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AD FAA-2020-0469

Airworthiness Directives; General Electric Company Turbofan Engines

Resumen

The FAA is adopting a new airworthiness directive (AD) for all General Electric Company (GE) GE90-110B1 and GE90-115B model turbofan engines with a certain interstage high-pressure turbine (HPT) rotor seal installed. This AD requires initial and repetitive ultrasonic inspections (USIs) of the interstage HPT rotor seal and, depending on the results of the inspection, replacement of the interstage HPT rotor seal with a part eligible for installation. This AD also requires the removal of the interstage HPT rotor seal at the next engine shop visit. This AD was prompted by investigative findings from an event involving an uncontained interstage HPT rotor seal failure that resulted in debris penetrating the fuselage and the other engine. The FAA is issuing this AD to address the unsafe condition on these products.

Detalles de la directiva

Número de AD

FAA-2020-0469

Número de documento

2020-10048

Tipo

Rule

Fecha de publicación

May 12, 2020

Fecha de entrada en vigor

May 27, 2020

Fabricante afectado

General Electric Company Turbofan

Criticidad

important

Emergencia

No

Docket ID

Docket No. FAA-2020-0469

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de General Electric Company Turbofan →

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