Resumo
The FAA is superseding Airworthiness Directive (AD) 2011-12-08 for Bell Helicopter Textron Inc. (Bell), Model 205A, 205A-1, 205B, 212, 412, 412CF, and 412EP helicopters. AD 2011-12-08 required a one-time inspection of the tail rotor (T/R) blade for corrosion and pitting. This new AD retains the requirements of AD 2011-12-08 while excluding certain T/R blades from the applicability. This AD was prompted by new manufacturing and inspection procedures implemented by Bell that correct the unsafe condition on more recently manufactured T/R blades. The actions of this AD are intended to address an unsafe condition on these products.
Detalhes da diretiva
Número da AD
FAA-2018-0866
Número do documento
2020-12592
Tipo
Rule
Data de publicação
June 11, 2020
Data de vigência
July 16, 2020
Fabricante afetado
Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.)
Criticidade
routine
Emergência
Não
Docket ID
Docket No. FAA-2018-0866
Documentos oficiais
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