As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK DAMGE ON THE STRINGER S-21L, AT AFT SIDE OF STA 2180(<P>REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02 REV 33. ACCOMPLISHED EI NO T2021A53M-939 REV 1. REINSTALLED FASTENERS IAW SRM 51-40-02 REV 33 AND DWG NO 146U2200 SHEET 153 REV -. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)