# STC SR11337SC - Type: Supplemental type certificate - Status: Current, Issued - Holder: S-TEC Corporation - Description: Installation of an S-TEC Single/Dual Pilot instrument Flight Rules (JER) HeliSAS Stability Augmentation System and Autopilot - Status date: February 14, 2019 - Data sheets: H13EU - Certificate PDF: https://openairdocs.org/files/sha256/ef/e6/efe644f4e399375fcced8b59bd633e3029f0510ae4f722d7f6bad17ae8db3fbc - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105804518520230518132607.0001 - Page: https://openairdocs.org/stc/SR11337SC ## ADs that name it None. ## Approved models (1) - Airbus Helicopters Deutschland GmbH MBB-BK 117 C-2 (TCDS H13EU) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. S Vnitet[Statesoffimerica (Departmentofctransportation 4 cFeiera(fiviationj4iministratjon Supp(ementa(TypeCertficate gs1um5er:SV1337SC ThiScartflcateissueeIto:S-TECCorporation OneS-TecWay MineralWells,Texas76067-9236 certifiesthatthec/langeinthetypeiesignforthefolT[owingproifuctwit/Itiletmitationsanc[cond?tionsthereforeas specifielfiereonmeetstheairworthinessrequirementsof(Part 29oftilecFederatJ4viation(Pgu[ations.*Cyation 6asisis setfort/Iin¶ljipeCertificate(Data SheetT(YDSJ-(13V. OriginalProduct- TypeCertificateNumber:HI3E1.J 'DescriptiDuof23'pe'DesignCfiange Make: AirbusHelicoptersDeutsehiandGmbH Model: MBB-BKI17C-2(e)(ECl45e) Installationof anS-TECSingle/DualPilotinstrumentFlightRules(JER)HeliSASStabilityAugmentationSystemand AutopilotinAirbusHelicoptersDeutschlandGmbl-lmodelMBB-BKI17C-2(e)(ECI45e)inaccordancewithFAAApproved MasterDataList,ST-956-MDL-0001, RevisionCdatedFebruaryii, 2019, orIaterFAAApprovedRevisions. Linritationsare!Conditions: II.Theinstallationshouldnot beincorporatedinanyaircraftunlessitis determinedthattheinterrelationshipbetweenthis installationandanypreviouslyapprovedconfigurationwillnot introduceanyadverseeffectupontheairworthinessofthe aircraft. 2. Theapprovalofthismodificationappliesto theabovenotedrotorcraftmodelonly. (Seecontinuationonpage3) Thiscart!flcateanitfie supportingdztawfiic/Iis tilet5asisforapprovaf s/la([remainineffictunti[sui'renc[ered suspendTedanIrevo&eIoratermination&iteisotherwiseesta6[zsfie16ythe14ImmistratoroftheTedera(J4viation J4dministrat1on. Dateof Application:July28, 2016 DateReissued: Dateof issuance:February14,2019 DateAmended: (By®irectionofIimijtis1jrator Signature .... - - czit1S.Fnce'Gix Manager,DSO Branch17iO>çomplianceandAirworthiness Division,AircjaltCertificationService Any alterationof thiscertificateis punishablebya line of not exceeding$1000, or lrnpilsonment noteeeding 3 years,orboth.Thiscertificatemaybe transferredormadeavailableto thirdpersonsby licensingagreements in accordancewith14CFR21.47.Possessionof this SupplementalType Certificate(STC)documentby personsother alan the STCholderdoesnotconstituterightsto thedesigndatanorto alteranaircraftaircraftengine,or propeller. The STCs supporting documentation(drawings,instruolions,spedficatiOns,eightmanualsupplements,eto.) is the property of the STC holder, An STe holder who allows a personto usetile STC to alter anaircraftaircraft engine, or propeller must provide that personwith written permissionacceptableto theFM. (Ref.14 CFR21.120). FAA Form8110-2(6114) Page 1 of 4 S rUniteiStatesofmerka (Departmentofransportation Fe6era(J4viationj4éministration Suppkmenta(TypeCertflcate LimitationsaniConditions(cont) 3. Iftheholderagreesto permitanotherpersonto usethiscertificateto altertheproduct,theholdershallgive theother personwrittenevidenceofthatpermission. 4. FAAacceptedInstructionsforContinuedAirworthiness,ST-956-ICA-0001,Revision-,datedDecember3, 2018or laterFAAapprovedrevisionsmust bemadeavailableto theoperator at thetimeof installation. 5. FAAapprovedRotorcraftFlightManualSupplement,ST-956-RFMS-0001,Revision-,datedFebruary 13,2019or laterFAAapprovedrevisionsisrequiredonboardthemodifiedrotorcraft. 6. Thisinstallationmust be installedconcurrentlywiththefollowing:a) STCSR02482AKas amendedFebruary 14,2019; andb) a [minimumj24yDC, 40 Amperehourbattery forbackupelectricalpowerto beeligibleforInstrumentFlight Rules(IFR)flightoperations. Cerification(Basis: Basedon14CFR§ 21.115and21.101,andtheFAApolicyforsignificantchangesinFAAOrder8110.48,the certificationbasisfortheAirbusHelicoptersDeutschlandCixnbHMBB-BK117C-2(e)(EC145e)is asfollows: a. Thetype certificationbasisforparts not changedornot affectedbythechangeisshowninTCDSH13EIJ. b. Themodificationcertificationbasisforparts changedor affectedbythischangesincethereferenceapplication dateJuly28,2016,isbaseduponPart29andPart29 AppendixB withspecificamendmentsasbelow: 14CFRPart29 Amdt 14CFRPart29 Amdt 29.1 39 29.561(a)(b) 38 29.21(a) 24 29.601 0 29.29 15 29.603 17 29.31 0 29.605(a) 17 29.141 24 29.607 5 29.143 51 29.609 0 29.151 24 29.610 53 29.161 24 29.611 0 29.171 0 29.613 30 29.173 51 29.623 0 29.175 51 29.671(a)(b) 24 29.181 24 29.672 24 29251 0 29.674 30 29.301 0 29.681(b) 0 29.303 0 29.683 0 29.305 0 29.685 12 29.307(a) 30 29.771 24 29.321 0 29.773(a) 3 29.337(a) 30 29.777(a) 0 29.395(b)(3) 300 29.1301 0 Any alterationof thiscertificateis punishableb aTineof notexceeding$1,000,orImprisonmentnotexceeding3 years,orboth.Thiscertificatemaybe transferredor madeavallabieto thirdpersonsby licensingagreementsInaccordancewith 14 CFR21.47.PossessionorthisSuppiementaiType Certificate(STC)documentby personsotherthan the STCholderdoes rot Constituterights to the design datanorto alteran aircraft,aircraft engine, or propeller.The STC's supporting documentation(drawings,instructions,specifications, flight manualsupplements,etc.) isthe property of the STC holder.An STCholderwhoallowsapersonto usethe STCto alteranaircraft,aircraftengine, orpropellermust providethat personwithwritten permissionacceptableto theFAA..(Ref.14 CFR21.120). FAAForm8110.2 (5/14) Page3of 4 CertificationWasis(csnt Vnitei Statesoffimerica (DepartmentofTransportation Teiera(J4v1ationJ41ministration SuppiementatTypeCertflcate Amdtl4CFRPart29 Anidt I4CFRPart29 29.1309 53 29.1505 24 29.1316(a) 53 29.1519 0 29.1317(aXb)(c) 49 29.1523 0 29.I322(c)(d) - 12 29.1525 24 29.1329 42 29.1527 15 29.1351(a) 42 29.1529 20 29.1353(a) 15 29.1541 0 29.1357(a)(b)(c)(d) 24 29.1581(a)(bXd) 15 29.1501 15 29.1583 24 29.1503 0 29.1585 24 t4CFRPart29 I4CFRPart29 AmdtAppendixB Amdt AppendixB 29 App B 1 21 29App B VI J 21 29AppB11 21 29AppB Vii ] _ 51 _ 29AppB11i 21 29AppB VIII I 40 29AppB1V _ 21 _ 29AppB1X 21 29AppBV 21 - -END-- Any alterationof this certificateis punishable by a fine of not exceeding 51.000, orimprisonmentnot exceeding 3 years,or both.Thiscertificatemay be transferredorrnadeavailableto thirdpersonsby licensing agreements InaccordancewIth14 CFR21.47.PossessionofthisSupplementalType Certificate(SIC) documentbi personsotherthantheSIC holderdoesnotconstitutenghtsto thedesigndatanorto alteranaircraft,aiTcraftengine,or propeller.The STCs supporting doctJmentation(drawings,instructions,specifications, flight manualsupplements,etc.) IsthepropertyoftheSIC holder.An SIC holderwhoallowsa personto usethe STCto alteranaircraft,aircraftengIne,orpropellermust provIdethatpersonwith written permissionacceptabletothe FAA.(Ref. 14CFR21.120). FAA Form 8110-2 (5/14) Page4 of 4 ## Every issue (1) - February 14, 2019: Issued, Current. [certificate](https://openairdocs.org/files/sha256/ef/e6/efe644f4e399375fcced8b59bd633e3029f0510ae4f722d7f6bad17ae8db3fbc) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.