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AD FAA-2017-1000

Airworthiness Directives; General Electric Company Turbofan Engines

Resumo

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.

Detalhes da diretiva

Número da AD

FAA-2017-1000

Número do documento

2017-24700

Tipo

Rule

Data de publicação

November 15, 2017

Data de vigência

November 30, 2017

Fabricante afetado

General Electric Company Turbofan

Criticidade

routine

Emergência

Não

Docket ID

Docket No. FAA-2017-1000

Tópicos

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiais

Ver todas as ADs de General Electric Company Turbofan →

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