As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
1) CRACK - STRINGER OF FUSELAGE STA 820 S12L(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40 AND DWG 142U3312 SH 8 REV C AND EI T2023A53M-2151 REV 0. 2) ACCOMPLISHED EI T2023A53M-2151 REV 1 AND EI ATTACHED TO W/OO 8538401 (066). 3) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)