As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .25 INCH CRACK IN RT WING AFT SPAR AT I/B ACTUATOR HINGE FORWARD FORGING FROM I/B LOWER BOLT AREA, APPROXIMATELY XRS 164. THE FASTENERS WERE REMOVED AND THE CRACKED SECTION OF SPAR WAS CUT OUT. A NEW SPAR SECTION WAS INSTALLED USING SPLICES INSIDE AND OUTSIDE IAW DRAWING J060165 AND EA 5761-01001.