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routineProposed Rule

AD FAA-2018-0142

Airworthiness Directives; General Electric Company CF34-8E Engines

Resumen

We propose to adopt a new airworthiness directive (AD) for all General Electric Company (GE) CF34-8E turbofan engines. This proposed AD was prompted by a report from GE regarding a quality escape of nonconforming thrust reverser fire seals. This proposed AD would require a one-time inspection of the gap between the core cowl seal and the pylon seal of the thrust reverser for correct gap width, and replacement of the seals, if needed. We are proposing this AD to address the unsafe condition on these products.

Detalles de la directiva

Número de AD

FAA-2018-0142

Número de documento

2018-07819

Tipo

Proposed Rule

Fecha de publicación

April 17, 2018

Cierre de comentarios

June 1, 2018

Fabricante afectado

General Electric Company CF34-8E

Criticidad

routine

Emergencia

No

Docket ID

Docket No. FAA-2018-0142

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de General Electric Company CF34-8E →

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