What was found
(CAN) CRACK IN HEAD WALL BETWEEN FINS 11 AND 12 COUNTING FROM BARREL, ON EXHAUST SIDE OF CYLINDER.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) CRACK IN HEAD WALL BETWEEN FINS 11 AND 12 COUNTING FROM BARREL, ON EXHAUST SIDE OF CYLINDER.