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 5950-01-386-7069
NSN 6610-00-841-8221
NSN 5990-01-304-7597
NSN 5855-01-461-9207
NSN 6620-01-504-5756
NSN 6150-00-952-2766
NSN 7035-01-029-7221
NSN 6320-00-004-9158
NSN 6150-00-147-3680
NSN 5930-00-724-8129
NSN 6685-01-571-4039
NSN 6685-00-754-4111