What was found
ENGINE WAS IN-FLIGHT, SHUT DOWN. DISASSEMBLY INSPECTION REVEALED ONE LIBERATED 10TH STAGE STATOR VANE AT THE CONVEX END OF ONE QUADRANT AT 9:00. THREE ADDITIONAL VANES IN THE SAME CLUSTER OF FIVE ARE FRACTURED THROUGH AT THE OUTSIDE DIAMETER SHROUD VANE BRAZE FILLET. METALLURIGCAL ANALYSIS OF THE 10TH STATOR AND 11TH BLADES IS BEING CONDUCTED BY PRATT AND WHITNEY MERL TO VERIFY FAILURE.