Cessna 210A
STCs that may be installed · 331
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 ('2073408')
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 ('2073408')
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 SA02119SE PAGE 1Installation of Garmin GDL 88 ADS-B UAT Transceiver SystemSTC SA01969SEInstallation of a Mid-Continent MD302 Standby Attitude ModuleSTC SA00648SEFabrication of R.M.D. Aircraft Lighting, Inc., wing-tip and landing light Kit No. 00190-C.STC SA01107SERMD Aircraft Lighting high intensity discharge wingtip lightSTC SA3685NMInstallation of fiberglass wing tips; each tip having a 100 watt recognition light and a clear plastic lens.STC SA01229SE PAGE 1Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radiosSTC SA02442AK PAGE 1Approval of the L-3 Communications NGT 2000/2500 ADS-B systemSTC SA02049SEInstallation of Stene Aviation, Inc. Wing Tips with LED lightsSTC SA01933LA-D PAGE 1Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation
SystemSTC SA01669CHInstallation of Challenger Reusable Air FilterSTC 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) InstrumentsSTC SA10682SCInstallation of alternator and voltage regulatorSTC SA2162NMInstallation of the Precise Flight stand-by vacuum system (SVS)STC SA02283SE PAGE 1Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30PSTC SA02402SE PAGE 1Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30CSTC SA01744WIInstallation of an Induction Manifold Fuel Drain Line FilterSTC SA02121SEInstallation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic SystemSTC SA01380CHInstallation of wing fuel tank quick valve drains.STC 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.STC SA02717NY PAGE 1Installation of VoiceFlight Systems LLC VFS101 Speech Recognition ModuleSTC SA02015SE-DInstallation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System.STC SA00897CHInstallation of Domed (Bubble) WindowSTC SA1305WEInstallation of Brittain Model PCA-1 Pitch Assist with Altitude HoldSTC SA245WEInstallation of Brittain/Clarkson AutopilotSTC SA469WEInstallation of Brittain Model PC-1 Pitch Assist and Model AH-1 Altitude Hold (optional)STC SA662WEInstallation of Brittain Industries, Inc., Model B1-400 Hi-Lo Sensitivity AdaptorSTC SA1343WEInstallation of Brittain Industries Model B-4 Flight Control System.STC SA618WEInstallation of Brittain Industries, Inc. Model B-4 Flight Control System, including PC-1 Pitch Assist, AH-1 Altitude Hold and NAV-1 Navigation CouplerSTC SA627WEInstallation of Brittain Industries, Inc. Model B-4 Flight Control System, including PC-1 Pitch Assist, AH-1 Altitude Hold and NAV-1 Navigation CouplerSTC SA674WEInstallation of Brittain Model B-4 Flight Control System including PC-1 Pitch Assist, AH-1 Altitude Hold and NAV-1 Navigation CouplerSTC SA1606WEInstallation of Brittain Industries B-4A Flight Control System.STC SA1672WEInstallation of Brittain Industries Model B-5 Flight Control SystemSTC SA1887WEInstallation of Brittain Model NAV-2B Flight Control SystemSTC SA00432SEInstallation of EGT 701 series fuel flow instrument.STC SA00861SEInstallation of J.P. Instruments (JPI) fuel flow indicating systemSTC SA1471WEInstallation of Brittain Industries Model CSA-1 Stability Augmentation SystemSTC SA1527WEInstallation of twelve gallon auxiliary fuel tank in each wing inboard of tip.STC SA1618WEInstallation of Brittain Industries, Inc. Model B2C Flight Control SystemSTC SA01026SEImproved fuel gascolator assembly.STC SA02825NY PAGE 1Installation of Aerospace Logic Aircraft InstrumentsSTC SA01692SEInstallation of a Garmin GMX 200 Multi-Function DisplaySTC SA03148NYThe installation of the Latitude Technologies Corporation S100 Tracking SystemSTC SA2067NMInstallation of BAS, Inc. TSO Shoulder Harness and BAS Inc. Harness SystemSTC SA02016SE-DInstallation of Garmin GTS 800, GTS 820 or GTS 850 Traffic SystemSTC SA1230GLInstall SAF-T-STOP auxiliary seat stop device.STC SA5156NMFabrication and installation of Pulsar-MOSFET Landing Light Flasher SystemSTC SA01487SE-DInstallation of a GDL 69 or GDL 69A XM Satellite ReceiverSTC SA00281BOInstallation 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 700-00165-000STC SA02434NYInstallation of a Digital Engine Monitoring system.STC SA957SWInstallation of Plane Booster Kit 101-C 1000 in accordance with Upper Valley Drawing 101-24250-6, dated January 10, 1965, and Installation Instructions, Revision 2, dated June 3, 1968.
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