Bell 212/UH1-N Iroquois



General Data		Notes
First Flown	1970	In production
Length	42 ft 4 in
Height	14 ft 10 in
Rotor Span	48 ft 2 in
Lift Capability	5,000 lb
Range	243 nm
Top Speed	117 mph
Empty Weight	6,097 lb
Max Gross Weight	at take off 11,200 lb
Service Ceiling	unknown
Armament	n/a
Engines	1 Pratt & Whitney Canada PT6T-3B Turbo Twin Pac rated at 1,800 shp
Accommodations	2 Pilots and 14 passengers
Cargo	5,000 lb
Operators	Argentina, Austria, Austrailia, Bahrain, Bangledash, Bolivia, Brunei, Chilie, 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