Summary
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.
Directive Details
AD Number
FAA-2016-9120
Document Number
2016-29242
Type
Rule
Publication Date
December 8, 2016
Effective Date
January 12, 2017
Affected Manufacturer
M7 Aerospace LLC
Criticality
routine
Emergency
No
Docket ID
Docket No. FAA-2016-9120
Topics
Official Documents
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