What was found
STRUCTURE ABOVE RT WING ATTACH POINT IS CRACKED AT WIRE BUNDLE ATTACH POINT. REMOVED, FABRICATED, AND INSTALLED THE STIFFENER IAW DWG A57240205, & SRM 51-40-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STRUCTURE ABOVE RT WING ATTACH POINT IS CRACKED AT WIRE BUNDLE ATTACH POINT. REMOVED, FABRICATED, AND INSTALLED THE STIFFENER IAW DWG A57240205, & SRM 51-40-21.