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AD FAA-2018-0216

Airworthiness Directives; Honeywell International Inc. Turboprop Engines

Resumen

We are superseding Airworthiness Directive (AD) 88-12-10 for certain Honeywell International Inc. (Honeywell) TPE331 turboprop engines. AD 88-12-10 required reducing the life limit for certain second stage turbine rotors. This AD requires removing certain second stage turbine rotors from service at a reduced life limit. This AD was prompted by report that a TPE331-11U engine experienced an uncontained rotor separation. In addition, cracks were discovered through eddy current inspection (ECI) in the bore of the second stage turbine rotor assembly after publication of AD 88-12-10. We are issuing this AD to address the unsafe condition on these products.

Detalles de la directiva

Número de AD

FAA-2018-0216

Número de documento

2018-23775

Tipo

Rule

Fecha de publicación

November 5, 2018

Fecha de entrada en vigor

December 10, 2018

Fabricante afectado

Honeywell International Inc. Turboprop

Criticidad

routine

Emergencia

No

Docket ID

Docket No. FAA-2018-0216

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de Honeywell International Inc. Turboprop →

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