Aerospatiale / Sud-Aviation SA 318C / SE 313B Alouette II
Photo ©: Karsten Palt
SA 318C / SE 313B Alouette II
Light Utility Helicopter
| | ||
| Propulsion | 1 Turboshaft Engine |
| Engine Model | Turbomeca
Artouste II C6 |
| Engine Power | 265 kW | 355 hp |
| | ||
| Speed | 185 km/h | 100 kts |
| | ||
| Empty Weight | 895 kg | 1.973 lbs |
| max. Takeoff Weight | 1.600 kg | 3.527 lbs |
| | ||
| Rotor Blades (main/tail) | 3/2 | 3/2 |
| Main Rotor Diameter | 10,20 m | 33,5 ft |
| Tail Rotor Diameter | 1,81 m | 5,9 ft |
| Rotor Disc Area | 81,7 m² | 881 ft² |
| Length | 9,70 m | 31,8 ft |
| Height | 2,75 m | 9,0 ft |
| | ||
| First Flight | 31.07.1952 (SE 3120),
12.03.1955 (SE 3130) |
| Production Status | out of production |
| Total Production | ca. 1300 |
| | ||
| FAA TCDS | 7H1 |
| | ||
| Data for (Version) | Aerospatiale SE 313B |
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