Airbus Helicopters Logo

About us

Helicopter Models

Sales & Marketing

Optional Equipment

Markets

Customer support

Training

Safety

Suppliers

Quality

Environmental Policy

Awards

News

Careers




Company Store Button

Products > H155 (formerly known as EC155) specifications

H155 (formerly known as EC155) specifications

EC155 Specification image

At a glance

Max weight: 10,846 lbs.

Capacity: 1 or 2 pilots + 12 passengers

Powerplant: 2 Turbomeca Arriel 2C2

Fast cruise speed: 143 kts.

External dimensions

Rotor diameter: 41.3 ft

Length with all blades: 46.9 ft.

Overall width: 11.4 ft.

Documentation

H155 technical files

General data

Empty weight of standard aircraft: 5,574 lbs.

Maximum takeoff weight: 10,846 lbs.

Useful load: 5,072 lbs.

Maximum takeoff weight (with external load): 10,846 lbs.

Usable fuel capacity (standard tank): 332 gal.

Powerplant: 2 Turbomeca Arriel 2C2

Cabin volume: 235.20 cu. ft.

Baggage compartment volume: 88.29 cu. ft.

Standard seating capacity: 1/2+12

*Performance data

Never exceed speed: 175 kts.

Fast cruise speed: 143 kts.

Maximum range (with no reserves): 423 nm.

Maximum endurance (with no reserves): 4.1 hrs.

Hover in ground effect ceiling (5 ft. skid height): 7,050 ft.

Hover out of ground effect ceiling: 8000 ft.

Takeoff power per engine: 943 shp.

Rate of climb (all engines operative, MCP): 1,154 fpm.

Rotor Journal image