H-19C under the U.S. Army, HRS-1 under the US Navy.  By the glossary definition, with a Useful Load of 2250 lb (1021 kg), the calculated Empty Weight is approximately 2245 kg.

Overview

Data on design, manufacture and status

Design authority: Sikorsky Aircraft Corp.

Primary manufacturer: Sikorsky Aircraft Corp.

Parent type: Sikorsky S-55/H-19

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: TBA in Side-by-side arrangement

Landing gear: Wheels (non-retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

Related VFS Resources

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Related Public Resources

Resources related to the S-55C (UH-19C, HRS-1), provided by public sources across the internet.

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