Developed in 1967, the Mi-14PL anti-submarine warfare (ASW) helicopter is designated 'Haze-A' by NATO.  There was a strike version prototype equipped with anti-ship missiles, as well.  The Mi-14PL differed and started the variation of having the tail rotor on the left side of the boom, rotating in the opposite direction.  Cabin capacity is 19 passengers in addition to the four 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: 4

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: Motor Sich TV3-117M turbine

Engine manufacturer: Motor Sich

Max continuous power: 1103 kW (1479 hp)

Take-off / rated power: 1454 kW (1949 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 14000 kg (30865 lb)

Max Range: 800 km (432 nm)

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