Aviation Industries of Iran AVA-202

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AVA-202 (آوا-202)
Role Training aircraft
National origin Iran
Manufacturer Aviation Industries of Iran
First flight3 June 1997 [1]
Introduction1997
Number built4 by 2002 [1]
Developed from Van's Aircraft RV-6A

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. [2] [3]

Contents

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. [2] [3]

The aircraft is made from aluminum sheet. Its 8.74 m (28.7 ft) 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 7.01 m (23.0 ft) from which it is derived. The AVA-202's wing has an area of 10.87 m2 (117.0 sq ft) and is equipped with flaps. The standard engine fitted is the 160 hp (119 kW) Lycoming AEIO-320-B2B four-stroke aerobatic powerplant. [2] [3] [4]

Specifications

Data from Jane's All The World's Aircraft 2003–2004 [1]

General characteristics

Performance

See also

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References

  1. 1 2 3 Jackson 2003, pp. 267–268.
  2. 1 2 3 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 156. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  3. 1 2 3 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 142. Flying Pages Europe SARL, 2015. ISSN   1368-485X
  4. Lednicer, David (2010). "The Incomplete Guide to Airfoil Usage". Archived from the original on 19 July 2011. Retrieved 3 January 2012.