[PDF] EASA SPECIFIC AIRWORTHINESS SPECIFICATION No. EASA

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EASA.SAS.A.176D SND601D‘Corvette"D PageD1DofD9D

Issue:D02DDDate:D18DMarchD2016D

EASA

SPECIFIC AIRWORTHINESS

SPECIFICATION

No.DEASA.SAS.A.176

for

SND601D'CORVETTE'

Serial Number : 028 and 039

D D

Airworthiness Category: Large Aeroplanes

D D

ForDModels:DSND601D

This Specific Airworthiness Specification is issued in accordance with Regulation (EC)

216/2008 Article 20(1)(b). There is no valid Type Certificate for this aircraft type. The

former type certificate holder was

List of effective Pages:

Page 1 2 3 4 5 6 7 8 9

Issue 02 02 02 02 02 02 02 02 02

D EASA.SAS.A.176D SND601D‘Corvette"D PageD2DofD9D

Issue:D02DDDate:D18DMarchD2016D

D D D D D D D D D D D D D D D D D D D D D D D D

IntentionallyDleftDblankD

D D D EASA.SAS.A.176D SND601D‘Corvette"D PageD3DofD9D

Issue:D01DDDate:D03DAugustD2011D

TABLE OF CONTENTS

SECTION 0: Disclaimer ............................................................................................ 4

SECTION 1: Aircraft Design Definitions ................................................................. 4

I. Certification Specification............................................................................................ 4

I.I Certification DateD.....................................................................................................D4

I.II Certification BasisD..................................................................................................D4

I.III Technical Characteristics and Operating LimitationsD.........................................D4

II. Design Data .................................................................................................................. 5

SECTION 2: Airworthiness Directives .................................................................... 5

SECTION 3: Mandatory policy ................................................................................. 8

I. Airborne Collision Avoidance System (ACAS) II .................................................... 8

SECTION 4: Occurrence Reporting ......................................................................... 8

SECTION 5: Other Limitations ................................................................................. 8

SECTION 6: Administrative ...................................................................................... 8

I. Acronyms and Abbreviations ...................................................................................... 8

II. Change Record ............................................................................................................ 9

D D EASA.SAS.A.176D SND601D‘Corvette"D PageD4DofD9D

Issue:D01DDDate:D03DAugustD2011D

SECTION 0: Disclaimer

certificateDholderDwas:D D

Airbus SAS

1,DRond-PointDMauriceDBELLONTED

31700DBLAGNACDCedexD

FRANCED

D

ThisD SpecificD AirworthinessD SpecificationD (SAS)D isDissuedD inD accordanceD withD RegulationD (EC)D

SECTION 1: Aircraft Design Definitions

I. Certification Specification

I.I Certification Date

D

I.II Certification Basis

D

4,DdatedDOctoberD1990D-DSectionD11D

I.III Technical Characteristics and Operating Limitations EngineDcharacteristicsD ReferDtoDAnnexD1:DSN601D‘Corvette"DTypeDDesignDDataDSheetD(FicheD D OilDCapacityD ReferDtoDAnnexD1:DSN601D‘Corvette"DTypeDDesignDDataDSheetD(FicheD D FuelDCapacityD ReferDtoDAnnexD1:DSN601D‘Corvette"DTypeDDesignDDataDSheetD(FicheD D MaximumDWeightD ReferDtoDAnnexD1:DSN601D‘Corvette"DTypeDDesignDDataDSheetD(FicheD D C.G.DRangeD ReferDtoDAnnexD1:DSN601D‘Corvette"DTypeDDesignDDataDSheetD(FicheD D AirspeedDLimitsD ReferDtoDAnnexD1:DSN601D‘Corvette"DTypeDDesignDDataDSheetD(FicheD D MaximumDAltitudeDOperationD ReferDtoDAnnexD1:DSN601D‘Corvette"DTypeDDesignDDataDSheetD(FicheD D MaximumDloadDfactorD ReferDtoDAnnexD1:DSN601D‘Corvette"DTypeDDesignDDataDSheetD(FicheD EASA.SAS.A.176D SND601D‘Corvette"D PageD5DofD9D

Issue:D02DDDate:D18DMarchD2016D

DD D AnyDotherDlimitationsD ReferDtoDAnnexD1:DSN601D‘Corvette"DTypeDDesignDDataDSheetD(FicheD D MinimumDequipmentDD ReferDtoDAnnexD1:DSN601D‘Corvette"DTypeDDesignDDataDSheetD(FicheD D NumberDofDSeatsD ReferDtoDAnnexD1:DSN601D‘Corvette"DTypeDDesignDDataDSheetD(FicheD D ForD theD approvedD seatD dispositions,D referD toD AnnexD 1:D SN601D D MaximumDBaggageD ReferDtoDAnnexD1:DSN601D‘Corvette"DTypeDDesignDDataDSheetD(FicheD D ControlDSurfaceDMovementsD ReferDtoDAnnexD1:DSN601D‘Corvette"DTypeDDesignDDataDSheetD(FicheD D TyreDcharacteristicsD ReferDtoDAnnexD1:DSN601D‘Corvette"DTypeDDesignDDataDSheetD(FicheD D FlightDManualD Ref:D 601-A-100D 7FD approvedD byD SGACD onD 1974,D 28D May,D andD subsequentDapprovedDupdates.D D

II. Design Data

4,DdatedDOctoberD1990D-DSectionD1.D

D

SECTION 2: Airworthiness Directives

-D ADDreference,D -D ADDApplicability,D -D AirworthinessDissueD/DRequiredDactionsD -D ApprovedDsupportDdocumentationD D D applicable.D D

76-077-2(B)D

ServiceDBulletinD57-10.D

D

78-191-3(B)D

Applicability:D AllD MSND -D RegulatoryD disposalsD forD certificationD -D ApplicationD ofD SNIASD ServiceD

BulletinsD30-5DandD27-14.D

EASA.SAS.A.176D SND601D‘Corvette"D PageD6DofD9D

Issue:D02DDDate:D18DMarchD2016D

DD D

80-126-4(B)D

D

86-161-5(B)D

D

89-196-006(B)R1D

D

90-057-007(B)R1D

D

90-115-008(B)D

Applicability:D AllD MSND havingD embodiedD AérospatialeD ModificationD 1390D orD AérospatialeD ServiceD

D

91-044-009(B)D

BulletinD 52-13D -D InspectionD /D ModificationD onD emergencyD exitD edgingD plateD -D ApplicationD ofD

AérospatialeD ServiceD BulletinD 52-12,D andD dependingDtheD inspectionD resultsD AérospatialeD ServiceD

BulletinsD 53-9D (orD embodimentD ofD AérospatialeD ModificationD 1408)D orD 52-13D (orD embodimentD ofD

AérospatialeDModificationD1426).D

D

91-045-010(B)R1D

Applicability:D AllD MSND havingD embodiedD AérospatialeD ModificationD 1049D orD AérospatialeD ServiceD

25D configurationD -D InspectionD onD wingD rootD upperD andD lowerD surfacesD reinforcementD platesD -D

D

91-046-011(B)D

Applicability:D AllD MSND havingD embodiedD AérospatialeD ModificationD 1291D orD AérospatialeD ServiceD

53-23DRev1.D

D

91-047-012(B)D

Applicability:D AllD MSND notD havingD embodiedD AérospatialeD ModificationD 1291,andD 1368D orD D

91-048-013(B)R1D

D

91-100-014(B)D

EASA.SAS.A.176D SND601D‘Corvette"D PageD7DofD9D

Issue:D02DDDate:D18DMarchD2016D

DD D

91-101-015(B)D

BulletinD 53-13D -D InspectionD /D ModificationD ofD junctionD stripD atD frameD 10D -D AérospatialeD ServiceD

D

91-102-016(B)D

D

91-174-017(B)D

BulletinD 53-28D -D InspectionD /D ModificationD ofD internalD beamsD betweenD framesD 20D andD 22D -D

D

91-260-018(B)D

BulletinD21-6.D

D

95-054-019(B)R1D

Applicability:D AllD MSND notD havingD embodiedD AérospatialeD ServiceD BulletinD 57-26D -D inspectionD /D

D

95-102-020(B)D

D

98-179-021(B)D

InstructionDn°D20403DIssueD2.D

D

2003-343(B)D

D

F-2004-169D

BulletinDCorvetteDNo.D32-17.D

(This AD is approved under EASA Reference No 2004-10566 dated October 20, 2004) D

F-2006-034D

Applicability:D AllD MSND -D DocumentationD updateD (CheckD ofD GearD ControlD Lever)D -D AFMD CorvetteD

5DandD6.D

(This AD is approved under EASA Reference No 2006-0028 dated January 24, 2006) D

2008-0192D

D

2009-0041D

CorvetteDServiceDBulletinDNoD32-19.D

NOTE

1. AirworthinessDDirectivesDpublishedDafterDJuneD2007DcanDbeDfoundDonDtheDEASADwebsiteD

http://ad.easa.europa.eu)D

2. AirworthinessDDirectivesDpublishedDpriorDJuneD2007DcanDbeDconsultedDbesideDDGAC-FD/DOSAC.D

3. ServiceDBulletinsDcanDbeDobtainedDfromDAirbusDSAS.

EASA.SAS.A.176D SND601D‘Corvette"D PageD8DofD9D

Issue:D02DDDate:D18DMarchD2016D

DD

SECTION 3: Mandatory policy

I. Airborne Collision Avoidance System (ACAS) II

SAS.D

SECTION 4: Occurrence Reporting

ThisDSpecificDAirworthinessDSpecificationDmayDbeD usedDasDaDbasisDforDtheDissueDofDaDRestrictedD D a)D TheD holderD ofD aD RestrictedD CertificateD ofD AirworthinessD basedD onD thisD SpecificD safetyDofDoperation 1.D D b)D SuchDreportsDshallDbeDdispatchedDwithinD72DhoursDofDtheDtimeDwhenDtheDoccurrenceDwasD D

c)D TheD StateD ofD RegistryD shallD forwardD theD informationD receivedD underD (a)D toD theD AgencyD

whenD itDrelatesDtoDfailures,Dmalfunctions,DdefectsDorDotherDoccurrencesD whichDcauseDorD

SECTION 5: Other Limitations

D D

AnyD otherD limitationsD includedD throughD theD AeroplaneD TypeD CertificateD DataD SheetD enclosedD inD

D ForDtheD approvedD documentation,DreferDtoD AnnexD1:D SN601D ‘Corvette"DTypeDDesignDDataDSheetD

SECTION 6: Administrative

I. Acronyms and Abbreviations

Acronyms Designation

ADD AirworthinessDDirectiveD

AFMD AircraftDFlightDManualD

DGAC-FD DirectionDGénéraleDdeDl"AviationDCivileD-DFranceD EASA.SAS.A.176D SND601D‘Corvette"D PageD9DofD9D

Issue:D02DDDate:D18DMarchD2016D

DD

EASAD EuropeanDAviationDSafetyDAgencyD

LHD/DRHD LeftDHandD/DRightDHandD

MSND ManufacturerDSerialDNumberD

OSACD OrganismeDdeDlaDSécuritéDAérienneD

P/ND PartDNumberD

SASD SpecificDAirworthinessDSpecificationD

SBD ServiceDBulletinD

TCDSD TypeDCertificateDDataDSheetD

D

II. Change Record

D

Issue Date Changes

IssueD01D 03DAugustD2011D InitialDIssueD

IssueD02D 18DMarchD2016D SectionD3DaddedD

AnnexD3DaddedD

ReformattingD

D D D S

PECIF FISAFRWORTHFNCPPS

PECIF FIATFONS

forS S

PNS601'Iorvette'S

TypeSPN601

S S S S S S S S S S S

AnnexS1S

S

PN601S3Iorvette'S

TypeSIert'f'dDt'onSsDtDSPieetSNoS1gcS

S

REPUBLIQUE FRANCAISE

DIRECTION GENERALE

DE L'AVIATION CIVILE

Edition du BUREAU VERITAS

Organisme delegue

FICHE DE NA VIGABILITE N° 147

Avion SN 601 "CORVETfE"

Type SN601

Constructeur autorise : Societe Nationale Industrielle

AEROSPA TIALE

37, Boulevard Monunorency

75016

PARIS (FRANCE)

Certificat

de Navigabilite de Type nO 74 d6livre Ie 29 Mai 1974 et

Certificat

de type de limitation de nuisances N° N-74 delivre Ie 29 Mai 1974 (associe a 1a fiche de donnees N° N-147)

FICHE N° 147

A vions

SN 601

Edition nO 4

Octabre 1990

Nombre

de pages: 14 . Fiche de navigabilitt nO 147 -Ed. 4 -10/90

SOMMAIRE

1· DEFINITION DE L'A VI ON SN 601 "CORVETTE"

2· INST ALLA TION MOTRICE

2·1 Moteurs

• 2 reacteurs IT 15D4 -Poussee statique

Temperature et vitesse de rotation maximales

2·2 Circuit d'huiIe

-Specifications Iubrifiant -Capacitt des reservoirs de lubrifiant

2·3 Carburants et additifs

• Specifications carburants -Specifications additifs • Capacitt des reservoirs carburant et parametres -Systeme Vide-Vite baIIonnets

3· LIMITATIONS A VION

3-1 Limitations de masse

3·2 Limitations de centrage • Train sorti

3-3 Limitations de

"itesse

3·4

Altitude maxima Ie d'utiJisation

3·5 Limitations facteur de charge en manreuvre

3-6 Autres limitations

4· EQUIPAGE MINIMAL DE CONDUITE

s· NOMBRE MAXIMAL DE SIEGES PASSAGERS

Page 3

Page 4

6· CHARGEMENT DE BAGAGES

6-1 Compartiment avant

6·2 Compartiments arrieres

6·3 Resistance des planchers

7· REPERES DE MISE A NIVEAU

8· BRAQUAGE MAXIMAL DES GOUVERNES

Gouverne de profondeur

Plan horizontal reglable

Gouverne de direction

Ailerons

Spoilers

Aerofreins

Volets hypersustentateurs

Fiche de navigabilit.e nO 147 -Ed. 4 -

9· CHARGE MAXIMALE SUR LES TRAINS D'ATTERRISSAGE

Train auxiliaire

Train principal

Coefficient de piste

10· DOCUMENTS RELATIFS A L'UTILISA TION DE L'A VlON

11· BASES

DE CERTIFICA TION

12· DIVERS

. Fiche de navigabilitt nO 147 -Ed. 4 -10/90

1· DEFINITION DE L'AVION SN 601 "CORVETTE"

Repertoire des dessins de Jiasse Ref. 00.601.AJXJ7 .012 associe au Registre general des modifications

SN 601.A.007.009 -demiere edition.

Liste des

Cquipements requis pour certification:

Ref. DEP/YDA 6On4.

Liste des Cquipements : Ref. DEP/CRA N° 900n4.

(Ceue liste enumere tous les equipements autorises de montage sur l'avion)

2· INSTALLATIONMOTRICE

2·1 Moteurs

2 reacteurs a double flux JTI5D-4 fabriques par:

• UNITED AIRCRAFT OF CANADA LIMITED (U.A.C.L.) Certificat de Navigabilitt de Type Moteur M-IM 1 du 9 Mai 1974. -UNITED AIRCRAFT CORPORATION PRA IT AND WHITNEY AIRCRAFT DIVISION Certificat de Navigabilit.e de Type Moteur M-IM 2 du 7 Octobre 1974. Nota: On peut monter simultanement un reacteur de fabrication V.A.C.L. et un reacteur de fabrication P & W.quotesdbs_dbs18.pdfusesText_24

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