What was found
"INITIAL INSPECTION: CORROSION ON INTERNAL STGR 18R BTW FS394 TO FS409. THE STRINGER WAS REPAIRED IAW SRM 53-00-03-201-001-A02, FIG.53-00-03-995-807,SOLUTION II.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
"INITIAL INSPECTION: CORROSION ON INTERNAL STGR 18R BTW FS394 TO FS409. THE STRINGER WAS REPAIRED IAW SRM 53-00-03-201-001-A02, FIG.53-00-03-995-807,SOLUTION II.