As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT AILERON UPPER L/E IS CHAFED. C-CHECK, RO 4/1/15, REMOVED DAMAGE FROM RT AILERON UPPER L/E. ORIGINAL MATERIAL THICKNESS IS .090", REMAINING MATERIAL AFTER BLEND OUT IS .088", TOTAL MATERIAL REMOVED IS .002". REPAIR FOUND TO BE WITHIN LIMTS. REF REO AND SRM.