Utility variant for the U.S. Marine Corps.

Overview

Data on design, manufacture and status

Design authority: Sikorsky Aircraft Corp.

Primary manufacturer: Sikorsky Aircraft Corp.

Parent type: Sikorsky S-65/H-53

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 2

Crew seating: Side-by-side

Landing gear: Wheels (all retractable)

Overall Dimensions

Data on aircraft size

Overall Height: 7.59 m (24.9 ft)

Overall Length: 26.88 m (88.2 ft)

Overall Width: 21.95 m (72.0 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: GE T64-GE-413 turbine

Engine manufacturer: GE Aviation

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 19051 kg (42000 lb)

Max Range: 543 km (293 nm)

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