As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DAMAGE WAS NOTED TO THE TAIL BOOM UPPER SKIN PANEL (PN: 350A23-0020.21) AS WELL AS THE YAW COMPENSATOR CHANNEL REINFORCEMENT (PN: 355A23-2000.20) IN THE FORM OF CHAFE DAMAGE. THE CHAFE DAMAGE TO THE TAIL BOOM UPPER SKIN WAS MEASURED TO BE 1.70” X 0.40” AND 0.010” DEEP. THE YAW CHANNEL REINFORCEMENT WAS CHAFED THROUGH AND WILL NEED TO BE REPLACED.