As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CENTER WING REAR SPAR VAPOR WEB HAS AN APPROXIMATE 18 INCH CRACK BEGINNING INBOARD OF THE SYS.A HYD. PRESSURE MODULE INBOARD MOUNT AND EXTENDING APPROX. 6 INCHES TO LEFT OF LBL 45.64 STIFFENER.<[01] C/W EA 23-157-02932;[02] COMPLIED WITH EA 23-157-02932. ALSO REFERENCE PREVIOUS DOCUMENTATION OF CRACK; PERMANENT REPAIR AND INTERIM REPAIR. TTG8Q00M8KD2; TTG8Q00M8B6K; TSR 2023005578; TTG8Q00NBF8B; TTG8Q00NBFEQ AND TTG8Q00M8RRZ