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Ikar Ai 10 Ikar

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Wingspan
  
9.06 m

First flight
  
1999

Length
  
6.21 m

Manufacturer
  
Ikar Aero Club

Ikar Ai-10 Ikar httpsuploadwikimediaorgwikipediacommonsthu

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

Contents

Design and development

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

Specification (with 912ULS engine)

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

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

    • Performance

  • 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

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

    References

    Ikar Ai-10 Ikar Wikipedia
    (Text) CC BY-SA


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