As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK DAMAGES ON THE STRAP AND INNER CORD OD STA 2231 FRAME AT S-16L & S-17L(<P>ACCOMPLISHED THE REPAIR IAW <SPAN>EI # T2022A53M-748 REV 1 AND SRM 53-60-15-2R-2 REPAIR 2 REV 94 AND DWG #65B0500 SH 19 REV D. JOB COMPLETED AND COND CHK NORMAL.</SPAN></P>)