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TCDSNo.:EASA.IM.A.570BDͲ500Page1of28

Issue:20Date:09May2023

Proprietarydocument.Printedcopiesarenot

Anagency

oftheEuropeanUnion

TYPEͲCERTIFICATE

DATA SHEE T

No.EASA.IM.A.570

For

BDͲ500

TypeCertificateHolder:

AirbusCanadaLimitedPartnership

13100HenriͲFabreBlvd.

Mirabel,Québec,Canada

J7N3C6

ForModels:BDͲ500Ͳ1A10

BDͲ500Ͳ1A11

AnagencyoftheEuropeanUnion

Intentionallyleftblank

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TABLEOFCONTENTS

6.StateofDesign

SheetNo...............................7

6.2.Cabin

7.Propellers

12.OperatingLimitations

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3.

4.StateofDesign

2.ReferenceDate

5.4.EnvironmentalProtection

19

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21.WheelsandTyres

V.OperationalSuitability

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SECTION1:MODELBDͲ500Ͳ1A10

I.General

1.Type/Model/Variant

BDͲ500/BDͲ500Ͳ1A10

2.PerformanceClass

A

3.CertifyingAuthority

TransportCanadaCivilAviation

Initial:10December2009

Deferred:31December2011

5.EASATypeCertificationApplicationDate

Initial: 4March2010

Deferred:31December2011

17December2015

7.EASATypeCertificationDate

15June2016

II.CertificationBasis

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revisions)

5.EASAAirworthinessRequirements

5.1SpecialConditions

BͲ01FlightinIcingConditions

BͲ03MotionandEffectsofCockpitControls

EnergyAwareness

BͲ05

BͲ14FlightEnvelopeProtectionDesign

SteepApproach

BͲ17NormalLoadFactorLimitingSystem

CͲ06DesignDiveSpeed

CͲ07DesignManoeuvreLoad

CͲ13AutomaticBrakingSystemLoads

DͲ08InͲFlightFire-Composite

andUnusualConstruction

DͲ14TowbarlessTowing

EͲ01Water/IceFuelSystem

FͲ01HIRFProtection

FͲ11FlightRecorders,Data

LinkRecording

FͲ21AirborneSystems&NetworkSecurity

FͲ29LithiumBatteryInstallations

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5.2.Deviations

None.

5.3.EquivalentSafetyFindings

BͲ24OutofTrim

DͲ13PackͲoffDispatch

DͲ23BurnthroughonWTBF

DͲ30APUDoorsESF

EͲ13FanZoneNonFireZone

EͲ14DigitalOnlyDisplaysofPowerͲ

PlantInstruments

EͲ15EngineIgnitionSwitches

5.4.EnvironmentalProtectionRequirements

6.OperationalSuitabilityRequirements

6.1FlightCrewData

InitialIssue,31January2014

6.2.CabinCrewData

Ͳ31January2014.

6.3.MasterMinimumEquipmentList

31January2014(Book1only)

February2014(asAMC/GM)

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1.TypeDesignDefinition

Rev.Aorlaterapprovedrevisions.

approvedrevisions,theapprovedtypedesign serialnumber).

2.Description

engines.

ReinforcedPlastic

3.Equipment

4.Dimensions

Wingspan35.1m(115ft1in)

OverallLength34.9m(114ft9in)

Height 11.8m(38ft8in)

5.Engines

6.AuxiliaryPowerUnit

One(1)Honeywell131Ͳ9(C)

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7.Propellers

N/A

8.Fluids(Fuel,Oil,Additives,Hydraulics)

8.1Fuel

8.2Oil

10200Ͳ00.

8.3Hydraulics

3AB48Ͳ10200Ͳ00.

9.FluidCapacities

9.1Fuel

9.2Oil

10.AirspeedLimits

knotsMach

VMOandMMOͲͲ

SeaLevelto8,000ft.300Ͳ

10,000ft.to27,500ft.330Ͳ

Above27,500ft.Ͳ0.82

11.FlightEnvelope

MaximumOperatingAltitude:

BD500Ͳ314004orMod314004

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Enroute:41,000ft(12,497m)

12.OperatingLimitations

12.1ApprovedOperations

ͲVisual(VFR)

ͲInstrument(IFR)

ͲIcingConditions

ͲDitching(seeNote2)

12.2OtherLimitations

MinimumAmbientTemperatureforTakeoff Ͳ54°C

PostSBBD500Ͳ278001

Runwayslope+/Ͳ2%

13.MaximumCertifiedWeights

Weightkglb

MaximumRampWeight(MRW)64183141500

MaximumTakeoffWeight(MTOW)63730140500

MaximumLandingWeight(MLW)54658120500

MaximumZeroFuelWeight(MZFW)52617116000

14.CentreofGravityRange

15.Datum

16.LevellingMeans

rearfuselage/aftequipmentbayatFS1390.83.

17.MinimumFlightCrew

Two(2)-PilotandCoͲPilot

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18.MinimumCabinCrew

Three(3)

interior.

19.MaximumAircraftOccupants

Passengers*)

orpassengers andthe thecertificationrequirements.

127C-IIIͲCͲͲͲ35

0NoneBasicAirbusCorporate

Jet(ACJ)00

20.Baggage/CargoCompartment

MaximumLoading

lbkg

FwdCargoCompartment37421697

AftCargoCompartment45482063

21.WheelsandTyres

21.1Wheels

NoseLandingGear:12"

MainLandingGear:21"

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21.2Tyres

22.ETOPS

EASAapprovedrevisions.

ModelEngineTypeUpto120min.

ApprovaldateUpto180min.

Approvaldate

IV.OperatingandServiceInstructions

1.AirplaneFlightManual(AFM)

MaintenanceReview

3.WeightandBalanceManual(WBM)

code.

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V.OperationalSuitabilityData(OSD)

1.MasterMinimumEquipmentList

2.FlightCrewData

3.CabinCrewData

1A10(CS100)Report,Issue1,dated

June1st2016",orlaterapprovedrevisions.

VI.Notes

1. ImportRequirements:

definedinTCDS

2. Ditching:TheBDͲ500Ͳ1A10ModelconfiguredwiththeBasicAirbusCorporateJet(ACJ)

forditching,

3. RAZͲBA500Ͳ027AppendixA,RevisionMorlaterrevisions,providesguidancetocompletion

generalapplicableconditions,or considerationsregarding: thecompletioncentre(N/Ato theBasicACJaircraft)

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includesreferencestoinstallation,

4. ModelairplaneBDͲ500Ͳ1A10receivesthecommercialdesignationA220Ͳ100.

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SECTION2:MODELBDͲ500Ͳ1A11

I.General

1.Type/Model/Variant

BDͲ500/BDͲ500Ͳ1A11

2.PerformanceClass

Aquotesdbs_dbs4.pdfusesText_8

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