Zenair CH 300 explained

The Zenair Tri-Z CH 300 is a three-seat Canadian homebuilt light aircraft. A single-engined low-winged monoplane, the CH 300 first flew in 1977, with several hundred kits sold.

Development and design

The CH 300 is an enlarged three-seat derivative of the Zenair Zenith CH 200, designed by Chris Heintz in the mid 1970s as the Tri-Zénith.[1] Like the CH 200, it is a low-winged monoplane of all-metal construction with a fixed nosewheel undercarriage, but is larger and more powerful, and is fitted with a rear bench seat capable of accommodating a third adult or two children, and is fitted with a forward sliding canopy. It is designed to be powered by an engine giving between 125 and 180 hp (93 and 134 kW).[2]

The first example made its maiden flight on 9 July 1977, with over 400 sets of plans sold by 1982. One CH 300, modified with extra fuel tanks and piloted by Robin "Red" Morris, made a non-stop trans-Canada flight between Vancouver International Airport and Halifax International Airport on 1–2 July 1978, covering the 2,759 mile (4,440 km) in 22 hours, 44 mins, setting three FAI Class C-1c point-to-point speed records.[3]

Plans for the CH 300 remained on sale in 1999.[4] The Zenair CH 300 formed the basis for the factory built Zenair CH-2000, which first flew in 1993.[4] [5]

Variants

CH 300
  • Basic model with tricycle landing gear
    CH 300 TD
  • "Taildragger" model with conventional landing gear

    Aircraft on display

    References

    Notes and References

    1. Taylor 1976, p.458.
    2. [Zenair]
    3. "List of records established by the 'Zenair Tri-Z'". Fédération Aéronautique Internationale. Retrieved 27 February 2010.
    4. Taylor 1999, p.535.
    5. Taylor 1999, p.401.
    6. Web site: Zenair CH-300 Tri-Z. 9 June 2012. Canada Aviation and Space Museum. n.d..