9 photos from Wikimedia Commons · credits & licences
- 1. Mil Mi-34S1 (modified): Aleksandr Medvedev· CC BY-SA 4.0
- 2. Mi-34 (4629506603): Aleksandr Markin· CC BY-SA 2.0
- 3. Mi-34S1 at MAKS-2011 airshow: Nockson· CC BY-SA 3.0
- 4. Mil Mi-34 Dubove 1: Varga Attila· CC BY-SA 3.0
- 5. Mil Mi-34 Dubove 2: Varga Attila· CC BY-SA 3.0
- 6. Mil Mi-34 Dubove 3: Varga Attila· CC BY-SA 3.0
- 7. Mil Mi-34: Sergey Ryabtsev· GFDL 1.2
- 8. Mil Mi-34S: Vitaly Kuzmin· CC BY-SA 4.0
- 9. Mil Mi-34S1: Aleksandr Medvedev· GFDL
what is it?
The Mil Mi-34 (NATO reporting name: Hermit) 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.
How to recognise it: 1 piston engine · 10 m main rotor
base stats
Bars compare against all aircraft: 3,500 km/h, 20,000 km, 850 seats; size and number built on a log scale up to 640 t (An-225) and 45,000 built (Cessna 172).
fun facts
- First flew 40 years ago, in 1986.
- Top speed is 1.6× a car on the Dutch motorway (130 km/h).
- Rotor of 10 m: about 2 cars parked nose to tail.
piston: A car-like piston engine turning a propeller: simple and cheap, the classic small plane.
spec sheet
- first flight
- 1986-11-17
- introduced
- 1989
- status
- retired
- number built
- 27
- role
- helicopter
- origin
- 🇷🇺 Soviet Union
- makers
- Mil Moscow Helicopter Plant
- engines
- 1× Vedeneyev M-14V-26V / Vedeneyev M14P
- crew
- 1
- passengers
- 2
- length
- 11.4 m
- rotor diameter
- 10 m
- height
- 2.8 m
- max take-off weight
- 1,450 kg
- top speed
- 210 km/h
- cruise speed
- 170 km/h
- range
- 356 km
- ceiling
- 4,000 m
Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.
Sources: Wikidata Q1704320, Wikipedia: Mil Mi-34 (CC BY-SA 4.0).Updated 2026-10-24.