As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WING CENTER SECTION, BETWEEN LBL 45.61 AND LBL 70.85, BETWEEN REAR SPAR AND STIFFENER S-2C UPPER SKIN WITH CORROSION. NOTE: IT WAS REPAIRED, AS PER AW AVIATION TECH SERVICES ENGINEERING ORDER NUMBER 2020-1012 (REF: JOB: A1J185 NRI: 2-17).