Yak-18T specifications
Details of this extensively redesigned four seat cabin version of the Yak-18 were given for the first time at the 1967 Paris Air Show.

450 test flights were completed in 1968-1969. During this period the planes were fitted with the more powerful Vedeneev M-14P radial engine. Full production was ordered at Smolensk. The 18T became a basic trainer at Aeroflot flying schools used for circuits, instrument training, navigation and aerobatics.

Specification of Yak 18T

  • Engine Veedeneev M-14P 360hp 9 cylinder radial
  • Max take off weight 1650 Kg
  • Empty weight 1217 Kg
  • Max level flight speed 290 Km/hr
  • Cruising speed 210-250 Km/hr
  • Landing speed 125 Km/hr
  • fuel capacity (standard) 190 litres
  • fuel consumption 40-45 litres/hr
  • Max stress (1500kg weight) +6.4 to -3.2 G
  • Take off run 370 Metres
  • Landing run 350 Metres
Outline and Colour scheme
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