What was found
DURING HEAVY MAINTENANCE, LATE FINDING: CORROSION ON FUSELAGE INTERNAL STRUCTURE STR 23L FR 90.;REF TOMX WO# 1708 NR# 00594 SECTION OF STRINGER 23LH BTW FR89 TO FR90 WAS REPAIRED PER EMB190 SRM 53-30-03 / REPAIR 51P.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HEAVY MAINTENANCE, LATE FINDING: CORROSION ON FUSELAGE INTERNAL STRUCTURE STR 23L FR 90.;REF TOMX WO# 1708 NR# 00594 SECTION OF STRINGER 23LH BTW FR89 TO FR90 WAS REPAIRED PER EMB190 SRM 53-30-03 / REPAIR 51P.