Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Airbus Helicopters H135 Light Utility Helicopter (LUH).
2 x Safran Helicopter Engines (Turbomeca) "Arrius" 2B2+ turboshaft engines developing 633 horsepower each OR 2 x Pratt & Whitney Canada PW206B3 turboshaft engines developing 621 horsepower each and driving four-bladed main rotor and shrouded multi-bladed tail rotor.
Propulsion
180 mph
290 kph | 157 kts
Max Speed
20,013 ft
6,100 m | 4 miles
Service Ceiling
395 miles
635 km | 343 nm
Operational Range
1,500 ft/min
457 m/min
Rate-of-Climb