As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT HORIZONTAL STABILIZER TO FUSELAGE AT AFT ATTACH FITTING LOWER SIDE SKIN PLATE DIRECTLY BELOW THE FITTING CHAFED/KNIFE EDGED. ACFT GROUNDED. REMOVED DAMAGE AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01-1A-1, FIG 101. R & R LWR SIDE SCREW PLATE IAW SRM 51-40-02-0G-0, PARA 4B AND AMM 20-50-11-912-002.