AW109 Light Utility Helicopter (LUH)
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-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 | 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 | 598 l 158 USgal |
4-cell fuel system | 713 l 188 USgal |
5-cell fuel system | 880 l 232 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 | 283 km/h 153 kts |
Rate of climb | 8.53 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 with 230 USgal fuel - no reserve - @5000 ft |
Max endurance | 4 h 46 min with 230 USgal fuel - no reserve - @5000 ft |
Equipment |
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Avionics |
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Armament |
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NEWSLETTER
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