As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CRACK ON NR 1 BLADE OF NR 2 ENGNE PROP ASSEMBLY. REMOVED NR 1 BLADE OF NR 2 ENGINE PROP ASSEMBLY IAW HAMILTON SUNDSTRAND MM 61-10-00, PATE 307-311 PARA 5A. INSTALLED NEW PROP BLADE IAW HAMILTON SUNSTRAND MM 61-10-00, PAGE 705-714 PAR, G/H. GROUND RUN-UP CHECK GOOD. (M)