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  • Aerospatiale SA330 Puma

    SA330E Puma

    1970





    Model




    First flight November 25, 1970 produced by Westland as the Puma HC.1. 48 built, all but ZA941 for the RAF.




    Specifications


    Engine: 2 x Safran (Turbomeca) Turmo IV C 1261 shp
    Capacity: 3 + 16
    Length: (m) 18.15
    Height: (m) 5.14
    Blades: 4
    Rotor diam.: (m) 15
    Disc area: (m2) 177
    Weight: (kgs) Empty: 3500     Max: 7000
    Speed: (km/h) Cruise: 257     Max: 273
    Range: (km) 580
    Ceiling: (m) 4800
    Rate/Climb: (m/min) 426
    blueprints


    List of Operators of Aerospatiale SA330E Puma


    From Organisation with model SA330E Puma
    1971
    united kingdom Royal Air Force
        SA330 Puma 55 1971/12


    Construction Numbers on database of SA330E Puma

    48sa330e






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