As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
"THE FUSELAGE FRAME AT FS 1088.20 WAS FOUND WITH CORROSION DAMAGE AT TWO LOCATIONS BETWEEN STGR 26R TO 26L. PERFORM PERMANENT REPAIR IAW CRJ7/9 SRM 51-00-00, THE FUSELAGE FRAME IS CLASSIFIED AS PRIMARY STRUCTURE. 2. PERFORM PERMANENT REPAIR IAW CRJ7/9 SRM 51-13-02, TABLE 1, THE FUSELAGE FRAME IS LISTED AS FATIGUE CRITICAL BASELINE STRUCTURE (FCBS) THEREFORE, DTE IS REQUIRED FOR THIS REPAIR. "