T-10 is a very light multipurpose aircraft, intended for pilot training, crop spraying, and aerial patroing. The airplane’s fugelage frame work has truss structure, made of stainless steel. The wing (double spar, all wooden) and horizontal empennage are foldable along the fuselage, which facilitates the airplane’s assembly, disassembly, transportation and storage.
T-10 tricycle non-retractable landing gear, enables it to operate from ground, grass and paved runways. As additional option it can be equipped with a Cobra recovery system. The T-10 Frigate as a ready-to-fly airplane 2009 Price: 42500 euro or as a kit (21 600 euro).
Stall: 33 kt / 39 mph / 62 kmh Cruise: 81 kt / 93 mph / 150 kmh VNE: 103 kt / 118 mph / 190 kmh Empty Weight: 315 kg / 694 lbs MTOW Weight: 550 kg / 1213 lbs Climb Ratio: 1200 ft/min / 6,2 m/s Glide Ratio: 11 Take-off distance (50ft obstacle): 360 ft / 110 m Landing distance (50ft obstacle): 230 ft / 70 m
A new high wing sister ship to the Sting the carbon fiber composite TL-3000 Sirius first series of test flights was completed, piloted by TL-Ultralight founder and president, Jiri Tlusty.
The Sirius displayed very responsive low speed handling and docile flight characteristics, powered by the Rotax series of aircraft engines and was available in an ULM and LSA version.
TL 3000 Sirius Wingspan: 9.4 m / 30 ft 10 in Wing area; 11.25 sq.m / 121 sq.ft Height: 2 m / 6 ft 6 in Length: 7 m / 23 ft Stall: 32 kt / 37 mph / 60 kmh Empty Weight: 295 kg / 650 lbs MTOW Weight: 472 kg / 1041 lbs LSA MTOW: 600 kg / 1320 lb Cruise: 116 kt / 134 mph / 215 kmh VNE: 141 kt / 163 mph / 262 kmh Climb Ratio: 1200 ft/min / 6.2 m/s Fuel capacity: 130 lt / 34 Imp.Gal Baggage capacity: 43 kg / 95 lb Luggage compartment: 110x54x70cm / 43.3×21.2×27.5in
The TL-2000 Sting was designed to achieve the highest speed of flight. The Whole Aicraft is made from Carbon Fibre, stressed to +6/-4 g, is fully certified by the Czech Civil Aviation Authorities.
The aircraft is fitted with dual steering and standard nose wheel configuration with the two main wheels being disc braked and a durable nose wheel, and can be dismantled for road transport in 10 minutes (similar to a glider). This Rotax-powered aircraft has split wing flaps and independent main wheel disc brakes.
The TL-2000 Sting Carbon maximum speed in horizontal flight of about 285 km/h and a minimum 63 km/h to a Vne of 305 km/h. The TL-2000 Sting Carbon offers an optional in flight adjustable propeller electronically controlled.
The TL-2000 Sting Carbon two seat, side by side cabin is roomy and an optional cabin heater can be installed. All control and flight instruments have been ergonomically positioned to maximise ease of use even when securely strapped in. The flaps to extend in two positions. take off is 15 degrees and for landing, 35 degrees.
The very latest in construction techniques enable a strong light and durable aircraft to be produced. If you need to take your Sting home, you can remove the wings easily in 10 minutes. The TL-STING is equipped with Rotax 912, 912 S or 914, and there are many types and construction of propellers.
In 1996 the company started development of complete new type, the TL 96 Star. This took 2 years and it meant transition to complete new materials and technology. Star is made of glass fiber.
It is certificated in Germany, Spain, Italy, and others.
The TL-96 Star is a high performance glasscomposite aircraft with an empty weight of 265 kg. The cruise speed of the TL-96 is 200 km/hr.
2009 Price: 56000 EURO
TL-96 STAR Stall: 35 kt / 40 mph / 65 kmh Cruise: 108 kt / 124 mph / 200 kmh VNE: 148 kt / 171 mph / 275 kmh Empty Weight: 288 kg / 635 lbs MTOW Weight: 450 kg / 992 lbs Climb Ratio: 1200 ft/min / 6 m/s Glide Ratio: 15:1 Take-off distance (50ft obstacle): 890 ft / 270 m Landing distance (50ft obstacle): 980 ft / 300 m
Engine: Roax 912, 80 hp Wing span: 9 m Wing area: 12.1 sq.m MAUW: 450 kg Empty weight: 290 kg Fuel capacity: 60 lt Max speed: 280 kph Cruise speed: 250 kph Minimum speed: 65 kph Climb rate: 5.8 m/s Certification: vVz Seats: 2 Fuel consumption: 9 lt/hr Price (1998): 95 000 DM
The TL Ultralight TL-232 Condor Plus is a two-seat ultralight. The TL-232 Condor Plus is a further development of the TL-132 Condor. It is a two-place ultralight airplane with seats side-by-side. The TL-232 Condor Plus is the first Czech ultralight aircraft certified also for towing of ultralight and light gliders. It is feasible to tow banners, too.
It is an ideal platform for flight training and touristic flying including long-distance flights as well. The basic version is powered by Rotax 503 engine, equipped by a two-blade wooden propeller and basic flight instrumentation only. Upon request it could be delivered with all other Rotax engines (including Rotax 912), various propellers (including electrically in-flight adjustable ones), a wide range of other instruments as for example a GPS set, fuel consumption computer etc. A rocket recovery system belongs to optional extras.
It is a two-place ultralight airplane of latest generation with seats side-by-side in roomy and comfortable cockpit. The seats are adjustable and have inclinable backrests.
The TL-232 Condor Plus is a further development of the TL-132 Condor.
In 1993, the TL 132 Condor was introduced, a two-place ultralight airplane with seats side-by-side, a further development of the TL-32. The cruise speed of the TL132 is 123-130km/h with a consumption of 11 litres fuel per hour. Many flying schools used the TL132 Condor. This ultralight airplane has certification in Germany, France, Holland, Spain.
The Titan Aircraft T-51 Mustang is a two-seat, dual control, tandem seat aircraft. It can be built as an N-numbered amateur built experimental aircraft or as a Light Sport Aircraft.
The kit has an estimated build time of 1600 hours and includes all required material, components and fasteners. The kit does not include the engine, propeller and instruments. When equipped with the Rotax 912S engine, controllable propeller, and a full compliment of necessary flight instruments, the finished T-51 should cost well under US$55,000.00.
The T-51 Mustang is rated at a +6g / -4g load limit capability at a gross weight of 1450 pounds. When operating with the 912S engine and landing gear retracted the cruise speed is 150mph. The stall speed in landing configuration is 39mph. 2009 Kit price: 37500 US$ The centre of the spinner is 7 ft from the ground, and its length is 23.5 ft. It is equipped with 2 seats, dual control, and retractable gear.
With a Suzuki Vitara 2.5 lt fuel injected V-6 developing around 170 hp and driving an Aerotek 2000 four blade prop, takeoff speed is 65-70 mph at 4800 rpm, and cruise is 150 mph at 4200-4500 rpm, 25 in manifold pressure.
T-51 Mustang Engines: ROTAX 912S, 914, Jabiru 332a, Suzuki V6, Honda V6 Power: 100 -270 HP Length: 23’ 6” / 7.16 m Height: 9’ 2” / 2.80 m Wing span: 24 ft / 7.32 m Wing area: 118 sq ft / 10.96 sq m Empty weight: 850-1180 lb / 385-536.4 kg Gross weight: 1320-1800 lb / 545.5-743.8 kg Fuel capacity: 25 US GAL / 94.5 lt Vne: 197 mph / 316.97 kph Cruise speed: 150-185 mph / 241.35-299.7 kph Stall speed: 42-52 mph / 62.75-84.24 kph Range: 720 mi / 1158.5 km Climb rate: 1200-3000 f/m / 6.1-15.2 m/s Take off run: 250-400 ft / 91.44-121.95 m Landing roll: 300-400 ft / 91.44-121.95 m Ceiling: 16000-18000 ft /4876.8-5487.8 m Cabin width: 26 in / 66.04 cm Cabin head room: 48 in / 121.96 cm Cabin leg room: 46 in / 116.84 cm Kit price 2009: $54,900 U.S.
Engine: Suzuki Vitara 2.5 lt fuel injected V-6, 170 hp Prop: Aerotek 2000 four blade Takeoff speed: 65-70 mph at 4800 rpm Cruise: 150 mph at 4200-4500 rpm, 25 in mp MTOW: 1750 lb Empty weight: 1150 lb Stall: 48 mph Climb rate; 2200 fpm Takeoff run: 350 ft Landing soll: 350 ft Seats: 2 Length: 23.5 ft
Engine: Rotax 912S, 100 hp HP range: 100-170 Length: 24 ft Wing span: 24 ft Wing area: 118 sq.ft Empty Weight: 386 kg / 850 lbs MTOW Weight: 658 kg / 1450 lbs Fuel capacity: 23 USG Stall: 34 kt / 39 mph / 63 kmh Cruise: 130 kt / 150 mph / 241 kmh VNE: 171 kt / 197 mph / 317 kmh Climb Ratio: 1200 ft/min / 6 m/s Take-off distance: 300 ft / 91 m Landing distance: 300 ft / 91 m Range: 625nm Seats: 2 Landing gear: tail wheel / retractable
Tornado S is a two seat high wing pusher with stretched fuselage, full cantilevered wing, and aluminum construction which qualifies as a Light Sport Aircraft
The kit has an estimated build time of 150 – 300 hours and includes all required material, components and fasteners. The kit does not include the engine, propeller and instruments.
The Tornado 912 is designed to a +6g / -4g limit load capability at 1000 pounds gross weight. When operating with the 912S engine the cruise speed is in excess of 120 mph. The stall speed in landing configuration flying solo is 35 mph.
The Titan Tornado SS Super Stretch has a 1200 lb gross weight, 560 lb useful load and qualifies as a Light Sport Aircraft
Tornado SS
Two place kit (not including engine and options) includes much longer & taller fuselage, 33% larger back door, full size rear seat, 4″ more headroom over standard Tornado II, 26 ft wingspan, Matco hydraulic brakes, 150 mph Vne upgrade, Kevlar aft panels, extended range 15 gallon fuel tank, aileron controls located behind rear seat, aluminum rudder, aluminum stabilator with 8′ span, electric flaps and aileron spades.
Tornado S Engines: Rotax 503, 912, Jabiru Power: 46 – 120 HP Length: 19 ft 4 in Height: 6 ft 8 in Wing span: 23 ft 6 in Wing area: 108 sq ft Empty weight: 590 Lb Gross weight: 1,140 Lb Fuel capacity: 15 Gallons Cabin width: 28.5 Cabin head room: 41 Cabin leg room: 43.5 Vne: 150 mph Cruise speed: 90 – 125 mph Stall speed: 35 mph Range: 350 – 500 Miles Climb rate: 800 – 2000 f/min Take off run: 300 Feet Landing roll: 250 Feet Ceiling: 16,000 ft Kit price 2009: $18,139 U.S.
Tornado S Engine: Rotax 912S, 100 hp HP range: 100 Length: 19 ft Wing span: 23.6 ft Wing area: 108 sq.ft Empty weight: 540 lb Gross weight: 1140 lb Fuel capacity: 15 USG Cruise: 135 mph Stall: 35 mph Range: 550 sm Rate of climb: 1800 fpm Takeoff dist: 300 ft Landing dist: 250 ft Seats: 2 tandem Cockpit width: 26 in Landing gear: nosewheel LSA: yes
Tornado SS Engines: Rotax 912 or Jabiru Power: 80-120 hp. Length: 19 ft 11 in Height: 6 ft 11 in Wing span: 26 ft Wing area: 120 sq. ft. Empty weight: 640 lbs. Gross weight: 1200 lbs. Fuel capacity: 15 UUSgallons Cabin width: 28.5 in Cabin head room: 43 in Cabin leg room: 43.5 in Vne: 150 mph Cruise speed: 105-125 mph Stall speed: 40 mph Range: 315-630 miles Climb rate: 800-2000 fpm Take off run: 250 feet Landing roll: 250 feet Ceiling: 16,000 ft Kit price 2009: $21,439 US
Tornado SS Engine: Rotax 912S, 100 hp HP range: 80-120 Length: 9.9 ft Wing span: 26 ft Wing area: 120 sq.ft Empty weight: 640 lb Gross weight: 1200 lb Fuel capacity: 15 USG Cruise: 130 mph Stall: 40 mph Range: 360 sm Rate of climb: 800 fpm Takeoff dist: 250 ft Landing dist: 250 ft Seats: 2 tandem Cockpit width: 26 in Landing gear: nosewheel LSA: yes
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