Mil Mi-34 Hermit
Summary
Category | Training aircraft |
Origin country | 🇨🇳 Ex-USSR |
First flight | 17 November 1986 |
Year of introduction | 1993 |
Number produced | 27 units |
Description
The Mil Mi-34 Hermit is a light multi-purpose military helicopter designed and manufactured by the Russian company Mil Moscow Helicopter Plant. Developed as a successor to the earlier Mi-1 helicopter, the Mi-34 was specifically designed for training, observation, and light utility missions. The aircraft features a conventional single-rotor design with a tail rotor and offers seating for a pilot and two passengers. With its compact size and maneuverability, the Mi-34 is well-suited for operation in various environments, including urban areas and remote regions. Although primarily used for military purposes, this helicopter has found application in civil aviation as well.
Technical specifications
Version: Mi-34S | |
---|---|
Crew | 1 pilot |
Maximum speed | 210 km/h (130 mph) |
Height | 2.8 m (9.0 ft) |
Length | 11.4 m (37.4 ft) |
Service ceiling | 4000 m (13123 ft) |
Empty weight | 950 kg (2094 lbs) |
Max. takeoff weight | 1450 kg (3197 lbs) |
Powerplant | 1 × pistons engine Vedeneyev M14V-26 delivering 239 kW |
Current operating countries
Country | Units | ||
---|---|---|---|
Nigeria | 1 |
Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.