As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER FUSELAGE, BS 897, BODY FAIRING ATTACHMENT FRAME AT BL 0, CORROSION FOUND. CORROSION REMOVED IAW SRM 51-10-02, MATERIAL REMOVED 0.072 " (L-18" W-1") ORIGINAL MATERIAL THICKNESS MEASURED 0.090" AND FOUND OUT CORROSION STILL EXISTS IAW BSOPM 20-20-02 REV 5. DAMAGED FRAME ATTACHMENT R & R IAW SRM 51-40-02.