An example of this aircraft is in the National Air and Space Museum (Udvar-Hazy Center)

Overview

Data on design, manufacture and status

Design authority: Bell Helicopter Textron, Inc.

Primary manufacturer: Bell Helicopter Textron, Inc.

Parent type: Bell Model 204/UH-1 Iroquois

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: Skids

Overall Dimensions

Data on aircraft size

Overall Height: 4.41 m (14.5 ft)

Overall Length: 17.62 m (57.8 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Lycoming T53-L-13 turbine

Engine manufacturer: Lycoming Engines

Max continuous power: 933 kW (1250 hp)

Take-off / rated power: 1045 kW (1400 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 4309 kg (9500 lb)

Related VFS Resources

Resources related to the UH-1H Iroquois, provided by the Vertical Flight Society.
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Related Public Resources

Resources related to the UH-1H Iroquois, provided by public sources across the internet.

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