Airbus Helicopters H175
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A pair of prototypes and one production-quality airframe served in the EC175 testing program for Airbus Helicopters - the series introduced in late-2014.
Detailing the development and operational history of the Airbus Helicopters H175 Medium-Lift Utility Helicopter. Entry last updated on 11/18/2017. Authored by Staff Writer. Content ©www.MilitaryFactory.com
The EC175 is a conventional helicopter through and through. It holds a well-sloped, windowed nose cone offering expanded forward views from the two-seat cockpit. Pilots sit in a traditional side-by-side arrangement. Passenger seating behind the flight deck is expansive as medium helicopters go with each fuselage side covered by a sliding access door - total accommodation numbering up to eighteen depending on the internal seating configuration used. The pilots enter and exit the cockpit through conventional, automobile-style hinged doors. The tail stem houses the drive shaft powering the tail rotor which is seated to portside. The main rotor sits atop the twin-engine layout which themselves are seated atop the passenger cabin. The helicopter features an all-wheel undercarriage that is wholly retractable. Horizontal tailplanes are featured along the tail section, though well-aft of the tail stem and are found at the base of the vertical tail fin.
Power to the type is through 2 x Pratt & Whitney Canada PT6C-67E turboshaft engines developing 1,776 shaft horsepower each. This will provide a maximum speed of 195 miles per hour with a cruising speed of about 177 miles per hour. Range is listed to be 782 miles with a service ceiling of 19,685 feet.
While the helicopter is set to be produced in France as the EC175, AVIC of China has been granted local production of the type as the AC352. These will carry the in-house WZ-16 series turboshaft engine.
Any available statistics for the Airbus Helicopters H175 Medium-Lift Utility Helicopter are showcased in the areas immediately below. Categories include basic specifications covering country-of-origin, operational status, manufacture(s) and total quantitative production. Other qualities showcased are related to structural values (namely dimensions), installed power and standard day performance figures, installed or proposed armament and mission equipment (if any), global users (from A-to-Z) and series model variants (if any).
Our Data Modules allow for quick visual reference when comparing a single entry against contemporary designs. Areas covered include general ratings, speed assessments, and relative ranges based on distances between major cities.
Relative Maximum Speed Rating
This entry's maximum listed speed (172mph).
Graph average of 150 miles-per-hour.
Graph showcases the Airbus Helicopters H175's operational range (on internal fuel) when compared to distances between major cities.