Wing Span = 9,75 m.
Cabin Width = 1,09 m
Baggage Capacity = 4,24 m3
Rate of Climb = 1800FPM
Cruise = 168 km/h
Stall (Flaps Full) = 51 km/h
Takeoff (Ground Roll) = 45,7 m
Landing (Ground Roll) = 53,3 m
Max Gross (EXP) = 700 kg
kitfoxaircraft.com
Wing Span = 9,75 m.
Cabin Width = 1,09 m
Baggage Capacity = 4,24 m3
Rate of Climb = 1800FPM
Cruise = 168 km/h
Stall (Flaps Full) = 51 km/h
Takeoff (Ground Roll) = 45,7 m
Landing (Ground Roll) = 53,3 m
Max Gross (EXP) = 700 kg
kitfoxaircraft.com
Capacity: 1 passenger + 50 kg baggage
Length: 6.22 m
Wingspan: 8.50 m
Height: 2.15 m
Wing area: 9.94 m2
Gross weight: 472.5 kg
Powerplant: 1 × Rotax 912S 4-cylinder, 4-stroke liquid/air-cooled engine, 75 kW (101 hp)
Max. speed: 230 km/h
Cruise speed: 207 km/h
Service ceiling: 4,572 m
Capacity: 1 passenger + 50 kg baggage
Length: 6.22 m
Wingspan: 8.50 m
Height: 2.15 m
Wing area: 9.94 m2
Gross weight: 472.5 kg
Powerplant: 1 × Rotax 912S 4-cylinder, 4-stroke liquid/air-cooled engine, 75 kW (101 hp)
Max. speed: 230 km/h
Cruise speed: 207 km/h
Service ceiling: 4,572 m
2 × Austro Engine E4 turbocharged diesel engine, 125 kW each. Max speed: 365 km/h
2 × Austro Engine E4 turbocharged diesel engine, 125 kW each. Max speed: 365 km/h
Engine: 1× Pratt & Whitney PT6A-67AG turboprop;
Cruise speed: 356 km/h at 2,440 m
Engine: 1× Pratt & Whitney PT6A-67AG turboprop;
Cruise speed: 356 km/h at 2,440 m
now Vulcanair P68, is a light aircraft designed by Luigi Pascale. It made its first flight on 25 May 1970. The six-seat high-wing monoplane is powered by twin piston engines Lycoming IO-360-A1B6 and is used for light transport and training. Cruise speed: 301 km/h at 3,050 m
now Vulcanair P68, is a light aircraft designed by Luigi Pascale. It made its first flight on 25 May 1970. The six-seat high-wing monoplane is powered by twin piston engines Lycoming IO-360-A1B6 and is used for light transport and training. Cruise speed: 301 km/h at 3,050 m
A two-seater aircraft, a high-wing biplane with a non-retractable undercarriage and a steerable nose wheel. The aircraft is designed for daytime visual flights in normal weather conditions. 100 hp Rotax-912 ULS/ Rotax-912 iS engine. A reliable, safe and time-tested aircraft.
A two-seater aircraft, a high-wing biplane with a non-retractable undercarriage and a steerable nose wheel. The aircraft is designed for daytime visual flights in normal weather conditions. 100 hp Rotax-912 ULS/ Rotax-912 iS engine. A reliable, safe and time-tested aircraft.