
-
light
-
light/intermediate
-
intermediate
-
medium
-
medium/heavy
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. This ability 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.
Technical Data
| Weights | ||||
|---|---|---|---|---|
| Max take off | 3000/ 3175 | kg | 6614/ 7000 | lb |
| Standard configuration empty weight | 1970 | kg | 4343 | lb |
| Engine Rating (2 x Turbomeca Arrius 2K-1) | ||||
|---|---|---|---|---|
| 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 | 534 | kW | 716 | 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 | 161 | USgal |
| 4-cell fuel system | 716 | l | 233 | USgal |
| 5-cell fuel system | 881 | l | 233 | 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 | 1.94 | m | 6.36 | ft |
| Performance (ISA, 3000 kg /6614 lb) | ||||
|---|---|---|---|---|
| VNE | 311 | km/h | 168 | kts |
| Cruise speed | 282 | km/h | 152 | kts |
| Rate of climb | 8.33 | m/sec | 1640 | ft/min |
| Hovering IGE (TOP) | 5305 | m | 17400 | ft |
| Hovering OGE (TOP) | 3475 | m | 11400 | ft |
| Service ceiling (MCP) | 6096 | m | 20000 | ft |
| Max Range* | 926 | km | 500 | nm |
| Max endurance* | 4 h 46 min | |||
* with 230 USG fuel - no reserve - @5000 ft
Equipment
- 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 / 600 lbs)
- Emergency floats
- Rotor brake
- Engine fire extinguishers
- External loudspeakers
- FLIR / LLTV
- Laser warning
- Missile approach warning system
- Radar warning
- Searchlight
- Rear view mirror
- Snow skis / slump protection pads
- Windshield wipers
- Wire strike protection system
Avionics
- Flight Management System
- Radio Management System
- VHF-UHF / AM-FM radio
- HF / SSB radio
- ADF
- DME
- GPS
- Doppler Velocity Sensor
- AHRS
- Stormscope
- IFF Transponder
- Radar altimeter
- ELT system
- VOR / ILS
- Digital Map Generator
- ICS
Armament
- 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)
Brochures
AW109 Light Utility Helicopter
.pdf (843 KB)