Resumo
We are superseding Airworthiness Directive (AD) 2013-24-17 for General Electric Company (GE) GE90-110B1 and GE90-115B turbofan engines with certain high-pressure compressor (HPC) rotor stage 2-5 spools installed. AD 2013-24-17 required removing these spools from service at times determined by a drawdown plan. This AD retains the same requirements as AD 2013-24-17. This AD also adds additional part number (P/N) HPC spools to the applicability. This AD was prompted by reports of cracking on these additional spools. We are issuing this AD to correct the unsafe condition on these products.
Detalhes da diretiva
Número da AD
FAA-2013-0879
Número do documento
2017-06715
Tipo
Rule
Data de publicação
April 6, 2017
Data de vigência
April 21, 2017
Fabricante afetado
General Electric Company Turbofan
Criticidade
routine
Emergência
Não
Docket ID
Docket No. FAA-2013-0879
Tópicos
Documentos oficiais
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