Designed to meet the rigorous standards of those who demand the best.
The AW139 surpasses all other intermediate twin-engine helicopters in capability, speed, ride quality and passenger cabin space.

The AW139 is the market-leading intermediate twin-engine helicopter – the benchmark for safety design features, performance capabilities and productivity in challenging multi-role operations all over the world.

The aircraft features leading edge technology, including a Honeywell Primus Epic fully integrated avionics system and 4-axis digital AFCS and benefits from the best-in-class power reserve and outstanding power to weight ratio, which provides Category A performance capabilities with no limitations in a wide range of operating conditions, including ‘hot and high’.

Passengers and mission operators benefit from the largest, most comfortable cabin in the intermediate twin-engine class.

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Max Take-Off Weight 6400/6800/7000 Kg
Max useful load 2650/3050 Kg
Engine Rating (Pratt & Whitney PT6C-67C)
Take off power 2 x 1679 shp
Maximum continuous power 2 x 1631 shp
Take off power 2200 shp
Maximum continuous power 2000 shp
Fuel Capacity
Standard 1568 litre
Auxiliary 500 litre
Pilots / Passengers 1-2 / 15
External Dimensions
Length (rotors turning) 16,66m
Overall height 4,98m
Main rotor diameter 13,80 m
Vne 167 kts
Max cruise speed 165 kts
Hovering IGE (TOP) 15360 ft
Hovering OGE (TOP) 8130 ft
Service ceiling (MCP) 20000 ft
Max range 675 nm*
Max endurance 5 h 56 min*

*: With 1654 kg fuel – no reserve – @ 6000 ft