As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON MID CAP ANGLE LOWER SURROUND STRUCTURE PASSENGER DOOR (SM)[FUS]. CORROSION ON ANGLE MID CAP WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 BLENDED AREA WAS MEASURED. ORIGINAL THICKNESS IS 0.060'' AND MINIMUN REMAINING THICKNESS IS 0.038'' THEREFORE IT'S OUT OF LIMITS PER SRM 53-21-23-101-001-A01. MID CAP ANGLE AT LOWER SURROUND STRUCTURE OF PASSENGER DOOR WAS REPLACED PER SRM 51-41-02-001-001-A01.