As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULED STRUCTURAL INSP A CRACK IN THE LT HORIZONTAL STABILIZER LOWER TEE EXTRUSION WAS DISCOVERED. REPAIRED THE CRACKED TEE EXTRUSION BY SPLICING IN A NEW SECTION OF TEE EXTRUSION IAW FR-CO-02598. 2 REPAIR ANGLES WERE FABRICATED USING A SECTION OF THE NEW TEE EXTRUSION, PN 101-620029-11.