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 BACR15BB5D4, an item that traces back to the manufacturer The Boeing Company. Listed with NSN 5320001176771, this listing is available for purchase from our website at any time. If you are interested in part number BACR15BB5D4 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 |
---|---|---|---|---|---|---|
5320-00-117-6771 Item PartTypeName: RIVET,SOLID | 5320 | 001176771 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
MS20470D5-4 | 2 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
AASB | FASTENER LENGTH | 0.240 INCHES MINIMUM AND 0.260 INCHES MAXIMUM |
AASK | HEAD STYLE | UNIVERSAL |
AASU | HEAD HEIGHT | 0.067 INCHES MINIMUM AND 0.077 INCHES MAXIMUM |
AAZE | SHANK DIAMETER | 0.155 INCHES MINIMUM AND 0.160 INCHES MAXIMUM |
AAZF | SHANK STYLE | STRAIGHT |
AAZG | HEAD MAJOR DIAMETER | 0.296 INCHES MINIMUM AND 0.328 INCHES MAXIMUM |
ANEE | GRIP LENGTH | 0.006 INCHES MINIMUM AND 0.026 INCHES MAXIMUM |
CQSX | SHEAR STRENGTH | 33000 SINGLE POUNDS PER SQUARE INCH |
MATT | MATERIAL | ALUMINUM ALLOY 2017 OVERALL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-430 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
SFTT | SURFACE TREATMENT | ANODIZE OVERALL OR OXIDE FILM OVERALL |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625 MIL SPEC 1ST TREATMENT RESPONSE OVERALL OR MIL-C-5541 MIL SPEC 2ND 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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