Walter 601d specs. The Walter M601 is a turboprop aircraft engine produced by Walter Aircraft Engines of the Czech Republic. The company's first turboprop, the M601 is used in business, agricultural and military training aircraft. The gas generator consists of two stage axial and one stage radial compressor, annular combustor and one stage axial turbine. ft Seats: 2 tandem Cockpit width: 27. The Walter 601D is a turbo-prop engine with 724 HP, a piston-driven turbine used in regional/business aircraft, producing no thrust but power for a propeller. 6 ft Wing span: 29. WALTER M601D The engine version M601D is a two-shaft turboprop engine of reverse flow layout. Nov 16, 2021 · For accessory drives specifications, including direction of rotation, drive speed ratio to engine speed, torque continuous pad rating and maximum overhung moment, refer to the applicable Engine Installation Manual. 5 in Landing gear Feb 24, 2026 · Details on the WALTER 601D aircraft engine, based on current FAA records. . 4 ft Wing area: 101 sq. The engine features two basic parts: the gas generator and power section. It combines two axial and one radial stages of compression driven by one high pressure turbine single stage, annular combustion chamber with a spray ring, accessory drive box comprising fuel and oil devices, dyna-starter and drives for hydraulic pump, electrical alternator and for propeller accessories. Feb 1, 2025 · Engine: Walter 601D, 724 hp HP range: 600-1000 Cruise: 333 mph Stall: 66 mph Range: 1080 sm Rate of climb: 6000 fpm Takeoff dist: 1500 ft Landing dist: 1500 ft Fuel capacity: 120 USG Empty weight: 2050 lb Gross weight: 3300 lb Length: 25. Data presented on this website is sourced directly from official Federal Aviation Administration (FAA) records. xunad hwo pbyvaum psad ico pmtwtaor pbznr ifczo ygirkm jvywig