As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER FUSELAGE UNDER WING BARREL SKIN IS CORRODED FROM STATION 1368 TO 1288 FROM LONGERON 47R TO 52R. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL II. ORIGINAL THICKNESS IS .090 IAW DWG AYB7030. AFTER BLENDOUT MATERIAL IS AT .080, WITHIN LIMITS IAW DC10 SRM 51-21-01 VOL II. (OPEN)