BRAND and MODEL
TL ULTRALIGHT STING S-4
TYPE
Two-seat light sport aircraft
ORIGIN
Czech Republic
ENGINE
One 60 kw (80 hp) Rotax 912 four-cylinder, four-stroke, liquid-and-air-cooled, dual carburettor, electronic ignition engine
SPECIFICATIONS
Wingspan: 8.44 m (27 ft 6 in)
Length: 5.93 m (19 ft 5 in)
Height: 2.3 m (7 ft 6 in)
Wing area: 9.8 m² (105 sq ft)
Max speed: 280 km/h (175 mph)
Economical cruising speed: 120 km/h (75 mph)
Max cruising speed: 260 km/h (165 mph)
Stalling speed with flaps: 62 km/h (39 mph)
Rate of climb: 480 m/min (1,575 ft/min)
Fuel capacity [standard]: 69 litres ( 15 imp gals)
Fuel capacity [optional]: 100 litres (22 imp gals)
Empty weight: 300 kg (661 lb)
Loaded weight: 540 kg (1,190 lb)
PHOTO
Airliners.net:Source of phothograph
