As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION (C53-224-01, 1) AROUND FASTENER THROUGH FLANGE OF SEAT TRACK AT BS 344 LBL 24 WL 208. REMOVED CORROSION ON UPPER SEAT TRACK FLANGE BS 344 LBL 24 WL 208 IN AN AREA 1 INCH BY .5 INCH BY .0135 INCH. ORIGINAL THICKNESS WAS .070, REMAINING MATERIAL THICKNESS IS .0565 AND WAS FOUND TO BE WITHIN LIMITS IAW FEDEX SRM 53-10-1.