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General characteristics
• Crew : one
• Capacity : three passengers
• Length : 27 ft 2 in (8.28 m)
• Wingspan : 36 ft 1 in (11.00 m)
• Height : 8 ft 11 in (2.72 m)
• Wing area : 174 sq ft (16.2 m2)
• Aspect ratio : 7.32
• Airfoil : modified NACA 2412
• Empty weight : 1,691 lb (767 kg)
• Gross weight : 2,450 lb (1,111 kg)
• Fuel capacity : 56 US gallons (212 litres)
• Powerplant : 1 × Lycoming IO-360-L2A four cylinder, horizontally opposed aircraft engine, 160 hp (120 kW)
• Propellers : 2-bladed metal
Performance
• Cruise speed : 122 kn (140 mph; 226 km/h)
• Stall speed : 47 kn (54 mph; 87 km/h) (power off, flaps down)
• Never exceed speed : 163 kn (188 mph; 302 km/h) (IAS)
• Range : 696 nmi (801 mi; 1,289 km) with 45 minute reserve, 55% Power, at 12,000 ft
• Service ceiling : 13,500 ft (4,100 m)
• Rate of climb : 721 ft/min (3.66 m/s)
2010. 12. 21.
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