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2840-01-493-9814

Aircraft Gas Turbine Engine Turbine Rotor

2840014939814 014939814 5056T83G25

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

2840-01-493-9814 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014939814 014939814

Managed by United States
NSN Created on 28 Jan 2002
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-01-493-9814 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014939814 014939814 1/1
NSN 2840-01-493-9814 (Generic Image) 1/1

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2840-01-493-9814 Demil Restrictions 2840-01-493-9814

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

2840-01-493-9814 is a Aircraft Gas Turbine Engine Turbine Rotor that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. 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.

2840-01-493-9814 HTS and ScheduleB Import and Export 2840-01-493-9814

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Spain (YB01)
Effective Date:
1 Jan 2002

2840-01-493-9814 Manufacturers Approved Sources 2840-01-493-9814

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2840-01-493-9814 has freight characteristics.. 2840-01-493-9814 has a variance between NMFC and UFC when transported by rail and the description should be consulted.