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.<!-- reference -->
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General characteristics
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|crew=1
|capacity=3 passengers
|length m=7.40
|length ft=
|length in=
|length note=
|span m=10.42
|span ft=
|span in=
|span note=
|height m=2.70
|height ft=
|height in=
|height note=
|wing area sqm=16.40
|wing area sqft=
|wing area note=
|aspect ratio=6.7:1
|airfoil=NACA 23012
|empty weight kg=670
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=1100
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=160 L (35.2 Imp Gallons)
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Powerplant
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|eng1 number=1
|eng1 name=Continental IO-360
|eng1 type=air-cooled flat-six
|eng1 kw=<!-- prop engines -->
|eng1 hp=210<!-- prop engines -->
|eng1 note=
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Performance
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|max speed kmh=
|max speed mph=
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|max speed mach=<!-- supersonic aircraft -->
|cruise speed kmh=225
|cruise speed mph=
|cruise speed kts=
|cruise speed note=max cruise at 1,800 m (5,900ft)
|stall speed kmh=64.5<!-- aerobatic -->
|stall speed mph=<!-- aerobatic -->
|stall speed kts=
|stall speed note=flaps down
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=800
|range miles=
|range nmi=
|range note=(max fuel)
|endurance=<!-- if range unknown -->
|ceiling m=6000
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|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|glide ratio=<!-- sailplanes -->
|climb rate ms=
|climb rate ftmin=1180
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|sink rate ms=<!-- sailplanes -->
|sink rate ftmin=<!-- sailplanes -->
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|wing loading lb/sqft=
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References
;Notes
;BIbliography
- Taylor, John W. R. Jane's All The World's Aircraft 1971–72. London:Jane's Yearbooks,1971. .