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TECNAM P2010
SPECIFICATIONS
PERFORMANCE
Max Cruise Speed 146 kts (270 km/h)
Stall Speed (Flaps Down Power Off) 52 kts (96 km/h)
Practical Ceiling 12,000 ft (3658 m)
Take off run 1365 ft (416 m)
Take off distance 2054 ft (626 m)
Rate of climb 784 ft/min (4 m/sec)
Landing Run 778 ft (237 m)
Landing Distance 1709 ft (521 m)
Range 591 NM (1094 km)
WEIGHT & LOADING
Maximum Take Off Weight 2,557 lb (1,160 kg)
Empty Weight, Standard** 1,698 lb (770 kg)
Useful Load 860 lb (390 kg)
Fuel tank capacity 64 US Gal (240 lt)
Baggage allowance 88 lb (40 kg)
POWERPLANT
Engine Manufacturer Lycoming IO-390-C3B6
Engine Power 215 HP
Propeller 3 Bladed VP Propeller
Fuel Consumption 11 USG/hr (42 lt/hr)
Fuel Type Avgas
DIMENSIONS
EXTERIOR
Length 25.98 ft (7,92 m)
Height 8.66 ft (2,64 m)
Wingspan 33.79 ft (10,3 m)
Area 149 ft2 (13,9 m2)
INTERIOR
Door Width 33.86 in (860 mm)
Door Height 36.61 in (930 mm)
Cabin Width 3.74 ft (1.14 m)
Cabin Length 7.54 ft (2.3 m)
Max Seating capacity 4
CERTIFICATIONS
CS23/FAR23
