MRAZ M-1C SOKOL

 

ORIGIN:

Czechoslovakia

DESCRIPTION:

Three-seat light sport monoplane

POWER PLANT:

One 78 kw (105 hp) Walter Minor 4-III four-cylinder in-line air-cooled engine

SPECIFICATIONS:

  • Wingspan: 10.02 m (32 ft 9¾ in)
  • Length: 7.34 m (24 ft 1 in)
  • Height: 1.98 m (6 ft 5 in)
  • Wing area: 13.79 m² (148.5 sq ft)
  • Max speed at sea level: 241 km/h (150 mph)
  • Cruising speed: 212 km/h (132 mph)
  • Initial rate of climb: 200 m/min (656 ft/min)
  • Ceiling: 4,999 m (16,400 ft)
  • Range at cruising speed: 579 km (360 miles)
  • Max range: 998 km (620 miles)
  • Empty weight: 408 kg (900 lb)
  • Loaded weight: 774 kg (1,707 lb)

PHOTO SOURCE:

File:MRAZ M.1C Sokol OK-AHN (8191924330).jpg - Wikimedia Commons

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