As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:3C, LT OTBD AILERON UPPER L/E EDGE PANEL IS CRACKED AT 3EA OTBD HINGES STRICKERS. IDENTIFIED DAMAGED AREAS. PERFORMED TAP TESTS FOR DELAMINATION. CUTOUT DAMAGED AREAS. REPAIRED DAMAGED AREAS WITH COMPOSITE MATERIAL IAW SRM 57-60-80, REPAIR 1. ACCOMPLISHED WEIGHT AND BALANCE IAW SRM 51-91-07. ACCOMPLISHED EA 011-5750-01-A3445, REV IR AND EO MD11-5750-44299A.