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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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