Model: V2-141-057-17

Special Features:

Cres, m3603, fscm 91547, rockwell a scale 69 min, 73 max hardness, 3.805 in. Min, 3.815 in. Max o/a lg, 9.820 in. Nom od disk, 1.394 in.Min, 1.397 in. Max lg disk, 60 blade grooves equally spaced on diskod, 2 stepped hubs, 2.830 in. Min, 2.840 in. Max od 1st step 1st end, 0.700 in. Nom lg 1st step 1st end, 3.320 in. Nom diameter 2nd step 1stend, 0.603 in. Min, 0.607 in. Max lg 2nd step 1st end, externalsplines 1st step 2nd end, 69 teeth, 30 degrees pressure angle, 2.8750 in.Nom pitch dia, 0.380 in. Min, 0.420 in. Max lg splines, 0.681 in.Min, 0.738 in. Max lg 2nd step 2nd end, stepped bore, 3.805 in. Min, 3.815 in. Max o/a lg bore, 2.5576 in. Min, 2.5579 in. Max diameter 1ststep 1st end, 0.950 in. Nom lg 1st step 1st end, 2.566 in. Min, 2.576 in. Max diameter 2nd step 1st end, 0.600 in. Nom lg 2nd step 1stend, 2.2133 in. Min, 2.2137 in. Max diameter 1st step 2nd end, 0.275 in.Min, 0.295 in. Max lg 1st step 2nd end, 2.425 in. Min, 2.435 in. Maxdia 2nd step 2nd end, 0.165 in. Min, 0.205 in. Max lg 2nd step 2ndend, internal splines 3rd s

Properties:

Inc 61833 cancelled/replaced by ,inc 50566, fiig a10700, app-key f ,inc 50565, fiig a10700, app-key f ,on 021513 ~(all except usa). A disk having provisions on the outer periphery for attaching turbine blades and an integral hub that provides support for the turbine and/or a means of attachment for a shaft. See also disk,turbine,turbine engine.