page_title: Eurocopter EC130
section_title: Specifications (EC130 B4)
hierarchical_section_title: Eurocopter EC130 / Specifications (EC130 B4)
caption_attribution_description: English: The cockpit of an Eurocopter EC 130.
context_page_description: The Eurocopter EC130 is a single engine light utility helicopter developed from the earlier Eurocopter AS350 Écureuil, one of the primary changes from which was the adoption of a Fenestron anti-torque device in place of a conventional tail rotor. It was launched and produced by the Eurocopter Group, which would later be rebranded as Airbus Helicopters.
context_section_description: Data from 
  General characteristics
  Crew: 1
  Capacity: 6 passengers (2 at front and four in the rear) can be modified to take 7 passengers (3 at front and four in the rear)
  Length: 10.68 m (35 ft 0 in)
  Height: 3.34 m (10 ft 11 in)
  Empty weight: 1,377 kg (3,036 lb)
  Max takeoff weight: 2,427 kg (5,351 lb)
  Fuel capacity: 540 l (140 US gal; 120 imp gal)
  Usable fuel: 538.7 l (142.3 US gal; 118.5 imp gal)1
  Powerplant:  × Turbomeca Arriel 2B1 turboshaft engine, 632 kW (848 hp)
  Main rotor diameter:  10.69 m (35 ft 1 in)
  Main rotor area: 89.75 m² (966.1 sq ft) three blades
  Performance
  Cruise speed: 240 km/h (150 mph, 130 kn)
  Never exceed speed: 287 km/h (178 mph, 155 kn) power on (less 3 kt/1 000 ft)
  231.5 km/h (143.8 mph; 125.0 kn) power off (less 3 kt/1 000 ft)
  Range: 610 km (380 mi, 330 nmi)
  Service ceiling: 7,010 m (23,000 ft) max permitted in cruise
  Rate of climb: 9 m/s (1,800 ft/min)
  Avionics
  
  Vehicle and Engine Multifunction Display (VEMD) with First Limit Indicator (FLI) fitted as standard.
caption: Cockpit of an EC130
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