1993 INTERAVIA E 3

1993

INTERAVIA

E-3

Used

VFR

The Interavia I-3 is a Russian aerobatic aircraft, a production version of the earlier SP-91. The design is similar to the Sukhoi Su-26 family as it was designed by the same designer. It is an aerobatic competition aircraft and can be changed from single-seat to two-seat configuration. The I-3 is a metal construction low-wing cantilever monoplane with a conventional landing gear with a tail-wheel. It is powered by a Vedeneyev M14P radial piston engine. General characteristics Crew: one or two Length: 7.00 m (23 ft 0 in) Wingspan: 8.40 m (27 ft 7 in) Wing area: 11.7 m2 (126 sq ft) Aspect ratio: 6.03 Empty weight: 800 kg (1,764 lb) Max takeoff weight: 1,080 kg (2,381 lb) Powerplant: 1 × Vedeneyev M14P Nine-cylinder radial engine, 270 kW (360 hp) Propellers: 3-bladed MT Performance Maximum speed: 300 km/h (186 mph; 162 kn) Stall speed: 105 km/h (65 mph; 57 kn) Never exceed speed: 450 km/h (280 mph; 243 kn) Range: 1,300 km (808 mi; 702 nmi) with full fuel g limits: +11, - 9 (single-seat) or +12, -10 (two-seat) Rate of climb: 17.0 m/s (3,350 ft/min)

304.0

304

SNEW

MP14P

MT9

2

Current Conditional Inspection by A& I