As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C, CARGO COMPARTMENT FLOOR PANEL ASSEMBLY UPPER SKIN AND CORE DAMAGE ABOUT 9"X0.6"0.01" AT STA 1197+89 LBL 4.7 AND RBL 4.7 CUT OUT THE UPPER SKIN AND CORE LXW=1.6"X9.4". REPAIR IAW REV:52 SRM 53-00-50. REPAIR GENERAL FIG 201, PARA 4.D.