2840-01-476-6468

Aircraft Gas Turbine Engine Turbine Rotor

2840014766468 014766468 815967

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

2840-01-476-6468 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014766468 014766468

Managed by United States
NSN Created on 18 Jul 2000
Data Last Changed
November 2023
NATO Update Count
4
NATO Data Quality
2840-01-476-6468 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014766468 014766468 1/1
NSN 2840-01-476-6468 (Generic Image) 1/1

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2840-01-476-6468 Related Documents Related Documents 2840-01-476-6468 5+ Documents (More...)

Documents 2840-01-590-6515 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/us 2840-01-476-6468
2003 2840-01-590-6515 Avis Assy 220 Core 201045038-10RNCC: 3 | RNVC: 2 | DAC: 5 14 Dec 2010 2840-01-476-6468
9476 Aircraft Gas Turbine Engine Turbine Rotor 9995M27G11RNCC: 3 | RNVC: 2 | DAC: 4 26 Nov 2002 2840-01-476-6468
5340-00-245-7738 5340002457738 002457738 is a preformed item of rigid or semirigid material designed to partially surround other items such as cable(s), conduit(s), pipe(s), tube(s), or rod(s) or to completely surround them by means of a bridge strap(s) (which does not tightly clamp against the complete periphery). it is designed to retain and/or position the items close to a structure. it may be fastened to the structure on one end, both ends, or in the center. see also clamp, loop. excludes bracket, pipe; strap, leather and strap, webbing.
CAGE 46MS2 Gtd Inc. in Rockford, IL United States

2840-01-476-6468 Demil Restrictions 2840-01-476-6468

DEMIL: Q | DEMILI: 3 | CRITICALITY: Y | HMIC: N | PMIC: A | EDC: | ADPEC: 0

2840-01-476-6468 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 has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a confirmed Commerce Control List Item (CCLI). This item is not suspected to be hazardous. This item does not contain a precious metal.

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