Special Features:

Material is a crystal rene n6, a precipitation strengthened alloy; rotor has a new redesigned stg 1 blade with the new material; increased life of blade; blades are still dovetail and are identical to the old configuration p/n 1475m47p01; new blades are interchangeable in complete sets only; intermixing of blades, old and new, will notbe allowed; since dovetails are identical and will fit in the same disk, no changes to disk

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, 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.