A variant of the Mil Mi-34, certified by the Interstate Aviation Committee Aviation Register.  The Russian light training-multipurpose helicopter is capable of all aerobatic maneuvers.

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: No type defined

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 1-2

Crew seating: Side-by-side

Landing gear: Skids

Overall Dimensions

Data on aircraft size

Overall Height: 2.75 m (9.0 ft)

Overall Length: 11.42 m (37.5 ft)

Overall Width: 10.00 m (32.8 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Vedeneyev M-14V26 reciprocating

Engine manufacturer: Vedeneyev

Take-off / rated power: 242 kW (325 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 1350 kg (2976 lb)

Max Range: 420 km (227 nm)

Max Endurance: 2.4 hrs (2.4 hrs)

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