As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING INVESTIGATION OF ELEVATOR TRIM TAB CLEVIS , BUSHINGS P/N 50-524024-1 AND P/N 90-610010-5 FOUND LIGHTLY CORRODED AND PARTIALY SEIZED . BOLT AND NUTWERE FOUND INSTALLED CORRECTLY WITH THE CORRECT TORQUE. NEW BUSHINGS AND BOLTS ON ORDER. A/C GROUNDED