As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING AILERON PANEL 559AB HAS AREAS OF CHAFING. BLENDED DAMAGED AREA IAW SRM 51-12-00. ORG THICKNESS .055 AFTER BLENDING MIN THICKNESS .048 TOOL REF 326 (CAL DUE 6/14/12. WITHIN LIMITS IAW REO 601R-57-60-020. NDT INSPECTION ALODINED, PRIMED, TOP COATED IAW SRM 51-21-11, 51-25-06, 51-25-16.