As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE-C, INTERNAL FUSELAGE FOUND CORROSION AT LAP JOINT FROM BS 1880 TO BS 1940 RT STR 4. REMOVED CORROSION FROM BS 1860 TO BS 1940 ACC TO SRM 51-10-01 WITHIN LIMITS ACC SRM 53-30-01. DELAMINATED LAP SPLICE REPAIRED ACC TO SRM 53-30-03 FIG 10 FROM BS 1860 TO BS 1940 STR 4 RT.