As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON INNER PAN BETWEEN BEAMS 1 AND 2 AFT EDGE AT FWD CARGO COMPARTMENT DOOR. HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM PART 6, 06-10-01.001 AND ONE CRACK WAS DELIMTED OF 2.000" LENGHT. REPARIED IAW SRM 52-30-02-2R-4. FIGURE 201.