As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND FUSELAGE SKIN DENTED AND STRINGER DAMAGED AT STA 400, STRINGER 18L. THE DAMAGED AREA OF STRINGER WAS REMOVED IAW SRM 53-10-3. THE SKIN WAS RETURNED TO ORIGINAL CONTOUR IAW SRM 51-70, FIGURE 4. REPAIR PARTS FOR STRINGER WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-2 AND 51-30-2.