As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND FUSELAGE SKIN PANEL IS CHAFED AND GOUGED JUST BELOW THE LT HORIZ STAB. BLENDED DAMAGED AREA OF SKIN, PERFORMED HFEC INSPECTION OF BLEND AREA TO ENSURE NO OTHER DEFECTS EXIST. FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER IAW ASA EA 5380-01016 AND AAR EA 11314.