Steel, ams 6415, rockwell c35-40 hardness, 1.354-1.365 in. Thk, 20.017-20.027 in. Od, 11.995-12.005 in. Id, 103 blade slots equallyspaced around od, sixteen 0.437-0.440 in. Holes equally spaced on 8.000in. Centerline radius, 32 scallops equally spaced on 7.260 in.Centerline radius, thirty-two 0.108-0.113 in. Holes equally spaced on7.260 in. Centerline radius
An item having provisions on the outer periphery for attaching a designated number of blade, turbine rotor, aircraft gas turbine engine. It also has provisions for attachment to a hub, turbine, aircraft gas turbine engine.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 6610-00-100-1195
NSN 5998-01-659-3905
NSN 5999-01-415-3897
NSN 5895-01-283-5733
NSN 6110-01-439-8224
NSN 5998-01-543-7590
NSN 5920-00-125-7757
NSN 6685-00-141-4300
NSN 6240-00-304-7015
NSN 6220-01-155-2357
NSN 2925-01-573-1067
NSN 5855-01-218-3735