Tecnam 2010
Overview
The Tecnam P2010 (P Twenty-Ten) is a premier, four-seat high-wing aircraft that seamlessly blends advanced composite technology with classic flight stability. Designed for both superior flight training and comfortable cross-country travel, it features a unique three-door configuration for effortless cabin access and a sleek carbon-fiber fuselage for maximum aerodynamic efficiency.
General characteristics- Garmin G1000
Crew: one
Capacity: three passengers
Length: 26 ft (7.79 m)
Wingspan: 33.79 ft (10.30 m)
Height: 8.66 ft (2.64 m)
Wing area: 149 sq ft (13.9 m2)
Aspect ratio: 7.63
Airfoil: modified NACA 63A
Empty weight: 1,631 lb (740 kg)
Gross weight: 2,557 lb (1,160 kg)
Fuel capacity: 63.4 US gallons (240 litres)
Propellers: 2-bladed Wooden Propeller
Powerplant: 1 × Lycoming IO-360-M1A four cylinder, horizontally opposed aircraft engine, 180hp
Performance
Cruise speed: 134 kts (154 mph; 248 km/h)
Stall speed: 52 kts (59 mph; 96 km/h) (power off, flaps down)
Never exceed speed: 166 kts (191 mph; 307 km/h) (IAS)
Service ceiling: 13,000 ft (3,962 m)
Rate of climb: 784 ft/min (4 m/s)
Range: 591 NM (680 mi; 1,094 km) with 45 minute reserve, 55% Power, at 12,000 ft
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