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BRAND and MODEL
CESSNA 120 And 140
TYPE
Two-seat light cabin monoplane
ORIGIN
United States of America
ENGINE
One 63 kw (85 hp) Continental C-85-12 four-cylinder horizontally-opposed air-cooled engine
SPECIFICATIONS
Wingspan: 10 m (32 ft 10 in)
Length: 6.4 m (20 ft 11¾ in)
Height: 1.91 m (6 ft 3¼ in)
Wing area: 14.8 m² (159.3 sq ft)
Max speed: 198 km/h (123 mph)
Cruising speed at 80% power: 171 km/h (106 mph)
Landing speed: 68 km/h (42 mph)
Initial rate of climb: 195 m/min (640 ft/min)
Service ceiling: 4,724 m (15,500 ft)
Stalling speed: 64 km/h (40 mph)
Ceiling: 4,724 m (15,500 ft)
Cruising range: 676 km (420 miles)
Take-off run over 15 m (50 ft) obstacle: 442 m (1,450 ft)
Fuel capacity: 95 litres (21 Imp gals)
Empty weight: 356 kg (785 lb)
Useful load: 302 kg (665 lb)
Loaded weight: 656 kg (1,450 lb)
PHOTO
aviationconsumer.com:Source of phothograph
