As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK - STRINGER OF FUSELAGE STA 820 S12R(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40, DWG 142U3312 SH 8 REV C AND EI T2023A53M-2152 REV 0. 2) ACCOMPLISHED EI T2023A53M-2152 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL. 4) ORIGINAL EI ATTACHED WITH TC 8545120</P>)