Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Mil Mi-2T Light Utility / Training Helicopter.
1 x PZL GTD-350P turboshaft engines developing 400 horsepower each and driving four-bladed main rotor and two-bladed tail rotor.
Propulsion
124 mph
200 kph | 108 kts
Max Speed
13,123 ft
4,000 m | 2 miles
Service Ceiling
273 miles
440 km | 238 nm
Operational Range
885 ft/min
270 m/min
Rate-of-Climb
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).