Aerospatiale sa330 puma

1970

SA330E Puma


1970




Model

Aerospatiale SA330E Puma

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 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
blueprints

Organisations

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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