As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK INSPECTION, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE IN THE LOWER TANG OF THE RIGHT WING INBOARD FLAP LOWER CLEVIS. REPAIRED CLEVIS BY INSTALLING A 2.0 INCH BY 2.0 INCH DOUBLER MADE OF .125 A1S1 301 1/2 H MATERIAL IAW EO 9606181. 8110-3 ISSUED BY DER SW-713.