Helicopter directory
Airbus H135 (EC135)
EASA TCDS R.009: bearingless four-blade main rotor, Fenestron with 10 blades, skid-type landing gear.
EASA TCDS R.009: bearingless four-blade main rotor, Fenestron with 10 blades, skid-type landing gear.
At a glance
- Maker
- Airbus Helicopters (Airbus Helicopters Deutschland on TCDS)
- Country
- Germany / Europe
- Engines
- Two: Safran Arrius 2B2 Plus or Pratt & Whitney Canada PW206B3, FADEC
- Seats
- 1 or 2 pilots + 5 or 6 passengers depending on configuration
- Range
- Up to 626 km (338 NM) standard tanks
- Maximum weight
- Airbus page: 2,980 kg MTOW (3,100 kg AGW). TCDS EASA.R.009 sections show Maximum Mass 2,720 kg for earlier EC135 variants - the two sources differ because they describe different variants
- EASA type certificate
- EASA.R.009 (EC135 / EC635 family), Issue 21
Check first
Figures come from the manufacturer's own page and the EASA type certificate data sheet read on 3 November 2026. Variants differ; check the exact model.
Official links
- Manufacturer page airbus.com
- EASA type certificate data sheet easa.europa.eu
- EASA noise data easa.europa.eu
Sources and checks
Facts on this page come from these sources, last checked 2026-11-03. Where a source could not be reached or did not say, we left the fact out.
- airbus.com airbus.com
- easa.europa.eu easa.europa.eu