As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 100 HR. INSPECTION IAW SB 1131 THE LT MAIN GEAR UPPER STRUT CYLINDER WAS CRACKED AS DEPICTED IN THE BULLETIN. THE PART WAS DYE CHECKED AT THE PREVIOUS INSPECTION WITH NO CRACK EVIDENT. THE CRACK IS APPROX. 2 IN. LONG STARTING AT THE BOTTOM OF THE OUTBOARD (EAR).