As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON COMPLIANCE OF 1C-CHECK TASK 5310-122-01E, THE FUSELAGE RT FWD LOWER SKIN WAS FOUND TO BE DENTED. THE DAMAGED PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMB120 SRM 53-00-01, FIGURE 201.