Overview

Data on design, manufacture and status

Design authority: Sikorsky Aircraft Corp.

Primary manufacturer: Sikorsky Aircraft Corp.

Parent type: Sikorsky S-80/H-53E

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: TBA

Crew seating: Side-by-side

Landing gear: Wheels (all retractable)

Overall Dimensions

Data on aircraft size

Overall Height: 8.55 m (28.0 ft)

Overall Length: 30.19 m (99.0 ft)

Overall Width: 24.08 m (79.0 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 3

Engine designation: GE T64-GE-416 turbine

Engine manufacturer: GE Aviation

Maximum power: 3267 kW (4380 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 31638 kg (69750 lb)

Max Gross Weight (airborne): 33339 kg (73500 lb)

Max Range: 2074 km (1120 nm)

Related VFS Resources

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Related Public Resources

Resources related to the CH-53E (S-65E) Super Stallion, provided by public sources across the internet.

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