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
Documentos oficiales
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