Aérospatiale AS.332 Super Puma
Aérospatiale AS.332 Super Puma is a multi-purpose helicopter.
There are 2 versions of the helicopter, civilian and military.
First flew 09/13/1978, mass production started in 1980.
AS.332 “Super Puma” was produced in various versions:
AS 332 L1
- Number of crew members: 2-3
- The greatest number of passengers: 20
- Length: 18.7m
- Fuselage length with tail rotor: 16.29 m
- Rotor Diameter: 15.6m
- Tail rotor diameter: 3.05m
- Height: 4.92m
- Rotor swept area²: 191.13m
- Base chassis: 5.25m
- Track: 3.0m
- Empty Weight: 4460kg
- The highest take-off weight: 8600kg
- The highest take-off weight with a suspended load: 9350kg
- Engine: 2 × TurbomecaMakila1A1 TVD
- Power: 2 × 1820hp (1357kw)
- Maximum allowable speed: 278km / h
- Echelon Speed: 261 Passengers
- Practical range: 870km
- Practical ceiling: 4600m
- Static ceiling: 3250 / 2300m
- Rate of climb: 8.1m / s
- Deadweight: 260
AS 332 L2
- Number of crew members: 2-3
- The greatest number of passengers: 24
- Length: 19.5m
- Fuselage length with tail rotor: 16.79m
- Rotor Diameter: 16.2m
- Tail rotor diameter: 3.15m
- Height: 4.97m
- The area swept by the rotor²: 206,12 sq.m
- Base chassis: 5.25m
- Track: 3.0m
- Empty Weight: 4686kg
- The highest take-off weight: 9300kg
- The highest take-off weight with suspended load: n / a
- Engine: 2 × TurbomecaMakila1A2 TVD
- Power: 2 × 1845 (1376kW)
- Maximum allowable speed: 315km / h
- Tier Speed: 277kW
- Practical range: 1215km
- Practical ceiling: 5180m
- Static ceiling: 3120 / 2250m
- Rate of climb: 7.35m / s
- Thrust-to-weight ratio: 260W / kg
