ROBIN R2120

 

Origin:

France / New Zealand

Type:

Two-seat light touring and training aircraft

Engine:

One 88 kw (118 hp) Textron Lycoming O-235-L-2A four-cylinder horizontally-opposed air-cooled engine

Specifications:

  • Wingspan: 8.33 m (27 ft 4 in)
  • Length: 6.64 m (21 ft 9½ in)
  • Height: 2.13 m (7 ft)
  • Wing area: 12.50 m² (134.5 sq ft)
  • Cruising speed at 2,591 m (8,500 ft) at 75% power: 193 km/h (120 mph)
  • Ceiling: 4,572 m (15,000 ft)
  • Max rate of climb at sea level: 192 m/min (630 ft/min)
  • Take-off run: 230 m (754 ft)
  • Range at 65% power: 944 km (586 miles)
  • Range at 75% power: 850 km (528 miles)
  • Fuel capacity: 120 litres (26 imp gals)
  • Take-off distance over 15 m (50 ft) obstacle: 490 m (1,608 ft)
  • Landing distance over 15 m (50 ft) obstacle: 480 m (1,575 ft)
  • Empty weight: 544 kg (1,199 lb)
  • Useful load: 256 kg (565 lb)
  • Loaded weight: 800 kg (1,764 lb)

Photo source: Peter Lewis 2009

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