Technical data
Type Mi-17-1VA
Function utility
Year 1980
Crew ?
Engines 2*2250(1950?)hp Isotov TV-3-117VM
Rotor Span 21.2m
Length 25.3m
Height 4.70m
Disc Area 365m2
Empty Weight 7100kg
Maximum Weight 13000kg
Speed 262(250?)km/h
Ceiling 6000(5000?)m
Range 465(495?)km
Load 4000kg
or 24 seats

Mi-17, M.L.Mil 'Hip-H'

30k Mi-17, lost WEB site;

Improved Mi-8, with more powerful engines for 'hot and high' conditions. The designation Mi-17 is for export; the USSR armed forces called it Mi-8MT. The Mi-17 can be recognized because it has the tail rotor at the starboard side, instead of the port side.

PredecessorsModificationsDevelopments

Mi-8
?


More Links...
  • Mi-17, Mi-171, Mi-172
  • Mi-17
  • Mi-17 at Mil Moscow Helicopters Plant
  • The International Workhorse - the Mi-17
  • Kazan Helicopters Plant is a manufacturer of the Mi-17 and its variants
  • RUSSIA INTENDS TO EXPAND EXPORT OF Mi-17-1V HELICOPTERS
  • MAKS-97 overview
  • Mi-8/9/...
  • Mi-17, Mil 'Hip'
  • Mi-17MD HELICOPTER: VERSATILE CAPABILITIES;

  • Created January 25, 1996
    Modified April 23, 1998
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