As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT O/B FORE FLAP LEADING EDGE I/B AREA WS 397-438 HAS SEVERAL CHAFED MARKS. BLENDED OUT CHAFED AREAS, ORIG MAT .080-MAT LOSS .020, OUT OF LIMITS, CUT OUT DAMAGE. FABBED REPAIR PLATE DOUBLERS AND STRAPS IAW SRM 57-33-01. INSTALLED PARTS IAW SRM 57-53-01 FIG 202.