Resumen
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.
Detalles de la directiva
Número de AD
FAA-2018-0866
Número de documento
2020-12592
Tipo
Rule
Fecha de publicación
June 11, 2020
Fecha de entrada en vigor
July 16, 2020
Fabricante afectado
Bell Textron Inc. (Type Certificate Previously Held by Bell Helicopter Textron Inc.)
Criticidad
routine
Emergencia
No
Docket ID
Docket No. FAA-2018-0866
Documentos oficiales
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