What was found
WORN RT CABLE CLAMP OF TAIL CONE RELEASE SYSTEM ALSO RUSTED HARDWARE ON PULLEY AT 11 HRS POSITION. THE CABLE CLAMP WAS REPLACED IAW AMM 53-52-01 AND HARDWARE ON PULLEY WAS REPLACED IAW AMM 20-00-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WORN RT CABLE CLAMP OF TAIL CONE RELEASE SYSTEM ALSO RUSTED HARDWARE ON PULLEY AT 11 HRS POSITION. THE CABLE CLAMP WAS REPLACED IAW AMM 53-52-01 AND HARDWARE ON PULLEY WAS REPLACED IAW AMM 20-00-02.