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General Info

Airbus Helicopters EC155 Dauphin II


General information
Type Passenger transport helicopter
National origin Multinational
Manufacturer Eurocopter
Airbus Helicopters
Status Active
History
Manufactured 1997-present
Introduction date March 1999
First flight 17 June 1997
Developed from Eurocopter AS365 Dauphin
Variants KAI LCH
Developed into Eurocopter X³
KAI LAH

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History  Airbus Helicopters H155 (formerly Eurocopter EC155)
Manufactured 1997-present First flight 17 June 1997

Design

EC155 B1 of Kingfisher Airlines in India

The EC155 B features a completely redesigned cabin providing 30% more passenger space than previous Dauphin helicopter models, plus a 130% increase in baggage hold volume. Other major improvements include a five-blade Spheriflex composite main rotor combined with the familiar shrouded Fenestron tail rotor to reduce vibration levels significantly. The EC155 B is powered by two 635 kW (851 shp) Turbomeca Arriel 2C1 turboshaft engines which feature a dual-channel Full Authority Digital Engine Control (FADEC) system. The EC155 B1 features uprated 697 kW (935 shp) Arriel 2C2s. The helicopter can be fitted with an anti-icing system to enable the aircraft to operate in very cold climates. The all-glass cockpit is equipped with an 'Avionique Nouvelle' integrated digital flight control system featuring Eurocopter's Vehicle and Engine Management Display (VEMD), which utilizes active matrix liquid crystal displays. The EC155 is also equipped with a four-axis digital autopilot, coupled to the engine FADECs for full-envelope protection, and is offered with a Health and Usage Monitoring System (HUMS).

Variants

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Km

Ceiling

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Km

Range

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Km/H

Aircraft Speed

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Max Crew

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Airbus Transport

Airbus Helicopters H155 (formerly Eurocopter EC155) Manufactured 1997-present
 First flight 17 June 1997

1

General characteristics

        • Crew: 1 or 2 (pilots)
        • Capacity: 13 passengers or 2,301 kg (5,073 lb) payload
        • Length: 14.3 m (46 ft 11 in)
        • Height: 4.35 m (14 ft 3 in)
        • Empty weight: 2,618 kg (5,772 lb)
        • Gross weight: 4,950 kg (10,913 lb)
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  • Powerplants

      • Max takeoff weight: 4,920 kg 
      • Powerplant: 2 × Turbomeca Arriel 2C2 turboshaft engines, Take-off Power, 935 hp) each
      • Main rotor diameter: 12.6 m 
      • Main rotor area: 124.7 m2 
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Specifications

  • Never exceed speed: 324 km/h (201 mph, 175 kn)
  • Range: 857 km (533 mi, 463 nmi)
  • Ferry range: 985 km (612 mi, 532 nmi)
  • Service ceiling: 4,572 m (15,000 ft)
  • Rate of climb: 8.9 m/s (1,750 ft/min)
Special Links Airbus Helicopters H155 (formerly Eurocopter EC155) Manufactured 1997-present First flight 17 June 1997

Links to Youtube & Others

In March 1999, deliveries of the EC155 B commenced, the German Federal Police became the first operator of the type. Between March 1999 and June 2003, roughly 50 EC155 Dauphins were sold, mainly to VIP and off-shore customers

Airbus Helicopters 
EC155 Dauphin II

The LCH is to enter service in 2020, and the LAH will follow in 2022 to replace the MD 500 Defender and AH-1J/S Cobra.

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Youtube Link

In 2015, Airbus Helicopters and Korean Aerospace Industries (KAI) formed an agreement to transfer principle manufacturing activity for the EC155 to South Korea

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