As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT MAIN LANDING GEAR SHOCK STRUT DOOR MISSING. DOOR APPEARS TO HAVE HAD DOOR FASTENERS FAIL AT LWR FWD ATTACH POINT. DMG TO WING PANELS, TRUNION DR & MLG LUG ATTACHMNTS SUGGEST THIS PATTERN. PANEL DID NOT CAUSE FLR. REPLACED DOOR. AC RETURNED TO SERVICE READY STATUS. DOOR EXPERIENCES AIR LOADS DURING LANDING & TAKEOFF. SUSPECT VIBRATION CAUSED FAILURE OF DOOR ATTACH FITTINGS.