As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING ROUTINE POST FLIGHT INSPECTION, A 6 INCH CRACK WAS NOTED, ALONG WHEEL FLANGE AT TIRE BEAD ATTACHMENT. ON DISASSEMBLE INSPECTION THE CRACK EXTENDING TO 7.51INCH ON THE INSIDE OF WHEEL FLANGE. NO VISIBLE DAMAGE NOTED ON INNER WHEEL HALF MATE. BUT WAS REMOVED AND SENT FOR NDI INSPECITON.