Airbus Helicopters is responsible for the H175's main gearbox, tail rotor, avionics, autopilot, hydraulic and electrical systems, doors and transparencies. Airbus Helicopters is also the technical lead and system integrator, and built two of the three prototypes (the first and third). HAIG is responsible for the airframe, tail and intermediate gearboxes, main rotor, fuel system, flight controls and landing gear. Each firm separately handles marketing, customer support, and certification efforts for the type. Both the design and production of the rotorcraft made extensive use of
computer-aided design/computer-aided manufacturing (CAD/CAM). CAD allowed Airbus Helicopters and HAIG to create a virtual mock-up, simplifying coordination between partners based 10,000 km apart. Airbus Helicopters-built H175s are powered by two 1,325 kW (1,775 shp) class,
Full Authority Digital Engine Control (FADEC)-equipped
Pratt & Whitney Canada PT6C-67E turboshaft engines, which provide for a 5,000-hour
time between overhaul (TBO) and on-condition maintenance. Chinese-produced AC352s are equipped with two
modular 1,800 shp class, dual-FADEC
Turbomeca Ardiden 3C/WZ16 turboshaft engines, which were specifically developed by a joint partnership between
Turbomeca and
AVIC Engine for the rotorcraft. The engines drive the rotorcraft's five-blade Spheriflex main rotor and a three-blade tail rotor. The EC175's main gearbox will incorporate two accessory gearboxes and will be de-clutchable, avoiding the cost and weight of an
auxiliary power unit (APU). The gears and the casing of the H175's main gearbox were developed using
CATIA V5, a first for Airbus Helicopters. The H175 was designed to exceed EASA CS-29
crashworthiness requirements. It is capable of performing full Category A dual-pilot operation; additionally, it possesses
Sea State 6 capability, and can be equipped with two oversized 18-passenger life rafts and an emergency flotation system. Airbus Helicopters states that the H175's noise signature is "way below"
International Civil Aviation Organization (ICAO) requirements. The H175 is built for civilian and parapublic applications, its primary markets being support of the oil and gas industry and search and rescue missions. Other applicable roles include parapublic operations, homeland security, air medical services, utility missions and corporate transportation. The EC175 is offered with multiple interior seating configurations, housing up to 18 passengers in an oil and gas transport configuration, 9-12 passengers in an executive layout, and 6-8 in a VIP configuration It is fitted with wide sliding doors for ease of access and oversized jettisonable windows for emergency egress. The H175 has a flat floor without any partition between the cockpit and the cabin area, which enables various flexible layouts to be adopted. Either auxiliary fuel tanks or a storage area can be installed beneath the cabin floor, which can be accessed internally; a large luggage compartment externally accessible from either side is present in some configurations. The Helionix avionics suite is used on the H175; much of the state-of-the-art avionics are derived from those developed for the
Eurocopter EC225; one such system is the Automatic Flight Control System (AFCS), a 4-axis dual-duplex autopilot which is linked to the rotorcraft's
Flight Management System. The cockpit features a total of four 6X8-inch multi-function
LCD displays, plus an optional central mission display. The H175's cockpit is
night vision goggles-compatible. A sensor operator's console can be installed in the main cabin area, and a chin-mounted electrical-optical sensor can be equipped. ==Operational history==