As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C CHECK- COCKPIT PANEL FLOOR SUPPORT ANGLE AT FS 280 SHOWS SIGNS OF CORROSION. BLENDED CORROSION, FOUND CORROSION OUT OF LIMITS IAW SRM5300-00-001-A01 PAGE 3. LOCATED FASTENER HOLE IN NEW ANGLE IAW SRM51-40-11-001-001-A01. INSTALLED NEW A IAW SRM 51-42-21-001-001-A01. PRIMED, TOP-COATED FASTENERS IAW SRM 51-25-06-001-001-A01 AND 51-25-16-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND IAW SRM 51-21-11-001-001-A01.