As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN CABIN FLOOR PANEL 80 CRACKED ON EDGE. REMOVED DAMAGE ON FLOOR PANEL 1 X 2 INCHES PER ERA 490094-14 AND IAW DC9 SRM 53-01 FIG 4.NDT VERIFIED CRACK IS REMOVED IAW NDT SPM 06-10-01. FABBED REPAIR DOUBLER 3 X 2.5 INCHES & FILLER 2 X 1.5 INCHES. LOCATED AND DRILLED AND DEBURRED IAW DC9 SRM 51-10-4 & TREATED AND PRIMED IAW DC9 SRM 51-10-3 AND IAW DC9 SRM 51-30-2. INSTALLED ID TAG PER DPS 900-5-1 NO 4.