERVICE BULLETIN

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 2 Nut

References

Drawing R51415002

Replace 2 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

2 Attachment-Retention ASNA2531-4 Discard

(b) Install :

2 Nut ASNA2531-4

(4) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 220

5

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@A330

SERVICE BULLETIN

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

**CONF 012

(1) Subtask 533183-832-001-006 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

540

640

570

670

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

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 3, C7 and 20.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, replace the nut before next flight.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 221

5

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@A330

SERVICE BULLETIN

(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)

R51415002.

(2) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 222

5

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@A330

SERVICE BULLETIN

(3) Subtask 533183-960-007-006 - Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

Work Zones and Access Panels

Zone Access/Work location

540 Access Panel 541AB

Work location from Rib 1 to Rib 2

640 Access Panel 641AB

Work location from Rib 1 to Rib 2

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA09

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

(b) Install :

4 Nut ASNA2531-4

(4) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 223

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

**CONF 013

(1) Subtask 533183-832-001-007 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

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 area C7.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 224

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SERVICE BULLETIN

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

R51415002.

(2) Subtask 533183-960-007-001 - Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

Work Zones and Access Panels

Zone Access/Work location

540 Access Panel 541AB

Work location from Rib 1 to Rib 2

640 Access Panel 641AB

Work location from Rib 1 to Rib 2

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 1 Nut

References

Drawing R51415002

Replace 1 nut as described in Repair Instruction (RI) R51415002.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 225

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@A330

SERVICE BULLETIN

(a) Remove :

1 Attachment-Retention ASNA2531-4 Discard

(b) Install :

1 Nut ASNA2531-4

**CONF 014

(1) Subtask 533183-832-001-007 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

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 area C7.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 226

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@A330

SERVICE BULLETIN

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)

R51415002.

(2) Subtask 533183-960-007-003 - Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

Work Zones and Access Panels

Zone Access/Work location

540 Access Panel 541AB

Work location from Rib 1 to Rib 2

640 Access Panel 641AB

Work location from Rib 1 to Rib 2

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA10

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 11 Nut

References

Drawing R51415002

Replace 11 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

11 Attachment-Retention ASNA2531-4 Discard

(b) Install :

11 Nut ASNA2531-4

**CONF 015

(1) Subtask 533183-832-001-007 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

540

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 227

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@A330

SERVICE BULLETIN

640

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

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 area C7.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

R51415002.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 228

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@A330

SERVICE BULLETIN

(2) Subtask 533183-960-007-004 - Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

Work Zones and Access Panels

Zone Access/Work location

540 Access Panel 541AB

Work location from Rib 1 to Rib 2

640 Access Panel 641AB

Work location from Rib 1 to Rib 2

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA11

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 12 Nut

References

Drawing R51415002

Replace 12 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

12 Attachment-Retention ASNA2531-4 Discard

(b) Install :

12 Nut ASNA2531-4

**CONF 017

(1) Subtask 533183-832-001-009 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

100

190

260

540

640

570

670

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 229

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@A330

SERVICE BULLETIN

Manpower Resources

Manhours 4.00

Minimum number of person 4

Subtask elapsed time 1.00

Skills AIRFRAME

References

Drawing R51415002

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, 2a, 2b, 2c, 3

20 and C4 concession 1.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

R51415002.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 230

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@A330

SERVICE BULLETIN

(2) Subtask 533183-960-001-001 - Area 1a, replace the nuts in FWD LH and RH hard

points

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ, Door 831

Work location from Frame 16 to Frame 17

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

(b) Install :

4 Nut ASNA2531-4

(3) Subtask 533183-960-003-001 - Area 2a, replace the 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 6.00

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 231

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 60 Nut

References

Drawing R51415002

Replace 60 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

60 Attachment-Retention ASNA2531-4 Discard

(b) Install :

60 Nut ASNA2531-4

(4) Subtask 533183-960-004-001 - Area 2b, replace nuts of LH and RH flight control

fittings

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 40

from Stringer 38 to Stringer 40

Manpower Resources

Manhours 2.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 26 Nut

References

Drawing R51415002

Replace 26 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

26 Attachment-Retention ASNA2531-4 Discard

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 232

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@A330

SERVICE BULLETIN

(b) Install :

26 Nut ASNA2531-4

(5) Subtask 533183-960-005-001 - Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(6) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 233

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(7) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 234

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@A330

SERVICE BULLETIN

(8) Subtask 533183-960-012-003 - Area C4 concession 1

Work Zones and Access Panels

Zone Access/Work location

260 Access Door 831

Work location Frame 54

150 Access Door 822

Work location Frame 54

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA20

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 6 Nut

References

Drawing R51415002

Replace 6 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

6 Attachment-Retention ASNA2531-4 Discard

(b) Install :

6 Nut ASNA2531-4

**CONF 018

(1) Subtask 533183-832-001-001 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

100

190

540

640

570

670

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 235

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@A330

SERVICE BULLETIN

Manpower Resources

Manhours 4.00

Minimum number of person 4

Subtask elapsed time 1.00

Skills AIRFRAME

References

Drawing R51415002

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, 2a, 2b, 2c, 3,

C7 and 20.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

R51415002.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 236

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@A330

SERVICE BULLETIN

(2) Subtask 533183-960-001-001 - Area 1a, replace the nuts in FWD LH and RH hard

points

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ, Door 831

Work location from Frame 16 to Frame 17

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

(b) Install :

4 Nut ASNA2531-4

(3) Subtask 533183-960-003-001 - Area 2a, replace the 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 6.00

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 237

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 60 Nut

References

Drawing R51415002

Replace 60 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

60 Attachment-Retention ASNA2531-4 Discard

(b) Install :

60 Nut ASNA2531-4

(4) Subtask 533183-960-004-001 - Area 2b, replace nuts of LH and RH flight control

fittings

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 40

from Stringer 38 to Stringer 40

Manpower Resources

Manhours 2.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 26 Nut

References

Drawing R51415002

Replace 26 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

26 Attachment-Retention ASNA2531-4 Discard

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 238

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@A330

SERVICE BULLETIN

(b) Install :

26 Nut ASNA2531-4

(5) Subtask 533183-960-005-001 - Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(6) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 239

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(7) Subtask 533183-960-007-007 - Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

Work Zones and Access Panels

Zone Access/Work location

540 Access Panel 541AB

Work location from Rib 1 to Rib 2

640 Access Panel 641AB

Work location from Rib 1 to Rib 2

Manpower Resources

Manhours 2.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA13

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 23 Nut

References

Drawing R51415002

Replace 23 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

23 Attachment-Retention ASNA2531-4 Discard

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 240

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@A330

SERVICE BULLETIN

(b) Install :

23 Nut ASNA2531-4

(8) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

**CONF 019

(1) Subtask 533183-832-001-010 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

100

190

540

640

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 241

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@A330

SERVICE BULLETIN

Manpower Resources

Manhours 4.00

Minimum number of person 4

Subtask elapsed time 1.00

Skills AIRFRAME

References

Drawing R51415002

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, 2a, 2b, 2c, 3

and 20.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

R51415002.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 242

5

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@A330

SERVICE BULLETIN

(2) Subtask 533183-960-001-001 - Area 1a, replace the nuts in FWD LH and RH hard

points

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ, Door 831

Work location from Frame 16 to Frame 17

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

(b) Install :

4 Nut ASNA2531-4

(3) Subtask 533183-960-003-001 - Area 2a, replace the 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 6.00

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 243

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 60 Nut

References

Drawing R51415002

Replace 60 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

60 Attachment-Retention ASNA2531-4 Discard

(b) Install :

60 Nut ASNA2531-4

(4) Subtask 533183-960-004-001 - Area 2b, replace nuts of LH and RH flight control

fittings

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 40

from Stringer 38 to Stringer 40

Manpower Resources

Manhours 2.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 26 Nut

References

Drawing R51415002

Replace 26 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

26 Attachment-Retention ASNA2531-4 Discard

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 244

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@A330

SERVICE BULLETIN

(b) Install :

26 Nut ASNA2531-4

(5) Subtask 533183-960-005-001 - Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(6) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 245

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(7) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 246

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@A330

SERVICE BULLETIN

**CONF 020

(1) Subtask 533183-832-001-001 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

100

190

540

640

570

670

Manpower Resources

Manhours 4.00

Minimum number of person 4

Subtask elapsed time 1.00

Skills AIRFRAME

References

Drawing R51415002

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, 2a, 2b, 2c, 3,

C7 and 20.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 247

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@A330

SERVICE BULLETIN

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)

R51415002.

(2) Subtask 533183-960-001-001 - Area 1a, replace the nuts in FWD LH and RH hard

points

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ, Door 831

Work location from Frame 16 to Frame 17

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

(b) Install :

4 Nut ASNA2531-4

(3) Subtask 533183-960-003-001 - Area 2a, replace the nuts of LH and RH keel lower

angle fittings

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 40

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 248

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@A330

SERVICE BULLETIN

Manpower Resources

Manhours 6.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 60 Nut

References

Drawing R51415002

Replace 60 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

60 Attachment-Retention ASNA2531-4 Discard

(b) Install :

60 Nut ASNA2531-4

(4) Subtask 533183-960-004-001 - Area 2b, replace nuts of LH and RH flight control

fittings

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 40

from Stringer 38 to Stringer 40

Manpower Resources

Manhours 2.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 26 Nut

References

Drawing R51415002

Replace 26 nuts as described in Repair Instruction (RI) R51415002.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 249

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@A330

SERVICE BULLETIN

(a) Remove :

26 Attachment-Retention ASNA2531-4 Discard

(b) Install :

26 Nut ASNA2531-4

(5) Subtask 533183-960-005-001 - Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(6) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 250

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@A330

SERVICE BULLETIN

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(7) Subtask 533183-960-007-002 - Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

Work Zones and Access Panels

Zone Access/Work location

540 Access Panel 541AB

Work location from Rib 1 to Rib 2

640 Access Panel 641AB

Work location from Rib 1 to Rib 2

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA08

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 2 Nut

References

Drawing R51415002

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 251

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@A330

SERVICE BULLETIN

Replace 2 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

2 Attachment-Retention ASNA2531-4 Discard

(b) Install :

2 Nut ASNA2531-4

(8) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

**CONF 021

(1) Subtask 533183-832-001-007 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

540

640

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 252

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@A330

SERVICE BULLETIN

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

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 area C7.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

R51415002.

(2) Subtask 533183-960-007-001 - Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

Work Zones and Access Panels

Zone Access/Work location

540 Access Panel 541AB

Work location from Rib 1 to Rib 2

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 253

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@A330

SERVICE BULLETIN

640 Access Panel 641AB

Work location from Rib 1 to Rib 2

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 1 Nut

References

Drawing R51415002

Replace 1 nut as described in Repair Instruction (RI) R51415002.

(a) Remove :

1 Attachment-Retention ASNA2531-4 Discard

(b) Install :

1 Nut ASNA2531-4

**CONF 022

(1) Subtask 533183-832-001-005 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

Fig. A-FBCAA

Flow Chart

Sheet 01

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 254

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@A330

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 3 and 20.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

R51415002.

(2) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 255

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(3) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 256

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@A330

SERVICE BULLETIN

**CONF 023

(1) Subtask 533183-832-001-006 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

540

640

570

670

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

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 3, C7 and 20.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 257

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@A330

SERVICE BULLETIN

3 Perform the replacement of the half remaining nuts.

NOTE: If the fastener rotates, refer to Repair Instruction (RI)

R51415002.

(2) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(3) Subtask 533183-960-007-001 - Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

Work Zones and Access Panels

Zone Access/Work location

540 Access Panel 541AB

Work location from Rib 1 to Rib 2

640 Access Panel 641AB

Work location from Rib 1 to Rib 2

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 258

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@A330

SERVICE BULLETIN

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 1 Nut

References

Drawing R51415002

Replace 1 nut as described in Repair Instruction (RI) R51415002.

(a) Remove :

1 Attachment-Retention ASNA2531-4 Discard

(b) Install :

1 Nut ASNA2531-4

(4) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 259

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@A330

SERVICE BULLETIN

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

**CONF 024

(1) Subtask 533183-832-001-011 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

100

540

640

570

670

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

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 3, 20 and C1

concession 1.

- For inspection areas, refer toRepair Instruction (RI)

R51415002.

- For inspection report, Appendix 01 Inspection Report .

3 If no finding, replace the nut before next flight.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 260

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@A330

SERVICE BULLETIN

(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)

R51415002.

(2) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 261

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@A330

SERVICE BULLETIN

(3) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(4) Subtask 533183-960-009-001 - Area C1 concession 1, replace the nuts

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA15

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 1 Nut

References

Drawing R51415002

Replace 1 nut as described in Repair Instruction (RI) R51415002.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 262

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@A330

SERVICE BULLETIN

(a) Remove :

1 Attachment-Retention ASNA2531-4 Discard

(b) Install :

1 Nut ASNA2531-4

**CONF 025

(1) Subtask 533183-832-001-006 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

540

640

570

670

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

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 3, C7 and 20.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, replace the nut before next flight.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 263

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@A330

SERVICE BULLETIN

(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)

R51415002.

(2) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 264

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@A330

SERVICE BULLETIN

(3) Subtask 533183-960-007-001 - Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

Work Zones and Access Panels

Zone Access/Work location

540 Access Panel 541AB

Work location from Rib 1 to Rib 2

640 Access Panel 641AB

Work location from Rib 1 to Rib 2

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 1 Nut

References

Drawing R51415002

Replace 1 nut as described in Repair Instruction (RI) R51415002.

(a) Remove :

1 Attachment-Retention ASNA2531-4 Discard

(b) Install :

1 Nut ASNA2531-4

(4) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 265

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

**CONF 026

(1) Subtask 533183-832-001-008 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

100

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

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, 3, and 20.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 266

5

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@A330

SERVICE BULLETIN

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

R51415002.

(2) Subtask 533183-960-001-001 - Area 1a, replace the nuts in FWD LH and RH hard

points

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ, Door 831

Work location from Frame 16 to Frame 17

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 267

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@A330

SERVICE BULLETIN

(b) Install :

4 Nut ASNA2531-4

(3) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(4) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 268

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

**CONF 027

(1) Subtask 533183-832-001-012 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

100

540

640

570

670

Manpower Resources

Manhours 2.00

Minimum number of person 2

Subtask elapsed time 1.00

Skills AIRFRAME

References

Drawing R51415002

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: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 269

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@A330

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, 3, 20 and C2

concession 1.

- For inspection areas, refer toRepair Instruction (RI)

R51415002.

- For inspection report, Appendix 01 Inspection Report .

3 If no finding, 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)

R51415002.

(2) Subtask 533183-960-001-001 - Area 1a, replace the nuts in FWD LH and RH hard

points

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ, Door 831

Work location from Frame 16 to Frame 17

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 270

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@A330

SERVICE BULLETIN

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

(b) Install :

4 Nut ASNA2531-4

(3) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(4) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 271

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@A330

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(5) Subtask 533183-960-010-001 - Area C2 concession 1

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA16

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 1 Nut

References

Drawing R51415002

Replace 1 nut as described in Repair Instruction (RI) R51415002.

(a) Remove :

1 Attachment-Retention ASNA2531-4 Discard

(b) Install :

1 Nut ASNA2531-4

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 272

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@A330

SERVICE BULLETIN

**CONF 028

(1) Subtask 533183-832-001-008 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

100

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

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, 3, and 20.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 273

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@A330

SERVICE BULLETIN

3 Perform the replacement of the half remaining nuts.

NOTE: If the fastener rotates, refer to Repair Instruction (RI)

R51415002.

(2) Subtask 533183-960-001-001 - Area 1a, replace the nuts in FWD LH and RH hard

points

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ, Door 831

Work location from Frame 16 to Frame 17

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

(b) Install :

4 Nut ASNA2531-4

(3) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 274

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(4) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 275

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@A330

SERVICE BULLETIN

**CONF 029

(1) Subtask 533183-832-001-013 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

100

540

640

570

670

Manpower Resources

Manhours 4.00

Minimum number of person 4

Subtask elapsed time 1.00

Skills AIRFRAME

References

Drawing R51415002

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,

3, C7 and area 20.

- For inspection areas, refer toRepair Instruction (RI)

R51415002.

- For inspection report, Appendix 01 Inspection Report .

3 If no finding, 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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 276

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@A330

SERVICE BULLETIN

3 Perform the replacement of the half remaining nuts.

NOTE: If the fastener rotates, refer to Repair Instruction (RI)

R51415002.

(2) Subtask 533183-960-001-001 - Area 1a, replace the nuts in FWD LH and RH hard

points

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ, Door 831

Work location from Frame 16 to Frame 17

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

(b) Install :

4 Nut ASNA2531-4

(3) Subtask 533183-960-002-001 - Area 1b, replace the nuts of 800VU FR18 LH support

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ

Work location from Frame 18 to Frame 19

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 277

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

(b) Install :

4 Nut ASNA2531-4

(4) Subtask 533183-960-003-001 - Area 2a, replace the 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 6.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 60 Nut

References

Drawing R51415002

Replace 60 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

60 Attachment-Retention ASNA2531-4 Discard

(b) Install :

60 Nut ASNA2531-4

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 278

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@A330

SERVICE BULLETIN

(5) Subtask 533183-960-004-001 - Area 2b, replace nuts of LH and RH flight control

fittings

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 40

from Stringer 38 to Stringer 40

Manpower Resources

Manhours 2.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 26 Nut

References

Drawing R51415002

Replace 26 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

26 Attachment-Retention ASNA2531-4 Discard

(b) Install :

26 Nut ASNA2531-4

(6) Subtask 533183-960-005-001 - Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 279

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(7) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 280

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@A330

SERVICE BULLETIN

(b) Install :

16 Nut ASNA2531-4

(8) Subtask 533183-960-007-001 - Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

Work Zones and Access Panels

Zone Access/Work location

540 Access Panel 541AB

Work location from Rib 1 to Rib 2

640 Access Panel 641AB

Work location from Rib 1 to Rib 2

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA07

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 1 Nut

References

Drawing R51415002

Replace 1 nut as described in Repair Instruction (RI) R51415002.

(a) Remove :

1 Attachment-Retention ASNA2531-4 Discard

(b) Install :

1 Nut ASNA2531-4

(9) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 281

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@A330

SERVICE BULLETIN

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

**CONF 030

(1) Subtask 533183-832-001-015 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

130

150

250

260

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

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: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 282

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@A330

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 C4 concession 1

and C5 concession 1.

- For inspection areas, refer toRepair Instruction (RI)

R51415002.

- For inspection report, Appendix 01 Inspection Report .

3 If no finding, 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)

R51415002.

(2) Subtask 533183-960-012-006 - Area C4 concession 1

Work Zones and Access Panels

Zone Access/Work location

260

150

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA21

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 5 Nut

References

Drawing R51415002

Replace 5 nuts as described in Repair Instruction (RI) R51415002.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 283

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@A330

SERVICE BULLETIN

(a) Remove :

5 Attachment-Retention ASNA2531-4 Discard

(b) Install :

5 Nut ASNA2531-4

(3) Subtask 533183-960-013-003 - Area C5 concession 1

Work Zones and Access Panels

Zone Access/Work location

130 Access Door 831, Door 821

Work location Frame 38

Stringer 36

Stringer 43

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA24

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 1 Nut

References

Drawing R51415002

Replace 1 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

5 Attachment-Retention ASNA2531-4 Discard

(b) Install :

1 Nut ASNA2531-4

**CONF 031

(1) Subtask 533183-832-001-014 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

130

150

250

260

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 284

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@A330

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 2

Subtask elapsed time 0.50

Skills AIRFRAME

References

Drawing R51415002

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 C4 concession 2,

C5 concession 3 and C6 concession 1.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, refer to Appendix 01 Inspection

Report .

3 If no finding, 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)

R51415002.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 285

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@A330

SERVICE BULLETIN

(2) Subtask 533183-960-012-004 - Area C4 concession 2

Work Zones and Access Panels

Zone Access/Work location

260 Access Door 831

Work location Frame 54

Stringer 07

Stringer 21

150 Access Door 822

Work location Frame 54

from Stringer 55 to Stringer 56

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA21

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 5 Nut

References

Drawing R51415002

Replace 5 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

5 Attachment-Retention ASNA2531-4 Discard

(b) Install :

5 Nut ASNA2531-4

(3) Subtask 533183-960-013-004 - Area C5 concession 3

Work Zones and Access Panels

Zone Access/Work location

130 Access Door 831, Door 821

Work location Frame 38

from Stringer 37 to Stringer 41

Stringer 30

Stringer 26

250 Access Door 831

Work location Frame 38

Stringer 04

Stringer 18

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 286

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@A330

SERVICE BULLETIN

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA25

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 12 Nut

References

Drawing R51415002

Replace 12 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

13 Attachment-Retention ASNA2531-4 Discard

(b) Install :

12 Nut ASNA2531-4

(4) Subtask 533183-960-014-001 - Area C6 concession 1

Work Zones and Access Panels

Zone Access/Work location

130 Access Door 831

Work location Frame 39

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA26

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 1 Nut

References

Drawing R51415002

Replace 1 nut as described in Repair Instruction (RI) R51415002.

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(a) Remove :

1 Attachment-Retention ASNA2531-4 Discard

(b) Install :

1 Nut ASNA2531-4

**CONF 032

(1) Subtask 533183-832-001-016 - Inspection / Repair

Work Zones and Access Panels

Zone Access/Work location

100

130

150

190

250

260

540

640

570

670

Manpower Resources

Manhours 4.00

Minimum number of person 4

Subtask elapsed time 1.00

Skills AIRFRAME

References

Drawing R51415002

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, 2a, 2b, 2c, 3,

C7, 20, C4 concession 1 and C5 concession 2.

- For inspection areas, refer to Repair Instruction (RI)

R51415002.

- For inspection report, , refer to Appendix 01 Inspection

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Report .

3 If no finding, 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)

R51415002.

(2) Subtask 533183-960-001-001 - Area 1a, replace the nuts in FWD LH and RH hard

points

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 821, Door 132AZ, Door 831

Work location from Frame 16 to Frame 17

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

(b) Install :

4 Nut ASNA2531-4

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(3) Subtask 533183-960-003-001 - Area 2a, replace the 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 6.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA03

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 60 Nut

References

Drawing R51415002

Replace 60 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

60 Attachment-Retention ASNA2531-4 Discard

(b) Install :

60 Nut ASNA2531-4

(4) Subtask 533183-960-004-001 - Area 2b, replace nuts of LH and RH flight control

fittings

Work Zones and Access Panels

Zone Access/Work location

190 Work location Frame 40

from Stringer 38 to Stringer 40

Manpower Resources

Manhours 2.50

Minimum number of person 1

Skills AIRFRAME

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Material necessary to do the job

Component COMPA04

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 26 Nut

References

Drawing R51415002

Replace 26 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

26 Attachment-Retention ASNA2531-4 Discard

(b) Install :

26 Nut ASNA2531-4

(5) Subtask 533183-960-005-001 - Area 2c, replace the nuts in center wing rear spar

inboard of rib 1, RH and LH

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

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SERVICE BULLETIN

(b) Install :

16 Nut ASNA2531-4

(6) Subtask 533183-960-006-001 - Area 3, replace the nuts in outer wing front/rear

spars just outboard of rib 1

Work Zones and Access Panels

Zone Access/Work location

140 Work location Frame 40

Frame 47

Rib 1

Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA06

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(7) Subtask 533183-960-007-005 - Area C7, replace the nuts in outer wing center spar

between ribs 1 and 2

Work Zones and Access Panels

Zone Access/Work location

540 Access Panel 541AB

Work location from Rib 1 to Rib 2

640 Access Panel 641AB

Work location from Rib 1 to Rib 2

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Manpower Resources

Manhours 1.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA12

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 14 Nut

References

Drawing R51415002

Replace 14 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

14 Attachment-Retention ASNA2531-4 Discard

(b) Install :

14 Nut ASNA2531-4

(8) Subtask 533183-960-008-001 - Area 20, replace the nuts in fixed inner shroud box

Work Zones and Access Panels

Zone Access/Work location

540

640

Manpower Resources

Manhours 1.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA14

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 16 Nut

References

Drawing R51415002

Replace 16 nuts as described in Repair Instruction (RI) R51415002.

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SERVICE BULLETIN

(a) Remove :

16 Attachment-Retention ASNA2531-4 Discard

(b) Install :

16 Nut ASNA2531-4

(9) Subtask 533183-960-012-002 - Area C4 concession 1

Work Zones and Access Panels

Zone Access/Work location

150 Access Door 831, Door 822

Work location from Stringer 4 to Stringer 5

Stringer 10

from Stringer 15 to Stringer 21

from Stringer 29 to Stringer 31

Stringer 39

Stringer 47

Stringer 52

Frame 54

Manpower Resources

Manhours 2.00

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA19

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 25 Nut

References

Drawing R51415002

Replace 25 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

25 Attachment-Retention ASNA2531-4 Discard

(b) Install :

25 Nut ASNA2531-4

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SERVICE BULLETIN

(10) Subtask 533183-960-013-002 - Area C5 concession 2

Work Zones and Access Panels

Zone Access/Work location

130 Access Door 831, Door 821

Work location Frame 38

Stringer 36

Stringer 43

Manpower Resources

Manhours 0.50

Minimum number of person 1

Skills AIRFRAME

Material necessary to do the job

Component COMPA23

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

ASNA2531-4 4 Nut

References

Drawing R51415002

Replace 4 nuts as described in Repair Instruction (RI) R51415002.

(a) Remove :

4 Attachment-Retention ASNA2531-4 Discard

(b) Install :

4 Nut ASNA2531-4

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 533183-941-002-033 - 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 533183-942-001 001 Close-up .

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(a) In the cockpit, on the panel 235VU, push the push-button switches :

- BAT 1, BAT 2, APU BAT ;

- GEN 1, (2, 3, 4), APU GEN ;

- EXT A (B).

(b) Remove the warning notices.

(c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801)

(2) Subtask 533183-865-001-001 - 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 533183-941-003-001 - 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: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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(c) Do the operational test of lights (Refer to AMM Task 33-14-00-710-801).

(d) Do the operational test of the avionics-equipment ventilation system (Refer to AMM

Task 21-26-00-710-803).

(e) Do the BITE test of the auto flight system (SYSTEM TEST) (Refer to AMM Task

22-96-00-740-801).

(f) Do the operational test of the ECAM control panel (Refer to AMM Task

31-50-00-710-803).

(g) Do the test of FWS (Refer to AMM Task 31-50-00-740-801).

(h) Do the operational test of EIS (Refer to AMM Task 31-60-00-710-802).

(4) Subtask 533183-700-002-001 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, 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) If removed during preparation, 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).

**CONF 002

(1) Subtask 533183-941-002-033 - 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 533183-942-001 002 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.

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(c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801)

(2) Subtask 533183-865-001-001 - 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 533183-941-003-001 - 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).

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(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 533183-700-002-002 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-21-41-400-801

Task 25-23-41-400-801

(a) 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).

(b) If removed during preparation, do the test procedure as specified after the

installation of the passenger seats (Refer to AMM Task 25-21-41-400-801).

**CONF 003

(1) Subtask 533183-941-002-033 - 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 533183-942-001 003 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 533183-865-001-001 - C/B Closing

Manpower Resources

Skills AIRFRAME

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(a) Close the following circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742 701PP 10PB1 72 S

742 702PP 10PB2 71 S

(3) Subtask 533183-941-003-001 - 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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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(4) Subtask 533183-700-002-003 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-21-41-400-801

Task 25-23-41-400-801

Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, 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) If removed during preparation, 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 ceiling panels (Refer to AMM Task 25-23-41-400-801).

(d) If removed during preparation, do the test procedure as specified after the

installation of the passenger seats (Refer to AMM Task 25-21-41-400-801).

**CONF 004

(1) Subtask 533183-941-002-033 - 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 533183-942-001 001 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 533183-865-001-001 - C/B Closing

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

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(a) Close the following circuit breakers :

PANEL DESIGNATION FIN LOCATION SEE

NOTES

742 701PP 10PB1 72 S

742 702PP 10PB2 71 S

(3) Subtask 533183-941-003-001 - 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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 302

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SERVICE BULLETIN

(4) Subtask 533183-700-002-001 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, 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) If removed during preparation, 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).

**CONF 005

(1) Subtask 533183-941-002-033 - 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 533183-942-001 005 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 533183-865-001-001 - 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: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 303

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SERVICE BULLETIN

(3) Subtask 533183-941-003-001 - 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 533183-700-002-004 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 304

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SERVICE BULLETIN

(a) If removed during preparation, 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) If removed during preparation, 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).

**CONF 006

(1) Subtask 533183-941-002-033 - 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 533183-942-001 006 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 305

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@A330

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 533183-700-002-005 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-21-41-400-801

Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after the

installation of the passenger seats (Refer to AMM Task 25-21-41-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 306

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@A330

SERVICE BULLETIN

(b) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

(c) If removed during preparation, 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).

**CONF 007

(1) Subtask 533183-941-002-033 - 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 533183-942-001 007 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 307

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@A330

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 533183-700-002-006 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 308

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 008

(1) Subtask 533183-941-002-033 - 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 533183-942-001 007 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 309

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@A330

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 533183-700-002-006 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 310

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 009

(1) Subtask 533183-941-002-033 - 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 533183-942-001 007 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 311

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@A330

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 533183-700-002-006 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 312

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 010

(1) Subtask 533183-941-002-033 - 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 533183-942-001 007 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 313

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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 533183-700-002-006 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 314

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 011

(1) Subtask 533183-941-002-033 - 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 533183-942-001 011 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 315

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@A330

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 533183-700-002-007 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 316

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 012

(1) Subtask 533183-941-002-033 - 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 533183-942-001 011 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 317

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@A330

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 533183-700-002-007 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 318

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 013

(1) Subtask 533183-941-002-033 - 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 533183-942-001 013 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 319

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@A330

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 533183-700-002-008 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 320

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 014

(1) Subtask 533183-941-002-033 - 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 533183-942-001 013 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 321

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@A330

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 533183-700-002-008 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 322

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 015

(1) Subtask 533183-941-002-033 - 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 533183-942-001 013 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 323

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@A330

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 533183-700-002-008 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 324

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 017

(1) Subtask 533183-941-002-033 - 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 533183-942-001 016 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 325

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@A330

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 533183-700-002-009 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-21-41-400-801

Task 25-23-41-400-801

Task 57-17-11-400-801

Task 57-27-11-400-801

(a) 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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 326

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@A330

SERVICE BULLETIN

(b) If removed during preparation, do the test procedure as specified after the

installation of the passenger seats (Refer to AMM Task 25-21-41-400-801).

(c) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

(d) If removed during preparation, 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).

**CONF 018

(1) Subtask 533183-941-002-033 - 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 533183-942-001 001 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 327

5

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@A330

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 533183-700-002-001 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 328

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 019

(1) Subtask 533183-941-002-033 - 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 533183-942-001 018 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 329

5

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@A330

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 533183-700-002-010 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 330

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 020

(1) Subtask 533183-941-002-033 - 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 533183-942-001 001 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 331

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@A330

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 533183-700-002-001 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 332

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 021

(1) Subtask 533183-941-002-033 - 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 533183-942-001 013 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 333

5

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@A330

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 533183-700-002-008 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 334

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 022

(1) Subtask 533183-941-002-033 - 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 533183-942-001 007 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 335

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@A330

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 533183-700-002-006 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 336

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 023

(1) Subtask 533183-941-002-033 - 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 533183-942-001 011 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 337

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@A330

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 533183-700-002-007 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 338

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 024

(1) Subtask 533183-941-002-033 - 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 533183-942-001 023 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 339

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@A330

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 533183-700-002-011 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 340

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 025

(1) Subtask 533183-941-002-033 - 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 533183-942-001 011 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 341

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@A330

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 533183-700-002-007 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 342

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 026

(1) Subtask 533183-941-002-033 - 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 533183-942-001 006 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 343

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@A330

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 533183-700-002-005 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-21-41-400-801

Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after the

installation of the passenger seats (Refer to AMM Task 25-21-41-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 344

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@A330

SERVICE BULLETIN

(b) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

(c) If removed during preparation, 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).

**CONF 027

(1) Subtask 533183-941-002-033 - 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 533183-942-001 026 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 345

5

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@A330

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 533183-700-002-012 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 346

5

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 028

(1) Subtask 533183-941-002-033 - 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 533183-942-001 006 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 347

5

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@A330

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 533183-700-002-005 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-21-41-400-801

Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after the

installation of the passenger seats (Refer to AMM Task 25-21-41-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 348

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@A330

SERVICE BULLETIN

(b) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

(c) If removed during preparation, 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).

**CONF 029

(1) Subtask 533183-941-002-033 - 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 533183-942-001 028 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 349

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@A330

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 533183-700-002-013 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 57-17-11-400-801

Task 57-27-11-400-801

(a) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 350

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@A330

SERVICE BULLETIN

(b) If removed during preparation, 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).

**CONF 030

(1) Subtask 533183-941-002-033 - 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 533183-942-001 029 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 533183-865-001-001 - 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 533183-941-003-001 - Preliminary Tests

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 351

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@A330

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 533183-700-002-014 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-23-41-400-801

(a) 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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 352

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@A330

SERVICE BULLETIN

**CONF 031

(1) Subtask 533183-941-002-033 - 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 533183-942-001 030 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 533183-865-001-001 - 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 533183-941-003-001 - 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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 353

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@A330

SERVICE BULLETIN

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 533183-700-002-015 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-21-41-400-801

Task 25-23-41-400-801

(a) 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).

(b) If removed during preparation, do the test procedure as specified after the

installation of the passenger seats (Refer to AMM Task 25-21-41-400-801).

**CONF 032

(1) Subtask 533183-941-002-033 - Test Job Set-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 24-41-00-861-801

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 354

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@A330

SERVICE BULLETIN

NOTE: Before the tests, do not forget to install the parts and/or equipment as

required in SUBTASK 533183-942-001 031 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 533183-865-001-001 - 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 533183-941-003-001 - 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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 355

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@A330

SERVICE BULLETIN

(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 533183-700-002-016 - Tests

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-21-41-400-801

Task 25-23-41-400-801

Task 57-17-11-400-801

Task 57-27-11-400-801

(a) 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).

(b) If removed during preparation, do the test procedure as specified after the

installation of the passenger seats (Refer to AMM Task 25-21-41-400-801).

(c) If removed during preparation, do the test procedure as specified after installation

of the underwing fuel tank access panels (Refer to AMM Task 57-27-11-400-801).

(d) If removed during preparation, 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).

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 533183-942-001-001 - Close-up

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 356

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

Task 52-30-00-080-801

Task 52-30-00-410-801

Task 53-35-11-400-801

Task 53-35-13-400-801

Task 57-17-11-400-801

Task 57-41-37-400-801

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

equipment.

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the wing to fuselage fairing (Refer to AMM Task

53-35-11-400-801).

2 If removed install access panels (Refer to AMM Task 57-41-37-400-801).

3 If removed install fairing panels (Refer to AMM Task 53-35-13-400-801).

4 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the avionics compartment door 132AZ.

(d) Close the forward 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).

(e) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(f) Restore the systems and the aircraft to normal operating condition.

(g) Remove the access platform.

**CONF 002

(1) Subtask 533183-942-001-002 - Close-up

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 357

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 25-23-41-400-801

Task 25-23-43-400-802

Task 25-24-61-400-801

Task 25-53-00-400-801

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 53-00-00-400-803

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

equipment.

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 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 If removed install cargo floor panels (Refer to AMM Task 25-53-00-400-801).

3 If removed install cargo sidewall panels (Refer to AMM Task

53-00-00-400-803).

4 If removed install sidewall panels (Refer to AMM Task 25-23-43-400-802).

5 If removed, install the overhead stowage-compartments at FR38 and/or FR54

(Refer to AMM Task 25-24-61-400-801).

6 If removed install ceiling panels (Refer to AMM Task 25-23-41-400-801)

(c) Close the forward and aft cargo compartment door 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).

(d) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(e) Restore the systems and the aircraft to normal operating condition.

(f) Remove the access platform.

**CONF 003

(1) Subtask 533183-942-001-003 - Close-up

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 358

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 25-24-61-400-801

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 53-35-11-400-801

Task 53-35-13-400-801

Task 57-17-11-400-801

Task 57-27-11-400-801

Task 57-41-37-400-801

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

equipment.

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 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 If removed install cargo sidewall panels (Refer to AMM Task

25-52-00-400-801).

3 If removed install the wing to fuselage fairing (Refer to AMM Task

53-35-11-400-801).

4 If removed install access panels (Refer to AMM Task 57-41-37-400-801).

5 If removed, install the overhead stowage-compartments at FR38 and/or FR54

(Refer to AMM Task 25-24-61-400-801).

6 If removed install fairing panels (Refer to AMM Task 53-35-13-400-801).

7 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

8 If removed install the fuel tank access covers (Refer to AMM Task

57-27-11-400-801).

(c) Close the avionics compartment door 132AZ.

(d) Close the forward 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).

(e) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(f) Restore the systems and the aircraft to normal operating condition.

(g) Remove the access platform.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 359

5

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@A330

SERVICE BULLETIN

**CONF 004

(1) Subtask 533183-942-001-001 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

Task 52-30-00-080-801

Task 52-30-00-410-801

Task 53-35-11-400-801

Task 53-35-13-400-801

Task 57-17-11-400-801

Task 57-41-37-400-801

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

equipment.

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the wing to fuselage fairing (Refer to AMM Task

53-35-11-400-801).

2 If removed install access panels (Refer to AMM Task 57-41-37-400-801).

3 If removed install fairing panels (Refer to AMM Task 53-35-13-400-801).

4 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the avionics compartment door 132AZ.

(d) Close the forward 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).

(e) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(f) Restore the systems and the aircraft to normal operating condition.

(g) Remove the access platform.

**CONF 005

(1) Subtask 533183-942-001-005 - Close-up

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 360

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

Task 52-30-00-080-801

Task 52-30-00-410-801

Task 53-35-11-400-801

Task 57-17-11-400-801

Task 57-27-11-400-801

Task 57-41-37-400-801

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

equipment.

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the wing to fuselage fairing (Refer to AMM Task

53-35-11-400-801).

2 If removed install access panels (Refer to AMM Task 57-41-37-400-801).

3 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

4 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the avionics compartment door 132AZ.

(d) Close the forward 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).

(e) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(f) Restore the systems and the aircraft to normal operating condition.

(g) Remove the access platform.

**CONF 006

(1) Subtask 533183-942-001-006 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

Task 57-17-11-400-801

Task 57-27-11-400-801

Task 57-41-37-400-801

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 361

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SERVICE BULLETIN

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

equipment.

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install access panels (Refer to AMM Task 57-41-37-400-801).

2 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

3 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the avionics compartment door 132AZ.

(d) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(e) Restore the systems and the aircraft to normal operating condition.

(f) Remove the access platform.

**CONF 007

(1) Subtask 533183-942-001-007 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

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) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

2 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(d) Restore the systems and the aircraft to normal operating condition.

(e) Remove the access platform.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 362

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@A330

SERVICE BULLETIN

**CONF 008

(1) Subtask 533183-942-001-007 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

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) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

2 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(d) Restore the systems and the aircraft to normal operating condition.

(e) Remove the access platform.

**CONF 009

(1) Subtask 533183-942-001-007 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

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) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

2 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 363

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SERVICE BULLETIN

(c) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(d) Restore the systems and the aircraft to normal operating condition.

(e) Remove the access platform.

**CONF 010

(1) Subtask 533183-942-001-007 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

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) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

2 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(d) Restore the systems and the aircraft to normal operating condition.

(e) Remove the access platform.

**CONF 011

(1) Subtask 533183-942-001-011 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 364

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@A330

SERVICE BULLETIN

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

2 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(d) Restore the systems and the aircraft to normal operating condition.

(e) Remove the access platform.

**CONF 012

(1) Subtask 533183-942-001-011 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

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) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

2 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(d) Restore the systems and the aircraft to normal operating condition.

(e) Remove the access platform.

**CONF 013

(1) Subtask 533183-942-001-013 - Close-up

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 365

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

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) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

2 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(d) Restore the systems and the aircraft to normal operating condition.

(e) Remove the access platform.

**CONF 014

(1) Subtask 533183-942-001-013 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

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) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

2 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(d) Restore the systems and the aircraft to normal operating condition.

(e) Remove the access platform.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 366

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@A330

SERVICE BULLETIN

**CONF 015

(1) Subtask 533183-942-001-013 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

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) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

2 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(d) Restore the systems and the aircraft to normal operating condition.

(e) Remove the access platform.

**CONF 017

(1) Subtask 533183-942-001-016 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-23-41-400-801

Task 25-24-61-400-801

Task 25-52-00-400-801

Task 25-53-00-400-801

Task 25-63-61-400-801

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 53-35-11-400-801

Task 53-35-13-400-801

Task 57-17-11-400-801

Task 57-27-11-400-801

Task 57-41-37-400-801

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 367

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@A330

SERVICE BULLETIN

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

equipment.

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 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 If removed install after cargo sidewall panels (Refer to AMM Task

25-53-00-400-801).

3 If removed install forward cargo sidewall panels (Refer to AMM Task

25-52-00-400-801).

4 If removed, install the overhead stowage-compartments at FR38 and/or FR54

(Refer to AMM Task 25-24-61-400-801).

5 If removed install light covers (Refer to AMM Task 25-63-61-400-801).

6 If removed install ceiling panels (Refer to AMM Task 25-23-41-400-801)

7 If removed install the wing to fuselage fairing (Refer to AMM Task

53-35-11-400-801).

8 If removed install access panels (Refer to AMM Task 57-41-37-400-801).

9 If removed install fairing panels (Refer to AMM Task 53-35-13-400-801).

10 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

11 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the avionics compartment door 132AZ.

(d) Close the forward and aft cargo compartment door 821 and 822 (Refer to AMM

Task 52-30-00-410-801).

1 Remove the safety lock (Refer to AMM Task 52-30-00-080-801).

(e) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(f) Restore the systems and the aircraft to normal operating condition.

(g) Remove the access platform.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 368

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@A330

SERVICE BULLETIN

**CONF 018

(1) Subtask 533183-942-001-001 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

Task 52-30-00-080-801

Task 52-30-00-410-801

Task 53-35-11-400-801

Task 53-35-13-400-801

Task 57-17-11-400-801

Task 57-41-37-400-801

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

equipment.

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the wing to fuselage fairing (Refer to AMM Task

53-35-11-400-801).

2 If removed install access panels (Refer to AMM Task 57-41-37-400-801).

3 If removed install fairing panels (Refer to AMM Task 53-35-13-400-801).

4 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the avionics compartment door 132AZ.

(d) Close the forward 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).

(e) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(f) Restore the systems and the aircraft to normal operating condition.

(g) Remove the access platform.

**CONF 019

(1) Subtask 533183-942-001-018 - Close-up

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 369

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

Task 52-30-00-080-801

Task 52-30-00-410-801

Task 53-35-11-400-801

Task 53-35-13-400-801

Task 57-17-11-400-801

Task 57-27-11-400-801

Task 57-41-37-400-801

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

equipment.

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the wing to fuselage fairing (Refer to AMM Task

53-35-11-400-801).

2 If removed install access panels (Refer to AMM Task 57-41-37-400-801).

3 If removed install fairing panels (Refer to AMM Task 53-35-13-400-801).

4 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

5 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the avionics compartment door 132AZ.

(d) Close the forward 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).

(e) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(f) Restore the systems and the aircraft to normal operating condition.

(g) Remove the access platform.

**CONF 020

(1) Subtask 533183-942-001-001 - Close-up

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 370

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

Task 52-30-00-080-801

Task 52-30-00-410-801

Task 53-35-11-400-801

Task 53-35-13-400-801

Task 57-17-11-400-801

Task 57-41-37-400-801

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

equipment.

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the wing to fuselage fairing (Refer to AMM Task

53-35-11-400-801).

2 If removed install access panels (Refer to AMM Task 57-41-37-400-801).

3 If removed install fairing panels (Refer to AMM Task 53-35-13-400-801).

4 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the avionics compartment door 132AZ.

(d) Close the forward 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).

(e) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(f) Restore the systems and the aircraft to normal operating condition.

(g) Remove the access platform.

**CONF 021

(1) Subtask 533183-942-001-013 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 371

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@A330

SERVICE BULLETIN

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

2 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(d) Restore the systems and the aircraft to normal operating condition.

(e) Remove the access platform.

**CONF 022

(1) Subtask 533183-942-001-007 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

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) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

2 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(d) Restore the systems and the aircraft to normal operating condition.

(e) Remove the access platform.

**CONF 023

(1) Subtask 533183-942-001-011 - Close-up

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 372

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

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) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

2 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(d) Restore the systems and the aircraft to normal operating condition.

(e) Remove the access platform.

**CONF 024

(1) Subtask 533183-942-001-023 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

Task 52-30-00-080-801

Task 52-30-00-410-801

Task 53-35-11-400-801

Task 53-35-13-400-801

Task 57-17-11-400-801

Task 57-27-11-400-801

Task 57-41-37-400-801

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

equipments

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install fairing panels (Refer to AMM Task 53-35-13-400-801).

2 If removed install the wing to fuselage fairing (Refer to AMM Task

53-35-11-400-801).

3 If removed install access panels (Refer to AMM Task 57-41-37-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 373

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@A330

SERVICE BULLETIN

4 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

5 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the forward 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) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(e) Restore the systems and the aircraft to normal operating condition.

(f) Remove the access platform.

**CONF 025

(1) Subtask 533183-942-001-011 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

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) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

2 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(d) Restore the systems and the aircraft to normal operating condition.

(e) Remove the access platform.

**CONF 026

(1) Subtask 533183-942-001-006 - Close-up

Manpower Resources

Skills AIRFRAME

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 374

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@A330

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

Task 57-17-11-400-801

Task 57-27-11-400-801

Task 57-41-37-400-801

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

equipment.

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install access panels (Refer to AMM Task 57-41-37-400-801).

2 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

3 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the avionics compartment door 132AZ.

(d) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(e) Restore the systems and the aircraft to normal operating condition.

(f) Remove the access platform.

**CONF 027

(1) Subtask 533183-942-001-026 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

Task 52-30-00-080-801

Task 52-30-00-410-801

Task 53-35-11-400-801

Task 53-35-13-400-801

Task 57-17-11-400-801

Task 57-27-11-400-801

Task 57-41-37-400-801

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

equipment.

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install fairing panels (Refer to AMM Task 53-35-13-400-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 375

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@A330

SERVICE BULLETIN

2 If removed install the wing to fuselage fairing (Refer to AMM Task

53-35-11-400-801).

3 If removed install access panels (Refer to AMM Task 57-41-37-400-801).

4 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

5 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the forward 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) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(e) Restore the systems and the aircraft to normal operating condition.

(f) Remove the access platform.

**CONF 028

(1) Subtask 533183-942-001-006 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

Task 57-17-11-400-801

Task 57-27-11-400-801

Task 57-41-37-400-801

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

equipment.

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install access panels (Refer to AMM Task 57-41-37-400-801).

2 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

3 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the avionics compartment door 132AZ.

(d) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 376

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@A330

SERVICE BULLETIN

(e) Restore the systems and the aircraft to normal operating condition.

(f) Remove the access platform.

**CONF 029

(1) Subtask 533183-942-001-028 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-801

Task 52-30-00-080-801

Task 52-30-00-410-801

Task 53-12-13-400-801

Task 53-35-11-400-801

Task 53-35-13-400-801

Task 57-17-11-400-801

Task 57-27-11-400-801

Task 57-41-37-400-801

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

equipment.

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 Test Job Set-up .

1 If removed install the wing to fuselage fairing (Refer to AMM Task

53-35-11-400-801).

2 If removed install access panels (Refer to AMM Task 57-41-37-400-801).

3 If removed install fairing panels (Refer to AMM Task 53-35-13-400-801).

4 If removed install the floor panel and assy panel in electronic compartment

FR20 (Refer to AMM Task 53-12-13-400-801).

5 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

6 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the avionics compartment door 132AZ.

(d) Close access door Z811.

(e) Close the forward 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).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 377

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SERVICE BULLETIN

(f) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

(g) Restore the systems and the aircraft to normal operating condition.

(h) Remove the access platform.

**CONF 030

(1) Subtask 533183-942-001-029 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-23-41-400-801

Task 25-24-61-400-801

Task 25-52-00-400-801

Task 25-53-00-400-801

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 53-00-00-400-802

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

equipment.

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 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 If removed install cargo floor panel (Refer to AMM Task 53-00-00-400-802).

3 If removed install forward cargo sidewall panel (Refer to AMM Task

25-52-00-400-801).

4 If removed install after cargo sidewall panel (Refer to AMM Task

25-53-00-400-801).

5 If removed, install the overhead stowage-compartments at FR38 and/or FR54

(Refer to AMM Task 25-24-61-400-801).

6 If removed install upper ceiling panels .(Refer to AMM Task

25-23-41-400-801).

(c) Close the forward and aft cargo compartment door821 and 822 (Refer to AMM

Task 52-30-00-410-801).

1 Remove the safety lock (Refer to AMM Task 52-30-00-080-801).

(d) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 378

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SERVICE BULLETIN

(e) Restore the systems and the aircraft to normal operating condition.

(f) Remove the access platform.

**CONF 031

(1) Subtask 533183-942-001-030 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-23-41-400-801

Task 25-23-43-400-802

Task 25-23-61-400-801

Task 25-24-61-400-801

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 53-00-00-400-803

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

equipment.

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 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 If removed install cargo floor panel (Refer to (Refer to AMM Task

53-00-00-400-803).

3 If removed install cargo sidewall panel (Refer to AMM Task

25-52-00-400-801).

4 If removed install sidewall panel (Refer to AMM Task 25-23-43-400-802).

5 If removed, install the overhead stowage-compartments at FR38 and/or FR54

(Refer to AMM Task 25-24-61-400-801).

6 If removed install light covers (Refer to AMM Task 25-23-61-400-801).

7 If removed install ceiling panels (Refer to AMM Task 25-23-41-400-801).

(c) Close the forward and aft cargo compartment door 821 and 822 (Refer to AMM

Task 52-30-00-410-801).

1 Remove the safety lock (Refer to AMM Task 52-30-00-080-801).

(d) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 379

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@A330

SERVICE BULLETIN

(e) Restore the systems and the aircraft to normal operating condition.

(f) Remove the access platform.

**CONF 032

(1) Subtask 533183-942-001-031 - Close-up

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) 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 25-51-41-400-801

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 53-00-00-400-802

Task 53-00-00-400-803

Task 53-35-11-400-801

Task 53-35-13-400-801

Task 57-17-11-400-801

Task 57-27-11-400-801

Task 57-41-37-400-801

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

equipment.

(b) Parts and/or equipment removed for access, to be installed before SUBTASK

533183-941-002 033 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 If removed install forward cargo floor panel (Refer to AMM Task

53-00-00-400-802).

3 If removed install after cargo floor panel (Refer to AMM Task

53-00-00-400-803).

4 If removed install cargo sidewall panels (Refer to AMM Task

25-52-00-400-801)

5 If removed install dado panels (Refer to AMM Task 25-23-44-400-801).

6 If removed install sidewall panels (Refer to AMM Task 25-23-43-400-802).

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 380

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SERVICE BULLETIN

7 If removed, install the overhead stowage-compartments at FR38 and/or FR54

(Refer to AMM Task 25-24-61-400-801).

8 If removed install light covers (Refer to AMM Task 25-23-61-400-801).

9 If removed install ceiling panels (Refer to AMM Task 25-23-41-400-801).

10 If removed install the passenger seats (Refer to AMM Task

25-51-41-400-801).

11 If removed install the wing to fuselage fairing (Refer to AMM Task

53-35-11-400-801).

12 If removed install access panels (Refer to AMM Task 57-41-37-400-801).

13 If removed install fairing panels (Refer to AMM Task 53-35-13-400-801).

14 If removed install the fuel tank access panels (Refer to AMM Task

57-27-11-400-801).

15 If removed install the fuel tank access covers (Refer to AMM Task

57-17-11-400-801).

(c) Close the avionics compartment door 132AZ.

(d) Close access door Z811.

(e) Close the forward and aft cargo compartment door 821 and 822 (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) Restore the systems and the aircraft to normal operating condition.

(h) Remove the access platform.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 381

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@A330

SERVICE BULLETIN

**CONF ALL

NO FURTHER ACTION

QUESTION

ACTION

FINDING

PERFORM DETAILED INSPECTION OF NUTS

P/N ASNA2531−4 AT THRESHOLD GIVEN IN THE

PLANNING INFORMATION PARAGRAPH E.(2)

NUT MISSING

SEND INSPECTION

REPORT TO AIRBUS

REPLACE THE NUT BEFORE NEXT FLIGHT AS

DESCRIBED IN THE MODIFICATION TASK

533183−831−801−001 AND IN REPAIR DRAWING R51415002

INFORM AIRBUS

BEFORE NEXT FLIGHT

NO NUT CRACKED YES

NO YES

FILL THE TABLE OF INSPECTION

REPORT IN CASE OF FINDING(S)

CONTACT AIRBUS

BEFORE NEXT FLIGHT

FOR FURTHER INSTRUCTIONS

G_SB_533183_5_BCAA_01_02

Figure A-FBCAA - Sheet 01

Flow Chart

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 382

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@A330

SERVICE BULLETIN

Appendix 01 Inspection Report

**CONF ALL

The results of the inspection, including no finding, replacement or action to be done, must be forwarded

to Airbus department SEES1, on the attached inspection report sheet

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 1

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@A330

SERVICE BULLETIN

Appendix 01 Inspection Report

**CONF ALL

INSPECTION REPORT

SERVICE BULLETIN No. : A330−53−3183

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

G_SB_533183_5_AAAA_01_01

NO MISSING NUT AND NO CRACKED NUT (IN CASE OF FINDING(S) FILL THE TABLE BELOW)

Figure A-FAAAA - Sheet 01

Inspection Report

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 2

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@A330

SERVICE BULLETIN

Appendix 02 Elapsed Time Assumptions

**CONF ALL

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 1

5

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@A330

SERVICE BULLETIN

Appendix 02 Elapsed Time Assumptions

**CONF 001, 004, 018, 020

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−53−3183

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)

306.50

106.00

STEPS

136.00 45.00 4

0 49 106

INSPECTION 4.00 1.00 4

0.50 0.50 1

6.00 6.00 1

2.50 2.50 1

1.50 1.50 1

0.50 0.50 1

0.50 0.50 1

1.00 1.00 1

TEST 4.00 4.00 1

CLOSE UP 150.00 50.00 4

NUT REPLACEMENT IN

AREA 1A

NUT REPLACEMENT IN

AREA 2A

NUT REPLACEMENT IN

AREA 2B

NUT REPLACEMENT IN

AREA 2C

NUT REPLACEMENT IN

AREA 3

NUT REPLACEMENT IN

AREA 19

NUT REPLACEMENT IN

AREA 20

1 43 44 45 46 47 48 50 51 52 53 54 55 104 105

G_SB_533183_5_ABAA_01_01

56 57

Figure A-FABAA - Sheet 01

Elapsed Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 2

5

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@A330

SERVICE BULLETIN

Appendix 02 Elapsed Time Assumptions

**CONF 002

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−53−3183

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)

45.75

30.50

STEPS

19.25 13.00 2

0

INSPECTION 1.00 0.50 2

1.00 1.00 1

0.50 0.50 1

TEST 1.00 1.00 1

CLOSE UP 23.00 15.00 2

NUT REPLACEMENT IN

AREA C4 CONCESSION 1

NUT REPLACEMENT IN

AREA C5 CONCESSION 2

1 10

G_SB_533183_5_ABAB_01_00

2 3 4 5 6 7 8 9 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31

Figure A-FABAB - Sheet 01

Elapsed Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 3

5

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@A330

SERVICE BULLETIN

Appendix 02 Elapsed Time Assumptions

**CONF 003

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−53−3183

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)

331.00

116.00

STEPS

147.50 50.00 4

0 54 116

INSPECTION 4.00 1.00 4

0.50 0.50 1

6.00 6.00 1

2.50 2.50 1

1.50 1.50 1

1.50 1.50 1

1.00 1.00 1

0.50 0.50 1

TEST 4.00 4.00 1

CLOSE UP 162.00 55.00 4

NUT REPLACEMENT IN

AREA 1A

NUT REPLACEMENT IN

AREA 2A

NUT REPLACEMENT IN

AREA 2B

NUT REPLACEMENT IN

AREA 2C

NUT REPLACEMENT IN

AREA 3

NUT REPLACEMENT IN

AREA 20

NUT REPLACEMENT IN

AREA C3 CONCESSION 1

1 48 49 50 51 52 53 55 56 57 58 59 60 114 115

G_SB_533183_5_ABAC_01_01

61 62

Figure A-FABAC - Sheet 01

Elapsed Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 4

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@A330

SERVICE BULLETIN

Appendix 02 Elapsed Time Assumptions

**CONF 005

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−53−3183

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)

43.00

26.00

STEPS

16.50 10.00 2

0

INSPECTION 2.00 1.00 2

0.50 0.50 1

1.50 1.50 1

0.50 0.50 1

1.00 1.00 1

0.50 0.50 1

TEST 1.00 1.00 1

CLOSE UP 19.50 12.00 2

NUT REPLACEMENT IN

AREA 1A

NUT REPLACEMENT IN

AREA 3

NUT REPLACEMENT IN

AREA 19

NUT REPLACEMENT IN

AREA 20

NUT REPLACEMENT IN

AREA C3 CONCESSION 1

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26

G_SB_533183_5_ABAD_01_00

Figure A-FABAD - Sheet 01

Elapsed Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 5

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@A330

SERVICE BULLETIN

Appendix 02 Elapsed Time Assumptions

**CONF 007 thru 010, 022

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−53−3183

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)

35.75

23.00

STEPS

11.75 8.00 2

0

INSPECTION 1.00 0.50 2

1.50 1.50 1

1.00 1.00 1

TEST 1.00 1.00 1

CLOSE UP 19.50 12.00 2

NUT REPLACEMENT IN

AREA 3

NUT REPLACEMENT IN

AREA 20

23

G_SB_533183_5_ABAE_01_00

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22

Figure A-FABAE - Sheet 01

Elapsed Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 6

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@A330

SERVICE BULLETIN

Appendix 02 Elapsed Time Assumptions

**CONF 011 thru 012, 023, 025

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−53−3183

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)

30.50

20.00

STEPS

11.75 8.00 2

0

INSPECTION 1.00 0.50 2

1.50 1.50 1

1.00 1.00 1

TEST 1.00 1.00 1

CLOSE UP 13.75 9.00 2

NUT REPLACEMENT IN

AREA 3

NUT REPLACEMENT IN

AREA 20

20

G_SB_533183_5_ABAF_01_00

NUT REPLACEMENT IN 0.50 0.50 1

AREA 19

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19

Figure A-FABAF - Sheet 01

Elapsed Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 7

5

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@A330

SERVICE BULLETIN

Appendix 02 Elapsed Time Assumptions

**CONF 013 thru 015, 021

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−53−3183

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)

13.00

13.00

STEPS

5.00 5.00 1

0

INSPECTION 0.50 0.50 1

0.50 0.50 1

CLOSE UP 6.00 6.00 1

NUT REPLACEMENT IN

AREA 19

TEST 1.00 1.00 1

G_SB_533183_5_ABAG_01_00

1 2 3 4 5 6 7 8 9 10 11 12 13

Figure A-FABAG - Sheet 01

Elapsed Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 8

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@A330

SERVICE BULLETIN

Appendix 02 Elapsed Time Assumptions

**CONF 006, 026, 028

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−53−3183

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)

41.00

25.00

STEPS

16.50 10.00 2

0

INSPECTION 1.00 0.50 2

0.50 0.50 1

1.00 1.00 1

TEST 1.00 1.00 1

CLOSE UP 19.50 12.00 2

NUT REPLACEMENT IN

AREA 1

NUT REPLACEMENT IN

AREA 20

25

NUT REPLACEMENT IN 1.50 1.50 1

AREA 3

G_SB_533183_5_ABAH_01_00

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24

Figure A-FABAH - Sheet 01

Elapsed Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 9

5

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@A330

SERVICE BULLETIN

Appendix 02 Elapsed Time Assumptions

**CONF 017

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−53−3183

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)

307.50

106.00

STEPS

136.00 45.00 4

0 49 106

INSPECTION 4.00 1.00 4

0.50 0.50 1

6.00 6.00 1

2.50 2.50 1

1.50 1.50 1

1.50 1.50 1

1.00 1.00 1

0.50 0.50 1

TEST 4.00 4.00 1

CLOSE UP 150.00 50.00 4

NUT REPLACEMENT IN

AREA 1A

NUT REPLACEMENT IN

AREA 2A

NUT REPLACEMENT IN

AREA 2B

NUT REPLACEMENT IN

AREA 2C

NUT REPLACEMENT IN

AREA 3

NUT REPLACEMENT IN

AREA 20

NUT REPLACEMENT IN

AREA C2 CONCESSION 1

1 43 44 45 46 47 48 50 51 52 53 54 55 104 105

G_SB_533183_5_ABAI_01_01

56 57

Figure A-FABAI - Sheet 01

Elapsed Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 10

5

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@A330

SERVICE BULLETIN

Appendix 02 Elapsed Time Assumptions

**CONF 019

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−53−3183

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)

131.00

44.00

STEPS

51.00 17.00 4

0 21 44

INSPECTION 4.00 1.00 4

0.50 0.50 1

6.00 6.00 1

2.50 2.50 1

1.50 1.50 1

1.50 1.50 1

1.00 1.00 1

TEST 1.00 1.00 1

CLOSE UP 62.00 19.00 4

NUT REPLACEMENT IN

AREA 1A

NUT REPLACEMENT IN

AREA 2A

NUT REPLACEMENT IN

AREA 2B

NUT REPLACEMENT IN

AREA 2C

NUT REPLACEMENT IN

AREA 3

NUT REPLACEMENT IN

AREA 20

1 2 15 16 17 18 19 20 22 23 24 25 26 27 42 43

G_SB_533183_5_ABAJ_01_00

Figure A-FABAJ - Sheet 01

Elapsed Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 11

5

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@A330

SERVICE BULLETIN

Appendix 02 Elapsed Time Assumptions

**CONF 024

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−53−3183

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)

36.50

23.00

STEPS

12.00 8.00 2

0

INSPECTION 1.00 0.50 2

1.50 1.50 1

1.00 1.00 1

TEST 1.00 1.00 1

CLOSE UP 19.50 12.00 2

NUT REPLACEMENT IN

AREA 3

NUT REPLACEMENT IN

AREA 20

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23

G_SB_533183_5_ABAK_01_00

NUT REPLACEMENT IN 0.50 0.50 1

AREA C1 CONCESSION 1

Figure A-FABAK - Sheet 01

Elapsed Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 12

5

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@A330

SERVICE BULLETIN

Appendix 02 Elapsed Time Assumptions

**CONF 027

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−53−3183

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)

43.50

27.00

STEPS

16.50 10.00 2

0

INSPECTION 2.00 1.00 2

0.50 0.50 1

1.50 1.50 1

1.00 1.00 1

0.50 0.50 1

TEST 2.00 2.00 1

CLOSE UP 19.50 12.00 2

NUT REPLACEMENT IN

AREA 1A

NUT REPLACEMENT IN

AREA 3

NUT REPLACEMENT IN

AREA 20

NUT REPLACEMENT IN

AREA C2 CONCESSION 1

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26

G_SB_533183_5_ABAL_01_01

27

Figure A-FABAL - Sheet 01

Elapsed Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 13

5

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@A330

SERVICE BULLETIN

Appendix 02 Elapsed Time Assumptions

**CONF 029

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−53−3183

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)

316.00

106.00

STEPS

139.00 45.00 4

0 49 106

INSPECTION 4.00 1.00 4

0.50 0.50 1

0.50 0.50 1

6.00 6.00 1

2.50 2.50 1

1.50 1.50 1

1.50 1.50 1

1.00 1.00 1

TEST 4.00 4.00 1

CLOSE UP 155.00 50.00 4

NUT REPLACEMENT IN

AREA 1A

NUT REPLACEMENT IN

AREA 1B

NUT REPLACEMENT IN

AREA 2A

NUT REPLACEMENT IN

AREA 2B

NUT REPLACEMENT IN

AREA 2C

NUT REPLACEMENT IN

AREA 3

NUT REPLACEMENT IN

AREA 20

1 43 44 45 46 47 48 50 51 52 53 54 55 104 105

NUT REPLACEMENT IN 0.50 0.50 1

AREA 19

G_SB_533183_5_ABAM_01_01

56 57

Figure A-FABAM - Sheet 01

Elapsed Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 14

5

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@A330

SERVICE BULLETIN

Appendix 02 Elapsed Time Assumptions

**CONF 030

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−53−3183

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)

35.00

21.00

STEPS

15.00 9.00 2

0

INSPECTION 1.00 0.50 2

0.50 0.50 1

0.50 0.50 1

TEST 1.00 1.00 1

CLOSE UP 17.00 10.00 2

NUT REPLACEMENT IN

AREA C4 CONCESSION 1

NUT REPLACEMENT IN

AREA C5 CONCESSION 1

1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21

G_SB_533183_5_ABAN_01_00

Figure A-FABAN - Sheet 01

Elapsed Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 15

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Appendix 02 Elapsed Time Assumptions

**CONF 031

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−53−3183

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)

55.50

35.00

STEPS

24.50 15.00 2

0

INSPECTION 1.00 0.50 2

0.50 0.50 1

1.00 1.00 1

TEST 1.00 1.00 1

CLOSE UP 27.00 17.00 2

NUT REPLACEMENT IN

AREA C4 CONCESSION 2

NUT REPLACEMENT IN

AREA C5 CONCESSION 3

1 2 3 4 5 6 7 8 9 10 11 12 13

NUT REPLACEMENT IN 0.50 0.50 1

AREA C6 CONCESSION 1

G_SB_533183_5_ABAO_01_00

14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35

Figure A-FABAO - Sheet 01

Elapsed Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 16

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330

SERVICE BULLETIN

Appendix 02 Elapsed Time Assumptions

**CONF 032

ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A330−53−3183

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)

396.00

136.00

STEPS

176.00 60.00 4

0 64 136

INSPECTION 4.00 1.00 4

0.50 0.50 1

6.00 6.00 1

2.50 2.50 1

1.50 1.50 1

1.50 1.50 1

1.50 1.50 1

2.00 2.00 1

TEST 4.00 4.00 1

CLOSE UP 195.00 65.00 4

NUT REPLACEMENT IN

AREA 1A

NUT REPLACEMENT IN

AREA 2A

NUT REPLACEMENT IN

AREA 2B

NUT REPLACEMENT IN

AREA 2C

NUT REPLACEMENT IN

AREA 3

NUT REPLACEMENT IN

AREA 19

NUT REPLACEMENT IN

AREA C4 CONCESSION 1

1 58 59 60 61 62 63 65 66 67 68 69 70 134 135

NUT REPLACEMENT IN 1.00 1.00 1

AREA 20

NUT REPLACEMENT IN 0.50 0.50 1

AREA C5 CONCESSION 2

G_SB_533183_5_ABAP_01_01

71 72

Figure A-FABAP - Sheet 01

Elapsed Time Assumptions

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 17

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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: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 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

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Comments:

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Please return this form to:

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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: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183

REVISION No.: 00 - Sep 30/10 Page: 1

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