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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.
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 ...
Zenith CH 650 Modernized version of the 601, with a larger cockpit, a larger canopy with more headroom, swept-back fin and rudder and engine options that include the 120 hp (89 kW) Jabiru 3300, 100 hp (75 kW) Continental O-200 and 100 hp (75 kW) Rotax 912ULS. One hundred had been completed and flown by December 2011. [1] [37] [38] Zenith CH 650E
The C90 was introduced in 1947 as a follow-on to the A65, which had been in production since 1939. [7] [8] Many of the designs powered by the C90 are upgraded variants of earlier A65 powered designs, such as the Piper J-3 Cub and PA-11 Cub Special, [9] Aeronca 7AC, [3] and Luscombe 8A. [10] The engine was developed from the earlier O-190 by increasing the stroke 1 ⁄ 4 inch.
They were joined in 1921 by Eugene F. McDonald, [4] and Zenith Radio Company was incorporated in 1923. The fledgling company soon became known for its high-quality radios and electronic innovations. Zenith introduced the first portable radio in 1924, [4] [5] the first mass-produced AC radio in 1926, [5] and push-button tuning in 1927. [4]
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. [1] [2] The CH 750 was first introduced in 2008. [3]
In 2011 the kit cost US$28,995, while finishing a completed aircraft was estimated to cost between US$45,000 to $99,000, depending on options, engine and avionics installed. In December 2011 there were 50 completed and flying. [1] [2]
Data from AMD Website General characteristics Crew: one Capacity: one passenger Length: 23 ft 0 in (7.01 m) Wingspan: 28 ft 10 in (8.79 m) Height: 6 ft 10 in (2.08 m) Wing area: 137 sq ft (12.7 m 2) Empty weight: 1,085 lb (492 kg) basic VFR-equipped Max takeoff weight: 1,692 lb (767 kg) Fuel capacity: 28 US Gallons (106 litres) Powerplant: 1 × Lycoming O-235-N2C four cylinder, horizontally ...