Aerospatiale / Sud-Aviation SA 316B / SA 319B Alouette III
Photo ©: Karsten Palt
SA 316B / SA 319B Alouette III
Light Utility Helicopter
| | ||
| Propulsion | 1 Turboshaft Engine |
| Engine Model | Turbomeca
Artouste IIIB |
| Engine Power | 410 kW | 550 hp |
| | ||
| Speed | 210 km/h | 113 kts |
| | ||
| Empty Weight | 1.230 kg | 2.712 lbs |
| max. Takeoff Weight | 2.200 kg | 4.850 lbs |
| | ||
| Rotor Blades (main/tail) | 3/3 | 3/3 |
| Main Rotor Diameter | 11,02 m | 36,2 ft |
| Tail Rotor Diameter | 1,91 m | 6,3 ft |
| Rotor Disc Area | 95,4 m² | 1029 ft² |
| Length | 10,03 m | 32,9 ft |
| Height | 3,00 m | 9,8 ft |
| | ||
| First Flight | 28.02.1959 |
| Production Status | out of production |
| Total Production | ca. 2000 |
| | ||
| FAA TCDS | H1IN |
| | ||
| Data for (Version) | Aerospatiale SA 316B |
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