Aerospatiale / Sud-Aviation SA 321 Super Frelon
SA 321 Super Frelon
Heavy Transport & Anti Submarine Helicopter
| | ||
| Propulsion | 3 Turboshaft Engines |
| Engine Model | Turbomeca
Turmo IIIC6 |
| Engine Power (each) | 1140 kW | 1529 shp |
| | ||
| Speed | 275 km/h | 148 kts |
| | ||
| Empty Weight | 6.863 kg | 15.130 lbs |
| max. Takeoff Weight | 13.000 kg | 28.660 lbs |
| | ||
| Rotor Blades (main/tail) | 6/5 | 6/5 |
| Main Rotor Diameter | 18,90 m | 62,0 ft |
| Tail Rotor Diameter | 5,04 m | 16,5 ft |
| Rotor Disc Area | 280,6 m² | 3019 ft² |
| Length | 19,40 m | 63,7 ft |
| Height | 6,76 m | 22,2 ft |
| | ||
| First Flight | 10.06.1959 |
| Production Status | out of production |
| Total Production | 99 |
| | ||
| FAA TCDS | H1EU |
| | ||
| Data for (Version) | Aerospatiale SA321G Super Frelon |
| Remarks | Total Production of 99 includes chinese license production. |
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