Eurocopter / Aerospatiale AS 355 Ecureuil 2 / AS 555 Fennec
Photo ©: Karsten Palt
AS 355 Ecureuil 2 / AS 555 Fennec
Light Utility Helicopter
| | ||
| Propulsion | 2 Turboshaft Engines |
| Engine Model | Turbomeca
Arrius 1A |
| Engine Power (each) | 340 kW | 456 shp |
| | ||
| Speed | 278 km/h | 150 kts |
| | ||
| Empty Weight | 1.382 kg | 3.047 lbs |
| max. Takeoff Weight | 2.600 kg | 5.732 lbs |
| | ||
| Rotor Blades (main/tail) | 3/2 | 3/2 |
| Main Rotor Diameter | 10,69 m | 35,1 ft |
| Tail Rotor Diameter | 1,96 m | 6,4 ft |
| Rotor Disc Area | 89,8 m² | 966 ft² |
| Length | 12,94 m | 42,5 ft |
| Height | 3,34 m | 11,0 ft |
| | ||
| First Flight | 28.09.1979 |
| Production Status | in production |
| | ||
| FAA TCDS | H11EU |
| EASA TCDS | A.146 |
| Data for (Version) | Eurocopter AS 555N Fennec |
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