Yakovlev Yak-112

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Yak-112, Zhukovski, 1997
Yak-112, Zhukovski, 1997

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: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


  • 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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