Airworthiness Directive

AD 2012-18-01 Amendment 39-17177

Federal Aviation Administration · 14 CFR part 39

FR document
2012-21536
Amendment
39-17177
Published
2012-09-06
Models covered
1
Last live check
Not yet re-verified
AD

2012-18-01

FR doc 2012-21536

AD 2012-18-01Published 2012-09-06Effective 2012-09-21

Requires repetitively inspecting the left and right forward (main) and aft spar wing-to-fuselage attach fittings for cracks and replacing any cracked fitting.

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-BC (C-26A), SA227-CC, SA227-DC (C-26B), SA227-AT, and SA227-TT airplanes. This AD requires repetitively inspecting the left and right forward (main) and aft spar wing-to-fuselage attach fittings for cracks and replacing any cracked fitting. This AD also requires reporting certain inspection results to the FAA. This AD was prompted by reports of fatigue cracking in the left and right forward (main) spar wing-to-fuselage attach fittings. We are issuing this AD to correct the unsafe condition on these products.

Applies to 1 model in our index