As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C M/D LT BS2231 FRAME INNER CHORD S24L-25L FOUND 1 HOLE CRACK AT FRAME STRAP RUNNING FWD APPROX 1/8". M/D BS2231 FRAME ATTACH INNER CHORD AND STRAP REPAIRED BTN STR22L TO 26L AREA AS PER SRM 53-10-04 FIG 115. CONTINUE INSPECTION ARE REQ AS PER SRM 53-10-04 FIG 115. REFER NRC51556 FOR WORKING DETAIL. (UPS MPI#P19306 RAISED FOR CONTINUE INSPECTION)