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AD FAA-2016-2701

Airworthiness Directives; Turbomeca S.A. Turboshaft Engines

Resumo

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.

Detalhes da diretiva

Número da AD

FAA-2016-2701

Número do documento

2016-06372

Tipo

Rule

Data de publicação

March 22, 2016

Data de vigência

April 6, 2016

Fabricante afetado

Turbomeca S.A. Turboshaft

Criticidade

routine

Emergência

Não

Docket ID

Docket No. FAA-2016-2701

Tópicos

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiais

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

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