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 AND KICK PLATE BTW FS 310.00 TO FS 349.00 AT PASSENGER DOOR FUSELAGE FRAME. CORROSION ON KICK PLATE BTW FS 310.00 TO FS 349.00 AT PASSENGER DOOR FUSELAGE FRAME WAS REMOVED AND EVALUATED WITHIN OF LIMITS PER CRJ-700 SRM 51-21-06-001-001-A01 AND SRM 53-21-23-101-001-A01. MID CAP ANGLE WAS REPLACED PER CRJ-700 SRM 51-41-02-001-001-A01