As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON FLOORBEAM BS 947 LBL 24 WL 208. REMOVED CORROSION ON FLOOR BEAM UPPER FLANGE BS947 LBL24 WL208 1"X1" AREA ORIGINAL MATERIAL THICKNESS IS 0.150" LOWEST MATERIAL THICKNESS IS 0.120" DAMAGE FOUND TO BE OUT LIMITS BS947 UPPER T-CHORD TO BE REPAIRED ALONG THE FULL UPPER FLANGE I.A.W SRM 53-70-51-2R-REPAIR 5 PAR 2.B ALTERNATIVE 1. ALL REPAIR TO BE PERFORM AND RECORDED ON CCN TTG8Q01DE4K3.