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Aero Boero AB-210

By Wikipedia,
the free encyclopedia,

http://en.wikipedia.org/wiki/Aero_Boero_AB-210

The Aero Boero AB-210 is an Argentine civil utility aircraft, a development of the AB-180 with improved performance delivered by a fuel-injected engine. Unlike previous aircraft by this manufacturer, it also featured tricycle undercarriage, but retained the same general high-wing configuration. Only a single prototype was built, first flying on 22 April 1971.

The aircraft was later re-engined with a more powerful Lycoming O-540 and redesignated the AB-260 (not to be confused with the unrelated Aero Boero 260AG). A second example was also built to this standard, but no serial production ensued.

Specifications (AB-210)

General characteristics

  • Crew: one, pilot
  • Capacity: 3 passengers
  • Length: 7.40 m (24 ft 3 in)
  • Wingspan: 10.40 m (34 ft 1 in)
  • Height: 2.70 m (8 ft 10 in)
  • Wing area: 16.4 m² (176 ft²)
  • Empty: 670 kg (1,474 lb)
  • Loaded: kg ( lb)
  • Maximum takeoff: 1,100 kg (2,420 lb)
  • Powerplant: 1x Continental IO-360, 155 kW (210 hp)

Performance

  • Maximum speed: 240 km/h (150 mph)
  • Range: 800 km (500 miles)
  • Service ceiling: m ( ft)
  • Rate of climb: 360 m/min (1,180 ft/min)
  • Wing loading: kg/m² ( lb/ft²)
  • Power/Mass: kW/kg ( hp/lb)





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Published - July 2009














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