As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON TOP OF FRAME ABOVE REPAIR STRAP AT STATION 1480, STRINGER 26R IN AFT CARGO COMPARTMENT. CORROSION ON FRAME BOTTOM FOUND TO BE OUT OF LIMITS. MATERIAL LOSS IS .038. ORIGINAL THICKNESS WAS .063, REMAINING THICKNESS IS .025. USING MIC ID MO1 IAW SRM 53-00-07 FIG 101, REMOVED, FABRICATED & INSTALLED NEW -69 FRAME IAW SRM 51-40-02 PARA 4 & 7 FIG 8 & 12 DWG 14N1030 SHT 10.