Beech C-45H
STCs that may be installed · 384
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 ('1151018', '1151019')
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 ('1151018', '1151019')
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 SA02016SE-DInstallation of Garmin GTS 800, GTS 820 or GTS 850 Traffic SystemSTC SA01487SE-DInstallation of a GDL 69 or GDL 69A XM Satellite ReceiverSTC SA407CEInstallation of Hoskins Twilighter Mark III High Intensity Lighting System consisting of Model A Wing Tip Lights and Model D or Model P Tail Light.STC SA97CEInstallation of Hoskins Supplemental High Intensity Position Light System consisting of Model A or B Wing Tip Lights, Model C or D Tail Lights with or without Model 1 or 2 Fuselage Lights.STC SA00243BOInstallation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200).STC SA2-433Installation of a carburetor air induction system.STC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.STC SA01473SEInstallation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote TranspondeSTC SA1708WERemoval of cargo door (approved under STC SA995WE) to permit aircraft to engage in special operations such as aerial photography, parachute jumping, etc.STC SA2557NMInstallation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system.STC SA01695SEInstallation of an antennaSTC SA00402SEInstallation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed)STC SA1-398Pratt & Whitney R-985 engine installation with Simmonds Aero- cessories 580047 fuel injectorSTC SA1-427Pratt & Whitney R-985 engine installation with Simmonds Aero- cessories 580047 fuel injector per STC SE1-391, and takeoff weight increase to 9,800 lbs. and landing weight to 9,400 lbs. per STC SA2-820.STC SA2-1230Installation of extended tail wheel assembly.STC SA2-1246Increase in take-off Gross Weight to10,200 pounds and landing weight to9800 pounds. Extension of Aft. C.G. limits to +120.5 at 10,200 pounds.STC SA2-1261Install Fiberglas bubble tail wheel enclosure doors (enclosing entire wheel).STC SA2-204Installation of one-peice windshield and flush cockpit side-windows.STC SA2-213Installation of modified wing tips.STC SA2-328Installation of Hartzell propeller unfeathering crossfeed system.STC SA2-383Raise horizontal stabilizer and installation of elevator seal assembly.STC SA2-621Installation of Hartzell propellers, Model HC-93Z30-2C, -2D/10152-5 1/2, or HC-B3Z30-2D/10152-5 1/2.STC SA2-622Approval of existing Jack and HeintzA3A autopilot installation.STC SA2-623Approval of existing installation of47 gallon nose fuel tanks.STC SA2-625Delete righthand rudder tab and system; install rudder control system bungee and shut-off valve.STC SA2-686Installation of Fiberglas Nose.STC SA2-725Installation of oil cooler, G & O Mfg. Co. #E703, modified with Fullerton Syphon DV5 thermostat.STC SA2-820Increase in take-off weight to 9800 pounds, and increase in landing weight to 9400 pounds, when P&W R-985-AN14B;-AN4 (modified per P&W Special Instruction No. 15F-45) or -AN10 (modified per P&W Special Instruction No. 15F-45) or -AN-1M1(with the Stromberg NAR-9B-19 carburetor with 2-3/4 inch venturi) is installed.STC SA2-992Installation of P&W R-985 Fuel Injection Engines, as modified by STC SE1-391.STC SA24CEOval passenger windows.STC SA27SOIncrease in landing weight to 9800 lbs. and extension of Aft. C.G. limits to +120.5. These limitations applicable to Beech D18S, C45H, TC45G, TC45H when modified to Airline Training Inc. CONRAD 9800 D.STC SA3-732Full-view passenger window.STC SA31SOTricycle landing gear and revised nose assembly with optional radome. (Model may also be designated as Conrad 10,200.)STC SA4-113Safety performance kit, increase gross weight to 9,000 lbs. takeoff and landing. Installation of P&W R-985-AN10, (Modified per P&W Special Instruction No. 15F-45 and eligible on C-45G, C45H, TC45G, & TC45H only), R-985-AN4 (modified per P&W Special Instruction No. 15F-45) or -AN14B Engine, associated powerplant installation changes, wheel well doors, and elevator hinge gap seals.STC SA4-119Revised horizontal stabilizer angle of incidence from -2 degrees to -1/2 degrees.STC SA4-120Dual airspeed system.STC SA4-152Two Model 940 Stewart-Warner heaters, install one in each wheel well.STC SA4-34Main landing gear door.STC SA53CEStewart-Warner heater 940B/24 in fuselage.STC SA2437WEModifications for increase in maximum weights.STC SP00400SEInstallation of various propeller electrical de-icer modelsSTC SA817GLInstallation of a digital fuel flow indicating system.STC SA111WEInstalled Volpar Mark IV tricycle landing gear.STC SA1171WEInstallation of two AiResearch TPE331 Series engines, tricycle landing gear, wing platform modifications, and related modifications.STC SA1223WESee STC SA1223WE Addendum.STC SA1752WEInstallation of AiResearch Air Conditioning system.STC SA1832WEInstallation of Volpar Tricycle Landing Gear.STC SA2204WEInstallation of 2 AiResearch TPE331-1 series turbo prop engines with Hartzell HCB3TN propellers: 8-1/2 inches extension of fuselage and ventral fin, tricycle landing gear installation and related modifications.STC SA285WENose strut snubber installation.STC SA3385WEInstallation of AiResearch TPE 331-1-101B engines and increase gross weight to 11500 pounds.
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