2016-25-12
FR doc 2016-29242 · 81 FR 88621AD 2016-25-12Published 2016-12-08Effective 2017-01-12
Requires repetitive inspections with replacement of fittings as necessary.
Full official abstract
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.
More directives for Fairchild SA226/SA227 Metro
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