Resumen
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.
Detalles de la directiva
Número de AD
FAA-2014-0440
Número de documento
2014-15527
Tipo
Rule
Fecha de publicación
July 15, 2014
Fecha de entrada en vigor
July 30, 2014
Fabricante afectado
Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter Deutschland GmbH Helicopters) (AHD)
Criticidad
routine
Emergencia
No
Docket ID
Docket No. FAA-2014-0440
Temas
Documentos oficiales
Seguimiento automatizado de cumplimiento de ADs
AeroCopilot asocia las ADs a su aeronave y rastrea el estado de cumplimiento. Incluido en cada plan desde $9.99 al mes.
Unlock AD-to-aircraft matching, compliance tracking, recurrence schedule with a free AeroCopilot account.
Sign up free to unlock AD-to-aircraft matching, compliance tracking, recurrence scheduleFree forever · No credit card · Sourced directly from FAA & NOAA pipelines