First flight 01 Jul 2015, Amarillo, TX

Overview

Data on design, manufacture and status

Design authority: Bell Helicopter Textron, Inc.

Primary manufacturer: Bell Helicopter Textron, Inc.

Parent type: Bell 525 Relentless

Aircraft status: In development

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

Engine designation: GE CT7-2F1 turbine

Engine manufacturer: GE Aviation

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 9072 kg (20000 lb)

Max Gross Weight (airborne): 9525 kg (21000 lb)

Max Range: 926 km (500 nm)

Related VFS Resources

Resources related to the 525 Relentless, provided by the Vertical Flight Society.
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Related Public Resources

Resources related to the 525 Relentless, provided by public sources across the internet.

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