BRAND and MODEL
CESSNA 400 CORVALIS
TYPE
Business and touring monoplane
ORIGIN
United States of America
ENGINE
One 230 kw (310 hp) Teledyne Continental TSIO-550-C six-cylinder, horizontally-opposed, turbocharged, fuel-injected, air-cooled engine
SPECIFICATIONS
Wingspan: 11 m (36 ft 1 in)
Length: 7.67 m (25 ft 2 in)
Height: 2.74 m (9 ft)
Wing area: 13.1 m² (141 sq ft)
Max speed: 435 km/h (270 mph)
Stalling speed: 111 km/h (69 mph)
Rate of climb at sea level: 427 m (1,400 ft/min)
Max operating altitude: 7,620 m (25,000 ft)
Fuel capacity: 280 kg (617 lb)
Take-off roll: 390 m (1,280 ft)
Landing roll: 384 m (1,260 ft)
Max range: 2,315 km (1,439 miles)
Empty weight: 1,157 kg (2,250 lb)
Useful load: 476 kg (1,050 lb)
Loaded weight: 1,633 kg (3,600 lb)
PHOTO
aeroweb.cz:Source of phothograph
