What was found
DURING ROUTINE INSPECTION, THE FWD PASSENGER ENTRANCE DOOR WAS FOUND TO BE CRACKED ON FWD UPPER CORNER AT 2.5 INCHES IN LENGTH ON DOOR PAN. REPAIRED FWD ENTRY DOOR IAW SRM 52-05 FIG 18A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE INSPECTION, THE FWD PASSENGER ENTRANCE DOOR WAS FOUND TO BE CRACKED ON FWD UPPER CORNER AT 2.5 INCHES IN LENGTH ON DOOR PAN. REPAIRED FWD ENTRY DOOR IAW SRM 52-05 FIG 18A.