What was found
THE FUSELAGE FRAME WAS FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-21-06 AND 51-12-00 AND 51-21-16, SRM 51-21-11. DEFECT LOCATION: FS 1088.20 BETWEEN STGR. 26R-26L
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE FUSELAGE FRAME WAS FOUND WITH CORROSION DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 51-21-06 AND 51-12-00 AND 51-21-16, SRM 51-21-11. DEFECT LOCATION: FS 1088.20 BETWEEN STGR. 26R-26L