As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING LOWER L/E PANEL 616 HB IS CHAFED. BLENDED AREA IAW SRM 57-00-01; VOL I; FIG 1-A. ORIGINAL MATERIAL THICKNESS 0.090 IAW SRM 57-31-01; VOL III. MATERIAL LOSS 0.022. REMAINING THICKNESS 0.068 AND FOUND OUT OF LIMITS IAW SRM 57-00-01; VOL I. CUT OUT THE DAMAGE IAW SRM 57-00-01; VOL I. FABRICATED THE FILLER AND DOUBLER IAW SRM 57-00-01; VOL I AND SRM 57-31-01; VOL III. ALODINED AND PRIMED IAW SRM 51-21-01; VOL II; PGS 21 - 24.