BRAND and MODEL
CESSNA 0-2
TYPE
Forward air control and psychological warfare aircraft
ORIGIN
United States of America
ENGINE
Two 157 kw (210 hp) Continental IO-360-D six-cylinder horizontally-opposed air-cooled engines
SPECIFICATIONS
Wingspan: 8.53 m (28 ft)
Length: 8.9 m (29 ft 2 in)
Height: 2.89 m (9 ft 5 in)
Wing area: 18.8 m² (202.5 sq ft)
Max speed (Vne): 353 km/h (219 mph)
Cruising speed: 259 km/h (161 mph)
Stalling speed: 109 km/h (68 mph)
Initial rate of climb: 360 m/min (1,180 ft/min)
Service ceiling: 5,182 m (17,000 ft)
Fuel capacity: 462 litres (101.6 Imp gals)
Empty weight: 1,383 kg (3,048 lb)
Useful load: 817 kg (1,802 lb)
Loaded weight: 2,200 kg (4,850 lb)
PHOTO
midamericaflightmuseum.com:Source of phothograph
