Eurocopter AS 332 Super Puma


Country of Origin
Medium lift utility helicopter
A larger development of the Puma (described under Aerospatiale), the Super Puma is a practical and proven medium lift twin helicopter, particularly popular for offshore oil rig support work. The original SA 330 Puma, on which the Super Puma is based, flew for the first time in April 1965. The first Super Puma first flew in September 1978 and was essentially a more powerful version of the Puma, featuring 1270kW (1700shp) Turboméca Makila turboshafts, new avionics, composite rotor blades and an enlarged fuselage. For a time Aerospatiale planned to fit the Super Puma with a Fenestron shrouded tail rotor, but testing revealed no significant performance benefits. Commercial versions were designated AS 332Cs. The AS 332L (or SA 332L before 1980) Super Puma introduced a stretched fuselage (by 76.5cm/2.5ft), first flew on October 10 1980 and was certificated in 1983. The updated AS 332L1 with Makila 1A1 engines appeared in 1986. Bristow Helicopters ordered 31 specially customised AS 332Ls for its North Sea offshore oil rig work, and these are named Tiger. The AS 332L remains in production but is progressively being replaced by the AS 332L2. The L2 Super Puma Mk II (known as the Cougar in military guise) features a further fuselage stretch permitting a further row of seats, EFIS flight instrumentation, spheriflex rotor heads and longer main rotor blades with parabolic tips. It was certificated in 1992.
AS 332L - Two 1325kW (1755shp) Turboméca Makila turboshafts driving a four blade main rotor and five blade tail rotor. AS 332L2 - Two 1375kW (1845shp) takeoff rated Turboméca Makila 1A2 turboshafts.
AS 332L - Max cruising speed 277km/h (150kt). Max inclined rate of climb 1810ft/min. Hovering ceiling in ground effect 9840ft. Range 850km (635nm). AS 332L2 - High speed cruise 277km/h (150kt), economical cruising speed 252km/h (136kt). Rate of climb at 130km/h (70kt) 1447ft/min. Hovering ceiling out of ground effect 9380ft. Range with max fuel, economical cruising speed and no reserves 1490km (805nm), with standard fuel and same conditions 850km (460nm). Endurance 4hr 54min.
AS 332L - Empty 4370kg (9635lb), max takeoff 9000kg (19,840lb). AS 332L2 - Empty 4686kg (10,331lb), max takeoff 9300kg (20,502lb).
AS 332L - Main rotor diameter 15.08m (49ft 6in), length overall rotors turning 18.70m (61ft 4in), fuselage length 15.52m (50ft 11in), height overall 4.92m (16ft 1in). AS 332L2 - Main rotor diameter 16.20m (53ft 2in), length overall rotors turning 19.50m (63ft 11in), height overall 4.97m (16ft 4in). Main rotor disc area 206.1m2 (2218.7sq ft).
Flightcrew of one (VFR ops), or two (IFR ops) pilots. AS 332 seating for 17, AS 332L and AS 332L2 max seating for 24.
Military and civil orders for all variants of the Super Puma total more than 540.
Related Links
Eurocopter AS 332 Super Puma
The backbone of this section is from the The International Directory of Civil Aircraft by Gerard Frawley and used with permission. To get your own copy of the book click here.