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Leonardo AW139
The AW139, first named AB139, was certified in Italy in June 2003 and by EASA in September 2003 as a large rotorcraft for Category A and B operations. A fully articulated five-blade main rotor 13.80 meters across is driven by two Pratt and Whitney Canada PT6C-67C or PT6C-67C1 turboshaft engines with electronic engine control. Up to 15 passengers fit in the cabin. The maximum take-off weight is 6,400 kg, with higher weights allowed when approved kits are fitted, and the operating altitude reaches 20,000 feet. The fuselage is 13.53 meters long, or 13.73 meters with the long nose, and the tanks hold 1,568 litres of usable fuel.
- Engines
- Two Pratt & Whitney Canada PT6C-67C or PT6C-67C1 turboshafts mounted above the fuselage
- Max takeoff weight
- 14,100 lb (6,400 kg)
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Specifications
| Length | 44 ft 5 in (13.53 m) |
|---|---|
| Height | 12 ft 2 in (3.72 m) |
| Ceiling | 20,000 ft (6,100 m) |
| Fuel capacity | 410 US gal (1,568 L) |
| Status | In service |
| Type codes | ICAO A139 |
Who flies it now
52 flights by other operators
From flights seen in US airspace in the last 14 days (public flight data).
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