As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT AILERON L/E UPPER SIDE IS CHAFE, C-CHECK, RO 4/1/15. REMOVED CHAFE DAMAGE ON LT AILERON UPPER L/E. ORIGINAL MATERIAL THICKNESS IS .090", REMAINING MATERIAL AFTER BLEND OUT IS .083", TOTAL MATERIAL REMOVED IS .007". REPAIR FOUND TO BE WITHIN LIMTS. REF REO AND SRM.