EC 135
- Maximum take-off weight (MTOW): 2910 kg
- Take-off power: 2 x 320 kW (2 x 435 KM)
- Maximum continuous power: 2×457 kW (2 x 621 KM)
- Maximum emergency power (OEI 30”): 526 kW (715 KM)
- Intermediate emergency power (OEI 2’): 513 kW (698 KM)
- Fuel tank capacity: 710 l
- Lenght: 10,21 m
- Length (rotor rotating): 12,19 m
- Maximum height: 3,62 m
- Main rotor diameter: 10,02 m
- Tail rotor diameter: 1,0 m
- Maximum speed, VNE (MTOW 2910 kg): 259 km/h
- Cruise speed (MTOW 2910 kg): 254 km/h
- Rate of climb (MTOW 2910 kg): 7,6 m/s
- Service ceiling: 13 000 ft
- Maximum range (MTOW 2910 kg, without fuel reserves, while maintaining economic speed and with long-range fuel tank configuration): 835 km
- Maximum flight time (parameters same as in point 16): 4,45h
- Crew: 1/2 pilots, paramedic/nurse, doctor
The interior of the EC 135 helicopter
