BRAND and MODEL
ZENAIR CH-801
TYPE
Four-seat light utility aircraft
ORIGIN
United States of America
ENGINE
One 134 kw (180 hp) Lycoming O-360 four-cylinder horizontally-opposed air-cooled engine
SPECIFICATIONS
Wingspan: 9.55 m (31 ft 4 in)
Length: 7.5 m (24 ft 6 in)
Height: 3.0 m (10 ft)
Wing area: 15.5 m² (167 sq ft)
Max speed: 180 km/h (112 mph)
Cruising speed at 75% power at 2,134 m (7,000 ft): 170 km/h (106 mph)
Stalling speed [flaps down]: 56 km/h (35 mph)
Stalling speed [flaps up]: 69 km/h (43 mph)
Rate of climb: 366 m/min ((1,200 ft/min)
Service ceiling: 4,877 m (16,000 ft)
Range [standard fuel]: 515 km (320 miles)
Fuel capacity [standard]: 114 litres (25 imp gals)
Take-off roll: 88 m (290 ft)
Empty weight: 522 kg (1,150 lb)
Useful load: 478 kg (1,050 lb)
Loaded weight:1,000 kg (2,200 lb)
PHOTO
Airliners.net:Source of phothograph
