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Eurocopter EC135

1994 · Twin-engine turbine helicopter

History C/N Operators Videos News
Twin-engine helicopter widely used amongst police, ambulance services and for executive transport. Originally developed by MBB from their Bo.108, was handed over to the new company Eurocopter in the 1990s incorporating the Fenestron tail rotor in the process. First flight achieved on February 15, 1994. The EC135 has been powered by a Turbomeca Arrius or by a Pratt & Whitney Canada PW206 and is equipped with a bearingless main rotor.

Manufactured at German site in Donauworth with first production aircraft (D-HQQQ) delivered on August 1st, 1996 to DRF. The 1000th EC135 was rolled out in 2011.

From January 1st, 2014 is known as Airbus Helicopters H135
blueprints EC135

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.