As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CABIN FLOOR PANEL 46 HAS SURFACE CORROSION ALONG ROW OD OTBD FASTENER HOLES. BLENDED CORRODED FASTENER HOLES IAW SRM 51-10-3 PG 46-47 ORIG MAT THICKNESS .020 IAW SRM 53-23-0 MAX MAT LOSS .020 OUT OF LIMITS IAW SRM 53-01. REMOVED IAW SRM 51-30-11 AND 51-30-2. REMOVED 8 EA RIVETS AND 2 HAT CHANNELS IAW SRM 51-60-0, PG 7, FIG 1 INSTALLED 2 EA HAT CHANNELS AND RIVETS IAW SRM 51-20-0, PG 10-11 AND 51-30-02, PG 2-4 AND 26B.