As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON LEFT WING OUTER WING SKIN PANEL AT STATION XRS 533.3, STRINGER 62 END FITTING. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA. FABRICATION AND INSTALLATION AN REPAIR FILLER, DOUBLER AND TRIPLER IN ACCORDANCE WITH FAA DER APPROVED DRAWINGS 3759035-1, 5612385-507 AND DACO STRUCTURAL REPAIR MANUAL.