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Mil Mi-34
Cold War (1970–1991)
The Mil Mi-34 is a light helicopter designed by the Mil Moscow Helicopter Plant in either a two or four seat configuration for utility and training. It was first flown on 17 November 1986 and introduced at the Paris Air Show in 1987. The Mi-34 entered production in 1993, and is capable of performing aerobatic manoeuvres, including rolls and loops.
Specifications
- Category
- Fixed Wing
- Domain
- Civil
- Era
- Cold War (1970–1991)
- Engine
- 1× 9-cylinder air-cooled radial piston engine
- Thrust / Power
- 239 kW
- Length (ft)
- 37
- Empty Weight (lb)
- 2094
- MTOW (lb)
- 3197
- Service Ceiling (ft)
- 13123
- Range (mi)
- 221
- Max Speed (mph)
- 130