What was found
CRACKED INNER PAN ON FWD UPPER CORNER AREA AT MAIN ENTRANCE DOOR INNER STRUCTURE. THE PAN WAS REPAIRED IAW SRM 52-05 FIG. 18A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED INNER PAN ON FWD UPPER CORNER AREA AT MAIN ENTRANCE DOOR INNER STRUCTURE. THE PAN WAS REPAIRED IAW SRM 52-05 FIG. 18A.