Resumen
We are superseding airworthiness directive (AD) 2013-08-17 for Airbus Helicopters Model SA-365N, SA-365N1, AS-365N2, AS 365 N3, and SA-366G1 helicopters. AD 2013-08-17 required initial and recurring inspections of the 9-degree fuselage frame for a crack and repairing the frame if a crack exists. This new AD modifies the compliance times and expands the inspection area of the 9-inch frame. The actions of this AD are intended to detect a crack in the 9-degree frame to prevent loss of structural integrity and subsequent loss of control of the helicopter.
Detalles de la directiva
Número de AD
FAA-2015-3741
Número de documento
2016-10286
Tipo
Rule
Fecha de publicación
May 6, 2016
Fecha de entrada en vigor
June 10, 2016
Fabricante afectado
Airbus Helicopters (Type Certificate Previously Held by Eurocopter France)
Criticidad
routine
Emergencia
No
Docket ID
Docket No. FAA-2015-3741
Temas
Documentos oficiales
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