As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A VISUAL INSPECTION OF THE WING, A CRACK WAS NOTED IN THE UPPER PORTION OF THE INBOARD WING BETWEEN THE FUSELAGE AND THE NACELLE (WS 49.0). FURTHER INVESTIGATION SHOWED THE TWO SUPPORT ANGLES THAT HOLD THE LANDING GEAR BUMPER ASSY (P/N 43016-00 AND P/N 43016-01) WERE CRACKED IN THE RADIUS OF THE SUPPORTING CHANNEL.