What was found
DURING THE C-CHECK INSPECTION, THE VERTICAL STAB TO FUSELAGE ATTACH ANGLE WAS FOUND CORRODED AND CRACKED ON THE LT FROM FORWARD OF THE FRONT SPAR TO CENTER SPAR. A REPAIR WAS PERFORMED PER ATI E.O. 53-DC8-223, AND DRAWING SKA95253-5, REV: A, DATED 1-23-96. THIS REPAIR WAS APPROVED ON FAA FORM 8110-3. (X)