As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C4 CHECK - PASSENGER DOOR MID CAP ANGLE CORRODED. BLENDED CORROSION 2"X .5"W X .040"D IAW SRM 51-21-06-001-001-A01 ORIGINAL THICKNESS .063", REMAINING THICKNESS .023" FOUND TO BE OUT OF LIMITS IAW CRJ700 53-21-23-101-001-A01. REMOVED MID CAP ANGLE IAW SRM 51-41-02-001-001-A01. LOCATED HOLES IN NEW MIDCAP ANGLE AND INSTALLED NEW ANGLE IAW SRM 51-41-02-001-001-A01.