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  2. Zenith Aircraft Company - Wikipedia

    en.wikipedia.org/wiki/Zenith_Aircraft_Company

    His son Sebastian is listed as the owner of Zenith Aircraft Company. [1] Kit designs manufactured by the company include the original two-seat STOL CH 701, a high-wing all-metal short take-off and landing design, the larger STOL CH 801 four-place aircraft, the STOL CH 750 light sport utility kit airplane, and the two-seat CH 650, an all-metal ...

  3. Zenair CH 640 - Wikipedia

    en.wikipedia.org/wiki/Zenair_CH_640

    The design was also influenced by the Zenith CH 601 and the Zenair CH 300. The design goals were to produce a simple four-seat aircraft capable of flying cross country flights with full seats. [2] The CH 640 is a four-seat, low-wing touring aircraft with tricycle landing gear and a single engine in tractor configuration. It has a standard empty ...

  4. Zenith STOL CH 701 - Wikipedia

    en.wikipedia.org/wiki/Zenith_STOL_CH_701

    A Zenith STOL CH 701 on wheels A Czech Aircraft Works-built CH 701 AMD-built CH 750 CH 750 CH 750 instrument panel CH 701 Turboprop CH 701 Turboprop in flight. The Zenith STOL CH 701 and CH 750 are a family of light, two-place kit-built STOL aircraft designed by Canadian aeronautical engineer Chris Heintz through his Midland, Ontario, based company, Zenair.

  5. Zenair CH 150 - Wikipedia

    en.wikipedia.org/wiki/Zenair_CH_150

    The Zenith CH 150 Acro Zenith is a Canadian single-engine, low wing, all-aluminum aircraft designed by Chris Heintz and produced by Zenair in kit form for amateur construction. The aircraft is intended for aerobatic use and was introduced at the Experimental Aircraft Association convention in 1980.

  6. Zenith STOL CH 801 - Wikipedia

    en.wikipedia.org/wiki/Zenith_STOL_CH_801

    While both aircraft look alike they do not share any common parts. [ 2 ] [ 4 ] The STOL CH 801 is made from sheet aluminium and employs a deep wing chord, full-length leading edge slats and trailing edge flaperons to develop high lift at low speed, while maintaining a short wing-span for maximum strength and ground maneuverability.

  7. Zenair CH 180 - Wikipedia

    en.wikipedia.org/wiki/Zenair_CH_180

    Data from Jane's All the World's Aircraft 1992-93 General characteristics Crew: 1 Length: 20 ft 3 in (6.17 m) Wingspan: 20 ft 2 in (6.15 m) Height: 5 ft 5 in (1.65 m) Wing area: 85 sq ft (7.9 m 2) Airfoil: NACA 0015 Empty weight: 800 lb (363 kg) Max takeoff weight: 1,150 lb (522 kg) Fuel capacity: 27 imp gal (32 US gal; 120 L) in two fuselage tanks Powerplant: 1 × Textron Lycoming IO-360 4 ...

  8. Zenair CH 200 - Wikipedia

    en.wikipedia.org/wiki/Zenair_CH_200

    The Zenair Zenith CH 200 and CH 250 are a family of Canadian single-engined homebuilt light aircraft. It is a low-winged single engine monoplane , that was first flown in France in 1970, with kits being made by the Canadian company Zenair from 1974, with hundreds built and flown.

  9. List of aircraft (Z) - Wikipedia

    en.wikipedia.org/wiki/List_of_aircraft_(Z)

    Download as PDF; Printable version; ... Zenair Cricket - Kit; ... (Zenith Aircraft Company, United States) Zenith CH 400 [9] Zenith CH 600;