Beech D18S

STCs that may be installed · 409

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 ('1151004')
    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.

STC SA02717NY PAGE 1Installation of VoiceFlight Systems LLC VFS101 Speech Recognition ModuleVoiceFlight Systems LLCSTC SA00432SEInstallation of EGT 701 series fuel flow instrument.J P InstrumentsSTC SA00861SEInstallation of J.P. Instruments (JPI) fuel flow indicating systemJ P InstrumentsSTC SA02825NY PAGE 1Installation of Aerospace Logic Aircraft InstrumentsAerospace Logic Inc.STC SA01692SEInstallation of a Garmin GMX 200 Multi-Function DisplayGarmin International IncSTC SA03148NYThe installation of the Latitude Technologies Corporation S100 Tracking SystemLatitude Technologies CorporationSTC SA02016SE-DInstallation of Garmin GTS 800, GTS 820 or GTS 850 Traffic SystemGarmin International IncSTC SA01487SE-DInstallation of a GDL 69 or GDL 69A XM Satellite ReceiverGarmin International IncSTC SA00281BOInstallation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000Avidyne CorporationSTC 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.BF Goodrich AerospaceSTC 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.BF Goodrich AerospaceSTC 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).Icarus Avionics, LLCSTC SA1315WEInstallation of Mixture Monitor (exhaust gas temperature probe, gage and selector) in accordance with Delta Products Part Lists A-192 and A-193, or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9, 1981, or later FAA approved revision and/or Drawing List MM-127 dated November 15, 1981, or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29, 1968, copy attached, or later FAA approved revision.Universal CorporationSTC SA00290BOInstallation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXXAvidyne CorporationSTC SA02110CHInstallation of a Time Trac Data RecorderP2 IncorporatedSTC SA2693NMInstallation of Electronics International digital volt/amp gauges and accessories.Electronics International Inc.STC SA2-433Installation of a carburetor air induction system.BlackHawk Aircraft Maintenance Inc.STC SA4-32Internal combustion heaters.Staggerwing Museum Foundation Inc.STC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.M-20 Oil Separators LLCSTC SA01473SEInstallation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote TranspondeGarmin AT Inc.STC SA4005NMPrecise Flight Inc. Pulselite Control SystemPrecise Flight IncSTC SA174CETwin-engine electronic sychronizer for aircraft equipped with Hartzell propellers.Ontic Engineering and Manufacturing Inc.STC SA250CEInstallation of Woodward electronic propeller synchraphaser system.Ontic Engineering and Manufacturing Inc.STC SA1708WERemoval of cargo door (approved under STC SA995WE) to permit aircraft to engage in special operations such as aerial photography, parachute jumping, etc.SOUTHWESTERN AERO EXCHANGE INC.STC SA1512WEInstallation of exhaust gas temperature monitoring systems Model EGT-1.K S Avionics IncSTC SA2557NMInstallation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system.K S Avionics Inc · Lists 18 SeriesSTC SA01695SEInstallation of an antennaGarmin AT Inc.STC SA1-398Pratt & Whitney R-985 engine installation with Simmonds Aero- cessories 580047 fuel injectorStaggerwing Museum Foundation Inc.STC 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.Staggerwing Museum Foundation Inc.STC SA2-1230Installation of extended tail wheel assembly.Staggerwing Museum Foundation Inc.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.Staggerwing Museum Foundation Inc.STC SA2-1261Install Fiberglas bubble tail wheel enclosure doors (enclosing entire wheel).Staggerwing Museum Foundation Inc.STC SA2-204Installation of one-peice windshield and flush cockpit side-windows.Staggerwing Museum Foundation Inc.STC SA2-213Installation of modified wing tips.Staggerwing Museum Foundation Inc.STC SA2-328Installation of Hartzell propeller unfeathering crossfeed system.Staggerwing Museum Foundation Inc.STC SA2-338Installation of two (2) 25,000 BTU Janitrol Heaters installed one (1) in each wheel well.Staggerwing Museum Foundation Inc.STC SA2-383Raise horizontal stabilizer and installation of elevator seal assembly.Staggerwing Museum Foundation Inc.STC SA2-686Installation of Fiberglas Nose.Staggerwing Museum Foundation Inc.STC SA2-725Installation of oil cooler, G & O Mfg. Co. #E703, modified with Fullerton Syphon DV5 thermostat.Staggerwing Museum Foundation Inc.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.Staggerwing Museum Foundation Inc.STC SA2-992Installation of P&W R-985 Fuel Injection Engines, as modified by STC SE1-391.Staggerwing Museum Foundation Inc.STC SA24CEOval passenger windows.Staggerwing Museum Foundation Inc.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.Staggerwing Museum Foundation Inc.STC SA3-732Full-view passenger window.Staggerwing Museum Foundation Inc.STC SA31SOTricycle landing gear and revised nose assembly with optional radome. (Model may also be designated as Conrad 10,200.)Staggerwing Museum Foundation Inc.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.Staggerwing Museum Foundation Inc.STC SA4-119Revised horizontal stabilizer angle of incidence from -2 degrees to -1/2 degrees.Staggerwing Museum Foundation Inc.STC SA4-120Dual airspeed system.Staggerwing Museum Foundation Inc.STC SA4-152Two Model 940 Stewart-Warner heaters, install one in each wheel well.Staggerwing Museum Foundation Inc.STC SA4-34Main landing gear door.Staggerwing Museum Foundation Inc.
Back to Beech D18S