Yakovlev Yak-112

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.

Specifications (Yak-112)

aircraft specifications

plane or copter?=plane
jet or prop?=prop

crew= One pilot, 2 passengers
length main= 6.96m
length alt= ft
span main= 10.25m
span alt= ft
height main= 2.9m
height alt= ft
area main= 16.96m²
area alt= ft²
empty weight main= 950 kg
empty weight alt= 2,094 lb
loaded weight main= 1,300 kg
loaded weight alt= 2,866 lb
max takeoff weight main= 1,520 kg
max takeoff weight alt= 3,351 lb

engine (prop)= Textron Lycoming IO-540 or Teledyne Continental Motors 10-550 air-cooled piston engine
type of prop=
propellers=1 Hartzell variable pitch three-blade metal propeller
number of props= 1
power main= 191 kW
power alt= 260 hp

max speed main= 230 km/h
max speed alt= 143 mph
cruise speed main= 193 km/h
cruise speed alt= 120 mph
never exceed speed main= km/h
never exceed speed alt= mph
stall speed main= km/h
stall speed alt= mph
range main= 1 000 km
range alt= 621 miles
ceiling main= 4000m
ceiling alt= ft
climb rate main= m/s
climb rate alt= ft/min
loading main= kg/m²
loading alt= lb/ft²
power/mass main= kW/kg
power/mass alt= hp/lb

* 3 seats.
* Estimated price USD $130,000.

References

* [http://www.yak.ru/ENG/PROD/current_112.php Yaklovlev English page on Yak-112]