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Aircraft Gas Turb Compressor Hub

Model / MPN: 9084M40P01 | NSN: 2840-01-144-2473
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
2840-01-144-2473
Sold in multiples of
1 EA
DEMIL
NO
Overall Length
Between 1.100 inches and 1.140 inches
Overall Width
Between 0.860 inches and 0.920 inches
Material Thickness
0.185 inches
End Application
Aircraft eng tf-39
Design Type
Compressor
Criticality Code Justification
Apgf and czbj and abhp and abmk and abpx
Engine Section Location
Compressor
Material
Steel hub
Material Specification
B50tf14, cl-a mfr ref 1st material response hub

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9084M40P01 Cross Reference