Airbus Helicopters

Manufacturer:

Airbus Helicopters

Country:

Europe

Commercial designation:

Ecureuil

Technical designation:

AS350

Version, Variant:

B2

Type:

Conventional

Currently produced:

Y

Typical missions:

Civil Utility Transport Law

Flight conditions:

First flight:

1974

Landing system:

skids

Blades number:

3

Tail blades number:

2

MTOW with external loads:

2250 kg

4961.25 lbs

MTOW with only internal loading:

2250 kg

4961.25 lbs

Empty weight:

1224 kg

2698.92 lbs

External payload:

0 kg

0 lbs

Internal payload:

1026 kg

2262.33 lbs

Standard fuel tank:

426 kg

939.33 lbs

with optionnal external fuel tank:

375 kg

826.875 lbs

Cruise speed:

235 km/h

126.9 kt

Maximum cruise speed:

0 km/h

0 kt

Vne:

287 km/h

154.98 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

0 km

0 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:

0 m/s

0 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:

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:

0 m

0 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:

Arriel 1D1

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:

466 kW

633.294 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

546 kW

742.014 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:

12.94 m

42.4432 ft

Rotor diameter:

10.69 m

35.0632 ft

Tail rotor diameter:

0 m

0 ft

Fuselage length:

10.93 m

35.8504 ft

Overall height:

3.34 m

10.9552 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:

87 dB EPNL

Noise at flyover, limit:

92 dB EPNL

Noise at takeoff, level:

89 dB EPNL

Noise at takeoff, limit:

93 dB EPNL

Noise at landing, level:

91 dB EPNL

Noise at landing, limit:

94 dB EPNL

Crew:

0

Max pax number:

0

Average price:

970000 $