As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C, CRACK FOUND APPROX 0.2" LENGTH DURING HFEC INSPECTION ON RT STA 903.5 BL 89 BELOW WL 200 AT FRAME INNER CHORD TRANSITION RADIUS. FRAME INNER CHORD TRANSITION RADIUS AT STA 903 RBL 89 CARRIED OUT REPAIR AS PER EO B767-5310-68072-A APPENDIX B.