As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPR WING PANEL ABOVE NR 19 L-E VARIABLE CAMBER FLAP HAS A 18 INCH CRACK APPROX 8 IN OTBD OF INBD END. PREPPED SURFACE FOR REPAIR, FABRICATED PATCH. NEEDS APPLIED & BAGGED, CURED. ACCOMPLISHED 250 DEG. OVER LAY REPAIR, PRIMED AND PAINTED.