Eurocopter EC130 (Airbus Helicopters H130)
About the helicopter
General characteristics:
Crew: 1–2 pilots
Length: 12.64 m
Fuselage length: 10.68 m
Main rotor diameter: 10.69 m
Maximum fuselage width: 2.03 m
Height: 3.61 m (with tail rotor)
Area , swept by the main rotor: 89.75 m²
Chassis track: 2.31 m
Empty weight: 1,360 kg
Maximum takeoff weight: 2,400 kg
with external load: 2 800 kg
External load weight: 1,160 kg
Fuel tank capacity : 540 l
Power source: 1 × turboshaft Turbomeca Arriel 2B1 with FADEC system
Engine power: 1 × 847 hp
(1 × 632 kW (takeoff))
Dimensions of the cargo compartment:
Length: 2.19 m
Width: 1.865 m
Height: 1.28 m
Useful volume: 3.7 m³
Flight performance
Maximum speed: 287 km / h
Maximum speed: 235 km / h
Service ceiling: 7,010 m
Static ceiling:
ground effect: 5,875 m
without ground effect: 5 320 m
Rate of climb: 11.6 m / s
Disc load: 26.74 kg / m² Thrust-to-weight ratio
: 226 W / kg (at maximum takeoff weight)
Technical Specifications
| Crew (pilot+passengers): | 1+6 |
| Year of manufacture: | |
| Flight time, hours: | |
| Operating temperature: | |
| Max. flight altitude: | м |
| Flight range: | км |
| Speed rotation of the screws: | об/мин |