Print this page | Close window
Swiss Air Force

Aérospatiale AS332M1 Super Puma

Super Puma

Manufacturer: Aérospatiale Marignane, France
Production: 1987 / 1989
Purpose: liaison, rescue, disaster relief
Crew: 2 Pilots
Transport capacity: 18 Passengers or max. 4 t inside or outside
Number in service: 15

Immatriculation: T-311 to T-325

 

In order to provide the capacity and performance necessary for increased aerial transport requirements, the Swiss Air Force had to procure medium size transport helicopters. In a first step, three Super Puma helicopters were introduced in 1987. With this, first experiences in the fields of operations and maintenance could be gathered and operational concepts were worked out.

The twin engine Super Puma is equipped for instrument flight and is suitable for many military and civilian purposes (e.g. disaster relief). In cases of emergency and crash-landings, the Super Puma is equipped with modern safety and security features providing better protection for the two pilots who fly it and for the passengers. With the ’98 armaments programme the procurement of an additional 12 Super Puma helicopters, which will be delivered within the next two years, was realised.

 

Technical Data

Maximum speed, VNE
(Never Exceed Speed):
278 km/h (150 kts)
Fast Cruise speed at MCP
(Max Continuous Power) :
258 km/h (139 kts)
Max. rate of climb:8 m/s
Max. operational ceiling:5600 m/M
Flight endurance:3 hours 20 Minutes
Range:approx. 800 km (the range can be doubled by installing additional fuel tanks. This, however reduces the transport capacity and carrier volume)
Structure:Lightly armed cockpit, framework reinforced with steel piping, light metal and composite body construction
Length:18.7 m (Rotor blade facing forwards)
Height:4.87 m
Width:3.36 m (Rotor blade folded)
Empty weight:5000 kg
Permissable load:4000 kg
Max. take-off mass (MTOM):9000 kg
Engine:Turboméca Makila 1A1 (Ets Turboméca SA, Bordes, France)
 Type: Turbo-Engine with 2370 kW
 Max. endourance power: 2 x 1185 kW
 Max. Take-off power: 2 x 1357 kW
Main rotor:Number of rotor blades: 4
 Diameter: 15.58 m
Equipment:Instrument flight equipment, skis, stretcher, load hook, rescue winch, cable cutter
    For questions about this page: Public Information Swiss Air Force
    Last updated: 04.04.2012
    Print this page | Close window