What was found
CORROSION ON FRAME ANGLE AT INTERNAL FUSELAGE STRUCTURE FS661.00 + 90.00 AND STGR 19RH. FRAME ANGLE AT INTERNAL FUSELAGE STRUCTURE FS661.00 + 90.00 AND STGR 19RH WAS REPAIRED PER EA CRJ953-21186 REV IR
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON FRAME ANGLE AT INTERNAL FUSELAGE STRUCTURE FS661.00 + 90.00 AND STGR 19RH. FRAME ANGLE AT INTERNAL FUSELAGE STRUCTURE FS661.00 + 90.00 AND STGR 19RH WAS REPAIRED PER EA CRJ953-21186 REV IR