Search results
Results from the WOW.Com Content Network
Data from Jane's All the World's Aircraft 2010-11 General characteristics Capacity: 2 Length: 6.50 m (21 ft 4 in) Wingspan: 9.20 m (30 ft 2 in) Height: 2.15 m (7 ft 1 in) Wing area: 12.20 m 2 (131.3 sq ft) Empty weight: 265 kg (584 lb) Gross weight: 450 kg (992 lb) limited by European ultralight category Fuel capacity: 50 L (11.0 Imp gal, 13.2 US gal) Powerplant: 1 × Rotax 912 UL-DCDI air ...
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.
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 ...
(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 ...
The civil aviation authorities in different countries have their own particular specifications and regulations which define the LSA category.. For example, in Australia the Civil Aviation Safety Authority defines a light-sport aircraft as a heavier-than-air or lighter-than-air craft, other than a helicopter, with a maximum gross takeoff weight of not more than 560 kg (1,235 lb) for lighter ...
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 ...
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 ...
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.