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  2. Rotax 912 - Wikipedia

    en.wikipedia.org/wiki/Rotax_912

    The Rotax 912 was first sold in 1989 in non-certificated form for use in ultralights and motorgliders. [3] The original 60 kW (80 hp) 912 UL engine has a capacity of 1,211 cc (73.9 cu in) and a compression ratio of 9.1:1, and is designed to work with regular automotive gasoline, with up to 10% ethanol.

  3. Australian Lightwing GR 912 - Wikipedia

    en.wikipedia.org/wiki/Australian_Lightwing_GR_912

    The Australian Lightwing GR 912 and Sport 2000 are a family of Australian light-sport aircraft, designed and produced by Australian Lightwing and introduced in 1986. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.

  4. Mainair Blade - Wikipedia

    en.wikipedia.org/wiki/Mainair_Blade

    Data from Bertrand and Kitplanes General characteristics Crew: one Capacity: one passenger Wingspan: 10.6 m (34 ft 9 in) Wing area: 15.6 m 2 (168 sq ft) Empty weight: 190 kg (419 lb) Gross weight: 390 kg (860 lb) Fuel capacity: 65 litres (14 imp gal; 17 US gal) Powerplant: 1 × Rotax 912 four cylinder, four-stroke aircraft engine, 60 kW (80 hp) Performance Maximum speed: 145 km/h (90 mph, 78 ...

  5. Rotax - Wikipedia

    en.wikipedia.org/wiki/Rotax

    The Rotax four-stroke aircraft engine line immediately dominated the emerging category of U.S.-certified "Light Sport Aircraft" (LSAs), powering most of them. [ 6 ] [ 14 ] One general aviation industry media reporter found that 70-80% of the 66,000 aircraft he'd identified, worldwide, used Rotax four-stroke engines. [ 14 ]

  6. Cosmos Phase II - Wikipedia

    en.wikipedia.org/wiki/Cosmos_Phase_II

    A variety of wings and engines can be fitted, each with a different model designation. When equipped with a 37 kW (50 hp) Rotax 503 or 48 kW (64 hp) Rotax 582 two-stroke engine, the aircraft is designated as a Phase II, and when equipped with a 60 to 75 kW (80 to 101 hp) Rotax 912 four-stroke engine, it is designated as a Phase III. Wings used ...

  7. Avid Flyer - Wikipedia

    en.wikipedia.org/wiki/Avid_Flyer

    Early versions with straight trailing edge rudder, foldable wings and either 45 hp (30 kW) Cayuna or 65 hp (49 kW) Rotax 532 engines. Mk IV Fuller, curved edge rudder and either a 64 hp (48 kW) Rotax 582 or a Rotax 912 engines. Baggage compartment added. Introduced 1992. The Mark IV was further developed into the Airdale Backcountry. [6] [7]

  8. Rotax 912U - Wikipedia

    en.wikipedia.org/?title=Rotax_912U&redirect=no

    Download as PDF; Printable version; From Wikipedia, the free encyclopedia. Redirect page. Redirect to: Rotax 912; Retrieved from " ...

  9. 3Xtrim 3X55 Trener - Wikipedia

    en.wikipedia.org/wiki/3Xtrim_3X55_Trener

    3Xtrim 3X55 showing its Rotax 912ULS engine installation 3Xtrim 3X55 showing its cockpit accommodation for two crew, side-by-side with vertically-hinged doors 3Xtrim 3X55 taxiing, showing front view of the aircraft 3Xtrim 3X55 with 30 degrees of flap deflection, showing the centre-section flap 3Xtrim 3X55 instrument panel