MX TECHNOLOGIES MX-2

 

ORIGIN:

United States of America

TYPE:

Two-seat high-performance aerobatic monoplane

ENGINE:

One 254 kw (340 hp) Lycoming AEIO-540 six-cylinder horizontally-opposed air-cooled engine

SPECIFICATIONS:

  • Wingspan: 7.32 m (24 ft)
  • Length: 6.55 m (21 ft 6 in)
  • Height: 1.83 m (6 ft)
  • Wing area: 9.48 m² (102.04 sq ft)
  • Max speed: 407 km/h (253 mph)
  • Stalling speed: 108 km/h (67 mph)
  • Max rate of roll: 400 degrees/sec
  • Max G-limit: +/- 14G
  • Rate of climb: 1,067 m/min (3,500 ft/min)
  • Range: 1,669 km (1,037 miles)
  • Take off run: 68 m (223 ft)
  • Fuel capacity: 220 litres (48 Imp gals)
  • Empty weight: 584 kg (1,287 lb)
  • Aerobatic weight: 839 kg (1,850 lb)
  • Loaded weight: 975 kg (2,150 lb)

PHOTO SOURCE:

Rob holland mx2 - MX Aircraft MX2 - Wikipedia