Aerodynamic innovations include a biplane tailplane stabiliser for greater low speed stability, and a quieter canted fenestron which combined produce an extra 80 kg of lift. The H160 is the first civilian helicopter to utilise a canted fenestron anti-torque tail rotor. The H160 is powered by two Turbomeca Arrano turboshaft engines.
General characteristics
Crew: 1/2
Capacity: 12
Length: 13.96m (45 ft 10 in)
Width: 3.54m (11 ft 7 in)
Height: 4.91m (16 ft 1 in)
Empty weight: 4,050 kg (8,929 lb)
Max takeoff weight: 6,050 kg (13,338 lb)
Useful load: up to 2,000 kg (4,409 lb)
Fuel capacity: 1,120 kg (2,469 lb)
Powerplant: 2 × Safran Arrano 1A turboshaft engines, 955 kW (1,280 shp) each
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