Products
AW109 LUH
The AW109 Light Utility Helicopter (LUH) has established itself as a best-selling military light-twin helicopter able to satisfy a wide range of military requirements. The ability of AW109 LUH to fulfil a wide range of missions makes the aircraft a true force multiplier, providing military commanders with excellent operational flexibility. The AW109 LUH is a rugged helicopter with excellent ballistic tolerance, redundancy of systems and crashworthiness for maximum safety and survivability. Avionics include an advanced digital cockpit, based on 3 AMLCDs and a digital 4-axis AFCS. A vast array of advanced equipment including sophisticated sensors are available. The integrated Mission Equipment Package (MEP) includes day/night and IFR avionics for single or dual pilot operations with a four-axis digital Automatic Flight Control System (AFCS). The availability of a wide range of mission equipment makes the LUH a real multi-role helicopter, able to perform all light helicopter roles including training, troop transport, medical evacuation, search and rescue, maritime patrol, observation, armed escort and anti-armour. In addition, the AW109 LUH can also be armed with rocket pods, machine gun pods, pintled mounted machine guns, anti-tank and air-to-air missiles.
| Weights | ||||
|---|---|---|---|---|
| Max take off | 3000 | kg | 6614 | lb |
| Basic empty weights | 1970 | kg | 4343 | lb |
| Engine Rating (2 x Turbomeca Arrius 2K-2) | ||||
|---|---|---|---|---|
| Take off power (5 min) | 2 x 530 | kW | 2 x 711 | 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 | 530 | kW | 711 | shp |
| Transmission Rating | ||||
|---|---|---|---|---|
| Maximum continuous power | 2 x 336 | kW | 2 x 450 | 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 | 588 | l | 155 | USgal |
| 4-cell fuel system | 703 | l | 186 | USgal |
| 5-cell fuel system | 870 | l | 230 | USgal |
| Crew | |
|---|---|
| Pilots / Passengers | 1 - 2 / 7 - 6 |
| External Dimensions | ||||
|---|---|---|---|---|
| Length (rotors turning) | 12.93 | m | 42.41 | ft |
| Length (rotors stopped) | 11.43 | m | 37.5 | ft |
| Maximum height | 3.42 | m | 11.22 | ft |
| Main rotor diameter | 10.83 | m | 35.53 | ft |
| Tail rotor diameter | 1.95 | m | 6.36 | ft |
| Performance (ISA, 3000 kg /6614 lb) | ||||
|---|---|---|---|---|
| VNE | 311 | km/h | 168 | kts |
| Cruise speed | 283 | km/h | 153 | kts |
| Rate of climb | 8.54 | m/sec | 1680 | ft/min |
| Hovering IGE (TOP) | 5334 | m | 17500 | ft |
| Hovering OGE (TOP) | 3505 | m | 11500 | ft |
| Service ceiling (MCP) | 6096 | m | 20000 | ft |
| Max Range* | 926 | km | 500 | nm |
| Max endurance* | 4 h 46 min | |||
* with 230 USgal fuel - no reserve - @5000 ft
- Bleed air heater
- Pilot / co-pilot armoured seats
- Crashworthy fuel system
- Self sealing fuel tanks
- Reinforced windshields
- Engine air particle separators
- 1 or 2 longitudinal stretcher installation
- Single or dual external cargo hook (1000 kg / 500 kg)
- Rescue hoist (272 kg)
- Emergency floats
- Rotor brake
- Engine fire extinguishers
- External loudspeakers
- FLIR / LLTV
- Laser warning
- Infrared jammer
- Missile approach warning system
- Searchlight
- Optic gyro
- Radar warning
- Rear view mirror
- Snow skis / slump protection pads
- Windshield wipers
- Wire strike protection system
- VHF-UHF / AM-FM
- HF / SSB
- Homing
- ADF
- DME
- GPS
- Doppler Velocity Sensor
- AHRS
- Stormscope
- IFF Transponder
- Radar altimeter
- ELT system
- VOR / ILS
- Digital Map Generator
- ICS
- Rocket launcher 7/12/19 tubes 70 mm
- Twin machine gun-pod 7.62 mm
- Machine gun-pod 12.7 mm
- Machine gun-pod 12.7 mm with 3 tubes 70 mm rockets
- Antitank missiles (TOW, HOT or Hellfire)
- Air-to-air missiles (Stinger or Mistral)
AW109 Light Utility Helicopter
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