As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TWO DAMAGED AREAS TO FUSELAGE SKIN AFT OF L1 DOOR AT FR21L AND BETWEEN STR 14L AND 15L. FIRST DAMAGE IS A PUNCTURE 16CM LONG WITH A DENT 24CM L X 17CM H X 1.5CM D. SECOND DAMAGE IS A GOUGE 3MM L X 7MM W X 3MM D, REFERENCE CP2180429-1. FILED CLOSED. COMPLIED WITH MAJOR REPAIR TO LT FWD FUSELAGE BETWEEN FR 21 AND FR22 BETWEEN STRINGERS 14L AND 15L PER EMBRAER ETD.