As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WO 209669 NR 200316 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE L/H UPPER SKIN PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION FRAMES 23-23A BETWEEN STRINGERS 6AL-7L. CORRECTIVE ACTION: REPAIRED PER SRAS CETS-3143/16...10437 ISSUE B, DATED 2/12/2020.