As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER REMOVAL MID CAP ANGLE, WAS FOUND CORRSION ON KICKPLATE ANGLE AT DOOR SURROUND STRUCTURE OF THE PASSENGER DOOR KICKPLATE ANGLE AT DOOR SURROUND STRUCTURE OF THE PASSENGER DOOR WAS EVALUATED OUT OF LIMITS PER SRM SRM 53-21-23-101-001-A02 AND WAS REPLACED PER SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01