3 crew required for load lift operations

Overview

Data on design, manufacture and status

Design authority: Sikorsky Aircraft Corp.

Primary manufacturer: Erickson Incorporated

Parent type: Sikorsky S-64/H-54

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: Tandem

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Overall Height: 7.82 m (25.7 ft)

Overall Length: 27.23 m (89.3 ft)

Overall Width: 21.95 m (72.0 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: P&W JFTD12A-4A turbine

Engine manufacturer: Pratt & Whitney

Take-off / rated power: 3357 kW (4500 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

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

Max Range: 402 km (217 nm)

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Related Public Resources

Resources related to the S-64E/CH-54A Aircrane, provided by public sources across the internet.

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