As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE INTERNAL STRUCTURE FR 54.3 L HAS A DENT APPROX 3/32 INCH DEEP AND 1.5 IN DIAM. BETWEEN STR 14-13 LT MEASURED DENT ON FR 54.3 AT STR. 13L-14L FOUND TO BE OUT OF LIMIT IAW SRM 53-16-13 . REPAIRED FR 54.3L IAW EA 6-5310-135243 INSTRUCTIONS AND SRM 53-10-12 PAR 5 AND REPAIR 202.