What was found
CRACK ON INNER PAN BETWEEN THE NR 1 BEAM AND FWD UPPER CORNER AT L1 DOOR. THE PAN WAS REPAIRED IAW SRM 52-10-02-2R-3 FIG.201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON INNER PAN BETWEEN THE NR 1 BEAM AND FWD UPPER CORNER AT L1 DOOR. THE PAN WAS REPAIRED IAW SRM 52-10-02-2R-3 FIG.201.