As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE: CM. BS 2231 S25L, ONE HOLE WAS FOUND CRACKED AT FRAME INNER ANGLE, CRACK RUNNING FORWARD 0.060" LONG APPROXIMATELY. REPAIRED IAW SRM 53-60-15-2R-2, FIG 201, REV 71 ORIGINAL MATERIAL 65B01849-7 WITH CRACK LENGTH 0.060" RUNNING FWD. FINAL TRIM OUT: 1.875" X 0.875" & 0.875" X 1" RESP. IT IS A CATEGORY B REPAIR.