TCDS A-765

STCs approved under this data sheet · 532

Current certificates first, most recently changed first.

Query with SQL
duckdb -csv -c "SELECT s.stc_number, s.description, s.holder, s.status, s.status_date
  FROM 'https://openairdocs.org/data/latest/faa_stc.parquet' s
  WHERE s.stc_number IN (SELECT stc_number FROM 'https://openairdocs.org/data/latest/faa_stc_model.parquet' WHERE tcds_number = 'A-765')
  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 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 SA2-993Installation 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.STC SA53CEStewart-Warner heater 940B/24 in fuselage.Staggerwing Museum Foundation Inc.STC SA2437WEModifications for increase in maximum weights.Staggerwing Museum Foundation Inc.STC SP00400SEInstallation of various propeller electrical de-icer modelsSMR TechnologiesSTC SA817GLInstallation of a digital fuel flow indicating system.Shadin AvionicsSTC SA111WEInstalled Volpar Mark IV tricycle landing gear.SOUTHWESTERN AERO EXCHANGE INC.STC SA1171WEInstallation of two AiResearch TPE331 Series engines, tricycle landing gear, wing platform modifications, and related modifications.SOUTHWESTERN AERO EXCHANGE INC.STC SA1223WESee STC SA1223WE Addendum.SOUTHWESTERN AERO EXCHANGE INC.STC SA1752WEInstallation of AiResearch Air Conditioning system.SOUTHWESTERN AERO EXCHANGE INC.STC SA1832WEInstallation of Volpar Tricycle Landing Gear.SOUTHWESTERN AERO EXCHANGE INC.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.SOUTHWESTERN AERO EXCHANGE INC.STC SA285WENose strut snubber installation.SOUTHWESTERN AERO EXCHANGE INC.STC SA3385WEInstallation of AiResearch TPE 331-1-101B engines and increase gross weight to 11500 pounds.SOUTHWESTERN AERO EXCHANGE INC.STC SA4-1069Remove original Arens controls and lock mechanism for left and right cowl flaps and replace with electronic actuators, control switches, and indicator.SOUTHWESTERN AERO EXCHANGE INC.STC SA554WEInstallation of square topped stair cabin door.SOUTHWESTERN AERO EXCHANGE INC.STC SA947WEInterior arrangement. Data not suitable for reproduction in other aircraft; installation for Beech C 45H, Serial No. AF 851 only.SOUTHWESTERN AERO EXCHANGE INC.STC SA4-1076Electrically-driven, mechanical, refrigerated air conditioner.Rotorcraft Enterprises LLCSTC SA1641WEInterior arrangement.SOUTHWESTERN AERO EXCHANGE INC.STC SA2400WEInstallation of fiberglass nose cap left hand outer wing leading edge.SOUTHWESTERN AERO EXCHANGE INC.STC SA3126WEInstallation of pilot cockpit door.SOUTHWESTERN AERO EXCHANGE INC.STC SA4-1397Installation of Tricycle landing gear and nose assembly.SOUTHWESTERN AERO EXCHANGE INC.STC SA4-1531Installation of Tricycle landing gear and revised nose assembly with optional radome.SOUTHWESTERN AERO EXCHANGE INC.STC SA4-855Addition of windows in cabin.SOUTHWESTERN AERO EXCHANGE INC.STC SA468WEReplacement of round window between Bulkhead Nos. 9 and 10 with Beech Super 18 type window.SOUTHWESTERN AERO EXCHANGE INC.STC SA4-1578Removal of the main cabin entrance door and installation of stair door.SOUTHWESTERN AERO EXCHANGE INC.STC SA4-1645Installation of Stewart-Warner Model 8259-A heater.SOUTHWESTERN AERO EXCHANGE INC.STC SA02192NYInterior configuration modification.Aerotech IndustriesSTC 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 SA3471WEModification for increase in maximum weight approved for model E-18S, serial number BA20.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.
Back to TCDS A-765