As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE IN FOR D-CHECK, MAINTENANCE REPORTED FUSELAGE SKIN UPPER LAP CORRODED BEYOND LIMITS AT STR 10R, FROM FS 1080-1122. REMOVED DAMAGE PER SRM 53-30-03 AND INSTALLED CONICAL WASHERS PER SRM 51-30-5 AND INSTALLED REPAIR PARTS PER SRM 51-30-5.