N97UT
STCs that may be installed · 160
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do. In force first, then newest.
Query with SQL
duckdb -csv -c "SELECT m.matched_by, s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
FROM (
SELECT stc_number, min(side) AS side, arg_min(matched_by, side) AS matched_by, arg_min(matched_model, side) AS matched_model
FROM (SELECT stc_number, 1 AS side, 'airframe' AS matched_by, matched_model FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet' WHERE aircraft_model_code = '4220014'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '52200')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
ORDER BY m.side, 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 m.matched_by, s.stc_number, s.description, s.holder, s.status, s.status_date, m.matched_model
FROM (
SELECT stc_number, min(side) AS side, arg_min(matched_by, side) AS matched_by, arg_min(matched_model, side) AS matched_model
FROM (SELECT stc_number, 1 AS side, 'airframe' AS matched_by, matched_model FROM 'https://openairdocs.org/data/latest/faa_aircraft_model_stc.parquet' WHERE aircraft_model_code = '4220014'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '52200')
GROUP BY stc_number
) m JOIN 'https://openairdocs.org/data/latest/faa_stc.parquet' s USING (stc_number)
ORDER BY m.side, 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.
Airframe · Hawker Beechcraft B200GT
STC SA03025CHInstallation of weather research equipment and weather modification equipment for the purpose of modifying weather conditionsSTC SA04617NYInstallation of the Medivac Audio SystemSTC SA4175NMInstallation of fully enclosed main landing gear door system for high-flotation- gear-equipped aircraft.STC SA01861SEFabrication and installation of Landing Light ControllerSTC SA02279ATInstallation of a Boom Beam bulb, starter, and ballastSTC SA04837NYInstallation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lightsSTC SA04221CHInstallation of Thermal Acoustic KitSTC SA02133SEInstallation of a Luma Technologies LT-4500 Series Integrated Light\Emitting Diode (LED) Display Panel and LT-3500 LED light modulesSTC SA11302DSInstallation of the Pro Line Fusion embedded display system (EDS) latest version 3.7 software upgrade and additional factory optionsSTC SA03930NYInstallation of King Air Belly Payload MountSTC SA02017WIThe Installation of the Parker-Meggitt iPRESS™ SystemSTC SA03275CHInstallation of an antiskid brake systemSTC SA01638WIPart Fabrication and Installation of Arm Ledge System and Table Assembly for aircraft cabin interiorSTC SA11158SCDemonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS)STC SA01535WI-DInstallation of the Garmin G1000 Integrated Avionics System and GFC 700 Automatic Flight Control System and optional Electronic Stability and Protection (ESP)STC SA10965SCInstallation of upgraded hardware to the Rockwell Collins Pro Line 21 FMS-3000 to provide Localizer Performance with Vertical Guidance (LPV)STC SA11300DSUpgrade previously installed Collins Aerospace Radar AltimeterSTC SA00184LAInstallation of Alternate Main Landing Gear Tires, Michelin P/N 026-335-0.STC SA00400BOInstallation of an Autothrottle System (ATS)STC SA02738CHInstallation of L-3 Communications Avionics SystemsSTC SA11133SCInstallation of a Rockwell Collins Pro Line 21 update to include optional TAWS mode 5 warnings during LPV approaches, optional ADS-B Out, optional synthetic vision system (SVS), optional Communication Management Unit (CMU) and 3rd VHF to support Controller Pilot Data LinkSTC SA00416BOInstallation of an Outerlink Satellite Communications System (Satcom) and Flight Data Monitoring System KitSTC SA11855IBInstallation of the Flap Roller Bearing AssemblySTC SA02038WIInstallation of the Universal Avionics ClearVision and Enhanced Vision System (EVS) equipmentSTC SA01848WIModification of a Rockwell Collins Global Positioning System (GPS)STC SA02386AKReplacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systemsSTC SA00294BOInstallation of a Night Vision Goggle (NVG) compatible Lighting SystemSTC SA00322BOInstallation of a Supplemental Exterior Lighting SystemSTC SA02033WIInstallation of the SmartSky LITE System.STC SA04051CHCertification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D TranspondersSTC SA01615SEInstallation of winglets and related system changesSTC SA01050WIInstallation of Emergency Vision Assurance System (EVAS).STC SA00418BOInstallation of the Chelton Avionics, Inc. dba Canyon AeroConnect (Canyon) RT-7000 tactical radio systemSTC ST02752SEInstallation of the Starlink Aviation SystemSTC SA03316CHActivation of an 802.11 a/b/g/n WiFi SystemSTC SA02658SEInstallation of Garmin GI 275 Multi-Function Display SystemSTC SA2698NM-SInstallation of a set of Hartzell/Raisbeck Quiet Turbofan Propellers or Swept Turbofan PropellersSTC SA1783NMInstall Mark VI system.STC SA3366NMInstallation of the Ram Air Recovery System.STC SA3591NMInstallation of lower aft fuselage strakes.STC SA00120IBInstallation of the Universal Kapture Cockpit Voice Recorder (CVR) with Recorder Independent Power Supply (RIPS)STC SA11223DSInstallation of Litef s LCR-100N attitude and heading reference system (AHRS) on Rockwell Collins Fusion (EDS) on a Textron Aviation B200GT/B200CGT aircraftSTC SA11224DSRockwell Collins Pro Line Fusion phase 2 or 3 as installed in a Textron Aviation B200GT/B200CGT aircraft satisfies the airworthiness requirements necessary to support operational approval of Category II approach proceduresSTC SA11228DSInstallation of a Fuel Temperature Indication SystemSTC SA00103IBInstallation of Operator Console structural provisions onlySTC SA00104IBnstallation of Equipment Rack structural provisions onlySTC SA02010WIInstallation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD)STC SA02001WIInstallation of Structural OML ProvisionsSTC SA02372AKInstallation of the Max-Viz Enhanced Vision System (EVS) Model-1500 or 2300 Enhanced Vision System (EVS)STC SA757GLReplace existing Main Wheel and Brakes by installing Parker Hannifin Conversion Kit 199-125