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| Mfg Part Number: 2 121 051 08 | Alternate P/N: 212105108 | NSN : 2840-00-779-3854 |
| NIIN : 007793854 | CAGE Code : 99193 | Manufacturer: Honeywell International Inc |
| Item Name : Disk And Hub Turbin | FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
Aviation Gamut, owned and operated by ASAP Semiconductor, is an all-inclusive purchasing platform for hard-to-find and in-demand parts 2 121 051 08 and components pertaining to the civil aviation, defense, aerospace, industrial, and electronic markets. An NSN is a 13-digit numeric code that serves to identify 'standardized material items of supply' as they have been recognized by all NATO countries and the United States Department of Defense. As such, we have an inventory of more than two billion new and obsolete parts, among which is an unparalleled selection of NSN parts and much more. This includes items such as Disk And Hub Turbin 2 121 051 08 from manufacturer Honeywell International Inc and many more, all of which are available with short lead times and competitive prices. For NSN parts, Aviation Gamut is the ultimate source.
Our website offers a number of parametric search capabilities, one of which allows you to search specifically for 2 121 051 08. This means you can quickly sort through National Stock Numbers such as 2840007793854 and find parts from quality manufacturers like Honeywell International Inc and many others. To begin the purchasing process immediately, submit an RFQ today. Our team of dedicated account managers is standing by and will respond to all inquiries in 15 minutes or less.
| MRC | Criteria | Characteristic |
|---|---|---|
| FEAT | SPECIAL FEATURES | CRES,M3603,FSCM 91547,ROCKWELL A SCALE 69 MIN,73 MAX HARDNESS,10.370 IN. MIN,10.380 IN. MAX O/A DIA,3.915 IN. MIN,3.925 IN. MAX O/A W,80 BLADE GROOVES EQUALLY SPACED,INTERNALLY SPLINED HUB,106 TEETH,30 DEG PRESSURE ANGLE,3.3125 IN. PITCH DI |
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We Hope that You Will Visit Us Again the Next Time You Need NSN Parts and Make Us Your Strategic Purchasing Partner.
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