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Mi-8T 1981 release year The diameter of the main rotor - 21.29 m, diameter tail rotor - 3.91 m, length - 18.17 m, height - 5.65 m, Weight:.... Empty - 6625 kg, the normal take-off - 11100 kg.. maximum take-off - 12,000 kg, engine Type -2 TBG Klimov TV2-117A, Power -.. 2 x 1257 kW, Maximum speed -. 250 km / h, speed -. 225 km / h Practical range -. 480 km ., Practical ceiling - 4500 m Static ceiling -. 1900 m, crew -. 2-3 people, payload -.. 32 soldiers or 12 stretchers with accompanying or 4000 kg of cargo in the cab or 3000 kg on the suspension, combat load - 1,000 kg on four hardpoints. 1 900 000 $