Resumen
We are publishing a new airworthiness directive (AD) for Enstrom Helicopter Corporation (Enstrom) Model F-28A, 280, F-28C, F- 28C-2, F-28C-2R, 280C, F-28F, F-28F-R, 280F, 280FX, and 480 helicopters. This AD was sent previously to all known U.S. owners and operators of these helicopters and supersedes Emergency AD (EAD) 2015- 04-51, dated February 12, 2015. This AD requires inspecting certain main rotor spindles (spindles) for cracks and reporting the inspection results to the FAA. This AD is prompted by a fatal accident and reports of spindles with cracks. The actions specified in this AD are intended to detect a crack in a spindle and prevent loss of a main rotor blade and subsequent loss of control of the helicopter.
Detalles de la directiva
Número de AD
FAA-2015-1537
Número de documento
2015-11732
Tipo
Rule
Fecha de publicación
May 18, 2015
Fecha de entrada en vigor
June 2, 2015
Fabricante afectado
The Enstrom Helicopter Corporation
Criticidad
critical
Emergencia
Sí
Docket ID
Docket No. FAA-2015-1537
Temas
Documentos oficiales
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