Thank you for taking an interest in the NSN 5320-01-333-6496 supplies and listing resources that we provide on Integrated Military Parts. At the top of this page, you will find an overview of NSN 5320-01-333-6496, including details on its associated item name, Federal Supply Group, Federal Supply Class, and more. You can also review a list of all manufacturers that our stock traces back to, each serving as a link to expanded catalogs if you wish to further your search.
Underneath our overview, part numbers like HLT115-14-20, and others that belong to our NSN 5320-01-333-6496 inventory have been listed out for your perusal. If any are of interest to you, click on the “RFQ” button to its right to access a quote request form. By filling out and submitting a form with detailed information on your requirements and expectations, you will be able to secure fully customized quotes for your comparisons. You can rest assured that you will receive highly competitive options when you shop on Integrated Military Parts, our staff working tirelessly to ensure streamlined fulfillment and satisfaction. Knowing how we intend to serve you, continue perusing solutions on this catalog and reach out as soon as you are ready.
Item Name | Pin Rivet |
Federal Supply Group (FSG) | Hardware and Abrasives |
Federal Supply Class (FSC) | 5320 Rivets |
National Item Identification Number (NIIN) | 01-333-6496 (013336496) |
NCB Code | USA (01) |
Manufacturer | Huck International Inc, Lisi Aerospace Canada Corp, Sps Technologies Inc, Alcoa Global Fasteners Inc, Hi Shear Corporation |
Part Number | Manufacturer | Item Name | Cage Code | RFQ |
---|---|---|---|---|
HLT115-14-20 | huck international inc | pin rivet | 97928 | RFQ |
HLT115-14-20 | lisi aerospace canada corp | pin rivet | l4528 | RFQ |
HLT115-14-20 | sps technologies inc | pin rivet | 56878 | RFQ |
HLT115-14-20 | alcoa global fasteners inc | pin rivet | 92215 | RFQ |
HLT115-14-20 | hi shear corporation | pin rivet | 73197 | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AASB | FASTENER LENGTH | 1.875 INCHES MINIMUM AND 1.895 INCHES MAXIMUM |
AAZF | SHANK STYLE | PIN-RIVET,STRAIGHT,THREADED |
AAZG | HEAD MAJOR DIAMETER | 0.6620 INCHES MINIMUM AND 0.6680 INCHES MAXIMUM |
CQSX | SHEAR STRENGTH | 108000 SINGLE POUNDS PER SQUARE INCH |
MATT | MATERIAL | STEEL COMP E4340 OVERALL OR STEEL COMP 4140 OVERALL OR STEEL COMP 8740 OVERALL |
SFTT | SURFACE TREATMENT | CADMIUM OVERALL AND CHROMATE OVERALL |
THSD | THREAD SERIES DESIGNATOR | UNJF |
AATB | WIDTH BETWEEN FLATS | 0.1895 INCHES MINIMUM AND 0.1930 INCHES MAXIMUM |
AAZE | SHANK DIAMETER | 0.4360 INCHES MINIMUM AND 0.4370 INCHES MAXIMUM |
ABAJ | LUBRICATION | CETYL ALCOHOL,SPEC 305,HI-SHEAR CORP |
CQBC | MINIMUM TENSILE STRENGTH | 180000 POUNDS PER SQUARE INCH |
CQJX | NOMINAL THREAD SIZE | 0.438 INCHES |
CRSQ | COUNTERSINK ANGLE | 100.0 DEGREES NOMINAL |
AASK | HEAD STYLE | CROWN COUTERSUNK GREATER THAN 135 DEGREES |
ANEE | GRIP LENGTH | 1.245 INCHES MINIMUM AND 1.260 INCHES MAXIMUM |
AAJD | THREAD CLASS | 3A |
AAJF | THREAD DIRECTION | RIGHT-HAND |
CMLP | THREAD QUANTITY PER INCH | 20 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-5000 MIL SPEC 1ST MATERIAL RESPONSE OVERALL OR MIL-S-5626 MIL SPEC 2ND MATERIAL RESPONSE OVERALL OR MIL-S-6049 MIL SPEC 3RD MATERIAL RESPONSE OVERALL |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TY 2,CL 2 FED SPEC SINGLE TREATMENT RESPONSE OVERALL |
Relevant Components for NSN - 5320-01-333-6496, 5320013336496 | ||||
5310-01-700-1085 (5310017001085) | 5306-01-481-1969 (5306014811969) | 5330-01-418-6684 (5330014186684) | 5330-01-089-1590 (5330010891590) | |
5330-01-511-3821 (5330015113821) | 5340-01-713-8703 (5340017138703) | 5310-00-847-3836 (5310008473836) | 5330-00-057-7715 (5330000577715) | |
5310-01-054-4652 (5310010544652) | 5330-01-692-4926 (5330016924926) | 5310-00-725-1363 (5310007251363) | 5310-00-291-2740 (5310002912740) | |
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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