As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION, THE RIGHT ELEVATOR LEADING EDGE SKIN WAS FOUND TO BE CRACKED AT THE SERVO TAB CONTROL ROD AT STA YH 1310. A HIGH FREQUENCY EDDY CURRENT INSPECTION WAS CARRIED OUT WITH NO CRACK LIKE INDICATIONS FOUND. THE RIGHT ELEVATOR LEADING EDGE SKIN AT THE SERVO TAB CONTROL ROD HINGES WAS REPAIRED IN ACCORDANCE WITH SRM 5520-01 AND SRM 51-40-02.