Aerospatiale / Sud-Aviation SA 330 Puma
Photo ©: Karsten Palt
SA 330 Puma
Medium Transport Helicopter
| Passengers | 20 |
| | ||
| Propulsion | 2 Turboshaft Engines |
| Engine Model | Turbomeca
Turmo IVC |
| Engine Power (each) | 1160 kW | 1556 shp |
| | ||
| Speed | 258 km/h | 139 kts |
| | ||
| Empty Weight | 3.766 kg | 8.303 lbs |
| max. Takeoff Weight | 7.400 kg | 16.314 lbs |
| | ||
| Rotor Blades (main/tail) | 4/5 | 4/5 |
| Main Rotor Diameter | 15,00 m | 49,2 ft |
| Tail Rotor Diameter | 3,05 m | 10,0 ft |
| Rotor Disc Area | 176,7 m² | 1901 ft² |
| Length | 18,15 m | 59,6 ft |
| Height | 5,14 m | 16,9 ft |
| | ||
| First Flight | 15.04.1965 |
| Production Status | out of production |
| Total Production | 697 |
| | ||
| FAA TCDS | H4EU |
| EASA TCDS | R.002 |
| Data for (Version) | Aerospatiale SA 330J Puma |
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