As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) WHILE PERFORMING A DETAIL INSPECTION OF THE CARGO DOOR INTERNAL STRUCTURE IN ACCORDANCE WITH TASK RJ2-52-830-506 , A CRACK WAS FOUND ON THE TOP FORWARD RADIUS OF SUPPORT FITTING. THE FITTING WAS REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-10-06.