What was found
(CAN) OIL LINE FROM TRANSMISSION P/N 212-040-237-003 TO OIL COOLER WAS PERFORATED AT ANCHOR POINT TO AIRFRAME STRUCTURE. ACCUMULATION OF DIRT/SAND AND OIL INSIDE THE CLAMP HAD WORN THRU THE LINE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) OIL LINE FROM TRANSMISSION P/N 212-040-237-003 TO OIL COOLER WAS PERFORATED AT ANCHOR POINT TO AIRFRAME STRUCTURE. ACCUMULATION OF DIRT/SAND AND OIL INSIDE THE CLAMP HAD WORN THRU THE LINE.