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  2. Rotax 503 - Wikipedia

    en.wikipedia.org/wiki/Rotax_503

    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 ...

  3. Rans S-12 Airaile - Wikipedia

    en.wikipedia.org/wiki/Rans_S-12_Airaile

    Standard engine was the Rotax 447 of 40 hp (30 kW), with the Rotax 503 of 50 hp (37 kW) and the Rotax 582 of 64 hp (48 kW) optional. Reported construction time 200 man-hours including complete cockpit fairing. Empty weight of 390 lb (177 kg) places the S-14 above the maximum category weight of the US FAR 103 Ultralight Vehicles category ...

  4. Air Command Commander Sport - Wikipedia

    en.wikipedia.org/wiki/Air_Command_Commander_Sport

    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 ...

  5. Affordaplane - Wikipedia

    en.wikipedia.org/wiki/Affordaplane

    When built as a Part 103 ultralight, the aircraft is intended to be powered by a 26 hp (19 kW) Rotax 277, 35 hp (26 kW) Rotax 377, or similar engine. Heavier and more powerful engines including the Rotax 503 may also be used, but will result in exceeding the FAR Part 103 less than 254 pound (115 kg) empty weight limit, if the aircraft is ...

  6. Category:Rotax engines - Wikipedia

    en.wikipedia.org/wiki/Category:Rotax_engines

    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 ...

  7. ISON Airbike - Wikipedia

    en.wikipedia.org/wiki/ISON_Airbike

    Single seat aircraft designed for the US ultralight category. Engine options were the 28 hp (21 kW) Rotax 277, 40 hp (30 kW) Rotax 447 or 22 hp (16 kW) Zenoah G-25. [1] [2] Tandem Airbike Two-seat aircraft designed as an ultralight trainer or amateur-built. Standard engine was the 50 hp (37 kW) Rotax 503. [1] [2]

  8. Rans S-4 Coyote - Wikipedia

    en.wikipedia.org/wiki/Rans_S-4_Coyote

    The original basic engine was the Rotax 277 of 28 hp (21 kW), with the Rotax 447 of 40 hp (30 kW) and the Rotax 503 of 50 hp (37 kW) available later as options. [ 1 ] [ 2 ] [ 11 ] The Coyote II two-seater was later developed from the S-5.

  9. Chotia Weedhopper - Wikipedia

    en.wikipedia.org/wiki/Chotia_Weedhopper

    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.