As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ACCOMPLISHMENT OF THE ALLEGIANT WORK CARD ZL325-01-1-001, EMPENNAGE VERTICAL STABILIZER TRAILING EDGE CORROSION WAS FOUND COMMON TO ATTACHMENT HOLES AT THE TRAILING EDGE PANEL ATTACHMENT FLANGES OF THE HINGE ARM 6 LH /RH SIDE. PERFORMED REPAIR AT VERTICAL STABILIZER TAIL HINGE ARM BR 6 LH AND RH FLANGE AND ATTACHMENT HOLES IAW EO # COO-EO-2024-20707-R01 AND AIRBUS RDAF 81450182/004/2024 ISSUE A.APPROVED UNDER ERO R5536-0059-R00,THIS IS MAJOR TEMPORARY REPAIR.