# STC SA5730

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: dB Partners
- Description: Installation of dB Partners Engine Exhaust Suppressor and Ejector Assemblies
- Status date: June 26, 1992
- Data sheets: A16WE, A16WE
- Certificate PDF: https://openairdocs.org/files/sha256/95/00/950069dc08bf6217dffa116f1c2b420312dfa556d39b6e1c2c6159ece678aaca
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141210649620231205155734.0001
- Page: https://openairdocs.org/stc/SA5730

## ADs that name it

None.

## Approved models (2)

- The Boeing Company 737-200 Series (TCDS A16WE)
- The Boeing Company 737-200C Series (TCDS A16WE)

## 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.

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)

%nlttdtatts of mntco .

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**

## Every issue (1)

- June 26, 1992: Issued, Current. [certificate](https://openairdocs.org/files/sha256/95/00/950069dc08bf6217dffa116f1c2b420312dfa556d39b6e1c2c6159ece678aaca)

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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.