Yakovlev Yak-112
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The Yakovlev Yak-112 is a Russian/Soviet civil utility aircraft that first flew in early 1990s. It is ready for serial production as of 2008 (50..70 "firm" orders awaited to begin). It is an all-metal high-wing braced monoplane with a non-retractable tricycle landing gear and a heavily glazed cabin.
[edit] Specifications (Yak-112)
General characteristics
- Crew: One pilot, 2 passengers
- Length: 6.96m (ft)
- Wingspan: 10.25m (ft)
- Height: 2.9m (ft)
- Wing area: 16.96m² (ft²)
- Empty weight: 950 kg (2,094 lb)
- Loaded weight: 1,300 kg (2,866 lb)
- Max takeoff weight: 1,520 kg (3,351 lb)
- Powerplant: 1× Textron Lycoming IO-540 or Teledyne Continental Motors 10-550 air-cooled piston engine, 191 kW (260 hp)
- Propellers: 1 Hartzell variable pitch three-blade metal propeller
Performance
- Never exceed speed: km/h (mph)
- Maximum speed: 230 km/h (143 mph)
- Cruise speed: 193 km/h (120 mph)
- Stall speed: km/h (mph)
- Range: 1 000 km (621 miles)
- Service ceiling 4000m (ft)
- Rate of climb: m/s (ft/min)
- Wing loading: kg/m² (lb/ft²)
- Power/mass: kW/kg (hp/lb)
- 3 seats.
- Estimated price USD $130,000.
[edit] References
The initial version of this article was based on material from aviation.ru. It has been released under the GFDL by the copyright holder.
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