Aircraft Exclusive Supplier in the Philippines

 

Welcome to our website for the territory of the Philippines. We may offer You all professional services, consultancy and aircraft sales including aircraft delivery. Czech High Quality Aircraft by TL-Ultralight light & sport aircraft factory now exclusively for the territory of the Philippines. Only the best products made by our professionals.

 

SIRIUS (TL-3000)   - Sting  - Stream  - Sirius Amphibian

 

 

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 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	472,5 kg (600 kg LSA)
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/h

 

SIRIUS AMPHIBIAN (TL-3000)   - Sirius  - Sting  - Stream

 

 

We have discovered extended potential of the Sirius far beyond our imagination. Its design was perfect for water landing. We agreed there was no need to hesitate and have created the LSA version – the TL 3000 Sirius with floats. Not only can the Sirius land on water, solid ground landing is no problem for this aircraft either. No restrictions exist – the TL-3000 Sirius is able to land everywhere.

 

 

Sirius Amphibian technical data:

Wing area	11,26 m2
Cabin width	1,13 m
Never exceed speed	220 km/h
Cruising speed	170 km/h
Minimum speed	60 km/h
Empty weight (according to type)	395 kg
Fuel tank capacity	130 l or 90 l

 

STING (TL-2000)   - Sirius  - Stream  - Sirius Amphibian

 

 

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 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	472,5 kg (600 kg LSA)
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)

 

STREAM (Highest Performance Aircraft)   - Sirius  - Sting  - Sirius Amphibian

 

 

Speed, safety, quality and a perfect design. It is the Stream. Take a seat inside the flight deck and experience the feeling of being a fighter pilot. The Stream will astound you. Its luxurious fly deck will envelop you with the best possible equipment. During the flight, you will have the feeling of being one with the aircraft. You will really start to enjoy flying.

 

 

A super-fast fighter jet? 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.

 

 

A perfect design, aerodynamically clean, with precise controls.

 

 

Power and propeller settings designed on the left hand side in the flight deck.

 

 

Detailed picture of the fully electric flaps to maximize Your comfort.

 

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 472.5 kg – UL	( 600 kg – LSA)
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	1400 km

 

 

HIGH PERFORMANCE GLIDERS

 

Shark   - TwinShark

 

 

High Performance Single Seater

The all-new HPH 304S is a high-performance single-seated, flapped racing class sailplane. It is offered in a convertible wing configuration with long and short wingtip extensions allowing both 15 and 18 meter wingspans.

 

 

Not simply a face lift of an existing technology, but the very latest in a long study of what was, until now, the “State-of-the-Art”. The new HPH 304S prototype was flown on November 23rd 2006. Test pilot Ludek Kluger was surprised with the excellent characteristic of the new glider. He reported excellent flying quality from the first moment. Testing and development continued intensively. Today, we have a technically mature product that fits any pilot need.

AERODYNAMICS WITH A WIZ

The airfoil, only 13.2% thick, was designed mainly in order to reduce the influence of insect contamination on the flight performance. Towards the wing root the thickness increases to 16.4%, with special care to the wing root transition. The wing ends with an elliptically-formed leading edge and 3D curved wingtips are specially shaped to minimize the induced drag. Three-part flaperons through the whole wing span are set in the wing trailing edge. This provides the pilot with good handling and improved flight performance. The wing inner structure and its reinforcement result from detailed FEM calculations in combination with numerous break tests. The result is a carbon fiber structure that makes the cruising flight very comfortable and offers maximum performance in both strong and weak thermals. The water ballast is located in integral wing tanks of 180 liter capacity. There are additional ballast tanks in the tail and optionally in the fuselage. The maximum take-off weight of the 18m version is 600 kg, raising the maximum surface loading up to 50.8 kg/m2. This combination results in a gliding ratio of more than 51 at 125 km/h. Three-stage air brakes are a must to reach sufficient sink rate and allow landing at high glide path rates and at exact landing points. All steering units have automatic connections. This also applies to the ballast tanks, release controls and the slide-in wing end. Locking proceeds by means of a simple hinge, and the flaperon attachment is automatic as well. Our aerodynamically covered wingtip wheels are highly welcomed by pilots because they facilitate take-off and landing, and prevent damage. The design shows an attention to even the smallest detail, such as the elevator trailing edge being elliptically formed thanks to CNC technology. It corresponds in design with the wing ends improving the parallel reduction of induced drag. The elevator connection is automatic, the locking proceeds by use of a single pin. And the perfect functioning of the rudders in a Glasflugel 304 is already legend…

 

 

SAFETY – INTEGRAL

Numerous FEM calculations, break tests and crash simulations led to a new safety cockpit that can help to save life and to minimize damage. For example, the »Roger hook«, for safe emergency removal of the cockpit, is an integrated standard in the solid frame.

ENGINE – at the push of a button.

The fuselage cutout is prepared for a power unit; which one depends on your individual preference: self-launcher (Solo 2625-01) or JET engine. The engine compartments and the fuel tanks are parts of the primary structure. In this manner we can carry out the installation of your desired engine version at any time.

The “COMFORT FACTOR“ – Safe and easy.

Cockpit ergonomics was always one of the main quality features of Glasflugel 304 sailplanes. The safety cockpit of the 304S takes advantage of the proven concept. As a glider pilot you know how important the feeling of comfort and safety is during the flight. These attributes are achieved by, among other factors, the use of hiqh-quality materials. Take pleasure in the massive carbon aramid frame, superior and durable leather interior, sensibly designed instrument panel as well as hand hugging controls. All details are finished with special care – take a look at the control stick or canopy locks! Also pilots above 6ft tall find a very good seat position thanks to enough space for elbows and shoulders. And, of course, we can make adjustments and customizations to suit your specific needs.

 

Shark technical data:

	JS (jet engine)	MS (selflauncher)	ES (electric sustainer)
Geometry
Wing span	18 m (59 ft)	18 m (59 ft)	18 m (59 ft)
Wing area	11.74 m2 / 126.3 ft2	11.74 m2 / 126.3 ft2	11.74 m2 / 126.3 ft2
Aspect ratio	27.43	27.43	27.43
Fuselage length	6.79 m / 22.28 ft	6.79 m / 22.28 ft	6.79 m / 22.28 ft
Profile	HPH xn2	HPH xn2	HPH xn2
Weights
Empty weight	355 kg / 783 lb	395 kg / 870 lb	365 kg / 805 lb
maximum take-off weight	600 kg / 1323 lb	600 kg / 1323 lb	600 kg / 1323 lb
Water ballast	200 l / 53 US gal	120 l / 32 US gal	180 l / 48 US gal
Min. wing loading	36.2 kg/m2 / 7.4 lb/ft2	39.6 kg/m2 / 8.1 lb/ft2	37 kg/m2 / 7.6 lb/ft2
Max. wing loading	51.1 kg/m2 / 10.47 lb/ft2	51.1 kg/m2 / 10.47 lb/ft2	51.1 kg/m2 / 10.47 lb/ft2
Glide Performance
Best glide ratio	> 50	> 50	> 50
at speed	125 km/h / 67.5 kts	125 km/h / 67.5 kts	125 km/h / 67.5 kts
min. sink rate (at min. weight)	0.47 m/s / 93 ft/min	0.49 m/s / 96 ft/min	0.50 m/s / 98 ft/min
at speed	68 km/h / 37 kt	71 km/h / 38 kt	68 km/h / 37 kt
Limitations
Stall speed (at max. weight)	88 km/h / 47.5 kt	88 km/h / 47.5 kt	88 km/h / 47.5 kt
VNE	263 km/h / 142 kt	263 km/h / 142 kt	263 km/h / 142 kt

 

 

HIGH PERFORMANCE GLIDER

 

TwinShark   - Shark

 

 

High Performance Double Seater

 

Why build a new double-seater? Why did we decide to build a new double-seater from the scratch? There are already several performing models on the market. Nevertheless, we believe that no one really thought of a double-seater as of a competition-ready, high-performance sailplane model. That is exactly what we had in mind, when we started to think of a double-seater as appealing and performing as a single-seat glider. Our Twin Shark has not only the performance to fly in the FAI double-seater 20m-class, it also is as comfortable to sit in and to fly as any single-seater from our factory – whichsoever of the both seats you prefer.

 

 

Calculated performance leads the 20m flapped class.

The aerodynamic performance of our Twin Shark is the result of extensive aerodynamic studies and wind-tunnel tests. It builds on the experience gained in our Shark family. A wing area of 15.38 plus an aspect ratio of 26.5 deliver class-leading performance, and advanced manufacturing techniques provide wing-loadings as low as 36kg/m2. At 800 kg maximum load, the loading is 52 kg/m2. An optimal curved leading edge and Shark winglets are maintained through high-end CNC techniques. Further performance is gained through the reflex-negative winglets on the tailplane which mimic a »shark« silhouette.

 

 

Class-leading cockpit environment.

The spacious cockpit easily accomodates tall pilots, and those of generous build. A single-piece, side-opening canopy and extended reflex over the wing deliver outstanding visibility for both pilots. The key cockpit features which made the Shark cockpit popular have been maintained in the Twin Shark. Additionally, a cockpit ventilation system, in addition to the canopy vent keeps temperatures comfortable. This is where you enjoy staying for hours – make it a comfortable experience!

 

TwinShark technical data:

	JTS (jet engine) IN DEVELOPMENT	MTS (selflauncher)
Geometry
Wing span	20 m (65.6 ft)	20 m (65.6 ft)
Wing area	15,3 m2 / 165 ft2	15,3 m2 / 165 ft2
Aspect ratio	26,5	26,5
Fuselage length	8,95 m / 29.36 ft	8,95 m / 29.36 ft
Profile	PW10-145/125 14,5-12,5%	PW10-145/125 14,5-12,5%
Weights
Empty weight	495 kg / 1091 lb	495 kg / 1091 lb
maximum take-off weight	850 kg / 1874 lb	850 kg / 1874 lb
Water ballast	240 l / 63,4 US gal	240 l / 63,4 US gal
Min. wing loading	39 kg/m2 / 8 lb/ft2	39 kg/m2 / 8 lb/ft2
Max. wing loading	55.5 kg/m2 / 11.4 lb/ft2	55.5 kg/m2 / 11.4 lb/ft2
Glide Performance
Best glide ratio	49	49
at speed	128 km/h / 69 kt	128 km/h / 69 kt
min. sink rate (at min. weight)	0,5 m/s / 98 ft/min	0,5 m/s / 98 ft/min
at speed	92 km/h / 50 kt	92 km/h / 50 kt
Limitations
Stall speed (at max. weight)	68 km/h / 37 kt	68 km/h / 37 kt
VNE	275 km/h / 148 kt	275 km/h / 148 kt