Aerospatiale SA330 Puma

Aerospatiale SA330E Puma

1970 · Twin-engine medium turbine helicopter

History C/N

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 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 SA330E Puma

Operators

1971-2012

Royal Air Force SA330 Puma