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Aircraft Gas Turb Compressor Hub NSN 2840-01-458-2759

Item Description

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.

NSN 2840-01-458-2759 NSN: 2840-01-458-2759

Features and Characteristics

Overall Length
12.726 inches
Diameter
Between 16.741 inches and 16.743 inches
End Application
Tf-33 aircraft gas turbine engine
Design Type
Axial compressor
Criticality Code Justification
Feat and abhp and abmz and czbj
Engine Section Location
Compressor
Special Features
P/n not to be procured; p/n taken off engine and put into supply then reworked up to p/n 753538 (01-160-6504); depending on repair it will get assigned a different p/n; if this p/n has cracks in the tie rod holes will be assigned p/n 784473; if this item has nocracks, is reworked to p/n 774659
Material
Steel
Material Specification
Ams6415 assn standard single material response
Reference Data And Literature
T.O. 2j-tf33-34, fig 6, ind 51
FSC
2840 Prime Moving; And Components Aircraft Gas Turbines And Jet Engines
NIIN
014582759
NSN
2840014582759

Manufacturer Part Numbers

Part numbers registered to this national stock number.
Part Number
Cage
Status
MSDS
Part Number:
635498
Cage Code:
77445
Status:
A
MSDS:

Foreign Trade & Schedule B

What is a Schedule B number? Find more information at help.cbp.gov
  • Schedule B Number: 8411997050
  • NAICS: 336412
  • SITC: 71499
  • Description: Parts of gas turbine aircraft engines, other than for use in civil aircraft
  • End Use (Code 50020):
    Engines and turbines for military aircraft

Q & A

Frequently asked questions for NSN 2840-01-458-2759
What are the manufacturers of nsn 2840014582759?
Does this nsn 2840014582759 have a shelf life?
No. This NSN does not have an applicable shelf life.
What is the formal definition of nsn 2840014582759
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.
Does nsn 2840014582759 contain any precious metals?
No precious metal content.
Does nsn 2840014582759 contain any hazardous materials?
No MSDS. No hazardous material.
What is the ESD classification of nsn 2840014582759?
No known electrostatic discharge.

Identification Group

Item Identification Guide (IIG) and Item Name Code (INC)
INC
FIIG
App. Key
Cond. Code
Status
INC:
50573
FIIG:
A10700
App. Key:
G
Cond. Code:
1
Status:
A

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