Eurocopter EC120 / Airbus Helicopters H120
The Eurocopter EC120 Colibri (ICAO model code EC20) is a single-engine rotorcraft, originally designed by Eurocopter Group, China National Aero-Technology Import and Export Corporation, Harbin Aviation Industries Group and Singapore Technologies Aerospace.
Technical specifications
• Crew: 1
• Capacity: 4 PAX / 755 kg (1,664 lb) payload
• Length: 11.52 m (37 ft 10 in) overall, 9.6 m (31 ft) fuselage
• Height: 3.4 m (11 ft 2 in)
• Empty weight: 960 kg (2,116 lb)
• Max takeoff weight: 1,715 kg (3,781 lb) internal load, 1,800 kg (3,968 lb) external load
• Fuel capacity: 416 L (110 US gal; 92 imp gal) in two tanks
• Powerplant: 1 × Turbomeca TM 319 Arrius 2F turboshaft, 376 kW (504 hp) for take-off 335 kW (449 hp) max continuous
• Main rotor diameter: 10.0 m (32 ft 10 in)
• Main rotor area: 78.54 m2 (845.4 sq ft)
• Cruise speed: 226 km/h (140 mph, 122 kn) max 191 km/h (119 mph; 103 kn)
• Never exceed speed: 278 km/h (173 mph, 150 kn)
• Range: 727 km (452 mi, 393 nmi) no reserves
• Endurance: 4 hours 32 minutes
• Service ceiling: 5,180 m (16,990 ft)
• Hover ceiling IGE: 2,820 m (9,252 ft)
• Hover ceiling OGE: 2,320 m (7,612 ft)
• Rate of climb: 6.1 m/s (1,200 ft/min)
• Disk loading: 21.8 kg/m2 (4.5 lb/sq ft) internal load, 22.9 kg/m2 (5 lb/sq ft) external load
• Power/mass: 0.19 kW/kg (0.12 hp/lb) internal load, 0.1835 kg (0 lb) external load
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