As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACKED PAN AT FWD CARGO DOOR BETWEEN BEAM 5 AND AFT EDGE. CRACKED ON PAN WAS STOPPED AND DRILLED IAW SRM 51-01, PAR 21. HFEC WAS ACCOMPLISHED. NO CRACKS WERE FOUND NDT SRM 06-10-01. REPAIR DOUBLER WAS FABRICATED IAW SRM 52-03, FIG 8. REPAIR DOUBLER WAS TREATED AND PAINTED IAW SRM 51-10- 3 PARS 1 AND 14. REPAIR DOUBLER WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5 AND 51-30-1.