As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/E NR 1 PYLON TOP PANEL P/N A572-44103-000 BACK SIDE HAS CHAFING MARKS IN NUMEROUS PLACES. BLENDED CHAFE MARKS IAW SRM 57-41-12 PG 102. MAT THICKNESS IS .035 IAW SRM 57-41-12, ITEM 60. MAT LOSS .006; MAT REMAINING .024, CHECKS TO BE OUT OF LIMITS IAW SRM 57-41-12. PAINTED NEW PANEL NR A57244103000; PO 610703.2 IAW SRM 51-23-10.