BRAND and MODEL
DOVA SKYLARK
TYPE
Two-seat light sport monoplane
ORIGIN
Canada
ENGINE
One 75 kw (100 hp) Rotax 912ULS four-cylinder horizontally-opposed liquid-and-air-cooled engine
SPECIFICATIONS
Wingspan: 8.14 m (26 ft 7 in)
Length: 6.62 m (21 ft 7 in)
Wing area: 9.44 m² (101.61 sq ft)
Cruising speed at 75% power: 222 km/h (138 mph)
Stalling speed: 67 km/h (41 mph)
Rate of climb: 366 m/min (1,200 ft/min)
Take-off distance over 15 m (50 ft) obstacle: 152 m (500 ft)
Landing distance over 15 m (50 ft) obstacle: 162 m (530 ft)
Fuel capacity: 90 litres (20 Imp gals)
Range with reserve: 889 km (552 miles)
Empty weight: 300 kg (661 lb)
Useful load: 300 kg (661 lb)
Loaded weight: 600 kg (1,323 lb)
Baggage capacity: 20 kg (44 lb)
PHOTO
aviastock.com:Source of phothograph
