Airbus H155

First developed in 1997, Airbus’ twin-engine H155 is designed for a wide range of missions, including private and business aviation, emergency medical services(EMS), rescues and safety operations and firefighting. Currently, KAI hold the technology to domestically produce the H155B1 which holds 30% passenger capacity and an extended of configuration of 130% cargo space.

Model LCH (H155B1 / EC155B1)
Pilot 2 Pilot
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)
Max takeoff Weight 4,920 kg (10,847 lb)
Engine 2 × Turbomeca Arriel 2C2 turboshaft engines, Take-off Power, 697 kW (935 hp) each
Main Rotor Diameter 12.6 m (41 ft 4 in)
Main Rotor Area 124.7 m2 (1,342 sq ft)
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)
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EC-155B1

Registration : HL9688
Pilot: 2
Capacity: 13Pax or Cargo 2,301 kg (5,073 lbs)
Operator: Gloria Aviation

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EC-155B1

Registration : HL9274
Pilot: 2
Capacity: 13Pax or Cargo 2,301 kg (5,073 lbs)
Operator: Gloria Aviation

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EC-155B1

Registration : HL9697
Pilot: 2
Capacity: 13Pax or Cargo 2,301 kg (5,073 lbs)
Operator: Gloria Aviation

14, Wangsan-ro, Dongdaemun-gu, Seoul, Republic of Korea, 02582

14, Wangsan-ro, Dongdaemun-gu, Seoul, Republic of Korea, 02582