As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CABIN FLOOR PANEL 241ADF HAS PUNCTURE DAMAGE ON TOP SURFACE; 20.25' FROM O/B EDGE AND 3' FROM AFT EDGE. / UPON EVALUATION OF PUNCTURE ON FLOOR PANEL 241ADF. FOUND IT BEYOUND LIMITS OF SRM 53-00-50-1A-1. REPAIRED I-A-W SRM 53-00-50-2R-1