The Bell Model 204B Commercial helicopter has a 10-passenger capacity.  Export version of the UH-1B.

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: 1

Crew seating: Side-by-side

Landing gear: Skids

Overall Dimensions

Data on aircraft size

Overall Length: 17.37 m (57.0 ft)

Overall Width: 14.63 m (48.0 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Lycoming T53-L-9 turbine

Engine manufacturer: Lycoming Engines

Maximum power: 669 kW (897 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

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

Max Endurance: 2.8 hrs (2.8 hrs)

Related VFS Resources

Resources related to the 204B , 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 204B , provided by public sources across the internet.

Images