A318/A319/A320/A321 SERVICE BULLETIN REV 00 Jan 28/21 A320-56-1022 Page 1 CONF ALL AIRBUS 2, ROND POINT EMILE DEWOITINE 31700 BLAGNAC FRANCE The content of this document is the property of Airbus. All rights including copyrights are reserved. It is supplied in confidence and commercial security on its contents must be maintained. It must not be used for any purpose other than that for which it is supplied, nor may information contained in it be disclosed to unauthorized persons. It must not be reproduced in whole or in part without permission in writing from the owners of the copyright. Requests for reproduction of any data in this document and the media authorized for it must be addressed to Airbus. MANDATORY MANDATORY MANDATORY ATA SYSTEM: 56 TITLE: WINDOWS - FIXED WINDOWS - INSPECTION OF SAINT-GOBAIN SULLY FRONT WINDSHIELD ON CEO AIRCRAFT MODIFICATION No.: None
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A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 1
CONF ALLAIRBUS2, ROND POINT EMILE DEWOITINE31700 BLAGNACFRANCE The content of this document is the property of Airbus. All rights including copyrights are reserved.It is supplied in confidence and commercial security on its contents must be maintained.It must not be used for any purpose other than that for which it is supplied, nor may informationcontained in it be disclosed to unauthorized persons.It must not be reproduced in whole or in part without permission in writing from the owners of thecopyright. Requests for reproduction of any data in this document and the media authorized for it mustbe addressed to Airbus.
MANDATORY MANDATORY MANDATORYATA SYSTEM: 56
TITLE: WINDOWS - FIXED WINDOWS - INSPECTION OF SAINT-GOBAIN SULLYFRONT WINDSHIELD ON CEO AIRCRAFT
MODIFICATION No.:None
A318/A319/A320/A321SERVICE BULLETIN
SUMMARY
REV 00 Jan 28/21 A320-56-1022Page 2
ATA SYSTEM: 56
TITLE: WINDOWS - FIXED WINDOWS - INSPECTION OF SAINT-GOBAIN SULLYFRONT WINDSHIELD ON CEO AIRCRAFT
SUMMARYThis summary is for information only and is not approved for modification of the aircraft.A. MODIFICATIONS
MODIFICATION CLASSIFICATIONMAJOR NoneMINOR None
NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on themass, balance, structural strength, reliability, operational characteristics affectingthe airworthiness of the product. All other changes are major changes.
B. REASON
(1) HistoryAirbus received a report on an in-service event on A319 aircraft about the loss of theRH side windshield in flight, during the cruise phase. The windshield was the originalfrom delivery, manufactured by SAINT-GOBAIN SULLY SAS (SGS). The investigationof the A319 event determined that both structural plies of the RH windshield weredamaged, due to a continuous arcing in the windshield heating system (at the levelof the power supply wires). Such electrical arcing requires a combination of at leastthe following contributing factors: mechanical damage to the insulation sleeve of thepower supply wires and water ingress resulting in the wires corrosion. Several tens ofseconds after the failure of the 2 structural plies, the last ply failed (outer ply, non-structural) and the windshield was ejected due to the pressurization loads.
(2) Objective/ActionThis Inspection Service Bulletin is published to advise all operators of the A320 familyaircraft of the issue of Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001, which providesinstructions to inspect the front windshields (FINs 3DG1 and 3DG2) potentiallyaffected by water ingress and corrosion within the windshield heating system. TheSGS PNs (all serial numbers) impacted have been defined in 3 groups:Group 1:
NOTE: This Service Bulletin is applicable to all of the above base PNs, regardless ofthe amendment letter.
(3) AdvantagesAccomplishment of this Inspection Service Bulletin will enable an early detection ofpotential water ingress and corrosion damage in the windshield electrical heatingsystem.
(4) Operational/Maintenance ConsequencesThe Operational/Maintenance Consequences of this Service Bulletin are covered bythe update of the affected publications detailed in "PLANNING INFORMATION".
CANCELS INSPECTION SB NO ETOPS AFFECTED NOPAX COMFORT AFFECTED NO POTENTIAL AD YESRELIABILITY AFFECTED NO STRUCTURAL LIFE EXTENSION NOLIFE LIMIT NO LINE MAINTENANCE AFFECTED NO
NOTE: Service Bulletin must be accomplished.
D. MAINTENANCE CONFIGURATIONNo specific aircraft maintenance configuration required.
E. MATERIAL PRICE INFORMATION
(1) Inspection of the PN of the Front Windshields Installed on the Aircraft(a) Task set A320-A-56-XX-1022-01000-93BA-A Inspection of the PN of the Front
Windshields Installed on the AircraftNo material
(2) Detailed Inspection of the Front Windshields for Group 1 (Depending on thePN of the Windshields)(a) Task set A320-A-56-XX-1022-02000-93BA-A Detailed Inspection of the Front
Windshields for Group 1 (Depending on the PN of the Windshields)
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS
Aircraft standard tools See SB See Note Windshield inspection tool
NOTE: Price information to be obtained from the given supplier.
(3) Detailed Inspection of the Front Windshields for Group 2 (Depending on thePN of the Windshields)
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SUMMARY
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(a) Task set A320-A-56-XX-1022-03000-93BA-A Detailed Inspection of the FrontWindshields for Group 2 (Depending on the PN of the Windshields)
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET QTYPER A/C PRICE PER A/C MAIN PARTS
Aircraft standard tools See SB See Note Windshield inspection tool
NOTE: Price information to be obtained from the given supplier.
(4) Detailed Inspection of the Front Windshields for Group 3 (Depending on thePN of the Windshields)(a) Task set A320-A-56-XX-1022-04000-93BA-A Detailed Inspection of the Front
Windshields for Group 3 (Depending on the PN of the Windshields)No material
(5) Replacement of the Front Windshields on the Aircraft (Depending on theInspection Result)(a) Task set A320-A-56-XX-1022-01000-93CA-A Replacement of the Front
Windshields on the Aircraft (Depending on the Inspection Result)No material
F. APPLICABILITYThis Service Bulletin is applicable to this (these) operator(s):01N 02K 03Q 06R 08M 09J 10N 11K 11S 11X 13Y 14S 15S 15T 17M 17R 19R 20M 23R 25P26L 27V 28M 29S 31V 31X 32Q 33T 34K 34L 36R 39K 39N 39V 40N 40S 41N 41S 43S 46L46O 46U 47P 48O 48P 48T 49N 49O 50T 51T 52K 52L 53Z 56O 58L 59Z 60U 60X 61W 66X68M 69X 72T 73W 75K 76W 78X 80X 81K 82M 82U 82W 83O 83Q 83V 85T 85Z 86K 86P 86Z87Q 87Z 89Q 90U 91X 95V 95W 96O 96Q 96U 98W 98X 99W A1L AAF AAL AAR AAV AAWAAY ABL ABN ABQ ABY ACA ACI ADY AEE AEG AFL AFR AHY AIC AIJ ALK AMC AMU AMV ANAANZ APJ ART ARU ASA ASL ASV AUA AUH AVA AVJ AWC AWG AWW AXE AXM AZA B2V BAVBAW BDJ BEC BEL BGF BGH BJN BKP BNL BRS BSX BTK BTN BUC BWJ C2C CBG CBJ CCA CCMCDC CEB CEF CES CFG CGH CHB CLH CQH CQN CRK CSA CSC CSN CSZ CTB CTN CTV CWSCYP D2F DAL DCS DKH DLH DNU DQA DRK EAF EDW EFA EIN ELB EOK ETD ETJ EVA EVE EWEEWG EXS EZY F2I FAD FBS FFT FHM FHY FIA FIN FLI FOO FRN G2X G4I G8E GAF GAP GBBGCR GFA GJM GJT GLG GMI GOW GSH GSW GTR GWI GWR GZQ HDA HES HFM HFY HIM HKEHKJ HVN HXA HYM HYR HYS IAC IAW IBE IBS IGO IND IRA IRB IRC IRM ISR IYE IZG JAD JAT JAVJBU JBW JCC JES JJP JOC JSA JST JZR KAC KAY KHV KIS KKK KME KNE KZR LAA LAN LAO LBTLDA LDM LFO LHT LKE LLM LMJ LMU LUR LVT LWA LYX LZB MAC MAU MEA MJF MJN MKR MLDMLM MMA MMM MMO MRJ MSC MSR MXA MYX NIA NKS NMA NMB NUM NVD NWK NWS O2XO8K OEW OHY OLY ONE ORF OTC OTF OZW PAL PGT PIA PIC PKZ PLM QAF QDA QQE QSMQTR R1T RBA RBG RIH RJA RJD RNA ROT RSD RSY RWZ RYL RZO S2A SAA SAS SAW SBI SDMSDR SEK SFJ SFW SGQ SHJ SHU SHY SKU SLK SND SNG SOL SOR SSG SSV SUD SVA SVR SVWSWM SWR SYR SZN T2R TAE TAI TAM TAP TAR TBA TBJ TBZ TCI TDR TGW THD THY TNA TSCTTW U6A UAE UAL UEA UKN UNA UZB VAW VIP VIV VJC VKG VLG VNL VOE VOI VRE VTI VVCWHT WRC WZZ
G. CONCURRENT REQUIREMENTSNone
H. NATURE OF THE WORK
(1) Inspection of the PN of the Front Windshields Installed on the Aircraft
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(a) Task set A320-A-56-XX-1022-01000-93BA-A Inspection of the PN of the FrontWindshields Installed on the Aircraft
AIRCRAFT NOEQUIPMENT YES
(2) Detailed Inspection of the Front Windshields for Group 1 (Depending on thePN of the Windshields)(a) Task set A320-A-56-XX-1022-02000-93BA-A Detailed Inspection of the Front
Windshields for Group 1 (Depending on the PN of the Windshields)
AIRCRAFT NOEQUIPMENT YES
(3) Detailed Inspection of the Front Windshields for Group 2 (Depending on thePN of the Windshields)(a) Task set A320-A-56-XX-1022-03000-93BA-A Detailed Inspection of the Front
Windshields for Group 2 (Depending on the PN of the Windshields)
AIRCRAFT NOEQUIPMENT YES
(4) Detailed Inspection of the Front Windshields for Group 3 (Depending on thePN of the Windshields)(a) Task set A320-A-56-XX-1022-04000-93BA-A Detailed Inspection of the Front
Windshields for Group 3 (Depending on the PN of the Windshields)
AIRCRAFT NOEQUIPMENT YES
(5) Replacement of the Front Windshields on the Aircraft (Depending on theInspection Result)(a) Task set A320-A-56-XX-1022-01000-93CA-A Replacement of the Front
Windshields on the Aircraft (Depending on the Inspection Result)
AIRCRAFT NOEQUIPMENT YES
I. MANPOWER
(1) Inspection of the PN of the Front Windshields Installed on the Aircraft(a) Task set A320-A-56-XX-1022-01000-93BA-A Inspection of the PN of the Front
Windshields Installed on the Aircraft
MANPOWERTOTAL MAN-HOURS 0.20 hELAPSED TIME (HOURS) 0.15 h
(2) Detailed Inspection of the Front Windshields for Group 1 (Depending on thePN of the Windshields)(a) Task set A320-A-56-XX-1022-02000-93BA-A Detailed Inspection of the Front
Windshields for Group 1 (Depending on the PN of the Windshields)
MANPOWERTOTAL MAN-HOURS 2.80 h
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MANPOWERELAPSED TIME (HOURS) 1.35 hAdditional man-hours related to Vendor SB; refer to:
Do a Detailed Inspection of theConnector in accordance with VSB(Depending on the Inspection Result)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
Prepare the Weather Seal beforeElectrical Tests in accordance with VSB(Depending on the Inspection Result)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
Repair the Weather Seal in accordancewith VSB (Depending on the InspectionResult)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
Do a Shop Inspection of the SpareWindshield in accordance with VSB(Depending on the Inspection Result)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
(3) Detailed Inspection of the Front Windshields for Group 2 (Depending on thePN of the Windshields)(a) Task set A320-A-56-XX-1022-03000-93BA-A Detailed Inspection of the Front
Windshields for Group 2 (Depending on the PN of the Windshields)
MANPOWERTOTAL MAN-HOURS 2.80 hELAPSED TIME (HOURS) 1.35 hAdditional man-hours related to Vendor SB; refer to:
Do a Detailed Inspection of theConnector in accordance with VSB(Depending on the Inspection Result)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
Prepare the Weather Seal beforeElectrical Tests in accordance with VSB(Depending on the Inspection Result)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
Repair the Weather Seal in accordancewith VSB (Depending on the InspectionResult)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
Do a Shop Inspection of the SpareWindshield in accordance with VSB(Depending on the Inspection Result)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
(4) Detailed Inspection of the Front Windshields for Group 3 (Depending on thePN of the Windshields)(a) Task set A320-A-56-XX-1022-04000-93BA-A Detailed Inspection of the Front
Windshields for Group 3 (Depending on the PN of the Windshields)
MANPOWERTOTAL MAN-HOURS 1.50 hELAPSED TIME (HOURS) 0.95 hAdditional man-hours related to Vendor SB; refer to:
Do a Detailed Inspection of theConnector in accordance with VSB(Depending on the Inspection Result)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
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MANPOWERDo a Shop Inspection of the SpareWindshield in accordance with VSB(Depending on the Inspection Result)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
(5) Replacement of the Front Windshields on the Aircraft (Depending on theInspection Result)(a) Task set A320-A-56-XX-1022-01000-93CA-A Replacement of the Front
Windshields on the Aircraft (Depending on the Inspection Result)
MANPOWERTOTAL MAN-HOURS 20.00 hELAPSED TIME (HOURS) 10.00 h
A318/A319/A320/A321SERVICE BULLETIN
SUMMARY
Figure ICN-A320-A-56XX1022-A-FAPE3-024F3-A-003-01 SHEET 1/1REV 00 Jan 28/21 A320-56-1022General Overview
Page 8
J. GENERAL OVERVIEWCONF ALL
A
FR1
FR12A
Z210
INSPECTION OF THE FRONT WINDSHIELDS
3DG1
3DG2
ICN-A320-A-56XX1022-A-FAPE3-024F3-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
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ATA SYSTEM: 56
TITLE: WINDOWS - FIXED WINDOWS - INSPECTION OF SAINT-GOBAIN SULLYFRONT WINDSHIELD ON CEO AIRCRAFT
1. PLANNING INFORMATIONA. APPLICABILITY
NOTE: This Service Bulletin is only applicable to aircraft fitted with SAINT-GOBAIN SULLYwindshield and with these PNs, regardless the amendment letters:- STA320-1-3-1- STA320-2-3-1- STA320-1-4-1- STA320-2-4-1- STA320-1-5-1- STA320-2-5-1- STA320-1-6-1- STA320-2-6-1- STA320-1-7-1- STA320-2-7-1- STA320-1-8-2- STA320-2-8-2
NOTE: This Service Bulletin is not applicable to aircraft on which both PNs STA320-1-9-3and STA320-2-9-3 are installed.
Configuration 001CONF 001 is applicable for all the aircraft affected by this Service Bulletin as astandard configuration.
B. CONCURRENT REQUIREMENTSNone
C. REASON
(1) HistoryAirbus received a report on an in-service event on A319 aircraft about the loss of theRH side windshield in flight, during the cruise phase. The windshield was the originalfrom delivery, manufactured by SAINT-GOBAIN SULLY SAS (SGS). The investigationof the A319 event determined that both structural plies of the RH windshield weredamaged, due to a continuous arcing in the windshield heating system (at the levelof the power supply wires). Such electrical arcing requires a combination of at leastthe following contributing factors: mechanical damage to the insulation sleeve of thepower supply wires and water ingress resulting in the wires corrosion. Several tens ofseconds after the failure of the 2 structural plies, the last ply failed (outer ply, non-structural) and the windshield was ejected due to the pressurization loads.
(2) Objective/ActionThis Inspection Service Bulletin is published to advise all operators of the A320 familyaircraft of the issue of Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001, which providesinstructions to inspect the front windshields (FINs 3DG1 and 3DG2) potentiallyaffected by water ingress and corrosion within the windshield heating system. TheSGS PNs (all serial numbers) impacted have been defined in 3 groups:Group 1:
NOTE: This Service Bulletin is applicable to all of the above base PNs, regardless ofthe amendment letter.
(3) AdvantagesAccomplishment of this Inspection Service Bulletin will enable an early detection ofpotential water ingress and corrosion damage in the windshield electrical heatingsystem.
(4) Operational/Maintenance ConsequencesThe Operational/Maintenance Consequences of this Service Bulletin are covered bythe update of the affected publications detailed in "PLANNING INFORMATION".
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D. DESCRIPTIONTo accomplish this Service Bulletin it is necessary to:(1) Inspection of the PN of the Front Windshields Installed on the Aircraft
(a) Task set A320-A-56-XX-1022-01000-93BA-A Inspection of the PN of the FrontWindshields Installed on the Aircraft1 Inspect the PN of the LH side Front Windshield on the Aircraft2 Inspect the PN of the RH side Front Windshield on the Aircraft
(2) Detailed Inspection of the Front Windshields for Group 1 (Depending on thePN of the Windshields)(a) Task set A320-A-56-XX-1022-02000-93BA-A Detailed Inspection of the Front
Windshields for Group 1 (Depending on the PN of the Windshields)1 Do the Inspection of the LH side Front Windshield2 Do the Inspection of the RH side Front Windshield3 Do a Detailed Inspection of the Connector in accordance with VSB
(Depending on the Inspection Result)4 Prepare the Weather Seal before Electrical Tests in accordance with VSB
(Depending on the Inspection Result)5 Repair the Weather Seal in accordance with VSB (Depending on the
Inspection Result)6 Do a Shop Inspection of the Spare Windshield in accordance with VSB
(Depending on the Inspection Result)7 Complete and Send the Inspection Report Sheet, LH side8 Complete and Send the Inspection Report Sheet, RH side
(3) Detailed Inspection of the Front Windshields for Group 2 (Depending on thePN of the Windshields)(a) Task set A320-A-56-XX-1022-03000-93BA-A Detailed Inspection of the Front
Windshields for Group 2 (Depending on the PN of the Windshields)1 Do the Inspection of the LH side Front Windshield2 Do the Inspection of the RH side Front Windshield3 Do a Detailed Inspection of the Connector in accordance with VSB
(Depending on the Inspection Result)4 Prepare the Weather Seal before Electrical Tests in accordance with VSB
(Depending on the Inspection Result)5 Repair the Weather Seal in accordance with VSB (Depending on the
Inspection Result)6 Do a Shop Inspection of the Spare Windshield in accordance with VSB
(Depending on the Inspection Result)7 Complete and Send the Inspection Report Sheet, LH side8 Complete and Send the Inspection Report Sheet, RH side
(4) Detailed Inspection of the Front Windshields for Group 3 (Depending on thePN of the Windshields)(a) Task set A320-A-56-XX-1022-04000-93BA-A Detailed Inspection of the Front
Windshields for Group 3 (Depending on the PN of the Windshields)
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1 Do the Inspection of the LH side Front Windshield2 Do the Inspection of the RH side Front Windshield3 Do a Detailed Inspection of the Connector in accordance with VSB
(Depending on the Inspection Result)4 Do a Shop Inspection of the Spare Windshield in accordance with VSB
(Depending on the Inspection Result)5 Complete and Send the Inspection Report Sheet, LH side6 Complete and Send the Inspection Report Sheet, RH side
(5) Replacement of the Front Windshields on the Aircraft (Depending on theInspection Result)(a) Task set A320-A-56-XX-1022-01000-93CA-A Replacement of the Front
Windshields on the Aircraft (Depending on the Inspection Result)1 Remove the Damaged Front Windshield from the Aircraft, LH side2 Remove the Damaged Front Windshield from the Aircraft, RH side3 Install the Front Windshield on the Aircraft, LH side4 Install the Front Windshield on the Aircraft, RH side
E. COMPLIANCE
(1) ClassificationMANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment TimescaleAccomplishment of this Service Bulletin must be done in accordance with theaccomplishment timescale given in the Appendix COMPLIANCE TIMES.This Service Bulletin has been classified Mandatory. It is expected that anAirworthiness Directive (AD) published by the European Union Aviation Safety Agency(EASA) will be issued to confirm this classification. It is anticipated that the AD willconfirm the thresholds given but reference should be made to the AD for confirmationof the mandated accomplishment timescale.NOTE: For the presentation of the compliance times, refer to Appendix COMPLIANCETIMES.NOTE: This SB considers the possibility of a configuration with PNs from differentGroups on the LH and RH sides on the same aircraft.NOTE: A review of aircraft delivery and/or maintenance records is acceptable to makethe determination of the part installed, provided those records can be relied uponfor that purpose and the PN and SN of the part can be positively identified from thatreview.
F. APPROVALThe technical content of this document is approved under the authority of the DesignOrganisation Approval ref. EASA.21J.031.If an aircraft listed in the applicability has a modification or repair embodied that is notof AIRBUS origin, and which affects the content of this Service Bulletin, the operatoris responsible for obtaining approval by its airworthiness authority for any adaptationnecessary before incorporation of the Service Bulletin.
G. MANPOWER
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The manpower estimates given in this Service Bulletin are based on the direct labor cost todo 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 notinclude the time to prepare, plan or inspect the work. Manufacture and procurement of partsand tools, drying times for paints, sealants, etc., and general administration work are alsonot included.(1) Inspection of the PN of the Front Windshields Installed on the Aircraft
(a) Task set A320-A-56-XX-1022-01000-93BA-A Inspection of the PN of the FrontWindshields Installed on the Aircraft
PREPARATIONJob Set-up 0.05 h
PROCEDUREInspect the PN of the LH side Front Windshield on theAircraft
0.05 h
Inspect the PN of the RH side Front Windshield on theAircraft
0.05 h
PREPARATION FOR TESTNone
TESTNone
CLOSE-UPClose-up 0.05 h
TOTAL MAN-HOURS 0.20 hELAPSED TIME (HOURS) 0.15 h
NOTE: The minimum man-hours necessary to accomplish this Service Bulletinare those for the Inspection. Depending on the inspection result,additional man-hours can apply.
(2) Detailed Inspection of the Front Windshields for Group 1 (Depending on thePN of the Windshields)(a) Task set A320-A-56-XX-1022-02000-93BA-A Detailed Inspection of the Front
Windshields for Group 1 (Depending on the PN of the Windshields)
PREPARATIONJob Set-up 0.10 hRemove for Access the Lining Panels from the Aircraft 0.10 h
PROCEDUREDo the Inspection of the LH side Front Windshield 1.10 hDo the Inspection of the RH side Front Windshield 1.10 hComplete and Send the Inspection Report Sheet, LH side 0.10 hComplete and Send the Inspection Report Sheet, RH side 0.10 h
PREPARATION FOR TESTNone
TESTNone
CLOSE-UP
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Install the Lining Panels Removed for Access on the Aircraft 0.10 hClose-up 0.10 h
TOTAL MAN-HOURS 2.80 hELAPSED TIME (HOURS) 1.35 hAdditional man-hours related to Vendor SB; refer to:
Do a Detailed Inspection of theConnector in accordance with VSB(Depending on the Inspection Result)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
Prepare the Weather Seal beforeElectrical Tests in accordance with VSB(Depending on the Inspection Result)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
Repair the Weather Seal in accordancewith VSB (Depending on the InspectionResult)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
Do a Shop Inspection of the SpareWindshield in accordance with VSB(Depending on the Inspection Result)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
NOTE: The minimum man-hours necessary to accomplish this Service Bulletinare those for the Inspection. Depending on the inspection result,additional man-hours can apply.
(3) Detailed Inspection of the Front Windshields for Group 2 (Depending on thePN of the Windshields)(a) Task set A320-A-56-XX-1022-03000-93BA-A Detailed Inspection of the Front
Windshields for Group 2 (Depending on the PN of the Windshields)
PREPARATIONJob Set-up 0.10 hRemove for Access the Lining Panels from the Aircraft 0.10 h
PROCEDUREDo the Inspection of the LH side Front Windshield 1.10 hDo the Inspection of the RH side Front Windshield 1.10 hComplete and Send the Inspection Report Sheet, LH side 0.10 hComplete and Send the Inspection Report Sheet, RH side 0.10 h
PREPARATION FOR TESTNone
TESTNone
CLOSE-UPInstall the Lining Panels Removed for Access on the Aircraft 0.10 hClose-up 0.10 h
TOTAL MAN-HOURS 2.80 hELAPSED TIME (HOURS) 1.35 hAdditional man-hours related to Vendor SB; refer to:
Do a Detailed Inspection of theConnector in accordance with VSB(Depending on the Inspection Result)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
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Prepare the Weather Seal beforeElectrical Tests in accordance with VSB(Depending on the Inspection Result)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
Repair the Weather Seal in accordancewith VSB (Depending on the InspectionResult)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
Do a Shop Inspection of the SpareWindshield in accordance with VSB(Depending on the Inspection Result)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
NOTE: The minimum man-hours necessary to accomplish this Service Bulletinare those for the Inspection. Depending on the inspection result,additional man-hours can apply.
(4) Detailed Inspection of the Front Windshields for Group 3 (Depending on thePN of the Windshields)(a) Task set A320-A-56-XX-1022-04000-93BA-A Detailed Inspection of the Front
Windshields for Group 3 (Depending on the PN of the Windshields)
PREPARATIONJob Set-up 0.10 hRemove for Access the Lining Panels from the Aircraft 0.10 h
PROCEDUREDo the Inspection of the LH side Front Windshield 0.50 hDo the Inspection of the RH side Front Windshield 0.50 hComplete and Send the Inspection Report Sheet, LH side 0.05 hComplete and Send the Inspection Report Sheet, RH side 0.05 h
PREPARATION FOR TESTNone
TESTNone
CLOSE-UPInstall the Lining Panels Removed for Access on the Aircraft 0.10 hClose-up 0.10 h
TOTAL MAN-HOURS 1.50 hELAPSED TIME (HOURS) 0.95 hAdditional man-hours related to Vendor SB; refer to:
Do a Detailed Inspection of theConnector in accordance with VSB(Depending on the Inspection Result)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
Do a Shop Inspection of the SpareWindshield in accordance with VSB(Depending on the Inspection Result)
Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
NOTE: The minimum man-hours necessary to accomplish this Service Bulletinare those for the Inspection. Depending on the inspection result,additional man-hours can apply.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 45
(5) Replacement of the Front Windshields on the Aircraft (Depending on theInspection Result)(a) Task set A320-A-56-XX-1022-01000-93CA-A Replacement of the Front
Windshields on the Aircraft (Depending on the Inspection Result)
PREPARATIONJob Set-up 4.50 h
PROCEDURERemove the Damaged Front Windshield from the Aircraft,LH side
2.50 h
Remove the Damaged Front Windshield from the Aircraft,RH side
2.50 h
Install the Front Windshield on the Aircraft, LH side 2.50 hInstall the Front Windshield on the Aircraft, RH side 2.50 h
PREPARATION FOR TESTJob set-up 0.50 h
TESTTest 0.50 h
CLOSE-UPClose-up 4.50 h
TOTAL MAN-HOURS 20.00 hELAPSED TIME (HOURS) 10.00 h
H. WEIGHT AND BALANCENot changed
I. ELECTRICAL LOAD DATANot changed
J. REFERENCES
(1) Inspection of the PN of the Front Windshields Installed on the Aircraft(a) Task set A320-A-56-XX-1022-01000-93BA-A Inspection of the PN of the Front
ELECTRICAL STANDARD PRACTICES MANUAL (ESPM)20-54-50 20-55-00
IN SERVICE INFORMATION (ISI)00.00.00179
MASTER MINIMUM EQUIPMENT LIST (MMEL)30-42-03A 30-42-03B
NON DESTRUCTIVE TEST MANUAL (NTM)51-90-00
STRUCTURAL REPAIR MANUAL (SRM)51-42-00
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TECHNICAL FOLLOW UP (TFU)56.11.00014
VENDOR SERVICE BULLETIN (VSB)SAINT-GOBAIN (F0360) VSB STA320-56-001
(5) Replacement of the Front Windshields on the Aircraft (Depending on theInspection Result)(a) Task set A320-A-56-XX-1022-01000-93CA-A Replacement of the Front
Windshields on the Aircraft (Depending on the Inspection Result)
ELECTRICAL STANDARD PRACTICES MANUAL (ESPM)20-55-00
ILLUSTRATED PART CATALOG (IPC)56-11-01
TECHNICAL FOLLOW UP (TFU)56.11.00014
K. PUBLICATION AFFECTEDAIRCRAFT MAINTENANCE MANUAL (AMM)MASTER MINIMUM EQUIPMENT LIST (MMEL)This Service Bulletin has an impact on flight operations documentation. Refer to ISI00.00.00135 paragraph "Flight Operations Products" for further information on the updateof affected Flight Operations Products.Technical queries should be addressed through TechRequest on AirbusWorld using "TechnicalData/Support to report Service Bulletins" form.
L. INDUSTRY SUPPORT INFORMATIONThis Service Bulletin is the subject of an AIRBUS monitored retrofit campaign.For the organization of this retrofit, you are kindly requested to contact AIRBUS retrofitmanagement department: [email protected].
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2. MATERIAL INFORMATIONA. MATERIAL APPLICABILITY
No material for task set A320-A-56-XX-1022-01000-93BA-A Inspection of the PN ofthe Front Windshields Installed on the AircraftMaterial for task set A320-A-56-XX-1022-02000-93BA-A Detailed Inspection of theFront Windshields for Group 1 (Depending on the PN of the Windshields)
MATERIAL QTY SEE NOTESAircraft standard tools See SBReferenced tools See SBConsumables See SBReferenced consumables See SBReferenced parts See SB
Material for task set A320-A-56-XX-1022-03000-93BA-A Detailed Inspection of theFront Windshields for Group 2 (Depending on the PN of the Windshields)
MATERIAL QTY SEE NOTESAircraft standard tools See SBReferenced tools See SBConsumables See SBReferenced consumables See SBReferenced parts See SB
Material for task set A320-A-56-XX-1022-04000-93BA-A Detailed Inspection of theFront Windshields for Group 3 (Depending on the PN of the Windshields)
MATERIAL QTY SEE NOTESReferenced tools See SBReferenced consumables See SBReferenced parts See SB
Material for task set A320-A-56-XX-1022-01000-93CA-A Replacement of the FrontWindshields on the Aircraft (Depending on the Inspection Result)
MATERIAL QTY SEE NOTESReferenced tools See SBReferenced consumables See SBReferenced parts See SB
B. TOOLINGAircraft standard tools for task set A320-A-56-XX-1022-02000-93BA-A DetailedInspection of the Front Windshields for Group 1 (Depending on the PN of theWindshields)
Procurement address D4296
AIRBUS Material, Logistics and SuppliersCustomer Order FulfilmentWeg beim Jaeger 15022335 HAMBURGGERMANYPhone: +49 (0) 40 50 76 40 02E-mail: Please contact your Single Point Of Contact(SPOC)
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 50
Internet: http://spares.airbus.comNOTE(S)
Customers with aircraft shown in the applicability of this Service Bulletin should senda purchase order to AIRBUS at the address given above and quote the number of thisService Bulletin.
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES98D56003001000(D4296) 1 WINDSHIE
Aircraft standard tools for task set A320-A-56-XX-1022-03000-93BA-A DetailedInspection of the Front Windshields for Group 2 (Depending on the PN of theWindshields)
Procurement address D4296
AIRBUS Material, Logistics and SuppliersCustomer Order FulfilmentWeg beim Jaeger 15022335 HAMBURGGERMANYPhone: +49 (0) 40 50 76 40 02E-mail: Please contact your Single Point Of Contact(SPOC)Internet: http://spares.airbus.com
NOTE(S)Customers with aircraft shown in the applicability of this Service Bulletin should senda purchase order to AIRBUS at the address given above and quote the number of thisService Bulletin.
ITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES98D56003001000(D4296) 1 WINDSHIE
Referenced tools for task set A320-A-56-XX-1022-02000-93BA-A DetailedInspection of the Front Windshields for Group 1 (Depending on the PN of theWindshields)To accomplish this Service Bulletin it is necessary to use the tools listed in:Ref. AMM Task 56-11-11-000-001Ref. AMM Task 56-11-11-400-001Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001Referenced tools for task set A320-A-56-XX-1022-03000-93BA-A DetailedInspection of the Front Windshields for Group 2 (Depending on the PN of theWindshields)To accomplish this Service Bulletin it is necessary to use the tools listed in:Ref. AMM Task 56-11-11-000-001Ref. AMM Task 56-11-11-400-001Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001Referenced tools for task set A320-A-56-XX-1022-04000-93BA-A DetailedInspection of the Front Windshields for Group 3 (Depending on the PN of theWindshields)To accomplish this Service Bulletin it is necessary to use the tools listed in:
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Ref. AMM Task 56-11-11-000-001Ref. AMM Task 56-11-11-400-001Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001Referenced tools for task set A320-A-56-XX-1022-01000-93CA-A Replacement ofthe Front Windshields on the Aircraft (Depending on the Inspection Result)To accomplish this Service Bulletin it is necessary to use the tools listed in:Ref. AMM Task 56-11-11-000-001Ref. AMM Task 56-11-11-400-001
C. CONSUMABLESConsumables for task set A320-A-56-XX-1022-02000-93BA-A Detailed Inspectionof the Front Windshields for Group 1 (Depending on the PN of the Windshields)
ITEM REFERENCE CML DESCRIPTION DRAWING SEE NOTES
06AFB1 Polysulfide Sealant -Windshield Fillet
06PAG1 Adhesion Promoter - ForPolysulfide Sealant
Consumables for task set A320-A-56-XX-1022-03000-93BA-A Detailed Inspectionof the Front Windshields for Group 2 (Depending on the PN of the Windshields)
ITEM REFERENCE CML DESCRIPTION DRAWING SEE NOTES
06AFB1 Polysulfide Sealant -Windshield Fillet
06PAG1 Adhesion Promoter - ForPolysulfide Sealant
Referenced consumables for task set A320-A-56-XX-1022-02000-93BA-A DetailedInspection of the Front Windshields for Group 1 (Depending on the PN of theWindshields)To accomplish this Service Bulletin it is necessary to use the consumable materials listed in:Ref. AMM Task 56-11-11-400-001Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001Referenced consumables for task set A320-A-56-XX-1022-03000-93BA-A DetailedInspection of the Front Windshields for Group 2 (Depending on the PN of theWindshields)To accomplish this Service Bulletin it is necessary to use the consumable materials listed in:Ref. AMM Task 56-11-11-400-001Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001Referenced consumables for task set A320-A-56-XX-1022-04000-93BA-A DetailedInspection of the Front Windshields for Group 3 (Depending on the PN of theWindshields)To accomplish this Service Bulletin it is necessary to use the consumable materials listed in:Ref. AMM Task 56-11-11-400-001Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001
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Referenced consumables for task set A320-A-56-XX-1022-01000-93CA-AReplacement of the Front Windshields on the Aircraft (Depending on theInspection Result)To accomplish this Service Bulletin it is necessary to use the consumable materials listed in:Ref. AMM Task 56-11-11-400-001
D. LIST OF NEW PARTSReferenced parts for task set A320-A-56-XX-1022-01000-93CA-A Replacement ofthe Front Windshields on the Aircraft (Depending on the Inspection Result)To accomplish this Service Bulletin it is necessary to use the expendable parts listed in:Ref. AMM Task 56-11-11-400-001NOTE: Depending on the findings, the windshield may have to be replaced. To choose anapproved spare part, use IPC 56-11-01.Referenced parts for task set A320-A-56-XX-1022-02000-93BA-A DetailedInspection of the Front Windshields for Group 1 (Depending on the PN of theWindshields)To accomplish this Service Bulletin it is necessary to use the expendable parts listed in:Ref. AMM Task 56-11-11-400-001Referenced parts for task set A320-A-56-XX-1022-03000-93BA-A DetailedInspection of the Front Windshields for Group 2 (Depending on the PN of theWindshields)To accomplish this Service Bulletin it is necessary to use the expendable parts listed in:Ref. AMM Task 56-11-11-400-001Referenced parts for task set A320-A-56-XX-1022-04000-93BA-A DetailedInspection of the Front Windshields for Group 3 (Depending on the PN of theWindshields)To accomplish this Service Bulletin it is necessary to use the expendable parts listed in:Ref. AMM Task 56-11-11-400-001
E. LIST OF EXISTING PARTSNo parts
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3. ACCOMPLISHMENT INSTRUCTIONSTask set A320-A-56-XX-1022-01000-93BA-A (A320-A-56-XX-1022-01ZZZ-93BZ-A)Inspection of the PN of the Front Windshields Installed on the Aircraft
WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONSINCLUDED IN THE REFERENCED PROCEDURES.
CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICALWIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLYSERVICEABLE). WHEN YOU DO A MAINTENANCE WORK, REPAIRS ORMODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS ANDTHE 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 ANDDAMAGE TO THE ELECTRICAL WIRING INSTALLATION.IF THERE IS CONTAMINATION, REFER TO Ref. ESPM 20-55-00.
NOTE: The accomplishment instructions of this Service Bulletin include procedures given inother documents or in other sections of the Service Bulletin. When the words “refer to”are used and the operator has a procedure accepted by the local authority he belongs to,the accepted alternative procedure can be used. When the words “in accordance with”are used then the given procedure must be followed.
NOTE: The access and close-up instructions, not comprising return to service tests, in thisService Bulletin do not constitute or affect the technical intent of the Service Bulletin.Operators can therefore, as deemed necessary, omit or add access and/or close-up stepsto add flexibility to their maintenance operations as long as the technical intent of theService Bulletin is met within the set parameters.
NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Referto paragraph 1.J., References, for the definition of acronyms.
NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory byan Airworthiness Directive (AD). The paragraphs 3.C. and 3.E. in these accomplishmentinstructions are Required for Compliance (RC) and must be done to comply with the AD.To allow more flexibility, the rule "refer to" and "in accordance with" will apply to theseparagraphs 3.C. and 3.E. Other paragraphs are recommended and may be deviated from,done as part of other actions or done with accepted methods different from those givenin the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can beput back into a serviceable condition.
NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance necessaryto ensure the continued airworthiness of the aircraft.For any deviations to the instructions, including Required for Compliance paragraphcontained herein, contact AIRBUS for further instructions and approval.
NOTE: The purpose of flowcharts is to supplement the information given in the Procedure andCompliance paragraphs and not to serve as the primary source for tasks or compliancetimes given in this Service Bulletin.
A. TASK SET ASSOCIATED INFORMATIONTask Manpower
TOTAL MAN-HOURS 0.20 hELAPSED TIME (HOURS) 0.15 h
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B. PREPARATION(1) Task A320-A-56-XX-1022-01001-540A-A (A320-A-56-XX-1022-01ZZZ-540Z-A)
Job Set-upJob Set-Up Information
Manpower/Resources/Skills
Man-hours 0.05 hMinimum Number of person 1Elapsed Time 0.05 h
Procedure(a) Standard Practices given in this procedure:
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.(b) Inspect the PN of the LH side front windshield on the aircraft in accordance with
PLANNING INFORMATION paragraph 1.E.(2):Refer to Ref. Fig. Inspection of the PN of the LH side Front Windshield on theAircraft and Ref. Fig. Flow Chart
NOTE: This Service Bulletin considers the possibility of a configuration with PNsfrom different Groups on the LH and RH sides of the same aircraft.
A318/A319/A320/A321SERVICE BULLETIN
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NOTE: A review of aircraft delivery and/or maintenance records is acceptableto make the determination of the part installed, provided those recordscan be relied upon for that purpose and the PN and SN of the part canbe positively identified from that review.
NOTE: The paper ID plate bonded on the internal side of the windshield mustbe used. If the paper ID plate is not available, the metallic ID plate onthe connector must be used.
1 If the PN of the LH side front windshield is STA320-1-7-1:a Do the inspection of the LH side front windshield for Group 1 in
accordance with Ref. Task set A320-A-56-XX-1022-02ZZZ-93BZ-A.2 If the PN of the LH side front windshield is STA320-1-8-2:
a Do a check of the sensor fault history from the date on which thewindshield has been first installed on the aircraft:
NOTE: To ease the review of sensor fault history and records, do acheck if no ECAM warning amber "ANTI ICE L(R) WINDSHIELD(ATA 30-42)". If this ECAM warning is not found in the aircraftmaintenance records, you can consider no sensor faultoccurred.
<1> If fault message "561000 L WINDSHIELD SENSOR" has beenrecorded or if unknown maintenance history:<a> Do the inspection of the LH side front windshield for Group
2, refer to Ref. Task set A320-A-56-XX-1022-03ZZZ-93BZ-A at the compliance time defined in accordance withPLANNING INFORMATION paragraph 1.E.(2).
<2> If fault message "561000 L WINDSHIELD SENSOR" has not beenrecorded:<a> Do a check of the age of the windshield to know if it is
more or less than 4 years or 10000 FC or 15000 FH sincefirst installation on an aircraft.
NOTE: Regarding the definition of windshield ageutilization:- For original windshield installed since the
aircraft delivery: take into account the ageof 4 years from aircraft delivery date
- For windshield installed after the aircraftdelivery (installed in-service as a newspare): take into account the age of 4 yearsfrom windshield first installation date on anyaircraft (current and previous aircraft).
<b> Do the inspection of the LH side front windshield for Group2, refer to Ref. Task set A320-A-56-XX-1022-03ZZZ-93BZ-A at the compliance time defined in accordance withPLANNING INFORMATION paragraph 1.E.(2).
3 If the PN of the LH side front windshield is STA320-1-3-1 or STA320-1-4-1 orSTA320-1-5-1 or STA320-1-6-1:a Do the inspection of the LH side front windshield for Group 3 in
accordance with Ref. Task set A320-A-56-XX-1022-04ZZZ-93BZ-A.
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4 If the PN of the LH side front windshield is different than STA320-1-3-1 orSTA320-1-4-1 or STA320-1-5-1 or STA320-1-6-1 or STA320-1-7-1 or STA320-1-8-2:a No further action is necessary with this Service Bulletin.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024F2-A-004-01 SHEET 1/1REV 00 Jan 28/21 A320-56-1022Inspection of the PN of the LH side
Front Windshield on the Aircraft Page 57
CONF ALL
A BVIEW LOOKING FWD VIEW LOOKING FWD
A
B
NOTE:01 USE THE PAPER ID PLATE TO IDENTIFY THE PN OF THE FRONT WINDSHIELD, 3DG1,
ON THE AIRCRAFT, LH SIDE
02
01
02 FIRST CHECK PAPER ID PLATE (AS SHOWN ON VIEW A). IF NOT FOUND CHECK THE CONNECTORON ALL 4 SIDES FOR THE IDENTIFICATION OF THE FRONT WINDSHIELD ON THE AIRCRAFT, LH SIDE
ICN-A320-A-56XX1022-A-FAPE3-024F2-A-004-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024EF-A-006-01 SHEET 1/1REV 00 Jan 28/21 A320-56-1022Flow Chart
Page 58
CONF ALL
DO THE OPERATIONAL TEST
NO
INSTALLED?PN STA320-1-8-2
IS
YES
01
DO THE INSPECTION OF THELH SIDE FRONT WINDSHIELD
FOR GROUP 1
01
LH SIDE FRONT WINDSHIELDON THE AIRCRAFT
INSTALLED?PN STA320-1-7-1
IS
IS PNSTA320-1-3-1 OR STA320-1-4-1
OR STA320-1-5-1 OR STA320-1-6-1INSTALLED?
YES
YES
01
DO THE INSPECTION OF THELH SIDE FRONT WINDSHIELD
FOR GROUP 3
NO FURTHER ACTION WITHTHIS SERVICE BULLETIN
NO
INSPECT THE PN OF THE
NO
HAS FAULTMESSAGE "561000 L
WINDSHIELD SENSOR"BEEN RECORDED?
> 4 YEARSOR > 10000 FCOR > 15000 FHSINCE FIRST
INSTALLATION ONAN AIRCRAFT?
WINDSHIELD AGE:IS THE
YES
01 02
FRONT WINDSHIELD FOR GROUP 2DO THE INSPECTION OF THE LH SIDE
01
IS FIRST INSTALLED ON THE AIRCRAFTFROM THE DATE ON WHICH THE WINDSHIELDDO A CHECK OF THE SENSOR FAULT HISTORY
NOYES
NO
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCETIMES GIVEN IN THIS SERVICE BULLETIN
01
IF A FAULT MESSAGE IS RECORDED OR IF THE MAINTENANCE HISTORY IS UNKNOWN, DO THE INSPECTION02
NOTE:IN ACCORDANCE WITH PLANNING INFORMATION PARAGRAPH 1.E.(2)
ICN-A320-A-56XX1022-A-FAPE3-024EF-A-006-01
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(2) Task A320-A-56-XX-1022-02001-900A-A (A320-A-56-XX-1022-02ZZZ-900Z-A)Inspect the PN of the RH side Front Windshield on the AircraftJob Set-Up Information
Working Area
Impacted Zone Access / Work Location212
Manpower/Resources/Skills
Man-hours 0.05 hMinimum Number of person 1Elapsed Time 0.05 hSkills Airframe
Procedure(a) Standard Practices given in this procedure:
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.(b) Inspect the PN of the RH side front windshield on the aircraft in accordance with
PLANNING INFORMATION paragraph 1.E.(2):Refer to Ref. Fig. Inspection of the PN of the RH side Front Windshield on theAircraft and Ref. Fig. Flow Chart
NOTE: This Service Bulletin considers the possibility of a configuration with PNsfrom different Groups on the LH and RH sides of the same aircraft.
NOTE: A review of aircraft delivery and/or maintenance records is acceptableto make the determination of the part installed, provided those recordscan be relied upon for that purpose and the PN and SN of the part canbe positively identified from that review.
NOTE: The paper ID plate bonded on the internal side of the windshield mustbe used. If the paper ID plate is not available, the metallic ID plate onthe connector must be used.
1 If the PN of the RH side front windshield is STA320-2-7-1:a Do the inspection of the RH side front windshield for Group 1 in
accordance with Ref. Task set A320-A-56-XX-1022-02ZZZ-93BZ-A.2 If the PN of the RH side front windshield is STA320-2-8-2:
a Do a check of the sensor fault history from the date on which thewindshield has been first installed on the aircraft:
NOTE: To ease the review of sensor fault history and records, do acheck if no ECAM warning amber "ANTI ICE L(R) WINDSHIELD(ATA 30-42)". If this ECAM warning is not found in the aircraftmaintenance records, you can consider no sensor faultoccurred.
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<1> If fault message "561000 R WINDSHIELD SENSOR" has beenrecorded or if unknown maintenance history:<a> Do the inspection of the RH side front windshield for
Group 2, refer to Ref. Task set A320-A-56-XX-1022-03ZZZ-93BZ-A at the compliance time defined in accordance withPLANNING INFORMATION paragraph 1.E.(2).
<2> If fault message "561000 R WINDSHIELD SENSOR" has not beenrecorded:<a> Do a check of the age of the windshield to know if it is
more or less than 4 years or 10000 FC or 15000 FH sincefirst installation on an aircraft.
NOTE: Regarding the definition of windshield ageutilization:- For original windshield installed since the
aircraft delivery: take into account the ageof 4 years from aircraft delivery date
- For windshield installed after the aircraftdelivery (installed in-service as a newspare): take into account the age of 4 yearsfrom windshield first installation date on anyaircraft (current and previous aircraft).
<b> Do the inspection of the RH side front windshield forGroup 2, refer to Ref. Task set A320-A-56-XX-1022-03ZZZ-93BZ-A at the compliance time defined in accordance withPLANNING INFORMATION paragraph 1.E.(2).
3 If the PN of the RH side front windshield is STA320-2-3-1 or STA320-2-4-1 orSTA320-2-5-1 or STA320-2-6-1:a Do the inspection of the RH side front windshield for Group 3 in
accordance with Ref. Task set A320-A-56-XX-1022-04ZZZ-93BZ-A.4 If the PN of the RH side front windshield is different than STA320-2-3-1 or
STA320-2-4-1 or STA320-2-5-1 or STA320-2-6-1 or STA320-2-7-1 or STA320-2-8-2:a No further action is necessary with this Service Bulletin.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024F4-A-004-01 SHEET 1/1REV 00 Jan 28/21 A320-56-1022Inspection of the PN of the RH side
Front Windshield on the Aircraft Page 61
CONF ALL
A
B
AVIEW LOOKING FWD
BVIEW LOOKING FWDNOTE:
01 USE THE PAPER ID PLATE TO IDENTIFY THE PN OF THE FRONT WINDSHIELD, 3DG2,ON THE AIRCRAFT, RH SIDE
02 FIRST CHECK PAPER ID PLATE (AS SHOWN ON VIEW A). IF NOT FOUND CHECK THE CONNECTORON ALL 4 SIDES FOR THE IDENTIFICATION OF THE FRONT WINDSHIELD ON THE AIRCRAFT, RH SIDE
02
01
ICN-A320-A-56XX1022-A-FAPE3-024F4-A-004-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024EP-A-006-01 SHEET 1/1REV 00 Jan 28/21 A320-56-1022Flow Chart
Page 62
CONF ALL
NO
YES
01
DO THE INSPECTION OF THERH SIDE FRONT WINDSHIELD
FOR GROUP 1
YES
YES
NO FURTHER ACTION WITHTHIS SERVICE BULLETIN
NONO
YES
01 02
FRONT WINDSHIELD FOR GROUP 2DO THE INSPECTION OF THE RH SIDE
01
IS FIRST INSTALLED ON THE AIRCRAFTFROM THE DATE ON WHICH THE WINDSHIELDDO A CHECK OF THE SENSOR FAULT HISTORY
NOYES
NO
01
RH SIDE FRONT WINDSHIELDON THE AIRCRAFT
INSPECT THE PN OF THE
INSTALLED?PN STA320-2-7-1
IS
INSTALLED?PN STA320-2-8-2
IS
01
DO THE INSPECTION OF THERH SIDE FRONT WINDSHIELD
FOR GROUP 3
IS PNSTA320-2-3-1 OR STA320-2-4-1
OR STA320-2-5-1 OR STA320-2-6-1INSTALLED?
HAS FAULTMESSAGE "561000 R
WINDSHIELD SENSOR"BEEN RECORDED?
> 4 YEARSOR > 10000 FCOR > 15000 FHSINCE FIRST
INSTALLATION ONAN AIRCRAFT?
WINDSHIELD AGE:IS THE
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCETIMES GIVEN IN THIS SERVICE BULLETIN
01
IF A FAULT MESSAGE IS RECORDED OR IF THE MAINTENANCE HISTORY IS UNKNOWN, DO THE INSPECTION02
NOTE:IN ACCORDANCE WITH PLANNING INFORMATION PARAGRAPH 1.E.(2)
ICN-A320-A-56XX1022-A-FAPE3-024EP-A-006-01
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D. PREPARATION FOR TESTNone
E. TESTNone
F. CLOSE-UP(1) Task A320-A-56-XX-1022-01001-740A-A (A320-A-56-XX-1022-01ZZZ-740Z-A)
Close-upJob Set-Up Information
Manpower/Resources/Skills
Man-hours 0.05 hMinimum Number of person 1Elapsed Time 0.05 h
Procedure
NOTE: If you intend to accomplish an associated Inspection Task during the samelayover period, the subsequent Close-up procedure is not necessary.
(a) Make sure that the work areas are clean and clear of tools and other items ofequipment.
(b) Put the aircraft back to its initial configuration.G. ADMINISTRATIVE
ProcedureConfirm in the applicable aircraft records that you have completed all the work definedin this Service Bulletin task set as required.
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Task set A320-A-56-XX-1022-02000-93BA-A (A320-A-56-XX-1022-02ZZZ-93BZ-A)Detailed Inspection of the Front Windshields for Group 1 (Depending on the PN of theWindshields)
WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONSINCLUDED IN THE REFERENCED PROCEDURES.
WARNING: BEFORE YOU START WORK, YOU MUST PUT ON A SAFETY HARNESS ANDATTACH IT TO THE ACCESS PLATFORM. WITHOUT A SAFETY HARNESS, YOUCAN FALL. THIS CAN KILL YOU OR CAUSE YOU INJURY.
WARNING: BEFORE YOU DO THIS TASK:- MAKE SURE THAT THE AREA BELOW THE WORK AREA IS CLEAR OF
PERSONS- PUT PROTECTION ON THE PARTS BELOW THE WORK AREA IF
APPLICABLE.IF OBJECTS FALL ACCIDENTALLY, THEY CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO THE AIRCRAFT.
CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICALWIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLYSERVICEABLE). WHEN YOU DO A MAINTENANCE WORK, REPAIRS ORMODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS ANDTHE 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 ANDDAMAGE TO THE ELECTRICAL WIRING INSTALLATION.IF THERE IS CONTAMINATION, REFER TO Ref. ESPM 20-55-00.
NOTE: The accomplishment instructions of this Service Bulletin include procedures given inother documents or in other sections of the Service Bulletin. When the words “refer to”are used and the operator has a procedure accepted by the local authority he belongs to,the accepted alternative procedure can be used. When the words “in accordance with”are used then the given procedure must be followed.
NOTE: The access and close-up instructions, not comprising return to service tests, in thisService Bulletin do not constitute or affect the technical intent of the Service Bulletin.Operators can therefore, as deemed necessary, omit or add access and/or close-up stepsto add flexibility to their maintenance operations as long as the technical intent of theService Bulletin is met within the set parameters.
NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Referto paragraph 1.J., References, for the definition of acronyms.
NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory byan Airworthiness Directive (AD). The paragraphs 3.C. and 3.E. in these accomplishmentinstructions are Required for Compliance (RC) and must be done to comply with the AD.To allow more flexibility, the rule "refer to" and "in accordance with" will apply to theseparagraphs 3.C. and 3.E. Other paragraphs are recommended and may be deviated from,done as part of other actions or done with accepted methods different from those givenin the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can beput back into a serviceable condition.
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NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance necessaryto ensure the continued airworthiness of the aircraft.For any deviations to the instructions, including Required for Compliance paragraphcontained herein, contact AIRBUS for further instructions and approval.
NOTE: The purpose of flowcharts is to supplement the information given in the Procedure andCompliance paragraphs and not to serve as the primary source for tasks or compliancetimes given in this Service Bulletin.
A. TASK SET ASSOCIATED INFORMATIONTask Manpower
TOTAL MAN-HOURS 2.80 hELAPSED TIME (HOURS) 1.35 hAdditional man-hours related to Vendor SB; refer to:SAINT-GOBAIN (F0360) VSB STA320-56-001
B. PREPARATION(1) Task A320-A-56-XX-1022-08001-540A-A (A320-A-56-XX-1022-08ZZZ-540Z-A)
Job Set-upJob Set-Up Information
Manpower/Resources/Skills
Man-hours 0.10 hMinimum Number of person 1Elapsed Time 0.10 h
NOTE: For the basic Aircraft configuration, refer to AMM Chapter “Introduction -Aircraft status for maintenance" in Manual Front Matter section.
(a) Make sure that the aircraft is electrically grounded, refer to Ref. AMM Task 12-34-24-869-002.
(b) Do the job set-up procedure as specified in the removal of the sidewall panels,refer to Ref. AMM Task 25-13-41-000-002.
NOTE: This procedure is necessary for the removal of the lining Panel 211MW.
(c) Do the job set-up procedure as specified in the removal of the windshields (FIN3DG1 and FIN 3DG2), refer to Ref. AMM Task 56-11-11-000-001.
NOTE: This procedure is necessary for the removal of the lining Panel 211LW.
(2) Task A320-A-56-XX-1022-09001-540A-A (A320-A-56-XX-1022-09ZZZ-540Z-A)Remove for Access the Lining Panels from the Aircraft
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Job Set-Up InformationWorking Area
Impacted Zone Access / Work Location210
Manpower/Resources/Skills
Man-hours 0.10 hMinimum Number of person 1Elapsed Time 0.10 hSkills Airframe
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-20-00, Page Block 001Task 56-11-11-000-001
SRM 51-42-00
Procedure(a) Standard Practices given in this procedure:
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 Remove and install fasteners in accordance with Ref. SRM 51-42-00.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.(b) Remove the lining Panel 211LW for access, refer to Ref. Fig. Removal of the
Lining Panels for Access.1 Release the stud assemblies, item (6), refer to Ref. Fig. Removal of the
Lining Panels for Access, sheet 01:
4 LOCKNUT Item (7) Retain
4 STUD ASSEMBLIES Item (6) Retain2 Loosen the fastener, item (5), refer to Ref. Fig. Removal of the Lining Panels
for Access, sheet 01 and sheet 02, view B.3 Remove the lining Panel 211LW, refer to Ref. Fig. Removal of the Lining
Panels for Access, sheet 01:
FIN 211LW1 LINING PANEL Item (4) Retain
NOTE: The lining Panel 211LW, item (4), prevents damage to the sensors.
(c) Remove the lining Panel 211MW for access, refer to Ref. Fig. Removal of theLining Panels for Access.1 Remove, refer to Ref. AMM Task 56-11-11-000-001 and Ref. Fig. Removal of
the Lining Panels for Access, sheet 01 and sheet 02, view C:
2 SCREW Item (2) Retain
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1 WASHER Item (3) Retain2 Remove the lining Panel 211MW, refer to Ref. AMM Task 56-11-11-000-001
and Ref. Fig. Removal of the Lining Panels for Access, sheet 01 and sheet02, view C:
FIN 211MW1 VERTICAL LINING PANEL Item (1) Retain
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024EZ-A-001-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Removal of the Lining Panels for Access
Page 68
CONF ALL
(4)211LW
(7)
(6)
(7)
(7)
(7) A
B
A
C
ICN-A320-A-56XX1022-A-FAPE3-024EZ-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024F0-A-002-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Removal of the Lining Panels for Access
Page 69
CONF ALL
(5)
(1)211MW
C
B
(2)
(2)
(3)
ICN-A320-A-56XX1022-A-FAPE3-024F0-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 70
C. PROCEDURE(1) Task A320-A-56-XX-1022-09001-311A-A (A320-A-56-XX-1022-09ZZZ-311Z-A)
Do the Inspection of the LH side Front WindshieldJob Set-Up Information
Working Area
Impacted Zone Access / Work Location211
Manpower/Resources/Skills
Man-hours 1.10 hMinimum Number of person 2Elapsed Time 0.55 hSkills Airframe
Material necessary to do the job
Aircraft standard toolsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
NOTE: This procedure is to be done only if the LH side front windshield installed onaircraft is in Group 1, refer to Ref. Task set A320-A-56-XX-1022-01ZZZ-93BZ-A.
(a) Standard Practices given in this procedure:1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the protection of the connectors, contacts and terminals, refer to Ref.
ESPM 20-54-50.(b) Do the inspection of the LH side front windshield for Group 1, refer to Ref.
Fig. Flow Chart at the compliance time defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2):1 Do a detailed visual inspection of the LH side front windshield from outside
to detect delamination or bubbles, refer to Ref. Fig. Criteria of Delaminationand Bubbles, LH side:
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a If delamination and/or bubbles are visible at inboard edge, topinboard edge corner and lower inboard edge corner:<1> Record the findings in the inspection report sheet, refer to Ref.
Task A320-A-56-XX-1022-07ZZZ-90AZ-A.<2> Fly under MMEL before next flight:
- Deactivate the windshield de-icing, refer to Ref. AMM Task56-10-00-040-001, and then fly under Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03BOrDo step (d) before next flight.
b If delamination and/or bubbles are visible at upper, outboard andlower edges, do a check for the width of the delamination and/orbubbles from the weather seal around the front windshield:<1> If delamination and/or bubbles are above the criteria defined in
Ref. Fig. Criteria of Delamination and Bubbles, LH side:<a> Record the findings in the inspection report sheet, refer to
Ref. Task A320-A-56-XX-1022-07ZZZ-90AZ-A.<b> Fly under MMEL before next flight:
- Deactivate the windshield de-icing, refer to Ref.AMM Task 56-10-00-040-001, and then fly under Ref.MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03BOrDo step (d) before next flight.
<2> If delamination and/or bubbles are not above the criteriadefined in Ref. Fig. Criteria of Delamination and Bubbles, LHside:<a> Record the findings in the inspection report sheet, refer to
Ref. Task A320-A-56-XX-1022-07ZZZ-90AZ-A.<b> Do step (b)2.
c If delamination and/or bubbles are not visible:<1> Record the nil finding in the inspection report sheet, refer to Ref.
Task A320-A-56-XX-1022-07ZZZ-90AZ-A.<2> Do step (b)2.
2 Do the operational test of the windshield anti-icing and defogging, refer toRef. AMM Task 30-42-00-710-001:a If fault found, use dedicated TSM.
3 Record the test result on the Inspection Report sheet in accordance withRef. Task A320-A-56-XX-1022-07ZZZ-90AZ-A.
WARNING: MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THEWEATHER RADAR ARE OPENED, SAFETIED AND TAGGED.
4 Open, safety/lock and tag this (these) circuit breaker(s):
NOTE: For the circuit breaker location, refer to Ref. AMM 24-50-00.
NOTE: For the circuit breaker safety practices, refer to Ref. AMM Task 20-16-00-912-001.
5 Disconnect the windshield connector from the aircraft wiring, refer to Ref.Fig. Disconnection/Connection of the Front Windshield Connector from theAircraft Wiring, LH side.
6 Open the connector in accordance with Ref. SAINT-GOBAIN (F0360) VSBSTA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-11ZZZ-311Z-A.
7 Do the detailed visual inspection of the connector in accordance with Ref.SAINT-GOBAIN (F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-11ZZZ-311Z-A:a If the connector cannot be opened for inspection:
<1> Close the connector in accordance with Ref. SAINT-GOBAIN(F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-11ZZZ-311Z-A.
<2> Connect the windshield connector to the aircraft wiring.<3> Fly under MMEL before next flight:
- Deactivate the windshield de-icing, refer to Ref. AMM Task56-10-00-040-001, and then fly under Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03BOrDo step (d) before next flight.
b If the connector can be opened for inspection:<1> Do a check for water ingress or corrosion in the windshield
connector:
NOTE: Refer to Ref. NTM 51-90-00 for using the recommendedendoscope or similar visual inspection aids.
<a> If water ingress or corrosion is found in the windshieldconnector:
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[1] Close the connector in accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001 and refer toRef. Task A320-A-56-XX-1022-11ZZZ-311Z-A.
[2] Connect the windshield connector to the aircraftwiring.
[3] Fly under MMEL before next flight:- Deactivate the windshield de-icing, refer to
Ref. AMM Task 56-10-00-040-001, and then flyunder Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03BOrDo step (d) before next flight.
<b> If water ingress or corrosion is not found in the windshieldconnector:[1] Do step (b)8.
8 Close the connector in accordance with Ref. SAINT-GOBAIN (F0360) VSBSTA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-11ZZZ-311Z-A.
9 Connect the windshield connector to the aircraft wiring, refer to Ref. Fig.Disconnection/Connection of the Front Windshield Connector from theAircraft Wiring, LH side.
10 Do the operational test of the windshield anti-icing and defogging, refer toRef. AMM Task 30-42-00-710-001:a If fault found, use dedicated TSM.
WARNING: MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THEWEATHER RADAR ARE OPENED, SAFETIED AND TAGGED.
11 Open, safety/lock and tag this (these) circuit breaker(s):
NOTE: For the circuit breaker location, refer to Ref. AMM 24-50-00.
NOTE: For the circuit breaker safety practices, refer to Ref. AMM Task 20-16-00-912-001.
12 Disconnect the windshield connector from the aircraft wiring, refer to Ref.Fig. Disconnection/Connection of the Front Windshield Connector from theAircraft Wiring, LH side.
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13 Do the dielectric test and then the insulation test, refer to Ref. AppendixELECTRICAL TESTS RESULT CHART:a Remove a part of the weather seal over the metallic Z bar in
accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001 andrefer to Ref. Task A320-A-56-XX-1022-04ZZZ-900Z-A.
WARNING: THE GSE TOOL 98D56003001000 USES HIGH VOLTAGEDURING THE TEST. BEFORE YOU START THE TEST, MAKESURE THAT ALL SAFETY PRECAUTIONS GIVEN IN THETOOL USER GUIDE ARE FOLLOWED. THE ELECTRICALPOWER IS SUFFICIENTLY STRONG TO CAUSE AN INJURYOR KILL YOU.
b Do the dielectric test (1500VAC during 1 minute) and insulation test(500VDC during 1 minute), use tool:
1 WINDSHIELDINSPECTION
98D56003001000
NOTE: You must obey the instruction given in the GSE tool userguide.
c Record the values in the Inspection Report sheet in accordancewith Ref. Task A320-A-56-XX-1022-07ZZZ-90AZ-A and refer to Ref.Appendix ELECTRICAL TESTS RESULT CHART.
d Connect the windshield connector to the aircraft wiring.e Examine the color classification of the results of the dielectric and
insulation tests, refer to Ref. Appendix ELECTRICAL TESTS RESULTCHART:<1> If the electrical tests result is in red area:
<a> Do step (c) or (d) before next flight.<2> If the electrical tests result is in green or amber area:
<a> Do step (d) or do the steps that follow:[1] Do the operational test of the windshield anti-icing
and defogging, refer to Ref. AMM Task 30-42-00-710-001:[a] If fault found, use dedicated TSM.
[2] Repair the weather seal in accordance with Ref.SAINT-GOBAIN (F0360) VSB STA320-56-001 andrefer to Ref. Task A320-A-56-XX-1022-02ZZZ-690Z-A.
[3] Send the result to AIRBUS in accordance with Ref.Task A320-A-56-XX-1022-07ZZZ-90AZ-A.
[4] Do again the inspection of the LH side frontwindshield for Group 1 at the compliance timedefined in accordance with PLANNING INFORMATIONparagraph 1.E.(2), refer to Ref. Task A320-A-56-XX-1022-09ZZZ-311Z-A.
(c) Do the operational test of the windshield anti-icing and defogging, refer to Ref.AMM Task 30-42-00-710-001 and Ref. Fig. Flow Chart at the compliance timedefined in accordance with PLANNING INFORMATION paragraph 1.E.(2).
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1 If fault found, use dedicated TSM.2 Repair the weather seal in accordance with Ref. SAINT-GOBAIN (F0360) VSB
STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-02ZZZ-690Z-A.3 Fly under MMEL:
- Deactivate the windshield de-icing, refer to Ref. AMM Task 56-10-00-040-001, and then fly under Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03B.
(d) Replace the damaged windshield with a spare windshield, refer to Ref. Fig.Flow Chart at the compliance time defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2):1 If this Service Bulletin is not applicable for the PN of the spare windshield:
a Replace the damaged windshield with a spare windshield inaccordance with Ref. Task set A320-A-56-XX-1022-01ZZZ-93CZ-A.
b Send the windshield inspection report to AIRBUS (Monitored retrofit)in accordance with Ref. Task A320-A-56-XX-1022-07ZZZ-90AZ-A.
c No further action is necessary with this Service Bulletin.2 If this Service Bulletin is applicable for the PN of the spare windshield:
a Do a check if the spare windshield was installed before on a differentaircraft:<1> If the spare windshield was not installed before on a different
aircraft:<a> Replace the damaged windshield with a spare windshield
in accordance with Ref. Task set A320-A-56-XX-1022-01ZZZ-93CZ-A and refer to Ref. Fig. Flow Chart.
<b> Send the windshield inspection report to AIRBUS(Monitored retrofit) in accordance with Ref. Task A320-A-56-XX-1022-07ZZZ-90AZ-A.
<c> Do again the inspection of the LH side front windshield:[1] If the spare windshield PN is in Group 1:
[a] Do again the inspection of the LH side frontwindshield for Group 1 at the compliancetime defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-09ZZZ-311Z-A.
[2] If the spare windshield PN is in Group 2:[a] Do again the inspection of the LH side front
windshield for Group 2 at the compliancetime defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-13ZZZ-311Z-A.
[3] If the spare windshield PN is in Group 3:[a] Do again the inspection of the LH side front
windshield for Group 3 at the compliancetime defined in accordance with PLANNING
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INFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-17ZZZ-311Z-A.
<2> If the spare windshield was installed before on a differentaircraft:<a> Do the shop inspection of the spare windshield in
accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-12ZZZ-311Z-A:[1] If there is finding during the shop inspection:
[a] Select another spare windshield and do step(d) again.
[2] If there is no finding during the shop inspection:[a] Replace the damaged windshield with a spare
windshield in accordance with Ref. Task setA320-A-56-XX-1022-01ZZZ-93CZ-A and refer toRef. Fig. Flow Chart.
[b] Send the windshield inspection report toAIRBUS (Monitored retrofit) in accordance withRef. Task A320-A-56-XX-1022-07ZZZ-90AZ-A.
[c] Do again the inspection of the LH side frontwindshield:- If the spare windshield PN is in Group 1:
- Do again the inspection of the LHside front windshield for Group 1at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),refer to Ref. Task A320-A-56-XX-1022-09ZZZ-311Z-A.
- If the spare windshield PN is in Group 2:- Do again the inspection of the LH
side front windshield for Group 2at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),refer to Ref. Task A320-A-56-XX-1022-13ZZZ-311Z-A.
- If the spare windshield PN is in Group 3:- Do again the inspection of the LH
side front windshield for Group 3at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),refer to Ref. Task A320-A-56-XX-1022-17ZZZ-311Z-A.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024M3-A-008-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Flow Chart
Page 77
CONF ALL
01NOTE:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE ANDCOMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCETIMES GIVEN IN THIS SERVICE BULLETIN
IN ACCORDANCE WITH PLANNING INFORMATION PARAGRAPH 1.E.(2)
A
DO A DETAILED VISUAL INSPECTION OF THELH SIDE FRONT WINDSHIELD FROM OUTSIDETO DETECT DELAMINATION AND/OR BUBBLES
01
01
FRONT WINDSHIELD FOR GROUP 1DO THE INSPECTION OF THE LH SIDE
IN ACCORDANCE WITH VSBDO THE DETAILED VISUAL INSPECTION OF THE CONNECTOR
CANCONNECTOR BE
OPENED FORINSPECTION?
YES
NO
IS WATER INGRESSOR CORROSION FOUND
IN THE WINDSHIELDCONNECTOR?
OR
A
B NO
NO
FLY AT FL230 MAXUNDER MMEL 30-42-03B
01
DE-ICING AND FLY UNDERMMEL 30-42-03A
01
DEACTIVATE THE WINDSHIELD
YES
C
01
IN THE INSPECTION REPORT SHEETINSULATION TEST AND RECORD THE VALUES
DO THE DIELECTRIC TEST AND THEN THE
ICN-A320-A-56XX1022-A-FAPE3-024M3-A-008-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024PQ-A-006-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Flow Chart
Page 78
CONF ALL
01NOTE:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE ANDCOMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCETIMES GIVEN IN THIS SERVICE BULLETIN
IN ACCORDANCE WITH PLANNING INFORMATION PARAGRAPH 1.E.(2)
A
OR
FLY AT FL230 MAXUNDER MMEL 30-42-03B
01
REPAIR THE WEATHER SEALIN ACCORDANCE WITH VSB
01
DE-ICING AND FLY UNDERMMEL 30-42-03A
01
DEACTIVATE THE WINDSHIELD
ARE THEDIELECTRIC AND INSULATION
VALUES RECORDED INTHE GREEN OR AMBER
AREA?NO
YESOR
ISTHIS SERVICE BULLETIN
APPLICABLE FOR THE PN OFTHE SPARE WINDSHIELD?
01
REPORT TO AIRBUS (MONITORED RETROFIT)SEND THE WINDSHIELD INSPECTION
NO FURTHER ACTION WITHTHIS SERVICE BULLETIN
SHOPINSPECTION?
FINDING DURINGIS THERE ANY
YES
OF THE SPARE WINDSHIELDDO THE SHOP INSPECTION
IN ACCORDANCE WITH VSB
01
NO
INSTALLED BEFORE ON ADIFFERENT AIRCRAFT?
SPARE WINDSHIELDWAS THE
YES
YES
REPORT TO AIRBUS (MONITORED RETROFIT) 01SEND THE WINDSHIELD INSPECTION
DO THE INSPECTION AGAINAT THE COMPLIANCE TIME DEFINED 01
NO
DO A CHECK OF THE PN OF A SPARE WINDSHIELDBEFORE THE REPLACEMENT OF THE
01DAMAGED WINDSHIELD
01
WINDSHIELD WITH THE REPLACE THE DAMAGED
SPARE WINDSHIELD
01
WINDSHIELD WITH THE REPLACE THE DAMAGED
SPARE WINDSHIELD
A
B
AC
OR
NO
B
01
WITH VSBREPAIR THE WEATHER SEAL IN ACCORDANCE
DO THE INSPECTIONS AGAINAT THE COMPLIANCE TIME DEFINED 01
ICN-A320-A-56XX1022-A-FAPE3-024PQ-A-006-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024FD-A-006-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Criteria of Delamination and Bubbles, LH side
Page 79
CONF ALL
FR1
FR12
Z210
AREA WHERE THE DELAMINATION AND BUBBLES ARE PERMITTED01
NOTE:
INSPECTION AREA
AREA WHERE THE DELAMINATION AND BUBBLES ARE NOT PERMITTED02
VIEW LOOKING AFT
VIEW LOOKING AFT
20 mm
(0.787 in)
A
A
A
A
AA
01
75 mm
(2.953 in)
60 mm
(2.362 in)
20 mm
(0.787 in)
02
20 mm
(0.787 in)
VIEW LOOKING AFT
A
B
A
3DG1
ICN-A320-A-56XX1022-A-FAPE3-024FD-A-006-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024P5-A-007-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Criteria of Delamination and Bubbles, LH side
Page 80
CONF ALL
A ATYPICAL VIEW
20 mm
(0.787 in)
POSSIBLE LOCATIONS OFDELAMINATION/BUBBLES
WEATHER SEAL
WINDSHIELD
TYPICAL VIEWEXAMPLE OF DELAMINATION
AND BUBBLES FINDINGS
FROM OUTSIDE, USE A RULER TO MEASURE 03THE WIDTH FROM THE WEATHER SEAL EDGE
03
NOTE:
B
ICN-A320-A-56XX1022-A-FAPE3-024P5-A-007-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024T2-A-001-01 SHEET 1/1REV 00 Jan 28/21 A320-56-1022Disconnection/Connection of the Front Windshield
Connector from the Aircraft Wiring, LH side Page 81
CONF ALL
A B
EXAMPLE OF THE WINDSHIELDHARNESS PLUG CONNECTED
TO THE WINDSHIELD CONNECTOR
VIEW LOOKING DOWN
FWD
EXAMPLE OF THE WINDSHIELDHARNESS PLUG DISCONNECTED
FROM THE WINDSHIELD CONNECTOR
VIEW LOOKING DOWN
FWD
A B
ICN-A320-A-56XX1022-A-FAPE3-024T2-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 82
(2) Task A320-A-56-XX-1022-10001-311A-A (A320-A-56-XX-1022-10ZZZ-311Z-A)Do the Inspection of the RH side Front WindshieldJob Set-Up Information
Working Area
Impacted Zone Access / Work Location212
Manpower/Resources/Skills
Man-hours 1.10 hMinimum Number of person 2Elapsed Time 0.55 hSkills Airframe
Material necessary to do the job
Aircraft standard toolsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
NOTE: This procedure is to be done only if the RH side front windshield installed onaircraft is in Group 1, refer to Ref. Task set A320-A-56-XX-1022-01ZZZ-93BZ-A.
(a) Standard Practices given in this procedure:1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the protection of the connectors, contacts and terminals, refer to Ref.
ESPM 20-54-50.(b) Do the inspection of the RH side front windshield for Group 1, refer to Ref.
Fig. Flow Chart at the compliance time defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2):1 Do a detailed visual inspection of the RH side front windshield from outside
to detect delamination or bubbles, refer to Ref. Fig. Criteria of Delaminationand Bubbles, RH side:a If delamination and/or bubbles are visible at inboard edge, top
inboard edge corner and lower inboard edge corner:
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 83
<1> Record the findings in the inspection report sheet, refer to Ref.Task A320-A-56-XX-1022-08ZZZ-90AZ-A.
<2> Fly under MMEL before next flight:- Deactivate the windshield de-icing, refer to Ref. AMM Task
56-10-00-040-001, and then fly under Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03BOrDo step (d) before next flight.
b If delamination and/or bubbles are visible at upper, outboard andlower edges, do a check for the width of the delamination and/orbubbles from the weather seal around the front windshield:<1> If delamination and/or bubbles are above the criteria defined in
Ref. Fig. Criteria of Delamination and Bubbles, RH side:<a> Record the findings in the inspection report sheet, refer to
Ref. Task A320-A-56-XX-1022-08ZZZ-90AZ-A.<b> Fly under MMEL before next flight:
- Deactivate the windshield de-icing, refer to Ref.AMM Task 56-10-00-040-001, and then fly under Ref.MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03BOrDo step (d) before next flight.
<2> If delamination and/or bubbles are not above the criteriadefined in Ref. Fig. Criteria of Delamination and Bubbles, RHside:<a> Record the findings in the inspection report sheet, refer to
Ref. Task A320-A-56-XX-1022-08ZZZ-90AZ-A.<b> Do step (b)2.
c If delamination and/or bubbles are not visible:<1> Record the nil finding in the inspection report sheet, refer to Ref.
Task A320-A-56-XX-1022-08ZZZ-90AZ-A.<2> Do step (b)2.
2 Do the operational test of the windshield anti-icing and defogging, refer toRef. AMM Task 30-42-00-710-001:a If fault found, use dedicated TSM.
3 Record the test result on the Inspection Report sheet in accordance withRef. Task A320-A-56-XX-1022-08ZZZ-90AZ-A.
WARNING: MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THEWEATHER RADAR ARE OPENED, SAFETIED AND TAGGED.
4 Open, safety/lock and tag this (these) circuit breaker(s):
PANEL DESIGNATION FIN LOCATION SEE NOTESLIGHTING/STBY/COMP/LIGHT 1LF
NOTE: For the circuit breaker location, refer to Ref. AMM 24-50-00.
NOTE: For the circuit breaker safety practices, refer to Ref. AMM Task 20-16-00-912-001.
5 Disconnect the windshield connector from the aircraft wiring, refer to Ref.Fig. Disconnection/Connection of the Front Windshield Connector from theAircraft Wiring, RH side.
6 Open the connector in accordance with Ref. SAINT-GOBAIN (F0360) VSBSTA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-11ZZZ-311Z-A.
7 Do the detailed visual inspection of the connector in accordance with Ref.SAINT-GOBAIN (F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-11ZZZ-311Z-A:a If the connector cannot be opened for inspection:
<1> Close the connector in accordance with Ref. SAINT-GOBAIN(F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-11ZZZ-311Z-A.
<2> Connect the windshield connector to the aircraft wiring.<3> Fly under MMEL before next flight:
- Deactivate the windshield de-icing, refer to Ref. AMM Task56-10-00-040-001, and then fly under Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03BOrDo step (d) before next flight.
b If the connector can be opened for inspection:<1> Do a check for water ingress or corrosion in the windshield
connector:
NOTE: Refer to Ref. NTM 51-90-00 for using the recommendedendoscope or similar visual inspection aids.
<a> If water ingress or corrosion is found in the windshieldconnector:[1] Close the connector in accordance with Ref. SAINT-
GOBAIN (F0360) VSB STA320-56-001 and refer toRef. Task A320-A-56-XX-1022-11ZZZ-311Z-A.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 85
[2] Connect the windshield connector to the aircraftwiring.
[3] Fly under MMEL before next flight:- Deactivate the windshield de-icing, refer to
Ref. AMM Task 56-10-00-040-001, and then flyunder Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03BOrDo step (d) before next flight.
<b> If water ingress or corrosion is not found in the windshieldconnector:[1] Do step (b)8.
8 Close the connector in accordance with Ref. SAINT-GOBAIN (F0360) VSBSTA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-11ZZZ-311Z-A.
9 Connect the windshield connector to the aircraft wiring, refer to Ref. Fig.Disconnection/Connection of the Front Windshield Connector from theAircraft Wiring, RH side.
10 Do the operational test of the windshield anti-icing and defogging, refer toRef. AMM Task 30-42-00-710-001:a If fault found, use dedicated TSM.
WARNING: MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THEWEATHER RADAR ARE OPENED, SAFETIED AND TAGGED.
11 Open, safety/lock and tag this (these) circuit breaker(s):
NOTE: For the circuit breaker location, refer to Ref. AMM 24-50-00.
NOTE: For the circuit breaker safety practices, refer to Ref. AMM Task 20-16-00-912-001.
12 Disconnect the windshield connector from the aircraft wiring, refer to Ref.Fig. Disconnection/Connection of the Front Windshield Connector from theAircraft Wiring, RH side.
13 Do the dielectric test and then the insulation test, refer to Ref. AppendixELECTRICAL TESTS RESULT CHART:
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 86
a Remove a part of the weather seal over the metallic Z bar inaccordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001 andrefer to Ref. Task A320-A-56-XX-1022-04ZZZ-900Z-A.
WARNING: THE GSE TOOL 98D56003001000 USES HIGH VOLTAGEDURING THE TEST. BEFORE YOU START THE TEST, MAKESURE THAT ALL SAFETY PRECAUTIONS GIVEN IN THETOOL USER GUIDE ARE FOLLOWED. THE ELECTRICALPOWER IS SUFFICIENTLY STRONG TO CAUSE AN INJURYOR KILL YOU.
b Do the dielectric test (1500VAC during 1 minute) and the insulationtest (500VDC during 1 minute), use tool:
1 WINDSHIELDINSPECTION
98D56003001000
NOTE: You must obey the instruction given in the GSE tool userguide.
c Record the values in the Inspection Report sheet in accordancewith Ref. Task A320-A-56-XX-1022-08ZZZ-90AZ-A and refer to Ref.Appendix ELECTRICAL TESTS RESULT CHART.
d Connect the windshield connector to the aircraft wiring.e Examine the color classification of the results of the dielectric and
insulation tests, refer to Ref. Appendix ELECTRICAL TESTS RESULTCHART:<1> If the electrical tests result is in red area:
<a> Do step (c) or (d) before next flight.<2> If the electrical tests result is in green or amber area:
<a> Do step (d) or do the steps that follow:[1] Do the operational test of the windshield anti-icing
and defogging, refer to Ref. AMM Task 30-42-00-710-001:[a] If fault found, use dedicated TSM.
[2] Repair the weather seal in accordance with Ref.SAINT-GOBAIN (F0360) VSB STA320-56-001 andrefer to Ref. Task A320-A-56-XX-1022-02ZZZ-690Z-A.
[3] Send the result to AIRBUS in accordance with Ref.Task A320-A-56-XX-1022-08ZZZ-90AZ-A.
[4] Do again the inspection of the RH side frontwindshield for Group 1 at the compliance timedefined in accordance with PLANNING INFORMATIONparagraph 1.E.(2), refer to Ref. Task A320-A-56-XX-1022-10ZZZ-311Z-A.
(c) Do the operational test of the windshield anti-icing and defogging, refer to Ref.AMM Task 30-42-00-710-001 and Ref. Fig. Flow Chart at the compliance timedefined in accordance with PLANNING INFORMATION paragraph 1.E.(2).1 If fault found, use dedicated TSM.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 87
2 Repair the weather seal in accordance with Ref. SAINT-GOBAIN (F0360) VSBSTA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-02ZZZ-690Z-A.
3 Fly under MMEL:- Deactivate the windshield de-icing, refer to Ref. AMM Task 56-10-00-
040-001, and then fly under Ref. MMEL 30-42-03AOr- Fly at FL 230 MAX under Ref. MMEL 30-42-03B.
(d) Replace the damaged windshield with a spare windshield, refer to Ref. Fig.Flow Chart at the compliance time defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2):1 If this Service Bulletin is not applicable for the PN of the spare windshield:
a Replace the damaged windshield with a spare windshield inaccordance with Ref. Task set A320-A-56-XX-1022-01ZZZ-93CZ-A.
b Send the windshield inspection report to AIRBUS (Monitored retrofit)in accordance with Ref. Task A320-A-56-XX-1022-08ZZZ-90AZ-A.
c No further action is necessary with this Service Bulletin.2 If this Service Bulletin is applicable for the PN of the spare windshield:
a Do a check if the spare windshield was installed before on a differentaircraft:<1> If the spare windshield was not installed before on a different
aircraft:<a> Replace the damaged windshield with a spare windshield
in accordance with Ref. Task set A320-A-56-XX-1022-01ZZZ-93CZ-A and refer to Ref. Fig. Flow Chart.
<b> Send the windshield inspection report to AIRBUS(Monitored retrofit) in accordance with Ref. Task A320-A-56-XX-1022-08ZZZ-90AZ-A.
<c> Do again the inspection of the RH side front windshield:[1] If the spare windshield PN is in Group 1:
[a] Do again the inspection of the RH side frontwindshield for Group 1 at the compliancetime defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-10ZZZ-311Z-A.
[2] If the spare windshield PN is in Group 2:[a] Do again the inspection of the RH side front
windshield for Group 2 at the compliancetime defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-14ZZZ-311Z-A.
[3] If the spare windshield PN is in Group 3:[a] Do again the inspection of the RH side front
windshield for Group 3 at the compliancetime defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-18ZZZ-311Z-A.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 88
<2> If the spare windshield was installed before on a differentaircraft:<a> Do the shop inspection of the spare windshield in
accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-12ZZZ-311Z-A:[1] If there is finding during the shop inspection:
[a] Select another spare windshield and do step(d) again.
[2] If there is no finding during the shop inspection:[a] Replace the damaged windshield with a spare
windshield in accordance with Ref. Task setA320-A-56-XX-1022-01ZZZ-93CZ-A and refer toRef. Fig. Flow Chart.
[b] Send the windshield inspection report toAIRBUS (Monitored retrofit) in accordance withRef. Task A320-A-56-XX-1022-08ZZZ-90AZ-A.
[c] Do again the inspection of the RH side frontwindshield:- If the spare windshield PN is in Group 1:
- Do again the inspection of the RHside front windshield for Group 1at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),refer to Ref. Task A320-A-56-XX-1022-10ZZZ-311Z-A.
- If the spare windshield PN is in Group 2:- Do again the inspection of the RH
side front windshield for Group 2at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),refer to Ref. Task A320-A-56-XX-1022-14ZZZ-311Z-A.
- If the spare windshield PN is in Group 3:- Do again the inspection of the RH
side front windshield for Group 3at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),refer to Ref. Task A320-A-56-XX-1022-18ZZZ-311Z-A.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024M4-A-008-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Flow Chart
Page 89
CONF ALL
01NOTE:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE ANDCOMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCETIMES GIVEN IN THIS SERVICE BULLETIN
IN ACCORDANCE WITH PLANNING INFORMATION PARAGRAPH 1.E.(2)
A
DO A DETAILED VISUAL INSPECTION OF THERH SIDE FRONT WINDSHIELD FROM OUTSIDETO DETECT DELAMINATION AND/OR BUBBLES
01
01
FRONT WINDSHIELD FOR GROUP 1DO THE INSPECTION OF THE RH SIDE
IN ACCORDANCE WITH VSBDO THE DETAILED VISUAL INSPECTION OF THE CONNECTOR
CANCONNECTOR BE
OPENED FORINSPECTION?
YES
NO
IS WATER INGRESSOR CORROSION FOUND
IN THE WINDSHIELDCONNECTOR?
NO
NO
YES
C
01
IN THE INSPECTION REPORT SHEETINSULATION TEST AND RECORD THE VALUES
DO THE DIELECTRIC TEST AND THEN THE
ICN-A320-A-56XX1022-A-FAPE3-024M4-A-008-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024PU-A-006-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Flow Chart
Page 90
CONF ALL
01NOTE:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE ANDCOMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCETIMES GIVEN IN THIS SERVICE BULLETIN
IN ACCORDANCE WITH PLANNING INFORMATION PARAGRAPH 1.E.(2)
A
OR
FLY AT FL230 MAXUNDER MMEL 30-42-03B
01
REPAIR THE WEATHER SEALIN ACCORDANCE WITH VSB
01
DE-ICING AND FLY UNDERMMEL 30-42-03A
01
DEACTIVATE THE WINDSHIELD
ARE THEDIELECTRIC AND INSULATION
VALUES RECORDED INTHE GREEN OR AMBER
AREA?NO
YESOR
ISTHIS SERVICE BULLETIN
APPLICABLE FOR THE PN OFTHE SPARE WINDSHIELD?
01
REPORT TO AIRBUS (MONITORED RETROFIT)SEND THE WINDSHIELD INSPECTION
NO FURTHER ACTION WITHTHIS SERVICE BULLETIN
SHOPINSPECTION?
FINDING DURINGIS THERE ANY
YES
OF THE SPARE WINDSHIELDDO THE SHOP INSPECTION
IN ACCORDANCE WITH VSB
01
NO
INSTALLED BEFORE ON ADIFFERENT AIRCRAFT?
SPARE WINDSHIELDWAS THE
YES
YES
REPORT TO AIRBUS (MONITORED RETROFIT) 01SEND THE WINDSHIELD INSPECTION
DO THE INSPECTION AGAINAT THE COMPLIANCE TIME DEFINED 01
NO
DO A CHECK OF THE PN OF A SPARE WINDSHIELDBEFORE THE REPLACEMENT OF THE
01DAMAGED WINDSHIELD
01
WINDSHIELD WITH THE REPLACE THE DAMAGED
SPARE WINDSHIELD
01
WINDSHIELD WITH THE REPLACE THE DAMAGED
SPARE WINDSHIELD
A
B
AC
OR
NO
B
01
WITH VSBREPAIR THE WEATHER SEAL IN ACCORDANCE
DO THE INSPECTIONS AGAINAT THE COMPLIANCE TIME DEFINED 01
ICN-A320-A-56XX1022-A-FAPE3-024PU-A-006-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024FH-A-006-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Criteria of Delamination and Bubbles, RH side
Page 91
CONF ALL
FR1
FR12
Z210
VIEW LOOKING AFT
AREA WHERE THE DELAMINATION AND BUBBLES ARE PERMITTED01
NOTE:
INSPECTION AREA
AREA WHERE THE DELAMINATION AND BUBBLES ARE NOT PERMITTED02
02
20 mm
(0.787 in)
A
A
A
A
AA
75 mm
(2.953 in)
20 mm
(0.787 in)
20 mm
01
60 mm
(2.362 in)
VIEW LOOKING AFT
VIEW LOOKING AFT
A3DG2
A
B
ICN-A320-A-56XX1022-A-FAPE3-024FH-A-006-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024P7-A-007-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Criteria of Delamination and Bubbles, RH side
Page 92
CONF ALL
A ATYPICAL VIEW
20 mm
(0.787 in)
POSSIBLE LOCATIONS OFDELAMINATION/BUBBLES
WEATHER SEAL
WINDSHIELD
TYPICAL VIEWEXAMPLE OF DELAMINATION
AND BUBBLES FINDINGS
FROM OUTSIDE, USE A RULER TO MEASURE 03THE WIDTH FROM THE WEATHER SEAL EDGE
03
NOTE:
B
ICN-A320-A-56XX1022-A-FAPE3-024P7-A-007-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024T3-A-001-01 SHEET 1/1REV 00 Jan 28/21 A320-56-1022Disconnection/Connection of the Front Windshield
Connector from the Aircraft Wiring, RH side Page 93
CONF ALL
A B
A B
EXAMPLE OF THE WINDSHIELDHARNESS PLUG CONNECTED
TO THE WINDSHIELD CONNECTOR
VIEW LOOKING DOWN
FWD
EXAMPLE OF THE WINDSHIELDHARNESS PLUG DISCONNECTED
FROM THE WINDSHIELD CONNECTOR
VIEW LOOKING DOWN
FWD
ICN-A320-A-56XX1022-A-FAPE3-024T3-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 94
(3) Task A320-A-56-XX-1022-11001-311A-A (A320-A-56-XX-1022-11ZZZ-311Z-A)Do a Detailed Inspection of the Connector in accordance with VSB(Depending on the Inspection Result)Job Set-Up Information
Procedure(a) Standard Practices given in this procedure:
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the protection of the connectors, contacts and terminals, refer to Ref.
ESPM 20-54-50.(b) Open the connector in accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-
56-001.(c) Do the detailed visual inspection of the connector in accordance with Ref. SAINT-
GOBAIN (F0360) VSB STA320-56-001.(d) Close the connector in accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-
56-001.(e) Continue the inspection of the front windshield:
1 For LH side windshield, go back to Ref. Task A320-A-56-XX-1022-09ZZZ-311Z-A, step (b)8.
2 For RH side windshield, go back to Ref. Task A320-A-56-XX-1022-10ZZZ-311Z-A, step (b)8.
(4) Task A320-A-56-XX-1022-04001-900A-A (A320-A-56-XX-1022-04ZZZ-900Z-A)Prepare the Weather Seal before Electrical Tests in accordance with VSB(Depending on the Inspection Result)Job Set-Up Information
(a) Standard Practices given in this procedure:1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.
(b) Prepare the weather seal before electrical tests in accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001 and refer to Ref. Fig. Preparation of theFront Windshield before Dielectric and Insulation Tests in accordance with VSB.
(c) Continue the inspection of the front windshield:1 For LH side windshield, go back to Ref. Task A320-A-56-XX-1022-09ZZZ-
311Z-A, step (b)13.a.2 For RH side windshield, go back to Ref. Task A320-A-56-XX-1022-10ZZZ-
311Z-A, step (b)13.a.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024RM-A-002-01 SHEET 1/1REV 00 Jan 28/21 A320-56-1022Preparation of the Front Windshield before Dielectric and Insulation Tests in accordance with VSB
Page 96
CONF ALL
FR1
FR12
Z210
A
3DG13DG2
LHRH
WEATHER SEAL
METALLIC Z BAR
ARH SHOWN
LH SYMMETRICAL
50 mm
(1.969 in)
TYPICAL WINDSHIELD
WEATHER SEAL
ICN-A320-A-56XX1022-A-FAPE3-024RM-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 97
(5) Task A320-A-56-XX-1022-02001-690A-A (A320-A-56-XX-1022-02ZZZ-690Z-A)Repair the Weather Seal in accordance with VSB (Depending on theInspection Result)Job Set-Up Information
Working Area
Impacted Zone Access / Work Location210
Material necessary to do the job
ConsumablesITEM REFERENCE CML DESCRIPTION DRAWING SEE NOTES
06AFB1 Polysulfide Sealant -Windshield Fillet
06PAG1 Adhesion Promoter - ForPolysulfide Sealant
Referenced Information
Manuals/Drawings References/SheetsAMM 06-20-00, Page Block 001CML CONSUMABLE MATERIAL LIST (CML)VSB SAINT-GOBAIN (F0360) VSB STA320-56-001
Procedure(a) Standard Practices given in this procedure:
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.(b) Repair the weather seal in accordance with Ref. SAINT-GOBAIN (F0360) VSB
STA320-56-001, use:
Polysulfide Sealant -Windshield Fillet
06AFB1
Adhesion Promoter - ForPolysulfide Sealant
06PAG1
NOTE: Refer to Ref. CML for alternative consumable materials.
(c) Continue the inspection of the front windshield:1 For LH side windshield, go back to Ref. Task A320-A-56-XX-1022-09ZZZ-
311Z-A, step (b)13.e.<2><a>[2].2 For RH side windshield, go back to Ref. Task A320-A-56-XX-1022-10ZZZ-
Procedure(a) Standard Practices given in this procedure:
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.(b) Do the shop inspection of the spare windshield in accordance with Ref. SAINT-
GOBAIN (F0360) VSB STA320-56-001.(c) Continue the inspection of the front windshield:
1 For LH side windshield, go back to Ref. Task A320-A-56-XX-1022-09ZZZ-311Z-A, step (d)2.a.<2><a>.
2 For RH side windshield, go back to Ref. Task A320-A-56-XX-1022-10ZZZ-311Z-A, step (d)2.a.<2><a>.
(7) Task A320-A-56-XX-1022-07001-90AA-A (A320-A-56-XX-1022-07ZZZ-90AZ-A)Complete and Send the Inspection Report Sheet, LH sideJob Set-Up Information
Manpower/Resources/Skills
Man-hours 0.10 hMinimum Number of person 1Elapsed Time 0.10 h
Referenced Information
Manuals/Drawings References/SheetsISI 00.00.00179
Procedure(a) Complete the inspection report sheet, LH side, refer to Ref. Fig. Inspection Report
Sheet, LH side.(b) Send the completed inspection report sheet in accordance with Ref. ISI
00.00.00179.
NOTE: To send the Inspection Report sheet is not Required for Compliance (RC).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024F6-A-004-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Inspection Report Sheet, LH side
Page 99
CONF ALL
INSPECTION REPORT
SERVICE BULLETIN No :
A/C MSN :
FLIGHT CYCLES (FC) :
A320-56-1022
DATE OF INSPECTION :
INSPECTION METHOD : DETAILEDINSPECTION
SEND THE COMPLETED INSPECTION REPORTSHEET IN ACCORDANCE WITH ISI 00.00.00179
OPERATOR
IN SHOPINSPECTION TYPE ON AIRCRAFT
INSPECTION DATE
WINDSHIELD INFORMATION
PART NUMBER (PN)
SERIAL NUMBER (SN)
FIRST INSTALLATION DATE
FC
FH
FLIGHT HOURS (FH) :
GROUP 2 ONLY
FAULT MESSAGE "561000 LWINDSHIELD SENSOR"
RECORDED SINCEWINDSHIELD INSTALLATION
ON AIRCRAFT?
NOYES
APPLICABLETHRESHOLD 4 MONTHS 12 MONTHS 24 MONTHS
GROUPS 1 AND 3 ONLY
VISUAL INSPECTION FORDELAMINATION AND BUBBLES NIL FINDINGFINDING
ALL GROUPS: CONNECTOR VISUAL INSPECTION RESULTS
CONNECTOR CANBE OPENED? NOYES
WATER INGRESS ORCORROSION INSIDE
CONNECTOR?NOYES
INSPECTION INFORMATION
ICN-A320-A-56XX1022-A-FAPE3-024F6-A-004-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024F7-A-004-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Inspection Report Sheet, LH side
Page 100
CONF ALL
DIELECTRIC TESTVALUE (mA)
INSULATION TESTVALUE (MOhms)
100000
10000
1000
400
10
100
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40
INSULATION (MOhms) Vs DIELECTRIC (mA)
DIELECTRIC (mA)
POST INSPECTION ACTIONS (TICK AND FILL THE CHOSEN OPTION INACCORDANCE WITH SERVICE BULLETIN REQUIREMENTS)
RESULTS AREA GREEN AMBER RED
REPEAT INSPECTION INTERVAL 4 MONTHS 24 MONTHS
WINDSHIELD REPLACEMENTPART NUMBER
INSTALLED
MMEL REFERENCEDISPATCH UNDER MMEL
R_I
NS
ULA
TIO
N (
MO
hms)
GROUPS 1 AND 2 ELECTRICAL TESTS RESULT: REPORT VALUES IN THE FOLLOWING CHART
ICN-A320-A-56XX1022-A-FAPE3-024F7-A-004-01
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(8) Task A320-A-56-XX-1022-08001-90AA-A (A320-A-56-XX-1022-08ZZZ-90AZ-A)Complete and Send the Inspection Report Sheet, RH sideJob Set-Up Information
Manpower/Resources/Skills
Man-hours 0.10 hMinimum Number of person 1Elapsed Time 0.10 h
Referenced Information
Manuals/Drawings References/SheetsISI 00.00.00179
Procedure(a) Complete the inspection report sheet, RH side, refer to Ref. Fig. Inspection Report
Sheet, RH side.(b) Send the completed inspection report sheet in accordance with Ref. ISI
00.00.00179.
NOTE: To send the Inspection Report sheet is not Required for Compliance (RC).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024M5-A-004-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Inspection Report Sheet, RH side
Page 102
CONF ALL
INSPECTION REPORT
SERVICE BULLETIN No :
A/C MSN :
FLIGHT CYCLES (FC) :
A320-56-1022
DATE OF INSPECTION :
INSPECTION METHOD : DETAILEDINSPECTION
SEND THE COMPLETED INSPECTION REPORTSHEET IN ACCORDANCE WITH ISI 00.00.00179
IN SHOPINSPECTION TYPE ON AIRCRAFT
INSPECTION DATE
WINDSHIELD INFORMATION
PART NUMBER (PN)
SERIAL NUMBER (SN)
FIRST INSTALLATION DATE
FC
FH
FLIGHT HOURS (FH) :
GROUP 2 ONLY
FAULT MESSAGE "561000 RWINDSHIELD SENSOR"
RECORDED SINCEWINDSHIELD INSTALLATION
ON AIRCRAFT?
NOYES
APPLICABLETHRESHOLD 4 MONTHS 12 MONTHS 24 MONTHS
GROUPS 1 AND 3 ONLY
VISUAL INSPECTION FORDELAMINATION AND BUBBLES NIL FINDINGFINDING
ALL GROUPS: CONNECTOR VISUAL INSPECTION RESULTS
CONNECTOR CANBE OPENED? NOYES
WATER INGRESS ORCORROSION INSIDE
CONNECTOR?NOYES
OPERATOR
INSPECTION INFORMATION
ICN-A320-A-56XX1022-A-FAPE3-024M5-A-004-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024M6-A-004-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Inspection Report Sheet, RH side
Page 103
CONF ALL
GROUPS 1 AND 2 ELECTRICAL TESTS RESULT: REPORT VALUES IN THE FOLLOWING CHART
DIELECTRIC TESTVALUE (mA)
INSULATION TESTVALUE (MOhms)
100000
10000
1000
400
10
100
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40
INSULATION (MOhms) Vs DIELECTRIC (mA)
DIELECTRIC (mA)
POST INSPECTION ACTIONS (TICK AND FILL THE CHOSEN OPTION INACCORDANCE WITH SERVICE BULLETIN REQUIREMENTS)
RESULTS AREA GREEN AMBER RED
REPEAT INSPECTION INTERVAL 4 MONTHS 24 MONTHS
WINDSHIELD REPLACEMENTPART NUMBER
INSTALLED
MMEL REFERENCE
R_I
NS
ULA
TIO
N (
MO
hms)
DISPATCH UNDER MMEL
ICN-A320-A-56XX1022-A-FAPE3-024M6-A-004-01
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D. PREPARATION FOR TESTNone
E. TESTNone
F. CLOSE-UP(1) Task A320-A-56-XX-1022-03001-740A-A (A320-A-56-XX-1022-03ZZZ-740Z-A)
Install the Lining Panels Removed for Access on the AircraftJob Set-Up Information
Working Area
Impacted Zone Access / Work Location210
Manpower/Resources/Skills
Man-hours 0.10 hMinimum Number of person 1Elapsed Time 0.10 hSkills Airframe
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-20-00, Page Block 001Task 56-11-11-400-001
SRM 51-42-00
Procedure
NOTE: If you intend to accomplish an associated Inspection/Repair Task during thesame layover period, the subsequent Close-up procedure is not necessary.
(a) Standard Practices given in this procedure:1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 Remove and install fasteners in accordance with Ref. SRM 51-42-00.
(b) Install the lining Panel 211MW removed for access, refer to Ref. Fig. Installationof the Lining Panels Removed for Access:1 Install the vertical lining Panel 211MW, refer to Ref. AMM Task 56-11-11-
400-001 and Ref. Fig. Installation of the Lining Panels Removed for Access,sheet 01 and sheet 02, view C:
FIN 211MW1 VERTICAL LINING PANEL Item (1) Retained
attach with:
2 SCREW Item (2) Retained
1 WASHER Item (3) Retained2 Tighten the screws, item (2), refer to Ref. Fig. Installation of the Lining
Panels Removed for Access, sheet 01 and sheet 02, view C.
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(c) Install the lining Panel 211LW removed for access, refer to Ref. Fig. Installation ofthe Lining Panels Removed for Access:1 Install the lining Panel 211LW, refer to Ref. Fig. Installation of the Lining
Panels Removed for Access, sheet 01 and sheet 02, view B:
FIN 211LW1 LINING PANEL Item (4) Retained
attach with:
4 STUD ASSEMBLIES Item (6) Retained
4 LOCKNUT Item (7) Retained2 Tighten the four stud assemblies, item (6), refer to Ref. Fig. Installation of
the Lining Panels Removed for Access, sheet 01.3 Lock the fastener, item (5), refer to Ref. Fig. Installation of the Lining Panels
Removed for Access, sheet 01 and sheet 02, view B.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024SX-A-001-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Installation of the Lining Panels Removed for Access
Page 106
CONF ALL
(4)211LW
(7)
(6)
(7)
(7)
(7) A
B
A
C
ICN-A320-A-56XX1022-A-FAPE3-024SX-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024SY-A-001-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Installation of the Lining Panels Removed for Access
Page 107
CONF ALL
(5)
(1)211MW
C
B
(2)
(2)
(3)
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(2) Task A320-A-56-XX-1022-04001-740A-A (A320-A-56-XX-1022-04ZZZ-740Z-A)Close-upJob Set-Up Information
Working Area
Impacted Zone Access / Work Location210
Manpower/Resources/Skills
Man-hours 0.10 hMinimum Number of person 1Elapsed Time 0.10 h
Referenced Information
Manuals/Drawings References/Sheets
AMM Task 25-13-41-400-002Task 56-11-11-400-001
Procedure
NOTE: If you intend to accomplish an associated Inspection/Repair Task during thesame layover period, the subsequent Close-up procedure is not necessary.
(a) Make sure that the work areas are clean and clear of tools and other items ofequipment.
(b) Do the close-up procedure as specified in the installation of the windshields (FIN3DG1 and FIN 3DG2), refer to Ref. AMM Task 56-11-11-400-001.
NOTE: This procedure is necessary for the installation of the lining Panel211LW.
(c) Do the close-up procedure as specified in the installation of the sidewall panels,refer to Ref. AMM Task 25-13-41-400-002.
NOTE: This procedure is necessary for the installation of the lining Panel211MW.
(d) Put the aircraft back to its initial configuration.G. ADMINISTRATIVE
ProcedureConfirm in the applicable aircraft records that you have completed all the work definedin this Service Bulletin task set as required.
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Task set A320-A-56-XX-1022-03000-93BA-A (A320-A-56-XX-1022-03ZZZ-93BZ-A)Detailed Inspection of the Front Windshields for Group 2 (Depending on the PN of theWindshields)
WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONSINCLUDED IN THE REFERENCED PROCEDURES.
WARNING: BEFORE YOU START WORK, YOU MUST PUT ON A SAFETY HARNESS ANDATTACH IT TO THE ACCESS PLATFORM. WITHOUT A SAFETY HARNESS, YOUCAN FALL. THIS CAN KILL YOU OR CAUSE YOU INJURY.
WARNING: BEFORE YOU DO THIS TASK:- MAKE SURE THAT THE AREA BELOW THE WORK AREA IS CLEAR OF
PERSONS- PUT PROTECTION ON THE PARTS BELOW THE WORK AREA IF
APPLICABLE.IF OBJECTS FALL ACCIDENTALLY, THEY CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO THE AIRCRAFT.
CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICALWIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLYSERVICEABLE). WHEN YOU DO A MAINTENANCE WORK, REPAIRS ORMODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS ANDTHE 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 ANDDAMAGE TO THE ELECTRICAL WIRING INSTALLATION.IF THERE IS CONTAMINATION, REFER TO Ref. ESPM 20-55-00.
NOTE: The accomplishment instructions of this Service Bulletin include procedures given inother documents or in other sections of the Service Bulletin. When the words “refer to”are used and the operator has a procedure accepted by the local authority he belongs to,the accepted alternative procedure can be used. When the words “in accordance with”are used then the given procedure must be followed.
NOTE: The access and close-up instructions, not comprising return to service tests, in thisService Bulletin do not constitute or affect the technical intent of the Service Bulletin.Operators can therefore, as deemed necessary, omit or add access and/or close-up stepsto add flexibility to their maintenance operations as long as the technical intent of theService Bulletin is met within the set parameters.
NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Referto paragraph 1.J., References, for the definition of acronyms.
NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory byan Airworthiness Directive (AD). The paragraphs 3.C. and 3.E. in these accomplishmentinstructions are Required for Compliance (RC) and must be done to comply with the AD.To allow more flexibility, the rule "refer to" and "in accordance with" will apply to theseparagraphs 3.C. and 3.E. Other paragraphs are recommended and may be deviated from,done as part of other actions or done with accepted methods different from those givenin the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can beput back into a serviceable condition.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 110
NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance necessaryto ensure the continued airworthiness of the aircraft.For any deviations to the instructions, including Required for Compliance paragraphcontained herein, contact AIRBUS for further instructions and approval.
NOTE: The purpose of flowcharts is to supplement the information given in the Procedure andCompliance paragraphs and not to serve as the primary source for tasks or compliancetimes given in this Service Bulletin.
A. TASK SET ASSOCIATED INFORMATIONTask Manpower
TOTAL MAN-HOURS 2.80 hELAPSED TIME (HOURS) 1.35 hAdditional man-hours related to Vendor SB; refer to:SAINT-GOBAIN (F0360) VSB STA320-56-001
B. PREPARATION(1) Task A320-A-56-XX-1022-10001-540A-A (A320-A-56-XX-1022-10ZZZ-540Z-A)
Job Set-upJob Set-Up Information
Manpower/Resources/Skills
Man-hours 0.10 hMinimum Number of person 1Elapsed Time 0.10 h
NOTE: For the basic Aircraft configuration, refer to AMM Chapter “Introduction -Aircraft status for maintenance" in Manual Front Matter section.
(a) Make sure that the aircraft is electrically grounded, refer to Ref. AMM Task 12-34-24-869-002.
(b) Do the job set-up procedure as specified in the removal of the sidewall panels,refer to Ref. AMM Task 25-13-41-000-002.
NOTE: This procedure is necessary for the removal of the lining Panel 211MW.
(c) Do the job set-up procedure as specified in the removal of the windshields (FIN3DG1 and FIN 3DG2), refer to Ref. AMM Task 56-11-11-000-001.
NOTE: This procedure is necessary for the removal of the lining Panel 211LW.
(2) Task A320-A-56-XX-1022-11001-540A-A (A320-A-56-XX-1022-11ZZZ-540Z-A)Remove for Access the Lining Panels from the Aircraft
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Job Set-Up InformationWorking Area
Impacted Zone Access / Work Location210
Manpower/Resources/Skills
Man-hours 0.10 hMinimum Number of person 1Elapsed Time 0.10 hSkills Airframe
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-20-00, Page Block 001Task 56-11-11-000-001
SRM 51-42-00
Procedure(a) Standard Practices given in this procedure:
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 Remove and install fasteners in accordance with Ref. SRM 51-42-00.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.(b) Remove the lining Panel 211LW for access, refer to Ref. Fig. Removal of the
Lining Panels for Access.1 Release the stud assemblies, item (6), refer to Ref. Fig. Removal of the
Lining Panels for Access, sheet 01:
4 LOCKNUT Item (7) Retain
4 STUD ASSEMBLIES Item (6) Retain2 Loosen the fastener, item (5), refer to Ref. Fig. Removal of the Lining Panels
for Access, sheet 01 and sheet 02, view B.3 Remove the lining Panel 211LW, refer to Ref. Fig. Removal of the Lining
Panels for Access, sheet 01:
FIN 211LW1 LINING PANEL Item (4) Retain
NOTE: The lining Panel 211LW, item (4), prevents damage to the sensors.
(c) Remove the lining Panel 211MW for access, refer to Ref. Fig. Removal of theLining Panels for Access.1 Remove, refer to Ref. AMM Task 56-11-11-000-001 and Ref. Fig. Removal of
the Lining Panels for Access, sheet 01 and sheet 02, view C:
2 SCREW Item (2) Retain
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1 WASHER Item (3) Retain2 Remove the lining Panel 211MW, refer to Ref. AMM Task 56-11-11-000-001
and Ref. Fig. Removal of the Lining Panels for Access, sheet 01 and sheet02, view C:
FIN 211MW1 VERTICAL LINING PANEL Item (1) Retain
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024EZ-A-001-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Removal of the Lining Panels for Access
Page 113
CONF ALL
(4)211LW
(7)
(6)
(7)
(7)
(7) A
B
A
C
ICN-A320-A-56XX1022-A-FAPE3-024EZ-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024F0-A-002-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Removal of the Lining Panels for Access
Page 114
CONF ALL
(5)
(1)211MW
C
B
(2)
(2)
(3)
ICN-A320-A-56XX1022-A-FAPE3-024F0-A-002-01
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C. PROCEDURE(1) Task A320-A-56-XX-1022-13001-311A-A (A320-A-56-XX-1022-13ZZZ-311Z-A)
Do the Inspection of the LH side Front WindshieldJob Set-Up Information
Working Area
Impacted Zone Access / Work Location211
Manpower/Resources/Skills
Man-hours 1.10 hMinimum Number of person 2Elapsed Time 0.55 hSkills Airframe
Material necessary to do the job
Aircraft standard toolsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
NOTE: This procedure is to be done only if the LH side front windshield installed onaircraft is in Group 2, refer to Ref. Task set A320-A-56-XX-1022-01ZZZ-93BZ-A.
(a) Standard Practices given in this procedure:1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the protection of the connectors, contacts and terminals, refer to Ref.
ESPM 20-54-50.(b) Do the inspection of the LH side front windshield for Group 2, refer to Ref.
Fig. Flow Chart at the compliance time defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2):1 Do the operational test of the windshield anti-icing and defogging, refer to
Ref. AMM Task 30-42-00-710-001:a If fault found, use dedicated TSM.
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2 Record the test result on the Inspection Report sheet in accordance withRef. Task A320-A-56-XX-1022-09ZZZ-90AZ-A.
WARNING: MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THEWEATHER RADAR ARE OPENED, SAFETIED AND TAGGED.
3 Open, safety/lock and tag this (these) circuit breaker(s):
NOTE: For the circuit breaker location, refer to Ref. AMM 24-50-00.
NOTE: For the circuit breaker safety practices, refer to Ref. AMM Task 20-16-00-912-001.
4 Disconnect the windshield connector from the aircraft wiring, refer to Ref.Fig. Disconnection/Connection of the Front Windshield Connector from theAircraft Wiring, LH side.
5 Open the connector in accordance with Ref. SAINT-GOBAIN (F0360) VSBSTA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-15ZZZ-311Z-A.
6 Do the detailed visual inspection of the connector in accordance with Ref.SAINT-GOBAIN (F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-15ZZZ-311Z-A:a If the connector cannot be opened for inspection:
<1> Close the connector in accordance with Ref. SAINT-GOBAIN(F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-15ZZZ-311Z-A.
<2> Connect the windshield connector to the aircraft wiring.<3> Fly under MMEL before next flight:
- Deactivate the windshield de-icing, refer to Ref. AMM Task56-10-00-040-001, and then fly under Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03B.OrDo step (d) before next flight.
b If the connector can be opened for inspection:
A318/A319/A320/A321SERVICE BULLETIN
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<1> Do a check for water ingress or corrosion in the windshieldconnector:
NOTE: Refer to Ref. NTM 51-90-00 for using the recommendedendoscope or similar visual inspection aids.
<a> If water ingress or corrosion is found in the windshieldconnector:[1] Close the connector in accordance with Ref. SAINT-
GOBAIN (F0360) VSB STA320-56-001 and refer toRef. Task A320-A-56-XX-1022-15ZZZ-311Z-A.
[2] Connect the windshield connector to the aircraftwiring.
[3] Fly under MMEL before next flight:- Deactivate the windshield de-icing, refer to
Ref. AMM Task 56-10-00-040-001, and then flyunder Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03B.OrDo step (d) before next flight.
<b> If water ingress or corrosion is not found in the windshieldconnector:[1] Do step (b)7.
7 Close the connector in accordance with Ref. SAINT-GOBAIN (F0360) VSBSTA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-15ZZZ-311Z-A.
8 Connect the windshield connector to the aircraft wiring, refer to Ref. Fig.Disconnection/Connection of the Front Windshield Connector from theAircraft Wiring, LH side.
9 Do the operational test of the windshield anti-icing and defogging, refer toRef. AMM Task 30-42-00-710-001:a If fault found, use dedicated TSM.
WARNING: MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THEWEATHER RADAR ARE OPENED, SAFETIED AND TAGGED.
10 Open, safety/lock and tag this (these) circuit breaker(s):
NOTE: For the circuit breaker location, refer to Ref. AMM 24-50-00.
NOTE: For the circuit breaker safety practices, refer to Ref. AMM Task 20-16-00-912-001.
11 Disconnect the windshield connector from the aircraft wiring, refer to Ref.Fig. Disconnection/Connection of the Front Windshield Connector from theAircraft Wiring, LH side.
12 Do the dielectric test and then the insulation test, refer to Ref. AppendixELECTRICAL TESTS RESULT CHART:a Remove a part of the weather seal over the metallic Z bar in
accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001 andrefer to Ref. Task A320-A-56-XX-1022-05ZZZ-900Z-A.
WARNING: THE GSE TOOL 98D56003001000 USES HIGH VOLTAGEDURING THE TEST. BEFORE YOU START THE TEST, MAKESURE THAT ALL SAFETY PRECAUTIONS GIVEN IN THETOOL USER GUIDE ARE FOLLOWED. THE ELECTRICALPOWER IS SUFFICIENTLY STRONG TO CAUSE AN INJURYOR KILL YOU.
b Do the dielectric test (1500VAC during 1 minute) and the insulationtest (500VDC during 1 minute), use tool:
1 WINDSHIELDINSPECTION
98D56003001000
NOTE: You must obey the instruction given in the GSE tool userguide.
c Record the values in the Inspection Report sheet in accordancewith Ref. Task A320-A-56-XX-1022-09ZZZ-90AZ-A and refer to Ref.Appendix ELECTRICAL TESTS RESULT CHART.
d Connect the windshield connector to the aircraft wiring.e Examine the color classification of the results of the dielectric and
insulation tests, refer to Ref. Appendix ELECTRICAL TESTS RESULTCHART:<1> If the electrical tests result is in red area:
<a> Do step (c) or (d) before next flight.<2> If the electrical tests result is in green or amber area:
<a> Do step (d) or do the steps that follow:[1] Do the operational test of the windshield anti-icing
and defogging, refer to Ref. AMM Task 30-42-00-710-001:[a] If fault found, use dedicated TSM.
[2] Repair the weather seal in accordance with Ref.SAINT-GOBAIN (F0360) VSB STA320-56-001 andrefer to Ref. Task A320-A-56-XX-1022-03ZZZ-690Z-A.
[3] Send the result to AIRBUS in accordance with Ref.Task A320-A-56-XX-1022-09ZZZ-90AZ-A.
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[4] Do again the inspection of the LH side frontwindshield for Group 2 at the compliance timedefined in accordance with PLANNING INFORMATIONparagraph 1.E.(2), refer to Ref. Task A320-A-56-XX-1022-13ZZZ-311Z-A.
(c) Do the operational test of the windshield anti-icing and defogging, refer to Ref.AMM Task 30-42-00-710-001 and Ref. Fig. Flow Chart at the compliance timedefined in accordance with PLANNING INFORMATION paragraph 1.E.(2).1 If fault found, use dedicated TSM.2 Repair the weather seal in accordance with Ref. SAINT-GOBAIN (F0360) VSB
STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-03ZZZ-690Z-A.3 Fly under MMEL:
- Deactivate the windshield de-icing, refer to Ref. AMM Task 56-10-00-040-001, and then fly under Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03B.
(d) Replace the damaged windshield with a spare windshield, refer to Ref. Fig.Flow Chart at the compliance time defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2):1 If this Service Bulletin is not applicable for the PN of the spare windshield:
a Replace the damaged windshield with a spare windshield inaccordance with Ref. Task set A320-A-56-XX-1022-01ZZZ-93CZ-A.
b Send the windshield inspection report to AIRBUS (Monitored retrofit)in accordance with Ref. Task A320-A-56-XX-1022-09ZZZ-90AZ-A.
c No further action is necessary with this Service Bulletin.2 If this Service Bulletin is applicable for the PN of the spare windshield:
a Do a check if the spare windshield was installed before on a differentaircraft:<1> If the spare windshield was not installed before on a different
aircraft:<a> Replace the damaged windshield with a spare windshield
in accordance with Ref. Task set A320-A-56-XX-1022-01ZZZ-93CZ-A and refer to Ref. Fig. Flow Chart.
<b> Send the windshield inspection report to AIRBUS(Monitored retrofit) in accordance with Ref. Task A320-A-56-XX-1022-09ZZZ-90AZ-A.
<c> Do again the inspection of the LH side front windshield:[1] If the spare windshield PN is in Group 1:
[a] Do again the inspection of the LH side frontwindshield for Group 1 at the compliancetime defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-09ZZZ-311Z-A.
[2] If the spare windshield PN is in Group 2:[a] Do again the inspection of the LH side front
windshield for Group 2 at the compliance
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 120
time defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-13ZZZ-311Z-A.
[3] If the spare windshield PN is in Group 3:[a] Do again the inspection of the LH side front
windshield for Group 3 at the compliancetime defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-17ZZZ-311Z-A.
<2> If the spare windshield was installed before on a differentaircraft:<a> Do the shop inspection of the spare windshield in
accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-16ZZZ-311Z-A:[1] If there is finding during the shop inspection:
[a] Select another spare windshield and do step(d) again.
[2] If there is no finding during the shop inspection:[a] Replace the damaged windshield with a spare
windshield in accordance with Ref. Task setA320-A-56-XX-1022-01ZZZ-93CZ-A and refer toRef. Fig. Flow Chart.
[b] Send the windshield inspection report toAIRBUS (Monitored retrofit) in accordance withRef. Task A320-A-56-XX-1022-09ZZZ-90AZ-A.
[c] Do again the inspection of the LH side frontwindshield:- If the spare windshield PN is in Group 1:
- Do again the inspection of the LHside front windshield for Group 1at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),refer to Ref. Task A320-A-56-XX-1022-09ZZZ-311Z-A.
- If the spare windshield PN is in Group 2:- Do again the inspection of the LH
side front windshield for Group 2at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),refer to Ref. Task A320-A-56-XX-1022-13ZZZ-311Z-A.
- If the spare windshield PN is in Group 3:- Do again the inspection of the LH
side front windshield for Group 3at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 121
refer to Ref. Task A320-A-56-XX-1022-17ZZZ-311Z-A.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024M9-A-007-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Flow Chart
Page 122
CONF ALL
01NOTE:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE ANDCOMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCETIMES GIVEN IN THIS SERVICE BULLETIN
IN ACCORDANCE WITH PLANNING INFORMATION PARAGRAPH 1.E.(2)
01
IN ACCORDANCE WITH VSBDO THE DETAILED VISUAL INSPECTION OF THE CONNECTOR
CANCONNECTOR BE
OPENED FORINSPECTION?
YESNO
YES
OR
IS WATER INGRESSOR CORROSION FOUND
IN THE WINDSHIELDCONNECTOR?
ARE THEDIELECTRIC AND INSULATION
VALUES RECORDED INTHE GREEN OR AMBER
AREA?
YES
OROR
NO
OR
FLY AT FL230 MAXUNDER MMEL 30-42-03B
01
DE-ICING AND FLY UNDERMMEL 30-42-03A
01
DEACTIVATE THE WINDSHIELD
NO
B
B
B
B
FRONT WINDSHIELD FOR GROUP 2DO THE INSPECTION OF THE LH SIDE A
REPAIR THE WEATHER SEALIN ACCORDANCE WITH VSB
01
01
IN THE INSPECTION REPORT SHEETINSULATION TEST AND RECORD THE VALUES
DO THE DIELECTRIC TEST AND THEN THE
01
WITH VSBREPAIR THE WEATHER SEAL IN ACCORDANCE
DO THE INSPECTIONS AGAINAT THE COMPLIANCE TIME DEFINED 01
A
ICN-A320-A-56XX1022-A-FAPE3-024M9-A-007-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024PY-A-006-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Flow Chart
Page 123
CONF ALL
01NOTE:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE ANDCOMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCETIMES GIVEN IN THIS SERVICE BULLETIN
IN ACCORDANCE WITH PLANNING INFORMATION PARAGRAPH 1.E.(2)
SHOPINSPECTION?
FINDING DURINGIS THERE ANY
YES
OF THE SPARE WINDSHIELDDO THE SHOP INSPECTION
IN ACCORDANCE WITH VSB
INSTALLED BEFORE ON ADIFFERENT AIRCRAFT?
SPARE WINDSHIELDWAS THE
01
YES
NO
DO A CHECK OF THE PN OF A SPARE WINDSHIELDBEFORE THE REPLACEMENT OF THE
01DAMAGED WINDSHIELD
ISTHIS SERVICE BULLETIN
APPLICABLE FOR THE PN OFTHE SPARE WINDSHIELD?
01
REPORT TO AIRBUS (MONITORED RETROFIT)SEND THE WINDSHIELD INSPECTION
NO FURTHER ACTION WITHTHIS SERVICE BULLETIN
REPORT TO AIRBUS (MONITORED RETROFIT) 01SEND THE WINDSHIELD INSPECTION
DO THE INSPECTION AGAINAT THE COMPLIANCE TIME DEFINED 01
01
WINDSHIELD WITH THE REPLACE THE DAMAGED
SPARE WINDSHIELD
YES
NO
01
WINDSHIELD WITH THE REPLACE THE DAMAGED
SPARE WINDSHIELD
NO
A
B
ICN-A320-A-56XX1022-A-FAPE3-024PY-A-006-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024T2-A-001-01 SHEET 1/1REV 00 Jan 28/21 A320-56-1022Disconnection/Connection of the Front Windshield
Connector from the Aircraft Wiring, LH side Page 124
CONF ALL
A B
EXAMPLE OF THE WINDSHIELDHARNESS PLUG CONNECTED
TO THE WINDSHIELD CONNECTOR
VIEW LOOKING DOWN
FWD
EXAMPLE OF THE WINDSHIELDHARNESS PLUG DISCONNECTED
FROM THE WINDSHIELD CONNECTOR
VIEW LOOKING DOWN
FWD
A B
ICN-A320-A-56XX1022-A-FAPE3-024T2-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 125
(2) Task A320-A-56-XX-1022-14001-311A-A (A320-A-56-XX-1022-14ZZZ-311Z-A)Do the Inspection of the RH side Front WindshieldJob Set-Up Information
Working Area
Impacted Zone Access / Work Location212
Manpower/Resources/Skills
Man-hours 1.10 hMinimum Number of person 2Elapsed Time 0.55 hSkills Airframe
Material necessary to do the job
Aircraft standard toolsITEM PART No. QTY (UM) KEYWORD DRAWING SEE NOTES
NOTE: This procedure is to be done only if the RH side front windshield installed onaircraft is in Group 2, refer to Ref. Task set A320-A-56-XX-1022-01ZZZ-93BZ-A.
(a) Standard Practices given in this procedure:1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the protection of the connectors, contacts and terminals, refer to Ref.
ESPM 20-54-50.(b) Do the inspection of the RH side front windshield for group 2, refer to Ref.
Fig. Flow Chart at the compliance time defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2):1 Do the operational test of the windshield anti-icing and defogging, refer to
Ref. AMM Task 30-42-00-710-001:a If fault found, use dedicated TSM.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 126
2 Record the test result on the Inspection Report sheet in accordance withRef. Task A320-A-56-XX-1022-10ZZZ-90AZ-A.
WARNING: MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THEWEATHER RADAR ARE OPENED, SAFETIED AND TAGGED.
3 Open, safety/lock and tag this (these) circuit breaker(s):
NOTE: For the circuit breaker location, refer to Ref. AMM 24-50-00.
NOTE: For the circuit breaker safety practices, refer to Ref. AMM Task 20-16-00-912-001.
4 Disconnect the windshield connector from the aircraft wiring, refer to Ref.Fig. Disconnection/Connection of the Front Windshield Connector from theAircraft Wiring, RH side.
5 Open the connector in accordance with Ref. SAINT-GOBAIN (F0360) VSBSTA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-15ZZZ-311Z-A.
6 Do the detailed visual inspection of the connector in accordance with Ref.SAINT-GOBAIN (F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-15ZZZ-311Z-A:a If the connector cannot be opened for inspection:
<1> Close the connector in accordance with Ref. SAINT-GOBAIN(F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-15ZZZ-311Z-A.
<2> Connect the windshield connector to the aircraft wiring.<3> Fly under MMEL before next flight:
- Deactivate the windshield de-icing, refer to Ref. AMM Task56-10-00-040-001, and then fly under Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03B.OrDo step (d) before next flight.
b If the connector can be opened for inspection:
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 127
<1> Do a check for water ingress or corrosion in the windshieldconnector:
NOTE: Refer to Ref. NTM 51-90-00 for using the recommendedendoscope or similar visual inspection aids.
<a> If water ingress or corrosion is found in the windshieldconnector:[1] Close the connector in accordance with Ref. SAINT-
GOBAIN (F0360) VSB STA320-56-001 and refer toRef. Task A320-A-56-XX-1022-15ZZZ-311Z-A.
[2] Connect the windshield connector to the aircraftwiring.
[3] Fly under MMEL before next flight:- Deactivate the windshield de-icing, refer to
Ref. AMM Task 56-10-00-040-001, and then flyunder Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03B.OrDo step (d) before next flight.
<b> If water ingress or corrosion is not found in the windshieldconnector:[1] Do step (b)7.
7 Close the connector in accordance with Ref. SAINT-GOBAIN (F0360) VSBSTA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-15ZZZ-311Z-A.
8 Connect the windshield connector to the aircraft wiring, refer to Ref. Fig.Disconnection/Connection of the Front Windshield Connector from theAircraft Wiring, RH side.
9 Do the operational test of the windshield anti-icing and defogging, refer toRef. AMM Task 30-42-00-710-001:a If fault found, use dedicated TSM.
WARNING: MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THEWEATHER RADAR ARE OPENED, SAFETIED AND TAGGED.
10 Open, safety/lock and tag this (these) circuit breaker(s):
NOTE: For the circuit breaker location, refer to Ref. AMM 24-50-00.
NOTE: For the circuit breaker safety practices, refer to Ref. AMM Task 20-16-00-912-001.
11 Disconnect the windshield connector from the aircraft wiring, refer to Ref.Fig. Disconnection/Connection of the Front Windshield Connector from theAircraft Wiring, RH side.
12 Do the dielectric test and then the insulation test, refer to Ref. AppendixELECTRICAL TESTS RESULT CHART:a Remove a part of the weather seal over the metallic Z bar in
accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001 andrefer to Ref. Task A320-A-56-XX-1022-05ZZZ-900Z-A.
WARNING: THE GSE TOOL 98D56003001000 USES HIGH VOLTAGEDURING THE TEST. BEFORE YOU START THE TEST, MAKESURE THAT ALL SAFETY PRECAUTIONS GIVEN IN THETOOL USER GUIDE ARE FOLLOWED. THE ELECTRICALPOWER IS SUFFICIENTLY STRONG TO CAUSE AN INJURYOR KILL YOU.
b Do the dielectric test (1500VAC during 1 minute) and the insulationtest (500VDC during 1 minute), use tool:
1 WINDSHIELDINSPECTION
98D56003001000
NOTE: You must obey the instruction given in the GSE tool userguide.
c Record the values in the Inspection Report sheet in accordancewith Ref. Task A320-A-56-XX-1022-10ZZZ-90AZ-A and refer to Ref.Appendix ELECTRICAL TESTS RESULT CHART.
d Connect the windshield connector to the aircraft wiring.e Examine the color classification of the results of the dielectric and
insulation tests, refer to Ref. Appendix ELECTRICAL TESTS RESULTCHART:<1> If the electrical tests result is in red area:
<a> Do step (c) or (d) before next flight.<2> If the electrical tests result is in green or amber area:
<a> Do step (d) or do the steps that follow:[1] Do the operational test of the windshield anti-icing
and defogging, refer to Ref. AMM Task 30-42-00-710-001:[a] If fault found, use dedicated TSM.
[2] Repair the weather seal in accordance with Ref.SAINT-GOBAIN (F0360) VSB STA320-56-001 andrefer to Ref. Task A320-A-56-XX-1022-03ZZZ-690Z-A.
[3] Send the result to AIRBUS in accordance with Ref.Task A320-A-56-XX-1022-10ZZZ-90AZ-A.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 129
[4] Do again the inspection of the RH side frontwindshield for Group 2 at the compliance timedefined in accordance with PLANNING INFORMATIONparagraph 1.E.(2), refer to Ref. Task A320-A-56-XX-1022-14ZZZ-311Z-A.
(c) Do the operational test of the windshield anti-icing and defogging, refer to Ref.AMM Task 30-42-00-710-001 and Ref. Fig. Flow Chart at the compliance timedefined in accordance with PLANNING INFORMATION paragraph 1.E.(2).1 If fault found, use dedicated TSM.2 Repair the weather seal in accordance with Ref. SAINT-GOBAIN (F0360) VSB
STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-03ZZZ-690Z-A.3 Fly under MMEL:
- Deactivate the windshield de-icing, refer to Ref. AMM Task 56-10-00-040-001, and then fly under Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03B.
(d) Replace the damaged windshield with a spare windshield, refer to Ref. Fig.Flow Chart at the compliance time defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2):1 If this Service Bulletin is not applicable for the PN of the spare windshield:
a Replace the damaged windshield with a spare windshield inaccordance with Ref. Task set A320-A-56-XX-1022-01ZZZ-93CZ-A.
b Send the windshield inspection report to AIRBUS (Monitored retrofit)in accordance with Ref. Task A320-A-56-XX-1022-10ZZZ-90AZ-A.
c No further action is necessary with this Service Bulletin.2 If this Service Bulletin is applicable for the PN of the spare windshield:
a Do a check if the spare windshield was installed before on a differentaircraft:<1> If the spare windshield was not installed before on a different
aircraft:<a> Replace the damaged windshield with a spare windshield
in accordance with Ref. Task set A320-A-56-XX-1022-01ZZZ-93CZ-A and refer to Ref. Fig. Flow Chart.
<b> Send the windshield inspection report to AIRBUS(Monitored retrofit) in accordance with Ref. Task A320-A-56-XX-1022-10ZZZ-90AZ-A.
<c> Do again the inspection of the RH side front windshield:[1] If the spare windshield PN is in Group 1:
[a] Do again the inspection of the RH side frontwindshield for Group 1 at the compliancetime defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-10ZZZ-311Z-A.
[2] If the spare windshield PN is in Group 2:[a] Do again the inspection of the RH side front
windshield for Group 2 at the compliance
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 130
time defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-14ZZZ-311Z-A.
[3] If the spare windshield PN is in Group 3:[a] Do again the inspection of the RH side front
windshield for Group 3 at the compliancetime defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-18ZZZ-311Z-A.
<2> If the spare windshield was installed before on a differentaircraft:<a> Do the shop inspection of the spare windshield in
accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-16ZZZ-311Z-A:[1] If there is finding during the shop inspection:
[a] Select another spare windshield and do step(d) again.
[2] If there is no finding during the shop inspection:[a] Replace the damaged windshield with a spare
windshield in accordance with Ref. Task setA320-A-56-XX-1022-01ZZZ-93CZ-A and refer toRef. Fig. Flow Chart.
[b] Send the windshield inspection report toAIRBUS (Monitored retrofit) in accordance withRef. Task A320-A-56-XX-1022-10ZZZ-90AZ-A.
[c] Do again the inspection of the RH side frontwindshield:- If the spare windshield PN is in Group 1:
- Do again the inspection of the RHside front windshield for Group 1at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),refer to Ref. Task A320-A-56-XX-1022-10ZZZ-311Z-A.
- If the spare windshield PN is in Group 2:- Do again the inspection of the RH
side front windshield for Group 2at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),refer to Ref. Task A320-A-56-XX-1022-14ZZZ-311Z-A.
- If the spare windshield PN is in Group 3:- Do again the inspection of the RH
side front windshield for Group 3at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 131
refer to Ref. Task A320-A-56-XX-1022-18ZZZ-311Z-A.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024M2-A-007-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Flow Chart
Page 132
CONF ALL
01NOTE:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE ANDCOMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCETIMES GIVEN IN THIS SERVICE BULLETIN
IN ACCORDANCE WITH PLANNING INFORMATION PARAGRAPH 1.E.(2)
01
IN ACCORDANCE WITH VSBDO THE DETAILED VISUAL INSPECTION OF THE CONNECTOR
CANCONNECTOR BE
OPENED FORINSPECTION?
YESNO
YES
OR
IS WATER INGRESSOR CORROSION FOUND
IN THE WINDSHIELDCONNECTOR?
OR
FLY AT FL230 MAXUNDER MMEL 30-42-03B
01
DE-ICING AND FLY UNDERMMEL 30-42-03A
01
DEACTIVATE THE WINDSHIELD
FRONT WINDSHIELD FOR GROUP 2DO THE INSPECTION OF THE RH SIDE
B
B
ARE THEDIELECTRIC AND INSULATION
VALUES RECORDED INTHE GREEN OR AMBER
AREA?
YES
OROR
NO
NO
B
B
A
REPAIR THE WEATHER SEALIN ACCORDANCE WITH VSB
01
01
IN THE INSPECTION REPORT SHEETINSULATION TEST AND RECORD THE VALUES
DO THE DIELECTRIC TEST AND THEN THE
01
WITH VSBREPAIR THE WEATHER SEAL IN ACCORDANCE
DO THE INSPECTIONS AGAINAT THE COMPLIANCE TIME DEFINED 01
A
ICN-A320-A-56XX1022-A-FAPE3-024M2-A-007-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024Q2-A-006-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Flow Chart
Page 133
CONF ALL
01NOTE:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE ANDCOMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCETIMES GIVEN IN THIS SERVICE BULLETIN
IN ACCORDANCE WITH PLANNING INFORMATION PARAGRAPH 1.E.(2)
SHOPINSPECTION?
FINDING DURINGIS THERE ANY
YES
OF THE SPARE WINDSHIELDDO THE SHOP INSPECTION
IN ACCORDANCE WITH VSB
INSTALLED BEFORE ON ADIFFERENT AIRCRAFT?
SPARE WINDSHIELDWAS THE
01
YES
NO
DO A CHECK OF THE PN OF A SPARE WINDSHIELDBEFORE THE REPLACEMENT OF THE
01DAMAGED WINDSHIELD
ISTHIS SERVICE BULLETIN
APPLICABLE FOR THE PN OFTHE SPARE WINDSHIELD?
01
REPORT TO AIRBUS (MONITORED RETROFIT)SEND THE WINDSHIELD INSPECTION
NO FURTHER ACTION WITHTHIS SERVICE BULLETIN
REPORT TO AIRBUS (MONITORED RETROFIT) 01SEND THE WINDSHIELD INSPECTION
DO THE INSPECTION AGAINAT THE COMPLIANCE TIME DEFINED 01
01
WINDSHIELD WITH THE REPLACE THE DAMAGED
SPARE WINDSHIELD
YES
NO
01
WINDSHIELD WITH THE REPLACE THE DAMAGED
SPARE WINDSHIELD
NO
A
B
ICN-A320-A-56XX1022-A-FAPE3-024Q2-A-006-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024T3-A-001-01 SHEET 1/1REV 00 Jan 28/21 A320-56-1022Disconnection/Connection of the Front Windshield
Connector from the Aircraft Wiring, RH side Page 134
CONF ALL
A B
A B
EXAMPLE OF THE WINDSHIELDHARNESS PLUG CONNECTED
TO THE WINDSHIELD CONNECTOR
VIEW LOOKING DOWN
FWD
EXAMPLE OF THE WINDSHIELDHARNESS PLUG DISCONNECTED
FROM THE WINDSHIELD CONNECTOR
VIEW LOOKING DOWN
FWD
ICN-A320-A-56XX1022-A-FAPE3-024T3-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 135
(3) Task A320-A-56-XX-1022-15001-311A-A (A320-A-56-XX-1022-15ZZZ-311Z-A)Do a Detailed Inspection of the Connector in accordance with VSB(Depending on the Inspection Result)Job Set-Up Information
Procedure(a) Standard Practices given in this procedure:
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the protection of the connectors, contacts and terminals, refer to Ref.
ESPM 20-54-50.(b) Open the connector in accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-
56-001.(c) Do the detailed visual inspection of the connector in accordance with Ref. SAINT-
GOBAIN (F0360) VSB STA320-56-001.(d) Close the connector in accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-
56-001.(e) Continue the inspection of the front windshield:
1 For LH side windshield, go back to Ref. Task A320-A-56-XX-1022-13ZZZ-311Z-A, step (b)7.
2 For RH side windshield, go back to Ref. Task A320-A-56-XX-1022-14ZZZ-311Z-A, step (b)7.
(4) Task A320-A-56-XX-1022-05001-900A-A (A320-A-56-XX-1022-05ZZZ-900Z-A)Prepare the Weather Seal before Electrical Tests in accordance with VSB(Depending on the Inspection Result)Job Set-Up Information
(a) Standard Practices given in this procedure:1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.
(b) Prepare the weather seal before electrical tests in accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001 and refer to Ref. Fig. Preparation of theFront Windshield before Dielectric and Insulation Tests in accordance with VSB.
(c) Continue the inspection of the front windshield:1 For LH side windshield, go back to Ref. Task A320-A-56-XX-1022-13ZZZ-
311Z-A, step (b)12.a.2 For RH side windshield, go back to Ref. Task A320-A-56-XX-1022-14ZZZ-
311Z-A, step (b)12.a.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024RM-A-002-01 SHEET 1/1REV 00 Jan 28/21 A320-56-1022Preparation of the Front Windshield before Dielectric and Insulation Tests in accordance with VSB
Page 137
CONF ALL
FR1
FR12
Z210
A
3DG13DG2
LHRH
WEATHER SEAL
METALLIC Z BAR
ARH SHOWN
LH SYMMETRICAL
50 mm
(1.969 in)
TYPICAL WINDSHIELD
WEATHER SEAL
ICN-A320-A-56XX1022-A-FAPE3-024RM-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 138
(5) Task A320-A-56-XX-1022-03001-690A-A (A320-A-56-XX-1022-03ZZZ-690Z-A)Repair the Weather Seal in accordance with VSB (Depending on theInspection Result)Job Set-Up Information
Working Area
Impacted Zone Access / Work Location210
Material necessary to do the job
ConsumablesITEM REFERENCE CML DESCRIPTION DRAWING SEE NOTES
06AFB1 Polysulfide Sealant -Windshield Fillet
06PAG1 Adhesion Promoter - ForPolysulfide Sealant
Referenced Information
Manuals/Drawings References/SheetsAMM 06-20-00, Page Block 001CML CONSUMABLE MATERIAL LIST (CML)VSB SAINT-GOBAIN (F0360) VSB STA320-56-001
Procedure(a) Standard Practices given in this procedure:
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.(b) Repair the weather seal in accordance with Ref. SAINT-GOBAIN (F0360) VSB
STA320-56-001, use:
Polysulfide Sealant -Windshield Fillet
06AFB1
Adhesion Promoter - ForPolysulfide Sealant
06PAG1
NOTE: Refer to Ref. CML for alternative consumable materials.
(c) Continue the inspection of the front windshield:1 For LH side windshield, go back to Ref. Task A320-A-56-XX-1022-13ZZZ-
311Z-A, step (b)12.e.<2><a>[2].2 For RH side windshield, go back to Ref. Task A320-A-56-XX-1022-14ZZZ-
Procedure(a) Standard Practices given in this procedure:
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.(b) Do the shop inspection of the spare windshield in accordance with Ref. SAINT-
GOBAIN (F0360) VSB STA320-56-001.(c) Continue the inspection of the front windshield:
1 For LH side windshield, go back to Ref. Task A320-A-56-XX-1022-13ZZZ-311Z-A, step (d)2.a.<2><a>.
2 For RH side windshield, go back to Ref. Task A320-A-56-XX-1022-14ZZZ-311Z-A, step (d)2.a.<2><a>.
(7) Task A320-A-56-XX-1022-09001-90AA-A (A320-A-56-XX-1022-09ZZZ-90AZ-A)Complete and Send the Inspection Report Sheet, LH sideJob Set-Up Information
Manpower/Resources/Skills
Man-hours 0.10 hMinimum Number of person 1Elapsed Time 0.10 h
Referenced Information
Manuals/Drawings References/SheetsISI 00.00.00179
Procedure(a) Complete the inspection report sheet, LH side, refer to Ref. Fig. Inspection Report
Sheet, LH side.(b) Send the completed inspection report sheet in accordance with Ref. ISI
00.00.00179.
NOTE: To send the Inspection Report sheet is not Required for Compliance (RC).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024F6-A-004-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Inspection Report Sheet, LH side
Page 140
CONF ALL
INSPECTION REPORT
SERVICE BULLETIN No :
A/C MSN :
FLIGHT CYCLES (FC) :
A320-56-1022
DATE OF INSPECTION :
INSPECTION METHOD : DETAILEDINSPECTION
SEND THE COMPLETED INSPECTION REPORTSHEET IN ACCORDANCE WITH ISI 00.00.00179
OPERATOR
IN SHOPINSPECTION TYPE ON AIRCRAFT
INSPECTION DATE
WINDSHIELD INFORMATION
PART NUMBER (PN)
SERIAL NUMBER (SN)
FIRST INSTALLATION DATE
FC
FH
FLIGHT HOURS (FH) :
GROUP 2 ONLY
FAULT MESSAGE "561000 LWINDSHIELD SENSOR"
RECORDED SINCEWINDSHIELD INSTALLATION
ON AIRCRAFT?
NOYES
APPLICABLETHRESHOLD 4 MONTHS 12 MONTHS 24 MONTHS
GROUPS 1 AND 3 ONLY
VISUAL INSPECTION FORDELAMINATION AND BUBBLES NIL FINDINGFINDING
ALL GROUPS: CONNECTOR VISUAL INSPECTION RESULTS
CONNECTOR CANBE OPENED? NOYES
WATER INGRESS ORCORROSION INSIDE
CONNECTOR?NOYES
INSPECTION INFORMATION
ICN-A320-A-56XX1022-A-FAPE3-024F6-A-004-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024F7-A-004-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Inspection Report Sheet, LH side
Page 141
CONF ALL
DIELECTRIC TESTVALUE (mA)
INSULATION TESTVALUE (MOhms)
100000
10000
1000
400
10
100
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40
INSULATION (MOhms) Vs DIELECTRIC (mA)
DIELECTRIC (mA)
POST INSPECTION ACTIONS (TICK AND FILL THE CHOSEN OPTION INACCORDANCE WITH SERVICE BULLETIN REQUIREMENTS)
RESULTS AREA GREEN AMBER RED
REPEAT INSPECTION INTERVAL 4 MONTHS 24 MONTHS
WINDSHIELD REPLACEMENTPART NUMBER
INSTALLED
MMEL REFERENCEDISPATCH UNDER MMEL
R_I
NS
ULA
TIO
N (
MO
hms)
GROUPS 1 AND 2 ELECTRICAL TESTS RESULT: REPORT VALUES IN THE FOLLOWING CHART
ICN-A320-A-56XX1022-A-FAPE3-024F7-A-004-01
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(8) Task A320-A-56-XX-1022-10001-90AA-A (A320-A-56-XX-1022-10ZZZ-90AZ-A)Complete and Send the Inspection Report Sheet, RH sideJob Set-Up Information
Manpower/Resources/Skills
Man-hours 0.10 hMinimum Number of person 1Elapsed Time 0.10 h
Referenced Information
Manuals/Drawings References/SheetsISI 00.00.00179
Procedure(a) Complete the inspection report sheet, RH side, refer to Ref. Fig. Inspection Report
Sheet, RH side.(b) Send the completed inspection report sheet in accordance with Ref. ISI
00.00.00179.
NOTE: To send the Inspection Report sheet is not Required for Compliance (RC).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024M5-A-004-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Inspection Report Sheet, RH side
Page 143
CONF ALL
INSPECTION REPORT
SERVICE BULLETIN No :
A/C MSN :
FLIGHT CYCLES (FC) :
A320-56-1022
DATE OF INSPECTION :
INSPECTION METHOD : DETAILEDINSPECTION
SEND THE COMPLETED INSPECTION REPORTSHEET IN ACCORDANCE WITH ISI 00.00.00179
IN SHOPINSPECTION TYPE ON AIRCRAFT
INSPECTION DATE
WINDSHIELD INFORMATION
PART NUMBER (PN)
SERIAL NUMBER (SN)
FIRST INSTALLATION DATE
FC
FH
FLIGHT HOURS (FH) :
GROUP 2 ONLY
FAULT MESSAGE "561000 RWINDSHIELD SENSOR"
RECORDED SINCEWINDSHIELD INSTALLATION
ON AIRCRAFT?
NOYES
APPLICABLETHRESHOLD 4 MONTHS 12 MONTHS 24 MONTHS
GROUPS 1 AND 3 ONLY
VISUAL INSPECTION FORDELAMINATION AND BUBBLES NIL FINDINGFINDING
ALL GROUPS: CONNECTOR VISUAL INSPECTION RESULTS
CONNECTOR CANBE OPENED? NOYES
WATER INGRESS ORCORROSION INSIDE
CONNECTOR?NOYES
OPERATOR
INSPECTION INFORMATION
ICN-A320-A-56XX1022-A-FAPE3-024M5-A-004-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024M6-A-004-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Inspection Report Sheet, RH side
Page 144
CONF ALL
GROUPS 1 AND 2 ELECTRICAL TESTS RESULT: REPORT VALUES IN THE FOLLOWING CHART
DIELECTRIC TESTVALUE (mA)
INSULATION TESTVALUE (MOhms)
100000
10000
1000
400
10
100
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40
INSULATION (MOhms) Vs DIELECTRIC (mA)
DIELECTRIC (mA)
POST INSPECTION ACTIONS (TICK AND FILL THE CHOSEN OPTION INACCORDANCE WITH SERVICE BULLETIN REQUIREMENTS)
RESULTS AREA GREEN AMBER RED
REPEAT INSPECTION INTERVAL 4 MONTHS 24 MONTHS
WINDSHIELD REPLACEMENTPART NUMBER
INSTALLED
MMEL REFERENCE
R_I
NS
ULA
TIO
N (
MO
hms)
DISPATCH UNDER MMEL
ICN-A320-A-56XX1022-A-FAPE3-024M6-A-004-01
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D. PREPARATION FOR TESTNone
E. TESTNone
F. CLOSE-UP(1) Task A320-A-56-XX-1022-06001-740A-A (A320-A-56-XX-1022-06ZZZ-740Z-A)
Install the Lining Panels Removed for Access on the AircraftJob Set-Up Information
Working Area
Impacted Zone Access / Work Location210
Manpower/Resources/Skills
Man-hours 0.10 hMinimum Number of person 1Elapsed Time 0.10 hSkills Airframe
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-20-00, Page Block 001Task 56-11-11-400-001
SRM 51-42-00
Procedure
NOTE: If you intend to accomplish an associated Inspection/Repair Task during thesame layover period, the subsequent Close-up procedure is not necessary.
(a) Standard Practices given in this procedure:1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 Remove and install fasteners in accordance with Ref. SRM 51-42-00.
(b) Install the lining Panel 211MW removed for access, refer to Ref. Fig. Installationof the Lining Panels Removed for Access:1 Install the vertical lining Panel 211MW, refer to Ref. AMM Task 56-11-11-
400-001 and Ref. Fig. Installation of the Lining Panels Removed for Access,sheet 01 and sheet 02, view C:
FIN 211MW1 VERTICAL LINING PANEL Item (1) Retained
attach with:
2 SCREW Item (2) Retained
1 WASHER Item (3) Retained2 Tighten the screws, item (2), refer to Ref. Fig. Installation of the Lining
Panels Removed for Access, sheet 01 and sheet 02, view C.
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(c) Install the lining Panel 211LW removed for access, refer to Ref. Fig. Installation ofthe Lining Panels Removed for Access:1 Install the lining Panel 211LW, refer to Ref. Fig. Installation of the Lining
Panels Removed for Access, sheet 01 and sheet 02, view B:
FIN 211LW1 LINING PANEL Item (4) Retained
attach with:
4 STUD ASSEMBLIES Item (6) Retained
4 LOCKNUT Item (7) Retained2 Tighten the four stud assemblies, item (6), refer to Ref. Fig. Installation of
the Lining Panels Removed for Access, sheet 01.3 Lock the fastener, item (5), refer to Ref. Fig. Installation of the Lining Panels
Removed for Access, sheet 01 and sheet 02, view B.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024SX-A-001-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Installation of the Lining Panels Removed for Access
Page 147
CONF ALL
(4)211LW
(7)
(6)
(7)
(7)
(7) A
B
A
C
ICN-A320-A-56XX1022-A-FAPE3-024SX-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024SY-A-001-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Installation of the Lining Panels Removed for Access
Page 148
CONF ALL
(5)
(1)211MW
C
B
(2)
(2)
(3)
ICN-A320-A-56XX1022-A-FAPE3-024SY-A-001-01
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(2) Task A320-A-56-XX-1022-07001-740A-A (A320-A-56-XX-1022-07ZZZ-740Z-A)Close-upJob Set-Up Information
Manpower/Resources/Skills
Man-hours 0.10 hMinimum Number of person 1Elapsed Time 0.10 h
Referenced Information
Manuals/Drawings References/Sheets
AMM Task 25-13-41-400-002Task 56-11-11-400-001
Procedure
NOTE: If you intend to accomplish an associated Inspection/Repair Task during thesame layover period, the subsequent Close-up procedure is not necessary.
(a) Make sure that the work areas are clean and clear of tools and other items ofequipment.
(b) Do the close-up procedure as specified in the installation of the windshields (FIN3DG1 and FIN 3DG2), refer to Ref. AMM Task 56-11-11-400-001.
NOTE: This procedure is necessary for the installation of the lining Panel211LW.
(c) Do the close-up procedure as specified in the installation of the sidewall panels,refer to Ref. AMM Task 25-13-41-400-002.
NOTE: This procedure is necessary for the installation of the lining Panel211MW.
(d) Put the aircraft back to its initial configuration.G. ADMINISTRATIVE
ProcedureConfirm in the applicable aircraft records that you have completed all the work definedin this Service Bulletin task set as required.
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Task set A320-A-56-XX-1022-04000-93BA-A (A320-A-56-XX-1022-04ZZZ-93BZ-A)Detailed Inspection of the Front Windshields for Group 3 (Depending on the PN of theWindshields)
WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONSINCLUDED IN THE REFERENCED PROCEDURES.
WARNING: BEFORE YOU START WORK, YOU MUST PUT ON A SAFETY HARNESS ANDATTACH IT TO THE ACCESS PLATFORM. WITHOUT A SAFETY HARNESS, YOUCAN FALL. THIS CAN KILL YOU OR CAUSE YOU INJURY.
WARNING: BEFORE YOU DO THIS TASK:- MAKE SURE THAT THE AREA BELOW THE WORK AREA IS CLEAR OF
PERSONS- PUT PROTECTION ON THE PARTS BELOW THE WORK AREA IF
APPLICABLE.IF OBJECTS FALL ACCIDENTALLY, THEY CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO THE AIRCRAFT.
CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICALWIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLYSERVICEABLE). WHEN YOU DO A MAINTENANCE WORK, REPAIRS ORMODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS ANDTHE 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 ANDDAMAGE TO THE ELECTRICAL WIRING INSTALLATION.IF THERE IS CONTAMINATION, REFER TO Ref. ESPM 20-55-00.
NOTE: The accomplishment instructions of this Service Bulletin include procedures given inother documents or in other sections of the Service Bulletin. When the words “refer to”are used and the operator has a procedure accepted by the local authority he belongs to,the accepted alternative procedure can be used. When the words “in accordance with”are used then the given procedure must be followed.
NOTE: The access and close-up instructions, not comprising return to service tests, in thisService Bulletin do not constitute or affect the technical intent of the Service Bulletin.Operators can therefore, as deemed necessary, omit or add access and/or close-up stepsto add flexibility to their maintenance operations as long as the technical intent of theService Bulletin is met within the set parameters.
NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Referto paragraph 1.J., References, for the definition of acronyms.
NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory byan Airworthiness Directive (AD). The paragraphs 3.C. and 3.E. in these accomplishmentinstructions are Required for Compliance (RC) and must be done to comply with the AD.To allow more flexibility, the rule "refer to" and "in accordance with" will apply to theseparagraphs 3.C. and 3.E. Other paragraphs are recommended and may be deviated from,done as part of other actions or done with accepted methods different from those givenin the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can beput back into a serviceable condition.
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NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance necessaryto ensure the continued airworthiness of the aircraft.For any deviations to the instructions, including Required for Compliance paragraphcontained herein, contact AIRBUS for further instructions and approval.
NOTE: The purpose of flowcharts is to supplement the information given in the Procedure andCompliance paragraphs and not to serve as the primary source for tasks or compliancetimes given in this Service Bulletin.
A. TASK SET ASSOCIATED INFORMATIONTask Manpower
TOTAL MAN-HOURS 1.50 hELAPSED TIME (HOURS) 0.95 hAdditional man-hours related to Vendor SB; refer to:SAINT-GOBAIN (F0360) VSB STA320-56-001
B. PREPARATION(1) Task A320-A-56-XX-1022-12001-540A-A (A320-A-56-XX-1022-12ZZZ-540Z-A)
Job Set-upJob Set-Up Information
Manpower/Resources/Skills
Man-hours 0.10 hMinimum Number of person 1Elapsed Time 0.10 h
NOTE: For the basic Aircraft configuration, refer to AMM Chapter “Introduction -Aircraft status for maintenance" in Manual Front Matter section.
(a) Make sure that the aircraft is electrically grounded, refer to Ref. AMM Task 12-34-24-869-002.
(b) Do the job set-up procedure as specified in the removal of the sidewall panels,refer to Ref. AMM Task 25-13-41-000-002.
NOTE: This procedure is necessary for the removal of the lining Panel 211MW.
(c) Do the job set-up procedure as specified in the removal of the windshields (FIN3DG1 and FIN 3DG2), refer to Ref. AMM Task 56-11-11-000-001.
NOTE: This procedure is necessary for the removal of the lining Panel 211LW.
(2) Task A320-A-56-XX-1022-13001-540A-A (A320-A-56-XX-1022-13ZZZ-540Z-A)Remove for Access the Lining Panels from the Aircraft
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Job Set-Up InformationWorking Area
Impacted Zone Access / Work Location210
Manpower/Resources/Skills
Man-hours 0.10 hMinimum Number of person 1Elapsed Time 0.10 hSkills Airframe
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-20-00, Page Block 001Task 56-11-11-000-001
SRM 51-42-00
Procedure(a) Standard Practices given in this procedure:
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 Remove and install fasteners in accordance with Ref. SRM 51-42-00.3 Tag all the parts you must remove and retain to make the subsequent
installation easier.4 Put all the retained hardware in identified plastic bags and attach the bags
to the related unit.(b) Remove the lining Panel 211LW for access, refer to Ref. Fig. Removal of the
Lining Panels for Access.1 Release the stud assemblies, item (6), refer to Ref. Fig. Removal of the
Lining Panels for Access, sheet 01:
4 LOCKNUT Item (7) Retain
4 STUD ASSEMBLIES Item (6) Retain2 Loosen the fastener, item (5), refer to Ref. Fig. Removal of the Lining Panels
for Access, sheet 01 and sheet 02, view B.3 Remove the lining Panel 211LW, refer to Ref. Fig. Removal of the Lining
Panels for Access, sheet 01:
FIN 211LW1 LINING PANEL Item (4) Retain
NOTE: The lining Panel 211LW, item (4), prevents damage to the sensors.
(c) Remove the lining Panel 211MW for access, refer to Ref. Fig. Removal of theLining Panels for Access.1 Remove, refer to Ref. AMM Task 56-11-11-000-001 and Ref. Fig. Removal of
the Lining Panels for Access, sheet 01 and sheet 02, view C:
2 SCREW Item (2) Retain
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1 WASHER Item (3) Retain2 Remove the lining Panel 211MW, refer to Ref. AMM Task 56-11-11-000-001
and Ref. Fig. Removal of the Lining Panels for Access, sheet 01 and sheet02, view C:
FIN 211MW1 VERTICAL LINING PANEL Item (1) Retain
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024EZ-A-001-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Removal of the Lining Panels for Access
Page 154
CONF ALL
(4)211LW
(7)
(6)
(7)
(7)
(7) A
B
A
C
ICN-A320-A-56XX1022-A-FAPE3-024EZ-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024F0-A-002-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Removal of the Lining Panels for Access
Page 155
CONF ALL
(5)
(1)211MW
C
B
(2)
(2)
(3)
ICN-A320-A-56XX1022-A-FAPE3-024F0-A-002-01
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C. PROCEDURE(1) Task A320-A-56-XX-1022-17001-311A-A (A320-A-56-XX-1022-17ZZZ-311Z-A)
Do the Inspection of the LH side Front WindshieldJob Set-Up Information
Working Area
Impacted Zone Access / Work Location211
Manpower/Resources/Skills
Man-hours 0.50 hMinimum Number of person 2Elapsed Time 0.25 hSkills Airframe
NOTE: This procedure is to be done only if the LH side front windshield installed onaircraft is in Group 3, refer to Ref. Task set A320-A-56-XX-1022-01ZZZ-93BZ-A.
(a) Standard Practices given in this procedure:1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the protection of the connectors, contacts and terminals, refer to Ref.
ESPM 20-54-50.(b) Do the inspection of the LH side front windshield for Group 3, refer to Ref.
Fig. Flow Chart at the compliance time defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2):1 Do a detailed visual inspection of the LH side front windshield from outside
to detect delamination or bubbles, refer to Ref. Fig. Criteria of Delaminationand Bubbles, LH side:a If delamination and/or bubbles are visible at inboard edge, top
inboard edge corner and lower inboard edge corner:<1> Record the findings in the inspection report sheet, refer to Ref.
Task A320-A-56-XX-1022-11ZZZ-90AZ-A.<2> Fly under MMEL before next flight:
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- Deactivate the windshield de-icing, refer to Ref. AMM Task56-10-00-040-001, and then fly under Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03BOrDo step (c) before next flight.
b If delamination and/or bubbles are visible at upper, outboard andlower edges, do a check for the width of the delamination and/orbubbles from the weather seal around the front windshield:<1> If delamination and/or bubbles are above the criteria defined in
Ref. Fig. Criteria of Delamination and Bubbles, LH side:<a> Record the findings in the inspection report sheet, refer to
Ref. Task A320-A-56-XX-1022-11ZZZ-90AZ-A.<b> Fly under MMEL before next flight:
- Deactivate the windshield de-icing, refer to Ref.AMM Task 56-10-00-040-001, and then fly under Ref.MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03BOrDo step (c) before next flight.
<2> If delamination and/or bubbles are not above the criteriadefined in Ref. Fig. Criteria of Delamination and Bubbles, LHside:<a> Record the findings in the inspection report sheet, refer to
Ref. Task A320-A-56-XX-1022-11ZZZ-90AZ-A.<b> Do step (b)2.
c If delamination and/or bubbles are not visible:<1> Record the nil finding in the inspection report sheet, refer to Ref.
Task A320-A-56-XX-1022-11ZZZ-90AZ-A.<2> Do step (b)2.
2 Do the operational test of the windshield anti-icing and defogging, refer toRef. AMM Task 30-42-00-710-001:a If fault found, use dedicated TSM.
3 Record the test result on the Inspection Report sheet in accordance withRef. Task A320-A-56-XX-1022-11ZZZ-90AZ-A.
WARNING: MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THEWEATHER RADAR ARE OPENED, SAFETIED AND TAGGED.
4 Open, safety/lock and tag this (these) circuit breaker(s):
PANEL DESIGNATION FIN LOCATION SEE NOTESLIGHTING/STBY/COMP/LIGHT 1LFCOM NAV/RADAR/1 5SQ1COM NAV/RADAR/2 5SQ2ANTI ICE/WINDOWS/L 4DG1
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PANEL DESIGNATION FIN LOCATION SEE NOTESANTI ICE/WINDOWS/R 4DG2ANTI ICE/WHC/1 5DG1ANTI ICE/WHC/2 5DG2ANTI ICE/L/WHSLD 1DG1ANTI ICE/R/WHSLD 1DG2
NOTE: For the circuit breaker location, refer to Ref. AMM 24-50-00.
NOTE: For the circuit breaker safety practices, refer to Ref. AMM Task 20-16-00-912-001.
5 Disconnect the windshield connector from the aircraft wiring, refer to Ref.Fig. Disconnection/Connection of the Front Windshield Connector from theAircraft Wiring, LH side.
6 Open the connector in accordance with Ref. SAINT-GOBAIN (F0360) VSBSTA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-19ZZZ-311Z-A.
7 Do the detailed visual inspection of the connector in accordance with Ref.SAINT-GOBAIN (F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-19ZZZ-311Z-A:a If the connector cannot be opened for inspection:
<1> Close the connector in accordance with Ref. SAINT-GOBAIN(F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-19ZZZ-311Z-A.
<2> Connect the windshield connector to the aircraft wiring, referto Ref. Fig. Disconnection/Connection of the Front WindshieldConnector from the Aircraft Wiring, LH side.
<3> Fly under MMEL before next flight:- Deactivate the windshield de-icing, refer to Ref. AMM Task
56-10-00-040-001, and then fly under Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03BOrDo step (c) before next flight.
b If the connector can be opened for inspection:<1> Do a check for water ingress or corrosion in the windshield
connector:
NOTE: Refer to Ref. NTM 51-90-00 for using the recommendedendoscope or similar visual inspection aids.
<a> If water ingress or corrosion is found in the windshieldconnector:[1] Close the connector in accordance with Ref. SAINT-
GOBAIN (F0360) VSB STA320-56-001 and refer toRef. Task A320-A-56-XX-1022-19ZZZ-311Z-A.
[2] Connect the windshield connector to the aircraftwiring, refer to Ref. Fig. Disconnection/Connection
A318/A319/A320/A321SERVICE BULLETIN
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of the Front Windshield Connector from the AircraftWiring, LH side.
[3] Fly under MMEL before next flight:- Deactivate the windshield de-icing, refer to
Ref. AMM Task 56-10-00-040-001, and then flyunder Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03BOrDo step (c) before next flight.
<b> If water ingress or corrosion is not found in the windshieldconnector:[1] Close the connector in accordance with Ref. SAINT-
GOBAIN (F0360) VSB STA320-56-001 and refer toRef. Task A320-A-56-XX-1022-19ZZZ-311Z-A.
[2] Connect the windshield connector to the aircraftwiring, refer to Ref. Fig. Disconnection/Connectionof the Front Windshield Connector from the AircraftWiring, LH side.
[3] Do the operational test of the windshield anti-icingand defogging, refer to Ref. AMM Task 30-42-00-710-001:[a] If fault found, use dedicated TSM.[b] Do again the inspection of the LH side front
windshield for Group 3 at the compliancetime defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-17ZZZ-311Z-A.
(c) Replace the damaged windshield with a spare windshield, refer to Ref. Fig.Flow Chart at the compliance time defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2):1 If this Service Bulletin is not applicable for the PN of the spare windshield:
a Replace the damaged windshield with a spare windshield inaccordance with Ref. Task set A320-A-56-XX-1022-01ZZZ-93CZ-A.
b Send the windshield inspection report to AIRBUS (Monitored retrofit)in accordance with Ref. Task A320-A-56-XX-1022-11ZZZ-90AZ-A.
c No further action is necessary with this Service Bulletin.2 If this Service Bulletin is applicable for the PN of the spare windshield:
a Do a check if the spare windshield was installed before on a differentaircraft:<1> If the spare windshield was not installed before on a different
aircraft:<a> Replace the damaged windshield with a spare windshield
in accordance with Ref. Task set A320-A-56-XX-1022-01ZZZ-93CZ-A and refer to Ref. Fig. Flow Chart.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 160
<b> Send the windshield inspection report to AIRBUS(Monitored retrofit) in accordance with Ref. Task A320-A-56-XX-1022-11ZZZ-90AZ-A.
<c> Do again the inspection of the LH side front windshield:[1] If the spare windshield PN is in Group 1:
[a] Do again the inspection of the LH side frontwindshield for Group 1 at the compliancetime defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-09ZZZ-311Z-A.
[2] If the spare windshield PN is in Group 2:[a] Do again the inspection of the LH side front
windshield for Group 2 at the compliancetime defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-13ZZZ-311Z-A.
[3] If the spare windshield PN is in Group 3:[a] Do again the inspection of the LH side front
windshield for Group 3 at the compliancetime defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-17ZZZ-311Z-A.
<2> If the spare windshield was installed before on a differentaircraft:<a> Do the shop inspection of the spare windshield in
accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-20ZZZ-311Z-A:[1] If there is finding during the shop inspection:
[a] Select another spare windshield and do step(c) again.
[2] If there is no finding during the shop inspection:[a] Replace the damaged windshield with a spare
windshield in accordance with Ref. Task setA320-A-56-XX-1022-01ZZZ-93CZ-A and refer toRef. Fig. Flow Chart.
[b] Send the windshield inspection report toAIRBUS (Monitored retrofit) in accordance withRef. Task A320-A-56-XX-1022-11ZZZ-90AZ-A.
[c] Do again the inspection of the LH side frontwindshield:- If the spare windshield PN is in Group 1:
- Do again the inspection of the LHside front windshield for Group 1at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),refer to Ref. Task A320-A-56-XX-1022-09ZZZ-311Z-A.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 161
- If the spare windshield PN is in Group 2:- Do again the inspection of the LH
side front windshield for Group 2at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),refer to Ref. Task A320-A-56-XX-1022-13ZZZ-311Z-A.
- If the spare windshield PN is in Group 3:- Do again the inspection of the LH
side front windshield for Group 3at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),refer to Ref. Task A320-A-56-XX-1022-17ZZZ-311Z-A.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-025DQ-A-004-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Flow Chart
Page 162
CONF ALL
01NOTE:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE ANDCOMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCETIMES GIVEN IN THIS SERVICE BULLETIN
IN ACCORDANCE WITH PLANNING INFORMATION PARAGRAPH 1.E.(2)
COMPLIANCE TIME DEFINEDDO THE INSPECTION AGAIN AT THE
B
NO
YES
OR
A
NO
FLY AT FL230 MAXUNDER MMEL 30-42-03B
01
DE-ICING AND FLY UNDERMMEL 30-42-03A
01
DEACTIVATE THE WINDSHIELD
DO A DETAILED VISUAL INSPECTION OF THERH SIDE FRONT WINDSHIELD FROM OUTSIDETO DETECT DELAMINATION AND/OR BUBBLES
01
01
IN ACCORDANCE WITH VSBDO THE DETAILED VISUAL INSPECTION OF THE CONNECTOR
CANCONNECTOR BE
OPENED FORINSPECTION?
YES
NO
01
FRONT WINDSHIELD FOR GROUP 3DO THE INSPECTION OF THE LH SIDE
B
ICN-A320-A-56XX1022-A-FAPE3-025DQ-A-004-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-025DR-A-003-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Flow Chart
Page 163
CONF ALL
01NOTE:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE ANDCOMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCETIMES GIVEN IN THIS SERVICE BULLETIN
IN ACCORDANCE WITH PLANNING INFORMATION PARAGRAPH 1.E.(2)
ISTHIS SERVICE BULLETIN
APPLICABLE FOR THE PN OFTHE SPARE WINDSHIELD?
01
REPORT TO AIRBUS (MONITORED RETROFIT)SEND THE WINDSHIELD INSPECTION
NO FURTHER ACTION WITHTHIS SERVICE BULLETIN
SHOPINSPECTION?
FINDING DURINGIS THERE ANY
YES
OF THE SPARE WINDSHIELDDO THE SHOP INSPECTION
IN ACCORDANCE WITH VSB
INSTALLED BEFORE ON ADIFFERENT AIRCRAFT?
SPARE WINDSHIELDWAS THE
01
YES
REPORT TO AIRBUS (MONITORED RETROFIT) 01SEND THE WINDSHIELD INSPECTION
DO THE INSPECTION AGAINAT THE COMPLIANCE TIME DEFINED 01
NO
DO A CHECK OF THE PN OF A SPARE WINDSHIELDBEFORE THE REPLACEMENT OF THE
01DAMAGED WINDSHIELD
01
WINDSHIELD WITH THE REPLACE THE DAMAGED
SPARE WINDSHIELD
01
WINDSHIELD WITH THE REPLACE THE DAMAGED
SPARE WINDSHIELD
B
A
NO
YES
NO
ICN-A320-A-56XX1022-A-FAPE3-025DR-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024FD-A-006-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Criteria of Delamination and Bubbles, LH side
Page 164
CONF ALL
FR1
FR12
Z210
AREA WHERE THE DELAMINATION AND BUBBLES ARE PERMITTED01
NOTE:
INSPECTION AREA
AREA WHERE THE DELAMINATION AND BUBBLES ARE NOT PERMITTED02
VIEW LOOKING AFT
VIEW LOOKING AFT
20 mm
(0.787 in)
A
A
A
A
AA
01
75 mm
(2.953 in)
60 mm
(2.362 in)
20 mm
(0.787 in)
02
20 mm
(0.787 in)
VIEW LOOKING AFT
A
B
A
3DG1
ICN-A320-A-56XX1022-A-FAPE3-024FD-A-006-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024P5-A-007-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Criteria of Delamination and Bubbles, LH side
Page 165
CONF ALL
A ATYPICAL VIEW
20 mm
(0.787 in)
POSSIBLE LOCATIONS OFDELAMINATION/BUBBLES
WEATHER SEAL
WINDSHIELD
TYPICAL VIEWEXAMPLE OF DELAMINATION
AND BUBBLES FINDINGS
FROM OUTSIDE, USE A RULER TO MEASURE 03THE WIDTH FROM THE WEATHER SEAL EDGE
03
NOTE:
B
ICN-A320-A-56XX1022-A-FAPE3-024P5-A-007-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024T2-A-001-01 SHEET 1/1REV 00 Jan 28/21 A320-56-1022Disconnection/Connection of the Front Windshield
Connector from the Aircraft Wiring, LH side Page 166
CONF ALL
A B
EXAMPLE OF THE WINDSHIELDHARNESS PLUG CONNECTED
TO THE WINDSHIELD CONNECTOR
VIEW LOOKING DOWN
FWD
EXAMPLE OF THE WINDSHIELDHARNESS PLUG DISCONNECTED
FROM THE WINDSHIELD CONNECTOR
VIEW LOOKING DOWN
FWD
A B
ICN-A320-A-56XX1022-A-FAPE3-024T2-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 167
(2) Task A320-A-56-XX-1022-18001-311A-A (A320-A-56-XX-1022-18ZZZ-311Z-A)Do the Inspection of the RH side Front WindshieldJob Set-Up Information
Working Area
Impacted Zone Access / Work Location212
Manpower/Resources/Skills
Man-hours 0.50 hMinimum Number of person 2Elapsed Time 0.25 hSkills Airframe
NOTE: This procedure is to be done only if the RH side front windshield installed onaircraft is in Group 3, refer to Ref. Task set A320-A-56-XX-1022-01ZZZ-93BZ-A.
(a) Standard Practices given in this procedure:1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the protection of the connectors, contacts and terminals, refer to Ref.
ESPM 20-54-50.(b) Do the inspection of the RH side front windshield for Group 3, refer to Ref.
Fig. Flow Chart at the compliance time defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2).1 Do a detailed visual inspection of the RH side front windshield from outside
to detect delamination or bubbles, refer to Ref. Fig. Criteria of Delaminationand Bubbles, RH side:a If delamination and/or bubbles are visible at inboard edge, top
inboard edge corner and lower inboard edge corner:<1> Record the findings in the inspection report sheet, refer to Ref.
Task A320-A-56-XX-1022-12ZZZ-90AZ-A.<2> Fly under MMEL before next flight:
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 168
- Deactivate the windshield de-icing, refer to Ref. AMM Task56-10-00-040-001, and then fly under Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03BOrDo step (c) before next flight.
b If delamination and/or bubbles are visible at upper, outboard andlower edges, do a check for the width of the delamination and/orbubbles from the weather seal around the front windshield:<1> If delamination and/or bubbles are above the criteria defined in
Ref. Fig. Criteria of Delamination and Bubbles, RH side:<a> Record the findings in the inspection report sheet, refer to
Ref. Task A320-A-56-XX-1022-12ZZZ-90AZ-A.<b> Fly under MMEL before next flight:
- Deactivate the windshield de-icing, refer to Ref.AMM Task 56-10-00-040-001, and then fly under Ref.MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03BOrDo step (c) before next flight.
<2> If delamination and/or bubbles are not above the criteriadefined in Ref. Fig. Criteria of Delamination and Bubbles, RHside:<a> Record the findings in the inspection report sheet, refer to
Ref. Task A320-A-56-XX-1022-12ZZZ-90AZ-A.<b> Do step (b)2.
c If delamination and/or bubbles are not visible:<1> Record the nil finding in the inspection report sheet, refer to Ref.
Task A320-A-56-XX-1022-12ZZZ-90AZ-A.<2> Do step (b)2.
2 Do the operational test of the windshield anti-icing and defogging, refer toRef. AMM Task 30-42-00-710-001:a If fault found, use dedicated TSM.
3 Record the test result on the Inspection Report sheet in accordance withRef. Task A320-A-56-XX-1022-12ZZZ-90AZ-A.
WARNING: MAKE SURE THAT THE CIRCUIT BREAKERS RELATED TO THEWEATHER RADAR ARE OPENED, SAFETIED AND TAGGED.
4 Open, safety/lock and tag this (these) circuit breaker(s):
PANEL DESIGNATION FIN LOCATION SEE NOTESLIGHTING/STBY/COMP/LIGHT 1LFCOM NAV/RADAR/1 5SQ1COM NAV/RADAR/2 5SQ2ANTI ICE/WINDOWS/L 4DG1
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 169
PANEL DESIGNATION FIN LOCATION SEE NOTESANTI ICE/WINDOWS/R 4DG2ANTI ICE/WHC/1 5DG1ANTI ICE/WHC/2 5DG2ANTI ICE/L/WHSLD 1DG1ANTI ICE/R/WHSLD 1DG2
NOTE: For the circuit breaker location, refer to Ref. AMM 24-50-00.
NOTE: For the circuit breaker safety practices, refer to Ref. AMM Task 20-16-00-912-001.
5 Disconnect the windshield connector from the aircraft wiring, refer to Ref.Fig. Disconnection/Connection of the Front Windshield Connector from theAircraft Wiring, RH side.
6 Open the connector in accordance with Ref. SAINT-GOBAIN (F0360) VSBSTA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-19ZZZ-311Z-A.
7 Do the detailed visual inspection of the connector in accordance with Ref.SAINT-GOBAIN (F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-19ZZZ-311Z-A:a If the connector cannot be opened for inspection:
<1> Close the connector in accordance with Ref. SAINT-GOBAIN(F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-19ZZZ-311Z-A.
<2> Connect the windshield connector to the aircraft wiring, referto Ref. Fig. Disconnection/Connection of the Front WindshieldConnector from the Aircraft Wiring, RH side.
<3> Fly under MMEL before next flight:- Deactivate the windshield de-icing, refer to Ref. AMM Task
56-10-00-040-001, and then fly under Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03BOrDo step (c) before next flight.
b If the connector can be opened for inspection:<1> Do a check for water ingress or corrosion in the windshield
connector:
NOTE: Refer to Ref. NTM 51-90-00 for using the recommendedendoscope or similar visual inspection aids.
<a> If water ingress or corrosion is found in the windshieldconnector:[1] Close the connector in accordance with Ref. SAINT-
GOBAIN (F0360) VSB STA320-56-001 and refer toRef. Task A320-A-56-XX-1022-19ZZZ-311Z-A.
[2] Connect the windshield connector to the aircraftwiring, refer to Ref. Fig. Disconnection/Connection
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 170
of the Front Windshield Connector from the AircraftWiring, RH side.
[3] Fly under MMEL before next flight:- Deactivate the windshield de-icing, refer to
Ref. AMM Task 56-10-00-040-001, and then flyunder Ref. MMEL 30-42-03A
Or- Fly at FL 230 MAX under Ref. MMEL 30-42-03BOrDo step (c) before next flight.
<b> If water ingress or corrosion is not found in the windshieldconnector:[1] Close the connector in accordance with Ref. SAINT-
GOBAIN (F0360) VSB STA320-56-001 and refer toRef. Task A320-A-56-XX-1022-19ZZZ-311Z-A.
[2] Connect the windshield connector to the aircraftwiring, refer to Ref. Fig. Disconnection/Connectionof the Front Windshield Connector from the AircraftWiring, RH side.
[3] Do the operational test of the windshield anti-icingand defogging, refer to Ref. AMM Task 30-42-00-710-001:[a] If fault found, use dedicated TSM.[b] Do again the inspection of the RH side front
windshield for Group 3 at the compliancetime defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-18ZZZ-311Z-A.
(c) Replace the damaged windshield with a spare windshield, refer to Ref. Fig.Flow Chart at the compliance time defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2):1 If this Service Bulletin is not applicable for the PN of the spare windshield:
a Replace the damaged windshield with a spare windshield inaccordance with Ref. Task set A320-A-56-XX-1022-01ZZZ-93CZ-A.
b Send the windshield inspection report to AIRBUS (Monitored retrofit)in accordance with Ref. Task A320-A-56-XX-1022-12ZZZ-90AZ-A.
c No further action is necessary with this Service Bulletin.2 If this Service Bulletin is applicable for the PN of the spare windshield:
a Do a check if the spare windshield was installed before on a differentaircraft:<1> If the spare windshield was not installed before on a different
aircraft:<a> Replace the damaged windshield with a spare windshield
in accordance with Ref. Task set A320-A-56-XX-1022-01ZZZ-93CZ-A and refer to Ref. Fig. Flow Chart.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 171
<b> Send the windshield inspection report to AIRBUS(Monitored retrofit) in accordance with Ref. Task A320-A-56-XX-1022-12ZZZ-90AZ-A.
<c> Do again the inspection of the RH side front windshield:[1] If the spare windshield PN is in Group 1:
[a] Do again the inspection of the RH side frontwindshield for Group 1 at the compliancetime defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-10ZZZ-311Z-A.
[2] If the spare windshield PN is in Group 2:[a] Do again the inspection of the RH side front
windshield for Group 2 at the compliancetime defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-14ZZZ-311Z-A.
[3] If the spare windshield PN is in Group 3:[a] Do again the inspection of the RH side front
windshield for Group 3 at the compliancetime defined in accordance with PLANNINGINFORMATION paragraph 1.E.(2), refer to Ref.Task A320-A-56-XX-1022-18ZZZ-311Z-A.
<2> If the spare windshield was installed before on a differentaircraft:<a> Do the shop inspection of the spare windshield in
accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-56-001 and refer to Ref. Task A320-A-56-XX-1022-20ZZZ-311Z-A:[1] If there is finding during the shop inspection:
[a] Select another spare windshield and do step(c) again.
[2] If there is no finding during the shop inspection:[a] Replace the damaged windshield with a spare
windshield in accordance with Ref. Task setA320-A-56-XX-1022-01ZZZ-93CZ-A and refer toRef. Fig. Flow Chart.
[b] Send the windshield inspection report toAIRBUS (Monitored retrofit) in accordance withRef. Task A320-A-56-XX-1022-12ZZZ-90AZ-A.
[c] Do again the inspection of the RH side frontwindshield:- If the spare windshield PN is in Group 1:
- Do again the inspection of the RHside front windshield for Group 1at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),refer to Ref. Task A320-A-56-XX-1022-10ZZZ-311Z-A.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 172
- If the spare windshield PN is in Group 2:- Do again the inspection of the RH
side front windshield for Group 2at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),refer to Ref. Task A320-A-56-XX-1022-14ZZZ-311Z-A.
- If the spare windshield PN is in Group 3:- Do again the inspection of the RH
side front windshield for Group 3at the compliance time definedin accordance with PLANNINGINFORMATION paragraph 1.E.(2),refer to Ref. Task A320-A-56-XX-1022-18ZZZ-311Z-A.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-025DT-A-004-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Flow Chart
Page 173
CONF ALL
01NOTE:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE ANDCOMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCETIMES GIVEN IN THIS SERVICE BULLETIN
IN ACCORDANCE WITH PLANNING INFORMATION PARAGRAPH 1.E.(2)
COMPLIANCE TIME DEFINEDDO THE INSPECTION AGAIN AT THE
B
NO
YES
OR
A
NO
FLY AT FL230 MAXUNDER MMEL 30-42-03B
01
DE-ICING AND FLY UNDERMMEL 30-42-03A
01
DEACTIVATE THE WINDSHIELD
DO A DETAILED VISUAL INSPECTION OF THERH SIDE FRONT WINDSHIELD FROM OUTSIDETO DETECT DELAMINATION AND/OR BUBBLES
01
01
FRONT WINDSHIELD FOR GROUP 3DO THE INSPECTION OF THE RH SIDE
B01
IN ACCORDANCE WITH VSBDO THE DETAILED VISUAL INSPECTION OF THE CONNECTOR
CANCONNECTOR BE
OPENED FORINSPECTION?
YES
NO
ICN-A320-A-56XX1022-A-FAPE3-025DT-A-004-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-025DU-A-003-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Flow Chart
Page 174
CONF ALL
01NOTE:
THE PURPOSE OF FLOWCHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE ANDCOMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR COMPLIANCETIMES GIVEN IN THIS SERVICE BULLETIN
IN ACCORDANCE WITH PLANNING INFORMATION PARAGRAPH 1.E.(2)
ISTHIS SERVICE BULLETIN
APPLICABLE FOR THE PN OFTHE SPARE WINDSHIELD?
01
REPORT TO AIRBUS (MONITORED RETROFIT)SEND THE WINDSHIELD INSPECTION
NO FURTHER ACTION WITHTHIS SERVICE BULLETIN
SHOPINSPECTION?
FINDING DURINGIS THERE ANY
YES
OF THE SPARE WINDSHIELDDO THE SHOP INSPECTION
IN ACCORDANCE WITH VSB
INSTALLED BEFORE ON ADIFFERENT AIRCRAFT?
SPARE WINDSHIELDWAS THE
01
YES
REPORT TO AIRBUS (MONITORED RETROFIT) 01SEND THE WINDSHIELD INSPECTION
DO THE INSPECTION AGAINAT THE COMPLIANCE TIME DEFINED 01
NO
DO A CHECK OF THE PN OF A SPARE WINDSHIELDBEFORE THE REPLACEMENT OF THE
01DAMAGED WINDSHIELD
01
WINDSHIELD WITH THE REPLACE THE DAMAGED
SPARE WINDSHIELD
01
WINDSHIELD WITH THE REPLACE THE DAMAGED
SPARE WINDSHIELD
B
A
NO
YES
NO
ICN-A320-A-56XX1022-A-FAPE3-025DU-A-003-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024FH-A-006-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Criteria of Delamination and Bubbles, RH side
Page 175
CONF ALL
FR1
FR12
Z210
VIEW LOOKING AFT
AREA WHERE THE DELAMINATION AND BUBBLES ARE PERMITTED01
NOTE:
INSPECTION AREA
AREA WHERE THE DELAMINATION AND BUBBLES ARE NOT PERMITTED02
02
20 mm
(0.787 in)
A
A
A
A
AA
75 mm
(2.953 in)
20 mm
(0.787 in)
20 mm
01
60 mm
(2.362 in)
VIEW LOOKING AFT
VIEW LOOKING AFT
A3DG2
A
B
ICN-A320-A-56XX1022-A-FAPE3-024FH-A-006-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024P7-A-007-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Criteria of Delamination and Bubbles, RH side
Page 176
CONF ALL
A ATYPICAL VIEW
20 mm
(0.787 in)
POSSIBLE LOCATIONS OFDELAMINATION/BUBBLES
WEATHER SEAL
WINDSHIELD
TYPICAL VIEWEXAMPLE OF DELAMINATION
AND BUBBLES FINDINGS
FROM OUTSIDE, USE A RULER TO MEASURE 03THE WIDTH FROM THE WEATHER SEAL EDGE
03
NOTE:
B
ICN-A320-A-56XX1022-A-FAPE3-024P7-A-007-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024T3-A-001-01 SHEET 1/1REV 00 Jan 28/21 A320-56-1022Disconnection/Connection of the Front Windshield
Connector from the Aircraft Wiring, RH side Page 177
CONF ALL
A B
A B
EXAMPLE OF THE WINDSHIELDHARNESS PLUG CONNECTED
TO THE WINDSHIELD CONNECTOR
VIEW LOOKING DOWN
FWD
EXAMPLE OF THE WINDSHIELDHARNESS PLUG DISCONNECTED
FROM THE WINDSHIELD CONNECTOR
VIEW LOOKING DOWN
FWD
ICN-A320-A-56XX1022-A-FAPE3-024T3-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 178
(3) Task A320-A-56-XX-1022-19001-311A-A (A320-A-56-XX-1022-19ZZZ-311Z-A)Do a Detailed Inspection of the Connector in accordance with VSB(Depending on the Inspection Result)Job Set-Up Information
Procedure(a) Standard Practices given in this procedure:
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 For the protection of the connectors, contacts and terminals, refer to Ref.
ESPM 20-54-50.(b) Open the connector in accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-
56-001.(c) Do the detailed visual inspection of the connector in accordance with Ref. SAINT-
GOBAIN (F0360) VSB STA320-56-001.(d) Close the connector in accordance with Ref. SAINT-GOBAIN (F0360) VSB STA320-
56-001.(e) Continue the inspection of the front windshield:
1 For LH side windshield, go back to Ref. Task A320-A-56-XX-1022-17ZZZ-311Z-A, step (b)7.
2 For RH side windshield, go back to Ref. Task A320-A-56-XX-1022-18ZZZ-311Z-A, step (b)7.
(4) Task A320-A-56-XX-1022-20001-311A-A (A320-A-56-XX-1022-20ZZZ-311Z-A)Do a Shop Inspection of the Spare Windshield in accordance with VSB(Depending on the Inspection Result)Job Set-Up Information
Complete and Send the Inspection Report Sheet, LH sideJob Set-Up Information
Manpower/Resources/Skills
Man-hours 0.05 hMinimum Number of person 1Elapsed Time 0.05 h
Referenced Information
Manuals/Drawings References/SheetsISI 00.00.00179
Procedure(a) Complete the inspection report sheet, LH side, refer to Ref. Fig. Inspection Report
Sheet, LH side.(b) Send the completed inspection report sheet in accordance with Ref. ISI
00.00.00179.
NOTE: To send the Inspection Report sheet is not Required for Compliance (RC).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024F6-A-004-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Inspection Report Sheet, LH side
Page 180
CONF ALL
INSPECTION REPORT
SERVICE BULLETIN No :
A/C MSN :
FLIGHT CYCLES (FC) :
A320-56-1022
DATE OF INSPECTION :
INSPECTION METHOD : DETAILEDINSPECTION
SEND THE COMPLETED INSPECTION REPORTSHEET IN ACCORDANCE WITH ISI 00.00.00179
OPERATOR
IN SHOPINSPECTION TYPE ON AIRCRAFT
INSPECTION DATE
WINDSHIELD INFORMATION
PART NUMBER (PN)
SERIAL NUMBER (SN)
FIRST INSTALLATION DATE
FC
FH
FLIGHT HOURS (FH) :
GROUP 2 ONLY
FAULT MESSAGE "561000 LWINDSHIELD SENSOR"
RECORDED SINCEWINDSHIELD INSTALLATION
ON AIRCRAFT?
NOYES
APPLICABLETHRESHOLD 4 MONTHS 12 MONTHS 24 MONTHS
GROUPS 1 AND 3 ONLY
VISUAL INSPECTION FORDELAMINATION AND BUBBLES NIL FINDINGFINDING
ALL GROUPS: CONNECTOR VISUAL INSPECTION RESULTS
CONNECTOR CANBE OPENED? NOYES
WATER INGRESS ORCORROSION INSIDE
CONNECTOR?NOYES
INSPECTION INFORMATION
ICN-A320-A-56XX1022-A-FAPE3-024F6-A-004-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024F7-A-004-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Inspection Report Sheet, LH side
Page 181
CONF ALL
DIELECTRIC TESTVALUE (mA)
INSULATION TESTVALUE (MOhms)
100000
10000
1000
400
10
100
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40
INSULATION (MOhms) Vs DIELECTRIC (mA)
DIELECTRIC (mA)
POST INSPECTION ACTIONS (TICK AND FILL THE CHOSEN OPTION INACCORDANCE WITH SERVICE BULLETIN REQUIREMENTS)
RESULTS AREA GREEN AMBER RED
REPEAT INSPECTION INTERVAL 4 MONTHS 24 MONTHS
WINDSHIELD REPLACEMENTPART NUMBER
INSTALLED
MMEL REFERENCEDISPATCH UNDER MMEL
R_I
NS
ULA
TIO
N (
MO
hms)
GROUPS 1 AND 2 ELECTRICAL TESTS RESULT: REPORT VALUES IN THE FOLLOWING CHART
ICN-A320-A-56XX1022-A-FAPE3-024F7-A-004-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 182
(6) Task A320-A-56-XX-1022-12001-90AA-A (A320-A-56-XX-1022-12ZZZ-90AZ-A)Complete and Send the Inspection Report Sheet, RH sideJob Set-Up Information
Manpower/Resources/Skills
Man-hours 0.05 hMinimum Number of person 1Elapsed Time 0.05 h
Referenced Information
Manuals/Drawings References/SheetsISI 00.00.00179
Procedure(a) Complete the inspection report sheet, RH side, refer to Ref. Fig. Inspection Report
Sheet, RH side.(b) Send the completed inspection report sheet in accordance with Ref. ISI
00.00.00179.
NOTE: To send the Inspection Report sheet is not Required for Compliance (RC).
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024M5-A-004-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Inspection Report Sheet, RH side
Page 183
CONF ALL
INSPECTION REPORT
SERVICE BULLETIN No :
A/C MSN :
FLIGHT CYCLES (FC) :
A320-56-1022
DATE OF INSPECTION :
INSPECTION METHOD : DETAILEDINSPECTION
SEND THE COMPLETED INSPECTION REPORTSHEET IN ACCORDANCE WITH ISI 00.00.00179
IN SHOPINSPECTION TYPE ON AIRCRAFT
INSPECTION DATE
WINDSHIELD INFORMATION
PART NUMBER (PN)
SERIAL NUMBER (SN)
FIRST INSTALLATION DATE
FC
FH
FLIGHT HOURS (FH) :
GROUP 2 ONLY
FAULT MESSAGE "561000 RWINDSHIELD SENSOR"
RECORDED SINCEWINDSHIELD INSTALLATION
ON AIRCRAFT?
NOYES
APPLICABLETHRESHOLD 4 MONTHS 12 MONTHS 24 MONTHS
GROUPS 1 AND 3 ONLY
VISUAL INSPECTION FORDELAMINATION AND BUBBLES NIL FINDINGFINDING
ALL GROUPS: CONNECTOR VISUAL INSPECTION RESULTS
CONNECTOR CANBE OPENED? NOYES
WATER INGRESS ORCORROSION INSIDE
CONNECTOR?NOYES
OPERATOR
INSPECTION INFORMATION
ICN-A320-A-56XX1022-A-FAPE3-024M5-A-004-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024M6-A-004-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Inspection Report Sheet, RH side
Page 184
CONF ALL
GROUPS 1 AND 2 ELECTRICAL TESTS RESULT: REPORT VALUES IN THE FOLLOWING CHART
DIELECTRIC TESTVALUE (mA)
INSULATION TESTVALUE (MOhms)
100000
10000
1000
400
10
100
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40
INSULATION (MOhms) Vs DIELECTRIC (mA)
DIELECTRIC (mA)
POST INSPECTION ACTIONS (TICK AND FILL THE CHOSEN OPTION INACCORDANCE WITH SERVICE BULLETIN REQUIREMENTS)
RESULTS AREA GREEN AMBER RED
REPEAT INSPECTION INTERVAL 4 MONTHS 24 MONTHS
WINDSHIELD REPLACEMENTPART NUMBER
INSTALLED
MMEL REFERENCE
R_I
NS
ULA
TIO
N (
MO
hms)
DISPATCH UNDER MMEL
ICN-A320-A-56XX1022-A-FAPE3-024M6-A-004-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 185
D. PREPARATION FOR TESTNone
E. TESTNone
F. CLOSE-UP(1) Task A320-A-56-XX-1022-08001-740A-A (A320-A-56-XX-1022-08ZZZ-740Z-A)
Install the Lining Panels Removed for Access on the AircraftJob Set-Up Information
Working Area
Impacted Zone Access / Work Location210
Manpower/Resources/Skills
Man-hours 0.10 hMinimum Number of person 1Elapsed Time 0.10 hSkills Airframe
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-20-00, Page Block 001Task 56-11-11-400-001
SRM 51-42-00
Procedure
NOTE: If you intend to accomplish an associated Inspection/Repair Task during thesame layover period, the subsequent Close-up procedure is not necessary.
(a) Standard Practices given in this procedure:1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.2 Remove and install fasteners in accordance with Ref. SRM 51-42-00.
(b) Install the lining Panel 211MW removed for access, refer to Ref. Fig. Installationof the Lining Panels Removed for Access:1 Install the vertical lining Panel 211MW, refer to Ref. AMM Task 56-11-11-
400-001 and Ref. Fig. Installation of the Lining Panels Removed for Access,sheet 01 and sheet 02, view C:
FIN 211MW1 VERTICAL LINING PANEL Item (1) Retained
attach with:
2 SCREW Item (2) Retained
1 WASHER Item (3) Retained2 Tighten the screws, item (2), refer to Ref. Fig. Installation of the Lining
Panels Removed for Access, sheet 01 and sheet 02, view C.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 186
(c) Install the lining Panel 211LW removed for access, refer to Ref. Fig. Installation ofthe Lining Panels Removed for Access:1 Install the lining Panel 211LW, refer to Ref. Fig. Installation of the Lining
Panels Removed for Access, sheet 01 and sheet 02, view B:
FIN 211LW1 LINING PANEL Item (4) Retained
attach with:
4 STUD ASSEMBLIES Item (6) Retained
4 LOCKNUT Item (7) Retained2 Tighten the four stud assemblies, item (6), refer to Ref. Fig. Installation of
the Lining Panels Removed for Access, sheet 01.3 Lock the fastener, item (5), refer to Ref. Fig. Installation of the Lining Panels
Removed for Access, sheet 01 and sheet 02, view B.
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024SX-A-001-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Installation of the Lining Panels Removed for Access
Page 187
CONF ALL
(4)211LW
(7)
(6)
(7)
(7)
(7) A
B
A
C
ICN-A320-A-56XX1022-A-FAPE3-024SX-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
Figure ICN-A320-A-56XX1022-A-FAPE3-024SY-A-001-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Installation of the Lining Panels Removed for Access
Page 188
CONF ALL
(5)
(1)211MW
C
B
(2)
(2)
(3)
ICN-A320-A-56XX1022-A-FAPE3-024SY-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 189
(2) Task A320-A-56-XX-1022-09001-740A-A (A320-A-56-XX-1022-09ZZZ-740Z-A)Close-upJob Set-Up Information
Manpower/Resources/Skills
Man-hours 0.10 hMinimum Number of person 1Elapsed Time 0.10 h
Referenced Information
Manuals/Drawings References/Sheets
AMM Task 25-13-41-400-002Task 56-11-11-400-001
Procedure
NOTE: If you intend to accomplish an associated Inspection/Repair Task during thesame layover period, the subsequent Close-up procedure is not necessary.
(a) Make sure that the work areas are clean and clear of tools and other items ofequipment.
(b) Do the close-up procedure as specified in the installation of the windshields (FIN3DG1 and FIN 3DG2), refer to Ref. AMM Task 56-11-11-400-001.
NOTE: This procedure is necessary for the installation of the lining Panel211LW.
(c) Do the close-up procedure as specified in the installation of the sidewall panels,refer to Ref. AMM Task 25-13-41-400-002.
NOTE: This procedure is necessary for the installation of the lining Panel211MW.
(d) Put the aircraft back to its initial configuration.G. ADMINISTRATIVE
ProcedureConfirm in the applicable aircraft records that you have completed all the work definedin this Service Bulletin task set as required.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 190
Task set A320-A-56-XX-1022-01000-93CA-A (A320-A-56-XX-1022-01ZZZ-93CZ-A)Replacement of the Front Windshields on the Aircraft (Depending on the Inspection Result)
WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONSINCLUDED IN THE REFERENCED PROCEDURES.
WARNING: BEFORE YOU START WORK, YOU MUST PUT ON A SAFETY HARNESS ANDATTACH IT TO THE ACCESS PLATFORM. WITHOUT A SAFETY HARNESS, YOUCAN FALL. THIS CAN KILL YOU OR CAUSE YOU INJURY.
WARNING: BEFORE YOU DO THIS TASK:- MAKE SURE THAT THE AREA BELOW THE WORK AREA IS CLEAR OF
PERSONS- PUT PROTECTION ON THE PARTS BELOW THE WORK AREA IF
APPLICABLE.IF OBJECTS FALL ACCIDENTALLY, THEY CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO THE AIRCRAFT.
CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICALWIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLYSERVICEABLE). WHEN YOU DO A MAINTENANCE WORK, REPAIRS ORMODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS ANDTHE 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 ANDDAMAGE TO THE ELECTRICAL WIRING INSTALLATION.IF THERE IS CONTAMINATION, REFER TO Ref. ESPM 20-55-00.
NOTE: The accomplishment instructions of this Service Bulletin include procedures given inother documents or in other sections of the Service Bulletin. When the words “refer to”are used and the operator has a procedure accepted by the local authority he belongs to,the accepted alternative procedure can be used. When the words “in accordance with”are used then the given procedure must be followed.
NOTE: The access and close-up instructions, not comprising return to service tests, in thisService Bulletin do not constitute or affect the technical intent of the Service Bulletin.Operators can therefore, as deemed necessary, omit or add access and/or close-up stepsto add flexibility to their maintenance operations as long as the technical intent of theService Bulletin is met within the set parameters.
NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms. Referto paragraph 1.J., References, for the definition of acronyms.
NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory byan Airworthiness Directive (AD). The paragraphs 3.C. and 3.E. in these accomplishmentinstructions are Required for Compliance (RC) and must be done to comply with the AD.To allow more flexibility, the rule "refer to" and "in accordance with" will apply to theseparagraphs 3.C. and 3.E. Other paragraphs are recommended and may be deviated from,done as part of other actions or done with accepted methods different from those givenin the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can beput back into a serviceable condition.
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 191
NOTE: This Service Bulletin contains the instructions for the on-aircraft maintenance necessaryto ensure the continued airworthiness of the aircraft.For any deviations to the instructions, including Required for Compliance paragraphcontained herein, contact AIRBUS for further instructions and approval.
NOTE: Discarded parts must be managed at the operator's discretion.
A. TASK SET ASSOCIATED INFORMATIONTask Manpower
TOTAL MAN-HOURS 20.00 hELAPSED TIME (HOURS) 10.00 h
B. PREPARATION(1) Task A320-A-56-XX-1022-02001-540A-A (A320-A-56-XX-1022-02ZZZ-540Z-A)
Job Set-upJob Set-Up Information
Manpower/Resources/Skills
Man-hours 4.50 hMinimum Number of person 2Elapsed Time 2.25 h
Referenced Information
Manuals/Drawings References/Sheets
AMM Task 12-34-24-869-002Task 56-11-11-000-001
Procedure
NOTE: If you intend to accomplish this Repair during the same layover period as theassociated Inspection, the subsequent Preparation procedure is not necessary.
NOTE: For the basic Aircraft configuration, refer to AMM Chapter “Introduction -Aircraft status for maintenance" in Manual Front Matter section.
(a) Make sure that the aircraft is electrically grounded, refer to Ref. AMM Task 12-34-24-869-002.
(b) Do the job set-up procedure as specified in the removal of the windshields (FIN3DG1 and FIN 3DG2), refer to Ref. AMM Task 56-11-11-000-001.
C. PROCEDURE(1) Task A320-A-56-XX-1022-01001-520A-A (A320-A-56-XX-1022-01ZZZ-520Z-A)
Remove the Damaged Front Windshield from the Aircraft, LH sideJob Set-Up Information
Working Area
Impacted Zone Access / Work Location211
Manpower/Resources/Skills
Man-hours 2.50 hMinimum Number of person 2Elapsed Time 1.25 h
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 192
Skills Airframe
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-20-00, Page Block 001Task 56-11-11-000-001
Procedure(a) Standard Practices given in this procedure:
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.(b) Remove, refer to Ref. AMM Task 56-11-11-000-001:
FIN 3DG11 WINDSHIELD-LH STA320-1-3-1 Discard
Or
FIN 3DG11 WINDSHIELD-LH STA320-1-4-1 Discard
Or
FIN 3DG11 WINDSHIELD-LH STA320-1-5-1 Discard
Or
FIN 3DG11 WINDSHIELD-LH STA320-1-6-1 Discard
Or
FIN 3DG11 WINDSHIELD-LH STA320-1-7-1 Discard
Or
FIN 3DG11 WINDSHIELD-LH STA320-1-8-2 Discard(2) Task A320-A-56-XX-1022-02001-520A-A (A320-A-56-XX-1022-02ZZZ-520Z-A)
Remove the Damaged Front Windshield from the Aircraft, RH sideJob Set-Up Information
Working Area
Impacted Zone Access / Work Location212
Manpower/Resources/Skills
Man-hours 2.50 hMinimum Number of person 2Elapsed Time 1.25 hSkills Airframe
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 193
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-20-00, Page Block 001Task 56-11-11-000-001
Procedure(a) Standard Practices given in this procedure:
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.(b) Remove, refer to Ref. AMM Task 56-11-11-000-001:
FIN 3DG21 WINDSHIELD-RH STA320-2-3-1 Discard
Or
FIN 3DG21 WINDSHIELD-RH STA320-2-4-1 Discard
Or
FIN 3DG21 WINDSHIELD-RH STA320-2-5-1 Discard
Or
FIN 3DG21 WINDSHIELD-RH STA320-2-6-1 Discard
Or
FIN 3DG21 WINDSHIELD-RH STA320-2-7-1 Discard
Or
FIN 3DG21 WINDSHIELD-RH STA320-2-8-2 Discard(3) Task A320-A-56-XX-1022-02001-720A-A (A320-A-56-XX-1022-02ZZZ-720Z-A)
Install the Front Windshield on the Aircraft, LH sideJob Set-Up Information
Working Area
Impacted Zone Access / Work Location211
Manpower/Resources/Skills
Man-hours 2.50 hMinimum Number of person 2Elapsed Time 1.25 hSkills Airframe
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-20-00, Page Block 001Task 56-11-11-400-001
A318/A319/A320/A321SERVICE BULLETIN
REV 00 Jan 28/21 A320-56-1022Page 194
Manuals/Drawings References/SheetsIPC 56-11-01
Procedure(a) Standard Practices given in this procedure:
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.(b) Install a new LH side front windshield, refer to Ref. IPC 56-11-01 and Ref. AMM
Install the Front Windshield on the Aircraft, RH sideJob Set-Up Information
Working Area
Impacted Zone Access / Work Location212
Manpower/Resources/Skills
Man-hours 2.50 hMinimum Number of person 2Elapsed Time 1.25 hSkills Airframe
Referenced Information
Manuals/Drawings References/Sheets
AMM 06-20-00, Page Block 001Task 56-11-11-400-001
IPC 56-11-01
Procedure(a) Standard Practices given in this procedure:
1 For the identification of zones, refer to Ref. AMM 06-20-00, Page Block 001.(b) Install a new RH side front windshield, refer to Ref. IPC 56-11-01 and Ref. AMM
Task 56-11-11-400-001.D. PREPARATION FOR TEST
(1) Task A320-A-56-XX-1022-07001-540A-A (A320-A-56-XX-1022-07ZZZ-540Z-A)Job set-upJob Set-Up Information
Manpower/Resources/Skills
Man-hours 0.50 hMinimum Number of person 2Elapsed Time 0.25 h
Procedure(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.(b) Do the close-up procedure as specified in the installation of the windshields (FIN
3DG1 and FIN 3DG2), refer to Ref. AMM Task 56-11-11-400-001.(c) Put the aircraft back to its initial configuration.
G. ADMINISTRATIVE(1) Task A320-A-56-XX-1022-02001-90AA-A (A320-A-56-XX-1022-02ZZZ-90AZ-A)
Administrative
ProcedureConfirm in the applicable aircraft records that you have completed all the work definedin this Service Bulletin task set as required.
A318/A319/A320/A321SERVICE BULLETIN
APPENDIX
REV 00 Jan 28/21 A320-56-1022Page 196
APPENDIXA. ELECTRICAL TESTS RESULT CHART
Electrical Tests Result Chart
A318/A319/A320/A321SERVICE BULLETIN
APPENDIX
Figure ICN-A320-A-56XX1022-A-FAPE3-024F1-A-002-01 SHEET 1/1REV 00 Jan 28/21 A320-56-1022Electrical Tests Result Chart
Page 197
CONF ALL
10000
1000
400
10
100
0.00 0.20 0.40 0.60 0.80 1.00 1.20 1.40
R_I
NS
ULA
TIO
N (
MO
hms)
INSULATION (MOhms) Vs DIELECTRIC (mA)
DIELECTRIC (mA)
100000
ICN-A320-A-56XX1022-A-FAPE3-024F1-A-002-01
A318/A319/A320/A321SERVICE BULLETIN
APPENDIX
REV 00 Jan 28/21 A320-56-1022Page 198
B. COMPLIANCE TIMESPresentation of the Compliance Times
A318/A319/A320/A321SERVICE BULLETIN
APPENDIX
Figure ICN-A320-A-56XX1022-A-FAPE3-025Z7-A-001-01 SHEET 1/2REV 00 Jan 28/21 A320-56-1022Presentation of the Compliance Times
Page 199
CONF ALL
THRESHOLD DEFINITION:
LH SIDE PN
PN
GROUP3
RH SIDE PNTHRESHOLD
STA320-1-3-1STA320-1-4-1STA320-1-5-1STA320-1-6-1
STA320-2-3-1STA320-2-4-1STA320-2-5-1STA320-2-6-1
THRESHOLD TO PERFORMCONNECTOR VISUAL INSPECTION & ELECTRICAL TESTS
CONDITIONS ON WINDSHIELDMAINTENANCE HISTORYLH SIDE PN
PN
STA320-1-8-2
RH SIDE PN
STA320-2-8-2
THRESHOLD TO CHECKWINDSHIELD AGEUTILIZATION AND
MAINTENANCE HISTORY
GROUP2
CONDITIONS ON WINDSHIELDAGE/UTILIZATION THRESHOLD VALUE
BEFORE EXCEEDING 750 FH OR 750 FC OR4 MONTH(s) WHICHEVER OCCURS FIRST FROM
THE ORIGINAL ISSUE DATE OF THISSERVICE BULLETIN
SINCE WINDSHIELD FIRSTINSTALLATION ON A/C OR
UNKNOWN MAINTENANCE HISTORY
FAULT MESSAGE "561000 L(R)WINDSHIELD SENSOR" RECORDED
NONE
BEFORE EXCEEDING 750 FHOR 750 FC OR 4 MONTH(s)
WHICHEVER OCCURS FIRSTFROM THE ORIGINAL ISSUE
DATE OF THIS SERVICE BULLETIN
NOT RECORDED SINCEWINDSHIELD FIRST INSTALLATION
FAULT MESSAGE "561000 L(R)WINDSHIELD SENSOR"
10000 FC OR 15000 FH
WINDSHIELD AGE/UTILIZATIONHIGHER THAN 4 YEARS OR
10000 FC AND 15000 FH
WINDSHIELD AGE/UTILIZATIONLOWER THAN 4 YEARS AND
BEFORE EXCEEDING 3750 FHOR 3750 FC OR 12 MONTH(s)WHICHEVER OCCURS FIRSTFROM THE ORIGINAL ISSUE
DATE OF THIS SERVICE BULLETIN
BEFORE EXCEEDING 7500 FHOR 7500 FC OR 24 MONTH(s)WHICHEVER OCCURS FIRSTFROM THE ORIGINAL ISSUE
DATE OF THIS SERVICE BULLETIN
THRESHOLDLH SIDE PN
PN
STA320-1-7-1
GROUP1
RH SIDE PN
STA320-2-7-1
BEFORE EXCEEDING 750 FH OR 750 FC OR4 MONTH(s) WHICHEVER OCCURS FIRST FROM
THE ORIGINAL ISSUE DATE OF THISSERVICE BULLETIN
BEFORE EXCEEDING 750 FH OR 750 FC OR4 MONTH(s) WHICHEVER OCCURS FIRST FROM
THE ORIGINAL ISSUE DATE OF THISSERVICE BULLETIN
ON A/C
ICN-A320-A-56XX1022-A-FAPE3-025Z7-A-001-01
A318/A319/A320/A321SERVICE BULLETIN
APPENDIX
Figure ICN-A320-A-56XX1022-A-FAPE3-025Z8-A-001-01 SHEET 2/2REV 00 Jan 28/21 A320-56-1022Presentation of the Compliance Times
Page 200
CONF ALL
INTERVAL DEFINITION:
LH SIDE PN
PN
STA320-1-7-1
GROUP1
RH SIDE PN
STA320-2-7-1
GREENAMBER
THRESHOLD
BEFORE EXCEEDING 750 FHOR 750 FC OR 4 MONTH(s)
WHICHEVER OCCURS FIRST
ELECTRICALTESTS RESULT
RED REPETITIVE INSPECTIONNOT ALLOWED
LH SIDE PN
PN
STA320-1-8-2
GROUP2
RH SIDE PN
STA320-2-8-2
GREEN
THRESHOLD
BEFORE EXCEEDING 7500 FHOR 7500 FC OR 24 MONTH(s)
WHICHEVER OCCURS FIRST
AMBERBEFORE EXCEEDING 750 FHOR 750 FC OR 4 MONTH(s)
WHICHEVER OCCURS FIRST
RED REPETITIVE INSPECTIONNOT ALLOWED
LH SIDE PN
PN
GROUP3
RH SIDE PNINTERVAL
BEFORE EXCEEDING 750 FHOR 750 FC OR 4 MONTH(s)
WHICHEVER OCCURS FIRST
STA320-1-3-1STA320-1-4-1STA320-1-5-1STA320-1-6-1
STA320-2-3-1STA320-2-4-1STA320-2-5-1STA320-2-6-1
ELECTRICALTESTS RESULT
ICN-A320-A-56XX1022-A-FAPE3-025Z8-A-001-01
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C. GLOSSARYGlossary
ACRONYM FULL FORMCEO Current Engine OptionFC Flight CycleFH Flight HoursFL Flight LevelGSE Ground Support EquipmentLH Left HandRH Right HandVAC Voltage Alternating CurrentVDC Voltage Direct Current
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D. REPORTING SHEET
TITLE: WINDOWS - FIXED WINDOWS - INSPECTION OF SAINT-GOBAIN SULLYFRONT WINDSHIELD ON CEO AIRCRAFT
MODIFICATION No.: None
(1) SB Reporting statusThis Service Bulletin will only be incorporated into affected customized Maintenanceand Flight Operations Products if it is duly reported to Airbus.
(2) GENERAL informationThe SB Reporting policy is published in ISI 00.00.00135. This document providesinformation regarding: the SB Reporting means and benefits, the update ofcustomized Maintenance Products and customized Flight Operations Products.If this Service Bulletin has an operational impact, refer to paragraph "Flight OperationsProducts" for further information on the update of affected Flight Operations Products.
(3) SB Reporting procedureStandard practice to report SB is to use the online reporting application onAirbusWorld.Refer to ISI 00.00.00179:
- For complete information on reporting means to Airbus, Question 2 "What arethe standard practices for SB Reporting?"
- If this SB requires previous or simultaneous accomplishment of other SBs,Question 3 "What about the reporting of prerequisite Service Bulletins?"
NOTE: ISI 00.00.00179 covers all the frequently asked questions about SB Reporting.It is revised on a regular basis.
A318/A319/A320/A321SERVICE BULLETIN
APPENDIX
REV 00 Jan 28/21 A320-56-1022Page 203
E. QUALITY PERCEPTION FORMUse 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 totake corrective action to further improve the quality of our Service Bulletin.We thank you for the time you have taken in completing this form.
Quality rating of this SB 4 3 2 1Quality rating of the Accomplishment Instructions 4 3 2 1Quality rating of the Illustrations 4 3 2 1Is this SB easy to understand ? Y / N
NOTE: Please rate on a scale of 1 to 4, with 4 being the highest score
If you have difficulties in the accomplishment of this SB please quote below the area(s) andgive a short description of the issue.
Planning Material InstructionsX Applicability X Tooling X PreparationX Reason X List of Materials
Operator SuppliedX Mod/Inspection
X Manpower X Kit content X TestX References X Re-identification X Close-upX Publication X IllustrationsX Industry Support
Comments :
Operator : Date :Name/TitlePlease return this form to :AIRBUS2, ROND POINT EMILE DEWOITINE31700 BLAGNACFRANCEOr via your Resident Customer Support Office.