Ikar Ai-10 Ikar
| Ai-10 Ikar | |
|---|---|
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| |
| 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 Kyiv.
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
Performance
- Cruise speed: 180 km/h (110 mph, 97 kn)
- Stall speed: 27 km/h (17 mph, 15 kn)
- Range: 1,000 km (620 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]
References[edit]
Notes[edit]
Bibliography[edit]
- Jackson, Paul, ed. (2003). Jane's All the World's Aircraft 2003-2004. Coulsdon, Surrey, United Kingdom: Jane's Information Group. ISBN 0-7106-2537-5.