AD 2014-19-05

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Turbomeca S.A. Turboshaft Engines

AD Number
2014-19-05
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2014-0164
FR Citation
79 FR 59091

Applicability

TypeManufacturerModelDetails
engine Turbomeca S Airworthiness Directives; Turbomeca S.A. Turboshaft Engines

Unsafe Condition

Reports of uncommanded in-flight shutdowns on Turbomeca S.A. Arriel 1 and Arriel 2 engines following rupture of the 41-tooth gear forming the 41/23-tooth bevel gear located in the engine accessory gearbox (AGB).

Required Actions

Perform a one-time vibration check of the AGB 41/23-tooth bevel gear meshing within 32 months of the effective date of this AD, and perform a vibration check of the AGB 41/23-tooth bevel gear meshing during each engine shop visit after the effective date of this AD. If the AGB does not pass the vibration check, replace the AGB with a part eligible for installation.

Compliance Time

Within 32 months of the effective date of this AD

Affected Aircraft

All Turbomeca S.A. Arriel 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1, 1E2, 1K1, 1S, 1S1, 2B, 2B1, 2C, 2C1, 2C2, 2S1, and 2S2 turboshaft engines.

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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