CESSNA 120 And 140

 

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