As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT REAR SPAR INTERNAL ANGLE NR 35 HOLE NDT INSPECTION FOUND A CRACK SIGNAL. REAMED THE AFFECTED HOLE THROUGH ALL LAYERS IAW SRM 51-40-44, PERFORM ROTOTEST INSPECTION OF THE HOLE IAW NTM51-10-01 & NTM51-10-18 AFTER EACH STEP AND NO CRACK FOUND. WET INSTALLED A FASTENER IAW SRM 51-40-21 & EO 6-5710-7-3322 B2 PT1. MAJOR REPAIR IAW GMM 6-2-100.