What was found
(CAN) A CRACK WAS IDENTIFIED ON THE OUTER EDGE OF THE WHEEL RIM RUNNING CIRCUMFERENTIALLY APPROX. 5 CM (TC 20091028006)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) A CRACK WAS IDENTIFIED ON THE OUTER EDGE OF THE WHEEL RIM RUNNING CIRCUMFERENTIALLY APPROX. 5 CM (TC 20091028006)