As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN CABIN FLOOR PNL 62 FASTENER HOLES ELONGATED, CHAFED AND BROKE OUT. ORIG MATERIAL THICKNESS .025 IAW SRM 53-23-0. MATERIAL LOSS MAXIMUM .009 MATERIAL REMAINING .016 IAW SRM 53-01, FIG 1. RECEIVED MATERIAL FOR WEB AND HAT CHANNEL IAW DWG 9957919. DRILLED WEB AND CHANNELS IAW SRM 51-10-2 AND 51-10-4. INSTALLED LOCATED WEB AND CHANNELS IAW DWG 9957919 & ER/A 488723-14 REV ORIGINAL. REQUIRED INSP COMPLETED BY Q948.