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 HOLDE ZONE 2, POSITION 5 OF VERTICAL STRINGER RADIUS IN CENTER FUSELAGE ON FRAME 36. CRACK DEPTH 0.127 INCH CRACK DIRECTION 8 AND 9 O'CLOCK VIEW LOOKING AFT; PERFORMED REPAIR IAW EC NO. A25-1157-01 AND EA 57-0117-25. WORK ACCOMPLISHED ON AEROMAN WO 2025-413/1 NR 2025-682310.