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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 ...
Between 1985 and 1995, 60,000 Rotax engines were sold for aircraft propulsion. [2] In the light aircraft class, in 1998 Rotax outsold all other aero engine manufacturers combined. [4] Their four-stroke engines powered most U.S.-certified light sport aircraft when they first appeared around 2004. [5]
Pages in category "Rotax engines" The following 17 pages are in this category, out of 17 total. ... Rotax 503; Rotax 532; Rotax 535; Rotax 582; Rotax 618; Rotax 912 ...
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.
To enable the Taurus to self-launch, a pop-out propeller is mounted on the rear fuselage driven by a Rotax 503 piston engine. [2] In 2007 the company developed the Taurus Electro with the piston engine replaced by a permanent magnet synchronous three-phase brushless motor. [3] [9] By 2011, Pipistrel had delivered 100 aircraft of the Taurus ...
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.
Birdman Chinook 2S showing the pentagonal cockpit cross-section Birdman Chinook 2S Birdman Chinook 2S cockpit Birdman Chinook 2S Rotax 503 engine installation. The Birdman Chinook is a family of single and two-place, pusher configuration, high-wing ultralight aircraft that was first flown on 12 December 1982 and produced by Birdman Enterprises of Edmonton, Alberta, Canada, starting in 1983.
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