2840-01-422-1606

Aircraft Gas Turbine Engine Turbine Rotor

2840014221606 014221606 167310-200A

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

2840-01-422-1606 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014221606 014221606

Managed by United States
NSN Created on 16 Apr 1997
Data Last Changed
November 2023
NATO Update Count
4
NATO Data Quality
2840-01-422-1606 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014221606 014221606 1/1
NSN 2840-01-422-1606 (Generic Image) 1/1

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2840-01-422-1606 Demil Restrictions 2840-01-422-1606

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

2840-01-422-1606 is a Aircraft Gas Turbine Engine Turbine Rotor This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.

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