By the glossary definition, with a Useful Load of 7932 lb (3598 kg), the calculated Empty Weight is approximately 6245 kg.

Overview

Data on design, manufacture and status

Design authority: Sikorsky Aircraft Corp.

Primary manufacturer: Sikorsky Aircraft Corp.

Parent type: Sikorsky S-70/H-60

Aircraft status: No longer flying

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 (non-retractable)

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: GE T700-GE-401C turbine

Engine manufacturer: GE Aviation

Max continuous power: 1240 kW (1662 hp)

Intermediate power: 1343 kW (1800 hp)

Maximum power: 1410 kW (1890 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Range: 833 km (450 nm)

Related VFS Resources

Resources related to the SH-60B (S-70L) Seahawk, provided by the Vertical Flight Society.
Forum Proceedings
 
Vertiflite articles
Enter a search term in the box above.
Web files from vtol.org
Enter a search term in the box above.
Webpages from vtol.org
Enter a search term in the box above.

Related Public Resources

Resources related to the SH-60B (S-70L) Seahawk, provided by public sources across the internet.

Images