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The TL Ultralight TL-96 Star is a single-engine, side-by-side configuration two seat ultralight, designed in the Czech Republic in the 1990s. More than 150 have been registered. More than 150 have been registered.
Summary of aircraft built by TL Ultralight; Model name First flight Number built Type TL-22 Duo: 1990s 50 (1998) Ultralight trike: TL-32 Typhoon: 1991 >200 Fabric covered high-wing ultralight aircraft: TL-96 Star: 1997 Composite low-wing ultralight aircraft TL-132 Condor: 1993 115 (2010) Fabric covered high-wing ultralight aircraft TL-232 ...
The Stream is the company's fastest design to date. It was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever low-wing, an enclosed cockpit with two-seats-in-tandem under a bubble canopy, retractable tricycle landing gear and a single engine in tractor configuration.
(TL Ultralight, Hradec Králové) TL Ultralight TL-22 Duo; TL Ultralight TL-32 Typhoon; TL Ultralight TL-96 Star; TL Ultralight TL-132 Condor; TL Ultralight TL-232 Condor Plus; TL Ultralight TL-232 Power Condor; TL Ultralight TL-2000 StingCarbon; TL Ultralight TL-2000 StingSport; TL Ultralight TL-2000 Sting S3; TL Ultralight TL-3000 Sirius; TL ...
Data from Jane's All the World's Aircraft 2010/11 General characteristics Capacity: 2 Length: 6.75 m (22 ft 2 in) excluding spinner Wingspan: 9.40 m (30 ft 10 in) Height: 2.25 m (7 ft 5 in) Wing area: 11.15 m 2 (120.0 sq ft) gross Empty weight: 297 kg (655 lb) Max takeoff weight: 472.5 kg (1,042 lb) ultralight; LSA 598 kg (1,320 lb) Fuel capacity: 130 L (34.3 US gal; 28.6 Imp gal) Powerplant ...
The standard engine of the Condor Plus is the 48.5 kW (65 hp) Rotax 582 UL-DCDI, driving a two blade propeller, but the 59.7 kW (80 hp) Rotax 912 UL-DCDI or the 74.6 kW (100 hp) Rotax 912 ULS, both with three blade airscrews, are options. With the 912 ULS engine, the TL-232 is known as the Power Condor.
TL Ultralight TL-32 Typhoon; TL Ultralight TL-96 Star; U. UL-Jih Fascination; Y. Yetti Air J-03
Data from Jane's All the World's Aircraft 2000/01 General characteristics Capacity: 2 Length: 5.90 m (19 ft 4 in) Wingspan: 10.70 m (35 ft 1 in) Height: 2.45 m (8 ft 0 in) Wing area: 15.20 m 2 (163.6 sq ft) gross Empty weight: 200 kg (441 lb) Max takeoff weight: 400 kg (882 lb) Powerplant: 1 × Rotax two cylinder two stroke Performance Maximum speed: 110 km/h (68 mph, 59 kn) Cruise speed: 90 ...