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.
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
Run 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 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 SA2-993Installation 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.STC SA4-1069Remove original Arens controls and lock mechanism for left and right cowl flaps and replace with electronic actuators, control switches, and indicator.STC SA554WEInstallation of square topped stair cabin door.STC SA947WEInterior arrangement. Data not suitable for reproduction in other aircraft; installation for Beech C 45H, Serial No. AF 851 only.STC SA4-1076Electrically-driven, mechanical, refrigerated air conditioner.STC SA1641WEInterior arrangement.STC SA2400WEInstallation of fiberglass nose cap left hand outer wing leading edge.STC SA3126WEInstallation of pilot cockpit door.STC SA4-1397Installation of Tricycle landing gear and nose assembly.STC SA4-1531Installation of Tricycle landing gear and revised nose assembly with optional radome.STC SA4-855Addition of windows in cabin.STC SA468WEReplacement of round window between Bulkhead Nos. 9 and 10 with Beech Super 18 type window.STC SA4-1578Removal of the main cabin entrance door and installation of stair door.STC SA4-1645Installation of Stewart-Warner Model 8259-A heater.STC SA02192NYInterior configuration modification.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 SA4-769Cambridge fuel air ratio analyzers.STC SA2414WEModification for increase in maximum weights.STC SA289WECarburetor air scoops.STC SA290WEMain landing gear doors.STC SA3-358Airplane and powerplant modifications related to civil conversion.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.STC SA305WECabin modified to G18 configuration.STC SA332WEPropeller spinners and increase in maximum continuous power to 450 hp.STC SA3471WEModification for increase in maximum weight approved for model E-18S, serial number BA20.STC SA356WEInstallation of A3A autopilot.STC SA4-1035Modification of door frame between cabin and cockpit for installation of folding door.
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