As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER END OF STRUT CRACKED BETWEEN INNER AND OUTER ATTACH LUGS (IN THE WEB) FROM BOTTOM OF STRUT UP .7500-1 INCH. THERE WERE NO ABNORMAL CIRCUMSTANCES THAT CAUSED THE CRACK. THE CRACK WAS VERY OBVIOUS, VIEW WAS UNOBSTRUCTED AND EASILY DETECTED DURING 100 HOUR INSP. DO NOT THINK THERE IS ANY WAY TO PREVENT THIS KIND OF CRACK.