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GP ONE SKYLEADER GP ONE

Carbon-composite two seater high wing monocoque

 Speeds  Km/h  Knots
 Never exceed speed (VNE)  250  134
 Cruise speed @ 75% power (VC)  175  94
 Maneuvering speed (VA)  149  80
 Min. speed without lift flaps (VS1)  55  30
 Min. speed with lift flaps (VS0)  50  26

 Weights
 Max. take-off weight  UL/LSA (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

 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

SKYLEADER GP ONE

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SKYLEADER 500 SKYLEADER 500

All metal, low wing two seater

The SKYLEADER 500 is an all metal, 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.

The aircraft is in LSA category furnished with standard instruments for flight and engine control. The Radio, Transponder, Glass Panel, GPS or another flight and engine instruments are installed on the customer’s request. Color painting, upholstery and internal cockpit surface adjustment of the aircraft is realized individually on basis of plentiful amount of offered services and products. The airplane is equipped with ROTAX 912 UL (80hp) engine, optionally with ROTAX 912 ULS (100hp) or ROTAX 914 UL (115hp turbo) engine. The engine is attached by welded bed with the use of rubber shock absorbers through the firewall into the fuselage stringers and central tunnel. Three (3) blade on-ground adjustable propeller is delivered with the plane as standard. As the optional order can be airplane equipped with mechanically or electrically in-flight adjustable propeller, two or three blade. The landing gear is retractable, controlled by electric motor with manual emergency control. Fixed Landing gear is determined for the Light Sport Aircraft category. Both wheels of main landing gear and the nose wheel are towed and they are sprung with rubber shock absorbers, created by circular rubber segments. The nose landing gear is at protuberant position connecting with the foot’s control and is controllable at +15° range. The main landing gear wheels are braked with a central manual hydraulic brake lever at the control stick. All metal tail units are standard alignment with a rudder and an elevator. The profile of Vertical Stabilizator and Horizontal Stabilizator is symmetrical to NACA 0012. They are created by spars, ribs and cover. An elevator is divided; therefore it is possible to take it down without disconnecting the controls. The same construction is used at the others control surfaces. A stabilizer is attached to the fuselage by four hinges and is possible to dismantle it without disconnecting the controls.

 Speeds  Km/h  Knots
 Never exceed speed (VNE)  260  140
 Cruise speed @ 75% power (Vc)  195  105
 Maneuvering speed (VA)  142  77
 Min. speed without lift flaps (VS1)  65  35
 Min. speed with lift flaps (VS0)  58  31

 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 500

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Sirius 3000 SIRIUS 3000

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

Sirius 3000

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SKYLEADER 400 SKYLEADER 400

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

Skyleader 400

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SKYLEADER 600 SKYLEADER 600

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

Skyleader 600

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Sting STING S4

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)

Sting S4

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Stream STREAM

A super-fast fighter turbojet?

After you climb into the Stream, you will experience the same feelings as military pilots. Seats placed behind each other and the well-thought-out shape of the aircraft. The most modern glass cockpit and the maximum amount of control elements on the sidestick. Power and propeller settings designed on the left hand side in the flight deck. Fully electric flaps to maximize Your comfort.

Stream

Stream technical data:

Length

6.785 m

Height

2.475 m

Wingspan

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

575 mm

Never exceed speed

335 km/h

Minimum speed

65 km/h

Climb rate (max. TOW)

6 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

10 + 15 kg

Fuel consumption (75% max. continuous power)

16.2 l/h

Fuel tank capacity

90 l

Flying range

1.400 km

Stream

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