9.215 in. Lg, 14.580 min 14.584 max in. Dia, 102 dovetail slots eq sp
A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the rotor, compressor, aircraft gas turbine engine and/or the rotor, fan, aircraft gas turbine engine through a shaft, turbine, aircraft gas turbine engine. It consists of disks, blades, hubs, and the like. It is the moving part of a turbine assembly, aircraft gas turbine engine. It has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5855-01-424-1090
NSN 5930-00-646-5232
NSN 5999-01-270-7810
NSN 6650-01-025-7425
NSN 5930-01-391-9730
NSN 6240-01-461-9635
NSN 7035-01-361-8821
NSN 5960-00-946-7767
NSN 7035-01-601-7936
NSN 5835-01-624-5666
NSN 5990-01-029-0868
NSN 5920-00-170-4247