Bell 214

Bell 214B

1974







Model



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


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)
blueprints


List of Operators of Bell 214B


From Organisation with model 214B
1976
norway Helikopter Service
    214 1976/10
oman Silāḥ al-Jaww as-Sulṭāniy ‘Umān
    214 1976/   
1981
ecuador Ejercito Ecuatoriano
    2 1981/98
norway Lufttransport AS
    214 1981/98
2001
norway Helitrans AS
    214 2 2001/   
2005
usa PJ Helicopters
    214 2005/   
Unknown!
Help

australia McDermott Aviation
    214
Construction Numbers on database of 214B

31214B






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