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AGUSTA AW139
Weights |
Max take Off |
6400 |
kg |
14112 |
lb |
Max Useful Load |
2778 |
kg |
6124 |
lb |
Engine Rating (2 x Pratt & Whitney PT6C-67C) |
Take Off |
1252 |
kW |
1679 |
SHP |
Maximum continuous |
1142 |
kW |
1531 |
SHP |
Transmission Rating |
Take Off |
n.a. |
kW |
n.a. |
SHP |
Max continuous |
n.a. |
kW |
n.a. |
SHP |
Fuel Capacity |
standard |
1562 |
l |
413 |
USG |
Auxiliary |
500 |
l |
132 |
USG |
Crew |
Pilot / Passengers |
1 / 15 |
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External Dimensions |
Length (rotors turning) |
16,65 |
m |
54,63 |
ft |
Overall height |
4,95 |
m |
16,24 |
ft |
Main rotor diameter |
13,80 |
m |
45,28 |
ft |
Performance (At MTOW - ISA) |
VNE |
310 |
km/h |
167 |
kts |
Max cruise speed |
290 |
km/h |
157 |
kts |
Rate of climb |
>10 |
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m/s |
>2000 |
ft/min |
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Hovering IGE |
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m |
15660 |
ft |
Hovering OGE |
>3600 |
m |
12014 |
ft |
Service ceiling |
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m |
19460 |
ft |
Max Range |
568 |
km |
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NM |
Max endurance |
3 h 54 min |
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