As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WO 209669 NR 200321 HEAVY CHECK COE/MAJOR REPAIR: FORWARD FUSELAGE R/H UPPER SKIN PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION FWD OF FRAME 23 BETWEEN STRINGERS 8R-10R. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0111812_01...15731 ISSUE A, DATED 1/21/2020.