As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
R1 DOOR LWR AFT CORNER HAS 1.5 INCH CRACK TWO CRACKS FROM DOOR CUTOUT .75 INCH LC RUNNING TO BOLT HOLE. ANOTHER .75 INCH LONG CRACK EMANATES FROM THE OPPOSITE SIDE OF THE SAME BOLT HOLE EXTERNAL SKIN. REPAIRED AFT LOWER DOOR CORNER AT R1 DOOR IAW SRM 53-10-01 FIG 201.