What was found
INTERIOR FUSELAGE TRANSVERSE BEAM UPPER FLANGE CRACKED IN 2 PLACES, FS 280.00 LBL 9.0 AND RBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-136 REV NC AND 601R-53-11-13 REV NC.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INTERIOR FUSELAGE TRANSVERSE BEAM UPPER FLANGE CRACKED IN 2 PLACES, FS 280.00 LBL 9.0 AND RBL 9.0. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-11-136 REV NC AND 601R-53-11-13 REV NC.