What was found
FUSELAGE INTERNAL STRUCTURE, BETWEEN FRAME 41 TO 46, FROM STRINGER 24R TO 28R, NDT CHECK FOUND ONE HOLE WITH CRACK SIGNAL AT FRAME 44, STRINGER 25R - 26R LOCATION, THE FIRST HOLE FROM UP TO DOWN. PERFORMED BUSHES INSTALLATION REPAIR IAW EA 6-5315-T0325510, PT1 EA. TITLE: FUSELAGE-FRAME FOOT-CRACKS, FRAME FEET ATTACHMENT HOLES "H1" ON FRAME 42, 43, 44, RT SIDE BETWEEN STR-25R TO STR-27R. THIS WAS CATEFORY "C" REPAIR, REPAIR LIFE LIMITATION WAS 6 MONTHS. THIS WAS A MAJOR REPAIR IAW GMM6-2-100.