As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT PRESSURE FLOOR SILL PANEL AND SILL ANGLES HAVE NUMEROUS AREAS OF CORROSION BETWEEN FS 409+128 AND 559. BLENDED OUT AREAS OF CORROSION IAW REO 601R-53-41-666. PERFORMED NDT IAW REO 601R-53-41-666 STEPS 5 & 12 AND CNDTM PT 1 51-20-06. NO INDICATIONS NOTED. FINISHED, SEALED AND APPLIED CORROSION INHIBITING COMPOUND IAW REO 601R-53-41-666.