Aerospatiale SA330 Puma

SA330E Puma



Aerospatiale SA330E Puma

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


Engine: 2 x Safran (Turbomeca) Turmo IV C 1261shp
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

List of Operators of Aerospatiale SA330E Puma

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

Construction Numbers on database of SA330E Puma


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