As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HEAVY MAINTENANCE, CORROSION STRINGER 28R AT LEVEL FR88 TO FR89 LOWER FUSELAGE; PERFORMED PERMANENT REPAIR ON STRINGER 29R AT LEVEL FR88 TO FR89 LOWER FUSELAGE IAW E190 SRM 53-23-03 REPAIR 51P TYPICAL SPLICE REPAIR OF STRINGERS ITEM 5 FIGURE 210.