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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. Aero-Works Aerolite 103 - Wikipedia

    en.wikipedia.org/wiki/Aero-Works_Aerolite_103

    Data from Aerolite 103 website & KitPlanes General characteristics Crew: one Length: 17 ft 0 in (5.19 m) Wingspan: 26 ft 10 in (8.18 m) Height: 6 ft 5 in (1.96 m) Wing area: 124 sq ft (11.54 m 2) Empty weight: 275 lb (125 kg) Max takeoff weight: 600 lb (272 kg) Powerplant: 1 × Rotax 447 fixed pitch, 40 hp (30 kW) Performance Maximum speed: 70 mph (113 km/h, 61 kn) Cruise speed: 63 mph (102 km ...

  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. Phantom X1 - Wikipedia

    en.wikipedia.org/wiki/Phantom_X1

    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

  6. Category:Rotax engines - Wikipedia

    en.wikipedia.org/wiki/Category:Rotax_engines

    Download as PDF; Printable version; ... Engines manufactured by Austrian company Rotax. ... Rotax 503; Rotax 532; Rotax 535; Rotax 582; Rotax 618; Rotax 912;

  7. 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.

  8. Rans S-6 Coyote II - Wikipedia

    en.wikipedia.org/wiki/Rans_S-6_Coyote_II

    Standard engine is the 100 hp (75 kW) Rotax 912ULS and the 2010 base price is US$99,000. [16] S-6S Super Six Improved version with dope and fabric covering, introduced in 1993. Standard engine is the 100 hp (75 kW) Rotax 912ULS. Available with standard wing, "116" wing and "light sport wing". In production in 2010. [3] [5] [6] [13]

  9. Hirth F-23 - Wikipedia

    en.wikipedia.org/wiki/Hirth_F-23

    A belt reduction drive system, fuel injection, tuned exhaust and electric start are optional. [1] [2] The engine runs on a 50:1 pre-mix of unleaded 93 octane auto fuel and oil. Recommended time between overhauls is 1000 hours. [1] [2] The F-23 produces 50 hp (37 kW) at 6150 rpm and 40 hp (30 kW) at 5500 rpm. [1] [2]