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tags: aw-139 Civil Transport Utility Rescue






Commercial designation:


Technical designation:


Version, Variant:



Currently produced:


Typical missions:

Civil Transport Utility Rescue

Flight conditions:


First flight:


Landing system:


Blades number:


Tail blades number:



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


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:

04:32:00 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



Engines quantity:


Powerplant category:


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:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 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:

0 kW

0 hp

OEI 30 sec transmission power:

0 kW

0 hp

OEI 2 min transmission power:

0 kW

0 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:

4.98 m

16.3344 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:

90 dB EPNL

Noise at flyover, limit:

97 dB EPNL

Noise at takeoff, level:

90 dB EPNL

Noise at takeoff, limit:

98 dB EPNL

Noise at landing, level:

94 dB EPNL

Noise at landing, limit:

99 dB EPNL

crew and pax



Max pax number:



Average price:

0 $


AgustaWestland AW139 AW139

from below

AgustaWestland AW139 AW139

front side

AgustaWestland AW139 AW139

left side

AgustaWestland AW139 AW139


rear side

AgustaWestland AW139 AW139

right side

AgustaWestland AW139 AW139