Ikar Ai-10 Ikar

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Ai-10 Ikar
Ai-10 RA-0775g taxing in flight.The glider prepares for flight (6900256835).jpg
Role Two-seat ultralight
National origin Ukraine
Manufacturer Ikar Aero Club
First flight 1999

The Ikar Ai-10 Ikar is a Ukrainian two-seat ultralight cabin monoplane, designed and built by the Ikar Aero Club of Kiev.

Design and development[edit]

First flown in 1999 the Ai-10 is a high-wing, strut-braced monoplane with a metal fuselage and fabric-covered wings.[1] It has a fixed conventional landing gear with a tailwheel.[1] The Ai-10 is powered by a tractor configuration Rotax 912UL, 912ULS or 914 flat-four piston engine with a three-bladed wooden propeller.[1] The enclosed cabin has room for two seated in side-by-side configuration.[1]

Specification (with 912ULS engine)[edit]

Data from Jane's All the World's Aircraft 1989-90[1]

General characteristics

  • Crew: 2
  • Length: 6.21 m (20 ft 4 in)
  • Wingspan: 9.06 m (29 ft 9 in)
  • Height: 1.70 m (5 ft 7 in)
  • Wing area: 11.74 m2 (126.4 sq ft)
  • Empty weight: 284 kg (626 lb)
  • Max takeoff weight: 510 kg (1,124 lb)
  • Powerplant: 1 × Rotax 912ULS flat-four piston, 74 kW (99 hp)
  • Propellers: 3-bladed


  • Cruise speed: 180 km/h (112 mph; 97 kn)
  • Stall speed: 27 km/h (17 mph; 15 kn)
  • Range: 1,000 km (621 mi; 540 nmi) max fuel
  • g limits: +6/-3
  • Rate of climb: 6.00 m/s (1,181 ft/min)

Incidents and accidents[edit]

June 9, 2013 near the village Friday Solnechnogorsk district, Moscow region, during a training flight fell plane Ikar Ai-10. Killed pilot and passenger.[2]




  • Jackson, ed. (2003). Jane's All the World's Aircraft 2003-2004. Coulsdon, Surrey, United Kingdom: Jane's Information Group. ISBN 0-7106-2537-5.  |first1= missing |last1= in Authors list (help)