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Data from Manufacturer General characteristics Crew: one Capacity: one passenger Length: 6.62 m (21 ft 9 in) Wingspan: 8.6 m (28 ft 3 in) Height: 2.315 m (7 ft 7 in) Wing area: 12.3 m 2 (132 sq ft) Empty weight: 388 kg (855 lb) Gross weight: 600 kg (1,323 lb) Fuel capacity: 114 litres (25 imp gal; 30 US gal) Powerplant: 1 × Rotax 912 ULS2, 73.5 kW (98.6 hp) Propellers: 3-bladed Woodcomp ...
The SportStar was the first special light-sport aircraft (S-LSA) approved by the US Federal Aviation Administration (FAA), and was named "S-LSA Aircraft of the Year" in 2011 by AeroNews Network. [1] According to Flight International , the SportStar held the number-one seller spot in 2005, which the periodical attributed to its high range of ...
Data from Jane's All the World's Aircraft 1910/11 p.176 General characteristics Crew: 1 Capacity: 1 Length: 6.45 m (21 ft 2 in) Wingspan: 10.10 m (33 ft 2 in) Height: 2.28 m (7 ft 6 in) Wing area: 13.00 m 2 (139.9 sq ft) gross Airfoil: MS316 at root, MS313 at tip Empty weight: 330 kg (728 lb) Max takeoff weight: 600 kg (1,323 lb) Fuel capacity: 130 L (28.6 Imp gal, 34.3 US gal) Powerplant: 1 ...
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 ...
In 2011 the company's aircraft line included the amphibious Mermaid, the SportCruiser and the streamlined Parrot, [1] [3] but from 2012 only the SportCruiser and PS-28 Cruiser have been produced. In June 2017 produced its 600th aircraft.
Data from AVweb and company website General characteristics Crew: one Capacity: one passenger Length: 6.45 m (21 ft 2 in) Wingspan: 8.13 m (26 ft 8 in) Height: 2.28 m (7 ft 6 in) Wing area: 10.5 m 2 (113 sq ft) Empty weight: 290 kg (639 lb) Gross weight: 472.5 kg (1,042 lb) Fuel capacity: 120 litres (26 imp gal; 32 US gal) Powerplant: 1 × Rotax 912ULS, 75 kW (100 hp) Performance Cruise speed ...
Data from Bayerl, Tacke and Aerospool General characteristics Crew: two Capacity: one passenger and one pilot Length: 6.40 m (21 ft 0 in) Wingspan: 9.00 m (29 ft 6 in) Height: 2 m (6 ft 7 in) Wing area: 10.35 m 2 (111.4 sq ft) Empty weight: 350 kg (772 lb) Gross weight: 600 kg (1,323 lb) MTOW depends on certification Fuel capacity: 75 litres (16 imp gal; 20 US gal) standard, 125 litres (27 imp ...
The Rans S-20 Raven is an American homebuilt aircraft that was designed by Randy Schlitter and is produced by Rans Designs of Hays, Kansas, introduced at AirVenture in August 2013. The aircraft is supplied as a kit for amateur construction and it is anticipated that it will later be offered as a complete ready-to-fly-aircraft in the light-sport ...