ZENAIR CH-801

 

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