As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN CABIN, FRAME 58 BETWEEN STRINGER 13L AND 14L DENTED AND GOUGED. REMOVED DAMAGE IAW SRM 53-10-13 FIG 202. FABRICATED A REPAIR ANGLE, TREATED AND PRIMED THE REPAIR ANGLE IAW SRM 51- 21-10. INSTALLED THE REPAIR ANGLE IAW SRM 53-10-13 FIG 202 MAJOR REPAIR.