MOONEY M-20

 

ORIGIN:

United States of America

TYPE:

Light cabin monoplane

ENGINE:

One 149 kw (200 hp) Lycoming IO-360-A1A four-cylinder horizontally-opposed air-cooled engine

SPECIFICATIONS:

  • Wingspan: 10.67 m (35 ft)
  • Length: 7.06 m (23 ft 2 in)
  • Height: 2.55 m (8 ft 4½ in)
  • Wing area: 15.5 m² (166.93 sq ft)
  • Max speed at sea level: 317 km/h (197 mph)
  • Max cruising speed at 2,286 m (7,500 ft): 301 km/h (187 mph)
  • Economical cruising speed at 3,048 m (10,000 ft): 270 km/h (168 mph)
  • Initial rate of climb: 341 m/min (1,120 ft/min)
  • Service ceiling: 5,944 m (19,500 ft)
  • Max range with max fuel: 1,648 km (1,024 miles)
  • Empty weight: 714 kg (1,575 lb)
  • Loaded weight: 1,168 kg (2,575 lb)

PHOTO SOURCE:

Mooney.m20j.g-muni.arp - Mooney M20 – Wikipedia, wolna encyklopedia

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