The AW109LUH is the militarized variant of the proven AW109 platform; the best-selling military light-twin helicopter, able to satisfy a wide range of military requirements with true multirole capabilities.
The platform features a rugged design, with excellent ballistic tolerance, redundancy of systems, crashworthiness and self sealing tanks for maximum safety and survivability. It can be equipped with external/internal weapons systems and a range of mission equipment for maximum mission flexibility.
The cockpit is equipped with a state-of-the-art avionics suite, providing an ideal training environment for crews moving to larger, more sophisticated aircraft.
Compact external dimensions ensure agility in flight and allow for small ship deployment.
MTOW: 3,175 kg
Power plant: 2 Turbomeca Arrius 2K2 (711 shp each)
Crew/Passengers: 1 or 2 pilots with up to 6 troops
Weights |
||||
---|---|---|---|---|
Max take off |
3000/ 3175 |
kg |
6614/ 7000 |
lb |
Standard configuration empty weight |
1970 |
kg |
4343 |
lb |
Engine Rating (2 x Turbomeca Arrius 2K2) |
||||
---|---|---|---|---|
Take off power (5 min) |
2 x 530 |
kW |
2 x 714 |
shp |
Maximum continuous power |
2 x 454 |
kW |
2 x 609 |
shp |
O.E.I. max contingency power (2.5 min) |
590 |
kW |
791 |
shp |
O.E.I. max continuous power |
534 |
kW |
714 |
shp |
Transmission Rating |
||||
---|---|---|---|---|
Maximum continuous power |
672 |
kW |
900 |
shp |
O.E.I. max contingency power (2.5 min) |
477 |
kW |
640 |
shp |
O.E.I. max continuous power |
418 |
kW |
560 |
shp |
Fuel Capacity |
||||
---|---|---|---|---|
3-cell fuel system |
608 |
l |
160 |
USgal |
4-cell fuel system |
716 |
l |
190 |
USgal |
5-cell fuel system |
881 |
l |
233 |
USgal |
Crew |
|
---|---|
Pilots / Passengers |
1 - 2 / 7 - 6 |
External Dimensions |
||||||
---|---|---|---|---|---|---|
Length |
13.04 |
m |
42 |
ft |
09 |
in |
Main rotor diameter |
10.83 |
m |
35 |
ft |
06 |
in |
Performance (ISA, 3000 kg / 6614 lb) |
||||
---|---|---|---|---|
VNE (SL) |
311 |
km/h |
168 |
kt |
Cruise speed (SL) |
283 |
km/h |
153 |
kt |
Rate of climb (SL) |
8.5 |
m/sec |
1680 |
ft/min |
Hovering IGE |
5334 |
m |
17500 |
ft |
Hovering OGE |
3505 |
m |
11500 |
ft |
Service Ceiling |
> 6096 |
m |
> 20000 |
ft |
OEI max service ceiling |
3688 |
m |
12100 |
ft |
Max Range* |
926 |
km |
500 |
nm |
Max endurance* |
4 h 46 min |
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