Previously designated EC175. Seeking to increase MGW to 7800kg (17200lb)

Overview

Data on design, manufacture and status

Design authority: Airbus Helicopters

Primary manufacturer: Airbus Helicopters

Parent type: Airbus Helicopters H175/EC175

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 2

Crew seating: Side-by-side

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Overall Height: 5.34 m (17.5 ft)

Overall Length: 18.06 m (59.3 ft)

Overall Width: 14.80 m (48.6 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: P&WC PT6C-67E turbine

Engine manufacturer: Pratt & Whitney Canada

Max continuous power: 1227 kW (1645 hp)

Take-off / rated power: 1324 kW (1775 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 7800 kg (17196 lb)

Max Range: 1060 km (572 nm)

Max Endurance: 5.7 hrs (5.7 hrs)

Related VFS Resources

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Related Public Resources

Resources related to the H175/EC175 , provided by public sources across the internet.

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