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Yakovlev UT-3

Military Aircraft

The Yakovlev UT-3, first known as the AIR-17 and then the Ya-17, was a twin-engine low-wing monoplane designed by Alexander Sergeyevich Yakovlev as a trainer for the Soviet Air Force. It was meant to train multi-engine pilots, air gunners, bomb aimers, navigators and radio operators. The airframe was built mostly of wood and fabric-covered mild steel tube, and the prototype used imported French Renault 6Q-01 engines of 220 hp while production aircraft may have used Voronezh MV-6 engines. Tested in 1938, it was approved as the UT-3 and ordered in 1940 at factories in Leningrad and Kazan, but only around thirty were built before the orders were cancelled, because the air force chose modified multi-engine combat aircraft with dual controls instead. A civil transport derivative, the Ya-19, was built once.

Facts
Year
1938 1
Engine Class
Piston 1
Status
Out of production 1
Top Speed (km/h)
260 1
Mass (kg)
2042 1
Maximum Mass (kg)
2627 1
Engine
Voronezh MV-6 6-cylinder inverted air-cooled in-line piston engines 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Yakovlev UT-3 (Wikipedia)

Of Make

Source Yakovlev UT-3 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Yakovlev UT-3 (Wikipedia)Lead
Quote, Lead
was a twin-engine low-wing monoplane aircraft designed by Alexander Sergeyevich Yakovlev for the Soviet Air Force (VVS)

Originated In

Also in Geography Atlas: where this subject originated.

Source Yakovlev UT-3 (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
designed by Alexander Sergeyevich Yakovlev for the Soviet Air Force (VVS)
Sources
1. Yakovlev UT-3 (Wikipedia)
  • Lead
    was a twin-engine low-wing monoplane aircraft designed by Alexander Sergeyevich Yakovlev for the Soviet Air Force (VVS)
  • Design and development, testing
    Testing was undertaken in 1938
  • Specifications, powerplant
    Powerplant: 2 × Voronezh MV-6 6-cylinder inverted air-cooled in-line piston engines
  • Specifications, engine fitted
    Powerplant: 2 × Voronezh MV-6 6-cylinder inverted air-cooled in-line piston engines
  • Specifications, empty weight
    Empty weight: 2,042 kg
  • Specifications, maximum weight
    Max takeoff weight: 2,627 kg
  • Specifications, maximum speed
    Maximum speed: 260 km/h
  • Status
    Only around thirty aircraft were built before orders were cancelled
  • Lead, country of origin
    designed by Alexander Sergeyevich Yakovlev for the Soviet Air Force (VVS)
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