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: 16.96 m² (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

• Yaklovlev English page on Yak-112

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