BRAND and MODEL
TL ULTRALIGHT STING TL-2000 CARBON
TYPE
Two-seat light sport monoplane
ORIGIN
Czech Republic
ENGINE
One 80 kw (100 hp) Rotax 912 four-cylinder horizontally-opposed liquid-and-air-cooled engine
SPECIFICATIONS
Wingspan: 8.44 m (27 ft 8 in)
Length: 5.93 m (19 ft 5 in)
Height: 2.3 m (7 ft 6 in)
Wing area: 9.85 m² (106.02 sq ft)
Never exceed speed: 333 km/h (207 mph)
Max speed: 287 km/h (178 mph)
Cruising speed at 75% power at 5,200 rpm: 265 km/h (165 mph)
Cruising speed at 65% power at 5,000 rpm: 245 km/h (152 mph)
Max speed in turbulence: 213 km/h (132 mph)
Stalling speed no flaps: 81 km/h (51 mph)
Stalling speed with 35 deg flaps: 65 km/h (40 mph)
Initial rate of climb: 351 m/min (1,150 ft/min)
Service ceiling: 5,485 m (18,000 ft)
Take-off roll on grass: 75 m (246 ft)
Take-off over 15 m (50 ft) obstacle: 220 m (722 ft)
Landing roll on grass: 100 m (328 ft)
Landing distance over 15 m (50 ft) obstacle: 200 m (656 ft)
Fuel capacity standard: 69 litres (15 imp gals)
Fuel capacity optional: 80 litres (17.7 imp gals)
Empty weight: 290 kg (639 lb)
Max payload: 280 kg (617 lb)
Loaded weight: 560 kg (1,235 lb)
PHOTO
blogspot.com:Source of phothograph
