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2840-01-184-0238

Aircraft Gas Turbine Engine Turbine Rotor

2840011840238 011840238 2184181 2183945 641955 716124

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. View more Aircraft Gas Turbine Engine Turbine Rotor

2840-01-184-0238 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840011840238 011840238

Managed by United States
NSN Created on 12 Jul 1984
Data Last Changed
November 2023
NATO Update Count
12
NATO Data Quality
2840-01-184-0238 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840011840238 011840238 1/1
NSN 2840-01-184-0238 (Generic Image) 1/1

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2184181 2183945 641955 716124 A single or multistage assembly designed to receive thermal energy from
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2840-01-184-0238 Demil Restrictions 2840-01-184-0238

DEMIL: C | DEMILI: | CRITICALITY: Y | HMIC: N | PMIC: A | EDC: | ADPEC:

2840-01-184-0238 is a Aircraft Gas Turbine Engine Turbine Rotor that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. This item is a US Munitions List or Commerce Control List Item where key elements must be removed and destroyed to prevent this item being restored or repaired. Only authorized parties may possess this item. This item is not suspected to be hazardous. This item does not contain a precious metal.

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