As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING FLAP TO FUSELAGE WEAR STRIP JUST BELOW OVERWING SLIDE HAS A .250 CRACK ON WEAR STRIP. CRACK LOCATED ON BOTTOM EDGE OF RUB STRIP, NOT IN AIR STREAM. STOP DRILLED CRACK. NEW STRIP 110-1031. SECONDARY STRUCTURE, WEAR STRIP. CRACK IS NOT NEAR ANY FASTENER HOLES. STRIP IS SECURE AND INTACT. RPLC'D CRACKED WEAR STRIP.