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 5996-01-381-1997
NSN 6145-00-141-8095
NSN 6135-01-231-0444
NSN 6240-00-698-3137
NSN 6240-01-502-7883
NSN 5998-01-612-6143
NSN 6105-00-068-7195
NSN 5905-01-429-8810
NSN 5930-01-614-4035
NSN 6685-00-651-9518
NSN 6220-01-338-2062
NSN 5996-01-391-4529