Version for the Royal Canadian Armed Forces

Overview

Data on design, manufacture and status

Latest or last design authority: Sikorsky Aircraft Corp.
Originally designed by Sikorsky Aircraft Division, United Aircraft and Transport Corporation

Latest or last primary manufacturer: Sikorsky Aircraft Corp.
Originally manufactured by Sikorsky Aircraft Division, United Aircraft and Transport Corporation

Parent type: Sikorsky S-61/H-3

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

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Weights and Performance

Data on aircraft weight and flight characteristics

Max Range: 837 km (452 nm)

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Related Public Resources

Resources related to the CH-124B , provided by public sources across the internet.

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