Beech C90A
STCs that may be installed · 260
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 ('1152911', '115291A')
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 ('1152911', '115291A')
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 SA01146ATInstallation of left hand side and right hand side leading edge fuel cell assemblies. (F90 S/N LJ1 AND UP, 99 ALL S/N'S, B100 S/N B1-89 AND UP, 65-B80 S/N LD-151 AND UP)STC SA01626AT-DInstallation of replacement fuel cell assembliesSTC SA00865AT-DInstallation of replacement fuel cell assembliesSTC SA0912AT-DInstallation of replacement fuel cell assembliesSTC SA10560SCInstallation of Wing Mounted Auxiliary Fuel Transfer TankSTC SA01004ATInstallation of right hand side nacelle fuel cell assembly.STC SA01203ATInstallation of left-hand side and right-hand side center section fuel cell assemblies.STC SA01251ATInstallation of left hand and right hand nacelle fuel cell assemblies. (E90 ALL S/N'S, F90 S/N LA2 AND UP)STC SA02963CHCargo interior modification of Beech 90 Series King Air in accordance with Aerospace Resources drawing 20-0090-1, Revision -, dated April 24, 2009, or later FAA approved revision.STC SA1726CEInstallation of camera window with sliding door cover and drift sight.STC SA2630CEInstallation of a four-place side facing divan.STC SA01473SEInstallation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote TranspondeSTC SA8710SWInstallation of exhaust stub.STC SA09544AC-DInstallation of S-TEC 01304 Digital Flight Control System (DFCS).STC SA2361CEInstall dynamic acoustic absorbers.STC SA4005NMPrecise Flight Inc. Pulselite Control SystemSTC SA03527ATInstallation of an Avidyne EXP5000 Primary Flight Display (PFD)STC SA2777CEInstall passenger seat with hinged backrest.STC SA09872SCInstallation of a Collins DPU-84 data processing unit and two Collins EFD-84 electronic flight displays on co-pilot's instrument panel.STC SA09896SCInstallation of a Honeywell KMH-880 Multi-Hazard Awareness System with a Multi-Function Display (MFD), an operational portion of the Honeywell IHAS 8000 (Integrated Hazard Awareness System), resulting in a Traffic Advisory System (TAS) and an Enhanced Ground Proximity Warning System (EGPWS) to reduce the likelihood of controlled flight into terrain and/or collision with another aircraft.STC SA09898SCInstallation of a Garmin GPS-400 Global Positioning System (GPS).STC SA09899SCInstallation of a Garmin GPS-400 Global Positioning System (GPS)STC SA09908SCInstallation of a 110 VAC Inverter with two (2) 110 VAC outlets in the cabin. Modifications.STC SA09545AC-DInstallation of Avidyne Primary Flight Display.STC SA01306WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation.STC SA01695SEInstallation of an antennaSTC SP00400SEInstallation of various propeller electrical de-icer modelsSTC ST01468CHInstallation of various SMR Technologies electrical propeller deicer models.STC SA1719GLInstallation of a Shadin engine performance recorder system.STC SA01860NYInstallation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.STC SA01141WI-DModification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94 Mode S Transponder System installation with CTL-92E control head.STC SA01670SEInstallation of a GWX 68 Weather RadarSTC SA02238ATReplace existing Pratt & Whitney PT6A enginesSTC ST00092ATInstallation of an Aircraft Security System.STC SA03098ATReplace the current PT6A-21 engines with PT6A-35 engines.STC SA01487SEInstallation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision.STC SA01313WI-DModification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installation in accordance with Collins Drawing Index as listed on AML No. SA01313WI-D, Revision -, or later FAA approved revision.STC SA02160CHInstallation of Medical Storage Cabinet.STC SA01158WIInstallation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.STC SA00161BOInstallation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.STC SA02154AKInstallation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500.STC SA02217AKInstallation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL 90 UAT Master Data List, P/N 560-0278-01, Revision A, dated November 12, 2004, or later FAA approved revision.STC SA10364SCInstallation of Pratt & Whitney Canada PT6A-135A engines and McCauley 4HFR34C762/94LMA-4 or 4HFR34C768/94LMA-4 propellers in accordance with Blackhawk Modifications, Inc. Drawing No. 19005-01, Rev. IR, dated March 15, 2004, Installation Instructions, or later FAA approved revision.
FAA approved AFMS Document No. 19005, Rev. IR, dated November 24, 2004, or later FAA approved revision is required.STC SA10339SCInstallation of CenTex Inc. proprietary engine torque indicating system including engine transducer and cockpit indicator in accordance with CenTex Aerospace, Inc. drawing no 008-0000-1000, Rev. A, dated September 2, 2004, or later FAA approved revision. Type design data is contained in CenTex Aerospace, Inc. Master Drawing List 008-0000-0000, Rev. A, dated September 2, 2004 or later FAA approved version. Required instructions for continued airworthiness are contained in CenTex Aerospace, Inc. drawing no 008-0000-1000, Rev. A, dated September 2, 2004, or later FAA approved revision.STC SA3066NMInstallation of monorail sun visor systemSTC SA01639NYReplacement of 12 refrigerant in air conditioning system with Enviro Refrigerant Hotshot R414B.STC SA867NEInstallation of lower wing front spar cap reinforcement kit. (C90A S/N LJ-1063 THUR LJ-1087 EXCEPT LJ-1085)STC SA2740SWInstallation of P&W Canada PT6A-135 engines and bleed air conditioning and pressurization system.STC SA01527LAInstallation of ACSS T2CASSTC SA01441LAInstallation of ACSS T2CAS
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