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  Eurocopter EC135  

The Eurocopter EC135 is a lightweight five/seven seat twin-turbine-engine multi-role helicopter with a radius of 720 km. The EC135 is offered with either Turbomeca Arrius 2B2 or Pratt and Whitney Canada PW206B2 engines. A militarized version called the EC 635 has been developed from the EC 135. Development of the Eurocopter EC135 started in the 80s as the MBB Bo.108 Advanced Technology Helicopter. The prototype BO108 with conventional tail rotor flew first on 15 October 1988. When the helicopter divisions of MBB from Germany and Aerospatiale from France merged in January 1992 to form the Eurocopter Group, the Bo108 program was transferred as well. An advanced low noise ducted 10-blade Fenestron tail rotor was, next to other modifications, incorporated into the design and the name of the helicopter was changed into Eurocopter EC135. The prototype of the EC135 (D-HBOX s/n S-01) flew first on 15 February 1994 and went into series production in 1996 at Donauwörth. After German certification was granted on 14 June 1996, was the first customer delivery on 31 July that year. Over 1050 have been delivered since the helicopter entered service in 1996 with the German rescue company DRF - Deutsche Rettungsflugwacht e.V.

The production and final assembly line of the EC 135 is at the Eurocopter Germany factory in Donauwörth in Germany. Next to the final assembly in Germany a second assembly line was put into operation at the Eurocopter Espana factory in Albacete, in the Castilla-La Mancha region in Spain. Next to this, as part of the Swiss light transport and training helicopter (LTSH) program for the Swiss air force, RUAG Aerospace opened an assembly line in Alpnach in Switzerland.

 Variants of the production EC135 models are: 
   - EC135 P1 (CDS)  
    Pratt & Whitney engine version with two PW 206 B engines. Firstly LBA approved on 14 June 1996. Serial numbers 0006 and upwards.  
   - EC135 P1 (CPDS)  
     Pratt & Whitney engine version with two PW 206 B engines.Firstly LBA approved on 06 November 1998. Serial number 0030 and upwards.  
   - EC135 P2 (CPDS)  
    Pratt & Whitney engine version with two PW 206 B2 engines.Firstly LBA approved on 10 July 2001. Serial numbers 0189 and upwards and upgraded EC135 P1 models.  
   - EC135 P2+    (EC135 P2i  is also used as marketing designation):  
   Pratt & Whitney engine version with two PW 206 B2 engines. Firstly EASA approved on 21 February 2006. Serial numbers 0505 and upwards and upgraded EC135 P2 models.  
   - EC135 T1 (CDS)  
 Turbomeca engine version with two Arrius 2B1A engines. Firstly LBA approved on 14 June 1996. Serial numbers 0005 and upwards.
 Early helicopters had 435kW Arrius 2B engines, later replaced by 500kW Arrius 2B1. Uprated Arrius 2B1A engine certified April 2001.
   - EC135 T1 (CPDS)  
   Turbomeca engine version with two Arrius 2B1A engines. Firstly LBA approved on 26 May 1999. Serial numbers 0028, 0092 and upwards.  
   Early helicopters had 435kW Arrius 2B engines, later replaced by 500kW Arrius 2B1. Uprated Arrius 2B1A engine certified April 2001.  
   - EC135 T2 (CPDS)  
   Turbomeca engine version with two Arrius 2B2 engines. Firstly LBA approved on 9 August 2002. Serial numbers 0243 and upwards and upgraded EC135 T1 models.  
 - EC135 T2+   (EC135 T2i  is also used as marketing designation)
 Turbomeca engine version with two Arrius 2B2 engines. Firstly EASA approved on 21 February 2006. Serial numbers 0506 and upwards ad upgraded EC135 T2 models.
 - EC635 T1 (CPDS): The military variant EC635 T1 (CPDS) corresponds to the EC135 T1 (CPDS) plus structural reinforcement of cabin structure.
   Military version with two Turbomeca Arius 2B1A engines. Firstly LBA approved on 31 August 2001. Serial numbers 0173 and upwards.  
 - EC635 P2+: The military variant EC635 P2+ corresponds to the EC135 P2+ plus structural reinforcement of cabin structure.
   Military version with two Pratt & Whitney PW 206 B2 engines. Firstly EASA approved on 6 December 2006. Serial numbers 0505 and upwards.  
 - EC635 T2+: The military variant EC635 T2+ corresponds to the EC135 T2+ plus structural reinforcement of cabin structure.
   Military version with two Turbomeca Arrius 2B2 engines. Firstly EASA approved on 6 December 2006. Serial numbers 0505 and upwards.  
 Non-production variants include:
 - EC135 ACT/FHS: Active control technology and flying helicopter simulator; German fly-by-light trials programme; first flight of modified production EC 135 (D-HECV) took place on 28 January 2002.
   - EC135 APH: Advanced Police Helicopter. Unified mission fit offered by McAlpine Helicopters of UK, 1997; allows simple outfitting with sensors and equipment, according to tasking, using underfuselage pod; typical equipment, including loudspeakers, searchlights, microwave downlink and multisensor turret, can be fitted externally; TV and video equipment earned internally. Pod reduces maximum speed by 9km/h.  
Click on any of the images for the larger version and extended historic info!
   
German Army 82+64 D-HDEC D-HDRC D-HDRL D-HGYN D-HHIT D-HHIT D-HHTS D-HIPT
D-HKUG D-HLDM D-HLGB D-HOEM D-HSAN D-HSOS D-HTMA D-HTMA D-HVBB
D-HVBE D-HZSD D-HZSE D-HZSG G-CEYF LN-OOH OE-XEA PH-ELP PH-EMS
         
PH-MAA PH-MMT PH-PXF PH-ULP

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  page last updated 09-07-2012 Copyright © Jack Wolbrink, Emmen, the Netherlands  
     
 

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