If your operations demand dependable items that fall under the NSN 5306-01-594-9269, look no further than the expansive product list featured on this page. For your convenience, all NSN 5306-01-594-9269 part numbers that we have in stock like NAS6205-47D, and others are listed below with their respective manufacturer. Should any of these products match your requirements, you may click on the “RFQ” button presented next to each listing to access our online quote request service. By providing our team with information like your desired part quantity, pricing, and fulfillment speed on the form you are directed to, we can offer a procurement solution that best accommodates your needs within 15 minutes of our receipt and review.
You never have to compromise any of your needs when you shop with us, as we always aim to offer competitive pricing and delivery times for every order. Furthermore, quality is a fundamental cornerstone of our operations, and we carry out various practices to guarantee the fit, form, and function of our NSN 5306-01-594-9269 products, starting with strictly sourcing from trustworthy NSN parts suppliers and manufacturers. To learn more about our diverse commitments and see why so many customers steadily depend on our services, connect with us by form, phone, or email at your earliest convenience.
| Item Name | Bolt Shear |
| Federal Supply Group (FSG) | Hardware and Abrasives |
| Federal Supply Class (FSC) | 5306 Bolts |
| National Item Identification Number (NIIN) | 01-594-9269 (015949269) |
| NCB Code | USA (01) |
| Manufacturer | National Aerospace Standards Com |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| NAS6205-47D | national aerospace standards com | bolt shear | RFQ |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAJD | Thread Class | 3A |
| MATT | Material | STEEL COMP 4140 OR STEEL COMP 4340 OR STEEL COMP 8740 OVERALL |
| CQBC | Minimum Tensile Strength | 160000 POUNDS PER SQUARE INCH |
| AATB | Width Between Flats | 0.492 INCHES MINIMUM AND 0.502 INCHES MAXIMUM |
| CMLP | Thread Quantity Per Inch | 24 |
| AASK | Head Style | HEXAGON |
| THSD | Thread Series Designator | UNJF |
| SFTT | Surface Treatment | CADMIUM OVERALL |
| AASA | Thread Length | 0.438 INCHES NOMINAL |
| AAWB | Shank Unthreaded Hole Diameter | 0.076 INCHES MINIMUM AND 0.086 INCHES MAXIMUM ALL HOLES |
| CRZS | Distance From Head Largest Bearing Surface To Shank Hole Center | 3.193 INCHES NOMINAL ALL HOLES |
| STDC | Surface Treatment Document And Classification | AMS-QQ-C-416, TYPE II, CLASS 2 ASSN STD SINGLE TREATMENT RESPONSE OVERALL |
| CXCY | Part Name Assigned By Controlling Agency | BOLT, TENSION, HEX HEAD, CLOSE TOLERANCE, ALLOY STEEL, SHORT THREAD, REDUCED MAJOR THREAD DIA., SELF-LOCKING AND NONLOCKING, 160 KSI FTU |
| ANEE | Grip Length | 2.927 INCHES MINIMUM AND 2.947 INCHES MAXIMUM |
| AHYM | Nominal Thread Diameter | 0.3215 INCHES |
| AAJF | Thread Direction | RIGHT-HAND |
| MDCL | Material Document And Classification | AMS6349 OR AMS6382 ASSN STD 1ST MATERIAL RESPONSE OR AMS6415 OR AMS6484 ASSN STD 2ND MATERIAL RESPONSE OR AMS6322 ASSN STD 3RD MATERIAL RESPONSE OVERALL |
| AASU | Head Height | 0.156 INCHES MINIMUM AND 0.171 INCHES MAXIMUM |
| AASB | Fastener Length | 3.360 INCHES MINIMUM AND 3.390 INCHES MAXIMUM |
| MRC | Decoded Requirement | Clear Text Reply |
| AAUR | Grip Diameter | 0.3110 INCHES MINIMUM AND 0.3120 INCHES MAXIMUM |
| Relevant Components for NSN - 5306-01-594-9269, 5306015949269 | ||||
| 5315-01-193-2252 (5315011932252) | 5305-00-282-9451 (5305002829451) | 5340-01-151-8391 (5340011518391) | 5315-01-482-3431 (5315014823431) | |
| 5360-01-616-7828 (5360016167828) | 5340-00-680-3497 (5340006803497) | 5330-01-492-4379 (5330014924379) | 5310-01-705-5442 (5310017055442) | |
| 5365-01-648-1970 (5365016481970) | 5340-01-524-2523 (5340015242523) | 5340-01-265-3907 (5340012653907) | 5306-01-333-8059 (5306013338059) | |
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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