As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SSI 53-23-003 FUSELAGE INTERNAL SKIN IS CORRODED BETWEEN FR 87-88 AND STGR 28R-27R (LEVEL 2 CORROSION)-C/A-BLENDED OUT CORROSION ON FUSELAGE INTERNAL SKIN BTW FR 87-88 AND STGR 28R-27R IAW EMB 170 SRM 51-10-03. BLENDED AREA ON FUSELAGE INTERNAL SKIN BTW FR 87-88 AND STGR 28R-27R FOUND TO BE WITHIN ALLOWABLE LIMITS IAW EMB 170 SRM 51-75-16.