Resumen
We are adopting a new airworthiness directive (AD) for all M7 Aerospace LLC Models SA226-AT, SA226-T, SA226-T(B), SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, SA227-DC (C-26B), and SA227-TT airplanes. This AD was prompted by corrosion and stress corrosion cracking of the pitch trim actuator upper attach fittings of the horizontal stabilizer front spar. This AD requires repetitive inspections with replacement of fittings as necessary. We are issuing this AD to correct the unsafe condition on these products.
Detalles de la directiva
Número de AD
FAA-2016-9120
Número de documento
2016-29242
Tipo
Rule
Fecha de publicación
December 8, 2016
Fecha de entrada en vigor
January 12, 2017
Fabricante afectado
M7 Aerospace LLC
Criticidad
routine
Emergencia
No
Docket ID
Docket No. FAA-2016-9120
Temas
Documentos oficiales
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