As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CRACK IN TRAILING EDGE PANEL WIGGLE PLATE WITH PLATE LOOSE AND HOLES ELONGATED. WING STRUCTURE HOLES ARE NOT ELONGATED. CRACK IS LOCATED 28 FROM INBD EDGE OF #12 SPOILER AND IS .320 IN LENGTH. CRACK GOES FROM RIVET HOLE TO FWD EDGE OF WIGGLE PLATE.<[01] REPAIRED PER EA 23-157-02318. ATTACHED TO TTG8Q00MD1EW