Cessna 210G
STCs that may be installed · 318
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 ('2073430')
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.
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 ('2073430')
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_numberRun it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
STC SA4172NMInstallation of Aviation Development oil filter.STC SA01988SEInstallation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.STC SA01834CHInstallation of the High Intensity Discharge Light Assembly Kit.STC SA02319CH-DInstallation of a Hartzell HC-J3YF-1RF/F7691+2 propeller and C-4582-(P) spinner.STC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.STC SA02411CHInstallation of the Aero Vent Cabin Ventilation System.STC SA01473SEInstallation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote TranspondeSTC SA4005NMPrecise Flight Inc. Pulselite Control SystemSTC SA01205WI-DInstallation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors.STC SA03510ATInstallation of Hartzell Propeller Models PHC-C3YF-1RF/F8068, PHC-G3YF-1RF/F8068 or PHC-J3YF-1RF/F8068 (82 inch diameter 3-blade)STC SA01105WI-DInstallation of Bendix/King KMD 550/850 Multi-Functional Display System with optional traffic, terrain and weather sensors. This STC applies to both single-engine and small multi-engine aircraft (see 1 of 2 for small twin-engine).STC SA02446CHInstallation of the Courtesy Light Kit.STC SA6GLInstallation of Grimes strobe anti-collision lights.STC SA3659SWInstallation of Jetton Alert II alarm system.STC SA01695SEInstallation of an antennaSTC SA00402SEInstallation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed)STC SA639GLInstallation of a Shadin Company Fuel Flow Indicating System.STC SA01860NYInstallation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.STC SA00812CHReplace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun Visor Assemblies.STC SA01487SEInstallation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision.STC SA00680SEInstallation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.STC SA01328LAModification of right hand side door to provide an openable window.STC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.STC SA00161BOInstallation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.STC SA01157LAInstallation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument.STC SA02154AKInstallation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500.STC SA02217AKInstallation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL 90 UAT Master Data List, P/N 560-0278-01, Revision A, dated November 12, 2004, or later FAA approved revision.STC SA02007NYInstallation of SMR Technologies pneumatic deicer models.STC SA02655ATInstallation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft.STC SA01436SECockpit sunvisor retrofit kit.STC SA2456CEInstallation of fuel inlets and and caps. (210R S/N 21058819 THRU 21064950) (P210R S/N P21000001 THRU P21000867) (T210R S/N T210-0198 THRU 21064950)STC SA02795ATInstallation of a PXE7300SR, In-Flight Entertainment SystemSTC SA4473NMInstallation of Lompoc Aero Specialties inner plexiglass pane in swing out window frames presently employing a single window, in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4, 1983, together with their FAA sealed Installation Instructions dated September 20, 1982, or later FAA approved revisions. Manufacturer of the windows is controlled by Lompoc Aero Specialties drawings LAS 1012 dated August 6, 1982, LAS 1013 dated October 5, 1982, and LAS 1014 dated October 6, 1982, or later FAA approved sealed revisions.STC SA5467NMInstallation of acrylic window liners. (206 SERIES 402B0301 AND ON)STC SA2602NMInstallation of Precise Flight, Inc. 100 Series Speedbrake System in accordance with Precise Flight, Inc. Speedbrake Installation Drawing No. 210S006A, dated October 17, 1988, and Drawing List No. 210S008A, dated October 20, 1988, or later FAA approved revisions. Or Installation of Precise Flight, Inc. Speedbrake 2000 System in accordance with PreciseSTC SA10126SCInstallation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.STC SA01077SEInstallation of fluoropolymer film.STC SA00954SEInstallation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711, Report 106P, Revision B, dated August 2, 2001, or later FAA approved revision.STC SA2382NMInstallation of Aileron and Flap Gap Seals.STC ST01700NYInstallation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature Indicator, CHT-100 Cylnder Head Temperature INdicator, FL-100 Dual Fuel Level Indicator, FP-100 Fuel Pressure and Ammeter Indicator, OL-100 Oil Pressure and Temperature Indicator, and VA-100 Voltmeter and Ammeter Indicator.STC ST02547ATInstallation of a voice alert system.STC SA3696NMCockpit Sun Visor installation in accordance with FAA approved Rosen Drawing List Number RCS-00DL, dated December 17, 1986, or later FAA approved revisions.STC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA00709LAInstallation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required.STC SA5821NMInstallation of an electronic digital engine tachmoter, Model P-1000.STC SA2-1178Replacement of right front seat with stretcher.STC SA3728SWInstall vacuum pump cooling shroud.STC SA09952SCInstallation of Teledyne Continental Motors IO-550 engine.STC SA00941SEInstallation of vortex generators on wings and tail surfaces in accordance with Drawing Package MA2156, Revision IR, dated April 18, 2001, and Installation Manual MA2157, Revision IR, dated July 3, 2001, or later FAA approved revision to either of these documents. If more than five vortex generators are damaged or missing, the aircraft is not airworthy.STC SA09470SCInstallation of Starter Indicator light system.
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