As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
IAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE WING TO FUSELAGE FITTING AT FRAME 27 TO HAVE A CRACK INDICATION AT BOLT HOLE NR 3 USING EDDY CURRENT INSPECTION METHOD IAW ATR-42 NDTM 53-56-03. MAINTENANCE REPAIRED THE CRACK IAW CONTINENTAL EXPERSS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5340-01034. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)