As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INITIAL INSPECTION: CORROSION ON FRAME FS=265 BTW STGR 26R / 26L AT INTERNAL STRUCTURE OF FWD FUSELAGE (SM) (TCI 100-06) SUMMARY: CORROSION ON FRAME FS=265 BTW STGR 26R / 26L AT INTERNAL STRUCTURE OF FWD FUSELAGE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN LIMITS PER CRJ900 SRM 53-00-00-101-001-A01.