Istra Ezhik

The Ezhik design begun in 1999 and first exhibited in August 2005 and flew some time after.^[1] The Ezhik is a conventional low-wing cantilever monoplane powered by a Walter Minor M-337A engine.^[1] It first appeared with a conventional single fin but was later modified with twin rectangular fins.^[1] It has a raised and enclosed cockpit with two tandem-seats and a conventional landing gear with a tailwheel.^[1] The Ezhik has a welded steel tube fuselage with aluminium skin forward of the cockpit with the rest of the fuselage and tail fabric covered.^[1] It has a monospar wing and a chemical hopper in the fuselage feeds eight rotary atomisers fitted beneath the wings.^[1]

Data from Jane's All the World's Aircraft 2008-2009^[1]

General characteristics

• Crew: 2
• Length: 9.20 m (30 ft 2.25 in)
• Wingspan: 12.00 m (39 ft 4.5 in)
• Height: 3.05 m (10 ft 0 in)
• Wing area: 24.25 m² (261 sq ft)
• Empty weight: 650 kg (1,433 lb)
• Gross weight: 1,150 kg (2,535 lb)
• Powerplant: 1 × Walter Minor M-337A engine , 157 kW (210 hp)

Performance

• Maximum speed: 180 km/h (112 mph, 97 kn)
• Range: 1,000 km (621 mi, 540 nmi)
• Rate of climb: 45 m/s (885 ft/min)

Notes

Bibliography