Airbus Helicopters

Manufacturer:

Airbus Helicopters

Country:

Europe

Commercial designation:

Ecureuil

Technical designation:

H125

Version, Variant:

Type:

Conventional

Currently produced:

Y

Typical missions:

Civil Utility Transport Law

Flight conditions:

First flight:

2011

Landing system:

skids

Blades number:

3

Tail blades number:

2

MTOW with external loads:

2800 kg

6174 lbs

MTOW with only internal loading:

2370 kg

5225.85 lbs

Empty weight:

0 kg

0 lbs

External payload:

1400 kg

3087 lbs

Internal payload:

0 kg

0 lbs

Standard fuel tank:

432 kg

952.56 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

235 km/h

126.9 kt

Maximum cruise speed:

258 km/h

139.32 kt

Vne:

287 km/h

154.98 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

651 km

351.54 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

04:28:00 h:min

Rate of climb @ SL:

10 m/s

1968 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

4023 m

13195.44 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:

3383 m

11096.24 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:

5044 m

16544.32 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:

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:

0 kW

0 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

632 kW

858.888 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:

0 m

0 ft

Rotor diameter:

0 m

0 ft

Tail rotor diameter:

0 m

0 ft

Fuselage length:

0 m

0 ft

Overall height:

0 m

0 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:

6

Average price:

0 $