Resumen
We are superseding airworthiness directive (AD) 2014-02-08 for Agusta Model A109C, A109S, A109K2, A109E, and AW109SP helicopters. AD 2014-02-08 required inspecting the lock wires securing the tail rotor (T/R) duplex bearing locking nut (locking nut) to determine whether any lock wires are missing or damaged. This AD retains some of the requirements of AD 2014-02-08 but removes the terminating action, expands the applicability, and adds a daily pilot check. This AD was prompted by reports of loosening T/R locking nuts. These actions are intended to prevent failure of the T/R and subsequent loss of control of the helicopter.
Detalles de la directiva
Número de AD
FAA-2015-1937
Número de documento
2015-13845
Tipo
Rule
Fecha de publicación
June 9, 2015
Fecha de entrada en vigor
June 24, 2015
Fabricante afectado
Agusta S.p.A. (Agusta)
Criticidad
important
Emergencia
No
Docket ID
Docket No. FAA-2015-1937
Temas
Documentos oficiales
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