The Mi-8AMT is a civil transport/military utility helicopter developed in 1991.  The cabin can carry 27 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 (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: Motor Sich TV3-117VM turbine

Engine manufacturer: Motor Sich

Weights and Performance

Data on aircraft weight and flight characteristics

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

Max Range: 570 km (308 nm)

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