AD 2018-12-03

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Safran Helicopter Engines, S.A., Turboshaft Engines

AD Number
2018-12-03
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2013-0024
FR Citation
83 FR 31325

Applicability

TypeManufacturerModelDetails
engine Safran Helicopter Airworthiness Directives; Safran Helicopter Engines, S.A., Turboshaft Engines

Unsafe Condition

The presence of coking in the fuel manifold assemblies, which can reduce fuel flow and cause engine flameouts.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Replace the main fuel injector half-manifolds and preferred injector for Arrius 2B1 turboshaft engines, and replace the preferred injector and pipe injector preferred assemblies with assembly P/N 0 319 73 044 0 for Arrius 2F turboshaft engines.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 16 months after the effective date of this AD

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Affected Aircraft

Safran Helicopter Engines, Arrius 2B1 and 2F turboshaft engines.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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