Airworthiness Directive

AD 2016-25-12 Amendment 39-18738

Federal Aviation Administration · 14 CFR part 39

FR document
2016-29242
Amendment
39-18738
Published
2016-12-08
Models covered
1
Last live check
Not yet re-verified
AD

2016-25-12

FR doc 2016-29242

AD 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.

Applies to 1 model in our index