BRAND and MODEL
CIRRUS SR-20
TYPE
Four-seat cabin monoplane
ORIGIN
United States of America
ENGINE
One 149 kw (200 hp) Teledyne Continental IO-360-ES six-cylinder horizontally-opposed air-cooled engine
SPECIFICATIONS
Wingspan: 10.88 m (35 ft 7 in)
Length: 8.01 m (26 ft 3 in)
Height: 2.83 m (9 ft 3 in)
Wing area: 12.54 m² (135 sq ft)
Cruising speed at 75% power at 1,981 m (6,500 ft): 296 km/h (184 mph)
Rate of climb: 305 m/min (1,000 ft/min)
Service ceiling: 4,877 m (16,000 ft)
Stalling speed with flaps: 100 km/h (62 mph)
Range with 45 mins reserve: 1,482 km (921 miles)
Empty weight: 816 kg (1,800 lb)
Loaded weight: 1,315 kg (2,900 lb)
PHOTO
de.academic.ru:Source of phothograph
