2840-14-322-2335

Aircraft Gas Turbine Engine Turbine Rotor Blade

2840143222335 143222335 501-540-068-0-00B 501-540-068-0CL2

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

2840-14-322-2335 BLADE,TURBINE ROTOR,AIRCRAFT GAS TURBINE ENGINE 2840143222335 143222335

Managed by France
NSN Created on 1 Jan 1975
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-14-322-2335 BLADE,TURBINE ROTOR,AIRCRAFT GAS TURBINE ENGINE 2840143222335 143222335 1/1
NSN 2840-14-322-2335 (Generic Image) 1/1

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2840-14-322-2335 Related Documents Related Documents 2840-14-322-2335 5+ Documents (More...)

www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-330-4426 2840143304426 143304426,501-540-200-0-00B 2840-14-322-2335
2840143222335 143222335,501-540-068-0-00B 2840120270418 120270418 320-7921 2840-14-428-6754 031
-428-6747 2840-14-404-0950 330-4426 2840218961351 218961351 320-7921 2840-14-428-6754 322-2335 2840143222335
turbine section of an engine, gas turbine, aircraft. https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-322-2335
2840143222335 143222335,501-540-068-0-00B 2840-14-322-2335 2840143222335 143222335 is an item mounted
Documents 2840-14-330-4426 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-322-2335
2840143222335 143222335,501-540-068-0-00B 2840120270418 120270418 320-7921 2840-14-428-6754 2840
320-7921 2840-14-428-6754 2840-14-031-3722 2840-14-428-6747 2840-14-404-0950 2840-14-330-4426 2840-14-322-2335
2840-14-428-6754 2840-14-031-3722 2840-14-428-6747 https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-322-2335
2840143222335 143222335,501-540-068-0-00B -2840/de 2840-12-027-0418 2840120270418 120270418 320
320-7921 2840-14-428-6754 2840-14-031-3722 2840-14-428-6747 2840-14-404-0950 2840-14-330-4426 2840-14-322-2335
2840-14-031-3722 2840-14-428-6747 2840-14-404-0950 https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-322-2335
2840143222335 143222335,501-540-068-0-00B 027-0418 2840120270418 120270418 320-7921 2840-14-428
320-7921 2840-14-428-6754 2840-14-031-3722 2840-14-428-6747 2840-14-404-0950 2840-14-330-4426 2840-14-322-2335

2840-14-322-2335 Demil Restrictions 2840-14-322-2335

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

2840-14-322-2335 is a Aircraft Gas Turbine Engine Turbine Rotor Blade

2840-14-322-2335 End Users End Users 2840-14-322-2335

France (ZF)

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