As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ATL - DURING LETTER CHECK AT DALR, CORROSION WAS FOUND IN THE RIGHT WING REAR SPAR TO FUSELAGE UPPER WING ROOT TENSION FITTING BOLT HOLE. THE BOLT HOLE WAS OVESIZED TO CLEAN UP CORROSION PER DL ERA 270605-14. TT 38155 HRS. CYCLES, 18905. (X)