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 400 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 500

The SKYLEADER 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.

Techincal data

SPEEDS                                                         KILOMETERS       KNOTS         MILES

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

Cruise speed @ 75% power (Vc):                   195 km/h       105 knots        122 mph

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

Min. speed without lift flaps (VS1):                  65 km/h       35 knots          40 mph

Min. speed with lift flaps (VS0):                        58 km/h       31 knots          36 mph

 

weight

Max. take-off weight: UL/ LSA up to 580 kg / 1278 lbs.

Basic empty weight: 311 kg / 686 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:  90 L / 23.8 US gal / 143 lbs / 67 kg

Endurance:  6.5+0.5h

Range: 1100 km / 590 nm / 680 miles

 

take-off & landing

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

*Values depending on the aircraft configuration

SKYLEADER GP ONE

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.

Techincal 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):                        55 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, ULS 

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

Range: 1200 km / 640 nm / 750 miles

 

take-off & landing

Take-off distance: 185 m / 607 ft

Take-off run: 110m/ 361 Ft

Landing distance: 200 m / 656 ft

Landing run: 120m/ 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

SKYLEADER 200

The SKYLEADER 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.

Techincal data

SPEEDS                                                         KILOMETERS       KNOTS              MILES

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 lift flaps (VS1):                  71 km/h       38 knots          44 mph

Min. speed with lift flaps (VS0):                        50 km/h       27 knots          31 mph

 

weight

Max. take-off weight: 450 kg / 992 lbs. (472.5 kg / 1042 lbs. with parachute system)

Basic empty weight: 298 kg / 657 lbs.

 

engine & propeller

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

 

fuel capacity & endurance

with additional tanks: 90 L / 23.8 US gal / 143 lbs / 67 kg
Endurance: 5.5+0.5h

Range: 1050 km / 570 nm / 650 miles

 

take-off & landing

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

*Values depending on the aircraft configuration

SKYLEADER 200

UL-39 is an carbon-composite two-seat, low wing aircraft with non-convetional „Jet“ drive. The aircraft has tricycle retractable landing gear with steerable nose wheel. UL-39 is designed for operation in Ultralight (UL) category. During the construction was as well taken in consideration compliance with requirement of category CS-VLA. 

This ultralight airplane, powered by an unconventional power plant, consisting of a reciprocating internal combustion engine driving the fan, was conceived through the cooperation of the staff and students of the Department of Aerospace Engineering at the Faculty of Mechanical Engineering of the Czech Technical University Prague, and the companies LA composite, s.r.o., and Zall JIHLAVAN airplanes, s.r.o. When completed, this completely new and thus far never implemented concept of an ultralight airplane will off er the market the properties of a jet airplane in the ultralight category, where conventional jet propulsion with hot exhaust gases is not possible, due to legal constraints.

Techincal data

Maximum power: 142kW (193 PS)

 

SPEEDS                                                         KILOMETERS       KNOTS             

Never exceed speed (VNE):                            300 km/h       162 knots          

                                     (Vh):                               260 km/h       140 knots       

                                     (VC):                               230 km/h       124 knots      

Min. speed with lift flaps (VS0)                       65 km/h         35 knots         

 

weight

Basic empty weight: 322Kg / 722 Ibs

 

engine & propeller

Engine type: BMW S1000RR

 

fuel capacity & endurance

Fuel capacity:  100L/ 26,4 US gal
Endurance: 2.5 hours

Range: 550km/ 297 nm