As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ELEVATOR TAB CONTROL SYS RIGGING, MX FOUND ELEVATOR TRIM TAB CONTROL CABLES RUBBING ON FUSELAGE TAILCONE SKIN AT CUT OUT HOLES. TRIM CABLES, PULLEYS AND CABLE RUNS WERE INSPECTED AND FOUND CORRECT, NO DAMAGE OR DEFECTS. ENGINEERING WAS ADVISED AND ISSUED A RD TO DRESS THE TAILCONE SKIN AT THE TRIM CABLE EXIT HOLES SUFFICIENTLY TO ESTABLISH CLEARANCE. CAMPAIGN 851-27-30-050 WAS ISSUED.