As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LWR FWD CARGO CEILING FRAME 25 FLOORBEAM FWD SIDE 27" RT OF CTRLINE THE VERTICAL STIFFENER IS CRACKED AT THE TOP (APPROX. LENGTH IS 1/4IN) BLENDED CRACK AT FRME 25 IAW SRM 51-73-10. NDT VERIFIED REMOVAL OF CRACK. FABRICATED REPAIR ANGLE AND REPAIRED CROSSBEAM AT FR 25 AND 27" RT OF CTRLINE IAW SRM 53-10-15 FIG 203, SHEET 1.