Thank you for taking interest in Boeing Company The part number ST3M861V06B5, which is listed with the NSN 5320-01-475-9166 and a product description of “Pin Rivet.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5320-01-475-9166 Item PartTypeName: PIN-RIVET | 5320 | 014759166 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
ST3M861V06B5 | 5 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
AASK | HEAD STYLE | FLUSH COUNTERSUNK |
AAZE | SHANK DIAMETER | 0.189 INCHES MINIMUM AND 0.190 INCHES MAXIMUM |
AAZF | SHANK STYLE | STUMP |
AAZG | HEAD MAJOR DIAMETER | 0.293 INCHES MINIMUM AND 0.305 INCHES MAXIMUM |
ABAJ | LUBRICATION | DRY FILM OR SOLID FILM AND CETYL ALCOHOL |
AGAV | END ITEM IDENTIFICATION | F-18 HORNET |
ANEE | GRIP LENGTH | 0.313 INCHES NOMINAL |
CRSQ | COUNTERSINK ANGLE | 99.0 DEGREES MINIMUM AND 101.0 DEGREES MAXIMUM |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | PIN, RIVET, FROOVED, 100 DEG C SUNK HEAD, SHEAR, LOCKBOLT, STUMP TYPE, TITANIUM, 95 KSI |
FEAT | SPECIAL FEATURES | TPROCUREMENT SPECIFICATION NAS 621;RADIUS TO BE TANGENT TO SHANK AT 18.5 DEGREE ANGLE;DIMENTIONS BEFORE LUBRICATION;LOCKING GROOVES TO BE GROUND OR ROLLED AT MANUFACTURERES OPTION;CONICAL SURFACE OF HEAD TO SHANK WITHIN .003 TIR |
MATT | MATERIAL | TITANIUM OVERALL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | NAS621 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
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