Resumen
We are adopting a new airworthiness directive (AD) for Airbus Helicopters Model AS355E, AS355F, AS355F1, AS355F2, and AS355N helicopters. This AD requires measuring a vibration level in the tail rotor (T/R) drive. This AD was prompted by reports of bearing degradation. The actions of this AD are intended to prevent an unsafe condition on these helicopters.
Detalles de la directiva
Número de AD
FAA-2018-0438
Número de documento
2018-20487
Tipo
Rule
Fecha de publicación
September 25, 2018
Fecha de entrada en vigor
October 30, 2018
Fabricante afectado
Airbus
Criticidad
routine
Emergencia
No
Docket ID
Docket No. FAA-2018-0438
Temas
Documentos oficiales
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