What it approves
Installation of dB Partners Engine Exhaust Suppressor and Ejector Assemblies
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
tatuofmr&a rparnntnt of ransporttion-5dtraf tiiationdniinistration ¯ upp1enintaLettJpLZiti1katt /'iflh SA573ONM dBPartners * * * SeePage3 ofthisSTCfortheCertificationBasis.
Al6WE .4Ae': Boeing ,. 737-200and737-200CSeries Installatior'I'ofdBPartne"EngineExhaustSuppressorandEjectorAssemblies inaccordancewithFAAapproveddBPartnersMasterDrawingListDocument No.NDER-9102RevisionC,datedJune18,1992,orsubsequentFAAapprovedrevisions theretofortheModel737-200& 737-200CSeriesAircraft.
ThelimitationsandconditionsofTypeCertificateA16WEapplyexceptas outlinedinpages3 through5 ofthisSIC..A copyofthisSTCmustbe includedinthepermanentrecordsofeachaircraftmodifiedinaccordance withthisSTC. Approvalofthischangeintypedesignappliestothe BoeingModel737-200& 737-200CSeriesaircraftthatareotherwise unmodified.Thisapprovalshouldnotbeextendedto aircraftofthis modelonwhichotherpreviouslyapproved(SeeContinuationSheet) U fl' Id+4 "' April18,1990 _-", i.¯ June26,1992 .
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- (SignaturØ,/ Manager,Seattle'Aicraft CertificationOffice,ANM-100S (Title) Any alterationof this cer4Jica1eis punishableby a lineof not exceeding$1,000,or imprisonmentnot exceeding3years, or both.
This certificatemay be transferredin accordancewith FAR 21.47.
AA 8110-2(10-68)
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partnitntof ransportation-jdtrt iationdminitration *uppkmtntatijpt rt1fiau Q!ont1nuat1anhet) SA573ONM modificationsareincorporatedunlessitisdeterminedthattherelationshipbetween thischangeandanyofthoseotherpreviouslyapprovedmodifications,including changesintypedesign,willintroducenoadverseeffectupontheairworthinessof thataircraft.
I - Boeing737-200and737-200CSeriesasmodifiedby thisSIC Engine Ratings: P&WJT8D -9, -9A -15,-15A-17,-17A Takeoff(Normal)static thrust,standardday,sea levelconditions,(5mm.)
pounds. 14,500 15,500 16,000 Maximumcontinuousstatic thrust,standardday,sea levelconditions,pounds 12,600 13,750 15,200 ForengineoperatinglimitationsseeEngineTypeCertificateDataSheet E2EAfortheJT8D-9,-9A,-15,-15A,-17,and-17AortheFAAapproved dBPartnersAirplaneFlightManualSupplement(seeNote2).
Thrust Setting: TheAppropriateEPRorNiThrustSettingCurve,intheFAAapproveddB Partners Airplane Flight Manual Supplement or Airplane Flight Manual Appendicesmustbeusedforcontrolofenginethrust.
Eligible Serial Numbers: AllBoeingModel737-200& 737-200CSeriesSerialNumbersshownon AircraftTypeCertificateDataSheetA16WE.
Certification Basis: Forunmodifiedsystemsandstructures,thesameasshownonType CertificateDataSheetA16WEfortheModel737-200& 737-200CSeries.
S Any alterationof thiscertificateis punishableby aflne of notexceeding51,000,or imprisonmentnotexceeding3 years,or both.
FAA FORM 8110-2-1 (10-69) This certificatemaybetransferredin accordancewith FAR 21.47.
PAGE 3o 5PAGES FAAAC8203578
¶lntttd tatrsof mtrfca S 3tpartmntof ransportation-JdraItiation.dminiEration *uppIonntaLtjp rtiIkat (Zont1nuat1onht) SA573ONM Forneworextensivelymodifiedsystemsandstructures,thesameas shownonTypeCertificateDataSheetA16WEfortheModel737-200& 737-200CSerieswhichincludesPart25asamendedbyAmendments25-1 through25-3,25-7,25-8,and25-15,exceptwheresupersededbythe followingsectionsofPart25asamendedbyAmendment25-1through:
25-23(Section25.934Turbojetenginethrustreversersystemtests).
25-63(Section25.25,WeightLimits) Part36 oftheFederalAviationRegulationsthroughAmendment36-17.
Part34oftheFederalAviationRegulations.
S Production Basis: None Required Equipment: Thebasicequipmentasprescribedintheapplicableairworthiness regulationsmustbeinstalledintheaircraft.
Service Information:dBPartne ReportD6 airplanes bulletins statement rsStructuralRepairManualSupplement(NDER-65ND04)to Boeing -15565isFAAapprovedandisapplicableto allModel737 modifiedinaccordancewiththisSTC. dBPartnersservice andotherserviceinformation,whenFAAapproved,willcarrya tothateffect.
Note1. TheWeightandBalanceControlandLoadingManualD6-15066,together withtheSupplementAircraftReportapplicableto thespecificModel Designation,mustberevisedto showtheinstallationofthisSTC includingalistofequipmentincludedinthecertificatedemptyweight andloadinginstructions.TherevisedWeightandBalanceControland LoadingManualmustbeineachaircraftatthetimeoforiginal certificationandatalltimesthereafter,exceptinthecaseof opetors havinganapprovedweightcontrolsystem.
S Any alterationof thiscertificateispunishablebyafine of notexceeding51,000,or imprisonmentnotexceeding3 years,or both.
FAA FORM 8110-2-1 (10-69) Thiscertfwatemaybetransferredin accordancewith FAR 21.47.
PAGE 40F5PAGES C FAAAC8203578
i InIttd%tatrsof mnica .
3partiututof ransportation-jtdtra1tiiatIon.dininistration *uppkmntaLtjp &rtilkau (tontinuationht) SA573ONM Note2. Model737-200& 737-200CAdvancedairplaneoperationmustbein accordancewiththeFAAapproveddBPartnersAirplaneflightManual SupplementNDER-9200.XXXA.Model737-200& 737-200CNon-advanced airplaneoperationmustbeinaccordancewiththeFAAapproveddB PartnersAirplaneFlightManualSupplementNDER-9201.XXX.The.XXXwill reflectthesameBoeingModelDesignationnumberassignedto the existingFAAapprovedBasicAirplaneFlightManualsuchas.230and .2L9. EachFAAapprovedAFMSupplementliststheApplicableAppendices andairplaneSerialNumbers.AllplacardsrequiredineithertheFAA approvedAFMSupplement,theapplicableoperatingrulesorthe certificationbasismustbeinstalledintheairplane.
Note3. RequiredstructuralinspectionsforallModelsofthe737modifiedin accordancewiththisSTCarecontainedinthedB PartnersMaintenance Programprovidedto eachoperator.
Note4. Informationessentialtothepropermaintenanceofaircraftmodifiedin accordancewiththisSTCiscontainedinthedBPartnersSupplementto theBoeing737MaintenanceManual,documentnumberNDER-65ND02.
Note5. ThedB PartnersModeldesignationforairplanesmodifiedinaccordance withthisSTCis"B737-200HushKit".Thismodeldesignationappearson theFAAapproveddBPartnersAirplaneFlightManualSupplements(see Note2),OperationsManualSupplement(NDER-65ND05),StructuralRepair ManualSupplement(NDER-65ND04),MaintenanceManualSupplement (NDER-65ND02),IllustratedPartsCatalog(NDER-65ND03),andallother servicedocuments.ThesedocumentsarepreparedbyNORDAM,asanagent ofdBPartners.Thismodeldesignationdoesnotalterorreplacethe originalboeing737-200or737-200CSeriesmodeldesignations.
Note6. Pratt& WhitneyJT8DServiceBulletinsNumber5950fortheRespaced InletGuideVanes,Number5947fortheFanandExhaustMixerSystemduct AssemblyandNumber6077fortheAftEngineMountmodificationmustbe incorporatedoneachengineinaccordancewiththeapplicable installationinstructionsconcurrentlywiththisSTCmodification.
- END - S Any alterationof thiscertificateis punishablebyafine of notexceeding$1,000,or imprisonmentnotexceeding3 years,or both.
FAA FORM 8110-2-1 (10-69) Thiscertjficalcmaybetransferredin accordancewith FAR 21.47.
PAGE OF PAGES C FAAAC82-03578
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.