As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ROUTINE POST-FLIGHT VISUAL INSPECTION NOTED LONGITUDINAL CRACKS THROUGH RIVET POINT DUE TO EXPANSION FROM METAL CORROSION ON LEFT AND RIGHT MAIN LANDING GEAR ROD ASSEMBLES, MAIN LANDING GEAR FAIRING, REMOVED THE AFFECTED PARTS AND REPLACED WITH NEW.