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routineRule

AD FAA-2016-2701

Airworthiness Directives; Turbomeca S.A. Turboshaft Engines

Resumen

We are adopting a new airworthiness directive (AD) for certain Turbomeca S.A. Makila 2A and 2A1 turboshaft engines. This AD requires tightening the nut attaching the swivel union to the engine power turbine module M04. This AD was prompted by two occurrences of commanded in-flight shutdown following low oil pressure warning. We are issuing this AD to prevent loosening of the nut and oil leakage from the low-pressure oil system, which could lead to in-flight shutdown of the engine and forced landing.

Detalles de la directiva

Número de AD

FAA-2016-2701

Número de documento

2016-06372

Tipo

Rule

Fecha de publicación

March 22, 2016

Fecha de entrada en vigor

April 6, 2016

Fabricante afectado

Turbomeca S.A. Turboshaft

Criticidad

routine

Emergencia

No

Docket ID

Docket No. FAA-2016-2701

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de Turbomeca S.A. Turboshaft →

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