Derived from AB139
2005 · Twin-engine medium turbine helicopter
Specifications
| Engine | 2 x Pratt & Whitney Canada PT6C-67C 1679 shp |
|---|---|
| Capacity | 2 + 15 |
| Length (m) | 13.77 |
| Height (m) | 3.72 |
| Blades | 5 |
| Rotor diam. (m) | 13.8 |
| Disc area (m2) | 149 |
| Weight (kgs) | Empty: 3600 Max: 6400 |
| Speed (km/h) | Max: 310 |
| Range (km) | 1000 |
| Ceiling (m) | 6000 |
| Rate/Climb (m/min) | 654 |
Derivatives & Versions
| US139 | 2005 | The AgustaWestland/L-3 Communications US139 was the proposal entry for the US Army LUH programme. |
| → AW149 | 2009 | An enlarged military version of the AW139, the AW149 prototype first flew on November 13, 2009. |
| AW139M | 2011 | The AW139M designation was first used for the customized military version for the US Air Force Common Vertical Lift Support Program or CVLSP to seek a replacement for the UH-1N . |
| → MH-139A Grey Wolf | 2017 | First announced on March 2 2017, the MH-139 was Boeing proposal for the supply of up to 84 helicopters to replace the USAF UH-1N with a version of the Leonardo AW139 produced in Philadelphia. |