Beech TC-45G

STCs that may be installed · 259

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 ('1151016')
    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 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.Garmin AT Inc.STC SA4-769Cambridge fuel air ratio analyzers.Staggerwing Museum Foundation Inc.STC SA2414WEModification for increase in maximum weights.Staggerwing Museum Foundation Inc.STC SA289WECarburetor air scoops.Staggerwing Museum Foundation Inc.STC SA290WEMain landing gear doors.Staggerwing Museum Foundation Inc.STC SA3-358Airplane and powerplant modifications related to civil conversion.Staggerwing Museum Foundation Inc.STC SA3-632Beech Kit 581-1, except angle of incidence change (Item 602) and stall strips (Item 607c) of Spec. A-765; with STC SA2-383, with or without STC's SA2-204 and SA3-409; and wing spar mod. Maximum gross weight: takeoff 9,500 lbs., landing 9,400 lbs.Staggerwing Museum Foundation Inc.STC SA305WECabin modified to G18 configuration.Staggerwing Museum Foundation Inc.STC SA332WEPropeller spinners and increase in maximum continuous power to 450 hp.Staggerwing Museum Foundation Inc.STC SA356WEInstallation of A3A autopilot.Staggerwing Museum Foundation Inc.STC SA4-1035Modification of door frame between cabin and cockpit for installation of folding door.Staggerwing Museum Foundation Inc.STC SA4-1116Three additional windows.Staggerwing Museum Foundation Inc.STC SA4-1198Aft bulkhead removal.Staggerwing Museum Foundation Inc.STC SA4-1256Installed astrodome.Staggerwing Museum Foundation Inc.STC SA4-1299Voltage regulators moved to front side of forward bulkhead.Staggerwing Museum Foundation Inc.STC SA4-1368Replaced Airline Training Company L-12001B wing tips with American Turbine Engine Company wing tipsStaggerwing Museum Foundation Inc.STC SA4-1486Additional seats.Staggerwing Museum Foundation Inc.STC SA4-1536Picture window G18 type.Staggerwing Museum Foundation Inc.STC SA4-1595Installed American Turbine Engine Co. drawing B-138 divan.Staggerwing Museum Foundation Inc.STC SA4-718Installed auxiliary nose fuel tanks per American Turbine Engine Company Drawing B-3, Sheet 1, Sheet 2 and Sheet 3.Staggerwing Museum Foundation Inc.STC SA548WEAir stair door.Staggerwing Museum Foundation Inc.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.Garmin AT Inc.STC SA1636WEInstallation of AiResearch TPE 331 series engine, tricycle landing gear and ventral fin, extension of fuse- lage and related changes.Southwestern Aero Exchange IncSTC SA1016WEInstallation of United Aircraft of Canada Ltd. PT6 series engines.Staggerwing Museum Foundation Inc.STC SA1059WECargo door in fuselage.Staggerwing Museum Foundation Inc.STC SA1154CEInstall crack detection system.Staggerwing Museum Foundation Inc.STC SA1533WESpar reinforcement.Staggerwing Museum Foundation Inc.STC SA1998WEInstallation of Bendix Model M-4C automatic flight control system.Staggerwing Museum Foundation Inc.STC SA1999WEInstallation of cargo floor.Staggerwing Museum Foundation Inc.STC SA2353WEInstallation of cargo pod.Staggerwing Museum Foundation Inc.STC SA2494WEInstallation of extended nose section and modification to the elevator down spring system. (THESE MODELS MUST INCOPRORATE THE PROVISIONS OF STC SA2437WE TO BE ELIGIBLE FOR MODIFICATION.)Staggerwing Museum Foundation Inc.STC SA2737WEInstallation of spar strap extension to outboard wing panel.Staggerwing Museum Foundation Inc.STC SA2794WEA Bendix M-4C Autopilot System is installed.Staggerwing Museum Foundation Inc.STC SA2815WERemoval of fabric covering from the wing flaps, ailerons, rudders and elevators and replace and recover these surfaces with aluminum.Staggerwing Museum Foundation Inc.STC SA34WETwo 42.5-gallon auxiliary fuel tanks.Staggerwing Museum Foundation Inc.STC SA4-1323Installation of stair type entrance door, rectangular windows and outside opening baggage compartment.Staggerwing Museum Foundation Inc.STC SA4-1584Installation of two-piece plexi- glass windshield.Hamilton Avn Co IncSTC SA4-879Installation of 37-gallon auxiliary fuel tank in each outboard wing.Staggerwing Museum Foundation Inc.STC SA435WERemoval of large cargo door for special purpose operations as aerial photography, etc.Staggerwing Museum Foundation Inc.STC SA572WEIncrease in gross weight to 10,100 pounds. When aircraft has been modified, installation of nacelle vent manifold optional.Staggerwing Museum Foundation Inc.STC SA74WEModification of horizontal stabilizer and attachment to provide 1-1/2 degree angle of incidence increase and elevator down spring installation.Staggerwing Museum Foundation Inc.STC SA980WEModification made per FAA sealed summary, Drawing 25600, Sheet 3.Staggerwing Museum Foundation Inc.STC SA989WEInstallation of revised carburetor air mixing chamber and ram airscoop.Staggerwing Museum Foundation Inc.STC SA565WEInstallation of wing tips per FAA Sealed Drawing No s. ASP-2029 and API-2030.SOUTHWESTERN AERO EXCHANGE INC.STC SA1192WEModification of main spar.Vintage AircraftSTC SA3009WEInstallation of wing spar reinforcement.Vintage AircraftSTC SA3229WEInstallation of wing spar reinforcement.Vintage AircraftSTC SA572EAInstallation of Goodrich Model 5735K deicer kit (P/N 5735 deicer boot, P/N D-5735-1 cable, P/N 5735H hardware kit). Limited to aircraft which incorporate Goodrich Propeller Deicing Systems equipped with Goodrich Propeller Deicer Boot P/N 4E1185-5 on Hartzell propellers as listed on STC SA572EA eligibility list.Goodrich Corp.STC SA3-277Modify existing cabin port hole windows.Staggerwing Museum Foundation Inc.STC SA3-343Installation of one only, standard cabin window between bulkheads #8 and #9 right side opposite cabin door.Staggerwing Museum Foundation Inc.
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