Rockwell c35-40 hardness; 1.482-1.493 inch thickness; 19.825-19.835 inch od; 101 blade slots equally spaced around od; 16 0.4205-0.4235 inch holes equally spaced on 8 inch centerline radius; 16 0.437-0.440 inch holes equally spaced on 8.0 inch 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 6105-01-426-1852
NSN 5915-01-086-2283
NSN 7035-01-604-6735
NSN 6220-01-516-4926
NSN 6610-01-408-9557
NSN 5985-01-653-5873
NSN 5935-01-528-6332
NSN 5905-01-555-8077
NSN 2925-01-359-4027
NSN 6135-00-973-5632
NSN 5998-01-246-0040
NSN 6320-00-790-4844