2840-00-414-6888

Turbine Engine Axial-Centrifugal Compressor Rotor

2840004146888 004146888 3019921

2840-00-414-6888 COMPRESSOR ROTOR,AXIAL-CENTRIFUGAL,TURBINE ENGINE 2840004146888 004146888

Managed by United States
NSN Created on 9 Nov 1970
Data Last Changed
November 2023
NATO Update Count
6
NATO Data Quality
2840-00-414-6888 COMPRESSOR ROTOR,AXIAL-CENTRIFUGAL,TURBINE ENGINE 2840004146888 004146888 1/1
NSN 2840-00-414-6888 (Generic Image) 1/1

2840-00-414-6888 Stock and Availability Marketplace 2840-00-414-6888

Need Help?
Request a Quotation from participating marketplace vendors
eBay Updated Every Day
2840-00-414-6888 RQST NE eBay
eBay Updated Every Day
2840-00-414-6888 RQST eBay
Amazon Updated Every Day
2840-00-414-6888 RQST NE Amazon

2840-00-414-6888 Related Documents Related Documents 2840-00-414-6888 5+ Documents (More...)

3040-01-301-9921 3040013019921 013019921 is a shaft having two or more different diameters (greater than 0.031 inches (0.79 millimeter)) along its length. it must have one or more of the following conditions: a specified surface finish designation in the range 1 to 125 microinches (0.025 to 3.2 micrometers) arithmetical average (aa), machined peripheral flat(s), circular groove(s), keyway(s), splines, threads, or holes. the ends and/or shoulders may be machined to accommodate bearings, couplings, and the like. it is not designed for use in aligning by fitting into corresponding holes of another item. for items used to support rotating members see axle(1), shouldered. for items not having any of the above conditions see pin, shoulder, headless. excludes shaft(1), straight; and axle(1), straight.
6220-14-301-9921 6220143019921 143019921 is a light specifically designed to be permanently installed in aircraft for map reading or cockpit illumination. it may contain dimming features, switches, filters, and/or cables or coiled cables to permit portability within the length of the cable. if provided with cables or coiled cables, the mounting base must remain fixed to the aircraft and include a snap-in or similar locking device to permit detachment and attachment of the light. for items that supply general illumination for other compartments of an aircraft, see light, dome. excludes light (1), extension.
2910-12-301-9921 2910123019921 123019921 is a bracket specifically designed for the purpose of mounting and supporting miscellaneous accessories. excludes adjusting arms.

2840-00-414-6888 Demil Restrictions 2840-00-414-6888

DEMIL: C | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: U | EDC: | ADPEC:

2840-00-414-6888 is a Turbine Engine Axial-Centrifugal Compressor 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 a US Munitions List or Commerce Control List Item where key elements must be removed and destroyed to prevent this item being restored or repaired. Only authorized parties may possess this item. This item is not suspected to be hazardous. The precious metals content of this item is unknown.

2840-00-414-6888 Manufacturers Approved Sources 2840-00-414-6888

2840-00-414-6888 Related Items NATO Stock Numbers Related to 2840-00-414-6888