As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT MLG VEE FAILED ON BOTH STRUT TUBES APPROX .5" ABOVE SUPPORT ANGLES ON AXLE CLUSTER. IT APPEARS FROM VISUAL INSP THAT BOTH STRUT TUBES MAY HAVE HAD PREVIOUS STRESS FRACTURES PRIOR TO FAILURE DUE TO DARK CRACK WORKING INDICATIONS ADJACENT TO SHINY FRESH CRACK INDICATIONS. THIS AREA IS LIKELY TO BE COVERED BY FABRIC (LANDING GEAR VEE ASSY) AND MAY BE DIFFICULT TO INSPECT DURING ROUTINE AND ANNUAL INSPECTION.