Derived from Bo108
1994 · Twin-engine turbine helicopter
Derivatives & Versions
| EC135T1 | 1995 | Powered by two 435 kW (583 shp) Turbomeca Arrius 2B1/2B1A/2B1A1 |
| EC635T2 | 1995 | Military designation for EC135T1 |
| EC135P1 | 1996 | Powered by two 463 kW (621 shp) Pratt & Whitney Canada PW206B |
| EC135P2 | 2001 | Introduced in 2001 is powered by two 463 kW (621 shp) Pratt & Whitney Canada PW206B2 with increased thermodynamic and mechanic OEI ratings (128% OEI torque. |
| EC635P2 | 2001 | Military designation for EC135P2. |
| EC135T2 | 2002 | Powered by two 452 kW (606 shp) Turbomeca Arrius 2B2 |
| EC135P2+ | 2006 | Powered by two 463 kW (621 shp) Pratt & Whitney Canada PW206B2 with FADEC, extended component time between overhaul (TBOs) and a change in the main transmission lubricating oil. |
| EC135T2+ | 2006 | Powered by two 473 kW (634 shp) Arrius 2B2 with FADEC and others upgrades. |
| EC635P2+ | 2007 | Military designation for EC135P2+ |
| EC635T2+ | 2007 | Military designation for EC135T2+ |
| EC635VIP | 2008 | Military VIP |
| EC135 Hermès | 2009 | “l’Hélicoptère par Hermès”, VVIP variant |
| TH-135 | 2009 | EC. |
| → EC135/H135 | 2014 | Airbus production. |