Additional modification of the Mil Mi-1, the Mi-3  is equipped with the AI-26V radial engine (same as the Mi-1T derivative).  The capacity is increased to a pilot and three passengers.  Main rotor blade count is increased to four; maximum payload is 230 kg.

The designation 'Mi-3' is reused for a modification of the later Mil Mi-2.

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: Mil Mi-1

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: 1 in Single seater arrangement

Landing gear: Wheels (non-retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

Related VFS Resources

Resources related to the Mi-3 , provided by the Vertical Flight Society.
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Related Public Resources

Resources related to the Mi-3 , provided by public sources across the internet.

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