What was found
AFTER MID CAP REMOVAL, CORROSION ON KICKPLATE ANGLE WAS FOUND. KICKPLATE ANGLE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND 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 MID CAP REMOVAL, CORROSION ON KICKPLATE ANGLE WAS FOUND. KICKPLATE ANGLE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-10-06-001-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01