Английская Википедия:Aviation Industries of Iran AVA-202

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The Aviation Industries of Iran AVA-202 is an Iranian two-seat, light aircraft designed as a trainer and sporting aircraft. It was intended for the Iranian domestic market to avoid dependence on imports.[1][2]

Design and development

The AVA-202 was based on the Van's Aircraft RV-6A and was designed to comply with European JAR-22 and JAR-VLA aircraft certification rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed tricycle landing gear and a single engine in tractor configuration.[1][2]

The aircraft is made from aluminum sheet. Its Шаблон:Convert span wing employs a NACA 63-215 airfoil at the wing root and a NACA 63-015 airfoil at the wing tip. The wingspan is greater than the RV-6's wingspan of Шаблон:Convert from which it is derived. The AVA-202's wing has an area of Шаблон:Convert and is equipped with flaps. The standard engine fitted is the Шаблон:Convert Lycoming AEIO-320-B2B four-stroke aerobatic powerplant.[1][2][3]

Specifications

Шаблон:Aircraft specs

See also

References

Шаблон:Reflist

  • Jackson, Paul. Jane's All The World's Aircraft 2003–2004. Coulsdon, UK: Jane's Information Group, 2003. Шаблон:ISBN.

  1. 1,0 1,1 1,2 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 156. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. 2,0 2,1 2,2 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 142. Flying Pages Europe SARL, 2015. Шаблон:ISSN
  3. Шаблон:Cite web