As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, LT SIDE, FOUND TO HAVE A CRACK SIGNALS. PERFORMED ROTO-TEST INSPECTION TO ALL CRACKS IAW NTM 51-10-39. REAMED THROUGH ALL LAYERS BY 0.4 MM IAW SRM 51-40-44. FABRICATED WASHERS IAW DWG ASNA2394E9 & EA 6- 5710-T0306333 PT1 . INSTALLED FASTENERS & WASHERS IAW SRM 51-40-21 & EA 6-5710-T0306333 PT1. MAJOR REPAIR IAW GMM 6-2-100.