Resumo
We are adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. Models PA-31, PA-31-300, PA-31-325, and PA-31-350 airplanes. This AD was prompted by fatigue cracking in the fuselage station (FS) 332.00 bulkhead common to the horizontal stabilizer front spar attachment. This AD requires repetitive inspections to detect cracks in the bulkhead and any necessary repairs. This AD also provides an optional modification if no cracks are found that will greatly reduce the likelihood of the specified cracks. We are issuing this AD to correct the unsafe condition on these products.
Detalhes da diretiva
Número da AD
FAA-2016-9550
Número do documento
2017-10407
Tipo
Rule
Data de publicação
May 25, 2017
Data de vigência
June 29, 2017
Fabricante afetado
Piper Aircraft, Inc.
Criticidade
routine
Emergência
Não
Docket ID
Docket No. FAA-2016-9550
Tópicos
Documentos oficiais
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