What was found
FUSELAGE LOWER SKIN PANEL AT FS 310.00 TO FS 319.70 HAS CORROSION BETWEEN STR 27L AND 26L. PERFORMED A MAJOR PERMANENT REPAIR BY INCORPORATING REO 690-53-21-355 REV--AND RO CRJ9-53-1045.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE LOWER SKIN PANEL AT FS 310.00 TO FS 319.70 HAS CORROSION BETWEEN STR 27L AND 26L. PERFORMED A MAJOR PERMANENT REPAIR BY INCORPORATING REO 690-53-21-355 REV--AND RO CRJ9-53-1045.