Cessna 210M

STCs that may be installed · 355

In force first, then newest. The registry doesn’t record which STCs an aircraft has.

Query with SQL
duckdb -csv -c "SELECT s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
  FROM (
    SELECT stc_number, min(matched_model) AS matched_model
    FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet'
    WHERE aircraft_model_code IN ('2073450')
    GROUP BY stc_number
  ) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
  ORDER BY 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.

STC SA02768CHInstallation of Teledyne Continental Motors IO-520-A & -F (as modified by STC SE03704AT) or IO-550 F (as modified by STC SE03705AT) and Hartzell Propeller (P)HC-(C or J)3YF-1RF/F8468(B,K) 3 bladed metal propeller, or McCauley Propeller models D3A34C401/90DFA-() or D3A34C402/90DFA-()Vitatoe Aviation LLCSTC SA00606NYInstallation of O & N Aircraft Modifications low fuel warning device.Griggs Aircraft Refinishing LLCSTC SA01194NYInstallation of a Freon-Type electric motor driven Air Conditioning SystemGriggs Aircraft Refinishing LLCSTC SA1003NEConfiguration 1: Installation of an Allison 250-B17F Turboprop Engine (450Hp), (TCDS. E10CE) Hartzell HC-B3TF-7A/ T9212NK-2, Constant Speed reversing propeller, and, a 27.7 gallon Auxiliary Fuel Tank in the fuselage aft, baggage compartment. Configuration 2: Installation of a Rolls Royce Corporation, 250-B17F/2 engine (450Hp), (TCDS. E10CE). and Hartzell HCB3TF- 7A/T9212NK-2, Constant Speed reversing propeller.Griggs Aircraft Refinishing LLCSTC SA3753NMInstallation of stiffening ribs in the aileron and rudder surfaces and redistribution of the mass balance in the aileron, rudder and elevator surfaces.Griggs Aircraft Refinishing LLCSTC SA515NEInstallation of an aft baggage compartment auxiliary fuel tank and transfer system to the right wing tank.Griggs Aircraft Refinishing LLCSTC SA00353BOInstallation of an auto lean systemFlight Enhancements LLCSTC SA02276AKInstallation of AMSAFE Aviation Inflatable RestraintsAMSAFE Inc.STC SA00352BO PAGE 1Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),Avidyne CorporationSTC SA01734SEApplication of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.Andrew D. HumphreySTC SA00780SEInstallation of the True Lock Safety Retention Axle Lock Nut SystemTrue Lock LLCSTC SA01118WIInstallation of the Concorde FLA or VRSLA RG series batteriesConcorde Battery CorporationSTC SA09857ACInstallation of an ISTART Starting Enhancement SystemIStart Partners, Ltd.STC SA01816WIInstallation of an ADS-B compliant system, comprised of a Garmin GTX 330 Mode S Transponder and a Free Flight 1201 GPS receiver.Trego Dugan AviationSTC SA11172SCInstallation of an ADS600-B Automatic Dependent Surveillance-Broadcast (ADS-B) Universal Access Transceiver (UAT) and Global Positioning System (GPS) antennaNavWorx IncSTC SA00149BOInstallation of Aircraft Components, Inc. Volt and Vac Alert System, P/N 2044-1Aircraft Components IncSTC SA02547ATInstallation of a Voice Alert System.Aircraft Components IncSTC SA03658ATInstallation of a Voice Alert System to incorporate as primary annunciators for stall and gear warningsAircraft Components IncSTC SA02119SE PAGE 1Installation of Garmin GDL 88 ADS-B UAT Transceiver SystemGarmin International IncSTC SA01969SEInstallation of a Mid-Continent MD302 Standby Attitude ModuleMid-Continent Instruments and AvionicsSTC SA01107SERMD Aircraft Lighting high intensity discharge wingtip lightKnots 2U Ltd.STC SA3685NMInstallation of fiberglass wing tips; each tip having a 100 watt recognition light and a clear plastic lens.Knots 2U Ltd.STC SA01229SE PAGE 1Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radiosGarmin International IncSTC SA00172WIInstallation of TKS anti-icing system components, with placard stating 'Flight into known icing conditions is prohibited.'CAV Ice Protection IncSTC SA02442AK PAGE 1Approval of the L-3 Communications NGT 2000/2500 ADS-B systemADS-B Technologies, LLCSTC SA01933LA-D PAGE 1Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation SystemGarmin International IncSTC SA01669CHInstallation of Challenger Reusable Air FilterChallenger Aviation Products Inc.STC SA02930NYInstallation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 and 1200C model G4 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) InstrumentsInsight Instrument CorporationSTC SA2162NMInstallation of the Precise Flight stand-by vacuum system (SVS)Precise Flight IncSTC SA02283SE PAGE 1Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30PElectronics International Inc.STC SA02402SE PAGE 1Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30CElectronics International Inc.STC SA01744WIInstallation of an Induction Manifold Fuel Drain Line FilterHorsham Aviation ServicesSTC SA3531NMInstalling copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP)Bogert AviationSTC SA02121SEInstallation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic SystemGarmin International IncSTC SA00269BOInstallation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000.Avidyne CorporationSTC SA02717NY PAGE 1Installation of VoiceFlight Systems LLC VFS101 Speech Recognition ModuleVoiceFlight Systems LLCSTC SA02015SE-DInstallation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System.Garmin International IncSTC SA1305WEInstallation of Brittain Model PCA-1 Pitch Assist with Altitude HoldBrittain Industries, IncSTC SA245WEInstallation of Brittain/Clarkson AutopilotBrittain Industries, IncSTC SA469WEInstallation of Brittain Model PC-1 Pitch Assist and Model AH-1 Altitude Hold (optional)Brittain Industries, IncSTC SA662WEInstallation of Brittain Industries, Inc., Model B1-400 Hi-Lo Sensitivity AdaptorBrittain Industries, IncSTC SA1343WEInstallation of Brittain Industries Model B-4 Flight Control System.Brittain Industries, IncSTC SA618WEInstallation of Brittain Industries, Inc. Model B-4 Flight Control System, including PC-1 Pitch Assist, AH-1 Altitude Hold and NAV-1 Navigation CouplerBrittain Industries, IncSTC SA627WEInstallation of Brittain Industries, Inc. Model B-4 Flight Control System, including PC-1 Pitch Assist, AH-1 Altitude Hold and NAV-1 Navigation CouplerBrittain Industries, IncSTC SA674WEInstallation of Brittain Model B-4 Flight Control System including PC-1 Pitch Assist, AH-1 Altitude Hold and NAV-1 Navigation CouplerBrittain Industries, IncSTC SA1606WEInstallation of Brittain Industries B-4A Flight Control System.Brittain Industries, IncSTC SA1672WEInstallation of Brittain Industries Model B-5 Flight Control SystemBrittain Industries, Inc · Lists 210 SeriesSTC SA1887WEInstallation of Brittain Model NAV-2B Flight Control SystemBrittain Industries, Inc · Lists 210 SeriesSTC SA00432SEInstallation of EGT 701 series fuel flow instrument.J P InstrumentsSTC SA00861SEInstallation of J.P. Instruments (JPI) fuel flow indicating systemJ P Instruments
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