What was found
THE FUSELAGE SKIN WAS PUNCTURED BY GROUND EQUIPMENT AT FS 1100 BETWEEN STRINGERS 19L & 20L. THE DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUMDOUBLER INSTALLED PER ER/A 380183-14, REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE FUSELAGE SKIN WAS PUNCTURED BY GROUND EQUIPMENT AT FS 1100 BETWEEN STRINGERS 19L & 20L. THE DAMAGE WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUMDOUBLER INSTALLED PER ER/A 380183-14, REV A.