Sirius 3000 - 2 seater UL/LSA Category

Sirius the high-wing carbon composite aircraft focused on comfort. TL-Ultralight stands the experience of more than 700 of its low-wing siblings, the Star and the Sting. Ideas of larger fly deck with ultramodern equipment, unlimited aircraft view and surprisingly large luggage compartment have been added. Considered comfort for well-built pilots and passenger. Sirius minimum of vibrations and noise will surprise you. Space, deluxe body-countoured seats, perfect door lock system and convenient fly deck access will take your breath away. The word "comfort" will be on your mind everytime. Pilots may appreciate the dual yoke control of the aircraft, whilst passenger will fall in love with the generous luggage space. The Sirius will give you true sense of freedom in the air. It is prestigious aircraft, be it touring or sport.

Sirius 3000 technical data:

Length	6,97 m
Height	2,30 m
Wing span	9,4 m
Wing area	11,26 m2
Horizontal tail width	2 m
Horizontal tail area	2,68 m2
Vertical tail area	1,45 m2
Cabin width	1,13 m
Never exceed speed	253 km/h
Cruising speed	180 – 220 km/h
Minimum speed	59 km/h
Climb rate (max. TOW)	5 m/s
Empty weight (according to type)	297 kg
Maximum take-off weight	600 kg
Minimum crew weight	60 kg
Maximum crew weight	180 kg
Maximum luggage weight	25 kg
Fuel consumption (75% max. continuous power)	16,2 l/h
Fuel tank capacity	120 l or 90 l
Flying range	Max. 2000 km

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All metal, low wing two seater

The SKYLEADER 400 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.

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

Speeds	Km/h	Knots
Never exceed speed (VNE)	260	140
Cruise speed @ 75% power (Vc)	175	94
Maneuvering speed (VA)	142	77
Min. speed without lift flaps (VS1)	60	32
Min. speed with lift flaps (VS0)	53	28

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 (120) l / 21.1 (31,7)US gal / 132 (197)lbs / 59,5 (89,3)kg
Endurance	4,5 (7) + 0.5h
Range	850 (1250) km / 460 (675) nm / 530 (775) 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 / 4ft 2 in

*Values depending on the aircraft configuration

You can CONTACT US for more information.

All metal, low wing two seater

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.

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

Speeds	Km/h	Knots
Never exceed speed (VNE)	265	143
Cruise speed @ 75% power (VC)	220	122
Maneuvering speed (VA)	145	78
Min. speed without flaps (VS1)	72	39
Min. speed with flaps (VS0)	61	33

Weights
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

Takeoff & 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

You can CONTACT US for more information.

Sting S4 - 2 seater UL/LSA Category

Sting S4 builds on the experience of the Sting carbon, proven and well tested model. The legend, produced in nearly 400 units, has been innovated and improved on. We have collected more than 10 years of experience with this aircraft, and now we have managed to fine-tune it into perfection. Proven and popular features we have kept, while listened to the pilots and owners of the Sing carbon aircraft and taken into account all of their valuable feedback. In the end of this thorough process, the new Sting S4 was born. Do to sophisticated aerodynamic refinements, the Sting S4 is a fine competitor in speed to the Sting RG with retractable landing gear. Effortless maneuverability and high comfort make this aircraft suitable for all ages. It will leave you with impressions of agility and elegance. The Sting S4 is an unrivaled aircraft, be it traveling or sport.

Sting S4 technical data:

Length	6,45 m
Height	2,05 m
Wing span	9,12 m
Wing area	11,1 m2
Horizontal tail width	1,68 m
Horizontal tail area	1,06 m2
Vertical tail area	2,68 m2
Cabin width	1,13 m
Never exceed speed	305 km/h
Cruising speed	180 – 250 km/h
Minimum speed	65 km/h
Climb rate (max. TOW)	5 m/s
Empty weight (according to type)	297 kg
Maximum take-off weight	600 kg
Minimum crew weight	50 kg
Maximum crew weight	180 kg
Maximum luggagge weight	25 kg
Fuel consumption (75% max. continuous power)	16,2 l/h
Fuel tank capacity	77 l (+22 litres in auxiliary tanks in the wings)
Flying range	840 km (1370 km with external fuel tanks)

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Sparker - 2 seater UL/LSA Category

With Sparker, you'll have an elaborate and spacious cockpit. You’ll enjoy the look and feel that this modern design offers. Forget the pre-flight dilemma, with how much luggage you will be able to take. Sparker has the largest luggage compartment in the UL category. And because the compartment is accessible through exterior doors, it‘s convenient. As a result, you can sit back and enjoy your journey. That's why we created Sparker. Sparker Story When we were permitted to raise the MTOW in the UL category, we knew we had to create something special. Sparker is more than just a design recertified to a higher take off weight. Sparker has been completely designed from the ground up to accommodate this higher takeoff weight. Besides the additional load, you’ll also enjoy both comfort and performance. We set out to create a comfortable, spacious aircraft with ideal flight characteristics, and we accomplished our goals.

Sparker technical data:

Length	6,630 m
Height	2,575 m
Wing span	9,000 m
Wing area	9,962 m2
Horizontal tail width	2,96 m
Horizontal tail area	1,776 m2
Vertical tail area	0,995 m2
Cabin width	1250 mm
Never exceed speed (with Rotax 915 iS engine)	335 km/h
Minimum speed	83 km/h
Climb rate (max. TOW)	6 m/s
Empty weight (according to type)	350 kg
Maximum take-off weight	600 kg
Minimum crew weight	60 kg
Maximum crew weight	200 kg
Maximum luggage weight	25 kg
Fuel consumption (75% max. continuous power)	16,2 l/h
Fuel tank capacity	105 l
Flying range	1400 km
Luggage space volume	672 l
Front luggage compartment	12 l
Rear luggage compartment	660 l

You can CONTACT US for more information.