As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A VISUAL INSPECTION AS PER ALLEGIANT TASK IT WAS FOUND THE LOWER FUSELAGE SKIN WITH A NICK AT FR26+385MM BETWEEN STR42L AND STR43L. THE REPORTED DAMAGED AREA WAS REPAIRED I/A/W A320 SRM 53-21-11-300-076 PARAGRAPH 2A, FIGURE 001. SEE COOPESA WORK ORDER A1M146, 1-19 FOR FURTHER DETAILS.