Aérospatiale
Eurocopter AS332 Super Puma
The Eurocopter AS332 Super Puma, originally developed by France’s Aérospatiale in the late 1970s, entered service in 1981 as an advanced medium‑lift helicopter. It was conceived as the successor to the SA 330 Puma, incorporating more powerful engines, a reinforced airframe and modern avionics to meet both civil and military demands. Powered by twin Turbomeca Makila 1A1 turboshafts, the Super Puma delivers a maximum take‑off weight of roughly 9,000 kg and can transport up to 19 passengers or 3,000 kg of cargo over a range of 800 km. Its spacious cabin, optional ice‑protection systems and all‑weather navigation suite have made it popular for offshore oil‑platform support, search‑and‑rescue, and tactical troop deployment. The type’s reliability and adaptability led to numerous variants, including the AS332L1, the naval‑compatible Super Frelon‑derived AS532 Cougar, and the long‑range AS332M1 Super Puma Mk II. Over 1,200 units have been built, serving more than 25 nations. The Super Puma’s blend of performance, versatility and durability has cemented its role as a workhorse in modern aviation, influencing the design of subsequent Eurocopter and Airbus Helicopters platforms. Its continued upgrades keep it competitive in emerging markets and humanitarian missions worldwide.
Classification
Dimensions
- Length
- 14.82 metre
- Height
- 4.6 metre
Performance
- Maximum Speed
- 150 knot
- Range
- 460 nautical mile
Production & History
- First Flight
- 1978
- Service Entry
- 1981
Design & Classification
- Primary Use
- Country of Origin
- Manufacturer
- Aérospatiale
- Developer
- Aérospatiale
- Military Designation
- Hkp 10
- Operator
-
Albanian Air Force
- Wikidata ID
- Q12257149