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Aircraft Gas Turb Compressor Hub

Model / MPN: 4047224 | NSN: 2840-01-033-9081
ITAR Registered seal

A component of a rotor, compressor, aircraft gas turbine engine. it is designed to attach to the front and/or rear of the rotor providing support, alignment, and a means of attachment for a shaft, turbine, aircraft gas turbine engine. it may have provisions for installing bearings, and/or oil and air seals. see also disk and hub, compressor, aircraft gas turbine engine.

Product Details
NATO Stock Number
2840-01-033-9081
Sold in multiples of
1 EA
DEMIL
DEMIL/MLI
Overall Length
Between 4.004 inches and 4.014 inches
Diameter
Between 7.162 inches and 7.166 inches
End Application
F100-pw-100 aircraft engine
Design Type
Compressor
Criticality Code Justification
Feat
Part Name Assigned By Controlling Agency
Orig name nut, plain, round
Engine Section Location
Compressor
Stage Number
2
Material
Nickel alloy hub
Material Specification
Pwa1022 mfr ref single material response hub

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4047224 Cross Reference