Skyleader 200

 

skyleader 200 info

Velocitats

Never exceed speed (VNE) 260 km/h 140 knots 162 mph
Cruise speed @ 75% power (Vc) 220 km/h 119 knots 137 mph
Maneuvering speed (VA) 142 km/h 77 knots 88 mph
Min. speed without flaps (VS1) 71 km/h 38 knots 44 mph
Min. speed with flaps (VS0) 50 km/h 27 knots 31 mph

Pesos

Max. take-off weight 450 kg / 992 lbs. (472.5 kg / 1042 lbs. with parachute system)
Basic empty weight 298 kg / 657 lbs.

Motor i helix

Engine type Rotax® 912 UL, ULS ; 914 UL ; 912iS fuel injection
Maximum power 80HP - 115HP turbocharged
Propeller 2 or 3-blade ground or in flight adjustable

Combustible i autonomia

Fuel capacity 64 L / 16.9 US gal / 102 lbs / 46 kg
with additional tanks 90 L / 23.8 US gal / 143 lbs / 67 kg
Endurance 3.5+0.5h (standard) / 5.5+0.5h (additional tanks)
Range 760 km / 410 nm / 472 miles (standard) /
1050 km / 570 nm / 650 miles (w/ additional tanks)

Enlairament i aterratge

Take-off distance 185-200 m / 600 - 660 ft
Take-off run 90-100 m / 300 - 330 ft
Landing distance 200 m / 660 ft
Landing run 100 m / 330 ft

Dimensions

Wing span 9.9 m / 32 ft 5,5 in
Overall length 7.0 m / 23 ft 7,5 in
Overall height 2.6 m / 7 ft 2,6 in
Wing area 11.85 m2 / 127.5 sq. ft
Aspect ration 7.78
Cabin width 1.18 m / 3ft 10.5 in

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