Helicopter directory
Airbus H130 (EC130)
EASA TCDS R.008 EC 130 B4: three-blade main rotor, 'fan-in-fan' (Fenestron) ten-blade tail rotor, skid landing gear. Airbus page: Fenestron shrouded tail rotor.
EASA TCDS R.008 EC 130 B4: three-blade main rotor, 'fan-in-fan' (Fenestron) ten-blade tail rotor, skid landing gear. Airbus page: Fenestron shrouded tail rotor.
At a glance
- Maker
- Airbus Helicopters
- Country
- France / Europe
- Engines
- One Safran Arriel 2D turboshaft, dual-channel FADEC + independent backup channel
- Seats
- 1 pilot + up to 7 passengers (1+7, up to 8 on board)
- Cruise speed
- 128 (page says 'fast cruise speed', units not printed; assumed kt, NOT confirmed)
- Range
- 327 NM at MTOW
- EASA type certificate
- EASA.R.008 (AS 350 / EC 130 B4 / EC 130 T2), Issue 19
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