Mil Mi-6
Heavy Transport Helicopter
The Mil Mi-6 is a twin-engined heavy transport-helicopter developed by the Soviet manufacturer Mil OKB, today MIL Moscow helicopter plant, JSC (Russia).
Crew | 5 | |
Passengers | 65 |
Propulsion | 2 Turboshaft Engines | |
Engine Model | Soloviev D-25V(W) | |
Engine Power (each) | 4045 kW | 5424 shp |
Speed | 300 km/h | 162 kts 186 mph |
Service Ceiling | 4.500 m | 14.764 ft |
Range | 620 km | 335 NM 386 mi. |
Empty Weight | 27.240 kg | 60.054 lbs |
max. Takeoff Weight | 42.500 kg | 93.696 lbs |
Rotor Blades (main/tail) | 5/4 | |
Main Rotor Diameter | 35,00 m | 114 ft 10 in |
Tail Rotor Diameter | 6,30 m | 20 ft 8 in |
Rotor Disc Area | 962,1 m² | 10356 ft² |
Length | 41,74 m | 136 ft 11 in |
Height | 9,86 m | 32 ft 4 in |
First Flight | 05.06.1957 | |
Production Status | out of production | |
Total Production | >800 |
ICAO Code | MI6 | |
NATO Code | Hook | |
Data for (Version) | Mil Mi-6A |
[Photo-ID: 1496] © Karsten Palt 2008-09-27 | |
Mil Mi-6A Aeroflot Reg.: RA-21133 c/n: 715309 | |
Flugausstellung L.+P. Junior [Hermeskeil] |
[Photo-ID: 1497] © Karsten Palt 2008-09-27 | |
Mil Mi-6A Aeroflot Reg.: RA-21133 c/n: 715309 | |
Flugausstellung L.+P. Junior [Hermeskeil] |
[Photo-ID: 1498] © Karsten Palt 2008-09-27 | |
Mil Mi-6A Aeroflot Reg.: RA-21133 c/n: 715309 | |
Flugausstellung L.+P. Junior [Hermeskeil] |