As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FORWARD CABIN FLOORBEAM BETWEEN FR 20 TO FR 24 Y-189 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. ORIG MAT .080 DAMAGE DIM. L=6.0 W=2.0 D=.060. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. R & R FLOORBEAM IAW SRM 51-42-11.