1983 · Twin-engine intermediate turbine helicopter
Specifications
| Engine | 2 x Rolls-Royce Gem 2-1004D 815 shp |
|---|---|
| Capacity | 2 |
| Length (m) | 14.29 |
| Height (m) | 3.32 |
| Blades | 4 |
| Rotor diam. (m) | 11.9 |
| Disc area (m2) | 111.2 |
| Weight (kgs) | Empty: 2530 Max: 3700 |
| Speed (km/h) | Cruise: 265 Max: 315 |
Derivatives & Versions
| A129C | ||
| A129CBT | ||
| → AB139 | 2001 | Developed as a joint-venture between Italian Agusta and American Bell , the resulting Bell/Agusta AB139 first flew on February 3, 2001. |
| → AW129 Mangusta | 2007 | In 2007 Turkey signed with AgustaWestland an agreement to purchase 51 (+40 options) A129 Mangusta based on the A129 International and to be assembled in Turkey by TAI as the T-129 starting from 2013. |
Operators
| 1990- | Aviazione dell'Esercito |