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AD FAA-2007-28413

Airworthiness Directives; General Electric Company Turbofan Engines

Resumen

We are superseding airworthiness directives (ADs) 90-26-01, 91-20-02, and 2009-05-02 for all General Electric Company (GE) CF6-80C2 and CF6-80E1 series turbofan engines. This AD retains the requirements of those ADs and requires removal of additional fuel manifold part numbers (P/Ns), additional repetitive inspections, replacement as required of certain fuel manifold P/Ns and tube (block) clamps, and replacement of loop clamps. This AD was prompted by a report of an under-cowl fire caused by a manifold high-pressure fuel leak, and several additional reports of fuel leaks. We are issuing this AD to prevent failure of the fuel manifold, which could lead to uncontrolled engine fire, engine damage, and damage to the airplane.

Detalles de la directiva

Número de AD

FAA-2007-28413

Número de documento

2014-24697

Tipo

Rule

Fecha de publicación

October 23, 2014

Fecha de entrada en vigor

November 28, 2014

Fabricante afectado

General Electric Company Turbofan

Criticidad

important

Emergencia

No

Docket ID

Docket No. FAA-2007-28413

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de General Electric Company Turbofan →

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