As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND AROUND NUT PLATE HOLES ON FORWARD CARGO COMPARTMENT LT TRANSITION ANGLE BETWEEN BS 380 AND BS 480. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED ANGLE BETWEEN BS 380 AND BS 480; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW B737-200 SRM 51-30--02, PG. 1, FIG. 2 & 3.