PZL 103 GAWRON

 

Origin:

Poland

Type:

Single-engine utility aircraft

Engine:

One 194 kw (260 hp) Ivchenko AI-14R nine-cylinder air-cooled radial engine

Specifications:

  • Wingspan: 12.60 m (41 ft 4 in)
  • Length: 9.00 m (29 ft 6 in)
  • Height: 3.12 m (10 ft 3 in)
  • Wing area: 23.86 m² (256.8 sq ft)
  • Max speed: 160 km/h (99 mph)
  • Economical cruising speed: 130 km/h (81 mph)
  • Stalling speed, flaps down: 50 km/h (31 mph)
  • Service ceiling: 3,200 m (10,499 ft)
  • Rate of climb: 180 m/min (590 ft/min)
  • Take-off run in agricultural role: 102 m (335 ft)
  • Landing run in agricultural role: 90 m (295 ft)
  • Range: 525 km (326 miles)
  • Fuel capacity: 180 litres (40 Imp gals)
  • Empty weight: 642 kg (1,415 lb)
  • Loaded weight: 1,660 kg (3,660 lb)
  • Power loading: (14 lb/hp)

Photo source: Wikipedia

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