Aviation Industries of Iran AVA-202 explained

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 8.741NaN1 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 7.011NaN1 from which it is derived. The AVA-202's wing has an area of 10.87m2 and is equipped with flaps. The standard engine fitted is the 1600NaN0 Lycoming AEIO-320-B2B four-stroke aerobatic powerplant.[1] [2] [3]

See also

References

Notes and References

  1. Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 156. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 142. Flying Pages Europe SARL, 2015.
  3. Web site: The Incomplete Guide to Airfoil Usage. 3 January 2012. Lednicer. David. 2010. https://web.archive.org/web/20110719211015/http://www.ae.illinois.edu/m-selig/ads/aircraft.html. 19 July 2011. dead.