AgustaWestland

Manufacturer:

AgustaWestland

Country:

Europe

Commercial designation:

AW101

Technical designation:

AW101

Version, Variant:

Type:

Conventional

Currently produced:

Y

Typical missions:

Civil Transport Utility VIP Rescue

Flight conditions:

IFR

First flight:

1987

Landing system:

wheels

Blades number:

5

Tail blades number:

4

MTOW with external loads:

15600 kg

34398 lbs

MTOW with only internal loading:

15600 kg

34398 lbs

Empty weight:

0 kg

0 lbs

External payload:

4536 kg

10001.88 lbs

Internal payload:

6000 kg

13230 lbs

Standard fuel tank:

0 kg

0 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

257 km/h

138.78 kt

Maximum cruise speed:

278 km/h

150.12 kt

Vne:

0 km/h

0 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:

7.5 m/s

1476 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

3290 m

10791.2 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:

1460 m

4788.8 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:

3050 m

10004 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:

Y

Engine manufacturer:

General Electric

Model:

GE CT7-8E

Engines quantity:

3

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:

1522 kW

2068.398 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

1884 kW

2560.356 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:

22.8 m

74.784 ft

Rotor diameter:

18.6 m

61.008 ft

Tail rotor diameter:

0 m

0 ft

Fuselage length:

19.53 m

64.0584 ft

Overall height:

6.62 m

21.7136 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 $