AW119 Koala
| Weights | |
| Max take off (int. loads) | 2850 kg 6283 lb |
| Max take off (ext. loads) | 3150 kg 6945 lb |
| Basic empty weights | 1455 kg 3208 lb |
| Engine Rating | (Pratt & Whitney PT6B-37A) |
| Take off | 747 kW 1002 shp |
| Maximum continuous power | 650 kW 872 shp |
| Transmission Rating | |
| Take off | 684 kW 917 shp |
| Maximum continuous power | 671 kW 900 shp |
| Fuel Capacity | |
| 3-cell fuel system 605 l | 160 USgal |
| 4-cell fuel system 711 l | 188 USgal |
| 5-cell fuel system 870 l | 230 USgal |
| Crew Pilots/Passengers | 1-2 / 7-6 |
| External Dimensions | |
| Length (rotors turning) | 12.92 m 42.37 ft |
| Width (rotor blades at 45°) | 7.76 m 25.43 ft |
| Maximum height | 3.60 m 11.78 ft |
| Main rotor diameter | 10.83 m 35.53 ft |
| Tail rotor diameter | 1.94 m 6.36 ft |
| MR tip blade ground clearance | 2.83 m 9.3 ft |
| TR tip blade ground clearance | 1.15 m 3.77 ft |
| Fuselage ground clearance | 0.63 m 2.06 ft |
| Performance | (ISA, 2850 kg / 6283 lb) |
| VNE | 282 km/h 152 kt |
| Max speed | 256 km/h 138 kt |
| Rate of climb | 9.4 m/s 1850 ft/s |
| Hovering IGE (TOP) | 3352 m 11000 ft |
| Hovering OGE (TOP) | 2225 m 7300 ft |
| Service ceiling (MCP) | 4572 m 15000 ft |
| Max range | 954 km 515 nm with 230 USgal fuel - no reserve - @ 5000 ft |
| Max endurance | 5 h 20 min with 230 USgal fuel - no reserve - @ 5000 ft |
| Equipment |
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| Avionics |
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| Armament |
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