Eurocopter

Manufacturer:

Eurocopter

Country:

Europe

Commercial designation:

Super Puma

Technical designation:

AS332

Version, Variant:

L1e

Type:

Conventional

Currently produced:

N

Typical missions:

Civil Utility Transport Rescue

Flight conditions:

IFR

First flight:

2011

Landing system:

Blades number:

0

Tail blades number:

0

MTOW with external loads:

9350 kg

20616.75 lbs

MTOW with only internal loading:

8600 kg

18963 lbs

Empty weight:

4510 kg

9944.55 lbs

External payload:

4500 kg

9922.5 lbs

Internal payload:

4090 kg

9018.45 lbs

Standard fuel tank:

1616 kg

3563.28 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

0 km/h

0 kt

Maximum cruise speed:

262 km/h

141.48 kt

Vne:

278 km/h

150.12 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

841 km

454.14 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

00:00:00 h:min

Rate of climb @ SL:

8.2 m/s

1613.76 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

3250 m

10660 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:

2300 m

7544 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:

2895 m

9495.6 ft

Max operating altitude, empty weight:

0 m

0 ft

Highest use Temperature:

0 °C

0 °F

Lowest use Temperature:

0 °C

0 °F

APU in HC:

Engine manufacturer:

Turbomeca

Model:

Makila 1A1

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:

2370 kW

3220.83 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

2714 kW

3688.326 hp

OEI 30s power:

1400 kW

1902.6 hp

OEI 2min power:

1330 kW

1807.47 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:

0

Max pax number:

0

Average price:

0 $