The Mi-26T is a Russian civil transport helicopter with a cabin capacity of 82 passengers or up to 56000 kg payloads.

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: No type defined

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 5-6

Crew seating: Side-by-side

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Motor Sich D-136 turbine

Engine manufacturer: Motor Sich

Max continuous power: 4486 kW (6013 hp)

Take-off / rated power: 8382 kW (11236 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 56000 kg (123459 lb)

Max Range: 800 km (432 nm)

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