As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C-CHECK-COCKPIT FLOOR SUPPORT ANGLE ATTACHING FWD SIDE OF FS280 BEAM IS CORRODED. BLENDED .005" MATERIAL FROM ANGLE, ORIGINAL THICKNESS IS .063', MATERIAL REMAINING IS .058". BLEND IS WITHIN LIMITS IAW SRM 53-21-43-001-A01 PG 103. TREATED AND PRIMED IAW SRM 51-21-11-001-001-A01 AND 51-25-06-001-001-A01. APPLIED CORROSION INHIBITING COMPOUND TO ALL AFFECTED AREAS IAW SRM 51-21-11-001-001-A01.