2840-00-414-6888
Turbine Engine Axial-Centrifugal Compressor Rotor
2840004146888 004146888 3019921
Managed by United States
NSN Created on 9 Nov 1970
Data Last Changed
November 2023
November 2023
NATO Update Count
6
6
NATO Data Quality
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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.
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2910-12-301-9921 Engine Accessory Bracket 2910123019921
2910-12-301-9921 2910123019921 123019921 is a bracket specifically designed for the purpose of mounting and supporting miscellaneous accessories. excludes adjusting arms.
2820-00-301-9921 2820003019921 003019921
4020-99-301-9921 4020993019921 993019921 ROPE,FIBROUS
Restrictions 2840-00-414-6888
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.
Approved Sources 2840-00-414-6888
- Part Number
- Manufacturer
- Status
- 3019921
- Manufacturer
- 00198 - Pratt & Whitney Canada Cie (Active)
- Primary Buy
- Primary Buy
NATO Stock Numbers Related to 2840-00-414-6888
2840-15-060-2176 2840-15-061-3579 2840-15-060-2124 2840-15-060-2166 2840-15-061-3577 2840-15-060-2171 2840-15-061-3573 2840-15-060-2194 2840-00-032-2784 2840-15-060-2181 2840-15-060-2123 2840-15-060-2126 2840-15-061-3561 2840-15-060-2191 2840-15-061-3592 2840-15-061-3542 2840-15-061-3557 2840-15-060-2184