As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN CABIN METAL FLOOR PANEL NR 78, 1EA END HAS CORROSION AND 1EA PUNCTURED HOLE PARTS, RACK 22B BLENDED LIGHT CORROSION BY HAND ORIGINAL IS .025 NO METAL LOST IAW SRM 51-10-3. REMOVED PUNCTURED AREA IAW SRM 51-10-4. NDT VERIFIED CRACK IS REMOVED IAW NDT SPM 06-10-01.001. FABBED REPAIR DOUBLER IAW SRM 53-01, FIG 2 LOCATED, DRILLED AND DEBURRED IAW SRM 51-10-4. INSTALLED IAW SRM 51-20-2. REQUIRED INSP COMPLETED.