BRAND and MODEL
TL ULTRALIGHT STREAM
TYPE
Two-seat in tandem light sport monoplane
ORIGIN
Czech Republic
ENGINE
One 80 kw (100 hp) Rotax 912ULS four-cylinder horizontally-opposed liquid-and-air-cooled engine
SPECIFICATIONS
Wingspan: 9 m (29 ft 6 in)
Length: 6.785 m (22 ft 3 in)
Height: 2.48 m (8 ft 1 in)
Never exceed speed: 335 km/h (208 mph)
Max cruising speed: 250 km/h (155 mph)
Take-off speed: 137 km/h 85 km/h (53 mph)
Stalling speed no flaps: 109 km/h (68 mph)
Stalling speed with flaps: 69 km/h (43 mph)
Rate of climb: 360 m/min (1,181 ft/min)
Take-off roll: 175 m (574 ft)
Take-off distance over 15 m (50 ft) obstacle: 295 m (968 ft)
Landing distance over 15 m (50 ft) obstacle: 300 m (984 ft)
Endurance: 5 hours
Fuel consumption at 75% power: 18.5 litres/hr (4.06 Imp gals per hr)
Fuel capacity: 90 litres (19.8 Imp gals)
Range: 1,700 km (1,056 miles)
Empty weight: 297 kg (655 lb)
Useful load: 303 kg (668 lb)
Loaded weight: 600 kg (1,323 lb)
PHOTO
tl-ultralight.cz :Source of phothograph
