As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT FUSELAGE SKIN AT BS 198 ABOVE S-25 +2.0" WAS DENTED. THE DENT IS 3.65" LONG AND 2.5" WIDE AND DEPTH IS 0.065". REPAIRED THE DAMAGED SKIN BETWEEN BS 188 - 203.8, S21L-25L IAW ESR-WI 2024183-19-14589, & EC/RA 5310-08787. PERFORM AN INSPECTION OF THE FUSELAGE SKIN EXTERNAL REPAIR BETWEEN BS 188 - 203.8, STR 21L - 25L IAW PART 2 OF THE LATEST REVISION OF ECRA 5310-08787.