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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 ...
In 2009 the standard recommended engine was the Rotax 447, with the 46 hp (34 kW) Rotax 503 single carburettor engine optional. [ 6 ] [ 12 ] In 2021 an electric aircraft option was added as the manufacturer offered a complete electric drivetrain and up to four batteries as an alternative to gasoline powerplants.
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 ...
Up-engined model with a 50 hp (37 kW) Rotax 503 engine, many extras and an empty weight of 330 lb (150 kg) for the US amateur-built category. [9] [10] [1] Weedhopper II Current production two seat side-by-side seating model with a 50 hp (37 kW) Rotax 503 engine. Also known as the Weedhopper Two Place.
Download as PDF; Printable version; ... Engines manufactured by Austrian company Rotax. ... Rotax 503; Rotax 532; Rotax 535; Rotax 582; Rotax 618; Rotax 912;
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
Open-cockpit, conventional landing gear, ultralight trainer with two seats in tandem, standard engine is the Rotax 503 of 50 hp (37 kW) with the Rotax 582 of 64 hp (48 kW), 80 hp (60 kW) or the Rotax 912UL of 100 hp (75 kW) optional. The aircraft uses the wings, tailboom and tail of the S-12XL, but is fitted with a new steel tube cockpit structure.
The standard engine supplied is the Rotax 582 64 hp (48 kW) twin cylinder, two-stroke, liquid-cooled aircraft engine. The Rotax 503 50 hp (37 kW) air-cooled two-stroke engine and the four-stroke HKS 700E 60 hp (45 kW) and Rotax 912UL of 80 hp (60 kW) are also available.