As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION, A .75 INCH CRACK WAS FOUND NEAR A RIVET WHICH ATTACHES THE ENGINE NACELLE TRAILING EDGE FAIRING TO THE INBOARD FLAP. THE CRACK WOULD NOT HAVE RESULTED IN ANY DAMAGE, BUT SINCE IT IS PART OF A CONTROL SURFACE, RESULTED IN BEING A MAJOR REPAIR.