Aerospatiale / Sud-Aviation SA 315B Lama
Photo ©: Markus Herzig (swissheli.com)
SA 315B Lama
Light Utility Helicopter
| Crew | 1 | |
| Passengers | 4 | |
| Propulsion | 1 Turboshaft Engine | |
| Engine Model | Turbomeca Artouste IIIB | |
| Engine Power | 405 kW | 543 shp |
| Speed | 193 km/h | 104 kts 120 mph |
| Service Ceiling | 5.400 m | 17.715 ft |
| Range | 515 km | 278 NM 320 mi. |
| Empty Weight | 995 kg | 2.194 lbs |
| max. Takeoff Weight | 1.850 kg | 4.079 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 | 1027 ft² |
| Length (Fuselage) | 10,26 m | 33,7 ft |
| Length | 12,92 m | 42,4 ft |
| Height | 3,09 m | 10,1 ft |
| First Flight | 17.03.1969 | |
| Production Status | out of production | |
| Total Production | 647 | |
| Developed from | Alouette II | |
| ICAO Code | LAMA | |
| Data for (Version) | Aerospatiale SE 315B | |
| Extras | |
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