Special Features:

Wmaterial steel per ams 5365; 2.011 in long; vanes 6.495 in. Min and 6.505 in. Max od tapered to 4.428 in. Min and 4.434 in. Max dia; bore 1.0007 in. Min and 1.0009 in max diameter for forst stage; per af to. 2g-gtp70-24, fig 14, index 84

Properties:

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, nonaircraft gas turbine engine and/or the rotor, fan, nonaircraft gas turbine engine through a shaft, turbine, nonaircraft gas turbine engine. It consists of disks, blades, hubs, and the like. It is the moving part of a turbine assembly, nonaircraft gas turbine engine. It has facilities for attaching to a shaft, turbine, nonaircraft gas turbine engine.