Development of the Russian Mi-34 (NATO Designation: 'Hermit') light multipurpose/training helicopter began in 1980; production began in 1993.  Composed of the conventional pod and boom configuration, the light aircraft is capable of aerobatics.

Maximum internal and external payloads are 240 kg and 300 kg, respectively.  The cabin passenger capacity is 4, including the crew.

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: Mil Mi-34

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: 1-2 in Side-by-side arrangement

Landing gear: Skids

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

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