SKYLEADER 600

 The SKYLEADER 600 is an all metal two-seat, low wing constructed aircraft with a trapezoidal wing. The aircraft has a tricycle towed fixed landing gear with wheel pants and a steerable nose wheel, either retractable gear option. The aircraft are designated mainly for recreational flying, pilot training and special operations.

Aircraft can be customized based on your requirements. You will be impressed by the high safety standards, impressive flight characteristics and timeless design which is the result of real ASTM certified aeronautical production. Easy repairs & maintenance guarantees the low operational costs.


technical data

SPEEDS                                                         KILOMETERS      KNOTS           MILES

Never exceed speed (VNE):                          265 km/h      143 knots        165 mph

Cruise speed @ 75% power (VC):                 220 km/h      122 knots        137 mph

Maneuvering speed (VA):                              145 km/h        78 knots          90 mph

Min. speed without flaps (VS1):                      72 km/h        39 knots          44 mph

Min. speed with flaps (VS0):                            61 km/h        33 knots          37 mph

  

Weight

Weight: UL / LSA up to 600 kg / 1320 lbs.

Basic empty weight: 320 kg / 705 lbs.

 

Engine & propeller

Engine type: Rotax® 912 UL, ULS ; 914 UL ; 912iS fuel injection

Maximum power: (80HP) – 115HP turbocharged

Propeller: 2 or 3 – blade on the ground or in flight adjustable

  

fuel capacity & endurance

Fuel capacity: 120 L / 31.8 US gal / 198 lbs / 90 kg

Endurance: 8.5 + 0.5 h

 

Range: 1600 km / 860 nm / 1000 miles

 

take-off & landing

Take-off distance: 250 m / 820 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 4.5 in

Overall length: 7.1 m / 23 ft 3.5 in

Overall height: 2.46 m / 8 ft

Wing area: 11.85 m2 / 127.5 sq. ft

Aspect ration: 7.78

Cabin width: 1.28 m / 4 ft 2 in

*Values depending on the aircraft configuration



SKYLEADER 400

SKYLEADER aircraft introduces a new mid-line model, the JA-400 a racy ‘sports car-inspired’ aircraft with new features such as side opening canopy, aggressive cowling and easily manouverable fixed gear. Having trapezoidal wings with 80 liters of fuel endurance, available fuel injection and simple instrument panel, it appeals directly to sport aviation enthusiasts. The aircraft is designed for pilot training, recreational flying and for special operations. SKYLEADER 400 adds to the SKYLEADER Family tradition of Safety, Prestige and Emotion!

Techincal data

SPEEDS                                                         KILOMETERS       KNOTS         MILES

Never exceed speed (VNE):                            260 km/h    140 knots         162 mph

Cruise speed @ 75% power (Vc):                   175 km/h       94 knots        109 mph

Maneuvering speed (VA):                                142 km/h       77 knots          88 mph

Min. speed without lift flaps (VS1):                  60 km/h       32 knots          37 mph

Min. speed with lift flaps (VS0):                        53 km/h       28 knots          33 mph

 

weight

Max. take-off weight: UL/ LSA up to 600 kg / 1320 lbs.

Basic empty weight: 320 kg / 705 lbs.

 

engine & propeller

Engine type: Rotax® 912 UL, ULS , Continental O-200D

Maximum power:  80HP – 100HP

Propeller: 2 or 3 blade – on the ground or in flight adjustable

 

fuel capacity & endurance

Fuel capacity:  80 L / 21.1 US gal / 132 lbs / 60 kg

Endurance: 3.5 + 0.5h

Range: 600 km / 320 nm / 370 miles

 

take-off & landing

Take-off distance: 200 m / 660 ft

Landing distance: 200 m / 660 ft

 

 

dimensions

Wing span: 9.1 m

Overall length: 6.3 m

Overall height: 2.36 m

Wing area: 11.47 m2

Aspect ration: 7.78

Cabin width: 1.28 m / 4 ft 2 in

*Values depending on the aircraft configuration


SKYLEADER GP ONE