Steel, ams5355, 16 vanes, 5.755 in. Min, 5.765 in. Max od, 0.7784 in.Min, 0.7788 in. Max id, 2.440 in. Min, 2.460 in. Max o/a lg, 3 holes, no. 8, 0.164 in.-32 nc class 3b thd 0.380 in. Max deep, countersunk 110 degrees by0.154 in. Min, 0.174 in. Max dia.
Inc 60245 cancelled/replaced by ,inc 50588, fiig a10700, app-key j ,inc 50587, fiig a10700, app-key j ,on 021513 ~(all except usa). An item consisting of a series of blades on one or both sides of the rotor disk extending from the axis of rotation radially to the rim of the disk. It is designed to centrifugally cause the air between the blades to move outward to the rim of the compressor section of a turbine engine.
Classification: Parts of nonaircraft gas turbines
NSN 5990-01-625-5923
NSN 6620-00-824-4609
NSN 5999-01-268-3786
NSN 5920-01-569-3190
NSN 7035-00-574-4223
NSN 5950-01-576-5895
NSN 5998-00-419-3846
NSN 2925-01-247-8058
NSN 6220-01-352-5425
NSN 6130-01-270-2935
NSN 6110-01-315-1157
NSN 5990-00-490-5250