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 configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 2

Crew seating: Side-by-side

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Overall Width: 21.30 m (69.9 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Klimov TV2-117AG turbine

Engine manufacturer: JSC Klimov United Engine Corporation

Take-off / rated power: 1119 kW (1499 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 12000 kg (26455 lb)

Max Range: 520 km (281 nm)

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