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@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1
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 REVISION No.: 09 - Oct 21/09 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET CONF 001 Minor editorial or document structure change N Minor editorial or document structure change N Material Effectivity 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 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
WEIGHT AND BALANCE Minor editorial or document structure change N
ELECTRICAL LOAD DATA Minor editorial or document structure change N 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
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 DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006 REVISION No.: 09 - Oct 21/09 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
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.
DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006 REVISION No.: 09 - Oct 21/09 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
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 DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006 REVISION No.: 09 - Oct 21/09 Page: 4 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
SUMMARY AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 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 REVISION No.: 09 - Oct 21/09 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
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 relat ed to Vendor SB; refer to:
DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006 REVISION No.: 09 - Oct 21/09 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
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 relat ed 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 DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006 REVISION No.: 09 - Oct 21/09 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
SUMMARY This Page Intentionally Left Blank DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006 REVISION No.: 09 - Oct 21/09 Page: 4 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN AIRBUS
CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1
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 DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006 REVISION No.: 09 - Oct 21/09 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN 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 DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006 REVISION No.: 09 - Oct 21/09 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
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 DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006 REVISION No.: 09 - Oct 21/09 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
(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 DATE: Mar 14/97 SERVICE BULLETIN No.: A330-78-3006 REVISION No.: 09 - Oct 21/09 Page: 4 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.