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AD FAA-2012-1288

Airworthiness Directives; General Electric Company Turbofan Engines

Resumen

We are adopting a new airworthiness directive (AD) for General Electric Company (GE) CF34-8C and CF34-8E turbofan engines with certain part numbers (P/N) of operability bleed valves (OBV) installed. This AD was prompted by three failure events of ring lock fuel fittings on the OBV. Two of those events led to an engine fire. This AD requires the affected OBVs be removed from service and replaced with OBVs eligible for installation. We are issuing this AD to prevent failure of OBV ring lock fuel fittings, engine fuel leakage, uncontrolled fire, and damage to the airplane.

Detalles de la directiva

Número de AD

FAA-2012-1288

Número de documento

2013-07510

Tipo

Rule

Fecha de publicación

April 3, 2013

Fecha de entrada en vigor

May 8, 2013

Fabricante afectado

General Electric Company Turbofan

Criticidad

important

Emergencia

No

Docket ID

Docket No. FAA-2012-1288

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de General Electric Company Turbofan →

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