Airbus H135 (EC135)
Explore the Airbus H135 (EC135) in side view and top view to compare its silhouette and proportions.
From Wikipedia
The Airbus Helicopters H135 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. 1,400 units have been delivered up to September 2020, to 300 operators in 60 countries, accumulating over 5 million flight hours. It is mainly used for air medical transport (medevac), corporate transport, law enforcement, offshore wind support, and military flight training. Half of the units in service are in Europe and a quarter in North America. The H135M is the military variant.
Summary of “Eurocopter EC135” from Wikipedia, the free encyclopedia, used under CC BY-SA 4.0. Retrieved 2026-10-11.
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Drawing of the Airbus H135 (EC135) by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/EC35/), CC BY 4.0Specifications
- Length
- 12.16 m39.9 ft
- Rotor diameter
- 10.2 m33.5 ft
- Max take-off weight
- 2.91 t6,400 lb
- Cruise speed
- 254 km/h158 mph
- Max speed
- 287 km/h178 mph
- Range
- 635 km395 mi
- Ceiling
- 6,096 m20,000 ft
- Engines
- 2× Safran Arrius 2B2 (turboshaft)
- Power
- 2× 633 hp
- First flight
- 1994
- In service
- 1996
From the AirwayControl spec register, curated from Wikipedia and manufacturer pages. Figures vary by variant.
