As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DAMAGE TO THE ANCHOR SERVO CONTROL RH BEAM (PN: 350A23-4015.24) IN THE FORM OF A CHAFE LOCATED ON THE OUTSIDE SURFACE OF THE LOWER FLANGE BEND AT THE FWD END OF THE PART. THE CHAFE WAS MEASURED TO BE APPROXIMATELY 0.50” X 0.125” AND IS 0.014” DEEP. THERE IS ALSO CHAFING REPORTED IN THE LOWER EDGES OF 2EA OF THE PASS-THROUGH HOLES IN THE TAIL CONE JUNCTION FRAME REINFORCEMENT (PN: 350A21-1247.33). THE CHAFES WERE REPORTED TO BE 1/16” AND 1/32” DEEP INTO THE LOWER EDGES OF THE PASS-THROUGH HOLES.