Airbus H125

Overview

• More popularly known as the Astar or AS350, Airbus' H125 has a long and storied history in the light single-engine helicopter segment. With a powerful Safran Arriel 2D engine and seating configurations that create maximum flexibility, the H125 has been known to perform everything from owner-flown transportation to extractions off Mount Everest.

  Airbus Helicopter Training Center

Specifications

• Powerplant

  Safran Arriel 2D, 847 shp

• Propellers

• Length

• Height

• Wingspan

• Wing Area

• Wing loading

• Power loading

• Cabin Width

• Empty Weight

• Maximum gross weight

  4,960 lb

• Useful load

  2,152 lb

• Payload with full fuel

• Fuel capacity

  939 lb

• Baggage capacity

  105.9 cu ft

Performance

• Takeoff distance ground roll

• Takeoff distance over 50-ft obstacle

• Rate of climb sea level

• Service ceiling

  16,550 ft

• Landing distance over 50-ft obstacle

• Landing distance ground roll

• Cruise speed/endurance w/45-min rsv, std fuel (fuel consumption, ea engine) @ 75% power, best economy

  140 kt/4.4 hr

• Range

Limiting and Recommended Airspeeds

• V_X

• V_Y

• V_NE

  155 kt

• V_S1

• V_SO

For more information, contact Airbus Helicopters at or via https://www.airbushelicopters.ca/product/h125/

All specifications are based on manufacturer's calculations. All performance figures are based on standard day, standard atmosphere, sea level, gross weight conditions unless otherwise noted.