Gates Lear Jet 36
STCs that may be installed · 186
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 ('5170601')
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 ('5170601')
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 SA2876WEInstallation of vertical tail floodlights on the horizontal stabilizer.STC ST00392DEInstallation of a bleed air extraction system control improvement.STC ST00410WIInstallation of a JetCorp Fuel Pump Monitor System.STC ST00450WIInstallation of extended wingtip fuel tanks and underwing storesSTC SA00179WIInstallation of pressure dome provision for an infrared scanner in the camera door.STC ST00016WIInstallation of Electric Floorboard HeatersSTC SA4918SWInstallation of windshield defog system.STC SA2580CEInstallation of Fairchild Model GA100 Cockpit Voice RecorderSTC SA2639CEInstallation of Universal Navigation system model CVR-80 cockpit voice RecorderSTC SA2618CEInstallation of a single global Wulfsberg GNS-500A series 5(Program version 5M) navigation system.STC SA2668CEInstallation of a Second Emergency Battery with associated wiring to connect Number 1 Communication, Navigation, Audio and Transponder.STC SA3264WEInstallation of Global GNS-500A VLF navigation system.STC SA2659CEInstallation of Fairchild 17M703-274-00 Flight Data RecorderSTC SA2658CEReplace JET FC-200 autopilot with JET FC-530 Autopilot per Learjet Inc Airplane Accessory Kit AAK 83-2. Interface existing Collins FIS-84 Flight Instruments and Global Navigation System, GNS-500A, Long-Range Navigation SystemSTC SA2655CEInstallation of optional Universal Navigation System (UNS) fuel flow circuitry to Navigation Management System (NMS) and Compact Flight Management System (Compact FMS).STC SA1209CEInstallation of a Litton LTN-104
Inertial Navigation/RNAV SystemSTC SA3249WEInstallation of dual Collins ADF Systems.STC SA3328WEInstallation of flight data recorder Sundstrand Model FA542.STC SA3703NMInstallation of dual Universal Navigation Corp. UNS-1A flight management systems.STC SA3899WEInstallation of Collins F1S-84 Flight Instrument 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 SA4413NMInstallation of cockpit voice recorder.STC SA4434NMInstallation of Wulfsburg Flitefone.STC SA4435NMInstallation of an emergency locator transmitter.STC SA4436NMInstallation of Flight Instrument System.STC SA2661SWInstallation of Ray Model 7507A battery monitoring systemSTC SA5713SWInstallation of single Tracor7800 Omega/VLF navigation system and B&D Instruments 2504 true airspeed system.STC SA2657SWModification of air conditioner motorSTC SA2861SWAddition of Hydro seal fluid additive to nose and main gear shock struts.STC SA766NWInstallation of Raisbeck Mark IV performance systemSTC SA2788SWInstallation of tail-stringer antenna housing.STC SA82RMInstallation of Sperry SPI 80/81 Flight Director System, interfaced with J.E.T. FC-200 Automatic Flight Control System.STC ST02893ATInstallation of a Boom Beam Taxi/Landing Light SystemSTC ST01122SEGroup aircraft approval for Reduced Vertical Separation Minimum (RVSM) are contained in AeroMech Document No. AMI-QD-LJ-0213 Rev. New, dated May 2, 2003, or later FAA-approved revisions.
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