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Home Helicopter Profiles Bell Bell 212/UH1-N Iroquois

Bell 212/UH1-N Iroquois

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General Data
First Flown:
1970
Length:
42 ft 4 in
Lift Capability:
5,000 lb
Height:
14 ft 10 in
Range:
243 nm
Rotor Span:
48 ft 2 in
Top Speed:
117 mph
Empty Weight:
6,097 lb
Service Ceiling:
unknown
Max Gross Weight:
at take off 11,200 lb
Engines:
1 Pratt & Whitney Canada PT6T-3B Turbo Twin Pac rated at 1,800 shp
Armament:
n/a
Accommodations:
2 Pilots and 14 passengers Cargo: 5,000 lb
Operators:
Argentina, Austria, Australia, Bahrain, Bangladesh, Bolivia, Brunei, Chile, Dominican Republic, Ecuador, El Salvador, Ghana, Greece, Guatemala, Ghana, Guyana, Iran, Iraq, Israel, Italy, Jamaica, Japan, Lebanon, Malta, Mexico, Morocco, Oman, Panama, Peru, Philippines, Saudi Arabia, Singapore, Slovenia, South Korea, Spain, Sri Lanka, Somalia, Sudan, Thailand, Tunisia, Turkey, Uganda, Uruguay, Venezuela, Yemen, Zambia, UAE, UK, USA, UN

     
Similar Aircraft:
 
Other Features:
none

     

     
Notes
 
In production
 

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Last Updated on Sunday, 31 August 2008 17:21  

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