As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CRACK AT BOLT HOLE OF BLADE NR 1 LEADING EDGE BY LIQUID PENETRANT INSPECTION WHEN OVERHAULING PROPELLER. CRACK IS ABOUT .185 INCH LONG AND .060 INCH FROM EDGE OF BOLT HOLE. RETURNED TO SERVICE IAW AD 95-21-01 PER SB 219. RECOMMEND THAT LIQUID PENETRANT INSPECTION BE PERFORMED INSTEAD OF VISUAL INSPECTION PER SB 219.