Eurocopter EC135

EC135
Eurocopter EC135 T2+ of the German Federal Police
Role Light utility helicopter
National origin European Union
Manufacturer Eurocopter
First flight 15 February 1994
Produced over 1000 (2011)[1]
Unit cost ~US$4.2M, €3M
Variants Eurocopter EC 635

The Eurocopter EC135 is a twin-engine civil helicopter produced by Eurocopter, widely used amongst police and ambulance services and for executive transport. It is capable of flight under instrument flight rules (IFR).

Contents

Development

The EC135 can trace its history back to before the formation of Eurocopter. It was started as the BO 108 by MBB of Germany in the mid-eighties. A technology demonstrator ('V1') flew for the first time on 17 October 1988, powered by two Allison 250-C20R/1 engines. A second BO 108 ('V2') followed on 5 June 1991, this time with two Turboméca TM319-1B Arrius engines. Both these machines had a conventional tail rotor.

In late 1992, the design was revised with the introduction of the Fenestron tail rotor system, reflecting the creation of Eurocopter that year through the merger of Messerschmitt-Bölkow-Blohm (MBB) and Aérospatiale. The combination of lower accident potential from the enclosed rotor, and interior space, have made the EC135 popular with aeromedical helicopter operators. The EC135 is the best selling light twin of the past 10 years.

Two pre-production prototypes were built. They flew on 15 February and 16 April 1994, testing the Arrius 2B and Pratt & Whitney Canada PW206B engines, the older and less powerful Allison Model 250 powerplant having been rejected. A third helicopter followed on 28 November 1994.

Operational history

The EC135 made its US debut at the Heli-Expo in January 1995 at Las Vegas. After over 1,600 flight hours, European JAA certification was achieved on 16 June 1996, with FAA approval following on 31 July. Deliveries started on 1 August, when two helicopters (0005 and 0006) were handed over to Deutsche Rettungsflugwacht. The 100th EC135 was handed over to the Bavarian police force in June 1999. By that time the worldwide fleet had accumulated approximately 30,000 flight hours. As of 2008, the fleet total stood at over 1 million flight hours, with over 650 aircraft delivered.

Single-pilot IFR (SPIFR) certification was granted by the German LBA on 2 December 1999. Deliveries to the German Aviators Corps began on 13 September 2000 at the German Army Aviators School at Bückeburg Air Base near Achum, Germany. The EC135 received SPIFR certification from the UK CAA in December 2000.

In autumn 2000, Eurocopter announced the start of certification work for the Pratt & Whitney Canada PW206B2, a version of the PW207 which offers improved single-engine performance and 30 second emergency power. The LBA certification was achieved on 10 July 2001, and the first EC135 with the new engines was handed over to the Swedish National Police on 10 August 2001.

The world fleet leader in aircraft hours for this type is G-NESV (s/n 0067) operated by Cleveland Police Air Operations Unit based at Durham Tees Valley Airport, UK. This aircraft was originally delivered to the North East Air Support Unit in April 1999, and by 2009 it had clocked up almost 12,000 hours.

At the NBAA in March 2007 in Atlanta, Eurocopter unveiled ‘L’Hélicoptère par Hermès, a special-edition VIP model designed by Hermès International, S.A.. This variant features a specially-created luxury four-place main cabin, a sliding glass partition, a corporate baggage hold, redesigned skid landing gear and other external changes. Launch customer for ‘L’Hélicoptère par Hermès is Falcon Aviation Services (FAS), based in Abu Dhabi, United Arab Emirates.

2011, Eurocopter entered the Chinese business market licensing the Zhong-Ou International Group to produce the EC135 Luxury Helicopter in the Zhejiang province.[2]

Offshore Wind Support

In March 2009 the EC135 was the first aircraft selected for offshore wind support in the UK [3] after the UK Civil Aviation Authority approved helicopter operations to the Greater Gabbard offshore wind farm.[4] The EC135 had already been used for some time in Denmark, supporting the Horns Rev offshore wind farm where over 10,000 successful personnel transfers have taken place.[5][6]

Variants

EC135 P1 
Powered by two 463 kW (621 shp) Pratt & Whitney Canada PW206B. Later versions have the Center Panel Display System (CPDS). Initial maximum take-off weight (M.T.O.W.) of 2,631 kg (5,800 lbs), later raised to 2,721 kg (6,000 lbs) and then 2,835 kg (6,250 lbs).
EC135 T1 
Powered by two 435 kW (583 shp) Turbomeca Arrius 2B1/2B1A/2B1A1. Later versions have the CPDS. Initial M.T.O.W. of 2,631 kg (5,800 lbs), later raised to 2,721 kg (6,000 lbs) and then 2,835 kg (6,250 lbs).
EC135 P2 
Powered by two 463 kW (621 shp) Pratt & Whitney Canada PW206B2. Increased thermodynamic and mechanic OEI ratings (128% OEI torque). Replaced EC135 P1 in production in August 2001.
EC135 T2 
Powered by two 452 kW (606 shp) Turbomeca Arrius 2B2. Increased thermodynamic and mechanic OEI ratings (128% OEI torque). Replaced EC135 T1 in production in August 2002.
EC135 P2+ 
Latest production version with 498 kW (667 shp) PW206B2 (new power ratings based on a FADEC software upgrade), plus a 2,910 kg (6,415 lbs) M.T.O.W. upgrade, extended component time between overhaul (TBOs), and a change in the main transmission lubricating oil.[7] Built in Germany and Spain.
EC135 T2+ 
Latest production version with 473 kW (634 shp) Arrius 2B2 engines (new power ratings based on a FADEC software upgrade), plus a 2,910 kg (6,415 lbs) M.T.O.W. upgrade, extended component TBOs, and a change in the main transmission lubricating oil. Built in Germany and Spain.
EC135 P2i 
Marketing designation of aircraft upgraded to (rather than built to) EC135 P2+ standard.
EC135 T2i 
Marketing designation of aircraft upgraded to (rather than built to) EC135 T2+ standard.
EC 635 
Military variant operated by Jordan and Swiss Air Force

Operators

The EC135 is popular with air charter companies, air ambulance operators and is operated by private individuals and companies.

Notable accidents and incidents

Specifications (EC135 P2+/T2+)

Data from {Eurocopter EC135 2008 Tech Data book}

General characteristics

Performance

See also

Related development
Aircraft of comparable role, configuration and era

Related lists

References

http://www.aaib.dft.gov.uk/publications/bulletins/september_2003/corrigendum_023918.cfm

External links

External images
Cutaway drawing of EC-135