As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) WHILE RELOADING ACFT AT A FOB, AFT CROSSTUBE FAILED JUST INBD OF THE OUTER EDGE OF LT SADDLE BRACKET AND CLAMP ASSY. ON INVESTIGATION, SOME PITTING CORROSION WAS NOTED UNDER THE SADDLE AREA AT A POINT WHERE THE FRACTURE SEEMS TO HAVE ORIGINATED. ADDITIONAL DAMAGE TO SECONDARY STRUCTURE AS WELL AS COSMETIC DAMAGE OCCURED.