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#2103

Mil Mi-17

🇷🇺 Russia ·first flew 1975· utility, transport, armed capable helicopter

Mil Mi-17, photo 1 of 10
1/10 Staff Sgt. Todd Pouliot· Public domain

what is it?

The Mil Mi-17 (NATO reporting name: Hip) is a Soviet-designed Russian military helicopter family introduced in 1975 (Mi-8M), continuing in production as of 2024 at two factories in Russia, in Kazan and Ulan-Ude. It is known as the Mi-8M series in Russian service. The helicopter is mostly used as a medium twin-turbine transport helicopter, as well as an armed gunship version.

How to recognise it: 2 turboshaft engines · 21.3 m main rotor

base stats

  • speed 280 km/htop speed
  • range 800 kmwithout refuelling
  • seats 24passengers
  • size 13 tmax take-off weight
  • built 12,000made in total

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 51 years ago, in 1975.
  • Top speed is 2.2× a car on the Dutch motorway (130 km/h).
  • Rotor of 21.3 m: about 5 cars parked nose to tail.
  • Fully loaded it can weigh as much as 2 African elephants (~6 t each).

turboshaft: A turbine that turns a shaft, usually a helicopter rotor.

spec sheet

first flight
1975
introduced
1977
status
still flying
number built
12,000
role
utility, transport, armed capable helicopter
origin
🇷🇺 Russia
makers
Kazan Helicopters
engines
2× Klimov VK-2500PS-03 / Klimov TV3-117
crew
3
passengers
24
length
18.5 m
rotor diameter
21.3 m
height
5.7 m
max take-off weight
13 t
top speed
280 km/h
cruise speed
260 km/h
range
800 km
ceiling
6,000 m

Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.

family

Sources: Wikidata Q317288, Wikipedia: Mil Mi-17 (CC BY-SA 4.0).Updated 2026-10-24.

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