AgustaWestland / Agusta-Bell AW139 (AB139)
AW139 (AB139)
Medium Utility Helicopter
| Crew | 2 |
| Passengers | 15 |
| | ||
| Propulsion | 2 Turboshaft Engines |
| Engine Model | Pratt & Whitney Canada
PT6C-67C |
| Engine Power (each) | 1250 kW | 1676 shp |
| | ||
| Speed | 310 km/h | 167 kts |
| Service Ceiling | 6.096 m | 20.000 ft |
| Range | 1.061 km | 573 nm |
| | ||
| Empty Weight | 3.622 kg | 7.985 lbs |
| max. Takeoff Weight | 6.400 kg | 14.110 lbs |
| | ||
| Rotor Blades (main/tail) | 5/4 | 5/4 |
| Main Rotor Diameter | 13,80 m | 45,3 ft |
| Tail Rotor Diameter | 2,70 m | 8,9 ft |
| Rotor Disc Area | 149,6 m² | 1612 ft² |
| Length (Fuselage) | 13,53 m | 44,4 ft |
| Length | 16,65 m | 54,6 ft |
| Height | 4,95 m | 16,2 ft |
| | ||
| First Flight | 03.02.2001 |
| Production Status | in production |
| | ||
| ICAO Code | A139 |
| FAA TCDS | R00002RD |
| EASA TCDS | R.006 |
| | ||
| Data for (Version) | AgustaWestland AW139 |
| Remarks | Developed together with Bell as AB-139. Bell sold their rights on to AgustaWestland. |
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