As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE STRUCTURE INSPECTION WAS FOUND DOUBLER DENTED LOCATED IN THE UPPER CENTER FUSELAGE I BTWN FR23+350MM / FR24+165MM BTWN S-13L/16L. DUE TO IT, THIS CONDITION WAS REPAIRED IAW SRM PART II 53-21-01 REPAIR 62 PARAG. 4 FIG. 4, 201 AND PER 51-75-12 PARAG. 5 AND PER 51-75-17 PARAG. 5 AND DOCUMENTED IN THE COOPESA JOB A1R169 ITEM 21-8.