As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION PITS ON TOP REAR SKIN OF THS LT. REMAINING THICKNESS IS WITHIN LIMITS GIVEN IN SRM BUT MAXIMUM AFFECTED SURFACE AREAS ARE >400 MMXMM AND THEREFORE ARE OUT OF LIMIT AS PER SRM 55-10-00/CONFIG 2/TB 101, PIT AREAS BETWEEN 200 AND 1500 MMXMM) REWORK AREAS DOCUMENTED AND APPROVED PER EA 6-5510-92156 AND RAS/CASA/4264/2005 ISSUE A.