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AD FAA-2017-1000

Airworthiness Directives; General Electric Company Turbofan Engines

Resumen

We are adopting a new airworthiness directive (AD) for certain General Electric Company (GE) CF34-8C1, CF34-8C5, CF34-8C5A1, and CF34- 8C5B1 engines. This AD requires an inspection of the bleed air manifold link rod assemblies and the supply, return, and drain fuel fittings on the operability bleed valve (OBV). This AD was prompted by an engine fire that occurred as a result of malfunctions related to the OBV. We are issuing this AD to address the unsafe condition on these products.

Detalles de la directiva

Número de AD

FAA-2017-1000

Número de documento

2017-24700

Tipo

Rule

Fecha de publicación

November 15, 2017

Fecha de entrada en vigor

November 30, 2017

Fabricante afectado

General Electric Company Turbofan

Criticidad

routine

Emergencia

No

Docket ID

Docket No. FAA-2017-1000

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de General Electric Company Turbofan →

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