2840-21-869-4400

Aircraft Gas Turbine Engine Turbine Rotor Blade

2840218694400 218694400 615002

An item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the turbine section of an ENGINE, GAS TURBINE, AIRCRAFT. View more Aircraft Gas Turbine Engine Turbine Rotor Blade

2840-21-869-4400 BLADE,TURBINE ROTOR,AIRCRAFT GAS TURBINE ENGINE 2840218694400 218694400

Managed by Canada
NSN Created on 21 Mar 1974
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-21-869-4400 BLADE,TURBINE ROTOR,AIRCRAFT GAS TURBINE ENGINE 2840218694400 218694400 1/1
NSN 2840-21-869-4400 (Generic Image) 1/1

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2840-21-869-4400 Related Documents Related Documents 2840-21-869-4400 5+ Documents (More...)

www.nsnlookup.com /fsg-61/fsc-6110/uk 6110-99-769-9848 https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-21-869-4400
2840218694400 218694400,615002 Documents 2840-21-869-4400 5+ Documents ( More... ) https//www.nsnlookup.com
Documents 5998-99-544-3843 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ca 2840-21-869-4400
2840218694400 218694400,615002 electronic equipment. see also panel, test, electrical. https//www.nsnlookup.com
6110-99-563-2384 6110995632384 995632384 is a panel, upon which are mounted such items as indicator lights, meters, relays, switches and the like, which is specifically designed for the purpose of controlling the operation of electrical and electronic equipment. see also panel, test, electrical.
5940-15-101-6315 5940151016315 151016315 is two or more terminal boards having a common mounting or mounted on each other.
4820-98-857-1926 4820988571926 988571926 is a spherical shaped device with two or more ports used to prevent or regulate the flow of fluids in a valve, nozzle, or the like. it may include an integral valve stem. for valve balls that do not include ports see ball, check. excludes plug, rotary, valve.

2840-21-869-4400 Demil Restrictions 2840-21-869-4400

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

2840-21-869-4400 is a Aircraft Gas Turbine Engine Turbine Rotor Blade

2840-21-869-4400 End Users End Users 2840-21-869-4400

Canada (ZC)

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