As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 0083 011 NR 2 K-FLAP CORRODED AT I/B BONDING JUMPER TO BULLNOSE. REMOVED CORROSION ON NR 2 K-FLAP I/B BULLNOSE ATTACH (LOWER) POINT FLANGE THICKNESS .140. REMOVED .030 WITHIN LIMTS PER FED-EX DWG NR SR 27-57-010. UPPER ATTACH POINT OUT OF LIMITS. INSTALLED REPAIR PARTS IAW FED-EX SRM 57-50-3.