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AS332 C1 Super Puma

Detailed profile for this aircraft model.

Overview

AS332 C1 Super Puma is a helicopter model with turboshaft engine(s).

Specifications

ICAO: -

IATA: -

Engine Count: 2

Fuel capacity: 1556 litre

Height: 4.94 metre

Length: 15.53 metre

Main rotor blades: 4

Main rotor count: 1

Main rotor diameter: 15.6 metre

Maximum operating altitude: 20000 foot

Tail rotor blades: 5

Tail rotor count: 1

Tail rotor diameter: 3.05 metre

Width: 3.79 metre

MTOW: 8350 kilogram

MLW: 8350 kilogram

Vne: 167 knot

Aircraft Type

AS332 Super Puma / H215

Manufacturer

Airbus Helicopters