As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L2 DOOR CUTOUT AREA, INNER CHORD HAS CORROSION ON UPPER SURFACE BETWEEN BS 927 TO 992.8 APPROX. LBL-56. REMOVED CORROSION ON INNER CHORD UPPER SURFACE BS 927-992.8 LBL56. ORIGINAL THICKNESS IS .080, REMAINING THICKNESS IS .046, LOSS OF MATERIAL IS .034, FOUND OUT OF LIMITS IAW SRM 53-70-15-01-7.