What was found
(CAN) DURING ROUTINE INSPECTION AME DISCOVERED THAT THE HYDRAULIC PUMP BELT WAS TORN (APPROXIMATELY .3333 OF THE WIDTH) AT LAP JOINT AREA. BELT REPLACED AND AIRCRAFT RETURNED TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DURING ROUTINE INSPECTION AME DISCOVERED THAT THE HYDRAULIC PUMP BELT WAS TORN (APPROXIMATELY .3333 OF THE WIDTH) AT LAP JOINT AREA. BELT REPLACED AND AIRCRAFT RETURNED TO SERVICE.