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2840-01-209-5841

Aircraft Gas Turbine Engine Compressor Rotor

2840012095841 012095841 8513697

A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. It consists of disks, blades, hubs, and the like. It is the moving part of COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Compressor Rotor

2840-01-209-5841 ROTOR,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840012095841 012095841

Managed by United States
NSN Created on 1 Jun 1985
Data Last Changed
November 2023
NATO Update Count
9
NATO Data Quality
2840-01-209-5841 ROTOR,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE 2840012095841 012095841 1/1
NSN 2840-01-209-5841 (Generic Image) 1/1

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8513697 A single or multistage assembly designed to deliver air at the proper pressure, direction and
United States (US) 4. 2840-01-209-5841 Marketplace Restrictions Approved Sources Datasheet Management
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2840-01-209-5841 Demil Restrictions 2840-01-209-5841

DEMIL: C | DEMILI: | CRITICALITY: Y | HMIC: N | PMIC: A | EDC: | ADPEC: 0

2840-01-209-5841 is a Aircraft Gas Turbine Engine Compressor 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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