What was found
A .75 INCH CRACK FOUND IN STIFFENER AT FS 598 RT SIDE OF FUSELAGE AT FORWARD SECTION OF WING TO FUSELAGE FILLET INTERIOR. REMOVED FILLET AND SKATE ANGLE. FABRICATED AND INSTALLED REPAIR FILLET, INSTALLED NEW SKATE ANGLE IAW DC9 SRM 51-30-2, 51-10-2, 51-10-4, 51-10-2A, 51-30-5 AND RES 981686.