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EC 135

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

The interior of the EC 135 helicopter

               
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