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 |