Resumo
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.
Detalhes da diretiva
Número da AD
FAA-2018-0142
Número do documento
2018-07819
Tipo
Proposed Rule
Data de publicação
April 17, 2018
Encerramento dos comentários
June 1, 2018
Fabricante afetado
General Electric Company CF34-8E
Criticidade
routine
Emergência
Não
Docket ID
Docket No. FAA-2018-0142
Tópicos
Documentos oficiais
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