What was found
CRACKED PAN ABOVE THE NR 1 BEAM, FWD EDGE AT MAIN ENTRANCE DOOR. THE PAN WAS REPAIRED IAW SRM 52-05, PAR 14, FIG 18A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED PAN ABOVE THE NR 1 BEAM, FWD EDGE AT MAIN ENTRANCE DOOR. THE PAN WAS REPAIRED IAW SRM 52-05, PAR 14, FIG 18A.