Mfg Part Number: 6898782 | NSN : 2840-01-076-5887 | NIIN : 010765887 |
CAGE Code : 63005 | Manufacturer: Rolls Royce Corp | Item Name : Rotor Turbine Aircr |
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 6898782 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 Rotor Turbine Aircr 6898782 from manufacturer Rolls Royce Corp 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 6898782. This means you can quickly sort through National Stock Numbers such as 2840010765887 and find parts from quality manufacturers like Rolls Royce Corp 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.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-076-5887 Item Description: Rotor Turbine Aircr | 2840 | 010765887 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
6898782 | 1 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | T63-A-700 AND T63-A-720 ENGINES |
CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |
FEAT | SPECIAL FEATURES | CRES EMS73649-2,FSCM 73342,48 BLADES EQUALLY SPACED ON OUTER PERIPHERY,6.409 IN. MIN,6.411 IN. MAX OD,EXTERNAL SPLINE,17 TEETH,0.562 IN. MIN,0.567 IN. MAX OD,0.5313 IN. NOM PITCH DIA,30 DEG PRESSURE ANGLE,EXTERNAL THD,0.8438 IN.-32 UNJS CLA |
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