Resumen
We are adopting a new airworthiness directive (AD) for Airbus Helicopters Model EC225LP helicopters. This AD requires inspecting each main rotor rotating swashplate (swashplate) control rod attachment yoke (yoke). This AD is prompted by a finding that the yoke is susceptible to cracking. The actions of this AD are intended to address an unsafe condition on these products.
Detalles de la directiva
Número de AD
FAA-2018-0237
Número de documento
2018-08096
Tipo
Rule
Fecha de publicación
April 23, 2018
Fecha de entrada en vigor
May 8, 2018
Fabricante afectado
Airbus
Criticidad
routine
Emergencia
No
Docket ID
Docket No. FAA-2018-0237
Temas
Documentos oficiales
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