Thank you for taking an interest in the NSN 5320-00-687-5076 supplies and listing resources that we provide on Integrated Military Parts. At the top of this page, you will find an overview of NSN 5320-00-687-5076, 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 FFA260-13, NAS1674-4L13, and others that belong to our NSN 5320-00-687-5076 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 | Rivet Blind |
Federal Supply Group (FSG) | Hardware and Abrasives |
Federal Supply Class (FSC) | 5320 Rivets |
National Item Identification Number (NIIN) | 00-687-5076 (006875076) |
NCB Code | USA (00) |
Manufacturer | Custom Craft Products Inc, Monogram Aerospace Fasteners Inc, National Aerospace Standards Com |
MRC | Criteria | Characteristic |
---|---|---|
AASB | FASTENER LENGTH | 1.009 INCHES MINIMUM AND 1.039 INCHES MAXIMUM |
AASK | HEAD STYLE | HEXAGON COUNTERSUNK |
AASU | HEAD HEIGHT | 0.072 INCHES MINIMUM AND 0.079 INCHES MAXIMUM |
AAZE | SHANK DIAMETER | 0.258 INCHES MINIMUM AND 0.260 INCHES MAXIMUM |
AAZF | SHANK STYLE | THREADED SELF-PLUGGING SHANK W/SLEEVE |
ABAF | EXPANSION DEVICE | SERRATED STEM-TYPE W |
ABAJ | LUBRICATION | DRY FILM OR WAX |
ANEE | GRIP LENGTH | 0.781 INCHES MINIMUM AND 0.844 INCHES MAXIMUM |
ASDB | WIDTH ACROSS FLATS | 0.458 INCHES MINIMUM AND 0.472 INCHES MAXIMUM |
CQBC | MINIMUM TENSILE STRENGTH | 180000 POUNDS PER SQUARE INCH |
CQSX | SHEAR STRENGTH | 5300 DOUBLE POUNDS PER SQUARE INCH |
CRSQ | COUNTERSINK ANGLE | 99.0 DEGREES MINIMUM AND 101.0 DEGREES MAXIMUM |
HEAT | HEAT TREATMENT | ANNEALED OVERALL |
MATT | MATERIAL | ALUMINUM ALLOY 7075 BODY |
MATT | MATERIAL | STEEL COMP 303F SLEEVE |
MATT | MATERIAL | STEEL COMP 4130 STEM OR STEEL COMP 8740 STEM OR STEEL COMP 4140 STEM |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5641 ASSN STD SINGLE MATERIAL RESPONSE SLEEVE |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-6758 MIL SPEC 1ST MATERIAL RESPONSE STEM OR MIL-S-6049 MIL SPEC 2ND MATERIAL RESPONSE STEM OR MIL-S-5626 MIL SPEC 3RD MATERIAL RESPONSE STEM |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-282 FED SPEC SINGLE MATERIAL RESPONSE BODY |
SFTT | SURFACE TREATMENT | ANODIZE BODY |
SFTT | SURFACE TREATMENT | CADMIUM SLEEVE |
SFTT | SURFACE TREATMENT | CADMIUM STEM |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625,TY 2 MIL SPEC SINGLE TREATMENT RESPONSE BODY |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TY 1,CL 3 FED SPEC SINGLE TREATMENT RESPONSE SLEEVE |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TY 2,CL 3 FED SPEC SINGLE TREATMENT RESPONSE STEM |
Relevant Components for NSN - 5320-00-687-5076, 5320006875076 | ||||
5305-00-914-4182 (5305009144182) | 5365-01-075-0950 (5365010750950) | 5330-01-399-1658 (5330013991658) | 5330-01-241-5104 (5330012415104) | |
5331-01-617-5941 (5331016175941) | 5330-01-076-2895 (5330010762895) | 5342-01-264-1394 (5342012641394) | 5330-12-315-3724 (5330123153724) | |
5340-00-286-4189 (5340002864189) | 5360-01-293-4181 (5360012934181) | 5305-00-483-9495 (5305004839495) | 5305-12-157-6930 (5305121576930) | |
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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