BRAND and MODEL
TECNAM P-2010
TYPE
Four seat high-wing touring monoplane
ORIGIN
Italy
ENGINE
One 134 kw (180 hp) Lycoming IO-360-M1A four-cylinder horizontally-opposed air-cooled engine
SPECIFICATIONS
Wingspan: 10.30 m (33 ft 8 in)
Length: 7.76 m (25 ft)
Height: 2.70 m (8 ft)
Wing area: 13.90 m² (150 sq ft)
Max speed at sea level: 267 km/h (166 mph)
Cruising speed at 75% power at 1,981 m (6,500 ft): 252 km/h (157 mph)
Stalling speed: 102 km/h (63 mph)
Max rate of climb at sea level: 320 m/min (1,050 ft/min)
Service ceiling: 4,572 m (15,000 ft)
Max range: 1,223 km (760 miles)
Take-off distance at sea level: 245 m (804 ft)
Take off distance to 15 m (50 ft): 384 m (1,260 ft)
Landing distance ground roll: 200 m (656 ft)
Landing distance from 15 m (50 ft): 313 m (1,027 ft)
Fuel capacity: 240 litres (53 Imp gals)
Empty weight: 710 kg (1,565 kg)
Max useful load: 450 kg (992 lb)
Loaded weight: 1,160 kg (2,557 lb)
PHOTO
flugzeug-bild.de:Source of phothograph
