As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PRESSURE FLOOR TENSION STRAP SMALL AREA OF CORROSION ON UPPER SURFACE FS 559.00 BETWEEN BL 0.0 AND LBL9.0. BLENDED CORROSION ON PRESSURE FLOOR STRAP AT FS599.0 BETWEEN BL0.0 TO LBL9.0 IAW SRM ORIGINAL THICKNESS .063" REMOVED .005" LEAVING .058".