Aircraft STC directory
Hawker Beechcraft TC-45G STCs
The Jun 30, 2026 FAA DRS snapshot contains 29 selected supplemental type certificates with status Current whose public applicability data names the Hawker Beechcraft TC-45G. Use it to identify modification scope and recorded holders—not to determine serial-number effectivity, compatibility, installation approval, or commercial availability.
Modification demand surface
Recently revised TC-45G STCs
Showing the 29 most recently revised records. Each entry links to the FAA source and separates public approval data from private commercial claims.
Installation of a carburetor air induction system.
FAA holder: BlackHawk Aircraft Maintenance Inc.
Pratt & Whitney R-985 engine installation with Simmonds Aero- cessories 580047 fuel injector.
FAA holder: Staggerwing Museum Foundation Inc.
Installation of extended tail wheel assembly.
FAA holder: Staggerwing Museum Foundation Inc.
Increase 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.
FAA holder: Staggerwing Museum Foundation Inc.
Install Fiberglas bubble tail wheel enclosure doors (enclosing entire wheel).
FAA holder: Staggerwing Museum Foundation Inc.
Installation of one-peice windshield and flush cockpit side-windows.
FAA holder: Staggerwing Museum Foundation Inc.
Installation of modified wing tips.
FAA holder: Staggerwing Museum Foundation Inc.
Installation of Hartzell propeller unfeathering crossfeed system.
FAA holder: Staggerwing Museum Foundation Inc.
Raise horizontal stabilizer and installation of elevator seal assembly.
FAA holder: Staggerwing Museum Foundation Inc.
Installation of Hartzell propellers, Model HC-93Z30-2C, -2D/10152-5 1/2, or HC-B3Z30-2D/10152-5 1/2.
FAA holder: Staggerwing Museum Foundation Inc.
Approval of existing Jack and HeintzA3A autopilot installation.
FAA holder: Staggerwing Museum Foundation Inc.
Approval of existing installation of47 gallon nose fuel tanks.
FAA holder: Staggerwing Museum Foundation Inc.
Delete righthand rudder tab and system; install rudder control system bungee and shut-off valve.
FAA holder: Staggerwing Museum Foundation Inc.
Increase 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.
FAA holder: Staggerwing Museum Foundation Inc.
Installation of P&W R-985 Fuel Injection Engines, as modified by STC SE1-391.
FAA holder: Staggerwing Museum Foundation Inc.
Oval passenger windows.
FAA holder: Staggerwing Museum Foundation Inc.
Tricycle landing gear and revised nose assembly with optional radome. (Model may also be designated as Conrad 10,200.).
FAA holder: Staggerwing Museum Foundation Inc.
Safety 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.
FAA holder: Staggerwing Museum Foundation Inc.
Revised horizontal stabilizer angle of incidence from -2 degrees to -1/2 degrees.
FAA holder: Staggerwing Museum Foundation Inc.
Two Model 940 Stewart-Warner heaters, install one in each wheel well.
FAA holder: Staggerwing Museum Foundation Inc.
Stewart-Warner heater 940B/24 in fuselage.
FAA holder: Staggerwing Museum Foundation Inc.
Installation of a digital fuel flow indicating system.
FAA holder: Shadin Avionics