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AD FAA-2016-6990

Airworthiness Directives; Turbomeca S.A. Turboshaft Engines

Resumen

We are adopting a new airworthiness directive (AD) for certain Turbomeca S.A. Arriel 1, 1A, 1A1, 1A2, 1B, 1B2, 1C, 1C1, 1C2, 1D, 1D1, 1E, 1E2, 1K1, 1S, and 1S1 turboshaft engines. This AD requires removing the centrifugal impeller and replacing with a part eligible for installation. This AD was prompted by an anomaly that occurred during the grinding operation required by modification TU376, which increases the clearance between the rear curvic coupling of the centrifugal impeller and the fuel injection manifold. We are issuing this AD to prevent failure of the centrifugal impeller, uncontained centrifugal impeller release, damage to the engine, and damage to the helicopter.

Detalles de la directiva

Número de AD

FAA-2016-6990

Número de documento

2016-26184

Tipo

Rule

Fecha de publicación

November 1, 2016

Fecha de entrada en vigor

December 6, 2016

Fabricante afectado

Turbomeca S.A. Turboshaft

Criticidad

important

Emergencia

No

Docket ID

Docket No. FAA-2016-6990

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

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