N201BR
STCs that may be installed · 243
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 = '2730107'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '01517')
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 = '2730107'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '01517')
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 · Dassault-Breguet MYSTERE FALCON 20-C5
STC SA7321SW-DInstallation of the Collins traffic alert and collision avoidance (TCAS II) system.STC SA7273SW-DInstallation of the mscellaneous antennas.STC SA7297SW-DInstallation of the auxiliary radio rack.STC SA977GL-DRelocation of the exhaust oulet for the microturbo Saphir auxiliary power unit.STC SA1851WEInstallation of a single point pressure fueling system.STC SA974GL-DInstallation of cabin interior panels consisting of the headliner, window panels and sidewalls.STC SA7916SWInstallation of Honeywell/Sperry EDZ-605 five tube EFIS.STC SA7917SWInstallation of dual Honeywell/Sperry AZ-800 air data computer.STC SA2617CEInstallation of a Class C baggage compartment in the tailcone.STC SA2566CEInstallation of Fairchild model GA100 or A100 cockpt voice recorder system.STC SA973GL-DModification and relocation of the intake and exhaust for the solar auxiliary power unit, Model T62T39A.STC SA2567CERelocation of batteries.STC SA2565CEInstall cabin flood system.STC SA972GL-DRelocation of three computer emergency batteries (two optional installations).STC SA1336WEInstallation of a flight data recorder and a cockpit voice recorder.STC SA119GLElectrical cable harness assemblies for left and right engines; each consisting of starter-generator cables, starter-generator ground cable, master junction cable and fan tach sensor cable.STC SA3369WEInstallation of GNS-500A VLF/OMEGA Navigation System as a means of navigation (but not sole means) for EN ROUTE navigation per A.C. 90-45A within the 48 contiguous United States, the District of Columbia and Alaska.STC ST823SOInstallation of SEMCA 14640-113 air conditioning valve.STC SA36NWInstallation of Sundstrand Ground Proximity Warning SystemSTC SA1025WEInstallation of a Rain Repellent System.STC SA5018NMInstallation of pilot and co-pilot seats. Issued 11/9/90.STC ST00134ATInstallation of interior furnishing. Issued 2/22/93.STC SA2459CEInstallation of Garrett Model GTCP 36-150(W) Auxiliary Power Unit operating as a nonessential electrical and bleed air source for on board electrical and environmental systems. Data required: (1) Duncan Aviation Document List No. F20001 dated January 25, 1989; and (2) FAA Approved Flight Manual Supplement, dated February 13, 1989, or later FAA Approved Revisions to (1) or (2).
Engine · AiResearch TPE331 series
STC SE02538AKModification of Honeywell TPE331-12JR-702TT engineSTC SE03035ATInstallation of Royal Atlantic Aviation Engine Oil Filter Bypass Warning System, Kit P/N RAA2003-1-1STC SE00265ATInstall Ayres Fuel Manifold Purge Assembly Kit, P/N 21757-1 in accordance with "Installation Instructions - Ayres P/N 21757-1 Fuel Manifold Purge Assy-Kit" Dwg. No. 21757-1(1), Revision none, dated April 20, 1993, or later FAA approved revision.STC SE2924SOInstallation of Garrett TPE-331-10 combustor and turbine in the TPE331-8 engine.STC SE01461NYPropeller pitch control system modification. Hartzell HC-E4N-5D/D9690(B) propeller installed per STC SA01462NY. Not approved on serial numbers TC-398 through TC-418.STC SE01604CHConvert Honeywell TPE331-10AV-511B to a TPE331-10AV-511KA.STC SE00229ATInstallation of Garrett TPE331-10 Combustor and Turbine in TPE331-6 engine.STC SE00275ATInstallation of GarrettTPE331-10 combustor and turbine in the TPE331-5 engine.STC SE00691CHModification of a turboprop engine to a turboshaft configuration by incorporation of AlliedSignal (Garrett) TSE331-3U turboshaft gearbox components and other associated changes.STC SE383CHModification of engines.STC SE7547SWInstall Garrett P/N 865558-16 or865558-1E propeller pitch control cam.STC SE8029SWModify propeller pitch control, P/N 869130, by installing pitch control cam, Garrett P/N869386-1.STC SE1725CEModification to replace torque pressure compensator with a plug for raw torque pressure indicating provision.STC SE33WEModification of: ( 1) Manual fuel valve and beta cams; (2) Fuel control linkage and propeller servo cam; and (3)Automatic control of bleed valve and engine starting functions; S/N P61801 onlySTC SE35WEModification of the fuel control, linkage to permit 75% r.p.m. for low ground idle.STC SE39WEModification of the fuel control linkage to permit 75% r.p.m. for ground idle doe S/N 86001STC SE50WEOne engine only. Modification of a Model TPE331-25DAL to. incorporate the engine components associated with a torque and temperature 1imitinq system in accordance with AiResearch Kit PIN 896642-1. An en9ine incorporating this kit is reidentified as a Model TPE331-25DALT .STC SE68WEDeletion of fireshield installation kit.STC SE56WESerial Numbers P-06012 AND P-06024: Installation of heated compressor inlet temperature sensor lines.STC SE38WEModification of fuel control linkage to permit operation of 75% idle speed. S/N 61701 & 61702