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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 in July 2009.

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