As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULED MX INSPECTION, HORIZONTAL STABILIZER WAS REMOVED WHICH REVEALED DAMAGE TO THE ACFT FUSELAGE SKIN. DAMAGE APPEARS TO HAVE BEEN CAUSED BY THE L/E OF THE HORIZONTAL STABILIZER CHAFING INTO THE FUSELAGE SKIN. DAMAGED AREA RANGED FROM FS 342.24 TO 345.15 AND WL 104.38 TO 106.88. REPAIRED AS DETAILED IN AC 43.13-1B PARA 4-58.