As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NOSE WHEEL WELL-STA 1090/FR11, LIGHT SURFACE CORROSION FOUND ON W/W FWD WALL, LOCATED RBL8.0 BETWEEN STIFFENERS 5/6. REMOVED THE LIGHT CORROSION PER SRM 51-74-10. APPLIED ALODINE PER SRM 51-21-10. NO CRACK FOUND PER NTM 51-10-08. THE REMAINING THICKNESS IS 0.087 INCH PER NTM 51-10-04. REPAIR PER EA 6-5310-117363.