As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON NLG DOOR INTERNAL HOLES OF HINGE FITTINGS (2EAS) LH/RH AT FUSELAGE STRUCTURE WAS FOUND. CORROSION ON NLG DOOR INTERNAL HOLES OF HINGE FITTINGS (2EAS) LH/RH AT FUSELAGE STRUCTURE WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 51-10-06-001-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01.