Aérospatiale SA330 Puma
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Explore the Aérospatiale SA330 Puma in side view and top view to compare its silhouette and proportions.
18.15 m59.5 ft
From Wikipedia
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.
Summary of “Aérospatiale SA 330 Puma” from Wikipedia, the free encyclopedia, used under CC BY-SA 4.0. Retrieved 2026-10-11.
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Drawing of the Aérospatiale SA330 Puma by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/PUMA/), CC BY 4.0Specifications
- Length
- 18.15 m59.5 ft
- Rotor diameter
- 15 m49.2 ft
- Max take-off weight
- 7.4 t16,300 lb
- Cruise speed
- 248 km/h154 mph
- Max speed
- 273 km/h170 mph
- Range
- 580 km360 mi
- Ceiling
- 4,800 m15,700 ft
- Engines
- 2× Turbomeca Turmo IV (turboshaft)
- Power
- 2× 1 575 hp
- First flight
- 1965
- In service
- 1968
From the AirwayControl spec register, curated from Wikipedia and manufacturer pages. Figures vary by variant.
