Eurocopter

Manufacturer:

Eurocopter

Country:

Europe

Commercial designation:

EC130

Technical designation:

EC130

Version, Variant:

T2

Type:

Fenestron

Currently produced:

N

Typical missions:

Civil Utility Transport Law

Flight conditions:

IFR

First flight:

2012

Landing system:

skids

Blades number:

3

Tail blades number:

10

MTOW with external loads:

3050 kg

6725.25 lbs

MTOW with only internal loading:

2500 kg

5512.5 lbs

Empty weight:

1412 kg

3113.46 lbs

External payload:

1500 kg

3307.5 lbs

Internal payload:

1088 kg

2399.04 lbs

Standard fuel tank:

426 kg

939.33 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

0 km/h

0 kt

Maximum cruise speed:

236 km/h

127.44 kt

Vne:

287 km/h

154.98 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

606 km

327.24 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

04:00:00 h:min

Rate of climb @ SL:

8 m/s

1574.4 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

0 m

0 ft

IGE max hovering altitude, empty:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

OGE max hovering altitude, MTOW:

2950 m

9676 ft

OGE max hovering altitude, empty:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

Service ceiling ISA, MTOW:

0 m

0 ft

Max operating altitude, empty weight:

7010 m

22992.8 ft

Highest use Temperature:

50 °C

90 °F

Lowest use Temperature:

-40 °C

-72 °F

APU in HC:

N

Engine manufacturer:

Turbomeca

Model:

Arriel 2D

Engines quantity:

1

Powerplant category:

turbine

Main rotor rotation speed:

0 rpm

Fuel consumption @ SL @ max continuous speed:

0 kg/kW/h

0 lbs/hp/h

Minimum consumption speed @ SL:

0 km/h

0 kt

Fuel consumption @ eco cruise speed @SL:

0 kg/h

0 lbs/h

Fuel consumption @ min consumption speed @ SL:

0 kg/h

0 lbs/h

Engines nominal power:

638 kW

867.042 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

710 kW

964.89 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

0 kW

0 hp

OEI max continuous power :

0 kW

0 hp

OEI max continuous transmission power:

0 kW

0 hp

OEI 30 sec transmission power:

0 kW

0 hp

OEI 2 min transmission power:

0 kW

0 hp

Overall length:

12.16 m

39.8848 ft

Rotor diameter:

10.2 m

33.456 ft

Tail rotor diameter:

1 m

3.28 ft

Fuselage length:

10.2 m

33.456 ft

Overall height:

3.51 m

11.5128 ft

Main rotor blades chord:

0 m

0 ft

Tail rotor blades chord:

0 m

0 ft

Mast tilt angle:

0 °

Noise at flyover, level:

0 dB EPNL

Noise at flyover, limit:

0 dB EPNL

Noise at takeoff, level:

0 dB EPNL

Noise at takeoff, limit:

0 dB EPNL

Noise at landing, level:

0 dB EPNL

Noise at landing, limit:

0 dB EPNL

Crew:

1

Max pax number:

7

Average price:

0 $