As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT LOWER END OF INBOARD CHORD ANGLE OF FRAME RBL 65 AT TOP OF WING CENTER SECTION FRAME. INSTALLED FILLER, STIFFENING ANGLE AND TAPERED SHIM PER EA 64331 AND TR 53-62-01. (M)