FISHER DAKOTA HAWK

 

BRAND and MODEL
FISHER DAKOTA HAWK
TYPE
Two-seat light touring and training aircraft
ORIGIN
United States of America
ENGINE
One 60 kw (80 hp) Rotax 912UL four-cylinder, four-stroke, liquid-and-air-cooled engine
SPECIFICATIONS

Wingspan: 8.69 m (28 ft 6 in)

Length: 6.02 m (19 ft 9 in)

Height: 1.85 m (6 ft 1 in)

Wing area: 11.89 m² (128 sq ft)

Max speed: 193 km/h (120 mph)

Cruising speed: 145 km/h (90 mph)

Max cruising speed: 161 km/h (100 mph)

Stalling speed: 56 km/h (35 mph)

Initial rate of climb: 244 m/min (800 ft/min)

Service ceiling: 3,048 m (10,000 ft)

Range: 402 km (250 miles)

Fuel capacity: 45 litres (10 Imp gals)

Take-off run: 107 m (350 ft)

Landing run: 122 m (400 ft)

Empty weight: 272 kg (600 lb)

Useful load: 249 kg (550 lb)

Loaded weight: 522 kg (1,150 lb)

PHOTO
airwar.ru:Source of phothograph