10 photos from Wikimedia Commons · credits & licences
- 1. MAKS Airshow 2013 (Ramenskoye Airport, Russia) (522-03): Vitaly V. Kuzmin· CC BY-SA 4.0
- 2. CCCP-06141-Mi26-1348: MilborneOne· CC BY-SA 3.0
- 3. Cambodian Air Force Mil Mi-26T Nathalie: Gilles de Maximy· GFDL 1.2
- 4. MI-26 en Mexico: Andrés Tonini· Public domain
- 5. Mil Mi-26TC: Badseed· CC BY-SA 3.0
- 6. Mil Mi-26 Russian helicopter cargo compartment: Geromat· CC BY-SA 3.0
- 7. Rostvertol Mil Mi-26T2 Naumenko: Kirill Naumenko· CC BY-SA 3.0
- 8. UNOSOM II Mi-26 landed on the shores of Kismayo: SGT. G. D. Robinson· Public domain
- 9. 87 Blue - RF- Mil Mi-26 Russian Air Force (8132093997): Aeroprints.com· CC BY-SA 3.0
- 10. 87 Blue, 86 Blue Mil Mi-8's, 87 Blue - RF- Mil Mi-26, 84 Blue, 85 Blue Mil Mi-8's & 56 yellow - RF- & 51 Yellow - RF- Mil Mi-24VM's Russian Air Force (8131823280): Aeroprints.com· CC BY-SA 3.0
what is it?
The Mil Mi-26 (Russian: Миль Ми-26, NATO reporting name: Halo) is a Soviet/Russian heavy transport helicopter. Its product code is Izdeliye 90. Operated by both military and civilian operators, it is the largest helicopter to have gone into serial production.
How to recognise it: 2 turboshaft engines · 32 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 49 years ago, in 1977.
- Top speed is 2.3× a car on the Dutch motorway (130 km/h).
- Rotor of 32 m: about 7 cars parked nose to tail.
- Fully loaded it can weigh as much as 9 African elephants (~6 t each).
turboshaft: A turbine that turns a shaft, usually a helicopter rotor.
spec sheet
- first flight
- 1977-12-14
- introduced
- 1985
- status
- still flying
- number built
- 318
- role
- heavy lift transport helicopter
- origin
- 🇷🇺 Russia
- makers
- Rostvertol, Mil Moscow Helicopter Plant
- engines
- 2× ZMKB Progress D-136 / Lotarev D-136
- crew
- 5
- passengers
- 90
- length
- 40 m
- rotor diameter
- 32 m
- height
- 8.2 m
- max take-off weight
- 56 t
- top speed
- 295 km/h
- cruise speed
- 255 km/h
- range
- 500 km
- ceiling
- 4,600 m
Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.
Sources: Wikidata Q336150, Wikipedia: Mil Mi-26 (CC BY-SA 4.0).Updated 2026-10-24.