N397AL
STCs that may be installed · 441
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 = '1182202'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '52033')
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 = '1182202'
UNION ALL SELECT stc_number, 2, 'engine', matched_model FROM 'https://openairdocs.org/data/latest/faa_engine_model_stc.parquet' WHERE engine_model_code = '52033')
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 · Bell 412
STC SH8024SWInstallation of Kulite P/N APTE-138-50G fuel pressure transducer.STC SH8025SWInstallation of Kulite P/N APTE-138-50G engine oil pressure transducer.STC SR00092ATInstallation of engine exhaust ejector assembly.STC SR00032DEInstallation of an emergency medical system interior.STC SH8331SWInstallation of Kulite P/N APTE-139KBS-1000-1500SG transducer. in place of Kratos P/N 50579 or 50579-3 transmitter.STC SH5236NMInstallation of passenger grab barsSTC SH8148SWModification of seating arrangement to limit passenger seating to nine (9) or less passengers.STC SH8026SWInstallation of Kulite P/N APTE-138-100G main transmission and combining gear box oil pressure transducers.STC SH8022SWInstallation of a B & D model 89094 cockpit voice recorder.STC SH2211NMInstallation of Silver Instruments Fueltron IIIPT-IGS, IIIPT-IPS, IIIPT-ILS, IIIPT-IKS digital fuel flow indicating system.STC SH5201NMInstallation of an air medical transport unit.STC SH4062NMInstallation of a Spectrolab searchlight.STC SH7480SWInstallation of a freon air conditioning system.STC SH4088NMInstallation of a freon air conditioning system.STC SH733NWInstallation of weighing systemSTC SH7727SWLimit passenger seating to an approved configuration of 9 or less.STC SA4302NMInstallation of Electronics Int'l digital automatic engine analyzer.STC SH7586SWPersonnel lifting device.STC SH4068SWInstallation of Teledyne TDL-711 Loran C micro-navigator.STC SH7450SWInstallation of an alternate static system for the Bell Model 412.STC SH7418SWInstallation of a powered external step.STC SH463NWInstallation of an electronic weighing system (for monitoring cargo weight)STC SH3726NMInstallation of ARNAV Systems FC-10/FT-10 digital fuel flow indicating system.STC SH17NWInstallation of Chadwick Electronic weighing system C-47.STC SH468NEInstallation of 'zapper,' pulsed chip detection system Model1K1426.STC SH3553SWIncrease fuel system capacity.STC SH2281SWInstallation of environmental control unit.STC SH5996SWInstallation of Foxtronics CS-101 circuit control and F7722 overvolt sensor to control external power.STC SH5997SWInstallation of cabin entry door and cabin closure.STC SH5860SWInstallation of Bendix EFIS-10 and Series III avionics.STC SH2308NMInstallation of Bell P/N 205-706-045 series auxiliary fuel tank assemblies, Bell P/N206-706-324-003 litters and Bell P/N 204-070-023-011 rear facing attendant seats.STC SH5457SWFlite-trak 100 flight following systems.STC SR00426NYInstallation of ARNAV Systems, Model MPD5000 or MPD5200 multi-function display system and ARNAV Systems geolink computer/transceiver with GPS sensor.
Engine · Pratt & Whitney PT6 series
STC SE12225ACThis STC will incorporate P&W 1700 rpm propeller reduction gearbox on P&WC engines to allow 1700 rpm propeller installationSTC SE00010ENInstructions for Continued Airworthiness for the PT6A-25, and, -25A engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.STC SE000010ENInstructions for Continued Airworthiness for the PT6A-25 and PT6A-25A engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.STC SE000011ENInstructions for Continued Airworthiness for the PT6A-25C engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.STC SE00001ENEngines will be maintained IAW 'Maintenance or Reliable Engines(MORE) Program,' Rev 2, 8/16/95.STC SE00002ENInstructions for Continued Airworthiness for the PT6A-34, -34AG, -34B, -36, -114, -114A, -116, -135, and -135A engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.STC SE00003ENInstructions for Continued Airworthiness for the PT6A-6/C20, -20, -20A and, -20B engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.STC SE00004ENInstructions for Continued Airworthiness for the PT6A-11, -11AG, -15AG, -110 and-112 engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.STC SE00006ENInstructions for Continued Airworthiness for the PT6A-45A, -45B, and, -45R engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.STC SE00011ENInstructions for Continued Airworthiness for the PT6A-25C engine model that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.STC SE000ENEngines will be maintained IAW 'Maintenance or Reliable Engines(MORE) Program,' Rev 4, dated 8/16/95.STC SE10947SCThe conversion of the Pratt & Whitney Canada, Model PT6A-21 to a PT6A-28 turboprop engineSTC SE00482SEIncorporation of turbine engine into a twin power section turboprop assembly.STC SE10552SCConversion of Pratt & Whitney Canada Corp. Model PT6A-27 or -28 to a Model PT6A-34 turboprop engine.STC SE11139SCThe conversion of the Pratt & Whitney Canada, Model PT6A-135 to a PT6A-135A turboprop engineSTC SE11141SCThe conversion of the Pratt & Whitney Canada, Model PT6A-15AG to a PT6A-34AG turboprop engineSTC SE02170ATInstallation of Pc Safety Valve Kit