As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN WAS TORN AND GOUGED BY GROUND EQUIPMENT BETWEEN FS 654 + 44 AND FS 654 + 66 AND BETWEEN STRINGERS 34R AND 35R. THE DAMAGED SKIN WAS REMOVED WITH A 10 X 20 CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 367677-14.