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 model_key = '25D') ORDER BY s.status = 'Current' 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 model_key = '25D') ORDER BY s.status = 'Current' 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 SA01213CHInstall air ambulance conversion in accordance with Spectrum Aeromed Inc. Drawings as listed on AML SA01213CH, or later FAA approved revision.STC SA01452CHInstallation of an air ambulance conversion kit.STC SA1170CEStretcher installation in cabin area.STC SA1170GLExcept Model 55: Install Egan Aviation air ambulance stretcher P/N 125 using installation kit P/N 803, inverter/pump kit No. 808, 809, or 810. For Model 55, install air ambulance stretcher P/N 125 using installation kit P/N 804, medical oxygen system kit P/N 807, inverter/pump kit No. 808, 809, or810.STC SA1489CERemoval of 24-inch wide executive door and installation of 36-inch wide cargo door per AVCON Drawing List 36000 stamped FAA Approved with a date of May 8, 1979, July 3, 1980, November 15, 2010, or later approved revision for Learjet Models 25, 25A, 25B, 25C, 25D, 25F, 28, 29, 31, 31A, 35, 35A, 36, and 36A.STC SA1639GLInstall air ambulance conversion.STC SA1670SWInstallation of engine thrust reversers.STC SA2622NMInstallation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101)STC SA2661SWInstallation of Ray Model 7507A battery monitoring systemSTC SA2726SWInstallation of 6-pole rotary squat switches.STC SA2788SWInstallation of tail-stringer antenna housing.STC SA2876WEInstallation of vertical tail floodlights on the horizontal stabilizer.STC SA30GLInstallation of electronic engine synchronizer system.STC SA3249WEInstallation of dual Collins ADF Systems.STC SA3264WEInstallation of Global GNS-500A VLF navigation system.STC SA3328WEInstallation of flight data recorder Sundstrand Model FA542.STC SA3899WEInstallation of Collins F1S-84 Flight Instrument System.STC SA4053NMInstallation of emergency medical system.STC SA4060NMInstallation of emergency medical system.STC SA4218WEInstallation of Radio Corporation of America Primus-300SL Color Weather Radar System.STC SA4399NMInstallation of high frequency radio communications system.STC SA4403NMInstallation of third attitude indicator that meets the requirements of FAR 121.305(j).STC SA4433NMInstallation of communication and navigation systems electronic controls.STC SA4434NMInstallation of Wulfsburg Flitefone.STC SA4435NMInstallation of an emergency locator transmitter.STC SA4436NMInstallation of Flight Instrument System.STC SA4918SWInstallation of windshield defog system.STC SA4999NMInstallation of lifeport patient loading and support system.STC SA900NW: Installation of the Mark II performance system, including recontoured wing leading edge, recontoured flap leading edge, wing vortex generator removal, installation of wing stall strips and other minor refinements in accordance with Avcon Master Drawing List No. 1086 dated November 16, 2010, or later FAA approved revision. An FAA approved Airplane Flight Manual Supplement is required for each model.STC SA944NWInstallation of the XR Drag Reduction SystemSTC ST00016WIInstallation of Electric Floorboard HeatersSTC ST00098IBIntroduction of ADS-B OutSTC ST00226BOInstallation of Honeywell CAS-67A Airborne Collision Avoidance System (ACAS II) with dual MST-67A Mode S Transponders and copilot's Intercontinental Dynamics Corporation encoding altimeter with Static Defect Correction Module.STC ST00347BOModification to upgrade a BendixKing CAS 67A TCAS II system to CAS 67B TCAS II Change 7.1STC ST00361DEInstallation of Puritan Bennett or B/E Aerospace Sweep on 2000 or Zodiac Intertechnique EROS crew oxygen mask.STC ST00373BOInstallation of Rockwell Collins TDR-94D Transponders with ADS-B OutSTC ST00432WIInstallation of Avcon fins(Aft Body Strakes).STC ST00462LAModification of the engine exhaust system.STC ST00578DEReduce number of passenger seats installed from 8 to 4 passengers.STC ST00673WI-DModification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System installation.STC ST00682WI-DModification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation in accordance with Collins Installation Instructions as listed on AML No. ST00682WI-D, Revision -, or later FAA approved revisions.STC ST00738WIIncreased service life. Data required.STC ST00790DEInstallation of BendixKing CAS 67B Traffic Alert and Collision Avoidance System (TCAS) II Version 7.1STC ST00814WILanding Gear Life Extension.STC ST00835DEInstallation of Automatic Dependent Surveillance - Broadcast (ADS-B) Out and In functionality using the Garmin GTX 335R and GTX 345R Transponders plus qualified position sensorSTC ST00999WIInstallation of Special Mission Power and Control Wiring, provisions for Carriage of Mission Stores with
Hardpoints installed by STC SA1604SO or SA1670CE, and Takeoff weight increased to 16,300 lbs.STC ST01138DEInstallation of MidContinent MD23 standby altimeter and/or attitude indicatorsSTC ST01142WI-DModification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92E control head.STC ST01195WIInstallation of Rosemount Pitot/Static Probes, altimeters, and associated equipment in Learjet 20 series aircraft to obtain Reduced Vertical Separation Minimum approval.STC ST01271WIInstallation of IS&S Air Data Computer System Update with Rosemount Static Probes and associated equipment in Learjet series aircraft to obtain Reduced Vertical Separation Minimum approval.
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