As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING TRAILING EDGE DEFLECTION CONTROL ATTACH FITTING UPPER TAB IS CRACKED APPROXIMATELY 2.5' IN THE RADIUS. PICTURE ATTACHED.<[01] DAMAGE VERIFIED PER NDT PARTY 6 51-00-00 PROCEDURE 23.;[02] DAMAGE VERIFIED PER NDT PART 6 51-00-00 PROCEDURE 23.