ICAO: PUMA
helicopter • turboshaft • Aérospatiale
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ICAO Code: PUMA
IATA Code: -
Family: helicopter
Engine Family: turboshaft
Engine Count: 2
Manufacturer:Aérospatiale
MTOW: 7400 kilogram
MLW: 7400 kilogram
Maximum operating altitude: 13500 foot
Fuel capacity: 1544 litre
Vne: 167 knot
Main rotor diameter: 15.09 metre
Main rotor count: 1
Main rotor blades: 4
Length: 14.82 metre
Width: 3 metre
Height: 5.14 metre
SA330 Puma is a helicopter powered by turboshaft engine(s).
