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  • 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

    32214B






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