Airbus / Eurocopter H130 / EC 130
Light Utility Helicopter

Photo ©: Karsten Palt
The Eurocopter EC 130 Ecureuil is a light seven to eight seat single engine helicopter produced by the European manufacturer Eurocopter (a subsidiary of EADS).
| Propulsion | 1 Turboshaft Engine |
| Engine Model | Turbomeca Arriel 2B |
| Engine Power | 632 kW | 848 shp |
| max. Cruise Speed | 241 km/h | 130 kts 150 mph |
| max. Speed (vne) | 287 km/h | 155 kts 178 mph |
| Service Ceiling | 7.010 m | 23.000 ft |
| Rate of climb | 698 m/min | 2290 ft/min |
| Range | 644 km | 348 NM 400 mi. |
| Empty Weight | 1.360 kg | 2.998 lbs |
| max. Takeoff Weight | 2.400 kg | 5.291 lbs |
| Rotor Blades (main/tail) | 3/Fenestron |
| Main Rotor Diameter | 10,69 m | 35 ft 1 in |
| Tail Rotor Diameter | 1,00 m | 3 ft 3 in |
| Rotor Disc Area | 89,8 m² | 967 ft² |
| Length (Fuselage) | 10,68 m | 35 ft 0 in |
| Length | 12,64 m | 41 ft 6 in |
| Height | 3,34 m | 10 ft 11 in |
| First Flight | 06/1999 |
| Production Status | in production |
| Developed from | AS 350 |
| ICAO Code | EC30 |
| FAA TCDS | H9EU |
| EASA TCDS | R.008 |
| Data for (Version) | Eurocopter EC 130 |
| Variants | EC 130 B4 |