BRAND and MODEL
PILATUS P-3
TYPE
Two-seat military training monoplane
ORIGIN
Switzerland
ENGINE
One 194 kw (260 hp) Lycoming GO-435-C2A six-cylinder horizontally-opposed air-cooled engine
SPECIFICATIONS
Wingspan: 10.39 m (34 ft 1 in)
Length: 8.77 m (28 ft 8½ in)
Height: 3.04 m (10 ft)
Wing area: 16.44 m² (177 sq ft)
Max speed at sea level: 309 km/h (192 mph)
Max cruising speed: 275 km/h (170 mph)
Economical cruising speed: 249 km/h (155 mph)
Minimum speed: 100 km/h (62 mph)
Initial rate of climb: 420 m/min (1,378 ft/min)
Service ceiling: 5,499 m (18,040 ft)
Absolute ceiling: 6,100 m (20,000 ft)
Range at economic cruising speed: 750 km (466 miles)
Endurance: 3 hours
Fuel capacity: 319 litres (70.2 Imp gals)
Take-off run over 15 m (50 ft) obstacle: 372 m (1,221 ft)
Take-off run from grass: 430 m (1,290 ft)
Landing distance over 15 m (50 ft) obstacle: 430 m (1,290 ft)
Landing speed 114 km/h to 119 km/h: (71 to 74 mph)
Empty weight: 1,048 kg (2,310 lb)
Loaded weight: 1,497 kg (3,300 lb)
PHOTO
flugzeuginfo.net:Source of phothograph
