Resumo
We are adopting a new airworthiness directive (AD) for Airbus Helicopters Model SA341G and SA342J helicopters. This AD requires repetitive inspections of a certain part-numbered main rotor hub torsion bar (torsion bar). This AD was prompted by several cases of corrosion in the metal strands of the torsion bar. The actions of this AD are intended to detect corrosion and prevent failure of the torsion bar, loss of a main rotor blade, and subsequent loss of control of the helicopter.
Detalhes da diretiva
Número da AD
FAA-2015-5914
Número do documento
2016-07979
Tipo
Rule
Data de publicação
April 13, 2016
Data de vigência
May 18, 2016
Fabricante afetado
Airbus Helicopters (formerly Eurocopter France)
Criticidade
important
Emergência
Não
Docket ID
Docket No. FAA-2015-5914
Tópicos
Documentos oficiais
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