Upgraded civil transport version of the Mil Mi-8T, produced beginning in 1990.  The engine has updated carbon/graphite sealing that makes it more durable than its predecessor.  The cabin capacity is 24 passengers in addition to the two crew.

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: Mil Mi-8/Mi-14/Mi-17

Aircraft status: Status unknown

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: 2 in Side-by-side 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-8AT , provided by the Vertical Flight Society.
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Related Public Resources

Resources related to the Mi-8AT , provided by public sources across the internet.

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