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#2380

Eurocopter EC135

🇩🇪 Germany ·first flew 1994· light utility helicopter

Eurocopter EC135, photo 1 of 10
1/10 Stahlkocher· CC BY-SA 3.0

what is it?

The Airbus Helicopters H135 (formerly Eurocopter EC135) is a twin-engine civil light utility helicopter produced by Airbus Helicopters. It is capable of flight under instrument flight rules and is outfitted with a digital automatic flight control system. First flying in February 1994 and developed from the prototype Messerschmitt-Bölkow-Blohm MBB Bo 108, it entered service in 1996.

How to recognise it: 2 turboshaft engines · 10.2 m main rotor

base stats

  • speed 254 km/hcruise speed
  • range 635 kmwithout refuelling
  • size 2,910 kgmax take-off weight
  • built 1,400made in total

Bars compare against all aircraft: 3,500 km/h, 20,000 km, 850 seats; size and number built on a log scale up to 640 t (An-225) and 45,000 built (Cessna 172).

fun facts

  • First flew 32 years ago, in 1994.
  • Rotor of 10.2 m: about 2 cars parked nose to tail.

turboshaft: A turbine that turns a shaft, usually a helicopter rotor.

spec sheet

first flight
1994-02-01
introduced
1996
status
still flying
number built
1,400
role
light utility helicopter
origin
🇩🇪 Germany
makers
Airbus Helicopters
engines
2× Turbomeca Arrius 2B2
crew
1
length
10.2 m
rotor diameter
10.2 m
height
3.5 m
max take-off weight
2,910 kg
top speed
—
cruise speed
254 km/h
range
635 km
ceiling
6,096 m

Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.

Sources: Wikidata Q39654, Wikipedia: Eurocopter EC135 (CC BY-SA 4.0).Updated 2026-10-24.

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