BRAND and MODEL
EVEKTOR HARMONY
TYPE
Two-seat light sport and training aircraft
ORIGIN
Czech Republic
ENGINE
One 75 kw (100 hp) Rotax 912S-4 four-cylinder horizontally-opposed liquid-and-air-cooled engine
SPECIFICATIONS
Wingspan: 8.2 m (26 ft 10 in)
Length: 5.98 m (19 ft 6 in)
Height: 2.34 m (7 ft 7 in)
Width: 1.04 m (3 ft 4 in)
Wing area: 10.13 m² (109.04 sq ft)
Never exceed speed: 270 km/h (168 mph)
Max level speed: 240 km/h (149 mph)
Max cruising speed: 205 km/h (127 mph)
Stalling speed: 80 km/h (50 mph)
Max rate of climb: 300 m/min (984 ft/min)
Service ceiling: 5,000 m (16,404 ft)
Take-off run: 130 m (426 ft)
Landing run: 240 m (787 ft)
Range: 720 km (447 miles)
Fuel capacity: 67 litres (14.7 Imp gals)
Empty weight: 330 kg (728 lb)
Loaded weight: 575 kg (1,268 lb)
PHOTO
evektor.cz:Source of phothograph
