As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) CRACK WAS DISCOVERED AT INSPECTION NEXT TO EXHAUST TUBE USED TO SUPPLY ENGINE EXHAUST TO COWLING LIP DEICE. ABOUT ONE INCH FROM ENGINE MOUNTING FLANGE , CRACK WAS ABOUT ONE AND A QUARTER INCH LONG. REPAIR PERFORMED IAW MM CHAPTER 78 10-01.