Bell 214

Bell 214B

Bell 214B

The Bell 214B, produced between 1976 and 1981, is the civilian variant of the 214A which was originally developed for Iran. The 214B-1 is limited to a maximum 12,500 lb (5,670 kg) gross weight with an internal load due to different certification standards

Specifications 214B

Engine 1 x Lycoming LTC4B-8D / T55-08D 2970 shp
Capacity 2 + 14
Length (m) 14.63
Height (m) 3.9
Blades 2
Rotor diam. (m) 15.24
Disc area (m2) 182
Weight (kgs) Empty: 3440     Max: 6800
Speed (km/h) Cruise: 260
Range (km) 470
Ceiling (m) 5000
Rate/Climb (m/min)

  List of Operators of 214B

Years Model Org
1976/10 214 norway Helikopter Service
1976-    214 oman Silāḥ al-Jaww as-Sulṭāniy ‘Umān
1981/98 ecuador Ejercito Ecuatoriano
1981/98 214 norway Lufttransport AS
2001-    214 norway Helitrans AS
2005-    214 usa PJ Helicopters

214 australia McDermott Aviation

  Global Distribution of 214B


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