Neha Patil (Editor)

Aviation Industries of Iran AVA 202

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Top speed
  
259 km/h

Length
  
6.02 m

Wingspan
  
8.74 m

First flight
  
2005

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.

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.

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.

Specifications

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

General characteristics

  • Crew: 2
  • Length: 6.02 m (19 ft 9 in)
  • Wingspan: 8.74 m (28 ft 8 in)
  • Height: 2.04 m (6 ft 8 in)
  • Wing area: 10.87 m2 (117.0 sq ft)
  • Aspect ratio: 7.0:0
  • Airfoil: NASA 632-215
  • Empty weight: 500 kg (1,102 lb)
  • Max takeoff weight: 750 kg (1,653 lb)
  • Powerplant: 1 × Textron Lycoming AEIO-320-B2B air-cooled flat-four, 120 kW (160 hp)

    • Performance

  • Maximum speed: 259 km/h (161 mph; 140 kn) at sea level
  • Cruise speed: 250 km/h (155 mph; 135 kn) (75% power)
  • Stall speed: 84 km/h (52 mph; 45 kn) (flaps down)
  • Range: 1,000 km (621 mi; 540 nmi)
  • Service ceiling: 6,400 m (21,000 ft)
  • Rate of climb: 7.6 m/s (1,500 ft/min)

    • References

    Aviation Industries of Iran AVA-202 Wikipedia
    (Text) CC BY-SA