Английская Википедия:Fly-Fan Shark
Шаблон:Short description Шаблон:Use dmy dates Шаблон:Use British English
The Fly-Fan Shark is a Slovak light aircraft designed by Frantisek Sustek and initially developed by Fly-Fan of Trenčín. Development continues under the new owner of the design, AENEA Services. The design was introduced at the AERO Friedrichshafen show in 2007 as a mock up and in 2011 as a flying aircraft. The aircraft first flew on 29 June 2011 and is intended to be supplied as a complete ready-to-fly-aircraft.[1][2][3][4]
Design and development
The Shark was designed with the goal of providing similar performance to other twin-engined light aircraft, but on 30% less power. It features a cantilever low-wing, a five-seat enclosed cabin, retractable tricycle landing gear and twin wing-mounted engines in tractor configuration.[1][3]
The aircraft is made from Kevlar and carbon fibre. Its Шаблон:Convert span wing employs a Jd 16 (40) 162 airfoil at the wing root, transitioning to a Jd 17 (40) 157 at mid-span and a Jd 15 (35) 136 at the wing tip. The wing has an area of Шаблон:Convert and mounts split flaps that can be extended 50°. The standard engines fitted are a pair of Шаблон:Convert Lycoming O-320-D1A four-stroke powerplants.[1][3][5]
The aircraft has an empty weight of Шаблон:Convert and a gross weight of Шаблон:Convert, giving a useful load of Шаблон:Convert.[1]
Specifications (Shark)
References
External links
- ↑ 1,0 1,1 1,2 1,3 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 164. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ↑ Шаблон:Cite web
- ↑ 3,0 3,1 3,2 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 150. Flying Pages Europe SARL, 2015. Шаблон:ISSN
- ↑ Шаблон:Cite web
- ↑ Шаблон:Cite web
