Resumo
We are adopting a new airworthiness directive (AD) for AHD Model EC135P1, P2, P2+, T1, T2, and T2+ helicopters. This AD requires repetitive visual inspections of the ring frame X9227 for a crack and, if there is a crack, replacing the ring frame before further flight. This AD is prompted by a fatigue crack in the ring frame. These actions are intended to detect a crack in the ring frame and prevent loss of the tail rotor and subsequent loss of control of the helicopter.
Detalhes da diretiva
Número da AD
FAA-2014-0440
Número do documento
2014-15527
Tipo
Rule
Data de publicação
July 15, 2014
Data de vigência
July 30, 2014
Fabricante afetado
Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter Deutschland GmbH Helicopters) (AHD)
Criticidade
routine
Emergência
Não
Docket ID
Docket No. FAA-2014-0440
Tópicos
Documentos oficiais
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