Английская Википедия:Evektor VUT100 Cobra
Шаблон:Short description Шаблон:Use dmy dates Шаблон:Use British English
The Evektor VUT100 Cobra (also called the VUT 100 and VUT-100) is a Czech light aircraft under development by Evektor-Aerotechnik, of Kunovice. The aircraft is intended to be supplied as a complete ready-to-fly-aircraft.[1]
As of 2017 the manufacturer lists the aircraft as "in development".[2]
Design and development
The aircraft features a cantilever low-wing, a four-seat enclosed cabin, retractable tricycle landing gear and a single engine in tractor configuration.[1]
The VUT100 is a hybrid construction of metallic and composite materials. Its Шаблон:Convert span wing has an area of Шаблон:Convert and mounts flaps. The engines fitted vary, depending on the model and the cabin is Шаблон:Convert in width. The VUT100 is stressed for +3.8/-1.52g in the normal category and +4.4/-1.76g in the utility category.[1][3]
Although designed to European CS-23 and American FAR-23 certification standards, the VUT100 does not currently have a type certificate issued by the European Aviation Safety Agency or the Federal Aviation Administration.[4][5]
Variants
- Evektor VUT100-120i Cobra
- Base model with a Шаблон:Convert Lycoming IO-360-A1B6 four-stroke powerplant, an empty weight of Шаблон:Convert and a gross weight of Шаблон:Convert, giving a useful load of Шаблон:Convert.[1][3]
- Evektor VUT100-131i SuperCobra
- Higher powered model with a Шаблон:Convert Lycoming IO-580-B1A four-stroke powerplant, an empty weight of Шаблон:Convert and a gross weight of Шаблон:Convert, giving a useful load of Шаблон:Convert.[1][3]
Specifications (VUT100-131i SuperCobra)
References
External links
Шаблон:Evektor-Aerotechnik aircraft
- ↑ 1,0 1,1 1,2 1,3 1,4 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011–12, page 163. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ↑ Шаблон:Cite web
- ↑ 3,0 3,1 3,2 Шаблон:Cite web
- ↑ Шаблон:Cite web
- ↑ Шаблон:Cite web
