As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WEAR ON SEVERAL LUG OF PASSENGER DOOR HINGE (PASSENGER DOOR SIDE) WERE BLENDED OUT AND REWORKED AREA WAS MEASURED AND FOUND WITH THE FOLLOWING DIMENTION: MINIMUM REMAINING LUG WALL THICKNESS IS 0.104IN, THEREFORE REWORKED AREAS ARE WITHIN LIMITS PER CRJ-900 SRM 52-11-01-201-007-A01