TCDS 1A3
STCs approved under this data sheet · 180
Current certificates first, most recently changed first.
Query with SQL
duckdb -csv -c "SELECT s.stc_number, s.description, s.holder, s.status, s.status_date FROM 'https://openairdocs.org/data/latest/faa_stc.parquet' s WHERE s.stc_number IN (SELECT stc_number FROM 'https://openairdocs.org/data/latest/faa_stc_model.parquet' WHERE tcds_number = '1A3') 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 FROM 'https://openairdocs.org/data/latest/faa_stc.parquet' s WHERE s.stc_number IN (SELECT stc_number FROM 'https://openairdocs.org/data/latest/faa_stc_model.parquet' WHERE tcds_number = '1A3') ORDER BY s.status = 'Current' DESC, s.status_date DESC, s.stc_number
Run 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 SA2557NMInstallation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring 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 SA01860NYInstallation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.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 SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.STC SA2683NMInstallation of Precise Flight, Inc. stand-by vacuum system (SVS)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 SA02795ATInstallation of a PXE7300SR, In-Flight Entertainment SystemSTC SA8075SWInstallation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER)STC SA10126SCInstallation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.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 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 SA798WEInstallation of George M. Adams DGA-2000 or Bodell BMI-2000 Wheel Assemblies in lieu of Firestone DFA180 wheel assembly. Firestone CFA252 brakes or Bodell BMI252brakes required with this installation.STC SA1008WEInstallation of Poly-Fiber covering material.STC ST02547ATInstallation of a voice alert system.STC SA00695SEReplacement of certain Rotomaster and Rayjay scavenge pumpsSTC SA489EAInstallation of ARP Inc. carburetor ice detection systemSTC SA02520ATInstallation of M-20 Oil Separator, model 600-WP.STC SA09145AC-DInstallation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-615,STC SA09470SCInstallation of Starter Indicator light system.STC SA09367AC-DInstallation of S-TEC system 30 alt altitude hold system, Model ST-819.STC SA09365AC-DInstallation of S-TEC system 20/30 single and two axis automatic flight guidance systems, Model ST-818-20/30.STC SA5925NMInstallation of oil pressure/temperature instrument.STC SA5924NMInstallation of RPM instrument.STC SA157NEInstallation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent.STC SA666NWInstallation of Teflon control yoke bail or control yoke bushings.STC SA00061LAInstallation of JPI digital tachometer.STC SA00238SEInstallation of Aviation Development Corporation's sump mounted chip detectorSTC SA00215NYInstallation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system.STC SA8431SWInstallation of R15VON alternator control unit.STC SA5926NMInstallation of manifold pressure instrument.STC SA5159NMInstallation of chip detector system.STC SA2844CEInstallation of a plastic cap enclosure over the anti-collision strobe light system.STC SA6031SW-DInstallation of S-TEC System 60 two axis automatic flight guidance system, Model ST-151, with optional automatic electric trim system.STC SA6035SW-DInstallation of S-TEC manual electric trim system, Model ST-273.STC SA6032SW-DInstallation of S-TEC System 60 pitch stabilization system, Model ST-152, with optional automatic electric trim system.STC SA6033SW-DInstallation of S-TEC System 60 single axis automatic flight guidance system, Model ST-150.STC SA6034SW-DInstallation of S-TEC System40/50, single and two axis automatic flight guidance systems, Model ST-216-40/50.STC SA1196SWInstallation of Mitchell automatic flight system model AK309 consisting of Century I, automatic aileron stabilizer with omni tracker.STC SA981SWInstallation of Manual Electric Trim AK276.STC SA808SWInstallation of Mitchell Model AK246 omni-tracker. Applicable only to aircraft modified by STC SA615SW.STC SA869SWMitchell automatic flight system AK233 consisting of Century III autopilot with optional automatic pitch trim, aileron stabilizer, radio coupler, glide slope coupler.STC SA645SWInstallation of Mitchell Automatic Flight System AK215 consisting of Century II Autopilot with optional automatic aileron stabilizer and radio couplerSTC SA1351WEReplace existing fabric on wings, fuselage, empennage, and/or control surfaces, with Ceconite101 material. (262A Series -12)STC SA334SWInstallation of InterAv Alternator.STC SA294GLInstall Cleveland wheel 40-97A and brake 30-63A.
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