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 = '24A') 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 = '24A') 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 SA1639GLInstall air ambulance conversion.STC SA1670SWInstallation of engine thrust reversers.STC SA1RMInstallation of cargo restraint systemSTC SA2304SWReplacement of plunger type landing gear squat switch with rotary type switch.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 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 SA4059NMInstallation of emergency medical system.STC SA4060NMInstallation of emergency medical system.STC SA4218WEInstallation of Radio Corporation of America Primus-300SL Color Weather Radar System.STC SA4403NMInstallation of third attitude indicator that meets the requirements of FAR 121.305(j).STC SA4999NMInstallation of lifeport patient loading and support system.STC SA996EAInstallation of Shaw Aero fuel filler cap P/Ns 457-2, -266, -370, 431, -9R, -125, -1251.STC ST00016WIInstallation of Electric Floorboard HeatersSTC ST00098IBIntroduction of ADS-B OutSTC ST00361DEInstallation of Puritan Bennett or B/E Aerospace Sweep on 2000 or Zodiac Intertechnique EROS crew oxygen mask.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 ST01138DEInstallation of MidContinent MD23 standby altimeter and/or attitude indicatorsSTC ST01733WIInstallation of the Quiet Lear Hushkit or Avcon Noise SuppressorSTC ST01734WIInstallation of an Emergency Pneumatic Reservoir Assembly, EAS P/N 1260001-02STC ST01842SEInstallation of a Sandel Avionics Horizontal Situation Indicator (HSI) and Attitude Direction Indicator (ADI)STC ST01904CHInstallation of IS&S Air Data Display Units 9D-80130-15, Analog Interface Unit 9B-81040-30, and Rosemount model 0856NA pitot-static probes. Limited to Learjet 24 models with MKII wings, 300 kts Vmo airspeed limitation, and JET FC-110 autopilot. Excludes serial numbers 25-337, 25-352, 25-361, and 25-370 through 25-372.STC ST01930LAInstallation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI)STC ST01936WIInstallation of LED lightsSTC ST01946NYCockpit voice recorder replacement with Universal CVR 30B or CVR120.STC ST02004WIInstallation of the Garmin GI-275 Instantaneous Vertical Speed Indicators (IVSI)STC ST02016CHCertification for Reduced Vertical Separation Minimum (RVSM) operational capability. Excluding serial numbers 25-337, 25-352, 25-361, and 25-370 through 25-372.STC ST02097SEInstallation of replacement circuit boards for the FC-110 autopilotSTC ST02121CHCertification for Reduced Vertical Separation Minimum (RVSM) operational capability and installation of dual Honeywell AM-250 Altimeters and Rosemount model 0856NA Pitot-Static ProbesSTC ST02230SEThe installation of dual Garmin GTX-33ES Mode-S transponders and single or dual Garmin GTN 650/750 panel mounted navigation and global positioning system (GPS) units, or dual Garmin GTX-335R and/or GTX-345R Mode-S transponders and single or dual Garmin GTN 650/750/625/725 panel mounted navigation and GPS unitsSTC ST02265CHInstallation of Thrust Reverser Hydraulic System Modifications that were previously installed by STC SA1731SW, SA1669SW or SA1670SWSTC ST02316LAInstallation of a Crane Aerospace & Electronics Tire Sensor AssemblySTC ST02416SEInstallation of the replacement rate gyro, Butler National Part Number 501-1169-01 MOD A or 501-1169-02 MOD ASTC ST02417SEInstallation of the replacement stall warning vertical accelerometer, Butler National Part Number 02904001-101STC ST02472ATInstallation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIIISTC ST02500SEThe installation of the Garmin GDL-88 with the Flight Stream 210 to allow ADS-B(In) Flight Information Service Broadcast (FIS-B), independent of the ADS-B(Out) solution compliance.STC ST02635LAModification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B OutSTC ST02681AT-DInstallation of Cockpit / Cabin Blower AssySTC ST02893ATInstallation of a Boom Beam Taxi/Landing Light SystemSTC ST03132CHInstallation of a single or dual Collins TDR-94/94D Mode S Transponder using existing control head, aircraft wiring, and antenna(s)
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