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AD FAA-2015-5914

Airworthiness Directives; Airbus Helicopters (formerly Eurocopter France)

Resumen

We are adopting a new airworthiness directive (AD) for Airbus Helicopters Model SA341G and SA342J helicopters. This AD requires repetitive inspections of a certain part-numbered main rotor hub torsion bar (torsion bar). This AD was prompted by several cases of corrosion in the metal strands of the torsion bar. The actions of this AD are intended to detect corrosion and prevent failure of the torsion bar, loss of a main rotor blade, and subsequent loss of control of the helicopter.

Detalles de la directiva

Número de AD

FAA-2015-5914

Número de documento

2016-07979

Tipo

Rule

Fecha de publicación

April 13, 2016

Fecha de entrada en vigor

May 18, 2016

Fabricante afectado

Airbus Helicopters (formerly Eurocopter France)

Criticidad

important

Emergencia

No

Docket ID

Docket No. FAA-2015-5914

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de Airbus Helicopters (formerly Eurocopter France) →

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