What was found
DURING D-CHECK, RIB INSIDE RIGHT WING HAS 5 INCH CRACK AS SEEN THROUGH ACCESS HOLE NR 8811. REMOVED FASTENERS AND OPENED LOWER SKIN FOR ACCESS PER SRM 51-30-2. STOP DRILLED AT END OF CRACKS PER SRM 51-10-1. FABRICATED ANGLE REPAIR 2024-T3 .063 12 INCH BY 1 INCH BY 1.5 INCH. INSTALLED REPAIR AS PER SRM 51-40-2. REINSTALLED FASTENERS AT LOWER SKIN PER SRM 51-30-2.