What was found
(CAN) A CRACK WAS VISUALLY DETECTED AT THE UPPER END ON THE LT MAIN LANDING GEAR SHOCK ABSORBER STRUT. AT THE TIME THE AIRCRAFT WAS UNDERGOING A MAJOR INSPECTION AS REQUIRED BY THE MANUFACTURE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) A CRACK WAS VISUALLY DETECTED AT THE UPPER END ON THE LT MAIN LANDING GEAR SHOCK ABSORBER STRUT. AT THE TIME THE AIRCRAFT WAS UNDERGOING A MAJOR INSPECTION AS REQUIRED BY THE MANUFACTURE.