SAR variant of the Mil Mi-8.  The helicopter can operate in day or night under any weather conditions.  Fitted with a an LPG-300 winch to lift loads or up to two people; there is space in the cabin for 12 passengers or 6 stretchers.  In case of emergency landings, the aircraft is equipped with a device that allows buoyancy for up to 30 minutes.

 

The aircraft is part of the Mil Mi-17 export series.

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: 3

Crew seating: Other

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Overall Height: 5.65 m (18.5 ft)

Overall Length: 25.24 m (82.8 ft)

Overall Width: 21.29 m (69.8 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Motor Sich TV3-117 turbine

Engine manufacturer: Motor Sich

Take-off / rated power: 1640 kW (2198 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

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

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