As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING MAINTENANCE INSPECTION, THE LT FUSELAGE SKIN AFT OF THE PAX DOOR BETWEEN STRINGERS 13 & 14L AND FRAMES 21-22 FOUND TO BE GOUGED BEYOND LIMITS. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A FILLER-DOUBLER REPAIR IAW SRM 53-21-01, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.