- Aircraft Overview
- Layout
- Powerplant
- Main Rotor
- Tail Rotor
- Performance
- Operators
- Resources
- Images
- References
WSK Mi-2
A modification of the Mi-1, the Mi-2 was the first Russian light helicopter (NATO Designation: 'Hoplite') powered with two turboshaft engines. Although initially built and test flown in the USSR all subsequent development and production was carried out by WSK in Swidnik, Poland. (now PZL-Świdnik). Development began in 1960 and the Mi-2 became widely used in both the armed forces and civil aviation after it began production in 1965. The aircraft may be fitted with a sling system with a load capacity of 800 kg and a load hoist with a lifting capacity of 260 kg. The cabin can carry eight passengers in addition to the pilot.
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WSK Mi-2
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WSK Mi-2
This content is reserved for AHS members. If you are a current member, please use the Member Login link at the top of the page.
If you are not a member of AHS, why not join today? Be sure to also check out the many benefits enjoyed by AHS members.
WSK Mi-2
This content is reserved for AHS members. If you are a current member, please use the Member Login link at the top of the page.
If you are not a member of AHS, why not join today? Be sure to also check out the many benefits enjoyed by AHS members.
WSK Mi-2
This content is reserved for AHS members. If you are a current member, please use the Member Login link at the top of the page.
If you are not a member of AHS, why not join today? Be sure to also check out the many benefits enjoyed by AHS members.
WSK Mi-2
This content is reserved for AHS members. If you are a current member, please use the Member Login link at the top of the page.
If you are not a member of AHS, why not join today? Be sure to also check out the many benefits enjoyed by AHS members.
WSK Mi-2
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