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AD FAA-2015-1537

Airworthiness Directives; The Enstrom Helicopter Corporation

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

Docket ID

Docket No. FAA-2015-1537

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de The Enstrom Helicopter Corporation →

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