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Eurocopter EC155B1

2001 · Twin-engine intermediate turbine helicopter

History C/N Operators News
Built by Eurocopter France, was the succeesor of the EC155B and is powered by two Turbomeca Arriel 2C2 FADEC engines. Maximum take-off weight (MTOW) increased by 120 kg to 4,920 kg and with 10% extra engine power.

Eurocopter Southeast Asia was the first subsidiary certified to upgrade 155B airframes starting with those from SSFC.

From 2014 produced by Airbus Helicopters

Specifications

Engine2 x Safran Arriel 2C2 938 shp
Capacity2 + 13
Length (m)14.3
Height (m)4.35
Blades5
Rotor diam. (m)12.6
Disc area (m2)124.7
Weight (kgs)Empty: 2618 Max: 4920
Speed (km/h)Max: 324
Range (km)850
Rate/Climb (m/min)533
blueprints EC155B1