# @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. 

# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 53 

### TITLE: FUSELAGE - GENERAL - INSPECTION OF SUSPECTED NON CONFORMING NUTS ASNA2531-4 **CONF ALL MODIFICATIONS None REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES During structural parts assembly on the production line, some nuts were detected cracked. An investigation was immediately launched to determine the affected nut types and the associated batches. AIRBUS and the nut manufacturer, LISI Monadnock, have identified that the affected nut type is ASNA2531-4. These suspected non conforming nuts have been installed in production on aircraft listed in effectivity paragraph. Extensive static, fatigue and corrosion 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 5

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# @A330
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 REVISION No.: 00 - Sep 30/10 Page: 2 5

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# @A330
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 REVISION No.: 00 - Sep 30/10 Page: 3 5

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# @A330
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 REVISION No.: 00 - Sep 30/10 Page: 4 5

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# @A330
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 REVISION No.: 00 - Sep 30/10 Page: 5 5

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# @A330
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 REVISION No.: 00 - Sep 30/10 Page: 6 5

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# @A330
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 REVISION No.: 00 - Sep 30/10 Page: 7 5

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# @A330
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 REVISION No.: 00 - Sep 30/10 Page: 8 5

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# @A330
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 REVISION No.: 00 - Sep 30/10 Page: 9 5

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# @A330
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 REVISION No.: 00 - Sep 30/10 Page: 10 5

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# @A330
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 REVISION No.: 00 - Sep 30/10 Page: 11 5

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# @A330
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 REVISION No.: 00 - Sep 30/10 Page: 12 5

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# @A330
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 REVISION No.: 00 - Sep 30/10 Page: 13 5

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# @A330
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 5

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# @A330
SERVICE BULLETIN

AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 53 

### TITLE: FUSELAGE - GENERAL - INSPECTION OF SUSPECTED NON CONFORMING NUTS ASNA2531-4 MODIFICATION No.: None This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY The equivalent of this Service Bulletin has been 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 REVISION No.: 00 - Sep 30/10 Page: 1 5

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# @A330
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 REVISION No.: 00 - Sep 30/10 Page: 2 5

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# @A330
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 REVISION No.: 00 - Sep 30/10 Page: 3 5

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# @A330
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 REVISION No.: 00 - Sep 30/10 Page: 4 5

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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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 5 5

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# @A330
SERVICE BULLETIN

**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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 6 5

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# @A330
SERVICE BULLETIN

**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 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

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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 8 5

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# @A330
SERVICE BULLETIN

**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 REVISION No.: 00 - Sep 30/10 Page: 9 5

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# @A330
SERVICE BULLETIN

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 andanalysis 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 :

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

**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 REVISION No.: 00 - Sep 30/10 Page: 11 5

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# @A330
SERVICE BULLETIN

**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 REVISION No.: 00 - Sep 30/10 Page: 12 5

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SERVICE BULLETIN
(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 REVISION No.: 00 - Sep 30/10 Page: 13 5

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# @A330
SERVICE BULLETIN
(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
DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 14 5

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SERVICE BULLETIN
(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 5

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# @A330
SERVICE BULLETIN

**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 REVISION No.: 00 - Sep 30/10 Page: 16 5

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# @A330
SERVICE BULLETIN

**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 REVISION No.: 00 - Sep 30/10 Page: 17 5

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# @A330
SERVICE BULLETIN
(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 18 5

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# @A330
SERVICE BULLETIN

**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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 19 5

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# @A330
SERVICE BULLETIN
**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 underEASA Design Organisation Approval No. EASA21J.031. If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin.
DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 20 5

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# @A330
SERVICE BULLETIN

G. MANPOWER The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit operator’s circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying times for paints, sealants, etc., and general administration work are also not included. **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 DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 21 5

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# @A330
SERVICE BULLETIN

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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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# @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

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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 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

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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 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

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# @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

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# @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

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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 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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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

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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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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

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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

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This Page Intentionally Left Blank

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2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Component COMPA01 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 INFORMATIONAIRBUS will credit the manhours indicated in this Service Bulletin at the operator’s agreed inhouse warranty labor rate as well as the material costs for claims received not later than 90 days after completion of the last affected aircraft of your fleet. C. LIST OF COMPONENTS No Kit

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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.

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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

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NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. Component 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.

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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

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NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. Component 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.

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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

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NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. (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

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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

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**CONF 003 Zone 100 120 130 140 150 190 260 540 640Access 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

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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
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**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
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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
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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

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**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 5

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# @A330
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 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: 63 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 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 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 533183-832-001 002 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 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 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

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: 111 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 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

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 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

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 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 5

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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 5

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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 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 5

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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 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 5

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# @A330
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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 REVISION No.: 00 - Sep 30/10 Page: 128 5

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# @A330
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 5

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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 5

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# @A330
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 5

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# @A330
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 5

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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 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 5

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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). (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 5

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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 5

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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 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 5

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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 5

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# @A330
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 5

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# @A330
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(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 5

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# @A330
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 5

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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 5

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# @A330
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(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 5

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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 5

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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 5

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# @A330
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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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# @A330
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 5

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# @A330
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 REVISION No.: 00 - Sep 30/10 Page: 153 5

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# @A330
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 5

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# @A330
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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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# @A330
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 5

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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 5

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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 5

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

# @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 5

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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 5

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

# @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 5

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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 5

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

# @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 5

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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 5

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

# @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 5

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# @A330
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 5

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# @A330
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 5

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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) 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 5

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# @A330
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 5

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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 5

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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 5

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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 5

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# @A330
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 5

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# @A330
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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 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 5

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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 533183-960-003-001 - 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: 183 5

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# @A330
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 REVISION No.: 00 - Sep 30/10 Page: 184 5

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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

(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 5

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# @A330
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 5

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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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas C4 concession 1 DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 187 5

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# @A330
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 5

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# @A330
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 5

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# @A330
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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 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 5

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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: 191 5

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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: 192 5

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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: 193 5

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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 533183-960-008-001 - 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 5

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# @A330
SERVICE BULLETIN
(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 5

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# @A330
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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 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 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: 197 5

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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 5

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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 5

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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 5

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# @A330
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 5

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# @A330
SERVICE BULLETIN
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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 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 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 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 5

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# @A330
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 5

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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 5

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# @A330
SERVICE BULLETIN
(a) Perform a visual inspection of the nuts looking for cracked or missing nuts as described inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 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 5

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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 5

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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 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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 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

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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: 210 5

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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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 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

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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 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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 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

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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: 217 5

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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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on area C7.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 224 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 533183-960-007-001 - 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 5

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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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on 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 5

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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 5

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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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on 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 5

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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 5

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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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 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 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: 231 5

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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 5

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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 5

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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 5

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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 5

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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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 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 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: 237 5

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

# @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 5

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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 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

(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 5

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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 5

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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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 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

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

# @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 5

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

# @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 5

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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 5

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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 5

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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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 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 5

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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: 248 5

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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 5

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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: 250 5

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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 5

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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 5

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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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on 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 5

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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 5

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SERVICE BULLETIN
(a) Perform a visual inspection of the nuts looking for cracked or missing nuts as described inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 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 5

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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 5

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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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 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 5

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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 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 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 5

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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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 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 5

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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 5

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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 5

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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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 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 5

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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 5

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

# @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 5

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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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 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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- 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 5

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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 5

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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 inFig. 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 5

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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 5

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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 5

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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 5

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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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 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 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 533183-960-001-001 - 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 5

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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 5

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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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 1b, 2a, 2b, 2c, 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 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 533183-960-001-001 - 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 5

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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 5

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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 5

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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 5

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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 5

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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 inFig. 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 5

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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 5

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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 5

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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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 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 5

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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 5

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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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 287 5

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# @A330
SERVICE BULLETIN
(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 inFig. A-FBCAA

. 1 In case of missing nut, contact Airbus before next flight for additional instructions. 2 In case of cracked nut, inform Airbus and perform nut replacement before next flight. NOTE: This inspection must be performed on areas 1a, 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 DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 288 5

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# @A330
SERVICE BULLETIN
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
DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 289 5

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# @A330
SERVICE BULLETIN
(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 290 5

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# @A330
SERVICE BULLETIN
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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 291 5

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# @A330
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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 292 5

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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 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.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 293 5

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# @A330
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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 294 5

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# @A330
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 .

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 295 5

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# @A330
SERVICE BULLETIN
(a) In the cockpit, on the panel 235VU, push the push-button switches : - BAT 1, BAT 2, APU BAT ; - GEN 1, (2, 3, 4), APU GEN ; - EXT A (B). (b) Remove the warning notices. (c) Energize the aircraft electrical circuits (Refer to AMM Task 24-41-00-861-801) (2) Subtask 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 REVISION No.: 00 - Sep 30/10 Page: 296 5

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# @A330
SERVICE BULLETIN
(c) Do the operational test of lights (Refer to AMM Task 33-14-00-710-801). (d) Do the operational test of the avionics-equipment ventilation system (Refer to AMM Task 21-26-00-710-803). (e) Do the BITE test of the auto flight system (SYSTEM TEST) (Refer to AMM Task 22-96-00-740-801). (f) Do the operational test of the ECAM control panel (Refer to AMM Task 31-50-00-710-803). (g) Do the test of FWS (Refer to AMM Task 31-50-00-740-801). (h) Do the operational test of EIS (Refer to AMM Task 31-60-00-710-802). (4) Subtask 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. DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 297 5

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# @A330
SERVICE BULLETIN
(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). DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 298 5

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# @A330
SERVICE BULLETIN
(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

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 299 5

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# @A330
SERVICE BULLETIN
(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: 300 5

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# @A330
SERVICE BULLETIN
(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 REVISION No.: 00 - Sep 30/10 Page: 301 5

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# @A330
SERVICE BULLETIN
(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 5

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# @A330
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 5

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# @A330
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 5

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# @A330
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 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: 306 5

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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 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 533183-700-002-006 - 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 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 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 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 533183-700-002-006 - 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 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 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 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 533183-700-002-006 - 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 5

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

# @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 5

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

# @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: 314 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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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 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 533183-700-002-013 - 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 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 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 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 533183-700-002-014 - 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 5

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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 5

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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 5

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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 5

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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 5

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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 5

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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 systemsand 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 5

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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 5

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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 5

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

# @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 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 systemsand 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 systemsand 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 5

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

# @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 systemsand 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 5

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

# @A330
SERVICE BULLETIN
(c) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801). (d) Restore the systemsand 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 systemsand 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 5

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

# @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 systemsand 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 systemsand 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 5

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

# @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 systemsand 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 systemsand 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 5

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

# @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 systemsand 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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 5

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

# @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 systemsand 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 systemsand 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 5

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

# @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 systemsand 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 5

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

# @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 systemsand 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 systemsand 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 5

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

# @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 systemsand 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 5

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

# @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 systemsand 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 5

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

# @A330
SERVICE BULLETIN
(e) Restore the systemsand 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 5

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# @A330
SERVICE BULLETIN
(f) Close the passenger/crew door 831 (Refer to AMM Task 52-10-00-410-801). (g) Restore the systemsand 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 5

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# @A330
SERVICE BULLETIN
(e) Restore the systemsand 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 5

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# @A330
SERVICE BULLETIN
(e) Restore the systemsand 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 5

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# @A330
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 systemsand 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 5

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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 NUT CRACKED NO YES YES NO

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 5

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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 5

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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 5

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

# @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

49 106 0 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

46 45 47 48 50 51 52 53 44 43 55 54 1 105 104

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

10 1

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

54 116 0 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

51 50 52 53 55 56 57 58 49 48 60 59 1 115 114

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 5

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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

26 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

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 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 22 21 20 19 18 17 16 15 14 13 12 11 10

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 5

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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 0.50 0.50 1 NUT REPLACEMENT IN AREA 19

1 2 3 4 5 6 7 8 9 19 18 17 16 15 14 13 12 11 10

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

1.00 1.00 1 TEST

G_SB_533183_5_ABAG_01_00 8 7 6 5 4 3 2 1 10 11 12 13 9

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 5

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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 1.50 1.50 1 NUT REPLACEMENT IN AREA 3

G_SB_533183_5_ABAH_01_00 1 2 3 4 5 6 7 8 9 24 23 22 21 20 19 18 17 16 15 14 13 12 11 10

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

49 106 0 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

46 45 47 48 50 51 52 53 44 43 55 54 1 105 104

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

21 44 0 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

18 17 19 20 22 23 24 25 16 15 27 26 1 2 43 42

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

23 1 2 3 4 5 6 7 8 9 22 21 20 19 18 17 16 15 14 13 12 11 10

G_SB_533183_5_ABAK_01_00 0.50 0.50 1 NUT REPLACEMENT IN 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

26 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

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

49 106 0 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

46 45 47 48 50 51 52 53 44 43 55 54 1 105 104 0.50 0.50 1 NUT REPLACEMENT IN 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 21 20 19 18 17 16 15 14 13 12 11 10

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

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# @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 13 12 11 10 0.50 0.50 1 NUT REPLACEMENT IN 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

64 136 0 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

61 60 62 63 65 66 67 68 59 58 70 69 1 135 134 1.00 1.00 1 NUT REPLACEMENT IN AREA 20

0.50 0.50 1 NUT REPLACEMENT IN 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 5

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# @A330
SERVICE BULLETIN REPORTING SHEET 

### TITLE: FUSELAGE - GENERAL - INSPECTION OF SUSPECTED NON CONFORMING NUTS ASNA2531-4 MODIFICATION No.: None Please complete the appropriate item (A or B): A - SB WILL BEembodied YES/NO (if NO please comment) If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiment:

B - SB HAS BEENembodied on aircraft: Operator comments:

From Airline: Name/Title: Signature: Date: If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next normal revision or prior to SB embodiment, please indicate required service(s): Either: Modification Operational Impact (MOI), if available YES/NO Or : Intermediate revision YES/NO Important Information: This SB will only be incorporated in your maintenance and operational documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in - Updating of maintenance documentation to show pre and post SB data. - Updating of maintenance and operational documentation to show post SB data after embodiment. If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include them in the manual revisions. Refer to SIL 00-037 for detailed information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 93 28 06 e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, SB lists via letters or fax are also accepted.

DATE: 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 QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4 3 2 1 - Quality rating of the Accomplishment Instructions 4 3 2 1 - Quality rating of the Illustrations 4 3 2 1 - Is this SB easy to understand ? Y / N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations
Comments:

Operator: Date: Name/Title: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.

DATE: Sep 30/10 SERVICE BULLETIN No.: A330-53-3183 REVISION No.: 00 - Sep 30/10 Page: 1 5

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