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Military Helicopters ·Airbus Helicopters

H135M / EC365

European light utility helicopter, prominent in law enforcement, medical services, and military operations worldwide since the late 20th century.

Airbus Helicopters H135M / EC365 military helicopters side profile drawing
Side profile · Airbus Helicopters H135M / EC365 · length 12.2 m
Airbus Helicopters H135M / EC365 military helicopters in flight
Max speed
287km/h
Range
630km
Produced
1,400units
Avg unit price
$12 million
Active worldwide
193+32 on order
Technical SpecificationsVersion: EC135 T1
Length12.2 m (39.9 ft)
Wingspan10.2 m (33.5 ft)
Height3.5 m (11.5 ft)
Empty weight1,490 kg (3,285 lbs)
Max. takeoff weight2,900 kg (6,393 lbs)
Powerplant2 × turboshafts Turbomeca Arrius 2B1 519 kW each
PerformanceVersion: EC135 T1
Maximum speed287 km/h (178 mph)
Operational range630 km (391 mi)
Service ceiling6,096 m (20,000 ft)
Climb rate8.1 m/s (26.6 ft/s)
Operators — 2026
ActiveOn order
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H135M / EC365 vs
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🇦🇺 Australia· 🇧🇷 Brazil· 🇨🇦 Canada· 🇨🇭 Switzerland· 🇩🇪 Germany· 🇪🇸 Spain· 🇫🇷 France· 🇬🇦 Gabon· 🇬🇧 United Kingdom· 🇮🇪 Ireland· 🇮🇶 Iraq· 🇯🇴 Jordan· 🇯🇵 Japan· 🇲🇦 Morocco· 🇳🇬 Nigeria· 🇹🇭 Thailand

Description

The Airbus Helicopters H135 (formerly Eurocopter EC135) is a twin-engine light utility helicopter developed in Germany and produced by Airbus Helicopters. Entering service in 1996, the aircraft is used for emergency medical transport, law enforcement, offshore operations, corporate transport, and military flight training. A military derivative is designated as the H135M or EC635. By September 2020, 1,400 units had been delivered to operators across 60 countries, accumulating over 5 million flight hours.

Development

Development originated in the 1970s under Messerschmitt-Bölkow-Blohm (MBB) as the Bo 108 technology demonstrator, which first flew on 17 October 1988. Re-designated as the EC135 following the creation of Eurocopter, the design was revised to incorporate a Fenestron tail rotor and a hingeless main rotor, making its first flight in February 1994. European JAA certification was achieved in June 1996, followed by FAA approval in July 1996 and single-pilot instrument flight rules certification in December 1999. Primary assembly occurs at Donauwörth, Germany, with an additional final assembly line opened in Qingdao, China, in 2019 and a license agreement established in Yekaterinburg, Russia, in 2016.

Design

The H135 is a twin-engine rotorcraft featuring a four-bladed hingeless composite main rotor, an anti-resonance vibration isolation system, and a Fenestron shrouded tail rotor. Power is supplied by either two Turbomeca Arrius 2B or Pratt & Whitney Canada PW206B turboshaft engines, both managed by full-authority digital engine controls (FADEC). The flight deck can be configured with conventional instruments, the Thales-supplied Avionique Nouvelle glass cockpit, or the Helionix suite featuring a four-axis autopilot. The cabin is accessed via side doors or rear clamshell doors and can be outfitted for up to seven passengers, intensive care medical suites, or specialized mission equipment including electro-optical sensors, searchlights, and external cargo hooks rated up to 272 kg.

Operational History

Initial deliveries began in August 1996 to German emergency medical service provider Deutsche Rettungsflugwacht. Military operators include the German Army, which operates 19 H135 trainers at Bückeburg, the Japan Maritime Self-Defense Force with 13 TH-135 trainers, and the Royal Air Force with 29 Juno HT.1 training helicopters. The Australian Defence Force operates 15 EC135T2+ aircraft for pilot training alongside 5 H135T3 units leased from the UK Ministry of Defence in 2024, while the Iraqi Army Aviation Command operates 20 aircraft.

Variants

  • EC135 P1: Powered by two 463 kW Pratt & Whitney Canada PW206B engines, this initial production model features a maximum takeoff weight of up to 2,835 kg.

  • EC135 T1: Powered by two 435 kW Turbomeca Arrius 2B1 series engines, this initial variant shares the progressive weight upgrades of the P1.

  • H135 (EC135 T3): Powered by two 492 kW Arrius 2B2Plus engines, this variant introduces wider main rotor blades, repositioned engine air intakes, and a maximum takeoff weight of 2,980 kg.

  • EC635/H135M: Military variant designed for medical evacuation and fire support duties, operated by Jordan, Switzerland, and Iraq.

  • TH-135: Military training variant developed from the EC135 T2+ for military flight instruction.

Frequently Asked Questions

What type of aircraft is the H135M / EC365?
The Airbus Helicopters H135M / EC365 is a military helicopters aircraft developed by Airbus Helicopters and entered service in 1996.
What is the maximum speed of the H135M / EC365?
The Airbus Helicopters H135M / EC365 has a maximum speed of 287 km/h (178 mph).
What is the range of the H135M / EC365?
The Airbus Helicopters H135M / EC365 has an operational range of 630 km (391 miles). This range can vary based on payload, altitude, and mission profile.
When did the H135M / EC365 first fly?
The Airbus Helicopters H135M / EC365 made its first flight on February 15, 1994. It entered operational service in 1996.
How many H135M / EC365 have been built?
Approximately 1,400 units of the Airbus Helicopters H135M / EC365 have been produced since it entered service in 1996.
Which countries operate the H135M / EC365?
The Airbus Helicopters H135M / EC365 is operated by 15 countries with approximately 193 aircraft in active service. The largest operators include Spain, United Kingdom, and Iraq.
How much does a H135M / EC365 cost?
The Airbus Helicopters H135M / EC365 has an estimated unit cost of approximately $12.0 million. Actual prices vary based on configuration, quantity ordered, and included support packages.
What is the service ceiling of the H135M / EC365?
The Airbus Helicopters H135M / EC365 has a service ceiling of 6,096 meters (20,000 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
Wikipedia (CC BY-SA) and other open sources. Illustrations generated by AI. Last updated on 6 August 2026. Suggest a change
Latest Data Updates
  1. AUG 62026 Updated Description updated
  2. AUG 52026 Updated Powerplant updated in a site-wide editorial pass
  3. APR 72026 Updated Picture credits updated in a site-wide editorial pass
  4. FEB 72026 Updated H135M / EC365: top speed added; H135M / EC365: wingspan added
  5. JAN 122026 Updated Range updated in a site-wide editorial pass