@A330

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 78

TITLE: EXHAUST - THRUST REVERSER OPENING MECHANISM - INSPECT

REAR HINGE LUGS OF R.R. THRUST REVERSER.

MODIFICATION No.: None

This page transmits Revision No.09 of Service Bulletin No.A330-78-3006

ADDITIONAL WORK

**CONF ALL

NOTE: No additional work is required by this revision for aircraft modified by any previous

revision.

REASON

Revision No. 09 issued to update the effectivity.

CHANGES

Layout changes due to computerization of this revision are not identified.

SUMMARY

MODIFICATIONS Minor editorial or document structure change N

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

Minor editorial or document structure change N

GENERAL EVALUATION Minor editorial or document structure change N

MATERIAL PRICE INFORMATION Minor editorial or document structure change N

EFFECTIVITY Minor editorial or document structure change N

CONCURRENT REQUIREMENTS Minor editorial or document structure change N

REFERENCES / REPERCUSSIONS Minor editorial or document structure change N

NATURE OF THE WORK Minor editorial or document structure change N

MANPOWER Minor editorial or document structure change N

APPENDICES Minor editorial or document structure change N

PLANNING INFORMATION

EFFECTIVITY Effectivity updated. N

Configuration definition Minor editorial or document structure change N

DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

CONF 001 Minor editorial or document structure change N

Material Effectivity Minor editorial or document structure change N

Minor editorial or document structure change N

CONCURRENT REQUIREMENTS Minor editorial or document structure change N

REASON Minor editorial or document structure change N

History Minor editorial or document structure change N

Objective/Action Minor editorial or document structure change N

Advantages Minor editorial or document structure change N

Operational/Maintenance

Consequences

Minor editorial or document structure change N

DESCRIPTION Minor editorial or document structure change N

COMPLIANCE Minor editorial or document structure change N

Classification Minor editorial or document structure change N

Accomplishment Timescale Minor editorial or document structure change N

APPROVAL Minor editorial or document structure change N

Minor editorial or document structure change N

MANPOWER Minor editorial or document structure change N

Minor editorial or document structure change N

WEIGHT AND BALANCE Minor editorial or document structure change N

ELECTRICAL LOAD DATA Minor editorial or document structure change N

REFERENCES Minor editorial or document structure change N

Minor editorial or document structure change N

PUBLICATION AFFECTED Minor editorial or document structure change N

Minor editorial or document structure change N

INTERCHANGEABILITY/MIXABILITY Minor editorial or document structure change N

SPARES Minor editorial or document structure change N

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY Minor editorial or document structure change N

Procurement Addresses Minor editorial or document structure change N

Price and Availability Minor editorial or document structure change N

INDUSTRY SUPPORT INFORMATION Minor editorial or document structure change N

LIST OF COMPONENTS Minor editorial or document structure change N

LIST OF MATERIALS - OPERATOR

SUPPLIED

Minor editorial or document structure change N

Consumable Materials Minor editorial or document structure change N

Consumable CMLA01 Minor editorial or document structure change N

Components Minor editorial or document structure change N

Equipment Minor editorial or document structure change N

PARTS TO BE RE-IDENTIFIED BY

OPERATOR

Minor editorial or document structure change N

TOOLING Minor editorial or document structure change N

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REVISION TRANSMITTAL SHEET

ACCOMPLISHMENT INSTRUCTIONS

TASK 783006- 832-801-001-Inspection Minor editorial or document structure change N

Task associated data - 001 Minor editorial or document structure change N

Subtask 783006-910-001-001 Minor editorial or document structure change N

Subtask 783006-839-001-001 Minor editorial or document structure change N

Subtask 783006-800-001-001 Minor editorial or document structure change N

Subtask 783006-941-001-001 Minor editorial or document structure change N

Subtask 783006-832-001-001 Minor editorial or document structure change N

Subtask 783006-832-002-001 Minor editorial or document structure change N

Subtask 783006-942-001-001 Minor editorial or document structure change N

TASK 783006- 833-801-001-Repair Minor editorial or document structure change N

Task associated data - 001 Minor editorial or document structure change N

Subtask 783006-839-002-001 Minor editorial or document structure change N

Subtask 783006-833-001-001 Minor editorial or document structure change N

Subtask 783006-700-002-001 Minor editorial or document structure change N

Fig. A-FBAAA Minor editorial or document structure change N

Fig. A-FBAAA Sheet 01 Minor editorial or document structure change N

Appendix 1

APPENDIX CONTENT Minor editorial or document structure change N

Fig. A-FCAAA Minor editorial or document structure change N

Fig. A-FCAAA Sheet 01 Minor editorial or document structure change N

FILLING INSTRUCTIONS

This Service Bulletin has been generated electronically and is reissued as a complete document.

Replace the complete document.

Put this Revision Transmittal Sheet in front of the Service Bulletin.

HISTORY OF PREVIOUS REVISIONS

Revision No. 01 issued to add Airworthiness Directive and to change Compliance.

Revision No. 02 issued to add aircraft MSN 0234 and 0244 for customer CPA.

Revision No. 03 issued to add aircraft models 330-243 and 330-343.

Revision No. 04 is issued to add a threshold of 2,000 FC for aircraft on which Mod. No. 46879S14637

or Mod. No. 47358S14840 is embodied with a repetitive inspection every 2,000 FC.

Revision No. 05 issued to add aircraft in the effectivity.

Revision No. 06 issued to add aircraft in the effectivity.

Revision No. 07 issued to add aircraft in the effectivity.

Revision No. 08 issued to extend the effectivity.

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REVISION TRANSMITTAL SHEET

REVISION SEQUENCE

ORIGINAL: Mar 14/97

REVISION No.: 01 - Sep 15/97

REVISION No.: 02 - Jan 15/99

REVISION No.: 03 - Jan 18/00

REVISION No.: 04 - Jul 26/00

REVISION No.: 05 - Mar 06/01

REVISION No.: 06 - Mar 23/04

REVISION No.: 07 - Mar 16/07

REVISION No.: 08 - Jul 17/08

REVISION No. : 09 - Oct 21/09

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SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 78

TITLE: EXHAUST - THRUST REVERSER OPENING MECHANISM - INSPECT

REAR HINGE LUGS OF R.R. THRUST REVERSER.

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

During flight tests, unexpected fatigue high loads were measured at the time of the certification, on the

hinges integrated on the 12 o’clock beam which forms the upper extreme edge of the thrust reverser

unit C.duct.

To establish an interval of inspection on those hinges, more accurate testing was necessary. The thrust

reverser structure stress analysis has shown that when the high loads are imposed, the hinges are

unable to withstand a full aircraft life without the here above inspection.

This Inspection Service Bulletin is published to advise all operators of A330-243, A330-341, A330-342

and A330-343 aircraft powered by ROLLS ROYCE Trent 700 engines of the issue of ROLLS ROYCE

Inspection Service Bulletin No. RB.211-78-AB115 Revision No. 04 or later approved revision.

This Inspection Service Bulletin requires to do :

- A general visual inspection of the hinges assemblies and along the beam structure.

- A detailed visual inspection of the hinges 2, 3, 4 and 5.

- If necessary, the replacement of the right or/and left engine thrust reverser.

Accomplishment of this Service Bulletin will provide an immediate indication on the hinges reliability in

order to avoid further damages on the thrust reverser.

The life limitations are covered by an Airworthiness Directive (AD).

DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006

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SERVICE BULLETIN

SUMMARY

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY 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

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED YES

MATERIAL PRICE INFORMATION

No Material

EFFECTIVITY

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

78V 97X ACA AFL ALK AVA BMA CCA CES CHH CPA CRL CSC

CSN CYP DLH EDW ETD GFA GIA HDA HFY IWD IYE JAI LVG

MEA MLM MON MSR MXA OBS OMA SAS SGX SIA SWR TCX THA

TSC UAE UAF USA VKG XAX XLF

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 783006-832-801-001: Inspection

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 1.50

Additional manhours related to Vendor SB; refer to:

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SUMMARY

Task 783006-832-801-001: Inspection

Do a general visual inspection of the hinges assemblies

and along the beam structure.

ROLLS ROYCE Service Bulletin No.

RB.211-78-AB115 Revision No. 04

or later approved revision

Do a detailed visual inspection of the hinges 2, 3, 4 and 5. ROLLS ROYCE Service Bulletin No.

RB.211-78-AB115 Revision No. 04

or later approved revision

Task 783006-833-801-001: Repair

TOTAL MANHOURS 1.00

ELAPSED TIME (HOURS) 1.00

Additional manhours related to Vendor SB; refer to:

If necessary, replace the RH or/and the LH engine thrust

reverser.

ROLLS ROYCE Service Bulletin No.

RB.211-78-AB115 Revision No. 04

or later approved revision

APPENDICES

Appendix 1

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SUMMARY

This Page Intentionally Left Blank

DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006

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SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 78

TITLE: EXHAUST - THRUST REVERSER OPENING MECHANISM - INSPECT

REAR HINGE LUGS OF R.R. THRUST REVERSER.

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

NOTE: This Inspection Service Bulletin is applicable only on aircraft equipped with

ROLLS ROYCE Trent 700 engines.

(1) Models

330-243 330-341 330-342 330-343

(2) Effectivity by MSN

0012 0017 0071 0083 0098-0099 0102 0106 0109 0111 0113 0118 0121 0132 0138

0140 0144 0148 0153 0155 0165 0177 0234 0244 0248 0250-0251 0254 0261

0265-0266 0271 0276-0277 0279 0281 0283-0287 0293 0295 0301 0303 0306 0309

0311 0313-0314 0316 0320 0326 0328 0334 0340 0344-0345 0348-0349 0356-0357

0365 0369 0372 0382 0384 0386 0389 0392-0393 0396 0398 0400-0401 0404-0405

0407-0409 0412 0418-0421 0423 0427 0437 0439 0451-0452 0455-0456 0461-0462

0479-0480 0491 0494 0496-0497 0501 0505 0509 0512 0515 0518 0525-0527 0529

0532 0536 0539 0548 0551 0565 0568 0570 0576 0579 0581 0597 0600 0610 0625

0627 0629 0632 0635-0636 0642 0645 0648-0649 0652 0654 0656 0658 0662 0664

0666 0669-0670 0673 0679 0683 0687-0688 0692 0696 0701 0709 0713 0716-0717

0720 0724 0726 0728-0730 0732 0735 0737 0741 0750-0751 0756 0759 0773

0776-0777 0780-0782 0785-0786 0788 0791 0795 0797 0807 0809-0810 0815 0818

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0821 0824 0830 0832-0833 0836 0839-0840 0850-0852 0854-0855 0860 0862-0863

0866-0868 0873 0875 0879 0881 0884 0889-0890 0895-0896 0903 0905-0906

0908-0909 0913 0915-0916 0919 0922 0926 0928 0930 0935-0937 0941-0942 0944

0948 0952 0954 0957-0959 0963-0964 0966-0967 0971 0973-0975 0978 0982-0984

0986 0988-0992 0995 0997-0998 1000 1003 1006 1008-1012 1014-1016 1018 1020

1022 1026 1028-1029 1033 1035 1037-1038 1041 1044-1049 1052-1053 1058 1060

1063 1065-1066 1069 1071-1077 1080-1082 1084-1087 1089-1090 1093 1095

1097-1100

(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

78V 1033 1046

97X 1053

ACA 0277 0279 0284 0344 0400 0408 0412 0419

AFL 0963 0973 1014 1045 1047 1058 1065 1072 1077

ALK 0303 0306 0311 0313

AVA 0948 0967 1009 1016 1073

BMA 0398 0401 0404

CCA 0750 0756 0759 0780 0785 0797 0810 0815 0839 0860 0867 0873

0884 0890 0903 0909 0930 0941 0944 0957 1087

CES 0713 0720 0728 0732 0735 0773 0777 0781 0782 0791 0821 0830

0836 0851 0862 0866 0916 0928 0936 0942

CHH 0875 0881 0906 0919 0982

CPA 0012 0017 0071 0083 0099 0102 0109 0113 0118 0121 0155 0244

0386 0389 0393 0418 0420 0421 0423 0439 0539 0548 0565 0669

0673 0679 0776 0850 0855 0895 0915 0959

CRL 0285 0320

CSC 1082

CSN 0649 0652 0656 0664 0818 0840 0879 0889 0908 0935 0937 0954

0958 0964

CYP 0505 0526

DLH 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 0896 0905

0913 0922 0989

EDW 0369

ETD 0658 0688 0717 0724 0729 0730 0737 0788 0809 0824 0832 0852

0854 0868 0975 0991 1071 1081

GFA 0276 0281 0286 0287 0334 0340 0527 0529 0532 0992

GIA 0138 0140 0144 0148 0153 0165 0988 1020 1028 1052

HDA 0098 0106 0132 0234 0405 0479 0512 0581 0654 0662 0692 0716

0741 0786

HFY 1008

IWD 0670 0833 1097

IYE 0625 0632

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OPERATOR MSN

JAI 0751 0807

LVG 0551 0597 0627

MEA 0926 0984 0995 0998

MLM 0863

MON 0261 0265

MSR 0600 0610 0666 0683 0696 0709 0726

MXA 0966 0971

OBS 0461

OMA 1038 1044 1049 1063 1093

SAS 0496 0497 0515 0568

SGX 0407

SIA 0978 0983 0986 0997 1006 1010 1012 1015 1085 1098 1099

SWR 1000 1018 1026 1029 1084 1089

TCX 0254 0266 0301 0309 0357 0427 0456 0795

THA 0990 1003 1035 1037 1060 1074 1086 1090

TSC 0111 0177 0250 0271 0480

UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0345 0348 0365

0372 0382 0384 0392 0396 0409 0437 0451 0452 0455 0462 0491

0494 0509 0518 0525 0536

UAF 1080

USA 1011 1022 1041 1069 1076 1095 1100

VKG 0349 0356

XAX 0952 0974 1048 1066 1075

XLF 0501 0635

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(4) Configuration by MSN

MSN CONFIGURATION

0012 0017 0071 0083 0098 0099 0102 0106 0109 0111 0113

0118 0121 0132 0138 0140 0144 0148 0153 0155 0165 0177

0234 0244 0248 0250 0251 0254 0261 0265 0266 0271 0276

0277 0279 0281 0283 0284 0285 0286 0287 0293 0295 0301

0303 0306 0309 0311 0313 0314 0316 0320 0326 0328 0334

0340 0344 0345 0348 0349 0356 0357 0365 0369 0372 0382

0384 0386 0389 0392 0393 0396 0398 0400 0401 0404 0405

0407 0408 0409 0412 0418 0419 0420 0421 0423 0427 0437

0439 0451 0452 0455 0456 0461 0462 0479 0480 0491 0494

0496 0497 0501 0505 0509 0512 0515 0518 0525 0526 0527

0529 0532 0536 0539 0548 0551 0565 0568 0570 0576 0579

0581 0597 0600 0610 0625 0627 0629 0632 0635 0636 0642

0645 0648 0649 0652 0654 0656 0658 0662 0664 0666 0669

0670 0673 0679 0683 0687 0688 0692 0696 0701 0709 0713

0716 0717 0720 0724 0726 0728 0729 0730 0732 0735 0737

0741 0750 0751 0756 0759 0773 0776 0777 0780 0781 0782

0785 0786 0788 0791 0795 0797 0807 0809 0810 0815 0818

0821 0824 0830 0832 0833 0836 0839 0840 0850 0851 0852

0854 0855 0860 0862 0863 0866 0867 0868 0873 0875 0879

0881 0884 0889 0890 0895 0896 0903 0905 0906 0908 0909

0913 0915 0916 0919 0922 0926 0928 0930 0935 0936 0937

0941 0942 0944 0948 0952 0954 0957 0958 0959 0963 0964

0966 0967 0971 0973 0974 0975 0978 0982 0983 0984 0986

0988 0989 0990 0991 0992 0995 0997 0998 1000 1003 1006

1008 1009 1010 1011 1012 1014 1015 1016 1018 1020 1022

1026 1028 1029 1033 1035 1037 1038 1041 1044 1045 1046

1047 1048 1049 1052 1053 1058 1060 1063 1065 1066 1069

1071 1072 1073 1074 1075 1076 1077 1080 1081 1082 1084

1085 1086 1087 1089 1090 1093 1095 1097 1098 1099 1100

001

(5) Configuration definition

**CONF 001

Config. 01 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Consumable CMLA01 1

B. CONCURRENT REQUIREMENTS

None

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C. REASON

(1) History

During flight tests, unexpected fatigue high loads were measured at the time of the

certification, on the hinges integrated on the 12 o’clock beam which forms the upper

extreme edge of the thrust reverser unit C.duct.

To establish an interval of inspection on those hinges, more accurate testing was

necessary. The thrust reverser structure stress analysis has shown that when the high

loads are imposed, the hinges are unable to withstand a full aircraft life without the here

above inspection.

(2) Objective/Action

This Inspection Service Bulletin is published to advise all operators of A330-243,

A330-341, A330-342 and A330-343 aircraft powered by ROLLS ROYCE Trent 700

engines of the issue of ROLLS ROYCE Inspection Service Bulletin No. RB.211-78-

AB115 Revision No. 04 or later approved revision.

This Inspection Service Bulletin requires to do :

- A general visual inspection of the hinges assemblies and along the beam structure.

- A detailed visual inspection of the hinges 2, 3, 4 and 5.

- If necessary, the replacement of the right or/and left engine thrust reverser.

(3) Advantages

Accomplishment of this Service Bulletin will provide an immediate indication on the

hinges reliability in order to avoid further damages on the thrust reverser.

(4) Operational/Maintenance Consequences

The life limitations are covered by an Airworthiness Directive (AD).

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 783006-832-801-001: Inspection

(1) Do a general visual inspection of the hinges assemblies and along the beam

structure.

(2) Do a detailed visual inspection of the hinges 2, 3, 4 and 5.

Task 783006-833-801-001: Repair

(1) If necessary, replace the RH or/and the LH engine thrust reverser.

DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006

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E. COMPLIANCE

(1) Classification

MANDATORY

(2) Accomplishment Timescale

This Inspection Service Bulletin must be accomplished before accumulation of :

- 1,200 Flight Cycles (FC) for aircraft on which Mod. No. 46879S14637 and Mod.

No.47358S14840 are not embodied, with repetitive Inspection every 1,200 FC,

- 2,000 FC for aircraft on which Mod. No. 46879S14637 or Mod. No.47358S14840 is

embodied, with repetitive Inspection every 2,000 FC.

Accomplishment of this Service Bulletin has been rendered mandatory by the issue of an

Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA).

The AD must be used as the reference document for the mandatory accomplishment

timescale.

F. APPROVAL

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

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

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

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

before incorporation of the Service Bulletin.

G. MANPOWER

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

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

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

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

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

included.

Task 783006-832-801-001: Inspection

Get Access 1.00

Close-Up 2.00

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 1.50

Additional manhours related to Vendor SB; refer to:

Do a general visual inspection of the hinges

assemblies and along the beam structure.

ROLLS ROYCE Service Bulletin No.

RB.211-78-AB115 Revision No. 04

or later approved revision

Do a detailed visual inspection of the hinges 2, 3, 4

and 5.

ROLLS ROYCE Service Bulletin No.

RB.211-78-AB115 Revision No. 04

or later approved revision

DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006

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Task 783006-833-801-001: Repair

Tests 1.00

TOTAL MANHOURS 1.00

ELAPSED TIME (HOURS) 1.00

Additional manhours related to Vendor SB; refer to:

If necessary, replace the RH or/and the LH engine

thrust reverser.

ROLLS ROYCE Service Bulletin No.

RB.211-78-AB115 Revision No. 04

or later approved revision

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 12-34-24 78-32-49 78-32-51

78-32-52

Consumable Material List (CML)

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

Vendor Service Bulletin (VSB) ROLLS ROYCE Service Bulletin

No. RB.211-78-AB115 Revision

No. 04 or later approved revision

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 78-32-00

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

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SERVICE BULLETIN

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DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Modification of removed equipment should be negotiated directly with ROLLS ROYCE as

per instructions given in Service Bulletin No. RB.211-78-AB115 Revision No. 04.

(2) Price and Availability

Refer to the Vendor Service Bulletin No. RB.211-78-AB115 Revision No. 04 or later

approved revision for equipment modification sales terms.

B. INDUSTRY SUPPORT INFORMATION

Refer to the Vendor Service Bulletin (VSB) for the industry support terms.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Solvent 11-026 As required

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006

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SERVICE BULLETIN

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 783006-832-801-001 - 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

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 1.50

Additional manhours related to Vendor SB; refer

to:

ROLLS ROYCE Service Bulletin

No. RB.211-78-AB115 Revision

No. 04 or later approved revision

A. GENERAL

(1) Subtask 783006-910-001-001 - 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

Solvent 11-026 As required

References

Consumable Material List (CML)

DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006

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SERVICE BULLETIN

(a) Clean the surfaces to be inspected with cleaning agent

Solvent 11-026 As required

(b) For the specification of the material number (Mat. No.) refer to the CML.

(2) Subtask 783006-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

(3) Subtask 783006-800-001-001 - Work breakdown

Manpower Resources

Skills NON SPECIFIC

References

Vendor Service Bulletin (VSB) ROLLS ROYCE RB.211-78-AB115 Revision

No. 04 or later approved revision

Fig. A-FBAAA Sheet 01 - Flow Chart

The purpose of the synoptic chart (Refer to Fig. A-FBAAA Sheet 01) is to show the

various Inspection/Repair phases described in this Service Bulletin (Refer to ROLLS

ROYCE Service Bulletin No. RB.211-78-AB115 Revision No. 04 or later approved

revision).

B. PREPARATION

(1) Subtask 783006-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 12-34-24, Page Block 201

78-32-49, Page Block 401

(a) Make sure that the aircraft is electrically grounded, (Refer to AMM 12-34-24 Page

Block 201).

(b) Remove the hinge access covers (Refer to AMM 78-32-49 Page Block 401).

C. PROCEDURE

(1) Subtask 783006-832-001-001 - Do a general visual inspection of the hinges assemblies

and along the beam structure.

References

Vendor Service Bulletin (VSB) ROLLS ROYCE RB.211-78-AB115 Revision

No. 04 or later approved revision

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SERVICE BULLETIN

(a) Do a general visual inspection of the hinges assemblies and along the beam

structure as written in ROLLS ROYCE Service Bulletin No. RB.211-78-AB115

Revision No. 04 or later approved revision.

1 If a crack is found :

a Replace the RH or/and the LH thrust reverser of each engine

(Refer to SUBTASK 783006-833-001 001)

b Do again the general visual inspection of the hinges assemblies and

along the beam structure at :

- 1,200 FC for aircraft on which Mod. No. 46879S14637 and Mod.

No. 47358S14840 are not embodied, at the interval given in Para.

1.E.(2),

- or 2,000 FC for aircraft on which Mod. No. 46879S14637 or Mod.

No. 47358S14840 is embodied, at the interval given in Para. 1.E.(2).

2 If no crack is found :

a Refer to SUBTASK 783006-832-002 001.

(b) When the work is completed, you must report the inspection results to AIRBUS

(AI/SEE13), on the recording form attached.

Refer to Appendix 1 .

In case of findings, refer to the Service Bulletin instructions to do this report.

(2) Subtask 783006-832-002-001 - Do a detailed visual inspection of the hinges 2, 3, 4 and

5.

References

Vendor Service Bulletin (VSB) ROLLS ROYCE RB.211-78-AB115 Revision

No. 04 or later approved revision

(a) Do a detailed visual inspection of the hinges 2, 3, 4 and 5 as written in ROLLS

ROYCE Service Bulletin No. RB.211-78-AB115 Revision No. 04 or later approved

revision.

1 If no crack is found :

a Do again the general visual inspection of the hinges assemblies and

along the beam structure at :

- 1,200 FC for aircraft on which Mod. No. 46879S14637 and Mod.

No. 47358S14840 are not embodied, at the interval given in Para.

1.E.(2),

- or 2,000 FC for aircraft on which Mod. No. 46879S14637 or Mod.

No. 47358S14840 is embodied, at the interval given in Para. 1.E.(2).

DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006

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SERVICE BULLETIN

2 If a crack is found :

a Replace the RH or/and the LH thrust reverser of each engine.

(Refer to SUBTASK 783006-833-001 001)

b Do again the general visual inspection of the hinges assemblies and

along the beam structure at :

- 1,200 FC for aircraft on which Mod. No. 46879S14637 and Mod.

No. 47358S14840 are not embodied, at the interval given in Para.

1.E.(2),

- or 2,000 FC for aircraft on which Mod. No. 46879S14637 or Mod.

No. 47358S14840 is embodied, at the interval given in Para. 1.E.(2).

(b) When the work is completed, you must report the inspection results to AIRBUS

(AI/SEE13), on the recording form attached.

Refer to Appendix 1 .

In case of findings, refer to the Service Bulletin instructions to do this report.

D. TEST

None

E. CLOSE-UP

(1) Subtask 783006-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

(a) Remove the access platforms.

(b) Restore the systems and the aircraft to normal operating condition.

DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006

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SERVICE BULLETIN

Task 783006-833-801-001 - Repair

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

Manpower

TOTAL MANHOURS 1.00

ELAPSED TIME (HOURS) 1.00

Additional manhours related to Vendor SB; refer

to:

ROLLS ROYCE Service Bulletin

No. RB.211-78-AB115 Revision

No. 04 or later approved revision

A. GENERAL

(1) Subtask 783006-839-002-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

B. PREPARATION

None

DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006

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SERVICE BULLETIN

C. PROCEDURE

(1) Subtask 783006-833-001-001 - If necessary, replace the RH or/and the LH engine thrust

reverser.

References

Aircraft Maintenance Manual (AMM) 78-32-51, Page Block 401

78-32-52, Page Block 401

Vendor Service Bulletin (VSB) ROLLS ROYCE RB.211-78-AB115 Revision

No. 04 or later approved revision

(a) For the replacement of the thrust reverser, refer to ROLLS ROYCE Service Bulletin

No. RB.211-78-AB115 Revision No. 04 or later approved revision.

1 Refer to AMM 78-32-51 Page Block 401 and AMM 78-32-52 Page Block 401.

D. TEST

(1) Subtask 783006-700-002-001 - Tests

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 78-32-49, Page Block 401

78-32-51, Page Block 401

78-32-52, Page Block 401

(a) If it is necessary to replace the RH or/and the LH engine thrust reverser (crack) :

1 Do the test after the removal/installation of the right thrust reverser cowl door

(Refer to AMM 78-32-51 Page Block 401) and/or

2 Do the test after the removal/installation of the left thrust reverser cowl door

(Refer to AMM 78-32-52 Page Block 401)

(b) If it is not necessary to replace the RH or/and the LH engine thrust reverser (no

crack) :

1 Do the test after the removal/installation of the hinge access covers (Refer to

AMM 78-32-49 Page Block 401).

E. CLOSE-UP

None

DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006

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SERVICE BULLETIN

**CONF ALL

Yes Crack No

Replace the

RH or/and the LH

engine thrust

reverser

Replace the

RH or/and the LH

engine thrust

reverser

Do a general visual inspection

of the hinges assemblies and

along the beam structure

Do a detailed visual

inspection of the

hinges n°2, n°3, N°4 and N°5

on the LH and RH sides

on each engine

Do again this inspection:

Do again this inspection:

− every 1,200 FC for

 aircraft on which

 Mod. No. 46879S14637 and

 Mod. No. 47358S14840 are

 not embodied,

− or every 2,000 FC for

 aircraft on which

 Mod. No. 46879S14637 or

 Mod. No. 47358S14840 is

 embodied.

− every 1,200 FC for

 aircraft on which

 Mod. No. 46879S14637 and

 Mod. No. 47358S14840 are

 not embodied,

− or every 2,000 FC for

 aircraft on which

 Mod. No. 46879S14637 or

 Mod. No. 47358S14840 is

 embodied.

NOTE : For this inspection

refer to the vendor ROLLS ROYCE

Inspection Service Bulletin No. RB.211−78−AB115

revision No. 04 or later approved revision.

Aircraft on which

Mod. No. 46879S14637 and

Mod. No. 47358S14840 are

not embodied, must be inspected

before accumulation of 1,200 FC

Aircraft on which

Mod. No. 46879S14637 or

Mod. No. 47358S14840 is

embodied, must be inspected

before accumulation of 2,000 FC

G_SB_783006_5_BAAA_01_00

QUESTION

ACTION

FINDING

Yes Crack No

Figure A-FBAAA - Sheet 01

Flow Chart

DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006

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SERVICE BULLETIN

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SERVICE BULLETIN

Appendix 1

**CONF ALL

(1) The results of the inspection, including no findings, replacement or actions to be done, must be

forwarded to AIRBUS Department AI/SEE13, on the attached inspection report sheet.

DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006

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SERVICE BULLETIN

Appendix 1

**CONF ALL

INSPECTION REPORT

PLEASE PRECISE OTHER FINDINGS

DATE OF INSPECTION :

INSPECTION METHOD : VISUAL INSPECTION

RIGHT ENGINE

RIGHT ENGINE

23 5

HINGE N°. HINGE N°.

NO

YES

LEFT ENGINE

23 5

LH SIDE RH SIDE LH SIDE RH SIDE

A330−78−3006

VISUAL INSPECTION

4 4

LH SIDE RH SIDE

RIGHT ENGINE

NO

YES

LH SIDE RH SIDE

2

2

2 2

2

1

1

1

1

1

BEAM STRUCTURE

23 5

HINGE N°. HINGE N°.

NO

YES

4 23 5 4

LH SIDE RH SIDE

NO

YES

LH SIDE RH SIDE

2

2

2 2

2

1

1

1

1

1

BEAM STRUCTURE

GENERAL VISUAL INSPECTION DETAILED VISUAL INSPECTION

HINGE N°2 HINGE N°3 HINGE N°5 HINGE N°4

AREA TO BE INSPECTED (GENERAL VISUAL INSPECTION)

AREA TO BE INSPECTED (DETAILED VISUAL INSPECTION)

LEFT ENGINE LEFT ENGINE

REPLACE THE THRUST REVERSER IN ACCORDANCE WITH :

HINGES ASSEMBLIES

HINGES ASSEMBLIES

SERVICE BULLETIN N° :

A/C MSN :

FLIGHT HOURS :

FLIGHT CYCLES :

ROLLS ROYCE INSPECTION SERVICE BULLETIN N°.RB−211−78−AB115

CRACK

CRACK

CRACK

B

A

FWD

B B

A

A

CRACK

G_SB_783006_5_CAAA_01_00

Figure A-FCAAA - Sheet 01

Inspection Report

DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006

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SERVICE BULLETIN

REPORTING SHEET

TITLE: EXHAUST - THRUST REVERSER OPENING MECHANISM - INSPECT

REAR HINGE LUGS OF R.R. THRUST REVERSER.

MODIFICATION No.: None

Please complete the appropriate item (A or B):

A - SB WILL BE embodied YES/NO (if NO please comment)

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

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

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

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

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

Or : Intermediate revision YES/NO

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

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

the next feasible revision, this will result in

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

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

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

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

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

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

DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4 3 2 1

- Quality rating of the Accomplishment Instructions 4 3 2 1

- Quality rating of the Illustrations 4 3 2 1

- Is this SB easy to understand ? Y / N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials Operator Supplied X Mod/Inspection

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006

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