Resumo
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.
Detalhes da diretiva
Número da AD
FAA-2018-0438
Número do documento
2018-10494
Tipo
Proposed Rule
Data de publicação
May 17, 2018
Encerramento dos comentários
July 16, 2018
Fabricante afetado
Airbus
Criticidade
routine
Emergência
Não
Docket ID
Docket No. FAA-2018-0438
Tópicos
Documentos oficiais
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