What was found
CRACKED AFT INNER PAN LOCATED BETWEEN BEAMS NR 1 AND 2 AT THE CENTER CARGO DOOR. THE PAN WAS REPAIRED IAW SRM 52-05, PAR 25, FIG 26A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED AFT INNER PAN LOCATED BETWEEN BEAMS NR 1 AND 2 AT THE CENTER CARGO DOOR. THE PAN WAS REPAIRED IAW SRM 52-05, PAR 25, FIG 26A.