Aerospatiale / Sud-Aviation SA 330 Puma
Photo ©: Karsten Palt
SA 330 Puma
Medium Transport Helicopter
| Crew | 2 | |
| Passengers | 16-20 | |
| Propulsion | 2 Turboshaft Engines | |
| Engine Model | Turbomeca Turmo IVC | |
| Engine Power (each) | 1160 kW | 1556 shp |
| Speed | 257 km/h | 139 kts 160 mph |
| Service Ceiling | 4.800 m | 15.748 ft |
| Range | 780 km | 421 NM 484 mi. |
| 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 | 1902 ft² |
| Length (Fuselage) | 14,06 m | 46,1 ft |
| Length | 18,15 m | 59,5 ft |
| Height | 5,14 m | 16,9 ft |
| First Flight | 15.04.1965 | |
| Production Status | out of production | |
| Total Production | 697 | |
| ICAO Code | PUMA | |
| FAA TCDS | H4EU | |
| EASA TCDS | R.002 | |
| Data for (Version) | Aerospatiale SA 330J Puma | |
| Extras | |

