Thank you for taking an interest in the Rivet Solid NSN parts that we carry here on Buy Military Ground Vehicle Parts. You have reached the RFQ page for part number MIL-R-5674, an item that traces back to the manufacturer National Aerospace Standards Com. Listed with NSN 5320012955748, this listing is available for purchase from our website at any time. If you are interested in part number MIL-R-5674 and wish to learn more, be sure to fill out and submit the RFQ form found on this page. By presenting us information such as your target price and expected delivery date, we can best formulate and present a solution that closely caters to your unique needs and restrictions alike.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5320-01-295-5748 Item PartTypeName: RIVET,SOLID | 5320 | 012955748 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
MIL-R-5674 | 5 | 1 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AAPC | IDENTIFICATION CODE COLOR | YELLOW |
AASB | FASTENER LENGTH | 0.583 INCHES MINIMUM AND 0.603 INCHES MAXIMUM |
AASK | HEAD STYLE | UNIVERSAL |
AASU | HEAD HEIGHT | 0.080 INCHES MINIMUM AND 0.090 INCHES MAXIMUM |
AAZE | SHANK DIAMETER | 0.186 INCHES MINIMUM AND 0.191 INCHES MAXIMUM |
AAZF | SHANK STYLE | STRAIGHT W/RADIUS CHAMFERED TIP |
AAZG | HEAD MAJOR DIAMETER | 0.356 INCHES MINIMUM AND 0.394 INCHES MAXIMUM |
CQSX | SHEAR STRENGTH | 26000 SINGLE POUNDS PER SQUARE INCH |
HEAT | HEAT TREATMENT | T-4 SOLUTION HEAT TREATED OVERALL |
MATT | MATERIAL | ALUMINUM ALLOY 2117 OVERALL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-430,T4 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
SFTT | SURFACE TREATMENT | CHROMATE OVERALL |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-C-5541 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
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