As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 1 POSITION 6 OF VERTICAL STRINGER REDIUS IN CNETER FUSELAGE ON FRAME 36 CRACK DEPTH O.085 INCH CRACK DIRECTION 6 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC NO. A25-1157-01 AND EA NO. 57-0117-25. WORK ACCOMPLISHED ON AEROMAN NR 2025-682318.