Английская Википедия:Aero East Europe Sila

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Шаблон:Short description

The Aero East Europe Sila (English: force, power or strength[1] and also short for Serbian industry light aircraft) is a family of Serbian ultralight and light aircraft, designed and produced by Aero East Europe of Kraljevo and later of Jagodina, introduced at the AERO Friedrichshafen show in 2013. The design is supplied complete and ready-to-fly.[2][3][4]

Design and development

The Sila 450 C was designed to comply with the Fédération Aéronautique Internationale microlight rules, while the larger aircraft in the family fit into the EASA CS-VLA category. All feature a V-strut-braced high-wing, an enclosed cabin, fixed tricycle landing gear and a single engine in tractor configuration.[2]

Operational history

Reviewer Marino Boric described the design in a 2015 review as "very robust".[2]

Variants

Sila 450 C
Two seat "Cruiser" model, with a semi-monocoque structure made from aluminium sheet and a maximum take-off weight of Шаблон:Convert. Its Шаблон:Convert span wing employs a NACA 5417 airfoil, has an area of Шаблон:Convert and flaps. Standard engines available are the Шаблон:Convert Rotax 912UL, Шаблон:Convert Rotax 912ULS and the Шаблон:Convert Rotax 914 four-stroke powerplants. German LTF-UL and Serbian ultralight certified.[2][5]
Sila 750 C
Two seat "Cruiser" model, with a semi-monocoque structure made from aluminium sheet and a maximum take-off weight of Шаблон:Convert. Its Шаблон:Convert span wing employs a NACA 5417 airfoil, has an area of Шаблон:Convert and flaps. Standard engines available are the Шаблон:Convert Rotax 912ULS, the Шаблон:Convert Rotax 914 and the Шаблон:Convert Lycoming O-320 four-stroke powerplants. The aircraft is undergoing EASA CS-VLA and Serbian certification.[2][6]
Sila 750 S
Two seat STOL model with full-span Junkers flaperons and a maximum take-off weight of Шаблон:Convert.[2][7]
Sila 750 MT
Three seat Medical Transport model, with a semi-monocoque structure made from aluminium sheet and steel tubing and a maximum take-off weight of Шаблон:Convert. Its Шаблон:Convert span wing employs a NACA 65-018 airfoil, full-span Junkers flaperons, has an area of Шаблон:Convert. Standard engines available are the Шаблон:Convert Rotax 912ULS, the Шаблон:Convert Rotax 914 and the Шаблон:Convert Lycoming O-320 four-stroke powerplants. The aircraft is undergoing EASA VLA and Serbian certification.[2][8]
Sila 950
Four seat model, with a maximum take-off weight of Шаблон:Convert. Standard engines available are the Шаблон:Convert Rotax 914 and the Шаблон:Convert Lycoming O-320 four-stroke powerplants. The aircraft is no longer advertised on the company website.[2]

Specifications (Sila 450 C)

Шаблон:Aircraft specs

References

Шаблон:Reflist

External links

Партнерские ресурсы
Криптовалюты
Магазины
Хостинг
Разное

  1. ↑ Шаблон:Cite web
  2. ↑ 2,0 2,1 2,2 2,3 2,4 2,5 2,6 2,7 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 14. Flying Pages Europe SARL, 2015. Шаблон:ISSN
  3. ↑ Шаблон:Cite web
  4. ↑ Шаблон:Cite web
  5. ↑ Шаблон:Cite web
  6. ↑ Шаблон:Cite web
  7. ↑ Шаблон:Cite web
  8. ↑ Шаблон:Cite web
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