As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MULTIPLE DENTS TO THE LT FUSELAGE SKIN PANEL BETWEEN BS 270.50 - 291.40 AND STRINGER 11 - 12L. REPAIRED THE SKIN AND WITHIN LIMITS IAW RD 8-53-15535, INSPECTED THE REWORKED AREA FOR CRACKS AND DEBONDING INDICATIONS, NONE PERMITTED, AND PROTECTED THE AREA IAW ECO 008.53-18.05