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 DENTED FROM CONTACT WITH GROUND EQUIPMENT AT STRINGER 23R BETWEEN FS 654+22 & FS 654+44. THE DAMAGED SECTION OF STRINGER WAS REMOVED AND SPLICED PER THE B767 SRM. THE DAMAGE TO THE SKIN WAS REMOVED WITH A 9.8 X 1.2 CUTOUT AND A 4.3 X 1.4 CUTOUT. BOTH CUTOUTS WERE REPAIRED WITH A SINGLE ALUMINUM DOUBLER/TRIPLER REPAIR PER ER/A 377520-14, REV A.