Updated version of the Mil Mi-8MT produced in 1982.  The landing wheels were made retractable.  Created for the military, there is also the civil transport version; the cabin capacity is 30 passengers in addition to the three 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: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 3

Crew seating: Side-by-side

Landing gear: Wheels (all 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 TV3-117MT turbine

Engine manufacturer: JSC Klimov United Engine Corporation

Take-off / rated power: 1417 kW (1899 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 13000 kg (28660 lb)

Max Range: 580 km (313 nm)

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