10 photos from Wikimedia Commons · credits & licences
- 1. Mi-6, technical museum, Togliatti-2: ShinePhantom· CC BY-SA 3.0
- 2. Mi-6 (cropped): Rob Schleiffert· CC BY-SA 2.0
- 3. Mi-6 helicopter-riga: 54north· CC BY-SA 3.0
- 4. Mil Mi-6A, UTair Aviation AN1684257: parfaits· CC BY-SA 3.0
- 5. Mil Mi-6 CCCP-06174 LEB 19.06.65 edited-3: RuthAS· CC BY 3.0
- 6. Dózsa György út a Damjanich utcánál. Mi-6 típusú szovjet helikopter. Fortepan 12261: FOTO:Fortepan — ID 12261 : Adományozó/Donor: Beyer Norbert. archive copy at the Wayback Machine· CC BY-SA 3.0
- 7. Dózsa György út, Felvonulási tér, Mi-6 típusú szovjet helikopter. Fortepan 22425: FOTO:Fortepan — ID 22425 : Adományozó/Donor: Pálinkás Zsolt.· CC BY-SA 3.0
- 8. Mi-6 (6140173067): Aleksandr Markin· CC BY-SA 2.0
- 9. Mi-6 (6218933193): Aleksandr Markin· CC BY-SA 2.0
- 10. Mi-6 Hook: Lieutenant Colonel Joe B. Myers, U.S. Army Foreign Science and Technology Center· Public domain
what is it?
The Mil Mi-6 (NATO reporting name Hook), given the article number izdeliye 50 and company designation V-6, is a Soviet/Russian heavy transport helicopter that was designed by the Mil design bureau. It was built in large numbers for both military and civil use and was the largest helicopter in production until the Mil Mi-26 was put in production in 1980.
How to recognise it: 2 turboshaft engines · 35 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 69 years ago, in 1957.
- Top speed is 2.3× a car on the Dutch motorway (130 km/h).
- Rotor of 35 m: about 8 cars parked nose to tail.
- Fully loaded it can weigh as much as 7 African elephants (~6 t each).
turboshaft: A turbine that turns a shaft, usually a helicopter rotor.
spec sheet
- first flight
- 1957-06-05
- introduced
- 1963
- retired
- 2002
- status
- retired
- number built
- 926
- role
- heavy transport helicopter
- makers
- Mil Moscow Helicopter Plant, Rostvertol, Khrunichev State Research and Production Space Center
- engines
- 2× Soloviev D-25V / Soloviev D-25
- crew
- 6
- passengers
- 90
- length
- 33.2 m
- rotor diameter
- 35 m
- height
- 9.2 m
- max take-off weight
- 44 t
- top speed
- 300 km/h
- cruise speed
- 250 km/h
- range
- 970 km
- ceiling
- 4,500 m
Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.
Sources: Wikidata Q744635, Wikipedia: Mil Mi-6 (CC BY-SA 4.0).Updated 2026-10-24.