As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER 44L AT FRAMES 41 - 42 IN A/C BAY CORRODED. BLENED IAW SRM 51-74-10, PERFORMED DVI TO VERIFY NO CORROSION FOUND IAW NTM 51-70-00, PERFORMED ROTO TEST TO OPEN HOLES TO VERIFY NO CRACKS FOUND IAW NTM 51-10-01. FABRICATED THE REPAIR PARTS IAW SRM 53-10-14-201 PARA 4.C FIG 203 SHEET2. INSTALLED THE REPAIR IAW SRM 53-10-14-201 PARA 4. C FIG 203 SHEET 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.