The preceding U-2 biplane was no longer a suitable trainer for the faster modern aircraft entering service, and to fill the role, the UT-2 was designed as a trainer. The new aircraft was designed by Alexander Sergeevich Yakovlev's team at OKB-115. Originally designated AIR-10, it was based upon the AIR-9, but it was simpler, with tandem open cockpits, also omitting slats and flaps. It first flew on 11 July 1935. The AIR-10 won the competition in 1935 and, after minor changes, was accepted as the standard Soviet Air Force trainer. With the disgrace of Alexey Ivanovich Rykov under whom Yakovlev had been working, the initials AIR were replaced with Ya making what would have been the AIR-20 the Ya-20. The wood-and-metal mixed construction of the AIR-10 was simplified to use only wood to facilitate production, and the AIR-10s 120 hp Renault inline engine was replaced with the 112 kW Shvetsov M-11E radial on the prototype, and the 82 kW M-11Gs in early production aircraft. Serial production started in September 1937. The Soviet VVS assigned the aircraft the designation UT-2. The UT-2 was not easy to fly and easily entered into spins. The UT-2 model 1940 featured a lengthened forward fuselage, and a change to the 93 kW M-11D radial to attempt to rectify the problem. Despite improvements, the handling and flight characteristics remained challenging. To further improve handling and stability, the new UT-2M variant was developed in 1941 and it replaced the original UT-2 in production. The wing planform was redesigned, with a swept leading edge and a straight trailing edge, and the vertical stabilizer was enlarged. 7,243 UT-2 of all types were produced in five factories between 1937 and 1946. In the 1950s, the UT-2 was replaced by the Yak-18primary trainer and the Yak-11advanced trainer. Before and after World War II the UT-2 was used by civilian organizations, and after the war, UT-2s were also operated by the Polish and Hungarian Air Forces.
Variants
;AIR-10:precursor ;Ya-20:prototype ;UT-2:initial production variant ;UT-2 :improved spin characteristics. ;UT-2 :UT-2L ;UT-2 with MV-4:inline engine for tests. ;UT-2L:improved 1940 standard with canopy and engine cowling, fuselage similar to early Yak-18 but had fixed undercarriage. ;UT-2M:production from 1941, new wings and empennage ;UT-2MV:interim light bomber ;UT-2N :air cushion landing gear testbed ;UT-2V:bomber trainer ;VT-2:floatplane variant of basic UT-2 ;Yak-5:single-seat fighter-trainer development of UT-2L
