As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CORROSION AROUND 2 PANEL SCREW HOLES AT FS X 784.102 FLOOR LEVEL Z100.032 Y6.250 AND Y20. BLENDED OUT CORROSION AND FOUND IN LIMITS IAW SRM 51-21-00 AND RD 8/4-53-3835.. ALODINED IAW SRM 51-21-10-01. ENGINEERING REQUEST SENT TO MFG. PERFORMED ECI ON BLENDED AREA. NO CRACKS FOUND AT THIS TIME IAW NDTM PSM 1-84-7A. APPLIED PRIMER TOP COAT AND CIC IAW RD 8/4-53-3835.