As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SHV - DURING C-CHECK AN EDDY CURRENT INSPECTION OF THE AFT SERVICE DOOR STOP ATTACHMENT HOLE, FRAME 22, STRINGER 7R INDICATED A CRACK INDICATION. MAINTENANCE REAMED THE HOLE TO 5.31MM IAW EA5310-01054, SUBSEQUENT EDDY CURRENT INSPECTION REVEALED NO INDICATIONS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.