AF1090O1E6C6 by Allfast Fastening Systems Inc with NSN 5320014681680 - Submit a Quote
Part No. : AF1090O1E6C6 | Manufacturer : Allfast Fastening Systems Inc | NSN : 5320-01-468-1680 |
Item Name : Rivet Solid | CAGE Code : 53551 | FSC : 5320 Rivets |
ASAP Aviation Procurement is pleased to announce that part number AF1090O1E6C6 of NSN 5320014681680 is now available and in stock. We can get you one of the fastest and most competitive quotes on this part. Part number AF1090O1E6C6 is a rivet solid manufactured by allfast fastening systems inc under CAGE Code 53551. Simply fill out the Request for Quote (RFQ) form provided here to get started on your quote.In order to make sure that we get you your quote in a timely manner, please take the time to make sure that all fields are completely filled out, particularly the asterisk-marked (*) fields like Parts Needed By and Quantity (ea).
We will be using your response to these fields to calculate your quote. Within 15 minutes of receiving your RFQ, a member of our sales team will contact you with your quote. ASAP Aviation Procurement, owned and operated by ASAP Semiconductor, is a leading distributor of new and obsolete NSN parts for the aerospace, civil aviation, and defense industries. With our inventory of more than 2 billion parts sourced from over 5000 manufacturers from around the world, we do our level best to become your go-to one-stop shop. And to help us offer you the best streamlined parts procurement experience, we have advanced shipping facilities across USA. AF1090O1E6C6 allfast fastening systems inc is in stock.
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NSN Information for Part Number AF1090O1E6C6 with NSN 5320-01-468-1680, 5320014681680
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5320-01-468-1680 Item Description: Rivet Solid | 5320 | 014681680 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
Af1090o1e6c6 | 5 | 2 | 3 |
Characteristics Data of NSN 5320-01-468-1680, 5320014681680MRC Criteria Characteristic AASB Fastener Length 0.375 INCHES NOMINAL AAZG Head Major Diameter 0.257 INCHES MINIMUM AND 0.263 INCHES MAXIMUM AAZE Shank Diameter 0.187 INCHES MINIMUM AND 0.191 INCHES MAXIMUM SFTT Surface Treatment ANODIZE OVERALL AND ALUMINUM OVERALL AGAV End Item Identification C-17 AIRCRAFT MDCL Material Document And Classification QQ-A-430 FED SPEC SINGLE MATERIAL RESPONSE OVERALL AASK Head Style OVAL COUNTERSUNK CXCY Part Name Assigned By Controlling Agency RIVET,SOLID-100 DEGREE FLUSH CROWN SHEAR HEAD MATT Material ALUMINUM ALLOY 7050 OVERALL AAZF Shank Style STRAIGHT W/RADIUS CHAMFERED TIP FEAT Special Features DEBURR AND BREAK ALL EDGES .005-.015;.001 SHANK DIAMETER INCREASE PERMISSABLE WITHIN 100 OF BASE OF HEAD;HEAD COCKING ANGLE OF RIVET HEAD RELATIVE TO AXIS OF RIVET 1/2IN MAX;APPROXIMATE MATERIAL FOR FULL UPSET OF HEAD;CLOSED DIE CONFIGURATION REQUIRED;NO SHARP EDGES OR BURRS ON RIVET;DIMENTIONS APPLY AFTER COATING STDC Surface Treatment Document And Classification MIL-A-8625,TYPE1,CLASS1 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL CRSQ Countersink Angle 99.0 DEGREES MINIMUM AND 101.0 DEGREES MAXIMUM MRC Decoded Requirement Clear Text Reply
MRC | Criteria | Characteristic |
---|---|---|
AASB | Fastener Length | 0.375 INCHES NOMINAL |
AAZG | Head Major Diameter | 0.257 INCHES MINIMUM AND 0.263 INCHES MAXIMUM |
AAZE | Shank Diameter | 0.187 INCHES MINIMUM AND 0.191 INCHES MAXIMUM |
SFTT | Surface Treatment | ANODIZE OVERALL AND ALUMINUM OVERALL |
AGAV | End Item Identification | C-17 AIRCRAFT |
MDCL | Material Document And Classification | QQ-A-430 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
AASK | Head Style | OVAL COUNTERSUNK |
CXCY | Part Name Assigned By Controlling Agency | RIVET,SOLID-100 DEGREE FLUSH CROWN SHEAR HEAD |
MATT | Material | ALUMINUM ALLOY 7050 OVERALL |
AAZF | Shank Style | STRAIGHT W/RADIUS CHAMFERED TIP |
FEAT | Special Features | DEBURR AND BREAK ALL EDGES .005-.015;.001 SHANK DIAMETER INCREASE PERMISSABLE WITHIN 100 OF BASE OF HEAD;HEAD COCKING ANGLE OF RIVET HEAD RELATIVE TO AXIS OF RIVET 1/2IN MAX;APPROXIMATE MATERIAL FOR FULL UPSET OF HEAD;CLOSED DIE CONFIGURATION REQUIRED;NO SHARP EDGES OR BURRS ON RIVET;DIMENTIONS APPLY AFTER COATING |
STDC | Surface Treatment Document And Classification | MIL-A-8625,TYPE1,CLASS1 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL |
CRSQ | Countersink Angle | 99.0 DEGREES MINIMUM AND 101.0 DEGREES MAXIMUM |
MRC | Decoded Requirement | Clear Text Reply |
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