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U. S. Military Helicopter

 

 

U. S. Military Aircraft

 

Bell 214 / 214ST

 

Photo by Unknown

 

In late 1970 Bell Helicopters completed the construction of a prototype aircraft to which the identification Bell Model 214 Huey Plus was allocated. It was, in effect, an improved version of the well tried and proven UH-1H Iroquois, using the same airframe, but provided with increased power, some advanced features, and structural strengthening for operation at higher gross weights.

 

 

TECHNICAL DATA

Description  Specifications

Manufacturer: Bell

Height: 15 ft. 10.5 in.

First Flight: Empty Weight:
Model: Max. Weight: 17,599 lb.
Crew: 2 / 3 and 16-20 fully equipped troops. Pay Load: 7,700 lb.
Nickname:

Dimensions

Basic Role: Troop Transport / Armed Assault. Main Rotor Diameter: 52 ft. 0 in.
Other Versions: 214A, 214B, 214C Length Overall Rotor Turning:
Principal User : Main Rotor Disk Area:

Performance

Propulsion

Range: 533 miles. Power Plant: General Electric C17-2A turbo-shaft
Max. Speed: 161 mph. Horsepower: 1,625 shp.
Ceiling: Hover 6,400 ft. No. Of Engines: Two.
Climb Rate:  

 

 

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