Mil Mi-54
| Company type | Conceptual aircraft |
|---|---|
| Industry | Aerospace |
| Founded | 1992 |
| Products | Helicopters |
The Mil Mi-54 was a conceptual twin-engine civil utility helicopter introduced in 1992, designed as a successor to the Mi-2 and Mi-8 models. Its design featured two Saturn/Lyulka AL-32 turboshaft engines, each delivering 574 kW of power. The helicopter was equipped with four-bladed main and tail rotors, alongside fixed tricycle landing gear comprising a single nosewheel and dual rear wheels mounted on sponsons.
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