The Russian Helicopters Mi-171A2 is powered by FADEC equipped Klimov VK2500 turboshafts, a KBO-17 integrated avionics suite and a new tail rotor. The helicopter has a more efficient X-shaped steering screw and a new rotor with composite blades and an improved aerodynamic profile.
A standard Mi-8/17 was used as flying laboratory. The first prototype performed maiden flight on November 25, 2014.
One prototype involved in accident on August 2018.
The first foreign operator of Mi-171A2 was the Republic of Kazakhstan.
Offshore variant developed as Mi-171A3
A standard Mi-8/17 was used as flying laboratory. The first prototype performed maiden flight on November 25, 2014.
One prototype involved in accident on August 2018.
The first foreign operator of Mi-171A2 was the Republic of Kazakhstan.
Offshore variant developed as Mi-171A3
List of Operators of Mi-171A2 |
| Years | Model | Org | |
|---|---|---|---|
| 2007- | Mi-8/17 Hip (3rd Gen) | | |
| 2014- | | ||
| 2018- | | ||
| 2020- | | ||
| 2022- | | ||
| 2023- | |
Global Distribution of Mi-171A2 |
|
Construction Numbers |
| C/N | Year | History | |
|---|---|---|---|
| 171A02643140101U w/o 2018 | | ||
| 171A02643170102U | | ||
| 171A02643170103U | |



