As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REJECTED: L/H H-STAB RIB #7 STIFFENER #4 UPPER RADIUS CRACKED: SRM APPLICABILITY VALIDATION FOR REPAIR; AND NDT/VISUAL INSPECTIONS NOT PERFORMED AFTER DAMAGE REMOVAL.<[01] L/H H-STAB RIB #7 STIFFENER #4 UPPER RADIUS CRACKED: ACCOMPLISHED ON COSTUMER CARD TTG8Q00MP7C6:<BR>-SRM APPLICABILITY ON STEP 4.<BR>-NDT PERFORMED ON STEP 3.<BR>-GVI PERFORMED ON STEP 8.;[02] VERIFIED CORRECTIVE ACTION 1