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@A300-600
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: 31 TITLE: INSTRUMENTS - INDICAT ING / RECORDING SYSTEMS - ECAM SYSTEM - INSTALL NEW SGU ECAM W32.
MODIFICATION No.: 12691S22333 13051S22550 13081S22590 13149S22624 This page transmits Revision No.03 of Service Bulletin No.A300-31-6113
ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue.
REASON Revision No. 03 issued to update the compliance, the commercial policy and the effectivity.
CHANGES The main changes of this revision are:
- Effectivity updated
- COMPLIANCE paragraph updated from recommended to mandatory
- PUBLICATION AFFECTED paragraph updated
- MATERIAL INFORMATION paragraph updated
- PROCEDURE paragraph updated
- Minor changes applied.
FRONT MATTER
INSTRUMENTS - INDICATING /
RECORDING SYSTEMS - ECAM
SYSTEM - INSTALL NEW SGU ECAM W32.
CONFIGURATION UPDATED R DATE: Jan 04/06 SERVICE BULLETIN No.: A300-31-6113 REVISION No.: 03 - Jul 05/16 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
SUMMARY
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
MATERIAL PRICE INFORMATION TABLE
UPDATED R
EFFECTIVITY
OPERATOR LIST UPDATED R
CONCURRENT REQUIREMENTS
CONCURRENT REQUIREMENTS UPDATED R
CONCURRENT REQUIREMENTS UPDATED R
CONCURRENT REQUIREMENTS UPDATED R
CONCURRENT REQUIREMENTS UPDATED R
REFERENCES / REPERCUSSIONS
REFERENCES/REPERCUSSIONS TABLE
UPDATED R
MANPOWER
MANPOWER UPDATED R
MANPOWER UPDATED R
MANPOWER UPDATED R
MANPOWER UPDATED R
APPENDICES
APPENDICES UPDATED R Fig. A-FSAAA
FIGURE SOLUTION UPDATED
CONFIGURATION UPDATED R Fig. A-FSAAA Sheet 01
SHEET UPDATED R Fig. A-FSAAB
FIGURE SOLUTION ADDED N Fig. A-FSAAB Sheet 01
SHEET ADDED N
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 CONF 003
CONFIGURATION DEFINITION UPDATED
CONFIGURATION DESCRIPTION UPDATED R CONF 004
CONFIGURATION DEFINITION UPDATED
CONFIGURATION DESCRIPTION UPDATED R Material Effectivity
MATERIAL EFFECTIVITY UPDATED
CONFIGURATION UPDATED
MATERIAL SET UPDATED R
MATERIAL EFFECTIVITY UPDATED
CONFIGURATION UPDATED
MATERIAL SET UPDATED R DATE: Jan 04/06 SERVICE BULLETIN No.: A300-31-6113 REVISION No.: 03 - Jul 05/16 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
MATERIAL EFFECTIVITY UPDATED
CONFIGURATION UPDATED
MATERIAL SET UPDATED R
MATERIAL EFFECTIVITY UPDATED
CONFIGURATION UPDATED
MATERIAL SET UPDATED R
CONCURRENT REQUIREMENTS
CONCURRENT SB LIST UPDATED R
CONCURRENT SB LIST UPDATED R
CONCURRENT SB LIST UPDATED R
CONCURRENT SB LIST UPDATED R REASON History
HISTORY UPDATED R Objective/Action
OBJECTIVE/ACTION UPDATED R Advantages
ADVANTAGES UPDATED R Operational/Maintenance Consequences
OPERATIONAL/MAINTENANCE CONSEQUENCES
UPDATED R
DESCRIPTION
DESCRIPTION UPDATED R
COMPLIANCE Classification
CLASSIFICATION UPDATED R Accomplishment Timescale
ACCOMPLISHMENT TIMESCALE UPDATED R
APPROVAL
APPROVAL UPDATED R
MANPOWER
MANPOWER UPDATED R
MANPOWER UPDATED R
MANPOWER UPDATED R
MANPOWER UPDATED R
REFERENCES
REFERENCED DOCUMENTATION UPDATED R
REFERENCED DOCUMENTATION UPDATED R
REFERENCED DOCUMENTATION UPDATED R
REFERENCED DOCUMENTATION UPDATED R
PUBLICATION AFFECTED
PUBLICATIONS AFFECTED UPDATED R SPARES
SPARES 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
LIST OF COMPONENTS
LIST OF COMPONENTS UPDATED R
LIST OF MATERIALS - OPERATOR
SUPPLIED Components Component COMPA01
PART MATERIAL SET UPDATED R DATE: Jan 04/06 SERVICE BULLETIN No.: A300-31-6113 REVISION No.: 03 - Jul 05/16 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
ACCOMPLISHMENT INSTRUCTIONS TASK 316113- 831-802-001-OPTION 1 - Modification of the two ECAM SGUs (9WT1 and 9WT2) in accordance with VSB on Bench
TASK SOLUTION UPDATED
TASK TITLE UPDATED
NOTE UPDATED R Task associated data - 001
MAN HOURS UPDATED
ELAPSED TIME UPDATED R Task associated data - 002
MAN HOURS UPDATED
ELAPSED TIME UPDATED R Task associated data - 003
MAN HOURS UPDATED
ELAPSED TIME UPDATED R Task associated data - 004
MAN HOURS UPDATED
ELAPSED TIME UPDATED R Subtask 316113-910-002-003
SUBTASK SOLUTION ADDED N Subtask 316113-910-002-001
SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN D Subtask 316113-910-002-001
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED R Subtask 316113-910-002-001
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED R Subtask 316113-941-002-001
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
FIN UPDATED
REFERENCES UPDATED
NOTE UPDATED R Subtask 316113-941-002-002
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED R Subtask 316113-941-002-003
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
FIN UPDATED
REFERENCES UPDATED R Subtask 316113-941-002-003
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
FIN UPDATED
REFERENCES UPDATED R Subtask 316113-960-001-001
SUBTASK SOLUTION UPDATED
NOTE UPDATED
MANPOWER RESSOURCE UPDATED R Subtask 316113-831-015-001
SUBTASK SOLUTION UPDATED R Subtask 316113-420-001-001
SUBTASK SOLUTION UPDATED
MANPOWER RESSOURCE UPDATED R Subtask 316113-831-016-001
SUBTASK SOLUTION UPDATED R Subtask 316113-960-001-002
SUBTASK SOLUTION UPDATED
NOTE UPDATED
MANPOWER RESSOURCE UPDATED R Subtask 316113-831-015-002
SUBTASK SOLUTION UPDATED R DATE: Jan 04/06 SERVICE BULLETIN No.: A300-31-6113 REVISION No.: 03 - Jul 05/16 Page: 4 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET Subtask 316113-420-001-002
SUBTASK SOLUTION UPDATED
MANPOWER RESSOURCE UPDATED R Subtask 316113-960-001-003
SUBTASK SOLUTION UPDATED
NOTE UPDATED
MANPOWER RESSOURCE UPDATED R Subtask 316113-831-015-003
SUBTASK SOLUTION UPDATED R Subtask 316113-831-017-001
SUBTASK SOLUTION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED R Subtask 316113-420-001-003
SUBTASK SOLUTION UPDATED
MANPOWER RESSOURCE UPDATED R Subtask 316113-960-001-004
SUBTASK SOLUTION UPDATED
NOTE UPDATED
MANPOWER RESSOURCE UPDATED R Subtask 316113-831-015-004
SUBTASK SOLUTION UPDATED R Subtask 316113-831-017-002
SUBTASK SOLUTION UPDATED
FIGURE REFERENCE UPDATED
CONFIGURATION UPDATED
REFERENCES UPDATED R Subtask 316113-420-001-004
SUBTASK SOLUTION UPDATED
MANPOWER RESSOURCE UPDATED R Subtask 316113-700-002-001
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
FIN UPDATED
REFERENCES UPDATED R Subtask 316113-700-002-002
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED R Subtask 316113-700-002-003
SUBTASK SOLUTION UPDATED
FIN UPDATED
REFERENCED DOCUMENTATION UPDATED R Subtask 316113-700-002-003
SUBTASK SOLUTION UPDATED
FIN UPDATED
REFERENCED DOCUMENTATION UPDATED R Subtask 316113-942-002-002
SUBTASK SOLUTION UPDATED R Subtask 316113-942-002-001
SUBTASK SOLUTION UPDATED R Subtask 316113-942-002-001
SUBTASK SOLUTION UPDATED R Subtask 316113-942-002-001
SUBTASK SOLUTION UPDATED R TASK 316113- 831-801-001-OPTION 2 - Modification by Replacement of the two ECAM SGUs (9WT1 and 9WT2) on aircraft
TASK SOLUTION UPDATED
TASK TITLE UPDATED
NOTE UPDATED R Subtask 316113-910-001-005
SUBTASK SOLUTION ADDED N Subtask 316113-910-001-003
SUBTASK SOLUTION DELETED FOR
APPLICABLE MSN D Subtask 316113-910-001-003
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED R DATE: Jan 04/06 SERVICE BULLETIN No.: A300-31-6113 REVISION No.: 03 - Jul 05/16 Page: 5 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET Subtask 316113-910-001-003
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED R Subtask 316113-941-001-005
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
FIN UPDATED
REFERENCES UPDATED R Subtask 316113-941-001-006
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED R Subtask 316113-941-001-004
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
FIN UPDATED
REFERENCES UPDATED R Subtask 316113-941-001-004
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
FIN UPDATED
REFERENCES UPDATED R Subtask 316113-831-006-001
SUBTASK SOLUTION UPDATED R Subtask 316113-831-007-001
SUBTASK SOLUTION UPDATED R Subtask 316113-831-008-001
SUBTASK SOLUTION UPDATED R Subtask 316113-831-009-001
SUBTASK SOLUTION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED R Subtask 316113-831-013-001
SUBTASK SOLUTION UPDATED
FIGURE REFERENCE UPDATED
REFERENCES UPDATED R Subtask 316113-700-001-004
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
FIN UPDATED
REFERENCES UPDATED R Subtask 316113-700-001-005
SUBTASK SOLUTION UPDATED
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED R Subtask 316113-700-001-006
SUBTASK SOLUTION UPDATED
FIN UPDATED
REFERENCED DOCUMENTATION UPDATED R Subtask 316113-700-001-006
SUBTASK SOLUTION UPDATED
FIN UPDATED
REFERENCED DOCUMENTATION UPDATED R Subtask 316113-942-001-003
SUBTASK SOLUTION UPDATED R Subtask 316113-942-001-002
SUBTASK SOLUTION UPDATED R Subtask 316113-942-001-002
SUBTASK SOLUTION UPDATED R Subtask 316113-942-001-002
SUBTASK SOLUTION UPDATED R Fig. A-FBAAA
FIGURE SOLUTION UPDATED
CONFIGURATION UPDATED R Fig. A-FBAAA Sheet 01
SHEET UPDATED R Fig. A-FBAAB
FIGURE SOLUTION ADDED N Fig. A-FBAAB Sheet 01
SHEET ADDED N DATE: Jan 04/06 SERVICE BULLETIN No.: A300-31-6113 REVISION No.: 03 - Jul 05/16 Page: 6 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET Fig. A-FBAAC
FIGURE SOLUTION ADDED N Fig. A-FBAAC Sheet 01
SHEET ADDED N Fig. A-FBAAD
FIGURE SOLUTION ADDED N Fig. A-FBAAD Sheet 01
SHEET ADDED N Fig. A-FWDAA
FIGURE SOLUTION UPDATED R Fig. A-FHDAA
FIGURE SOLUTION UPDATED R Appendix 01 - Retrof itted Modifications
APPENDIX CONTENT
APPENDIX CONTENT UPDATED R Fig. A-FAAAA
FIGURE SOLUTION UPDATED R
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 No previous revisions.
Revision No. 01 is issued to :
replace in para. 1.A.(2).c Mod. 12691S22624 by Mod. 12691S22333 and to move MSN 0358, 0361, 0365, 0388, 0417, 0477, 0479 and 0543 from config. 03 to config. 02.
Revision No. 02 is issued to add the installation of module 83VT10 and add two wires.
REVISION SEQUENCE ORIGINAL: Jan 04/06 REVISION No. : 02 - Sep 04/14 REVISION No. : 03 - Jul 05/16 DATE: Jan 04/06 SERVICE BULLETIN No.: A300-31-6113 REVISION No.: 03 - Jul 05/16 Page: 7 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET This Page Intentionally Left Blank DATE: Jan 04/06 SERVICE BULLETIN No.: A300-31-6113 REVISION No.: 03 - Jul 05/16 Page: 8 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
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: 31 TITLE: INSTRUMENTS - INDICAT ING / RECORDING SYSTEMS - ECAM SYSTEM - INSTALL NEW SGU ECAM W32.
**CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION MAJOR 12691S22333 MINOR 13051S22550 13081S22590 13149S22624 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 This Service Bulletin is published to advise all operators of A300-600 aircraft, equipped with THALES AVIONICS Electronic Centralized Aircraft Monitoring (ECAM) Symbol Generator Units (SGUs) standard W30 (PN 9612670330, MOD No.
12134S21588 or Service Bulletin No. A300-31-6087) of the issue of THALES Service Bulletin No. 961267-31-050 .
The modification consists in:
- Replacing the two ECAM SGUs PN 9612670330 by two new ECAM SGUs PN 9612670332,
- Modifying the ECAM SGUs pin-programming of CARGO aircraft,
- Adapting the wiring of some aircraft.
New ECAM SGU W32 standard (PN 9612670332, MOD No.
12691S22333) has been launched to provide improvements of ECAM operation and to cancel OEB 112 applicable to aircraft equipped with ECAM SGU W30 standard PN 9612670330 installed by MOD No.
12134S21588 or Service Bulletin No.
A300-31-6087.
The following improvements have been implemented in the new ECAM SGU W32 standard:
- Basic improvements:
DATE: Jan 04/06 SERVICE BULLETIN No.: A300-31-6113 REVISION No.: 03 - Jul 05/16 Page: 1 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY . The MEMO message PARKING BRAKE ON is amber (instead of green) in the flight phases 3 to 10 (and green in the other flight phases 1,2,11 and 12).
. Improvement of the following ECAM alert procedures:
EXCESS CAB ALT
PITOT HEAT FAULT SMOKE alerts
TRIM TK AFT XFR NOT AVAIL TRIM TK PUMP 1+2 LO PR/OFF
MAIN DECK CARGO NOT CLOSED PITCH TRIM 1+2 FAULT/OFF
BLEED LEAK PACK 1 (and 2) OVHT
HOT AIR SUPPLY OVHT L/G alerts, which procedures deal with the autobrake Alerts, which procedures deal with the BRK/ANTI SKID
APU FUEL LO PR
L/G DOORS NOT CLOSED . Addition of "IF NO FUEL LEAK" before some "-FUEL X FEED IN LINE" action line in ECAM warning procedures asking to put the fuel cross feed in line.
. Modification of the Aileron scale on the FLT CTL page, . "IF" and "WHEN" philosophy completion in order to have a clear and homogeneous ECAM philosophy concerning the display of the action lines conditioned by an "IF " or a "WHEN".
. Harmonization of Quick Reference Handbook (QRH) and ECAM warning procedures.
- Basic improvements for aircraft equipped with the predictive windshear provisions: aircraft with MOD No.
10890S20867 (INSTALL WIRING PROVISIONS FOR BENDIX WEATHER RADAR WITH PREDICTIVE WINDSHEAR FUNCTION).
. Wiring modification to change the System Data Analog Converter (SDAC) input receiving the OFF position of the predictive windshear switch.
. Wiring modification to change the characteristics of the signal received by the SDAC from the T.O config.test push-button . This wiring modification has to be performed by implementing Service Bulletin No. A300-31-6117 (MOD No.
13062S22582) and must be accomplished before Service Bulletin No. A300-31-6113.
- Basic improvements for aircraft equipped with the predictive windshear function (aircraft with MOD No.
12132S21810 or MOD No.
12836S22439):
. The MEMO message PRED. W/S OFF is amber (instead of green) in approach flight phases (3, 4, 5, 6, 8, 9 and 10) and in flight phase 2 after a T.O. config. test.
- Basic improvement for all CARGO aircraft:
. Wiring modification to activate the "CARGO aircraft" ECAM SGU pin programming created within the ECAM SGU W32 standard to differentiate the SMOKE procedures between the CARGO aircraft and the Passengers aircraft.
DATE: Jan 04/06 SERVICE BULLETIN No.: A300-31-6113 REVISION No.: 03 - Jul 05/16 Page: 2 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY
- Basic wiring modification for some CARGO aircraft:
. For aircraft equipped with COURIER signs lighting (instead of SUPERNUMEMARY signs lighting), a SDAC wiring modification is required to provide related ECAM wording.
. For aircraft equipped with an EXIT selector (instead of a NO SMOKING selector) on the lighting signs panel, a SDAC wiring modification is required to provide related ECAM wording.
- Optional improvements:
. For aircraft equipped with optional MOD No.
12710S22349 ("Modification of Hydraulic Quantity Indicator", Service Bulletin No. A300-29-6052), modification of the scale giving the hydraulic quantity on the HYD syst em page to add 2 white lines symbolising an extended range in case of extreme temperature. A wiring modification is necessary to activate this option. This wiring modification has to be performed by implementing Service Bulletin No. A300-31-6116 (MOD No.
13073S22450).
. Introduction of a new optional software pin program combination allowing to suppress the trim tank from some specific aircraft configuration. This combination allows to combine the following ECAM options: A300-600 + GE CF6-80C motorization + FUEL TEMP. (FAA option ) + MESSIER CARBON brakes + BRAKE FAN + Lbs (instead of Kg) + degree F (instead of degree C)+ TAXI SPEED.
NOTE : For PAX to freighter converted aircraft by STC HOLDER a new modification activating cargo aircraft specificities on ECAM Display should be embodied.
NOTE : For PAX to freighter converted aircraft by STC HOLDER and equipped with COURIER signs lighting (instead of SUPERNUMERARY signs lighting), a SDAC wiring modification is required to provide related ECAM wording.
NOTE : For PAX to freighter converted aircraft by STC HOLDER and equipped with an EXIT selector (instead of a NO SMOKING selector) on the lighting signs panel, a SDAC wiring modification is required to provide related ECAM wording.
NOTE : For CARGO aircraft, with ECAM SGU in Softwa re pin programming configuration (the 2 plugs TP 14E and TP 11J of the ECAM SGU rear connector are grounded), a preliminary study has to be performed to adapt software pin prog configuration to hardware pin prog configuration.
This Service Bulletin cancels Operations Engineering Bulletin No. 112. Operators having programmed an OEB reminder should delete the reminder(s) from their system.
The Operational/Maintenance Consequences of this Service Bulletin are covered by the update of the affected publications detailed in ’PLANNING INFORMATION’.
This Service Bulletin has an impact on flight operations documentation; refer to AirbusWorld to consult the available Modification Operational Impact (MOI).
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE
MANDATORY
(1)
CANCELS INSPECTION SB NO
POTENTIAL AD YES
A/C OPERATION AFFECTED YES DATE: Jan 04/06 SERVICE BULLETIN No.: A300-31-6113 REVISION No.: 03 - Jul 05/16 Page: 3 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A300-600
SERVICE BULLETIN
SUMMARY
EVALUATION TABLE
RELIABILITY AFFECTED NO
PAX COMFORT AFFECTED NO
COST SAVING NO
ETOPS AFFECTED NO
STRUCTURAL LIFE EXTN NO
VENDOR SB INVOLVED YES 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 Equipment BFEA01 1 See SB
ECAM SGU Equipment BFEA02 1 See SB
ECAM SGU Component COMPA01 1 See SB contact **CONF 002
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Equipment BFEA01 1 See SB
ECAM SGU Equipment BFEA02 1 See SB
ECAM SGU **CONF 003
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Kit 316113A01R00 1
237.00 bundle Kit 316113A02R00 1
194.00 bundle TOTAL
431.00 Equipment BFEA01 1 See SB
ECAM SGU Equipment BFEA02 1 See SB
ECAM SGU **CONF 004
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
QTY PER A/C
PRICE PER
A/C (USD)
MAIN PARTS Kit 316113A01R00 1
237.00 bundle Kit 316113A02R00 1
194.00 bundle Kit 316113A03R00 1
258.00 bundle, module, hardware TOTAL
689.00 Equipment BFEA01 1 See SB
ECAM SGU DATE: Jan 04/06 SERVICE BULLETIN No.: A300-31-6113 REVISION No.: 03 - Jul 05/16 Page: 4 5 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.