Steel, ams 6415, rockwell c35-40 hardness, 3.210-3.221 in. Thk, 19.825-19.835 in. Od, 6.995-7.005 in. Id, 27 blade slots equally spacedaround od, sixteen 0.437-0.440 in. Holes equally spaced on 8.000 in.Centerline radius, thirty-two 0.101-0.113 in. Holes equally spaced on7.260 in. Centerline radius, thirty-two scallops equally spaced on 7.260in. 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 6320-01-592-6248
NSN 4140-00-944-2557
NSN 6135-00-575-8942
NSN 5960-00-211-2105
NSN 6620-00-829-1860
NSN 5910-01-603-4402
NSN 4140-01-166-0028
NSN 5930-01-088-6920
NSN 4140-01-461-2350
NSN 5925-00-515-2438
NSN 5835-01-143-9143
NSN 6130-01-471-2591