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THE ULTIMATE TRAINER
The Skyleader GP ONE is a 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.
PERFORMANCE SPECS
Never Exceed Speed (VNE)
250 km/h
134 kts
156 mph
Maneuvering Speed (VA)
149 km/h
80 kts
93 mph
Min. Speed with Flaps (VS0)
50 km/h
26 kts
30 mph
KM/H
KNOTS
MPH
SPEEDS
Cruise Speed @ 75% Power (VC)
175 km/h
94 kts
109 mph
Min. Speed without Flaps (VS1)
55 km/h
30 kts
35 mph
Engine Type
Rotax® 912 UL
Propeller
3 blade – on the ground adjustable
ENGINE & PROPELLER
Maximum Power
80HP
Fuel Capacity
105 L / 27.7 US gal / lbs / kg
Range
1200 km / 640 nm / 750 miles
FUEL CAPACITY & ENDURANCE
Endurance
7.0 + 0.5h
Take-off Distance
185 m / 607 Ft
Landing Distance
200 m / 656 Ft
Weight
UL / LSA (up to 600 kg / 1320 lbs.)
TAKE-OFF & LANDING
Take-off Run
110 m / 361 Ft
Landing Run
120 m / 394 Ft
Basic Empty Weight
297.5 kg / 656 lbs.
Wing Span
10.2 m / 33 ft 5.6 in
Overall Height
2.1 m / 6 ft 10.7 in
Aspect Ratio
9.32
DIMENSIONS
Overall Length
6.25 m / 20 ft 6.1 in
Wing Area
11.165 m2 / 120.18 sq. ft
Cabin Width
1.2 m / 3ft 11.3 in
* All data provided in specific configuration (propeller, engine) and under ISA
GALLERY
FULL GALLERY
SKYLEADER GP ONE
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