As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C-3, RIGHT CENTER L/E RIB CRACKED AT APPROX STA 379.000 VERIFIED BY NDT. STOP DRILL CRACK. MAT ID FOR RIB AT XFS 379 .063 7075-T6. MAT ID FOR REPAIR ANGLE 7075-T6 .080 PO 437138.5. ACCOMPLISHED HFEC INSP OF STOP DRILL IAW DAC NTSPM 06 10-01.001. FAB REPAIR ANGLE, ALODINED & PRIMED REPAIR ANGLE IAW DC8 SRM 51-1-8 AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0.