Helicopter directory
Leonardo AW139
EASA TCDS R.006: five-blade fully articulated main rotor, four-blade tail rotor, tricycle retractable landing gear.
EASA TCDS R.006: five-blade fully articulated main rotor, four-blade tail rotor, tricycle retractable landing gear.
At a glance
- Maker
- Leonardo Helicopters
- Country
- Italy
- Engines
- Two Pratt & Whitney PT6C-67C turboshafts, FADEC
- Seats
- Crew 1-2, up to 15 passengers
- Cruise speed
- 165 kt (306 km/h) max cruise at 5,000 ft, ISA, MGW, MCP
- Range
- 641 NM (1,187 km) max at 5,000 ft, ISA, MGW with auxiliary tank, no reserve
- Maximum weight
- 6,400 kg (14,110 lb); increased gross weight 6,800/7,000 kg. TCDS R.006: Maximum Take-Off Mass 6,400 kg - agrees
- EASA type certificate
- EASA.R.006 (AB139 / AW139), Issue 27, 24 Jun 2026
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 helicopters.leonardo.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.
- helicopters.leonardo.com helicopters.leonardo.com
- easa.europa.eu easa.europa.eu