As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING COMPLIANCE WITH AD 2010-23-14: AFTER REMOVAL OF FOAM RESIN, MAINTENANCE FOUND PASSENGER DOOR HAD LIGHT SURFACE CORROSION ON INNER SKIN. ALSO FOUND ATTACH ANGLE CORRODED ON DOOR NEAR HINGE LINE AT FS 320.10. REMOVED AND TREATED LITE SURFACE CORROSION IAW CRJ-200 SRM 51-21-06 AND REMOVED AND REPLACED ANGLE IAW CRJ-200 SRM 51-42-06 AND 51-24-36.