Antonov An-74TK-300

The conventional-airliner rebuild of the An-74, and the one that gave up what made the family distinctive: the engines were moved from above the wing to ordinary underwing pylons, trading the short-field lift of the exhaust-blown wing for cruise efficiency. Interstate Aviation Committee type certificate СТ 208-Ан-74ТК-300 gives a maximum take-off mass of 37,500 kg, a maximum ramp mass of 37,850 kg, a maximum landing mass of 34,000 kg and a maximum payload of 6,000 kg, with a maximum cruise altitude of 10,100 m and a maximum operating Mach of 0.65. Unlike the four-crew An-74 it is certificated for two pilots and up to 52 passengers. Only a handful were built.

• Карта данных сертификата типа № СТ 208-Ан-74ТК-300
  СТ 208-Ан-74ТК-300 rev Издание 01
  Aviation Register of the Interstate Aviation Committee · tier 1 · 12 figures · pages 2, 3, 4