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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: 53 TITLE: FUSELAGE - FORWARD FUSELAGE - REINFORCE CIRCUMFERENTIAL JOINT/STRING ER COUPLING IN AREA OF FR37.1 MODIFICATION No.: 204499D50871 204499D50928 This page transmits Revision No.01 of Service Bulletin No.A330-53-3251
ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue.
REASON Revision No. 01 issued to remove the jacking procedure.
The opportunity has been taken to update the effectivity.
CHANGES The main changes of this revision are:
- remove the Zero Stress Jacking procedure
- remove Zero Stress Jacking Appendix
- remove the DEFUEL/VENTILATION procedure
- add In-Service Information (ISI) 51.48.00001 and 00.00.00198
- update the Procurement Address
- add West Coast Industries (WCI) as an alternative to Fatigue Technology Inc. (FTI) for cold expansion tooling
- add Appendix for modification accomplishment
- update the Service Bulletin effectivity.
DATE: May 13/15 SERVICE BULLETIN No.: A330-53-3251 REVISION No.: 01 - Jun 23/16 Page: 1 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
FRONT MATTER
MODIFICATIONS
MODIFICATION NUMBER(S) UPDATED R
SUMMARY
MODIFICATIONS
MODIFICATION CLASSIFICATION UPDATED R
REASON/DESCRIPTION/OPERATIONAL
CONSEQUENCES
REASON UPDATED R
GENERAL EVALUATION
GENERAL EVALUATION TABLE UPDATED R
MATERIAL PRICE INFORMATION
MATERIAL PRICE INFORMATION TABLE
UPDATED R
MATERIAL PRICE INFORMATION TABLE
UPDATED R
EFFECTIVITY
OPERATOR LIST UPDATED R
REFERENCES / REPERCUSSIONS
REFERENCES/REPERCUSSIONS TABLE
UPDATED R
APPENDICES
APPENDICES UPDATED R Fig. A-GSAAA Fig. A-GSAAA Sheet 01
SHEET UPDATED R
PLANNING INFORMATION
EFFECTIVITY
EFFECTIVITY RELATED INFORMATION
UPDATED R Configuration definition CONF 001
CONFIGURATION DEFINITION UPDATED
CONFIGURATION DESCRIPTION UPDATED R CONF 002
CONFIGURATION DEFINITION UPDATED
CONFIGURATION DESCRIPTION UPDATED R Material Effectivity
MATERIAL EFFECTIVITY UPDATED
MATERIAL SET QUANTITY UPDATED
MATERIAL SET UPDATED R
MATERIAL EFFECTIVITY UPDATED
MATERIAL SET QUANTITY UPDATED
MATERIAL SET UPDATED R REASON Objective/Action
OBJECTIVE/ACTION UPDATED R Operational/Maintenance Consequences
OPERATIONAL/MAINTENANCE CONSEQUENCES
UPDATED R
COMPLIANCE Accomplishment Timescale
ACCOMPLISHMENT TIMESCALE UPDATED R
MANPOWER
MANPOWER UPDATED R
MANPOWER UPDATED R
REFERENCES
REFERENCED DOCUMENTATION UPDATED R
REFERENCED DOCUMENTATION UPDATED R
MATERIAL INFORMATION
MATERIAL - PRICE AND AVAILABILITY Procurement Addresses
PROCUREMENT ADDRESSES UPDATED R Price and Availability
PRICE AND AVAILABILITY UPDATED
MATERIAL PRICE UPDATED R
INDUSTRY SUPPORT INFORMATION
INDUSTRY SUPPORT INFORMATION UPDATED R DATE: May 13/15 SERVICE BULLETIN No.: A330-53-3251 REVISION No.: 01 - Jun 23/16 Page: 2 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
TOOLING Tooling - Price and Availability Procurement Addresses
PROCUREMENT ADDRESSES UPDATED
MATERIAL SET UPDATED R Price and Availability
PRICE AND AVAILABILITY UPDATED R Tools
TOOLS UPDATED R Standard tool TOOLD01
TOOL MATERIAL SET UPDATED
TOOL UPDATED
NOTE UPDATED
QUANTITY UPDATED R Standard tool TOOLD02
TOOL MATERIAL SET UPDATED
NOTE UPDATED
TOOL UPDATED
QUANTITY UPDATED R Standard tool TOOLD03
TOOL MATERIAL SET UPDATED
TOOL UPDATED
NOTE UPDATED
QUANTITY UPDATED R Standard tool TOOLD04
TOOL MATERIAL SET UPDATED
NOTE UPDATED
TOOL UPDATED
QUANTITY UPDATED R Standard tool TOOLD05
TOOL MATERIAL SET DELETED D
ACCOMPLISHMENT INSTRUCTIONS TASK 533251- 831-848-001-Modification
TASK SOLUTION UPDATED
CAUTION UPDATED
NOTE UPDATED R Task associated data - 001
ZONE UPDATED
PANEL UPDATED R Task associated data - 002
ZONE UPDATED
PANEL UPDATED R Subtask 533251-910-201-001
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED R Subtask 533251-910-201-001
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED R Subtask 533251-941-201-001
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED R Subtask 533251-010-201-001
SUBTASK SOLUTION UPDATED
PANEL UPDATED
ZONE UPDATED
REFERENCED DOCUMENTATION UPDATED
LOCATION UPDATED
REFERENCES UPDATED R Subtask 533251-941-201-001
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED R DATE: May 13/15 SERVICE BULLETIN No.: A330-53-3251 REVISION No.: 01 - Jun 23/16 Page: 3 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET Subtask 533251-010-201-001
SUBTASK SOLUTION UPDATED
PANEL UPDATED
ZONE UPDATED
REFERENCED DOCUMENTATION UPDATED
LOCATION UPDATED
REFERENCES UPDATED R Subtask 533251-831-201-002
SUBTASK SOLUTION UPDATED
ZONE UPDATED
TOOL UPDATED
NOTE UPDATED
QUANTITY UPDATED
REFERENCED DOCUMENTATION UPDATED
LOCATION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED R Subtask 533251-831-201-001
SUBTASK SOLUTION UPDATED
PANEL UPDATED
ZONE UPDATED
TOOL UPDATED
NOTE UPDATED
QUANTITY UPDATED
REFERENCED DOCUMENTATION UPDATED
LOCATION UPDATED
MATERIAL LIST UPDATED
REFERENCES UPDATED R Subtask 533251-942-201-001
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED R Subtask 533251-942-201-001
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED R Fig. A-GBAAB Fig. A-GBAAB Sheet 03
SHEET UPDATED R Appendix 01 - Manpower Gantt Chart Fig. A-GAAAB
FIGURE SOLUTION UPDATED R Fig. A-GAAAA
FIGURE SOLUTION UPDATED R Appendix 02 - Status of the aircraft after accomplishment of the Service Bulletin No.
A330-53-3251
APPENDIX CONTENT
APPENDIX CONTENT ADDED N
APPENDIX
APPENDIX DELETED D
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.
DATE: May 13/15 SERVICE BULLETIN No.: A330-53-3251 REVISION No.: 01 - Jun 23/16 Page: 4 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
HISTORY OF PREVIOUS REVISIONS No previous revision
REVISION SEQUENCE ORIGINAL: May 13/15 REVISION No. : 01 - Jun 23/16 DATE: May 13/15 SERVICE BULLETIN No.: A330-53-3251 REVISION No.: 01 - Jun 23/16 Page: 5 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET This Page Intentionally Left Blank DATE: May 13/15 SERVICE BULLETIN No.: A330-53-3251 REVISION No.: 01 - Jun 23/16 Page: 6 6 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: 53 TITLE: FUSELAGE - FORWARD FUSELAGE - REINFORCE CIRCUMFERENTIAL JOINT/STRING ER COUPLING IN AREA OF FR37.1 **CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION MAJOR 204499D50871 204499D50928 MINOR None NOTE : As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes.
REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Following Widespread Fatigue Damage (WFD) analysis, it has been demonstrated that some areas require reinforcement before reaching the Design Service Goal (DSG). The circumferential joint in the area of Frame (FR)37.1 has been identified as such area.
This Service Bulletin details the work necessary to reinforce the circumferential joint at FR37.1 by the cold working of some fastener holes and the installation of new fasteners with interference fit.
The procedure as described in this Service Bulletin is to be performed if no AIRBUS repair and/or repair improvement has been previously performed in the same area. In case of repairs performed previously, please contact AIRBUS Repair Support department for further instructions.
Accomplishment of this Service Bulletin will improve the fatigue characteristics of the circumferential joint at FR37.1.
This Service Bulletin is based on the aircraft configuration as known by AIRBUS (first aircraft delivery configuration and modified by the reported incorporation of AIRBUS Service Bulletins).
DATE: May 13/15 SERVICE BULLETIN No.: A330-53-3251 REVISION No.: 01 - Jun 23/16 Page: 1 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
SUMMARY Prior to Service Bulletin embodiment, specific attention must be paid to structural damage which may exist and to repairs which were performed on the aircraft because they may be affected by the Service Bulletin. It must be verified that all allowable damage limits and repairs performed (both in accordance with the Structural Repair Manual (SRM) and outside of the SRM) are still applicable and effective to the new Service Bulletin configuration.
There may be additional or modified maintenance requirements, such as temporary limits or additional inspections that apply with respect to the Service Bulletin configuration.
AIRBUS disclaims any liability for the effect which the Service Bulletin may have on repairs performed on the aircraft before embodiment of the Service Bulletin.
If the post Service Bulletin repair status is not covered by the SRM and for repairs outside of the SRM covered by a Repair Approval Sheet (RAS) issued by AIRBUS, AIRBUS Customer Services Repair Engineering Support department should be contacted. Repair review will be done by AIRBUS at conditions of the Customer Services Catalogue.
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
STRUCTURAL LIFE EXTN YES
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 Kit 533251D02R00 1 4,300.00 Bolts, Nuts Standard tool TOOLD01 1 See SB FTI Cold Working Tooling Standard tool TOOLD02 1 See SB WCI Cold Working Tooling **CONF 002
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Kit 533251D01R00 1 4,000.00 Bolts, Nuts Standard tool TOOLD03 1 See SB FTI Cold Working Tooling Standard tool TOOLD04 1 See SB WCI Cold Working Tooling DATE: May 13/15 SERVICE BULLETIN No.: A330-53-3251 REVISION No.: 01 - Jun 23/16 Page: 2 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
SUMMARY
EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :
34Z AAL
AAR AAW ACA AEA AFL ALK BEL
CAL CBJ
CCA CEB
CES CHH CPA CRK CRL CSA CSC CSN CSZ
DAL DLH EDW EIN ETD EVA EVE F2I
FIN FJI FWI GIA HDA HFY IBE JAI KAL
KLM LNI MAS MSR OBS
OHY OMA PAL QFA QTR RSY RWD SAA
SAS SIA SVA SWR TAX
THA THY TNA TSC VIR VKG WOW XAX XLF
CONCURRENT REQUIREMENTS **CONF 001 Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s):
Service Bulletin No. A330-53-3090 NOTE : - Service Bulletin No. A330-53-3090 - FUSELAGE - FORWARD FUSELAGE - REINFORCE CIRCUMFERENTIAL JOINT AT FR37.1 AND LONGITUDINAL JOINT AT STGR 9 LH/RH (which applies Modification Nos. 45490D40811, 45490D40809 and 45490D40808).
**CONF 002 Accomplishment of this Service Bulletin requires the simultaneous accomplishment of the following Service Bulletin(s):
Service Bulletin No. A330-53-3252 NOTE : - Service Bulletin No. A330-53-3252 - FUSELAGE - FORWARD FUSELAGE -
REINFORCE CIRCUMFERENTIAL JOINT /STRINGER COUPLING IN AREA OF FR37.1 (which applies Modification No. 204499D50860).
REFERENCES / REPERCUSSIONS **CONF ALL TFU None OEB None AOT None SIL 51-012 ISI
00.00.00198
51.48.00001
LINE MAINTENANCE AFFECTED No
LIFE LIMIT None OTHER None DATE: May 13/15 SERVICE BULLETIN No.: A330-53-3251 REVISION No.: 01 - Jun 23/16 Page: 3 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
SUMMARY
NATURE OF THE WORK
AIRCRAFT YES
EQUIPMENT NO HARD NO SOFT NO OBRM NO
MANPOWER **CONF 001 Task 533251-831-848-001: Modification
TOTAL MANHOURS
54.00
ELAPSED TIME (HOURS)
27.00 **CONF 002 Task 533251-831-848-001: Modification
TOTAL MANHOURS
52.00
ELAPSED TIME (HOURS)
26.00
APPENDICES **CONF ALL Appendix 01 - Manpower Gantt Chart Appendix 02 - Status of the aircraft after accomplishment of the Service Bulletin No. A330-53-3251 DATE: May 13/15 SERVICE BULLETIN No.: A330-53-3251 REVISION No.: 01 - Jun 23/16 Page: 4 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
SUMMARY **CONF ALL AD FR37.1 FR37.2A FR37
CIRCUMFERENTIAL
REINFORCEMENT
AREA OF MODIFICATION STGR13RH A Z250 STGR13LH G_SB_533251_6_SAAA_01_03 Figure A-GSAAA - Sheet 01 DATE: May 13/15 SERVICE BULLETIN No.: A330-53-3251 REVISION No.: 01 - Jun 23/16 Page: 5 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A330
SERVICE BULLETIN
SUMMARY This Page Intentionally Left Blank DATE: May 13/15 SERVICE BULLETIN No.: A330-53-3251 REVISION No.: 01 - Jun 23/16 Page: 6 6 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.