As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING SCHEDULED INSPECTION, THE TAIL CONE RELEASE CABLE RT UPPER SLIDER BLOCK WAS DETERMINED TO BE WORN AT BS 1510 AT THE 2 O'CLOCK POSITION. A NEW SLIDER BLOCK WAS INSTALLED IAW AMM 53-53. FUNCTIONAL CHECKS ACCOMPLISHED IAW AMDS WC 5130-01077-0101 AND THE REQUIRED INSPECTION WAS COMPLETED.