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Turbomeca Arriel

turboshaft helicopter engine family

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General referenceInterpretive dossier study · Crown Archives visual atlas
Record originEnglish Wikipedia
Text licenseCC BY-SA 4.0
Source revisionApr 18, 2026
Entity authorityQ431316 ↗
Source-derived summary

The Turbomeca Arriel is a series of French turboshaft engines that first ran in 1974.

Delivering 650 to 1,000 hp (480 to 750 kW), over 12,000 Arriel engines have been produced from 1978 to 2018, logging more than 50 million flight hours for 40 helicopter applications.

In June 2018, 1,000 Arriel 2D were in service, powering H125 and H130 single-engine helicopters, having logged one million flight hours since 2011.

After endurance tests and fleet data analysis, their TBO increased by 25% to 5,000 hours and mandatory inspection rose to 15 years with no hourly limit, lowering maintenance costs.

In 2021 Safran opened a production facility in Grand Prairie, Texas for production of Arriel 2E engines, which had previously only been produced in France.

Applications

AgustaWestland AW109

Eurocopter AS365 Dauphin

Eurocopter AS565 Panther

Eurocopter MH-65 Dolphin

Eurocopter EC130

Eurocopter EC145

Eurocopter EC155

Eurocopter AS350 Écureuil

Harbin Z-9

Harbin Z-19

Kopter AW09

MBB/Kawasaki BK 117

Robinson R88

Sikorsky S-76

Specifications (Arriel 2)

Data from EASA Type Certificate Data Sheet for Model 2B.

General characteristics

Type: Turboshaft engine

Length: 1.181 m (3 ft 10.5 in)

Diameter: 0.616 m (2 ft 0.3 in)

Dry weight: 134 kg (295 lb)

Components

Compressor: Single-stage axial plus single-stage centrifugal

Combustors: Annular combustion chamber

Turbine: Single-stage power turbine, two-stage gas generator turbine

Fuel type: Jet A1

Performance

Maximum power output: 747 shp (557 kW)

Overall pressure ratio: 8:1

Turbine inlet temperature: 915 °C (1,679 °F)

Power-to-weight ratio: 4.2 kilowatts per kilogram (2.6 hp/lb) approx

See also

Related lists

List of aircraft engines

References

Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. p. 166.

Editorial summary

“Turbomeca Arriel” enters the record as turboshaft helicopter engine family. Crown Archives preserves that source wording while asking what Turbomeca, Arriel and turboshaft can confirm, complicate or overturn.

Editorial reviewA concise reference frame for defining the subject, testing terminology and identifying the institution closest to the evidence. The current lead gives the account dated anchors—1974, 1978, 2018, 2011—that can be checked directly. The selected authority fields contribute no independent date. Its strongest next move is a source search built around Turbomeca, Arriel and turboshaft.
Editorial analysis

Why this record matters

“Turbomeca Arriel” is worth following because a concise public description often conceals a longer documentary argument. Here, Turbomeca, Arriel and turboshaft provides the most credible route into that argument.

Evidence profile

Named sources, stable identifiers and responsible institutions provide the strongest route from overview to verifiable evidence. The source revision retrieved here is dated Apr 18, 2026. The linked authority identifier is Q431316. None of the 0 selected statements returned an explicit reference. The first chronological checks are 1974, 1978, 2018 and 2011.

Critical limits

Overview language is designed for orientation and should not be treated as a substitute for the evidence cited beneath it. The lead is largely declarative, so disagreement and counter-evidence require a deliberate search beyond the opening account. Authority statements aid reconciliation but still require their own references, qualifiers and ranks to be checked.

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Source & attribution

This entry incorporates text from “Turbomeca Arriel” on English Wikipedia. Contributors are listed in the page history. Text is available under the Creative Commons Attribution-ShareAlike 4.0 License. Selected authority identifiers and statements are retrieved from Wikidata under CC0; their references and qualifiers remain part of the verification path.