Resumen
We propose to adopt a new airworthiness directive (AD) for Airbus Helicopters Model AS355E, AS355F, AS355F1, AS355F2, and AS355N helicopters. This proposed AD would require measuring a vibration level in the tail rotor (T/R) drive. This proposed AD is prompted by reports of bearing degradation. The actions of this proposed AD are intended to prevent an unsafe condition on these helicopters.
Detalles de la directiva
Número de AD
FAA-2018-0438
Número de documento
2018-10494
Tipo
Proposed Rule
Fecha de publicación
May 17, 2018
Cierre de comentarios
July 16, 2018
Fabricante afectado
Airbus
Criticidad
routine
Emergencia
No
Docket ID
Docket No. FAA-2018-0438
Temas
Documentos oficiales
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