PZL KOS

 

Origin:

Poland

Type:

Two-seat light touring and training monoplane

Engine:

One 71 kw (95 hp) Continental C-90-12F four-cylinder horizontally-opposed air-cooled engine

Specifications:

  • Wingspan: 8.50 m (27 ft 9 in)
  • Length: 7 m (22 ft 10 in)
  • Height: 1.88 m (6 ft 2 in)
  • Wing area: 11.05 m² (119 sq ft)
  • Max speed: 193 km/h (120 mph)
  • Cruising speed: 174 km/h (108 mph)
  • Stalling speed flaps down: 77 km/h (48 mph)
  • Rate of climb at sea level: 247 m/min (810 ft/min)
  • Service ceiling: 4,602 m (15,100 ft)
  • Endurance: 4 hrs 15 min
  • Range cruising at 164 km/h (102 mph): 644 km (400 miles)
  • Fuel capacity: 75 litres (16.5 Imp gals)
  • Take-off run: 208 m (682 ft)
  • Empty weight: 404 kg (809 lb)
  • Loaded weight: 630 kg (1,390 lb)

Photo source: Wikipedia

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