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 Aircraft operated by PHI and Air Methods under each company's FAA Part 135 On-Demand Air Carrier certificates
TECHNOLOGY
 The EC 135's aerodynamic fuselage-constructed from the latest composite technologies-contributes to its excellent speed and range.
 Its unique Bearingless Main Rotor and innovative Low Noise Fenestron™ tail rotor system...
 ...offers outstanding maneuverability as well as an exceptionally smooth and quiet ride.
"Phase modulation" by unequal blade spacing makes fenestron™ sound "pleasant".
 The cockpit can be either in conventional configuration or, with the "Avionique Nouvelle" glass cockpit.
MISSIONS
 PASSENGER TRANSPORT The EC 135 provides an outstanding work environment.There is room for five in the VIP configuration or up to seven passengers plus the pilot when used as a corporate shuttle.Luxury materials and practical fittings combine with extremely low noise and vibration levels to create a pleasant professional atmosphere.
 RESCUE This new generation of light-twin EMS helicopters was developed in close cooperation with doctors, rescue experts, designers and engineers and in compliance with the strictest guidelines of the JAR Part 27. Already in service worlwide, the EC 135 demonstrates its high standard and flexibility an the rescue and EMS business.
 POLICE OPERATION Whatever action the mission requires, the EC 135 is the convincing solution to any problem. In accordance with the requirements of many police forces around the world, a wide range of equipment has been developed ensuring the flexibility and reliable mission capability.
POWER PLANT
EC 135P2
 PRATT & WHITNEY PW 206B2 turbine engine
Power per engine in ISA, at sea level :
| On 1 Engine |
kW |
ch |
shp |
| One Engine Inoperative (30sec. power) |
609 |
828 |
816 |
| One Engine Inoperative (2.0min. power) |
580 |
789 |
777 |
| One Engine Inoperative (MCP) |
528 |
718 |
708 |
| On 2 engines |
kW |
ch |
shp |
| Take-off power (TOP) |
463 |
630 |
621 |
| Maximum continuous power (MCP) |
419 |
570 |
562 |
EC 135T2
 TURBOMECA Arrius 2B2 turbine engine
Power per engine in ISA, at sea level :
| On 1 Engine |
kW |
ch |
shp |
| One Engine Inoperative (30sec. power) |
609 |
828 |
816 |
| One Engine Inoperative (2.0min. power) |
580 |
789 |
777 |
| One Engine Inoperative (MCP) |
528 |
718 |
708 |
| On 2 engines |
kW |
ch |
shp |
| Take-off power (TOP) |
452 |
615 |
606 |
| Maximum continuous power (MCP) |
426 |
579 |
571 |
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