As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 PYLON STRUT INTERNAL SKIN HAS CORROSION ON LT SIDE AROUND PANEL 443GL CUT OUT AREA PP STA 106.20 - 119.95. REPAIR CARRIED OUT IAW EA F-5450-142340 (NACELLES/PYLONS - PYLON STRUCTURE - NR 2 STRUT FWD OTBD AND INBD SKIN PANEL CORROSION REPAIR). REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.