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 group. isbn 0-7106-0987-6. 
^ http://www.russianhelicopters.aero/en/helicopters/civil/mi-817/features.html