What was found
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 218 BELOW LONGERON 16L AFT OF MAIN CABIN DOOR. THE DENT WAS COLD WORKED AND A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 22.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 218 BELOW LONGERON 16L AFT OF MAIN CABIN DOOR. THE DENT WAS COLD WORKED AND A REPAIR WAS INSTALLED IAW SRM 53-04, FIGURE 38, SHEET 22.