AD 2018-07-17

final rule
Data completeness: 70%

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

AD Number
2018-07-17
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2018-0184
FR Citation
83 FR 15731

Applicability

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

Unsafe Condition

During an ARRIUS 2B2 engine ground run check, the ``Degrade'' indicator illuminated and unusual vibration occurred. At the same time, bluish smoke and debris came out of the exhaust pipe. Both engines were shut down without further occurrences. Investigations at Safran Helicopter Engines revealed that missing dampers on the PTW assembly caused rupture of PTW blades. Further investigations identified a batch of potentially affected PTW.

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

Required Actions

Inspecting the power turbine wheel (PTW) assembly and replacing the PTW if the turbine blade dampers are found missing.

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

Compliance Time

Within 20 flight hours or 30 days

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Affected Aircraft

Safran Helicopter Engines, Arrius 2B1, 2B1A, 2B2, and 2K1 turboshaft engines.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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