As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WO 205731 NR 200121 HEAVY CHECK COE/MAJOR REPAIR: CENTER FUSELAGE UPPER R/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 28D-29 BETWEEN STRINGERS 10R-11R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107986_01...15487 ISSUE A, DATED 11/20/2019.