As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C4 CHECK - MID CAP KICK PLATE ANGLE CORRODED. BLENDED CORROSION 1.8L X .8W X .015D IAW SRM 51-21-06-001-001-A01 ORIGINAL THICKNESS .063, REMAINING THICKNESS .048 FOUND TO BE OUT OF LIMITS IAW 53-21-23-101-001-A01. REMOVED KICK PLATE IAW SRM 51-42-21-001-001-A01. LOCATED HOLES IN NEW KICK PLATE IAW SRM 51-40-11-001-001-A01 AND INSTALLED NEW ANGLE IAW SRM 51-42-06-001-001-A01.