As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CABIN FLOOR STRAP AT 0BL STA 1016 END CORRODED. UNDER FLOOR PANEL 241AEF. / REMOVED CORROSION ON CABIN FLOOR STRAP AT 1016; BLO IAW SRM 51-10-02-0G-0 VERFIED LIMITS; ORIGINAL THICKNESS .071' ;LOSS OF .21: REMAINING .050' OUT OF LIMITS IAW SRM 53-70--51-1A-1. REMOVED AND REPLACED FLOOR STRAP IAW SRM 51-40-02-0G-0 AND BOEING DWG# 147A5600 REV-