18 passengers
2 Crew
150 kts
Speed
851 km
Range
2
Aircraft
1982
Year
The AS332 Super Puma is powered by a pair of Turbomeca Makila 1A1 turboshaft engines which drive the rotorcraft’s four-bladed main rotor and five-bladed tail rotor as well two separate hydraulic systems and a pair of electrical alternators. Fuel is housed in six internal fuel tanks, additional auxiliary and external tanks can be equipped for extended flight endurance. For safety, the fuel tanks use a crashworthy plumbing design and fire detection and suppression systems are installed in the engine bay. The monocoque tail boom is fitted with tail rotor strike protection, the forward portion of the boom accommodated a luggage compartment. The retractable tricycle landing gear is designed for high energy absorption qualities.