As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING INSPECTION, FLUID LEAK WAS FOUND AROUND FILLER AREA. EDDY CURRENT INSPECTION CONFIRMED A 1INCH CRACK IN THE WELD AT FILLER NECK. CRACK WAS WELD REPAIRED IAW MFG INSTRUCTIONS, PENETRANT INSPECTED AND RESERVOIR PROOF PRESSURE TESTED D TO 30 PSI.