As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C NOSE WHEEL WELL COMPARTMENT TUNNEL - AT STA 240 CEILING AREA THE CABIN HORI FLOOR SUPPORT WEB AREA AFT SURFACE CORROSION FOUND AT BL 0. FLOOR SUPT WEB REPAIRED IAW SRM 51-40-02 FIG.1 DUE TO BLENDED DEPTH 0.043 INCH, WIDTH .7500 INCH AND LENGTH 2 INCH EXCEEDS SRM 53-10-01 FIG.1 LIMITATION.