What was found
STRESS CRACK CORROSION FOUND AROUND RIVET ON SUB FLOOR AT FS 190, X22R. FABRICATED A NEW PANEL, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 551-10-2, 51-10-3, AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STRESS CRACK CORROSION FOUND AROUND RIVET ON SUB FLOOR AT FS 190, X22R. FABRICATED A NEW PANEL, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 551-10-2, 51-10-3, AND 51-30-2.