Aérospatiale SA 330 Puma Rotorcraft

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Manufacturer
Aérospatiale
Description
The Aérospatiale SA 330 Puma is a four-bladed, twin-engined medium transport/utility helicopter designed and originally produced by the French aerospace manufacturer Sud Aviation.
ICAO Code
PUMA
First Flight
1965-04-15
Entry Into service
1968-01-01
Production End
1987-01-01
Designer
Aérospatiale
Type
Utility helicopter
Length (m)
17.9832
Height (m)
4.8768
Cockpit Crew
3
Max Seating
16
Max Speed (km/h)
255.5758
Cruise Speed (km/h)
248.1678
Max Ceiling (m)
4800.6
Rate of Climb (m/s)
7.112
Armament
Guns:; Coaxial 7.62 mm (0.30 in) machine guns; Side-firing 20 mm (0.787 in) cannon; Various others
Capacity Description
16 passengers
National Origin
France
Number Built
697
Powerplant Description
2 × Turbomeca Turmo IVC turboshafts, 1174 kW (1575 hp) each
Primary Users
French Army, Royal Air Force (until 2025), Romanian Air Force, Pakistan Army
Status
In service
Wikipedia Article (URL)
en.wikipedia.org/wiki/A%C3%A9rospatiale_SA_330_Puma
Number of Engines
2
40 empty fields

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