As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCH CORRODED AREA AND OTHER SMALLER AREAS AT BS 237 LBL 24 TO RBL 24 NOSE WHEEL WELL UPPER CHORD ANGLE. FABRICATED NEW ANGLE AND INSTALLED, REPAIRED PER DRW 65-45819 SRM 51-10-1. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)