Английская Википедия:Canadian Phase I

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Шаблон:Short description Шаблон:Use dmy dates Шаблон:Use Canadian English

The Canadian Phase I is a Canadian powered parachute that was designed and produced by Canadian Powered Parachutes of Vegreville, Alberta, introduced in 2000.[1]

Design and development

The aircraft was designed to comply with Canadian basic ultralight rules. It features a parachute-style high wing made from rip-stop nylon, two seats in tandem accommodation, tricycle landing gear and a single Шаблон:Convert Rotax 582 engine in pusher configuration.[1]

The aircraft is built from bolted-together aluminium tubing. Inflight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw. On the ground the aircraft has lever-controlled nosewheel steering. The main landing gear incorporates shock absorber-type suspension. The standard canopy supplied was the Quantum Advantage High Performance of Шаблон:Convert area. This canopy provides a cruise speed of Шаблон:Convert and a payload of Шаблон:Convert. A larger canopy of Шаблон:Convert that provides a slower cruise speed of Шаблон:Convert, a slower stall speed, a higher rate of climb and a payload of Шаблон:Convert was also available.[1]

Factory optional equipment included a windshield, snow skis for winter operations, electric starting, a canopy-monitoring mirror and an agricultural aircraft kit.[1]

Specifications (Phase I with Quantum Advantage High Performance wing)

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References

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  1. 1,0 1,1 1,2 1,3 Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page D-5. Cybair Limited Publishing, 2001. Шаблон:ISBN