Yakovlev Yak-10

Yak-10
Role	Utility aircraft
National origin	Soviet Union
Manufacturer	Yakovlev
First flight	1944
Number built	40+
Developed from	Yakovlev AIR-6

The Yakovlev Yak-10 (Russian: Яковлев Як-10) was a Soviet light liaison aircraft designed and built by the Yakovlev design bureau in the 1940s.^[1]^[2]

Design and development

In the late 1940s the Soviet forces had a need for a light liaison aircraft that was smaller than the Antonov An-2.^[2] The company derived two four-seat aircraft with wooden wings and metal fuselages, from the earlier AIR-6.^[1] The Yak-10, a high-wing strut-braced monoplane with fixed landing gear and the Yak-13 a low-wing cantilever monoplane with a manually retractable landing gear.^[2] Both aircraft were powered by a 145 hp M-11MF radial engine.^[2] After tests in 1945, the Yak-10 was awarded a production contract for 40 aircraft, despite unimpressive performance.^[2] The company built a number of different variants but soon produced an improved design, the Yak-12, which, although of similar layout, was not a derivative of the Yak-10.^[2]

The Yak-10 only entered limited production before it was replaced by the superior Yakovlev Yak-12, and although the Yak-13 proved to be superior to the original Yak-10, production was not carried out.^[1]^[2]

Variants

Yak-10: Strut-braced high-wing monoplane powered by a Shvetsov M-11MF radial engine.^[2]
Yak-10G: Floatplane variant with twin floats.^[2]
Yak-10S: Ambulance variant with room for one stretcher.^[2]
Yak-10V: Dual control.^[1]
Yak-13: Low-wing monoplane derivative, using an almost identical fuselage and Shvetsov M-11MF engine installation, with a cantilevered wooden low wing for direct comparison with the Yak-10. One built.^[2]^[3]

Specifications (Yak-10)

Data from ^[1]The Osprey Encyclopaedia of Russian Aircraft 1875 – 1995

General characteristics

Crew: one
Capacity: three passengers
Length: 8.45 m (27 ft 8.63 in)
Wingspan: 12.0 m (39 ft 4.5 in)
Wing area: 22.0 m² (237 sq ft)
Empty weight: 820 kg (1,808 lb)
Gross weight: 1,250 kg (2,756 lb)
Powerplant: 1 × Shvetsov M-11FR radial engine , 119 kW (160 hp)

Performance

Maximum speed: 206 km/h (128 mph, 111 kn)
Range: 605 km (376 mi, 327 nmi)
Service ceiling: 3,500 m (11,480 ft)
Rate of climb: 3.0 m/s (600 ft/min) ^[4]

References

Notes

^ ^a ^b ^c ^d ^e ^f Gunston 1995, pp. 468-469
^ ^a ^b ^c ^d ^e ^f ^g ^h ⁱ ^j ^k Vaclav 1986, p. 303
^ Gunston 1995, p. 472
^ 5.5 min to 1,000 m (3,300 ft)

Bibliography

Gunston, Bill (1995). The Osprey Encyclopedia of Russian Aircraft from 1875 - 1995. London: Osprey Aerospace. ISBN 1-85532-405-9.
Nemecek, Vaclav (1986). The History of Soviet Aircraft from 1918. London: Willow Books. ISBN 0-00-218033-2.

[Gunston468-1] ^ ^a ^b ^c ^d ^e ^f Gunston 1995, pp. 468-469

[Vaclav-2] ^ ^a ^b ^c ^d ^e ^f ^g ^h ⁱ ^j ^k Vaclav 1986, p. 303

[Gunston472-3] Gunston 1995, p. 472

[4] 5.5 min to 1,000 m (3,300 ft)

[1]

[2]

[3]

[4]