Resumen
We are adopting a new airworthiness directive (AD) for Airbus Helicopters Model AS332C, AS332C1, AS332L, and AS332L1 helicopters. This AD requires inspecting the tail rotor (T/R) flapping hinge link (hinge) and reporting the results. This AD is prompted by a report of a damaged flapping hinge link. The actions of this AD are intended to prevent an unsafe condition on these products.
Detalles de la directiva
Número de AD
FAA-2018-0177
Número de documento
2018-04647
Tipo
Rule
Fecha de publicación
March 9, 2018
Fecha de entrada en vigor
March 26, 2018
Fabricante afectado
Airbus
Criticidad
routine
Emergencia
No
Docket ID
Docket No. FAA-2018-0177
Temas
Documentos oficiales
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