AgustaWestland

Manufacturer:

AgustaWestland

Country:

Europe

Commercial designation:

AW139

Technical designation:

AW139

Version, Variant:

M

Type:

Conventional

Currently produced:

Y

Typical missions:

Military Utility Rescue Transport Terrestrial Combat

Flight conditions:

IFR

First flight:

2001

Landing system:

wheels

Blades number:

5

Tail blades number:

4

MTOW with external loads:

6800 kg

14994 lbs

MTOW with only internal loading:

6800 kg

14994 lbs

Empty weight:

0 kg

0 lbs

External payload:

0 kg

0 lbs

Internal payload:

3070 kg

6769.35 lbs

Standard fuel tank:

1254 kg

2765.07 lbs

with optionnal external fuel tank:

1654 kg

3647.07 lbs

Cruise speed:

0 km/h

0 kt

Maximum cruise speed:

306 km/h

165.24 kt

Vne:

310 km/h

167.4 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

950 km

513 nm

Max range with auxiliary external tanks:

1250 km

675 nm

Max endurance @ min consumption speed:

05:56:00 h:min

Rate of climb @ SL:

10.9 m/s

2145.12 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

4682 m

15356.96 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:

2478 m

8127.84 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:

6096 m

19994.88 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:

Pratt & Whitney

Model:

PT6C-67C

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:

2284 kW

3103.956 hp

Transmission shaft max continuous power:

1491 kW

2026.269 hp

Transmission shaft max power:

1641 kW

2230.119 hp

Takeoff power 5 min:

2504 kW

3402.936 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

1396 kW

1897.164 hp

OEI max continuous power :

1252 kW

1701.468 hp

OEI max continuous transmission power:

1044 kW

1418.796 hp

OEI 30 sec transmission power:

0 kW

0 hp

OEI 2 min transmission power:

1193 kW

1621.287 hp

Overall length:

16.66 m

54.6448 ft

Rotor diameter:

13.8 m

45.264 ft

Tail rotor diameter:

2.7 m

8.856 ft

Fuselage length:

13.97 m

45.8216 ft

Overall height:

5.17 m

16.9576 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:

2

Max pax number:

15

Average price:

0 $