Specifications (Mi-8T) Mil Mi-8
data jane s world s aircraft 1992–93 general characteristics crew: 3 (pilot, copilot, flight engineer) capacity: ** 26 passengers or 12 stretchers , seat 1 medical attendant or 4,000 kg (8,800 lb) on internal/external hardpoints length: 18.17 m (59 ft 7 in) rotor diameter: 21.29 m (69 ft 10 in) height: 5.65 m (18 ft 6 in) disc area: 356 m² (3,832 ft²) empty weight: 7,260 kg (16,007 lb) loaded weight: 11,100 kg (24,470 lb) max. takeoff weight: 13,000 kg (26,659 lb) fuel max total capacity: 3,700 l (977 gal) powerplant: 2 × klimov tv3-117mt turboshafts, 1,454 kw (1,950 shp) each performance maximum speed: 260 km/h (140 kt) cruise speed: 123 knots, 141 mph (230 km/h) range: 328 nm, 378 mi (610 km) ferry range: 960 km (596 mi) service ceiling: 4,500 m (14,765 ft) armament 4,000 kg (8,800 lb) of disposable stores on 6 hardpoints, including 57 mm s-5 rockets, bombs, or 9m17 phalanga atgms. ^ mark lambert, ed. (1992). jane s world s aircraft,1992–93. coulsdon, surrey, uk: jane s information g