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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 ...
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.
The CH 601 HD (for heavy duty) was the follow-on to the original CH 600 and incorporated many improvements to the design. The HD version had a gross weight of 1200 lbs and a standard empty weight of 530 lbs. Aircraft kits were marketed by Zenair of Midland, Ontario in Canada and by Zenith Aircraft of Mexico, Missouri. [33] Zenair CH 601 HDS
A typical purpose-designed light STOL aircraft, the Zenith STOL CH 701 This is a list of aircraft which are classified as having Short Takeoff and Landing, or STOL , characteristics. The STOL class excludes vertical takeoff and landing ( VTOL ) types, rotorcraft , aerostats and most light aircraft .
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.
In 1996, Chris Heintz and Zenair Ltd. obtained FAA type-certification for the Zenith CH 2000, a two-seat low-wing aircraft based on his kit aircraft designs. Aircraft Manufacturing and Design (AMD) manufactures this aircraft as the AMD Alarus CH 2000. AMD also produces the CH 601 XL as a Light-sport aircraft (LSA).
The Mono-Z CH 100 is similar to the Zenith that preceded it, a low-winged cantilever monoplane of all metal construction. The aircraft features a large cockpit for taller pilots, with a pilot and baggage combined weight allowance of 240 lb (109 kg) and removable wings for storage and towing the aircraft behind a car.
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