PRODUCT PROFILE
Arriel 2
TURBOSHAFT PROPULSION SYSTEMS
Arriel 2
France · verified
- COUNTRY
- France
- PROGRAMME STATUS
- verified
Specifications
- Function
- Provides primary turboshaft propulsion for light and medium-class rotary-wing aircraft.
- Platform fit
- Integrated into airframes including the Airbus H125, Leonardo AW109 Trekker, and Harbin Z-9.
- Commercial model
- Sold via direct engine procurement, long-term support contracts, and licensed manufacturing agreements.
- Deployment status
- In active global production and service across civil, parapublic, and military fleets.
- Evidence to demand
- High market penetration is evidenced by thousands of units delivered to diverse international operators.
Description
The Arriel 2 is a modular turboshaft engine produced by Safran Helicopter Engines [Safran Helicopter Engines], serving as the advanced successor to the original Arriel series. It is characterised by a design featuring a single-stage centrifugal compressor and the integration of dual-channel Full Authority Digital Engine Control. The modular architecture is specifically intended to facilitate field-level component replacement, thereby increasing operational availability and simplifying maintenance procedures for civil and military users. This engine family is widely adopted as the primary power plant for light and medium-sized rotorcraft in the utility, emergency services, and corporate sectors. Key platforms include the H125 and H130 by Airbus Helicopters [Airbus Helicopters], and the AW109 Trekker by Leonardo [Leonardo]. In the Chinese aerospace sector, the engine is integrated into aircraft produced by the Harbin Aircraft Industry Group [哈尔滨飞机工业集团], including the Z-9 [直-9] and H425 [哈飞H425] series, often produced under local licence. Prospective buyers must note that service intervals and total time between overhaul figures differ between the various sub-variants of the 2-series. The desk would verify specific life-cycle costs for a given model and confirm the geographical proximity of authorised service centres. Furthermore, documentation regarding the current certification status for Sustainable Aviation Fuel blends should be validated against specific operator requirements and regional environmental mandates.
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SOURCE CITATION
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