MUDRY CAP 10B

 

ORIGIN:

France

TYPE:

Two-seat light aerobatic training aircraft

ENGINE:

One 134 kw (180 hp) Textron Lycoming AEIO-360-B2F four-cylinder horizontally-opposed air-cooled engine

SPECIFICATIONS:

  • Wingspan: 8.06 m (26 ft 5¼ in)
  • Length: 7.16 m (23 ft 6 in)
  • Height: 2.55 m (8 ft 4½ in)
  • Wing area: 10.85 m² (116.79 sq ft)
  • Max speed at sea level: 270 km/h (168 mph)
  • Max cruising speed at 75% power: 250 km/h (155 mph)
  • Stalling speed, flaps down: 85 km/h (53 mph)
  • Max rate of climb at sea level: 360 m/min (1,180 ft/min)
  • Service ceiling: 5,000 m (16,400 ft)
  • Range with max fuel:1,200 km (745 miles)
  • Empty weight (utility category): 540 kg (1,190 lb)
  • Loaded weight: 830 kg (1,829 lb)

PHOTO SOURCE:

CAP-10B No41 - Mudry CAP 10 - Wikipedia

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