BRAND and MODEL
SISLER SF-2A CYGNET
TYPE
Two-seat light sport aircraft
ORIGIN
United States of America
ENGINE
One 45 kw (60 hp) Hapi [1,834 cc] converted Volkswagen four-cylinder horizontally-opposed air-cooled engine
SPECIFICATIONS
Wingspan: 9.14 m (30 ft)
Length: 5.79 m (19 ft)
Height: 1.78 m (5 ft 10 in)
Wing area: 11.60 m² (124.8 sq ft)
Max speed: 174 km/h (108 mph)
Cruising speed at 2,440 m (5,000 ft): 161 km/h (100 mph)
Stalling speed power on: 68 km/h (42 mph)
Max rate of climb at sea level: 177 km/h (580 ft/min)
Take-off and landing run: 213 m (700 ft)
Range: 483 km (300 miles)
Fuel capacity: 57 litres ((12 Imp gals)
Empty weight: 265 kg (585 lb)
Loaded weight: 499 kg (1,100 lb)
PHOTO
flickr.com:Source of phothograph
