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 6685-00-532-9266
NSN 5975-00-785-9288
NSN 6320-01-486-8004
NSN 6145-01-448-0832
NSN 5950-00-556-0234
NSN 5905-00-021-2244
NSN 5996-01-241-3156
NSN 6150-01-096-8748
NSN 6220-01-169-4782
NSN 6610-00-021-2259
NSN 5935-01-604-5196
NSN 5905-00-491-9584