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Zenith Aircraft CH 701 by Zenith Aircraft Company - Zenair 3.6 66

Zenith Aircraft CH 701

Specifications | Video | More by Zenith Aircraft Company - Zenair | Buy & Sell | Top-10 aircraft | All aircraft Show MoreHIGH WING NOSE WHEEL STOL

Zenith Aircraft CH701 is an all metal STOL (short take-off and landing) aircraft. It features a high-lift wing with fixed full length slots, flaperons, inverted elevator and a flying rudder. The CH 701 was first introduced in 1986.

Large wheels combined with the STOL performance makes it possible to land and take-off from very short fields; however, the thick high-lift wing is not made for high speed, thus the speed performance is low. The CH 701 can be built and flown under the american LSA or the european microlight / ultralight rules.

With the CH701 Zenith aircraft has developed a winning concept for a STOL airplane

Specifications

Empty weight: 580 lbs (263 kg) MTOW: 1100 lbs (499 kg) Stall speed: 26 kts (30 mph) (48 kph) Cruise speed: 78 kts (90 mph) (144 kph) VNE: 96 kts (110 mph) (178 kph) Climb: 1600 ft/min (8.1 m/s) Glide ratio: 8 Take-off distance: 45 ft (14 m) Landing distance: 80 ft (24 m) Engine: Rotax 912S Fuel consumption: 3 GPH (11.4 LPH) For sale for: USD 42,000 / EUR 38,640

Watch 1 Video about the Zenith Aircraft CH 701

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  Zenith Aircraft Company

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