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 5999-01-212-8617
NSN 5910-00-543-7687
NSN 6620-01-162-2839
NSN 5905-01-337-7224
NSN 5930-01-268-2971
NSN 6135-01-384-4395
NSN 5835-01-538-8080
NSN 6105-00-141-5598
NSN 6240-00-244-0483
NSN 6135-00-950-2669
NSN 6240-00-698-5822
NSN 5855-00-631-4565