What was found
AS RECEIVED, PREVIOUS BLEND ON THE FORWARD FACE OF DOVETAIL CORNER NR 42 (CLOCK POSITION 3:30) IN SLOT FA WAS FOUND. THE BLEND MEASURES APPROXIMATELY 0.450 CIRCUMFERENTIAL LENGTH, 0.100 RADIAL WIDTH, AND 0.084 AXIAL HEIGHT. THERE APPEARS TO BE ONE THROUGH CRACK PRESENT IN THE BLENDED AREA (TWO INDICATIONS BACK TO BACK) THAT MEASURES 0.208 CIRCUMFERENTIAL LENGTH, LOCATED CENTRALLY ON THE DOVETAIL AND 0.050 DOWN AXIALLY. THE DAMAGE IS FREE FROM HIGH SPOTS AND BURRS. THE COMPONENT IS AT PIECE PART LEVEL AND WAS IN PROCESS UNDERGOING AN OVERHAUL WORKSCOPE AT BARNES AEROSPACE WINDSOR AIRMOTIVE DIVISION (FAA REPAIR STATION KC1R265K) WHEN THIS CONDITION WAS FOUND. THE PART IS CURRENTLY ON HOLD. PLEASE NOTE: ENGINE TSN AND CSN NOT PROVIDED NOR IS TIME SINCE LAST OVERHAUL OR REPAIR. INFORMATION NOT AVAILABLE AT TIME OF SUBMITTAL OF THIS SDR.