N414KB

STCs that may be installed · 402

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do. In force first, then newest.

Query with SQL
duckdb -csv -c "SELECT m.matched_by, s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
  FROM (
    SELECT stc_number, min(side) AS side, arg_min(matched_by, side) AS matched_by, arg_min(matched_model, side) AS matched_model
    FROM (SELECT stc_number, 1 AS side, 'airframe' AS matched_by, matched_model FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet' WHERE aircraft_model_code = '2075908'
      UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '17040')
    GROUP BY stc_number
  ) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
  ORDER BY m.side, s.status = 'Current' DESC, s.status_date DESC, s.stc_number"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

Airframe · Cessna 414

STC SA1867CEDC powered windshield installation. (421C EXCEPT 421C0801 THRU 421C1400)Wilco IncSTC SA2656SWAddition of Hydro Seal Fluid Additive to nose and main gear shock struts.Granville Lasseter/dba Granville's Aircraft Strut SealantSTC SA194RMNew slip joint exhaust manifold.Heliarc Welding Service Inc.STC SA2905SWInstallation of AVICON TZ1 fuel flow totalizer systemAvicon Development CorporationSTC SA2906SWInstallation of AVICON AF1 fuel flow processor.Avicon Development CorporationSTC SA2386SWInstallation of S.A.F.E., EGT, CHT Systems.Avicon Development CorporationSTC SA3682WEInstallation of Continental TSIO-520-N engine and associated installation components.Riley Aircraft CorpSTC SA1358CEChrome-plated brake disc installation.Engineering Plating & Processing, Inc.STC SA1393CEInstall forward baggage door warning system.Wells Aircraft, IncSTC SA109RMModify exhaust stacks by replacing existing bellows or seal type joints with a clampless sealess type slip joint.Heliarc Welding Service Inc.STC SA646CEInstall wing and tail pneumatic deice kit 702A on 401/402 aircraft(S/N 0135 and above), kit 702B on414 aircraft and kit 702C on 401/402 aircraft (S/N 0001 through 0134 only).Airborne Manufacturing CoSTC SA465SOInstallation of Bendix FCS-810 automatic flight control system including flight director indicator DH-841( ) and manual electric trim.Bendix Corporation Avionics DivSTC SA107GLConversion of oil lubricated de-ice pumps and related hardware to Airborne dry air pump 400 series conversion kits.Airborne Manufacturing CoSTC SA1040CEInstallation of AP-107 autopilot.Collins Aviation ServiceSTC SA732EAInstallation of radome Part No. 4004X.Norton Company, Performance PlacticsSTC SA584SOInstallation of Bendix YD-4 yaw damper system.Bendix Corporation Avionics DivSTC SA1642WEModification of exhaust system components.Wooley Tool & Mfg DivSTC SA3RMModification of engine exhaust stacks by replacement of expansion joint with slip fit joint.Heliarc Welding Svc IncSTC SA547SOInstallation of Bendix M-4D auto- matic flight control system in- cluding optional manual electric trim and optional flight director system in serial numbers 402B0301 and up, 4140351 and up, and421B0301 and up.Bendix Corporation Avionics DivSTC SA433SOInstallation of Bendix Model M4C flight control system.Bendix Corporation Avionics DivSTC SA536CEInstall electrical connectors in pressure bulkhead(s) at Station(s) 100 and/or 273.94.Peacock Charles OSTC SA780EAInstallation of Radome Kit No. 4004K-B for Bendix RDR-100 or RDR-110 series radar systems - 12-inch antenna.Norton CompanySTC SA3017WEInstallation of fuel flow instruments.Silver Instruments IncSTC SA00765DE PAGE 1Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensorPeregrineSTC SA02153LA-DInstallation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) SystemGarmin International IncSTC ST01085LAInstallation of the VNS 1000 Voice Navigation System.VNS IncorporatedSTC SA00281BO PAGE 1Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000Avidyne CorporationSTC SA02153LAInstallation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System.Garmin AT Inc.STC SA01933LAInstallation of Garmin Model 400W / 500W Series GPS-WAAS Navigation SystemGarmin AT Inc.STC SA5796SWInstallation of Alcor Tru-Flow indicating system, or SDI Hoskins fuel flow indicating system, or Silver Instruments Fueltron fuel flow indicating system.RAM Aircraft Limited PartnershipSTC SA01229SEInstallation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios.UPS Aviation TechnologiesSTC SA09971SCInstallation of Hartzell model PHC-C3YF-2UF/FC7693DF or PHC-C3YF-2UF/FC7693DFB propellers which are limited to aircraft previously approved to install 78-inch diameter props and have Tel Con Motors TSIO-520 series engines with maximum rated power from 285 hp to 350 hp. Also compatible with aircraft having TCM TSIO-520 engines modified by STC SE09261SC, SE09104SC, or SE4327SW for rated power increase.RAM Aircraft Limited PartnershipSTC SA09469SCModification of aircraft, and installation of Teledyne Continental Motors TSIO-520-NB engines, modified in accordance with STC SE09261SC or SE09104SC.RAM Aircraft Limited PartnershipSTC SA4535SWAuxiliary landing lights.RAM Aircraft Limited PartnershipSTC SA5998SWInstallation of Teledyne Continental TSIO-520-NB engines as modified by STC SE4327SW and Hartzell PHC-C3YF-2UF/FC7663D-2Q or PHC-C3YF-2UF/FC7663DB-2Q propellers. Airplane must be modified per STC SA48NW.RAM Aircraft Limited PartnershipSTC SA7570SWInstallation of Teledyne Continental TSIO 520-N or NB engine, modified by STC SE3714SW, installation of McCauley 3AF32C93/82NC or McCauley 3AF32C505/82NEA propellers and increased Maximum Takeoff Weight to 6510 pounds.RAM Aircraft Limited PartnershipSTC SA7633SWInstallation of Teledyne Continental Motors TSIOL-550-A 'Liquid-Cooled' engines. RAM winglets must be installed in accordance with STC SA4943SW. AFM 1031 dtd 8/10/89 required and must accompany this modification, except for aircraft concurrently modified with this STC and installation of Robertson Hi-Lift System with STC Sa892NM requires AFM 1081 dtd 3/29/96.RAM Aircraft Limited PartnershipSTC SA7984SWInstall Vortex generators on vertical stabilizer. Installation found to be compatible with STCs SA7570SW and SA4379SW.RAM Aircraft Limited PartnershipSTC SA8054SWInstallation of intercooler scoop.RAM Aircraft Limited PartnershipSTC SA8424SWIncrease the maximum takeoff weight to 6765 lbs. and maximum landing weight to 6430 lbs.RAM Aircraft Limited PartnershipSTC SA2350NMInstallation of Electronics International Inc digital carburetor/outside air temperature gauges listed on the attached continuation sheet and the associated accessories.Electronics InternationalSTC SA4379SW-DInstallation of Teledyne Continental TSIO-520-NB engines as modified by STC SE4327SW, and Hartzell PHC-C3YF-2UF/FC7663D-2Q or PHC-C3YF-2UF/FC7663DB-2 propellers or McCauley 3AF32C93/82NC-6.0 to-7.0 or 3AF32C505/82NEA-6.0 to-7.0 propellers.RAM Aircraft Limited Partnership

Engine · Continental TSIO-520 series

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