What was found
INSPECTION TYPE:C-3, RIGHT WING CTR L/E RIB CRACKED AT APPROX STA XFS 304 VERIFIED BY NDT. PERFORMED AFEC IAW DAC SPM NDT 06-10-001-01 TO VERIFY CRACK END AT FASTENER HOLE. MAT THICKNESS FOR RIB AT STA XFS 304 .063 7075-T6, MAT ID FOR REPAIR ANGLE 7075-T6 .080 PO 437138.5. FAB REPAIR ANGLE IAW DC8 SRM 57-2-0, ALODINED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0.