Helicopter directory
Airbus H125
EASA TCDS R.008: three-blade main rotor, two-blade conventional tail rotor, skid landing gear.
Hero image: Helicopta / Wikimedia Commons, CC BY 4.0
EASA TCDS R.008: three-blade main rotor, two-blade conventional tail rotor, skid landing gear.
At a glance
- Maker
- Airbus Helicopters
- Country
- France / Europe (TCDS holder Airbus Helicopters)
- Engines
- One Safran Arriel 2D turboshaft, 952 shp takeoff, dual-channel FADEC
- Seats
- Up to 7 occupants: 1 pilot + up to 6 passengers, or 2 pilots + up to 4 passengers
- Cruise speed
- 136 kt fast cruise at MTOW (252 km/h)
- Range
- 340 NM (630 km) at MTOW, standard fuel
- EASA type certificate
- EASA.R.008 (AS 350 / EC 130), Issue 19, 11 Dec 2025; TCDS states H125 = AS 350 B3e
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
- easa.europa.eu easa.europa.eu