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    Zenith STOL CH 701 - Wikipedia

    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. The CH 701 first flew in 1986 and the design is still in production. The CH 750 was first introduced in 2008. The CH … See more

    Designed for off-runway operations, the all-metal CH 701 has many features that contribute to the aircraft's capabilities, such as a high-lift wing with full-span, non-movable leading edgeSee more

    STOL CH 701 Original version. 960lbs gross and 10 gal header tank. steel spring gear and Rotax 503. STOL CH 701SP Comes with two … See more

    Data from Jane's All The World's Aircraft 1993-94 and Zenith Aircraft
    General characteristics
    • Crew: two
    • Length: 20 ft 11 in (6.38 m) See more

    Variants image
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    By the fall of 2007, 750 CH 701s had been completed and were flying. In July 2014, representatives of the company gathered volunteers of the … See more

    India
    Indian Air Force - ordered 85 aircraft, with options for a further 48 for use by the National Cadet Corps with … See more

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  2. Introduction STOL CH 701 - Zenith Aircraft Company

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    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. The CH 701 first flew in 1986 and the design is still in production. The CH 750 was first introduced in 2008.
    en.wikipedia.org/wiki/Zenith_STOL_CH_701
    The STOL CH 701 has the unique distinction of being what is probably the most copied light aircraft in production today. Several dozen unauthorized versions have been produced around the world.
    en.wikipedia.org/wiki/Zenith_STOL_CH_701
    Optional equipment Utility Options such as skis, floats, amphibious floats, etc. are available from Zenair for a variety of uses. Caution: The installation of skis floats, amphibious floats, or other equipment will change pilot must obtain proper the performance and characteristics of the STOL CH 701. Page 24 (close to their attachment points).
    www.manualslib.com/manual/1590562/Zenair-Stol-Ch-70…
    WING DESIGN: The STOL CH 701 uses a special airfoil design to achieve very high lift, low stall speeds, and high strength. A thick wing, full-length leading-edge slats and trailing edge Junker type flaperons develop a maximum wing lift coefficient of 3.10, while maintaining a short wing-span of 27 feet.
    www.zenithair.com/stolch701/7-design.html
  4. STOL CH701 Design - Zenith Aircraft Company

  5. ZENAIR STOL CH 701 AIRCRAFT FLIGHT MANUAL | ManualsLib

  6. STOL CH 701 Drawings & Manuals - Zenith Aircraft Company

  7. 2021: The Year of the STOL CH 701 - Zenith

  8. STOL CH 701 Design - Zenith Air

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