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 = '25') 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 = '25') 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 SA00179WIInstallation of pressure dome provision for an infrared scanner in the camera door.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 SA01858AT-DInstallation of a BF Goodrich Avionics Systems, Inc. TCAS791/A TCAS I system.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 SA1746SWInstallation of Ray Electronics Model 7107 battery fault warning system.STC SA175RMReplacement of throttle knob, Model EP-004, for 20 series Learjet equipped with Dee Howard thrust reversers.STC SA1RMInstallation of cargo restraint systemSTC SA225NWInstallation 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.STC 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 SA2657SWModification of air conditioner motorSTC SA2661SWInstallation of Ray Model 7507A battery monitoring systemSTC SA2726SWInstallation of 6-pole rotary squat switches.STC SA2788SWInstallation of tail-stringer antenna housing.STC SA2861SWAddition of Hydro seal fluid additive to nose and main gear shock struts.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 SA3343NMCockpit Sun Visor installationSTC SA36NWInstallation of Sundstrand Ground Proximity Warning SystemSTC SA3899WEInstallation of Collins F1S-84 Flight Instrument System.STC SA4053NMInstallation of emergency medical system.STC SA4060NMInstallation of emergency medical system.STC SA4073NMMSN 25-014 Installation of emergency medical systemSTC SA412CEInstallation of Woodward Electronic Engine synchronizer 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 SA4435NMInstallation of an emergency locator transmitter.STC SA4999NMInstallation of lifeport patient loading and support system.STC SA639ALInstallation of Model EP-110 starter/generator decoupler system on Models 23, 24, 25 airplanes using Bendix Model30B-37 starter generators.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 SA996EAInstallation of Shaw Aero fuel filler cap P/Ns 457-2, -266, -370, 431, -9R, -125, -1251.STC ST00016WIInstallation of Electric Floorboard HeatersSTC 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 ST00462LAModification of the engine exhaust system.STC ST00550DEModification and installation of an optical glass in forward right hand passenger window.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.
Back to Learjet 25