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Iran Aviation AVA-202



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.

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 and 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 sq.m (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.

First flown on 3 June 1997, four had been built by 2002.




Engine: 1 × Textron Lycoming AEIO-320-B2B, 120 kW (160 hp)
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 sq.m (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)
Maximum speed: 259 km/h (161 mph; 140 kn) at sea level
Cruising 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 (20,997 ft)
Rate of climb: 7.6 m/s (1,500 ft/min)
Crew: 2


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