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The Rotax 503 is a 37 kW (50 hp), inline 2-cylinder, two-stroke aircraft engine, built by BRP-Rotax GmbH & Co. KG of Austria for use in ultralight aircraft. [ 1 ] [ 2 ] For decades the engine was one of the most popular and reputedly reliable aircraft engines in its class (two-stroke, under 60 horsepower), [ 3 ] and it remains widely used and ...
The standard engine supplied was the twin cylinder, liquid-cooled, two-stroke, dual-ignition 64 hp (48 kW) Rotax 582 engine in pusher configuration. The 50 hp (37 kW) Rotax 503 and 40 hp (30 kW) Rotax 447 engines were factory options. [1] The aircraft fuselage is made from metal tubing, while the fairing is fiberglass. Its two-bladed rotor has ...
The early versions of the aircraft developed a poor reputation due to the lack of reliable engines available in the 1970s. This was rectified with the adoption of the Rotax 277 28 hp (21 kW) and later the Rotax 447 40 hp (30 kW) powerplant. [2] [12] Over 13,000 Weedhoppers have been sold.
The 40 hp (30 kW) Rotax 447 or the 50 hp (37 kW) Rotax 503 were optional engines, although the aircraft then falls into the US Experimental - amateur-built category. [2] [3] [4] The design features a forward fuselage of welded 4130 steel tubing, mated to an aluminum tailboom. The horizontal stabilizer, tail fin and wings are also constructed of ...
The aircraft has a standard empty weight of 220 lb (100 kg). It features a parachute-style high-wing, single-place accommodation, tricycle landing gear and a single 40 hp (30 kW) Rotax 447 engine in pusher configuration. The 50 hp (37 kW) Rotax 503 engine was a factory option. [1] [2]
The Dominator is an open frame autogyro, constructed of bolted aluminium tubing and powered by a 52 hp (39 kW) Rotax 503 engine with a pusher propeller. [1] [2] The Dominator has both a single-seat and tandem two-seat variants. [1] It was one of the first autogyros to use a high tailplane to reduce dynamic and aerodynamic torque. [1]
It features a parachute-style high-wing, two seats in tandem, tricycle landing gear and a single 50 hp (37 kW) Rotax 503 engine in pusher configuration. The 64 hp (48 kW) Rotax 582 liquid-cooled engine was a factory option. [1] [2] [3] The aircraft is built from a combination of bolted aluminium and 4130 steel tubing. In flight steering is ...
Standard engine is the 50 hp (37 kW) Rotax 503 with the 64 hp (48 kW) Rotax 582 as an option. [6] Phantom I-E Single seat ultralight aircraft with struts in place of cable-bracing and enclosed cockpit with removable doors. Standard engine is the 50 hp (37 kW) Rotax 503 with the 64 hp (48 kW) Rotax 582 as an option. [6] Phantom II