What was found
LEFT WING I/B MAIN FLAP O/B LEADING EDGE CHAFED. REMOVED DAMAGE & INSTALLED DOUBLER REPAIR PER SRM 57-53-01 FIG 201. DEFECT SIZE: 7.125"L X 0.187"W X 0.012"D.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING I/B MAIN FLAP O/B LEADING EDGE CHAFED. REMOVED DAMAGE & INSTALLED DOUBLER REPAIR PER SRM 57-53-01 FIG 201. DEFECT SIZE: 7.125"L X 0.187"W X 0.012"D.