Major Change / Major Repair easa.europa · 10072840 MAJOR CHANGE AIRBUS CANADA LIMITED PARTNERSHIP...

easa.europa.euMajor Change / Major RepairEASA Certificate

Number Application Nature Certificate HolderRev.level Models Description Certification basis

Associated TechnicalDocumentation Limitations/Conditions

Date ofIssue Status

10072332 MAJOR CHANGE 328 SUPPORTSERVICES GmbH

DORNIER 328-100 Update of AFM/AOM Normal Procedure(APU).Update of AFM Normal Procedures toprevent possible overload of 1 VEDCDistribution.

The Certification Basis (CB) for theoriginal product remains applicabletothis certificate/ approval.Therequirements for environmentalprotection and theassociatedcertified noise and/ oremissions levels of the product areunchangedand remain applicable tothis certificate/approval without anyim...

-CP-100483 Update of AFM/AOM Normal Procedure, IssueA, dated 12.07.2019-MDL100483 MasterDocument List, Issue A,dated14.01.2020-CS-100483Update of AFM/AOM NormalProcedure, Issue A, dated12.07.2019-328-100 AirplaneFlight Manual – Supplement001, Temporary Revision No.19-003, dated Jul 31/19 (E...

None 31/01/2020 Active


REV. 1 DORNIER 328-100 Localizer Performance with Vertical Guidance(LPV)Introduction of LPV approaches toperform RNAV (GNSS) approachesdowntothe LPV minimum decision altitude/height (MDA/H).


-CP-100440 LocalizerPerformance with VerticalGuidance (LPV), Issue C,dated13.12.2019-MDL 100440Master Document List, IssueB, dated 13.02.2020-CS-100440 LocalizerPerformance with VerticalGuidance (LPV), Issue A,dated17.12.2019-328-100 AirplaneFlight Manual, Doc. No. AM-AFM-050893-ENV: − AF...

Prior to installation of this change/repair it must be determinedthatthe interrelationship betweenthis change/repair and anyotherpreviously installed changeand/ or repair willintroduce noadverseeffect upon theairworthiness of the product.

20/02/2020 Active


DORNIER 328-300 DORNIER 328-100

AFM Change - Abnormal Procedures Avionics(FMS) – MSGThe amber PFD annunciation“MSG” is not yet covered in the AFM.Anabnormal procedure has to be added inorder to provide a procedure forall “caution”-level flight deck indications. The purpose ofthe amber“MSG” annunciation is to alert thepilotsh...


- CP-100430 AFM Change -Abnormal ProceduresAvionics (FMS)– MSG, IssueA,dated 09.08.2018-MDL100430 MasterDocument List, Issue A, dated09.12.2019- CS-100430 AFMChange - AbnormalProcedures Avionics (FMS) –MSG, IssueA, dated06.08.2017- 328-100 AirplaneFlight Manual – AbnormalProcedures, Tem...




Re-Design Bolt for Spring Tab LeverTo reducethe possibility of play in the Spring Tab Lever,the bolt wasre-designed with increaseddiameter.The new Spring Tab LeverAssemblies P/N 001A272A4020006(Do328-100) andP/N 001D272A4020002(Do328-300) are alternatives for the existingSpringTab Levers P/NT...


- CP-100519 Re-Design Boltfor Spring Tab Lever, Issue B,dated13.05.2020-MDL100519 MasterDocument List, Issue A, dated22.06.2020- CS-100519 Re-Design Bolt for Spring TabLever, Issue A,dated10.06.2020or laterrevisions of the above listeddocument(s) approved/acceptedunder the EASAsystem.



DORNIER 328-100 AFM Change - ECS flow mode controlStand-alone AFM change and MMEL change as animprovement to enable theflight crew toidentify the ECS Bleed Air system failurebyincorporation ofan additional ECS FLOWCONTROL TEST before the firstflight of theday and, in case of failure, to provide arectificatio...


- CP-100477 AFM Change –ECS flow mode control, IssueD, dated14.02.2020-MDL100477 MasterDocument List, Issue A, dated15.06.2020- CS-100477 AFMChange – ECS flow modecontrol, Issue A,dated28.05.2020- 328-100Airplane Flight Manual −Appendix 006 Doc. No.AM-AFM-050893-ENV: Issue Feb15/20- 328-1...


10/07/2020 Active

Page 1 of 242This report lists certificates issued during the period 01/01/2020 until 25/05/2021. In case you need a certificate not included, please contact [email protected].

An agency of the European Union




Date ofIssue Status


REV. 1 DORNIER 328-100 DU-875AF SW 2.03Introduction of SoftwareVersion 2.03 (P/N K9321062A02) for theDU-875AFdisplay units which have previouslybeen certified in Option 316K002(Primus EliteAdvanced Features, PEAF) and 316K001(DU-875 EnhancedFunctions) with softwareversion 2.02 (P/N K9321062A01). Thenewsoftware is i...


- CP-100530 CertificationProgram, DU-875AF SW 2.03,Issue A, dated13.03.2020-CS-100530 ComplianceStatement, DU-875AFSW2.03, Issue A,dated27.07.2020 (amended03.09.2020)- MDL100530Master Document List,DU-875AF SW 2.03, Issue A,dated29.07.2020- Dornier328−100 Airplane FlightManual Doc. No.o...




Incorporation of risk reduction measures forPED stowage onthe flightdeck.Installation ofplacards "NO PED STOWAGE" inthe cockpit atthe LH andRH FWD sideconsole stowages,provision of fire-resistant glovesincludingcorresponding placard"FIREGLOVES" and amendment of the AFMSMOKEemergency proced...


- CP-100480 CertificationProgram, Incorporation of riskreductionmeasures for PEDstowage on the flight deck<(>, Issue B,dated07.10.2019- CS-100480Compliance Statement,Incorporation of riskreductionmeasures for PEDstowage onthe flight deck,Issue A, dated 11.09.2019-MDL 100480 Maste...


10075605 MAJOR CHANGE AEROCLUBULROMANIEI

IS-29D2 IS-29D

Cancellation of lifetime limitation defined bycalendar time.Introduction of thorough andfrequent inspections.


Aircraft Flight Manual andMaintenance Manual changein accordance withAeroclubulRomaniei Master DocumentList 01.MDL.001, at revision1,dated April 19, 2018.or laterrevisions of the above listeddocument(s) approved/acceptedunder the EASAsystem.


09/02/2021 Active


IS-32A Removal of lifetime limitation in terms ofcalendar years and adjustmentof TBO.


Removal of the lifetimelimitation in terms of calendaryears andadjustment of TBOin accordance with AeroclubulRomaniei MasterDocumentList, AR.IS-32A.00102.MDL.001, revision 01,dated May 8, 2019;AircraftFlight and MaintenanceManual,IS-32A, at revision 18(1st AIssue May 2019);or laterrevisi...



IS-30 Removal of lifetime limitation in terms ofcalendar years and adjustmentof TBO


Removal of lifetime limitationin terms of calendar years andadjustmentof TBO inaccordance with AeroclubulRomaniei Master DocumentListAR.IS-30.001 02.MDL.001,initial revision, dated August18, 2020;MaintenanceManual, IS-30, at revison 9(2nd A Issue: August 2020);orlater revisions of the abov...







Date ofIssue Status

10075864 MAJOR CHANGE AEROPHILE S.A.S. AEROPHILE 5500 Installation of an updated LED banner modelfor Aerophile 5500.

The Certification Basis for the originalproduct as amendedby thefollowingadditional or alternativeairworthiness requirements:thefollowing paragraph(s) at a lateramendment: CS31TGB initial issue,1st of July 2013

Constitution de Dossier deDéfinition AERO5500PNF01REV.15 Etabli le 18Février2021Maintenance Manual forAEROPHILE 5500 – Edition 12– March 2021Flight Manualfor AEROPHILE 5500 – Edition15 – March 2021or laterrevisions of the above listeddocument(s) approved/acceptedunder the EASAsystem.


16/03/2021 Active

10075449 MAJOR CHANGE AEROSPOOL, SPOL.S.R.O.

CLUB Garmin GTX 335 XPDR with ADS-B Out.DYNON SkyView firmware v.15.4.7.

The Certification Basis for the originalproduct as amendedby thefollowingadditional or alternativeairworthiness requirements:- CS-ACNS, issue 2.The requirements forenvironmental protection and theassociatedcertified noise and/ oremissions levels of the product areunchangedand remain applicab...

- Master Document List,document number AS-RTC-20-004.A1, revision2,dated 14 January 2021.- Tobe installed according toService Bulletin, documentnumberSBRTC-2019-3,revision 0and ServiceBulleting, documentnumberSBRTC-2019-04,revision 0.- To be operatedaccording to Pilot’s OperatingHandbook...


22/01/2021 Active

10072462 MAJOR CHANGE AIRBUS CANADALIMITEDPARTNERSHIP

BD-500-1A11 Introduction of OWEED Dual Lane Slides onCS300.This designchange introduces two off-wing dual lane slides, one on eachside of theaircraft, as assisting evacuation meansassociated to theType III over the wingemergency exit doors (OWEED), instead ofthepreviously available single lane slides.


This airworthiness approvalcovers the following set ofModSums toachieve the finalconfiguration, as per DesignChangeCertificationPlanDCCP-500T800030 IssueG:-MS 500T100692 (for newon-production aircraft) OR MS500T101746 (for inserviceaircraft, through retrofit): thepurpose of this ModSums t...

This design change approval isvalid for BD-500-1A11 (A220-300)aircraft.Prior to installation of thischange/repair it must bedetermined thattheinterrelationship between thischange/repair and anyotherpreviously installed changeand/ orrepair will introduce noadverseeffect upon theairworthines...

07/02/2020 Active


BD-500-1A11 (A220-300) Standalone Airplane Flight Manual (AFM)Revision SubmissionRS-070: “Addstructuralweights, center of gravity limits and noisedata”.This AFM RS-070 introduces twoaircraft OptionCodes to beappliedconcurrently for an operating weightoption: Option Code 13001160C whichlimitsthe Maximum Take-off W...

The Certification Basis (CB) for theoriginal product remains applicabletothis certificate/ approval.Therequirements for environmentalprotection are unchanged butthiscertificate/ approval involves achange with an impact on thenoisedatabase and/or emissionlevels.

Standalone Airplane FlightManual (AFM) RevisionSubmissionRS-070:“Addstructural weights,center of gravity limits andnoise data”,or laterrevisions of the above listeddocument(s) approved/accepted onbehalf of EASA inaccordance with the TechnicalImplementationProcedures ofEU/ Canada Bil...

This AFM RS-070 EASAairworthiness approval coverssimultaneousimplementation onaircraft of the two option codes13001160C AND13001250C, forBD-500-1A11 (A220-300) aircraftequipped withPW1524G-3engines.Prior toinstallation of this change/repair itmust be determined thattheinterrelationship bet...

18/03/2020 Active


BD-500-1A11 (A220-300) BD-500-1A10 (A220-100)

Modification of Iridium SATCOM SystemInstallation to activate voicecapability.Thisdesign change introduces the AFIRS 228SIridium SATCOM system asreplacementinstallation to theexisting IRT-2110 IridiumSATCOM systeminstallation, in order tointroduce the SATCOM voicecommunicationcapability.


- ModSum 500T800522:Introduction of AFIRS-228SSATCOM installationoption,and- Design ChangeCertification PlanDCCP-500T800522, Issue D,dated2020-01-31, and-Airplane Flight Manual (AFM)Revision Submission RS-063:Add newAFIRSTM IridiumSATCOM System Capability,dated 03rd June 2019,whichupdate...

See those of AFM RS-063. 06/04/2020 Active






Date ofIssue Status


BD-500-1A11 (A220-300) BD-500-1A10 (A220-100)

Operational Suitability Data (OSD) Flight CrewA220 (BD-500) ReportRevision 6, dated 01stApril 2020


Airbus Canada LimitedPartnership OSD FC A220(BD-500) Report Revision6,document Ref. OSD - FlightCrew - A220_01 Apr2020_Rev 6, dated 01stApril2020,or later revisionsofthe above listed document(s) approved/acceptedonbehalf of EASA inaccordance with the TechnicalImplementationProcedure...

See those of OSD FC A220(BD-500) Report Revision 6.

20/04/2020 Active


BD-500-1A11 (A220-300) BD-500-1A10 (A220-100)

EASA Master Minimum Equipment List(MMEL) Issue 13 for aircraftmodelsBD-500-1A10 and BD-500-1A11


BD500-3AB48-12701-00 IssueNo. 13: EASA MMEL Issue 13for aircraftmodelsBD-500-1A10 andBD-500-1A11,or laterrevisions of the above listeddocument(s) approved/accepted onbehalf of EASA inaccordance with the TechnicalImplementationProcedures ofEU/ Canada BilateralAgreement

See those of EASA MMEL Issue 13. 28/04/2020 Active


BD-500-1A11 (A220-300) Standalone Airplane Flight Manual (AFM)Revision SubmissionRS-084: “Addstructuralweights, center of gravity limits and noisedata”.This AFM RS-084 introduces twoaircraft OptionCodes to beappliedconcurrently for an operating weightoption: Option Code 13001190C whichlimitsthe Maximum Ramp Weigh...


Standalone Airplane FlightManual (AFM) RevisionSubmissionRS-084:“Addstructural weights,center of gravity limits andnoise data”,or laterrevisions of the above listeddocument(s) approved/accepted onbehalf of EASA inaccordance with the TechnicalImplementationProcedures ofEU/ Canada Bil...

This AFM RS-084 EASAairworthiness approval coverssimultaneousimplementation onaircraft of the two option codes13001190C AND13001270C, forBD-500-1A11 (A220-300) aircraftequipped withPW1521G-3engines.Prior toinstallation of this change/repair itmust be determined thattheinterrelationship bet...

26/05/2020 Active


BD-500-1A11 BD-500-1A10

Standalone Airplane Flight Manual (AFM)Revision SubmissionRS-069:“Update theAuxiliary Power Unit (APU) bleed airlimitations andfigures”.


Standalone Airplane FlightManual (AFM) RevisionSubmissionRS-069:“Updatethe Auxiliary Power Unit(APU) bleed air limitationsandfigures”or later revisionsof the above listed document(s) approved/acceptedonbehalf of EASA inaccordance with the TechnicalImplementationProcedures ofEU/ Canada Bil...

See those of AFM RS-069 26/05/2020 Active


BD-500-1A11 (A220-300) BD-500-1A10 (A220-100)

Standalone Airplane Flight Manual (AFM)Revision SubmissionRS-087:“Various updatesto non-normal procedures andsupplements”.AFM Sections and contentupdated by this RS-087:Chapter 4 – Non-Normal procedures: - Slat-Flap Fail caution(only for BD-500-1A11 AFM). - Display unitfailure procedu...


Standalone Airplane FlightManual (AFM) RevisionSubmissionRS-087:“Variousupdates to non-normalprocedures andsupplements”,or laterrevisions of the above listeddocument(s) approved/accepted onbehalf of EASA inaccordance with the TechnicalImplementationProcedures ofEU/ Canada Bilateral...







Date ofIssue Status


BD-500-1A10 (A220-100) Steep Approach Landing Option -Temperature Envelope Expansion.The scopeof this major design change is to expand theOutside AirTemperature envelope specific tosteep approach operations. Nophysicalaircraft change is associated.The AFMcontent is updated to increase the steepapproach temperaturel...


-Design change ModSum500T800000 for newproduction aircraft OrModSum500T101040 for In-service aircraft, and-DesignChange Certification PlanDCCP-STEEP APPR EXP, IssueB, dated2020-05-20, and-Airplane Flight Manual (AFM)Revision Submission RS-070:Add expandedenvelope forhigher temperature, date...

Design change applicable toBD-500-1A10 (A220-100) aircraft.Seelimitations and conditions asper AFM RS-070.

24/06/2020 Active


BD-500-1A11 (A220-300) BD-500-1A10 (A220-100)

Standalone Airplane Flight Manual (AFM)Revision SubmissionRS-052:“Various updatesto limitations, procedures andsupplements”.AFM Sections and contentupdated by this RS-052:Front matter: .Option list.Chapter 2 – Limitations: . FlightManagement System (FMS). . Takeoff andlanding awa...


Standalone Airplane FlightManual (AFM) RevisionSubmissionRS-052:“Variousupdates to limitations,procedures andsupplements”,or laterrevisions of the above listeddocument(s) approved/accepted onbehalf of EASA inaccordance with the TechnicalImplementationProcedures ofEU/ Canada Bilatera...



BD-500-1A11 (A220-300) BD-500-1A10 (A220-100)

Update of the Operational Suitability Data(OSD) cabin crewdata (CCD)constituentcomponent.This OSD CCD design changecovers the cabin crew differencetrainingassociated with: A) The aft duallavatory door lock and unlock systemoperation and B) The cabin attendant seat(close to the dual a...


“A220-AFT Dual Lavatory doorlock/unlock system, AFT CabinCrew Seat”cabin crew datachange dossier, DocumentReferenceACLP-OSD-CC-0001-20Issue 1.0,orlater revisions of the abovelisted document(s) approved/acceptedunder the EASAsystem.

From the cabin crew training andoperation point of view,aeroplanessubject to the ModSum500T800530 are considered to be“the same variant”as theBombardier CSeriesBD-500-1A10/1A11 (CS100/-300).Cabin crewoperating onaeroplanes modifiedper thisModSum 500T800530mustcomplete minimal differencet...

30/06/2020 Active


BD-500-1A11 (A220-300) BD-500-1A10 (A220-100)

Introduction of Auxiliary Power Unit (APU)Electronic Control Unit (ECU)Software11.0.This design change introduces anupdated APU ECU Software versionV11.0through the Modsum 500T102863which incorporates severalfunctionalchanges.


- Design change ModSum500T102863, and- DesignChange Certification PlanDCCP-500T102863 Issue A,dated2020-01-30.or laterrevisions of the above listeddocument(s) approved/accepted onbehalf of EASA inaccordance with the TechnicalImplementationProcedures ofEU/ Canada BilateralAgreement.



BD-500-1A11 BD-500-1A10

Major Design Change FBW PC1 PFCC & REUSoftware Configuration Update.This buildchange in the Fly-by Wire (FBW) FlightControl System PC-1constitutes in a jointintroduction of Primary Flight ControlComputer(PFCC) and Remote Electronics Unit(REU) software configuration throughtheModsum 500T100581...


-Design change ModSum500T100581, and-DesignChange Certification PlanDCCP-500T100581 Issue C,and-Standalone AirplaneFlightManual (AFM) RevisionSubmission RS-046which isupdating AFM’sBD500-3AB48-22200-00 andBD500-3AB48-32200-00,applicable to aircraft modelsBD-500-1A10 andBD-500-1A11 respec...

See those of AFM RS-046. Inaddition, some periodic groundandfunctional checks have beenadded or modified, as per reportnumberRBR-BA500-167 RevisionAD

17/07/2020 Active






Date ofIssue Status


BD-500-1A11 (A220-300) BD-500-1A10 (A220-100)

Standalone Airplane Flight Manual (AFM)Revision SubmissionRS-083:“Update toSupplement 21 – Operation above 29000feet”.


AFM Revision SubmissionRS-083: “Update toSupplement 21 –Operationabove 29000feet”.or later revisions of theabove listed document(s)approved/accepted onbehalfof EASA in accordance withthe TechnicalImplementationProcedures ofEU/ Canada BilateralAgreement.



BD-500-1A11 (A220-300) BD-500-1A11 BD-500-1A10 (A220-100) BD-500-1A10

Major design change: Avionics SoftwareUpdate - Version 5.6.This Flight ManagementSystem (FMS) software update to Version 5.6(Build 8.0A2) incorporates several systemupgrades, among them:· Introduction ofpersistent FMS reset fault logging capability.·Revised logic for the Surface ManagementSyst...


· ModSum 500T102257 forthe forward fit of newproduction aircraft and·ModSum 500T102258 for theretrofit of In Service aircraft,and· Design ChangeCertification PlanDCCP-500T102257, Issue F,dated2020-07-15.or laterrevisions of the above listeddocument(s) approved/accepted onbehalf of EASAinP...

This EASA airworthiness approvaldoes not cover any operationalcreditor benefit from the physicalincorporation on aircraft of FMSv5.6software standard. Theincorporation of operational creditand benefitsof FMS v5.6 will besupported bythe AFM RS-062which will require itsown separateEASA airwo...

02/09/2020 Active


BD-500-1A11 (A220-300) BD-500-1A10 (A220-100)

High Altitude Airport Operations EnvelopeExpansion.The scope of this major designchange is to increase the maximumaltitudeairport operating limitation of aeroplanesModels BD-500-1A10and BD-500-1A11 fromcurrent airport altitude of 8,000 ft to 10, 000ft.In addition, this EASA major designchange...


Design Change CertificationPlan DCCP-HAAO-10000 FTIssue C, dated2020-04-10,andAirplane Flight Manual(AFM) Revision SubmissionRS-062: “Variousupdates toinclude Avionics 5.6 (Build8.0A2) and to expand thetakeoffand landingenvelope”or later revisions ofthe above listed document(s)approved/ac...

See those of AFM RS-062, which isproviding the airworthinessapprovalfor the operational creditand benefits from Avionics 5.6(Build 8.0A2)standard for the FMS,which is approved under theseparate EASAcertificate10074162 and that needsto beincorporated previouslyorsimultaneously in the aircra...

10/09/2020 Active


BD-500-1A11 (A220-300) BD-500-1A10 (A220-100)

Standalone Airplane Flight Manual (AFM)Revision SubmissionRS-061 - AddnewSupplement 11: Approach capability, glidepath angle from 3.5 to 4.1degrees.Thisairworthiness approvalcovers a standaloneAFM change to introducesteeperapproachangles up to 4.1 degrees. Theincrease in approachangles doe...


Standalone Airplane FlightManual (AFM) RevisionSubmissionRS-061: AddnewSupplement 11 Approachcapability, glidepathanglefrom 3.5 to 4.1degrees,or later revisions of theabove listed document(s)approved/accepted onbehalfof EASA in accordance withthe TechnicalImplementationProcedureso...



BD-500-1A11 (A220-300) BD-500-1A10 (A220-100)

Integrated Air System Controller (IASC)Software Update to V6.0The IASC Softwareversion 6.0, which is implemented throughModsums500T103085 (forward fit for newproduction aircraft) and 500T103157(offeredas retrofit for in-service aircraft), addressesmultiplechanges to resolve Problem Reports(PR...


- Design Change ModSum500T103085 for the forwardfit for new productionaircraft,and- ModSum 500T103157,offered as retrofit for in-service aircraft, and- DesignChange Certification PlanDCCP-500T103085 Issue C,dated2020-09-14.or laterrevisions of the above listeddocument(s) approved/accepted o...







Date ofIssue Status


BD-500-1A11 (A220-300) BD-500-1A10 (A220-100)

Introduction of Full Authority DigitalElectronic Control (FADEC)software version2.11.10This engine FADEC software versionSW 2.11.10 incorporates the followingdesignchanges: - Modification of engine N1 redlineto 95.2%N1 above 29000feetaltitude, and -Introduction of an automatic speed r...


- Design change ModSum500T103353, and- DesignChange Certification PlanDCCP-500T103353, Issue C,dated2020-06-05, and-Airplane Flight Manual (AFM)Revision Submission RS-085:ReviseSupplement 21 toinclude FADEC v2.11.10update.or laterrevisions of theabove listed document(s)approved/acceptedb...

See those of AFM RS-085.Prior toinstallation of this change/repair itmust be determined thattheinterrelationship between thischange/repair and anyotherpreviously installed changeand/ or repair will introduce noadverseeffect upontheairworthiness of the product.

07/10/2020 Active


BD-500-1A11 (A220-300) BD-500-1A10 (A220-100)

Fuel Quantity Computer (FQC) softwareversion SW 4.0.The scope of this majordesign change is:1),,To modify the thresholdfor FUEL IMBALANCE caution message from800to 1000 lbs, and2),,Change of FUEL MANXFR FAIL monitor threshold, and3),,Change ofthe refuelling SOV pre-check monitorthreshold.In a...


-Design Change CertificationPlan DCCP-500T102943 IssueE, and-Airplane Flight Manual(AFM) Revision SubmissionRS-088:“Update fortheinstallation of new FuelQuantity Computer (FQC)software 4.0”.or laterrevisions of the above listeddocument(s) approved/accepted onbehalf of EASA inaccordance wi...

See those of associated AFMRS-088Prior to installation of thischange/repair it must bedetermined thattheinterrelationship between thischange/repair and anyotherpreviously installed changeand/ or repair will introduce noadverseeffect upon theairworthiness of the product.

27/11/2020 Active


BD-500-1A11 (A220-300) Wireless In-Flight Entertainment (PanasoniceXW) CS300 ModSum500T812666_ATheeXW system enables passengers to access abrowser-based portalwirelessly through theirown Wi-Fi equipped laptop, tablet, smart-phone,or other portable electronicdevice.TheeXW architecture is comprised of thefollowing co...


-Design Change ModSum500T812666_A “Wireless In-Flight Entertainment(Panasonic eXW) CS300”, and-Design Change CertificationPlan DCCP-500T812666 IssueA, and-“A220-In-FlightEntertainment andConnectivity – Optional IFEC-ISPSSMaster Switch” cabincrew data change dossier,Document ReferenceACLP-OSD-...

This EASA Airworthiness Approvalalso covers the update of theEASAOperational Suitability Data(OSD) Cabin Crew Data (CCD)constituentcomponent associatedto the design change ModSum500T812666_A.Aeroplanesmodified per this ModSum500T812666_A (i.e. with WirelessIFEWith Switch) are consideredtoA...

20/01/2021 Active


BD-500-1A11 (A220-300) BD-500-1A10 (A220-100)

Update of the Operational Suitability Data(OSD) cabin crewdata (CCD)constituentcomponent.The scope of this OSD CCD designchange is to add a procedure stepduringdeployment of the cabin attendant seatinstalled together withthe optionalaft duallavatory in the cabin crew differencetrainingconte...


“A220 CCD – Additional stepin the operation of the AFTCabin Crew Seatassociatedwith Optional Dual lavatory”cabin crew data changedossier,Document ReferenceACLP-OSD-CC-0002-20 Issue1.0,or later revisions ofthe above listed document(s)approved/acceptedunder theEASA system.

Aeroplanes modified per thisModSum 500T800530 (i.e. withswivel AFTCAS at optional duallavatory) are considered to be “the same variant”as theBD-500-1A10/-1A11(A220-100/-300) baselineconfiguration (i.e.with regular AFTCAS). Cabin crew operatingaeroplanes modified perthisModSum must complet...

21/01/2021 Active


BD-500-1A11 (A220-300) BD-500-1A10 (A220-100)

Update of the Operational Suitability Data(OSD) cabin crewdata (CCD)constituentcomponent.The scope of this OSD CCD designchange consists in the addition of theoptionalSafety Pin to secure the door arming lever inthe disarmedposition.These CCD changes arecategorized design-related and therefo...


“A220 CCD – Installation of anoptional Safety Pin”” cabincrew datachange dossier,Document Reference ACLP-OSD-CC-0001-20 Issue 1.0.orlater revisions of the abovelisted document(s) approved/acceptedunder the EASAsystem.

Aeroplanes modified per ModSum500T811080 – FWD Doors &ModSum500T811081 – AFT Doors(i.e. with Door Slide Arming SafetyPin) areconsidered to be “ thesame variant” as the BD-100-1A10and -1A11(A220-100/-300)baseline configurations(i.e.without Door SlideArmingSafety Pin). Cabin crewmembers ope...

26/01/2021 Active






Date ofIssue Status


BD-500-1A11 (A220-300) BD-500-1A10 (A220-100)

Type design approval for Extended RangeOperation with Two EnginesAeroplanes(ETOPS).This EASA ETOPS airworthinessapproval covers maximum approveddiversiontimes up to 120 minutes and up to180 minutes.

The Certification Basis for the originalproduct as amendedby thefollowingadditional or alternativeairworthiness requirements:- Thefollowing paragraph(s) at a lateramendment:CS 25.1535atAmendment level 12, plus EASAAMC 20-6 rev. 2 “Extended RangeOperationwith Two-EngineAeroplanes ETOPS Cer...

Airbus Canada LimitedPartnership documents: -ETOPS Configuration,Maintenance and Procedures(CMP) documentreferenceBD500-3AB48-11200-00Issue 7, and - Airplane FlightManual (AFM) RevisionSubmission RS-097:updatethe AFMSupplement19 ETOPS to include theEASA type design ai...

This EASA initial ETOPS designairworthiness approval isapplicable tothe followingcombinations of aircraft models/powerplant installationandrequires the minimum aircraftconfiguration as defined in CMPETOPSBD500-3AB48-11200-00Issue 7:-) BD-500-1A10 aircraftfitted with two PW1524G engines,And-...

04/03/2021 Active


BD-500-1A11 (A220-300) BD-500-1A11 (Option) A220-300 MaximumTake-Off Weight (MTOW) Increase.The scopeof this design change to the BD-500-1A11(A220-300) airplanemodel is to increase theMaximum Take Off Weight (MTOW) by 7300lbs(with regards the previous approved valueof 149000 lbs,up to 156300 lbs) in order tooffer a...


- Design change ModSumMS-500T103123, and- DesignChange Certification PlanDCCP-500T103123 Rev D/D1/D2/D3, and- Airplane FlightManual (AFM) RevisionSubmission RS-068:IncreaseMaximum TakeoffWeight (MTOW) limitations,and- AirworthinessLimitationsdocument referenceBD500-3AB48-11400-02Issue012...

See those of associated AFMRS-068 and AWL documentreferenceBD500-3AB48-11400-02Issue 012.01, latest approvedrevisions.This MTOW/MRWincrease design change isapplicable to BD-500-1A11aircraftmodel. Revised performance,Vspeeds and weight &balancedatabases for the flightmanagement system are a...

11/03/2021 Active

10072544 MAJOR CHANGE AIRBUS DEFENCEAND SPACE S.A.

C-295 DC10943-E C-295 New Fire ExtinguishersThisDesign Change isissued in order to complywith the Europeanregulation regarding theuse of Halon. The purpose of this change istoremove the old hand-held portable fireextinguishers and to install thenew HalonFree hand-held portable fire extinguishers.T...

The Certification Basis for the originalproduct as amendedby thefollowingadditional or alternativeairworthiness requirements:thefollowing paragraph(s) at a lateramendment: CS 25.561 Amdt. 15,CS25.851 Amdt. 15, CS 25.1301Amdt. 15, 25.1309 Amdt. 15, FAR25.851 (a6)Amdt. 142, FAR 25.1301(a4) A...

-C-295 Fire ExtinguishersCertification Plan (EASAProject 10054862).Ref. TEA-5-DT-180401, Issue E, dated 5thFebruary 2020.-LIST OFMAJOR DESING CHANGESAND MODIFICATIONS TO BECONSIDERED INTHECERTIFICATION PLANTEA-5-DT-180401, IssueA,dated 5th February 2020orlater revisions of the aboveliste...


14/02/2020 Active


REV. 1 C-295 DC11090-E HLCU (High Lift Control Unit)ThisDesign Change implements a modificationperformed in the flapssystem. Current FECU(Flap Electronic Control Unit) and FVU(FlapValidation Unit) are replaced by HLCU(High Lift Control Unit). HLCUwill performcontrol and monitor functions of both FECUand F...

The Certification Basis for the originalproduct as amendedby thefollowingadditional or alternativeairworthiness requirements:thefollowing paragraph(s) at a lateramendment: CS 25.699 Amdt. 15,CS25.703 Amdt. 15, CS 25.1317Amdt. 17.The requirements forenvironmental protection and theassociate...

- C-295FW HLCUINSTALLATION CertificationPlan (EASA Project10054865).Ref. TEA-5-DT-180382, Issue E, dated26th February 2020.- LIST OFMAJOR DESING CHANGESAND MODIFICATIONS TOBECONSIDERED INTHECERTIFICATION PLANTEA-5-DT-180382. Ref. TEA-5-NT-200258, Issue A,dated27th February 2020.orlateru...


27/04/2020 Active


C-295 DC10965A C-295FW ALS RUDDER BOOSTThisDesign Change is issued to include on theALS, the development ofthe RudderBoostSystem (RBS) Test Procedure. Specificoperations thatshall be performed with theRudder Boost System areincluded.Additionally, structural inspectionsof VTP/HTP joints to fuselage...


-DC10965A C-295FW ALSRUDDER BOOST & VTP/HTPJOINTS TOFUSELAGELIMITATIONSUPDATE Certification Plan(EASA Project 10063748).Ref.TEA-5-DT-190534, Issue C,dated 27th February 2020.-C-295 FW VersionAirworthiness Limitations.Ref. TAE-5-DT-170120, IssueD,dated 23rd January 2020.-C-295 TS-03 ICA Com...

In accordance with the limitationsand instructions as defined intheabove listed AirworthinessLimitations certificationdocuments.Prior to installation ofthis change/repair it must bedetermined thattheinterrelationship between thischange/repair and anyotherpreviously installed changeand/ ore...

10/03/2020 Active






Date ofIssue Status


C-295 DC10998-E C-295 New ControlWheelReplacement of the former controlwheel by a new one which implementssamefunctionalities, while maintaining mechanicalinterfaces, and hasalso spare provisions foradditional functions to be implemented.ThisDesign Change DC10998-E is issued toreplace in the C-295f...

The Certification Basis for the originalproduct as amendedby thefollowingadditional or alternativeairworthiness requirements:thefollowing paragraph(s) at a lateramendment: CS 25 Amdt.15,paragraphs 25.1329, 25.1705,25.1301, 25.1459,25.1707,25.1715,25.1701, 25.1703, 25.1711,25.1713, 25.1717...

- C-295FW NEW CONTROLWHEEL Certification Plan(EASA Project 10054892).Ref.TEA-5-DT-180384, Issue C,dated 5th March 2020.-C-295FW, DC10998-E.Displays and Controls SystemAC 20-141BComplianceDocument. Ref.TEA-5-NT-200190, Issue A,dated 7th February 2020.-LIST OF MAJOT DESINGCHANGES AND MODIF...


10/03/2020 Active


C-295 C-295 Serial ModificationsThis modificationincludes several Serial Modificationsimplemented inthe C-295 aircraft: fuselagestructural changes for a new assemblyline;structural improvements on thehorizontal tail, elevator and centralbox;landing gear improvements; changes inelectrical, fire prot...

The Certification Basis for the originalproduct as amendedby thefollowingadditional or alternativeairworthiness requirements:Thefollowing paragraph(s) at a lateramendment: CS 25.899 at Amdt15for LDE. CS 25.1317 at Amdt 17 forHIRF. C-295 Step 2 CertificationBasis(CRI A-10 “EASA Certification...

- C-295. Serial ModificationsCertification Plan (EASAProject10054890), Ref. TEA-5-DT-180400, Issue F, dated30th April 2020.- List of MajorDesign Changes andModifications to beConsidered in theCertificationPlan TEA-5-DT-180400,IssueA, dated 8th May 2020.-C-295 FW VersionAirworthiness Limit...

In accordance with the limitationand instructions as defined intheabove listed approvedAirworthiness Limitationscertification documents.Prior toinstallation of this change/repair itmust be determined thattheinterrelationship betweenthischange/repair and anyotherpreviously installedchangee...

12/05/2020 Active


C-212-EE C-212-DF C-212-DD

DC30051S-E (C212C) NLG WHEELAUTOCENTERIThe Design Change is issued toinstall an auto centering system fornoselandinggear wheel.


Temporary Revision No. 22Issue 1 to C-212-DD DGAC-ApprovedAFMDT87-2501TemporaryRevision No. 22 Issue 1 toC-212-DF DGAC-ApprovedAFM DT88-2509TemporaryRevision No. 22 Issue 1toC-212-EE DGAC-ApprovedAFM DT97-2001or laterrevisions of the above listeddocument(s) approved/acceptedunder the EAS...



C-295 DC11416S-E ELT UPDATENew ELT compliantwith CRI F-25 related to Non RechargeableLithiumBatteries. The transmitter, antennaand control panel are replaced; theG-Switchmodule and portable antenna will beremoved and a buzzer isinstalled.

The Certification Basis for the originalproduct as amendedby thefollowingadditional or alternativeairworthiness requirements:SpecialCondition(s): SC F-25: (1), (2), (3), (4),(5), (6) (Safety,Display & Controls,Communications, Surveillance).thefollowing paragraph(s) at a lateramendment: CS 2...

-LIST OF MAJOR DESINGCHANGES ANDMODIFICATIONS TO BECONSIDERED INTHECERTIFICATION PLANTEA-5-DT-200176. Ref. TEA-5-NT-200432, Issue A, dated24November 2020.-C-295FWEASA-Approved AirplaneFlight Manual TAE-5-DT-160180 BasicRevision No.3, Issue D, dated 13November 2020.-C-295FWVersion Airworth...

To be installed in production only,from S/N 188 onwards, noretrofitallowed.Prior to installationof this change/repair it must bedetermined thattheinterrelationship between thischange/repair and anyotherpreviously installed changeand/ or repair will introduce noadverseeffect upon the airwort...

30/11/2020 Active


REV. 1 C-295 C-295 Avionics Version TS-03.02This DesignChange certifiesthe AHRS and FDU/ECUEquipment Installation(DC10973-E),theSecond Transponder Installation(DC10974-E), AFD 3710HW Update - GE4Improvement to solve HW reset(DC11678-E)and AFM update to include CTNF-33270spurious CAS(DC11680A-E), include...

The Certification Basis for the originalproduct as amendedby thefollowingadditional or alternativeairworthiness requirements:- Thefollowing paragraph(s) at a lateramendment:CS 25, Amdt 15:25.771(a) (FD & HF);25.773 (a2) (FD & HF);25.777 (a) (b) (c) (FD & HF); 25.1301All (FlightControl Syst...

- LIST OF MAJOR DESINGCHANGES ANDMODIFICATIONS TO BECONSIDERED INTHECERTIFICATION PLANTEA-5-DT-180396. Ref. TEA-5-NT-200212, Issue A, dated04December 2020- C-295FWEASA-Approved AirplaneFlight Manual TAE-5-DT-160180 BasicRevision No.3, Issue E,dated 03 December2020- C-295FW EASA-Approved Ai...

To be installed in production only,from S/N 188 onwards, noretrofitallowed.Prior to installationof this change/repair it must bedetermined thattheinterrelationship between thischange/repair and anyotherpreviously installed changeand/ or repair will introduce noadverseeffect upon the airwort...

10/12/2020 Active






Date ofIssue Status


CN-235, CN-235-100,CN-235-200 CN-235-300, C-295 C-295

TS03.02 Cyber Security Analysis and AvionicsVersion AdjustmentThe Design ChangeDC10915-E defines the electrical and avionicsversionadjustment of C-295 L304 version S/N188; theDC11448S-E removes themilitaryswitches from the flight deck on the C-295MSN 188, 189 and191; and the DC11571A-Eaddres...

Certification Basis for the originalproduct as amended by thefollowingadditional or alternativeairworthiness requirements:- SpecialCondition(s): SC F-05 SecurityProtection ofAircraft SystemsandNetworks, SC F-25 Non rechargeableLithium batteries.- Deviation(s): F-28User-Defined Approaches.-...

- LIST OF MAJOR DESINGCHANGES ANDMODIFICATIONS TO BECONSIDERED INTHECERTIFICATION PLANTEA-5-DT-200133. Ref. TEA-5-NT-200323, Issue A,dated 04 December 2020.-C-295FW EASA-ApprovedAirplane Flight Manual TAE-5-DT-160180 BasicRevision No.3, Issue E,dated 03 December2020- C-295FW EASA-Appr...

To be installed in production only,from S/N 188 onwards, noretrofitallowed

09/12/2020 Active


C-212-EE C-212-DF C-212-DD C-212-CE C-212-CD C-212-CC C-212-CB

DC30067S-E - C-212 cracks in FuselageFR5Cracks were found on the fuselage skin ofC-212 aeroplanes, and on FR 5underneaththe skin, near the leading edge of the wing,on both LH andRH sides.


TEA-2-DT-200007 Issue A“C212. DC30067S-E “SKIN &FRAME CRACKSREPAIR”(SB212-53-0055-00)Certification Plan. (EASAProject 60074653)”TEA-2-NT-210001 Issue A “LIST OFMAJOR DESING CHANGESAND MODIFICATIONSTO BECONSIDERED IN THECERTIFICATION PLAN TEA-2-DT-200007”or later revisionsof the above liste...



C-295 DC11736A-E AHRS EnvironmentalQualificationAdditional Evidences for closingEnvironmental Qualification deviationsforFDU-3000 (AHRS). This Design Change is onlyaffecting thequalification evidences of AHRSin order to provide EASA with theadditionaldata required to close the Open Action Item11 of...


Airbus Defence and Space,C-295 AHRS EnvironmentalQualificationCertificationPlan, doc. no. TEA-5-DT-210075, issue B, dated 04March2021.Airbus Defenceand Space, C-295 TS-03.02Version. Avionics System(Navigation) EquipmentQualificationData, doc. no.TEA-5-DT-180648 - F,issue F,dated 07 April 2...


10072171 MAJOR CHANGE AIRBUS HELICOPTERS EC 225 LP AS 332 L2

Splices material change at the X5295 framejunction (ref. MOD 07.28463).


Certification Program (CP) ref.332ABN0691 Issue E, dated05/11/2019.Technical Follow-Up Sheet Approval Civil ref.TFSAC 18.332.0001.adated22/03/2018.TechnicalFollow-Up Sheet ApprovalCivil ref. TFSAC 18.332.0002.adated22/03/2018.TechnicalFollow-Up Sheet ApprovalCivil ref. TFSAC 18.225.0001.ad...

The following modification is apre-requisite for the embodimentof thisdesign change:- MOD07.26517, “Retrofit for X5295reinforcement with newaluminiumsplice (2,5mm) andplate with 4 fingers(titanium)”.Prior to installation ofthis change/repair it must bedetermined thattheinterrelationship be...

08/01/2020 Active

10072328 MAJOR CHANGE AIRBUS HELICOPTERS AS 332 L1 Enhanced Ground Proximity Warning System(EGPWS) certification (ref.OP.28668).


Certification Program (CP) ref.332ABN0871 Revision C,dated13/12/2019.ComplianceRecord Document (CRD) forCivil Modification ref. OP.28668Revision 3, dated30/01/2020.AssociatedTechnical Documentation(Continuation):Flight Manual(FM) compliance documentref. 332N881507E_CS IssueB,dated 23/01/2...

The following modifications,defining AS 332 L1 equipped withAHCAS, area pre-requisite for theembodiment of this designchange:- MOD 07.26640 -Hydraulic and flight controladaptation for AFCSintegration;-MOD 07.26641 - VMS installation;-MOD 07.26642 - AFCS installation;-MOD 07.26643 - FDS inst...

31/01/2020 Active






Date ofIssue Status

10072583 MAJOR CHANGE AIRBUS HELICOPTERS EC 175 B Approval of mod. FSA EC175 20-02 00/1Bintroducing MMEL EC175-B NormalRevision 5Edit.2.


Certification ProgramDocument No.M150A0715E99 “CertificationProgramfor Civil ModificationNo: FSA EC175 20-02 00/1B –EC175 MMELimprovementsfor HLX step3e (ATA 28 and63)”, Revision B,dated07.02.2020.EC 175BMMEL Normal Revision NR5Edition 2, date code (20-05)Compliance Record DocumentNo. M15...


10072784 MAJOR CHANGE AIRBUS HELICOPTERS REV. 1 EC 175 B Certification of MOD 99A05501-00-M-ECP/07, introducing changes to theprimary flightcontrols to reduce roll and collectivesensitivity.


Certification Program No.CPM670A0774E99“CertificationProgramCPM670A0774E99for Civil Modification No:99A05501-00-M-ECP/06 –EC175MOD – Reduction ofRoll and CollectiveControlSensitivity”, RevisionB,dated15.11.2019.ComplianceRecordDocument No.CRD670A0778E99“ComplianceRecordDocument CRD67...


10072880 MAJOR CHANGE AIRBUS HELICOPTERS EC 155 B1 Certification of MOD no. 07 56B32 (including07-21C36, 07-25C72,07-52C69 and 07-56B31)for the installation of a new canopystructure.

The Certification Basis for the originalproduct as amendedby thefollowingadditional or alternativeairworthiness requirements:Thefollowing paragraph(s) at a lateramendment: JAR 29.631 first issue,inlieu of CRI C-03.The requirements forenvironmental protection and theassociatedcertified noise...

Certification Program No.365ABN0421 “CertificationProgramNo.365ABN0421 forCivil Modification No 365A07-56B32 whichincludesMODs07-21C36, 07-25C72,07-52C69 and 07-56B31 –Title: LCH contract – EC155B1New Canopy”, Issue C, dated10.04.2019.ComplianceRecord Document No. 0756B32 “Compliance Re...

This design change is incompatiblewith VIP with bulkheadbetweencockpit and cabin, andEmergency Floatation.

24/03/2020 Active

10073009 MAJOR CHANGE AIRBUS HELICOPTERS EC 175 B ALS revision to extend to 20000 FH/80000 TC(Torque Cycles)the servicelife limits (SLL) ofP/N 87201-81 (body, jack front, flanged) andP/N86791-82 (piston front) and to removethe “provisional” indication (P)on P/N87205-81 (body, jack rear) of the TailServocontrol P/N 6397H6.


Certification Program No.CPM672A0801E99 “EC175ALS - Tail ServocontrolSLLextension to 20 000FH”, IssueA dated 10.02.2020.ALS asrevised according to TFSAC20.175.0004.aComplianceRecord Document No.CRDM672A0705E99/A forTFSAC 20.175.0004.a“EC175ALS - Tail Servocontrol SLLextension to 20 000FH”...


10073088 MAJOR CHANGE AIRBUS HELICOPTERS EC 175 B ALS revision to introduce a mandatoryinspection on the overload slipclutch P/N44314-398 every 36 months (4 monthstolerance) / 2000 HC(Hoist Cycles), in lieu ofthe current 24 months / 1200 HC servicelifelimit (SLL), applicable to hoistsystem P/N704A41815120 (MP/N42325-16-6) and P/NM259A70A100...


- Certification Program No.CPM259A7737E99“Certification ProgramNo.CPM259A7737E99 for CivilModification No.: TFSAC20.175.0003.a”, Issue Adated02.03.2020.- ALS as revisedaccording to TFSAC20.175.0003- ComplianceRecord Document No.CRDM259A0715E99 for TFSAC20.175.0003“EC175 –Mandatory inspec...







Date ofIssue Status

10073134 MAJOR CHANGE AIRBUS HELICOPTERS AS 355 F2, AS 355 N, AS 355NP AS 355 E, AS 355 F, AS 355 F1AS 350 BB, EC 130 B4,EC 130T2 AS 350 B, AS 350 B1, AS 350B2 AS 350 B3, AS 350 BA, AS 350D

Improvement of MGB fitting assembly (MOD07.20049) as terminating actionfor theairworthiness directive EASA AD 2018-0152.


Change definition as per350ABN0424E_CRD“ComplianceRecordDocument forCivilModification No: 07.20049”,revision A, dated 23 April2020,or later revisionsof the above listed document(s) approved/acceptedunderthe EASA system.


27/04/2020 Active

10073140 MAJOR CHANGE AIRBUS HELICOPTERS EC 175 B EC175 RFM update according to EASA SIB2013-11R1 on ACAS II.


Certification ProgramM150A0718E99 “CertificationProgram for CivilModificationNo: FSA EC175 20-04 007/1B– Title: EC175 RFM SUP.34updatefor ACASII –Manoeuvres based on visualAcquisition of traffic”,RevisionA, dated 31.03.2020.RFM EC175 B: SUP.34 NormalRevision 1 Edition 2 – datecode 20-10Co...


10073295 MAJOR CHANGE AIRBUS HELICOPTERS AS 332 L2, EC 225 LP Introduction of mandatory inspections forthe hoist slip clutch MP/N44314-398 installedon Goodrich hoists MP/N 42325-type andMP/N44318-type (ref. MODs TFSAC19.225.0001, TFSAC 19.225.0002 andTFSAC19.332.0003).


Certification Program (CP) ref.332N892507E_CP Revision A,dated22/11/2019.TechnicalFollow-Up Sheet ApprovalCivil ref. TFSAC 19.225.0001.bdated27/11/2019.TechnicalFollow-Up Sheet ApprovalCivil ref. TFSAC 19.225.0002.adated27/11/2019.TechnicalFollow-Up Sheet ApprovalCivil ref. TFSAC 19.332.00...


18/05/2020 Active

10073297 MAJOR CHANGE AIRBUS HELICOPTERS EC 155 B, EC 155 B1 Update of EC 155 ALS Section 04-10according to TFSAC 19.155.0001.a, toremoveany reference to Main Rotor Blades P/N365A11 0082.00, since thepart has neverbeen released to service.


- Compliance RecordDocument for CivilModification No.TFSAC19.155.0001.a-CRD,Title: Update of ALS project §04-10 for Main RotorBladesATA 62, Revision 1, dated20.04.2020.- EC155 ALS as perTFSAC 19.155.0001.a, dated07.04.2020.or later revisionsof the above listed document(s) approved/accepted...


10073300 MAJOR CHANGE AIRBUS HELICOPTERS EC 175 B Certification of MOD 99A05783-00-M-ECP/00and 99A05784-00-M-ECP/03introducing theinstallation of SHUT-OFF VALVE P3 P/NM718A40T1003 as areplacement of BLEEDAIR SHUT-OFF VALVE P/N U718A40T1009.


Certification Program No.CPM710A0760E99“Certification ProgramNo.CPM710A0760E99 Issue Bfor Civil Modification No.99A05783-00-M-ECP/00,99A05784-00-M-ECP/03Title: EC175 MOD -Powerplant P3 Shut-offvalvereplacement”, RevisionB, dated04.03.2020.ComplianceRecord Document No.CRDM710A0761E99 “Cer...

MOD No. 99A05783-00-M-ECP/00and 99A05784-00-M-ECP/03 aremutuallyrequired.

19/05/2020 Active






Date ofIssue Status

10073397 MAJOR CHANGE AIRBUS HELICOPTERS EC 155 B, EC 155 B1 Replacement SEMA Old Generation (OG) byNew Generation 2 (NG2)The aim of thisproject is to certify the design change forreplacingthe Serial Electro-MechanicalActuator (SEMA) OLD Generation (OG)bySEMA New Generation 2 (NG2). Theimproved evolution SEMA NG2 wasdesignedin such that the physical di...


Certification Plan365ABN0484_CP RevDCompliance RecordDocument 07.22B81 Rev 2orlater revisions of the abovelisted document(s) approved/acceptedunder the EASAsystem.


03/06/2020 Active

10073710 MAJOR CHANGE AIRBUS HELICOPTERS AS 350 B3 Update of Normal Procedures for RotorcraftFlight Manual SupplementsSUP19 & 19.1,“Breeze” Electrical Hoist 204 kg (450lb).


AS 350 B3e RFM SUP.19, RR3ato NR2, data code (20-28)AS350B3e RFM SUP.19.1, RR3ato NR2, data code (20-28)Updated as per FSA ECU20-25 049 / 1B, dated 02 July2020or later revisions of theabove listed document(s)approved/acceptedunder theEASA system.


10073763 MAJOR CHANGE AIRBUS HELICOPTERS EC 225 LP New Direct Current Electrical Master Box(DCEMB) with 3rd TRU capability(ref. MOD07.28665).


Certification Program (CP) ref.332ABN0838 Revision C,dated28/05/2020.ComplianceRecord Document (CRD) forCivil Modification ref.07.28665Revision 1, dated09/07/2020.or later revisionsof the above listed document(s) approved/acceptedunderthe EASA system.


10/07/2020 Active

10073764 MAJOR CHANGE AIRBUS HELICOPTERS EC 225 LP RFM Section 3.3 Rush Revision (RR) to amendthe Vehicle MonitoringSystem (VMS) failureprocedure in case of double AircraftManagementComputer (AMC) failure (ref.MOD FSA_225_20-12 011_2B).


Compliance Record Document(CRD) for Civil ModificationFSA_225_20-12011_2B ref.332N041513ERevision 3,dated 03/06/2020.RotorcraftFlight Manual (RFM)compliance document ref.332N041515E_CCSIssue B,dated 18/05/2020, includingthe following EC225 LPRFMdocuments: -PSOFF2_225_20-12011_2B_PMVR...

The following modification is apre-requisite for the embodimentof thisdesign change:- MOD07.26845 (“AMC GE computerreplaced by AMC+”).Prior toinstallation of this change/repair itmust be determined thattheinterrelationship between thischange/repair and anyotherpreviously installed changean...

10/07/2020 Active

10073877 MAJOR CHANGE AIRBUS HELICOPTERS AS 332 L1 Single electrical hoist configurationcertification on AS332 L1 (ref.MOD SPMC.28730B).


Certification Program (CP) ref.32ABN0943E_CP Issue B,dated01/07/2020.ComplianceRecord Document (CRD) forCivil Modification ref. SPMC.28730BIssue 2, dated23/07/2020.Rotorcraft FlightManual (RFM) compliancedocument ref.332N041518E_CCSIssue B,dated 02/07/2020, includingthe following AS332 L1...

The following modifications,defining AS332 L1 equipped withAHCAS, area pre-requisite for theembodiment of this designchange:- MOD 07.26640 -Hydraulic and flight controladaptation for AFCSintegration;-MOD 07.26641 - VMS installation;-MOD 07.26642 - AFCS installation;-MOD 07.26643 - FDS insta...

24/07/2020 Active






Date ofIssue Status

10074054 MAJOR CHANGE AIRBUS HELICOPTERS EC 225 LP Certification of software VMS AMC+ V4.1 P/N707A49439530, applicable toaircraftmanagement computers AMC+.


Document No. 332ABN0917 –CP “Certification Program332ABN0917 forcivilmodification No:07.28743 – Title: MGB FailSafe monitoringdiscreteactivation on EC225LPAMC+ installation”, revision B,dated 04.03.2020.RFM EC 225LP update as per DocumentNo. 332N041522E_CCS“Coversheet ATA15-01 – AMC+ VMSD...

This design change requires priorembodiment of: ECP 07.26845“AMC+ LRUinstallation”.

17/08/2020 Active

10074056 MAJOR CHANGE AIRBUS HELICOPTERS EC 175 B ALS update as per TFSAC 20.175.0011.aincluding extension of servicelife limit andinspection interval extensions on rotor andmain gearboxsuspension components.


Certification Program No.CPM005A3702E99“CertificationProgramCPM005A3702E99issue A for Civil ModificationNo: TFSAC20.175.00xx.a –Title: Rotor and suspensionparts Inspection and ServiceLife Limitationextension”,Revision A, dated25.06.2020.EC175 ALSupdated as per TFSAC20.175.0011.a, dated 29...


10074062 MAJOR CHANGE AIRBUS HELICOPTERS EC 175 B Design change 00A03764-00-M-ECP/04introducing MGB suspensioncrossbeamassemblies M633A2101053 (forproduction) and M008A6334052 (forretrofit).Both assemblies include the new crossbeamP/N M633A2101103(equipped with bushings)made of Titanium alloy, to replace theexistingP/N M633A2101601 made of A...


Certification Program No.CPM633A0706E99“Certification Program forcivilmodification No:00A03764-00-M-ECP/04 –Title:EC175 MOD –Crossbeamreinforcement – New designand material”, Revision A,dated06.12.2018.EC175 B ALSupdated as per TSFAC20.175.0001.a, dated21.07.2020.ComplianceRecord Docume...


10074079 MAJOR CHANGE AIRBUS HELICOPTERS EC 175 B Extension of the ALS inspection interval 63-28to 800FH (+100FHtolerance), applicable tothe second lubrication pump, and extensionofthe CMR applicable to the secondarylubrication system to 900 FH.


Certification Program no.CPM040A0722E99“CertificationProgramCPM040A0722E99issue A for TFSAC.2020.175.xxxx.a”, Revision A,dated06.05.2020.EC175 B ALSupdated as per TFSAC20.175.0007.a, dated15.07.2020.ComplianceRecord Document no.CRDM040A0723E99“ComplianceRecordDocumentCRDM040A0723E99 iss...

None. 21/08/2020 Active

10074081 MAJOR CHANGE AIRBUS HELICOPTERS EC 175 B Design change 99A05898-00-M-ECP/00introducing a filter inside the maingearboxmast bearing lubrication duct equipped P/NM625A2012101.


Certification Program no.CPM620A0708E99“CertificationProgramCPM620A0708E99issue A for Civil ModificationNo: 99A05898-00-M-ECP/00 –Title: Additional filter on mastbearing lubrication”, RevisionA,dated08.06.2020.ComplianceRecord Document no.CRDM620A0707E99“ComplianceRecordDocumentCRDM620A...







Date ofIssue Status

10074085 MAJOR CHANGE AIRBUS HELICOPTERS AS 365 N3 ALS revision to introduce in chapter 04-20 amandatory inspection on theoverload slipclutch P/N 44314-398 every 36 months (4months tolerance)/ 2000 HC (Hoist Cycles), inlieu ofthe current 24 months / 1200HCservice life limit (SLL), applicable to hoistsystem P/N 704A41815.112(MP/N42325-16-5) a...


Certification Program no.365ABN0509E “CertificationProgram 365ABN0509EforCivil Modification No: TFSAC20.365.0001.a – Title:Mandatoryinspection forhoist slip clutch”, Revision A,dated 03.04.2020.AS365 N3ALS revised as per TFSAC20.365.0001.a, dated21.07.2020.ComplianceRecord Document no. DO...


10074146 MAJOR CHANGE AIRBUS HELICOPTERS EC 175 B Design change 99A06105-00-M-ECP/00,replacing Aluminium angles withTitaniumangles on the firewall separating the enginecompartment fromthe main gearboxcompartment.


Certification Program No.CPM710A0762E99“CertificationProgramCPM710A0762E99for Civil Modification No:99A06105-00-M-ECP/00 –Title:EC175 MOD – Firewallangles materialchange”,Revision A,dated23.06.2020.ComplianceRecord Document No.CRDM710A0763E99“ComplianceRecordDocumentCRDM710A0763E99 fo...


10074183 MAJOR CHANGE AIRBUS HELICOPTERS EC 175 B Modification of Aircraft Maintenance Manual(AMM) work card63-32-00,4-1 of ALS task63/32/00/000/000/160 to cancelthesystematic discardingof the crossbeamsuspension bolts P/N M633A2108501,associated to everydisassembly of thecrossbeam.


Certification Program no.CPM633A0709E99“CertificationProgramCPM633A0709E99issue A for H175A000706_DIR– Title: EC175 – Removalofsystematic suspension boltscrapping”, Revision A, dated18.05.2020.ComplianceRecord Document no.CRD633A0708E99“ComplianceRecordDocument no.CRD633A0708E99 issue A...


10074310 MAJOR CHANGE AIRBUS HELICOPTERS EC 130 B4, EC 130 T2 P/N correction of the MGB suspension crossbar laminated stop in ALS04-20.


Update of EC 130 B4 and EC130 T2 AirworthinessLimitation Section (ALS)inaccordance with TFSAC17.130.0004 / A, dated20 July2020,or later revisionsof the above listed document(s) approved/acceptedunderthe EASA system.

The revised ALS shall be madeavailable to operator/owner andany otherperson required tocomply with revised tasks,inaccordance with21.A.61.

21/09/2020 Active

10074441 MAJOR CHANGE AIRBUS HELICOPTERS EC 155 B, EC 155 B1 Design change 07.31B97 introducing SmartMultifunction Display (SMD)software P/NK185AAA03, released to solve previoussoftware bugs. Theinstallation of SW P/NK185AAA03 on applicable SMD HW creates anewprogrammed assembly P/N704A45751346 (manufacturing P/NC19267YA03)designated as “SMD45-NGWAAS...


Certification Program365ABN0504E “CertificationProgram 365ABN0504EforCivil Modification No:07.31B97 – Title: FailureIndication on SMD45 –SWcorrection”, Revision A, dated16.03.2020.ComplianceRecord DocumentDA07.31B97A “ComplianceRecordDocumentDA07.31B97A forCivil Modification No:DA07.31B...

SMD P/N 704A45751182,704A45751184, 704A45751306and 704A45751307 cannotberetrofitted to become P/N704A45751364 (manufacturer P/NC19267YA03),installing SWK1855AAA03.SMD P/N704A45751319 (manufacturer P/NC19267YA02), installing SW P/NK1855AAA02 can be retrofittedto become P/N 704A45751364(manu...

01/10/2020 Active






Date ofIssue Status

10074442 MAJOR CHANGE AIRBUS HELICOPTERS EC 175 B Design change 99A05940-00-M-ECP/00introducing the nose landing gear “A”frameP/N M322G50A3006.


Certification ProgramCPM332A0704E99“CertificationProgramCPM332A0704E99for Civil Modification No:99A05940-00-M-ECP/00 –Title:EC175 MOD – NoseLanding Gear Return to axismechanism redesignMP430”,Revision A, dated02.07.2020.EC 175 B ALSupdated as per TFSAC20.175.0010.a, dated29.06.2020.Comp...


10074576 MAJOR CHANGE AIRBUS HELICOPTERS EC 175 B Design change 99A04844-00-M-ECP/02,introducing a new MGB flexible shaftP/NM632A3810102.

The Certification Basis for the originalproduct as amendedby thefollowingadditional or alternativeairworthiness requirements:-Equivalent Safety Finding(s): CRIE-09.The requirements forenvironmental protection and theassociatedcertified noise and/ oremissions levels of the product areunchan...

Certification Program no.CPM630A0729E99“CertificationProgramCPM630A0729E99Issue B for Civil ModificationNo: 99A04844-00-M-ECP/02 –Title: EC175 MOD – Newdesign of MGB flexible shaft”,Revision B,dated06.03.2020.EC 175 BALS updated as per TFSAC20.175.0012.a, dated22.09.2020.ComplianceRecord...


10074581 MAJOR CHANGE AIRBUS HELICOPTERS EC 175 B Removal of EC175 B ALS penalty factorsrelated to Flight inLimitedIcing Conditions(FLIC), introducing the condition into thefatiguespectrum with FLIC maximum timeexposure.


Certification Program no.CPM000A0795E99“CertificationProgramCPM000A0795E99issue A for Civil modificationNo: TFSAC.175.2020.0xx.a –Title: EC175 ALS – Removal ofFLIC penalty factors”, RevisionA, dated01.09.2020.EC 175 BALS updated asper TFSAC20.175.0013.a, dated24.09.2020.ComplianceRecordD...


10074634 MAJOR CHANGE AIRBUS HELICOPTERS EC 130 T2 EC 130 B4, EC 130 T2 EC 130 B4 AS 355 NP AS 355 N AS 355 F2, AS 355 N, AS 355NP AS 355 F2 AS 355 F1 AS 355 F AS 355 E, AS 355 F, AS 355 F1AS 355 E AS 350 D AS 350 BB AS 350 B, AS 350 B1, AS 350B2 AS 350 BA AS 350 B3, AS 350 BA, AS 350D AS 350 B3 AS 350 B2 AS 350 B1 AS 350 B

Update of Airworthiness Limit

Major Change / Major Repair easa.europa · 10072840 MAJOR CHANGE AIRBUS CANADA LIMITED PARTNERSHIP...

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