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