Eurocopter

Manufacturer:

Eurocopter

Country:

Europe

Commercial designation:

Super Puma

Technical designation:

EC225

Version, Variant:

LP

Type:

Conventional

Currently produced:

N

Typical missions:

Civil Utility Transport Law Rescue

Flight conditions:

IFR

First flight:

2000

Landing system:

wheels

Blades number:

5

Tail blades number:

4

MTOW with external loads:

11200 kg

24696 lbs

MTOW with only internal loading:

11000 kg

24255 lbs

Empty weight:

5271 kg

11622.555 lbs

External payload:

4750 kg

10473.75 lbs

Internal payload:

5729 kg

12632.445 lbs

Standard fuel tank:

2268 kg

5000.94 lbs

with optionnal external fuel tank:

2742 kg

6046.11 lbs

Cruise speed:

269 km/h

145.26 kt

Maximum cruise speed:

276 km/h

149.04 kt

Vne:

324 km/h

174.96 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

877 km

473.58 nm

Max range with auxiliary external tanks:

974 km

525.96 nm

Max endurance @ min consumption speed:

05:38:00 h:min

Rate of climb @ SL:

0 m/s

0 ft/min

Rate of climb @ SL @MTOW:

7 m/s

1377.6 ft/min

IGE max hovering altitude, MTOW:

2772 m

9092.16 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:

0 m

0 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:

5530 m

18138.4 ft

Max operating altitude, empty weight:

0 m

0 ft

Highest use Temperature:

50 °C

90 °F

Lowest use Temperature:

-45 °C

-81 °F

APU in HC:

Engine manufacturer:

Turbomeca

Model:

Makila 2A

Engines quantity:

2

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:

0 kW

0 hp

OEI 30s power:

1800 kW

2446.2 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:

93 dB EPNL

Noise at flyover, limit:

99 dB EPNL

Noise at takeoff, level:

95 dB EPNL

Noise at takeoff, limit:

100 dB EPNL

Noise at landing, level:

98 dB EPNL

Noise at landing, limit:

101 dB EPNL

Crew:

1

Max pax number:

25

Average price:

30000000 $