Production: March 1961 to July 1966. Note Engine upgrades: T53-L9 1100 SHP T-53-L11 1100 SHP

Overview

Data on design, manufacture and status

Design authority: Bell Helicopter Company

Primary manufacturer: Bell Helicopter Company

Parent type: Bell Model 204/UH-1 Iroquois

Aircraft status: Status unknown

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: Skids

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Lycoming T53-L-5 turbine

Engine manufacturer: Lycoming Engines

Maximum power: 960 kW (1287 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 3856 kg (8500 lb)

Max Gross Weight (airborne): 3856 kg (8500 lb)

Related VFS Resources

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

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

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