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
Engine Class Top Speed (km/h) Maximum Mass (kg) EngineVoronezh MV-6 6-cylinder inverted air-cooled in-line piston engines 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Yakovlev UT-3 (Wikipedia)
Of Make
Source Yakovlev UT-3 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Yakovlev UT-3 (Wikipedia)LeadQuote, 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 originQuote, 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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