What was found
(CAN) WHEN LEFT ACTUATOR REMOVED TO ALLOW MOUNT BOLT REPLACEMENT, A CRACK WAS FOUND ON THE FORWARD INBOARD SIDE OF THE BEARING SHOULDER WHERE THE PIVOT OF THE LANDING LEG RESTS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) WHEN LEFT ACTUATOR REMOVED TO ALLOW MOUNT BOLT REPLACEMENT, A CRACK WAS FOUND ON THE FORWARD INBOARD SIDE OF THE BEARING SHOULDER WHERE THE PIVOT OF THE LANDING LEG RESTS.