Bell 214 American Medium-Lift Helicopter
Bell 214
Utility Helicopter
Other
Basic Information
Name
Bell 214 American Medium-Lift Helicopter
Designation
Bell 214
Alternate Designation
Bell 214
Equipment Type
Utility Helicopter
Manufacturer
—
Date of Introduction
1972
Description
The Bell 214 American Medium-Lift Helicopter is a medium-lift helicopter derived from Bell Helicopter's ubiquitous UH-1 Huey series. The Bell 214ST shares the same model number, but is a larger, much-modified twin-engine derivative.
Air & Air Defense Specifications
Crew
2
Engine
Turboshaft (2930 hp)
Cruise Speed
260.0 km/h
Range
411.0 km
Service Ceiling
5000 m
System
Alternative Designation
Bell 214
Type
Medium-Lift Helicopter
Crew
2 ea
Cargo Capacity
1,760 kg, including 14 troops, or 6 stretchers, or equivalent cargo
Blades, Main Rotor
2 ea
Blades, Tail Rotor
2 ea
Number of Engines
1 ea
Number of Hard Points
INA
Dimensions
Length
14.63 m
Main Rotor Diameter
15.0 m
Main Rotor Area
182.438 m2
Blade Section
Wortmann FX 69-H-098
Height
3.91 m
Empty Weight
3,442 kg
Gross Weight
6,260 kg
Maximum Takeoff Weight
6,804 kg) with slung load
Automotive
Engine Name
1 × Lycoming LTC4B-8D
Engine Type
Turboshaft
Engine Power
2,930 shp (2,180 kW)
Maximum Range
411 km at 5,000 m Alititude
Cruise Speed
260 km/h
Service Ceiling
5,000 m
Protection
Stealth Properties
No
Heat Signature Reduction
No
EW Counter Measures/CCM
INA
Counter Measures (Chaff/Flares)
INA
Details
Country of Origin
United States
Category
Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Filter Label
B
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
14.63 m
Width
—
Height
3.91 m
Weight
6260 kg
Operators (2)
Iran
Australia
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