As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE WAS STRUCK BY GROUND EQUIPMENT AT AN EXISTING REPAIR WHICH WAS INSTALLED BETWEEN FS 500 & 521 AND BETWEEN STRINGERS 33L & 39L. THE UPPER PORTION OF THE REPAIR WAS REMOVED AND THE ADDITIONAL SKIN DAMAGE REMOVED WITH AN ADDITIONAL CUTOUT. A NEW ALUMINUM SKIN DOUBLER WAS INSTALLED AND INCORPORATED INTO THE EXISTING REPAIR PER ER/A 379697-14, REV B.