Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Mil Mi-34 Light-class Utility / Trainer Helicopter.
1 x Vedeneyev M-14V-26V 9-cylinder air-cooled radial piston engine developing 320 horsepower and driving a four-bladed main rotor and two-bladed tail rotor.
Propulsion
130 mph
210 kph | 113 kts
Max Speed
13,123 ft
4,000 m | 2 miles
Service Ceiling
221 miles
355 km | 192 nm
Operational Range