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Eurocopter EC135 / Airbus H135 Light-Twin Helicopter Family

The Airbus H135 is a light twin-engine helicopter family that first flew as the Eurocopter EC135 in 1994. Its bearingless main rotor, shrouded Fenestron tail rotor, compact footprint, and alternative twin-turboshaft installations support emergency medical, utility, law-enforcement, corporate, offshore, and military-training missions. The EC135 and H135 names describe the same continuously developed family.

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Identity

Aliases
Eurocopter EC135EC135Airbus EC135H135EC635H135MJuno HT1CT-153 Juno
Family Name
Airbus H135
Full Name
Eurocopter EC135 / Airbus H135 Light-Twin Helicopter Family
Roles
businessutilitytrainermilitaryair_ambulance
Status
active
Type
aircraft

Details

Aircraft Specs
Configuration
rotorcraft
Operating Modes
land
Takeoff Landing Capabilities
vtol
Description
The Airbus H135 is a light twin-engine helicopter family that first flew as the Eurocopter EC135 in 1994. Its bearingless main rotor, shrouded Fenestron tail rotor, compact footprint, and alternative twin-turboshaft installations support emergency medical, utility, law-enforcement, corporate, offshore, and military-training missions. The EC135 and H135 names describe the same continuously developed family.
First Flight Year
1,994
Manufacturer
Propulsion Configurations
  • Entries
    • Count
      2
      Placement
      fuselage
      Propulsion System
      Role
      main
      Stage
      airframe
      Variant Notes
      Two exact Safran Arrius 2B2 turboshaft engines; the current uprated H135 application is marketed as Arrius 2B2Plus.
    Name
    H135 / EC135 T3 — Arrius option
    Notes
    Applies to the current T3 branch. Earlier T1 and T2 family members are intentionally outside this configuration.
  • Entries
    • Count
      2
      Placement
      fuselage
      Propulsion System
      Role
      main
      Stage
      airframe
      Variant Notes
      Two exact Pratt & Whitney Canada PW206B3 turboshaft engines.
    Name
    H135 / EC135 P3 — PW206B3 option
    Notes
    Applies to the current P3 branch. Earlier P1 and P2 family members are intentionally outside this configuration.
  • Entries
    • Count
      2
      Placement
      fuselage
      Propulsion System
      Role
      main
      Stage
      airframe
      Variant Notes
      Two exact Pratt & Whitney Canada PW206B2 turboshaft engines on the H135/EC135 P2 branch.
    Name
    H135 / EC135 P2 — PW206B2 option
    Notes
    Pratt & Whitney identifies PW206B2 on Airbus H135; this exact option is scoped to the H135/EC135 P2 branch and does not infer P1 or P3.
  • Entries
    • Count
      2
      Placement
      fuselage
      Propulsion System
      Role
      main
      Stage
      airframe
      Variant Notes
      Two exact Pratt & Whitney Canada PW206B turboshaft engines on the EC135 P1 branch.
    Name
    H135 / EC135 P1 — PW206B option
    Notes
    Pratt & Whitney identifies PW206B on Airbus EC135P1; this exact option is scoped to the H135/EC135 P1 branch and does not infer P2 or P3.

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Creation Time
July 29, 2026 at 23:39:48 UTC
Updated Time
August 13, 2026 at 12:54:33 UTC