PZL WILGA 2000

 

Origin:

Poland

Type:

Light utility aircraft

Engine:

One 224 kw (300 hp) Lycoming IO-540-K1B5 six-cylinder horizontally-opposed air-cooled engine

Specifications:

  • Wingspan: 11.12 m (36 ft 6 in)
  • Length: 8.1 m (26 ft 6 in)
  • Height: 2.58 m (9 ft 7 in)
  • Wing area: 15 m² (161.4 sq ft)
  • Max speed: 208 km/h (129 mph)
  • Cruising speed at 75% power: 190 km/h (118 mph)
  • Stalling speed with flaps and no power: 95 km/h 59 mph
  • Stalling speed with flaps and power: 72 km/h (45 mph)
  • Max rate of climb: 293 m/min (961 ft/min)
  • Service ceiling: 4,120 m (13,517 ft)
  • Range: 1,500 km (932 miles)
  • Endurance: 8 hrs 20 mins
  • Take-off run with full flap: 168 m (551 ft)
  • Landing run: 150 m (492 ft)
  • Fuel capacity: 400 litres (88 Imp gals)
  • Empty weight: 900 kg (1,984 lb)
  • Useful load: 500 kg (1,102 lb)
  • Loaded weight: 1,400 kg (3,086 lb)

Photo source: Wikipedia

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