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AD FAA-2016-9120

Airworthiness Directives; M7 Aerospace LLC

Resumo

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.

Detalhes da diretiva

Número da AD

FAA-2016-9120

Número do documento

2016-29242

Tipo

Rule

Data de publicação

December 8, 2016

Data de vigência

January 12, 2017

Fabricante afetado

M7 Aerospace LLC

Criticidade

routine

Emergência

Não

Docket ID

Docket No. FAA-2016-9120

Tópicos

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiais

Ver todas as ADs de M7 Aerospace LLC →

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