As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SIDE TAIL BOOM JUNCTION FRAME (PN 350A21-4503-20) HAS CHAFING DAMAGE FROM THE CABLE RUBBING ALONG THE EDGE OF A FEEDTHROUGH HOLE IN THE UPPER PORTION OF THE FRAME. THE DAMAGE IS UP TO 0.070” DEEP, 0.100” WIDE, AND 0.500” LONG.