SKYLEADER GP ONE

The SKYLEADER is carbon-composite two-seat

carbon-composite two-seat

Max speed
250 km/h

Range
1200 km

Category
664 lbs

Capacity
2

Carbon-compositetwo-seater high-wing monocoque

The SKYLEADER is carbon-composite two-seat, high wing aircraft with a monocoque construction. The aircraft has a tricycle towed fixed landing gear with wheel pants and a steerable nose wheel. This aircraft is designated mainly for pilot training and low-cost flying.

The aircraft is delivered with a wide range of standard equipment. You will be impressed by the use of high quality materials and great flight characteristics. Easy repairs & maintenance guarantees low operational costs.

Simply: Our aircraft provide safety, prestige and emotion to customers around the world.

Photogallery

Technical data

Speeds Kilometers Knots Miles
Never exceed speed (VNE) 250 km/h 134 knots 156 mph
Cruise speed @ 75% power (VC) 175 km/h 94 knots 109 mph
Maneuvering speed (VA) 149 km/h 80 knots 93 mph
Min. speed without lift flaps (VS1) 55 km/h 30 knots 35 mph
Min. speed with lift flaps (VS0) 50 km/h 26 knots 30 mph
Weight
Max. take-off weight UL / LSA (up to 600 kg / 1320 lbs.)
Basic empty weight 297.5 kg / 656 lbs.
Engine & Propeller
Engine type Rotax® 912 UL
Maximum power 80HP
Propeller 3 blade  – on the ground adjustable
Fuel capacity & Endurance
Fuel capacity 105 L / 27.7 US gal / lbs / kg
Endurance 7.0 + 0.5h
6,1+0,5h 1200 km / 640 nm / 750 miles
Take-off & Landing
Take-off distance 185 m / 607 Ft
Take-off run 110 m / 361 Ft
Landing distance 200 m / 656 Ft
Landing run 120 m / 394 Ft
Dimensions
Wing span 10.2 m / 33 ft 5.6 in
Overall length 6.25 m / 20 ft 6.1 in
Overall height 2.1 m / 6 ft 10.7 in
Wing area 11.165 m2 / 120.18 sq. ft
Aspect ration 9.32
Cabin width 1.2 m / 3ft 11.3 in

*Values depending on the aircraft configuration